M A S T E R M I N I M U M E Q U I P M E N T L I S T
BOMBARDIER BUSINESS JET
CANADAIR CHALLENGER
CL 600/601/601-3A/601-3R/604/605/650
TRANSMITTAL LETTER
This letter presents Revision 1 of the Challenger 600-Series EASA Master Minimum Equipment List (CSP 600-158)for all variants, dated 19 February 2016.
The associated Challenger 600 Dispatch Deviation Guide (DDG), containing the appropriate operational (O) andmaintenance (M) procedures, will be issued to support this MMEL. The DDG is to be issued within 30 days afterapproval.
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST
Bombardier Business Jet
CL 600/601/601-3A/601-3R/604/605/650
(CSP 600-158)
First issued: 25 Nov 2015Revision 1: 19 Feb 2016
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
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TABLE OF CONTENTS
Subject Chapter/Page
TRANSMITTAL LETTER PAGETITLE PAGETABLE OF CONTENTS TOC-1MANUAL APPROVAL PAGERECORD OF REVISIONS REV-1RECORD OF TEMPORARY REVISIONS TpRv-1USER COMMENTSLIST OF EFFECTIVE PAGES LEP-1HIGHLIGHTS OF CHANGE HOC-1DEFINITIONS DEF-1ABBREVIATIONS and ACRONYMS ABB-1PREAMBLE PRE-1EQUIPMENT LIST
Air Conditioning 21-1
Auto Flight 22-1
Communications 23-1
Electrical Power 24-1
Equipment/Furnishings 25-1
Fire Protection 26-1Flight Controls 27-1
Fuel 28-1
Hydraulic Power 29-1
Ice and Rain Protection 30-1
Indicating/Recording Systems 31-1
Landing Gear 32-1
Lights 33-1
Navigation 34-1Oxygen 35-1
Pneumatics 36-1
(Cont’d)
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TABLE OF CONTENTS (Cont’d)
Subject Chapter/Page
EQUIPMENT LIST (Cont’d)
Water /Waste 38-1
Central Maintenance System 45-1
Information Systems 46-1
APU 49-1
Doors 52-1
Windows 56-1
Power Plant 71-1
Engine Fuel and Control 73-1
Ignition 74-1
Engine Control 76-1
Engine Indicating 77-1
Exhaust 78-1
Oil 79-1
EUROPEAN AVIATION SAFETY AGENCY
MASTER MINIMUM EQUIPMENT LIST
CANADAIR CHALLENGER
CL-600 (CL-600-1A11)CL-601 (CL-600-2A12)CL-601-3A (CL600-2B16)CL-601-3R (CL600-2B16)CL-604 (CL600-2B16)CL-605 (CL600-2B16)CL-650 (CL600-2B16)
CL 600\601\601-3A\601-3R\604\605\650
Manual Approval
This Master Minimum Equipment List (MMEL) is issued by the EUROPEAN AVIATION SAFETY AGENCY at thebelow revision and is recommended for approval as the basis for the preparation and approval of individual
operator’s Minimum Equipment List (MEL) for aircraft of the above listed Types, as certified by and operated underthe jurisdiction of members States National Authorities.
Operational Suitability Data (OSD)Approval number:
10056329Date: 19 February 2016
Revision 1
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RECORD OF REVISIONS
Retain this index in the front of the manual. When Revisions are received and inserted, enter the relevantinformation in the columns below.
Revision # Pages Affected By
Original All Bombardier Aerospace
Revision 1 All Bombardier Aerospace
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RECORD OF TEMPORARY REVISIONS
Retain this index in the front of the manual. When Temporary Revisions are issued or cancelled, enter the date youinsert each revision in your manual.
TempRev #
PagesAffected
EASA approval Description of Revision Date IncorporatedSignature
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CL 600\601\601-3A\601-3R\604\605\650 BOMBARDIER Business Jet
MMEL USER COMMENTS
ON ERRORS, OMISSIONS, PROCEDURES (IF APPLICABLE), ETC.
FAX to: (514) 855-8751Bombardier AerospaceRM&S - Reliability, Maintainability and SafetyDepartment 643
OR
Email to: [email protected]
OR
Mail to: address on back of this page
From: Telephone No.:
Company: Email address:
Date:
The MMEL requires the following correction or clarification:
ATA Chapter/MMEL Item No.:
Page No.: Page Date:
OUR RESPONSE
Thank you for your comment;
F We will issue Temporary Revision No.____F We will include in Revision ___ scheduled for:
Comment:
Date:
--------------------------------------------------------------------------------------------------------------------------------------------------------
Bombardier AerospaceP.O.Box 6087, Station Centre-villeMontreal, QuebecH3C 3G9
Attention: Martin ZeppetelliRM&S - Reliability, Maintainability and SafetyDept. 643
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EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
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LIST OF EFFECTIVE PAGES
CHAPTERPAGE DATE
CHAPTERPAGE DATE
Title Page Feb 19/2016
Table of ContentsTOC-1 Feb 19/2016TOC-2 Feb 19/2016
Manual Approval Page
Bombardier’s Address Page
Record of RevisionsREV-1 Feb 19/2016REV-2 Feb 19/2016
Record of Temporary RevisionsTpRv-1 Feb 19/2016TpRv-2 Feb 19/2016
User CommentsPage Feb 19/2016
List of Effective PagesLEP-1 Feb 19/2016LEP-2 Feb 19/2016LEP-3 Feb 19/2016LEP-4 Feb 19/2016
Highlights Of ChangesHOC-1 Feb 19/2016HOC-2 Feb 19/2016
DefinitionsDEF-1 Feb 19/2016DEF-2 Feb 19/2016DEF-3 Feb 19/2016DEF-4 Feb 19/2016DEF-5 Feb 19/2016DEF-6 Feb 19/2016
Abbreviations and AcronymsABB-1 Feb 19/2016ABB-2 Feb 19/2016ABB-3 Feb 19/2016ABB-4 Feb 19/2016ABB-5 Feb 19/2016ABB-6 Feb 19/2016ABB-7 Feb 19/2016ABB-8 Feb 19/2016ABB-9 Feb 19/2016ABB-10 Feb 19/2016ABB-11 Feb 19/2016ABB-12 Feb 19/2016
PreamblePRE-1 Feb 19/2016PRE-2 Feb 19/2016
21 Air Conditioning21-1 Feb 19/201621-2 Feb 19/201621-3 Feb 19/201621-4 Feb 19/201621-5 Feb 19/201621-6 Feb 19/201621-7 Feb 19/201621-8 Feb 19/2016
22 Auto Flight22-1 Feb 19/201622-2 Feb 19/201622-3 Feb 19/201622-4 Feb 19/201622-5 Feb 19/201622-6 Feb 19/201622-7 Feb 19/201622-8 Feb 19/2016
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LIST OF EFFECTIVE PAGES (Cont’d)
CHAPTERPAGE DATE
CHAPTERPAGE DATE
23 Communications23-1 Feb 19/201623-2 Feb 19/201623-3 Feb 19/201623-4 Feb 19/201623-5 Feb 19/201623-6 Feb 19/2016
24 Electrical Power24-1 Feb 19/201624-2 Feb 19/201624-3 Feb 19/201624-4 Feb 19/201624-5 Feb 19/201624-6 Feb 19/201624-7 Feb 19/201624-8 Feb 19/2016
25 Equipment/Furnishings25-1 Feb 19/201625-2 Feb 19/201625-3 Feb 19/201625-4 Feb 19/201625-5 Feb 19/201625-6 Feb 19/201625-7 Feb 19/201625-8 Feb 19/201625-9 Feb 19/201625-10 Feb 19/2016
26 Fire Protection26-1 Feb 19/201626-2 Feb 19/201626-3 Feb 19/201626-4 Feb 19/2016
27 Flight Controls27-1 Feb 19/201627-2 Feb 19/201627-3 Feb 19/201627-4 Feb 19/2016
28 Fuel28-1 Feb 19/201628-2 Feb 19/201628-3 Feb 19/201628-4 Feb 19/201628-5 Feb 19/201628-6 Feb 19/201628-7 Feb 19/201628-8 Feb 19/201628-9 Feb 19/201628-10 Feb 19/2016
29 Hydraulic Power29-1 Feb 19/201629-2 Feb 19/201629-3 Feb 19/201629-4 Feb 19/2016
30 Ice & Rain Protection30-1 Feb 19/201630-2 Feb 19/201630-3 Feb 19/201630-4 Feb 19/201630-5 Feb 19/201630-6 Feb 19/201630-7 Feb 19/201630-8 Feb 19/201630-9 Feb 19/201630-10 Feb 19/2016
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LIST OF EFFECTIVE PAGES (Cont’d)
CHAPTERPAGE DATE
CHAPTERPAGE DATE
31 Instruments31-1 Feb 19/201631-2 Feb 19/201631-3 Feb 19/201631-4 Feb 19/201631-5 Feb 19/201631-6 Feb 19/201631-7 Feb 19/201631-8 Feb 19/201631-9 Feb 19/201631-10 Feb 19/2016
32 Landing Gear32-1 Feb 19/201632-2 Feb 19/201632-3 Feb 19/201632-4 Feb 19/2016
33 Lights33-1 Feb 19/201633-2 Feb 19/201633-3 Feb 19/201633-4 Feb 19/201633-5 Feb 19/201633-6 Feb 19/201633-7 Feb 19/201633-8 Feb 19/201633-9 Feb 19/201633-10 Feb 19/201633-11 Feb 19/201633-12 Feb 19/2016
34 Navigation34-1 Feb 19/201634-2 Feb 19/201634-3 Feb 19/201634-4 Feb 19/201634-5 Feb 19/201634-6 Feb 19/201634-7 Feb 19/201634-8 Feb 19/201634-9 Feb 19/201634-10 Feb 19/201634-11 Feb 19/201634-12 Feb 19/201634-13 Feb 19/201634-14 Feb 19/201634-15 Feb 19/201634-16 Feb 19/201634-17 Feb 19/201634-18 Feb 19/201634-19 Feb 19/201634-20 Feb 19/201634-21 Feb 19/201634-22 Feb 19/201634-23 Feb 19/201634-24 Feb 19/2016
35 Oxygen35-1 Feb 19/201635-2 Feb 19/201635-3 Feb 19/201635-4 Feb 19/2016
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LIST OF EFFECTIVE PAGES (Cont’d)
CHAPTERPAGE DATE
CHAPTERPAGE DATE
36 Pneumatics36-1 Feb 19/201636-2 Feb 19/2016
38 Water / Waste38-1 Feb 19/201638-2 Feb 19/2016
45 Central Maintenance Systems45-1 Feb 19/201645-2 Feb 19/2016
46 Information Systems46-1 Feb 19/201646-2 Feb 19/2016
49 Auxiliary Power Unit49-1 Feb 19/201649-2 Feb 19/2016
52 Doors52-1 Feb 19/201652-2 Feb 19/201652-3 Feb 19/201652-4 Feb 19/2016
56 Windows56-1 Feb 19/201656-2 Feb 19/2016
71 Powerplant71-1 Feb 19/201671-2 Feb 19/2016
73 Engine Fuel and Control73-1 Feb 19/201673-2 Feb 19/2016
74 Ignition74-1 Feb 19/201674-2 Feb 19/2016
76 Engine Control76-1 Feb 19/201676-2 Feb 19/2016
77 Engine Indicating77-1 Feb 19/201677-2 Feb 19/201677-3 Feb 19/201677-4 Feb 19/201677-5 Feb 19/201677-6 Feb 19/2016
78 Exhaust78-1 Feb 19/201678-2 Feb 19/2016
79 Oil79-1 Feb 19/201679-2 Feb 19/2016
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HIGHLIGHTS OF CHANGE
Revision 1 incorporates changes to each page header to include the marketing designation ‘650’ under AIRCRAFT
In addition, Revision 1 incorporates relief for Challenger 650 Avionics Block Upgrade for ATA items 23-11-4,34-34-1, 34-42-2, 34-43-1, 34-54-1, 34-54-2, 34-61-1, 34-61-2, 34-61-4, and 34-61-5. The ‘650’ marketingdesignation was added to all relief items that are applicable to the ‘605’ marketing designator with no technicalchange.
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DEFINITIONS
1. “ Affected ” refers to the subject item of equipment (component, system or function) listed in the Item column.
2. " Airplane Flight Manual (AFM) " is the document required for type certification and approved by the Agency.The approved AFM for the specific aircraft is listed on the applicable Type Certificate Data Sheet.
3. " Alphabetical Symbol " indicates a proviso (condition or limitation) that must be complied with for operationwith the listed item inoperative.
4. " Alternate procedures are established and used " or similar statement, means that alternate procedures (ifapplicable), to the affected process, must be drawn up by the operator as part of the MEL approval process,so that they have been established before the MEL document has been approved. Such alternate proceduresare normally included in the associated operations (O) procedure.
5. " Any in excess of those required by regulations " means that the listed item is required by applicablelegislation (e.g. Part OPS, Single European Sky legislation or the applicable airspace requirements) must beoperative and only excess items may be inoperative. When the item is not required, it may be inoperative forthe time specified by its rectification interval category. Whenever this condition is used in the MMEL, theapplicable regulations for the intended flight routes and the resulting dispatch restrictions need to be clarifiedat the operator’s MEL level.
6. " As required by (operational) regulations " means that the listed item of equipment is subject to certainprovisions (restrictive or permissive) expressed in the applicable legislation (e.g. regulation Air Operations,Single European Sky legislation or the applicable airspace requirements). When the equipment is not required,it may be inoperative for the time specified by its rectification interval category.
7. " Calendar Day " means a 24-hour period from midnight to midnight based on either UTC or local time, asselected by the operator. All calendar days are considered to run consecutively.
8. " Combustible Material " means the material which is capable of catching fire and burning. In particular: if aMEL item prohibits loading of combustible (or flammable or inflammable) material, no material may be loadedexcept the following:
1) Cargo handling equipment (unloaded, empty or with ballast);
2) Fly away kits (excluding e.g. cans of hydraulic fluid, cleaning solvents, batteries, capacitors, chemicalgenerators, etc.);
Note: If serviceable tires are included, they should only be inflated to a minimum pressure thatpreserves their serviceability; and
3) Inflight service material (return catering — only closed catering trolleys/boxes, no newspapers, noalcohol or duty free goods).
9. " Commencement of flight " is the point when an aircraft begins to move under its own power for thepurpose of preparing for take-off.
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DEFINITIONS(Cont’d)
10. " Considered Inoperative " as used in the dispatch conditions, means that item must be treated for dispatch,taxiing and flight purposes as though it were inoperative. The item shall not be used or operated until theoriginal deferred item is repaired. Additional actions include: documenting the item on the dispatch release (ifapplicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, includingany (M) and (O) procedures and observing the rectification interval.
11. " Crew Member " means a person assigned to duty in an aircraft during flight time.
12. " Dash (-) " in the Number Installed Column (respectively Number Required for Dispatch Column) indicates avariable number (quantity) of the item installed (respectively item required) or not applicable.
Note: Where the MMEL shows a variable number installed, the MEL should reflect the actual numberinstalled, as far as practical.
13. " Daylight " means the period between the beginning of morning civil twilight and the end of evening civiltwilight relevant to the local aeronautical airspace; or such other period, as may be prescribed by theappropriate authority.
14. " Day of discovery " means the calendar day that a malfunction was recorded in the aircraft maintenancerecord/log book.
15. " Deactivated " and " Secured " means that the specified component must be put into an acceptablecondition for safe flight. An acceptable method of securing or deactivating will be established by the operatorfor inclusion to their MEL.
16. " Deleted " in the remarks column after a sequence item indicates that the item was previously listed but isnow required to be operative if installed in the aircraft.
17. " Engine Indicating Crew Alerting System (EICAS) " that provides electronic messages refers to a systemcapable of providing different priority levels of system information messages (e.g., WARNING, CAUTION,ADVISORY and STATUS). Any airplane discrepancy message that affects dispatchability will be at theWARNING, CAUTION or STATUS level.
18. " Extended Overwater Operations " means operations over water at a horizontal distance of more than 50nautical miles from the nearest shoreline.
19. " Flight " for the purposes of this MMEL, means the period of time between the moment when an aircraftbegins to move under its own power, for the purpose of preparing for take-off, until the moment the aircraftcomes to a complete stop on its parking area, after the first landing.
20. " Flight Crew Member " means a crew member assigned to act as a pilot or flight engineer of an aircraftduring flight time.
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DEFINITIONS(Cont’d)
21. " Flight Day " a 24-hour period from midnight to midnight based on either UTC or local time, as selected bythe operator, during which at least one flight is initiated for the affected aircraft.
22. " Icing Conditions " means an atmospheric environment that may cause ice to form on the aircraft or in theengine(s) as defined in the AFM/RFM.
23. " If installed " means that the equipment is either optional or is not required to be installed on all aircraftcovered by the MMEL.
24. " Indication " is where a number if parameters are reported on a line replaceable unit. To allow relief forindividual parameters being inoperative rather than the entire unit, the word indication is used as opposed toindicator.
25. " Indicator " is a line replaceable unit. The parameters displayed can be analogue or digital. To allow relieffor the line replaceable unit rather than the individual parameters we use the word indicator
26. " Inoperative " means that the item does not accomplish its intended purpose or is not consistentlyfunctioning within its approved operating limits or tolerances.
27. " Intended flight route " corresponds to any point on the route including diversions to reach alternateaerodromes required to be selected by the operational rules.
28. " Is not used " in the provisions, remarks or exceptions for an MMEL item may specify that another itemrelieved in the MMEL ‘is not used’. In such cases, crew members should not activate, actuate, or otherwiseutilize that item under normal operations. It is not necessary for the operators to accomplish the (M)procedures associated with the item. However, operations-related provisions, (O) procedures must becomplied with. An additional placard must be affixed, to the extent practical, adjacent to the control or indicatorfor the item that is not used to inform crew members that an item is not to be used under normal operations.
29. " Item " means component, instrument, equipment, system or function.
30. "(M)" indicates a requirement for a specific maintenance procedure which must be accomplished prior tooperation with the listed item inoperative. Normally these procedures are accomplished by maintenancepersonnel, however, other personnel may be qualified and authorized to perform certain functions. Thesatisfactory accomplishment of all maintenance procedures, regardless of who performs them, is theresponsibility of the operator. Appropriate procedures are required to be published as part of the Operator’sManual or MEL.
31. " Master Minimum Equipment List (MMEL) " means a document approved by the Agency that establishesthe aircraft equipment allowed to be inoperative under conditions specified therein for a specific type ofaircraft."
32. Maximum distance from an adequate aerodrome for two-engine aeroplanes " as defined in SPA.ETOPSand CAT.OP.AH.140.
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DEFINITIONS(Cont’d)
33. " Minimum Equipment List " means a document established as specified under 8.a.3. of Annex IV toRegulation (EC) No 216/2008 and approved by the competent authority, in accordance with ORO.MLR.105,that authorises an operator to dispatch an aircraft with aircraft equipment inoperative as per CAT.IDE.A/H.105or NCC.IDE.A/H.105 under the conditions specified therein.
34. " NOTE " provide additional information for flight crew or maintenance consideration. Notes are used toidentify applicable material which is intended to assist with compliance, but do not relieve the operator of theresponsibility for compliance with all applicable requirements. Notes are not a part of the dispatch conditions.
35. " Number Installed " is the number (quantity) of items normally installed in the aircraft. This numberrepresents the aircraft configuration considered in developing this MMEL. Should the number be a variable(e.g. passenger cabin items), or not applicable, a number is not required; a ‘-’ is then inserted.
Note: Where the MMEL shows a variable number installed, the MEL should reflect the actual number installed,as far as practical.
36. " Number required for dispatch " is the minimum number (quantity) of items required for operation providedthe conditions specified are met. Should the number be a variable (e.g. passenger cabin items) or notapplicable, a number is not required; a ‘-’ is then inserted.
Note: Where the MMEL shows a variable number required for dispatch, the MEL should reflect the actualnumber required for dispatch, as far as practical, or an alternate means of configuration controlapproved by the competent authority.
37. " (O) " indicates a requirement for a specific operational procedure which must be accomplished in planningfor and/or operating with the listed item inoperative. Unless otherwise specified in the Remarks or Exceptionsor the procedure itself, the operations procedure must be performed on each flight made with the inoperativesystem or equipment. Normally these procedures are accomplished by the flight crew; however, otherpersonnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of allprocedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures arerequired to be published as a part of the operator’s manual or MEL.
Note: The (M) and (O) symbols are required in the operator’s MEL.
38. " Operating minima " means the set of requirements associated to operations requiring a specific approval(refer to Part-SPA).
39. " Placarding " Each inoperative item must be placarded, as applicable, to inform and remind the crewmembers and maintenance personnel of the item’s condition.
Note: To the extent practical, placards should be located adjacent to the control or indicator for the itemaffected; however, unless otherwise specified, placard wording and location will be determined bythe operator.
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DEFINITIONS(Cont’d)
40. “Rectification Intervals” Inoperative items or components, deferred in accordance with the MEL, must berectified at or prior to the rectification intervals established by the following letter designators:
Category ANo standard interval is specified. However, items in this category shall be rectified in accordance with theconditions stated in the MMEL.
(i) Where a time period is specified in calendar days or flight days, the interval excludes the day ofdiscovery.
(ii) Where a time period is specified other than in calendar days or flight days, it shall start at the pointwhen the defect is deferred in accordance with the operator’s approved MEL.
Category BItems in this category shall be rectified within three (3) calendar days, excluding the day of discovery.
Category CItems in this category shall be rectified within ten (10) calendar days, excluding the day of discovery.
Category DItems in this category shall be rectified within one hundred and twenty (120) calendar days, excluding the dayof discovery.
41. “ Reduced Vertical Separation Minimum (RVSM) airspace ” means any airspace or route where aircraftare separated by 1000 feet vertically between FL 290 and FL 410. RVSM Operations means operationsconducted in RVSM airspace.
42. " Remarks or Exceptions " include statements either prohibiting or allowing operation with a specific numberof items inoperative, provisos (conditions and limitations), notes, (M) and/or (O) symbols, as appropriate forsuch operation.
43. " Required Cabin Crew Seat " is a seat in the aircraft cabin which meets the following conditions:
a) Where the certification of the cabin requires this seat to be occupied by a qualified cabin crewmember as specified in the Operations Manual;
b) This seat is a part of the station to which a qualified cabin crew member is assigned for the flight; and
c) The qualified cabin crew member assigned to the station is a member of the minimum cabin crewdesignated for the flight
44. " System " means the group of directly related components which together perform a specified function; forexample, the N2 Tachometer System would include the N2 indicator, tachometer generator and associatedcircuitry.
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DEFINITIONS(Cont’d)
45. " System & Sequence Numbers " are based on Air Transport Association (ATA) Specification No. 100 anditems are numbered sequentially.
46. " Triple Asterisks (***) " means that the item is either optional or is not required to be installed on all aircraftcovered by the MMEL. This item may be included on the operator's MEL after the approving office hasdetermined that the item has been installed on one or more of the operator's aircraft. The symbol, however,shall not be carried forward into the operator's MEL. It should be noted that neither this policy nor the use ofthis symbol provides authority to install or remove an item from an aircraft. The "***" symbol may beconsidered equivalent to the term "if installed"
47. " Verified operative " means that a visual inspection or test is required to confirm unit or system operation orcondition, as applicable.
48. " Vertical Change Bar " A vertical bar in the margin indicates a change, addition or deletion in the adjacenttext for the current revision of that page only. The change bar is dropped at the next revision of that page.
49. " Visible Moisture " means an atmospheric environment containing water in any form that can be seen innatural or artificial light; for example, clouds, fog, mist, rain, sleet, hail, or snow.
50. " Visual Meteorological Conditions (VMC) " means the atmospheric environment is such that would allow aflight to proceed under the visual flight rules applicable to the flight. This does not preclude operating underInstrument Flight Rules.
51. " Visual Flight Rules (VFR) " is as defined by the Agency. This precludes a pilot from filing an InstrumentFlight Rules (IFR) flight plan.
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ABBREVIATIONS and ACRONYMS
The following abbreviations and acronyms may be used on flight compartment displays, radiotuning units and the flight management system or may be found in this manual. Someabbreviations may appear in upper or lower case letters. Abbreviations which have limitedusage are explained in the chapters where they are used.
A
A/C Air ConditioningA/G Air/GroundA/ICE Anti-iceA/P AutopilotA/S AirspeedA/SKID Anti-skidABS AbsoluteAC Alternating CurrentACARS ARINC Communications
Addressing andreporting System
ACCEL Acceleration,accelerate(d),accelerometers
ACM Air Cycle MachineACMP Alternating Current
Motor Pump/ ElectricHydraulic Pump
ACT ActiveACU Air Conditioning UnitADC Air Data ComputerADDR AddressADF Automatic Direction
FinderADG Air Driven GeneratorADI Attitude Director
IndicatorADS Air Data SystemAFCS Automatic Flight
Control SystemAFIS Airborne Flight
Information SystemAFM Airplane Flight
ManualAFT Afterward
AGL Above Ground LevelAHC Attitude Heading
ComputerAHRS Attitude Heading
Reference SystemAIL AileronALIGN Aligning, alignmentALPHA alphaALT Altitude, AltimeterALT Altitude Hold
(PFD/FD)ALT CAP Altitude Capture
(PFD/FD)ALT HOLD Altitude HoldALTN AlternateALTS Selected Altitude
Arm/Abort (PFD/FD)AM Amplitude ModulationAMB AmbientAMP AmperesANNUN AnnunciatorANT AntennaAOA Angle of AttackAP AutopilotAPC Auxiliary Power
ControlAPP ApproachAPPROX ApproximatelyAPR Automatic Performance
ReserveAPU Auxiliary Power Unit
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AIRCRAFT REVISION No: 1 Page
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ARINC Aeronautical RadioIncorporated
ARP Air Data ReferencePanel
ASYM AsymmetricalATA Air Transport
AssociationATC Air Traffic ControlATT AttitudeATTD Attitude
ATTND AttendantAUTO AutomaticAUTO BAL Automatic BalanceAUTO XFER Automatic TransferAUX AuxiliaryAV AvionicsAVAIL AvailableAZ Azimuth
B
B/AIR Bleed AirB/C Back CourseB/CRS Back CourseB/LEAK Bleed LeakBAG DR Baggage DoorBARO BarometricBAT BatteryBATT BatteryBDI Bearing Distance
IndicatorBFO Beat Frequency
OscillatorBITE Built-In-Test
Equipment
BK BrakeBLD BleedBOOM Headset microphoneBRG BearingBRKR(s) Breaker(s)BRT BrightBTL BottleBTMS Brake Temperature
Monitoring SystemBTMU Brake Temperature
Monitoring UnitBYPS Bypass
C
C Center, Caution,Cabin
CAL CalibrateCAP CaptureCAPT CaptainCAS Calibrated Air SpeedCAT CategoryCAT II Category IICB, C/B Circuit BreakerCBP Circuit Breaker PanelCCW Counter Clockwise
CDL ConfigurationDeviation List
CDP Compressor DischargePressure
CDU Control Display UnitCFM Cubic Feet Per MinuteCG Center of GravityCH Chapter, ChannelCHAN ChannelCHGR Charger
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AIRCRAFT REVISION No: 1 Page
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CHR ChronographCHRT ChartCK CheckCKPT CockpitCKT CircuitCLB ClimbCLK Clockcm CentimetersCMD CommandCMPS CompassCMPTR ComputerCO2 Carbon DioxideCOM CommunicationCOMM CommunicationCOMP Compressor,
ComparatorCOMPT CompartmentCOND Condition, Continued
CONFIG ConfigurationCONN ConnectionCONT Control, Continuous,
Contactor, ControllerCOOL CoolingCORR CorrectionCPAM Cabin Pressure
Acquisition ModuleCPLT CopilotCRS CourseCRT Cathode Ray TubeCRZ CruiseCSD Constant Speed DriveCTR CenterCVR Cockpit Voice
RecorderCW ClockwiseCYL Cylinder
D
DA Drift AngleDBU Data Base UnitDC Direct CurrentDCP Display Control PanelDCU Data Concentrator
UnitDECEL Decelerate(d)DECR DecreaseDEFL DefuelDEG DegreeDEPR DepressurizeDEPT DepartureDEST DestinationDET DetectorDEV DeviationDFDAU Digital Flight Data
Acquisition Unit
DFDR Digital Flight DataRecorder
DG Directional GyroDH Decision HeightDIFF DifferentialDIM DimmingDIR DirectDIS Distance (to way
point), DisconnectDISC DisconnectDISCH DischargeDISP Dispatch, DisplayDIST DistanceDME Distance Measuring
EquipmentDN DownDR DoorDUCT MON Duct Monitor
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AIRCRAFT REVISION No: 1 Page
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E
EADI Electronic AttitudeDirection Indicator
EAS Equivalent AirspeedECP EICAS Control PanelECS Environmental Control
SystemECU Electronic Control
UnitED EICAS DisplayEDP Engine Driven Pump/
Engine PrimaryHydraulic Pump
EFB Electronic Flight BagEFIS Electronic Flight
Instrument SystemEGT Exhaust Gas
TemperatureEICAS Engine Indication and
Crew Alerting SystemEHSI Electronic Horizontal
Situation IndicatorEL ElevationELEC Electrical
ELEV Elevator, ElevationELT Emergency Locator
TransmitterEMER(G) EmergencyEMI Electro-Magnetic
InterferenceENG EngineEPC External Power
ContactorEQUIP EquipmentERP Eye Reference
Position DatumESS EssentialET Elapsed TimeETA Estimated Time of
ArrivalETE Estimated Time
EnrouteEVAC EvacuationEVS Enhanced Vision
SystemEXH ExhaustEXTIN Extinguish(ed)
F
F/CTL Flight ControlsFAIL FailureFCC Flight Control
ComputerFCU Fuel Control UnitFD, F/D Flight DirectorFDAU Flight Data
Acquisition UnitFDR Flight Data Recorder
(Digital)FECU Flaps Electronic
Control UnitFEED FeederFF, F/F Fuel FlowFIRE BTL Fire Bottle
FIREX Fire ExtinguisherFL CH Flight Level ChangeFLD FieldFLT FlightFLT DIR Flight DirectorFLUOR FluorescentFM Fan MarkerFMS Flight Management
SystemFPM Feet Per MinuteFREQ Frequencyft Feet, FootFW Fire WallFWD Forward
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 ABB-5
G
G (+/-) Receiver GainG/S Glide slopeGA Go-aroundGAL GallonGALY GalleyGCS Ground Clutter
SuppressionGCU Generator Control
UnitGE General ElectricGEN Generator
GLD Ground Lift DumpingGMT Greenwich Mean TimeGND GroundGPM Gallons Per MinuteGPWS Ground Proximity
Warning SystemGR GearGRAV GravityGS Ground SpeedGUIDE GuidanceGW Gross Weight
H
HDG HeadingHDG HOLD Heading HoldHDG SEL Heading SelectHEAT HeaterHF High Frequency
(3 - 30 mHz)Hg MercuryHGS Head-up Guidance
SystemHI HighHIRF High Intensity
Radiated FieldsHLDR HolderHOR, HORIZ Horizontal
HOT High Oil TemperatureHP High PressureHPA Hecto PascalsHSI Horizontal Situation
IndicatorHSTA Horizontal Stabilizer
TrimHSTCU Horizontal Stabilizer
Trim Control UnitHTR HeaterHUD Heads-up DisplayHYD HydraulicHz Hertz
I
IB,I/B,INBD InboardI/C Intercom, Inspection
CheckIAPS Integrated Avionics
Processor SystemIAS Indicated Air Speed ICAO
International CivilAviation Organization
ICS Idle Corrected Speed
ID IdentificationIDENT IdentificationIDG Integrated Drive
GeneratorIFIS Integrated Flight
Information SystemIFR Instrument Flight
Rules
IGN IgnitionILS Instrument Landing
System
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
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IM ILS Inner MarkerIMC Instrument
MeteorologicalConditions
IMP. Imperialin. Inch, Inchesin. Hg Inches of MercuryINCR IncreaseIND Indication, IndicatorINFLT In FlightINHIB InhibitINOP InoperativeINPH InterphoneINSP InspectionINST(S) Instrument(s)INST, INSTR Instrument
INT Internal, Integral,Intersection
INTEG IntegralIRS Inertial Reference
SystemIRU Inertial Reference
UnitISA International
Standard AtmosphereISDU Inertial System
Display UnitISO International
Standard OrganizationISOL Isolation, IsolatedITT Inter Turbine
Temperature
K
K, KT, KTS Knotskg Kilogram(s)kHz KiloHertz
KIAS Knots IndicatedAirspeed
kW(s) KiloWatt(s)
L
L Left, LandingL/R Left/RightL/T Landing/TaxiLAV Lavatorylb Pound(s)LCN Load Classification
Number
LCV Load Control ValveLDG LandingLDG GR Landing GearLDU Lamp Driver UnitLE Leading EdgeLED Light Emitting Diode,
Leading Edge DeviceLDS Lightning Detection
SystemLG Landing GearLGC Landing Gear
ControllerLGW Landing Gross WeightLH Left HandLIM LimitLK LeakLN Left NoseLNAV Lateral NavigationLOC ILS LocalizerLOGO Logo Graphic
LOM, MM Compass Locator atOuter Marker
LOP Low Oil Pressure
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 ABB-7
LP Low PressureLPM Liter Per MinuteLR Left RearLRC Long Range CruiseLRU Line Replaceable Unit
LSB Lower Side BandLT(s) Light(s)LW Left WingLWD Left Wing DownLWR Lower
M
M Mach Numberm MeterMAA Maximum Authorized
IFR AltitudeMAC Mean Aerodynamic
ChordMAG MagneticMAINT MaintenanceMALF MalfunctionMAN ManualMAP Ground Map (WXR)MASI Mach Air Speed
IndicatorMAX MaximumMAZ MLS AzimuthMB MillibarsMCA Minimum Crossing
AltitudeMCT Maximum Continuous
ThrustMDA Minimum Descent
AltitudeMEA Minimum Enroute IFR
AltitudeMECH MechanicMED Medium
MEL Minimum EquipmentList
MFD Multifunction DisplayMGP MLS GlideslopeMHz MegaHertzMI MilesMIC MicrophoneMID AFT Middle AfterwardMID FWD Middle ForwardMILS .001 of an inchMIN MinimumMISC MiscellaneousMKR MarkerMLG Main Landing GearMLI Magnetic Level
IndicatorMLU Midlife Update
MLW Maximum LandingWeight
MM ILS Middle MarkerMMEL Master Minimum
Equipment ListMMO Maximum Operating
Speed in Mach Number
MOCA Minimum ObstructionClearance Altitude
MOD ModuleMON MonitorMPH Miles Per HourMRA Minimum Reception
AltitudeMSG MessageMSL Mean Sea Level
MTBF Mean Time BeforeFailure
MTG Miles to GoMTOW Maximum Takeoff
WeightMTW Maximum Taxi WeightMZFW Maximum Zero Fuel
Weight
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AIRCRAFT REVISION No: 1 Page
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Misc
% Percent& and
°C Degrees Centigrade°F Degrees Fahrenheit
N
N/A Not applicableN1 Low Pressure RotorN2 High Pressure RotorNAV NavigationND Nose Down, Navigation
DisplayNDB (ADF) Nondirectional Beacon
(Automatic DirectionFinder)
NEG NegativeNEUT Neutral
NL Nose LeftNLG Nose Landing GearNM Nautical Mile(s)No. NumberNOPT No Procedure Turn
RequiredNORM NormalNOSE NosewheelNR Nose RightNU Nose Up
O
OAT Outside AirTemperature
OB/OUTBD OutboardOBS ObserverOEI One Engine
InoperativeOEW Operating Empty
WeightOH, OVHD Overhead
OK OkayOM ILS Outer MarkerOVBD OverboardOVHT, OH OverheatOVLD OverloadOVSP OverspeedOVSPD OverspeedOVTEMP Over TemperatureOXY, O2 Oxygen
P
P#6 Panel 6P/S Pitot/StaticPA Passenger AddressPASS PassengerPBE Portable Breathing
Equipment (SmokeHood)
PCU Power Control UnitPDU Power Drive Unit
PF Pilot FlyingPFD Primary Flight
DisplayPLA Power Lever AnglePLT(s) Pilot(s)PNF Pilot Not FlyingPNLS(s) Panel(s)
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 ABB-9
PO Outside Air PressurePOS PositionPPH Pounds Per HourPRESS Pressure,
PressurizationPRI PrimaryPRIM PrimaryPROC ProcedurePROT ProtectionPROX ProximityPSEU Proximity Sensor
Electronics Unit
PSI Pounds Per SquareInch
PSIG Pounds Per SquareInch Gauge
PSS Proximity SensorSystem
PSU Passenger ServiceUnit
PT2 Engine Inlet PressurePTCT ProtectPTT Push To TalkPWR Power
Q
QAR Quick Access RecorderQEC Quick Engine ChangeQFE Local Station
Pressure
QNH Altimeter SettingQTY Quantity
R
R RightRA Radio Altitude
Resolution AdvisoryRAI Registro Aeronautico
Italiano (Italy)RAT Ram Air TurineRCCB Remote Controlled
Circuit BreakerRCDR RecorderRCVR ReceiverRDR RadarREC Receiver, RecorderRECOG RecognitionREF(s) Reference(s)REFL RefuelREV ReverseRH Right HandRIPS Recorder Independent
Power Supply
RMI Radio MagneticIndicator
RMU Radio Management Unit
ROT RotationRPM Revolutions Per
MinuteRT, R/T Receiver-TransmitterRTE RouteRTE DATA Route DataRTO Rejected TakeoffRTU Radio Tuning UnitRUD RudderRVR Runway Visual RangeRVSM Reduced Vertical
Separation MinimumRVSR ReverserRW Right WingRWD Right Wing DownRWY Runway
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AIRCRAFT REVISION No: 1 Page
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S
S StatusSAT Static Air
TemperatureSCAT Speed Command Attitude
ThrustSCAV ScavengeSDS Status Display SystemSEC Second, SecondarySECS Spoiler Electronic
Control SystemSECU Spoiler Electronic
Control UnitSEL Select, SelectorSEL CAL Selective CallSENS Sensitivity, SensorSERV, SVCE ServiceSMKG Smoking
SOV Shutoff ValveSP, SPD SpeedSPKR SpeakerSPLR(s) Spoiler(s)SQL SquelchSSB Single Side BandSTA StationSTAB StabilizerSTAT StatusSTBY StandbySTEER SteeringSUPPL SupplySW(s) SwitchesSYN SynchronizeSYNC SynchronousSYS, SYST System
T
T/C Top of ClimbT/D Top of DescentT/R Thrust ReverserTA Traffic AlertTACAN UHF Tactical Air
Navigation AidTAS True AirspeedTAT Total Air TemperatureTAWS Terrain Awareness and
Warning SystemTCAS Traffic Alert and
Collision AvoidanceSystem
TE Trailing Edge
TEMP TemperatureTGT TargetTO, T/O TakeoffTOC Top of ClimbTOD Top of DescentTOL ToleranceTRB, TURB TurbulenceTRK TrackTRM TrimTRU Transformer
RectifierUnit
TT2 Engine InletTemperature
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AIRCRAFT REVISION No: 1 Page
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U
UHF Ultra High FrequencyUNSCHD UnscheduledUSB Upper Side Band
USG United States GallonsUTIL Utility
V
V VoltVA Design Maneuvering
SpeedVB Design Speed for
Maximum GustIntensity
VC Design Cruising SpeedVD Design Diving SpeedVDF/MDF Demonstrated flight
diving speed.VF Design Flap SpeedVDF/MFC Maximum Speed for
StabilityCharacteristics
VFE Maximum Flap ExtendedSpeed
VH Maximum Speed inLevel Flight withMaximum ContinuousPower
VLE Maximum Landing GearExtended Speed
VLO Maximum Landing GearOperating Speed
VLOF Lift-off SpeedVMC Minimum Control Speed
with the CriticalEngine Inoperative
VMO/MMO Maximum OperatingLimit Speed
VMU Minimum Unstick SpeedVNE Never-exceed SpeedVNO Maximum Structural
Cruising SpeedVR Rotation Speed
VS Stalling Speed or theMinimum Steady FlightSpeed at which theAirplane isControllable
VS0 Stalling Speed or theMinimum Steady FlightSpeed in the LandingConfiguration
VS1 Stalling Speed or theMinimum Steady FlightSpeed Obtained in aSpecificConfiguration
VX Speed for Best Angleof Climb
VY Speed for Best Rateof Climb
V1 Takeoff DecisionSpeed (formerlyDenoted as CriticalEngine Failure Speed)
V2 Takeoff Safety SpeedV2 MIN Minimum Takeoff
Safety Speed
V/S Vertical SpeedVERT VerticalVFR Visual Flight RulesVG Vertical GyroVHF Very High Frequency
(30 - 300 mHz)VIB VibrationVMC Visual Meteorological
Conditions
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 ABB-12
VNAV Vertical NavigationVOL VolumeVOLT VoltageVOR VHF Omnidirectional
Range Station
VORTAC VOR and TACANCo-located
VSI Vertical SpeedIndicator
W
W WarningW/C Wind ComponentW/S Wind ShearW/W Wheel WellWARN WarningWF Runway Length Limited
WeightWGT WeightWHLS Wheels
WIND WindowWOW Weight-On-WheelsWPT(s) Waypoint(s)WRN WarningWS Second Segment
Limited WeightWSHLD WindshieldWX WeatherWXR Weather Radar
X
X Cross TransferXFER, XFR TransferXFLOW Cross FlowXMIT Transmit
XPNDR TransponderXTK Cross TrackXWC Cross Wind Component
Y
YD, Y/D Yaw Damper
Z
ZFW Zero Fuel Weight
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 PRE-1
PREAMBLE
IntroductionThe following is applicable for operators under European air operations regulations (Regulation AirOperations). Paragraph 1.c.2 of Annex I to Article 5 (essential requirements for airworthiness) of Regulation(EC) No 216/2008 (the ‘Basic Regulation’) requires that all equipment installed on an aircraft required for typecertification or by operating rules shall be operative. However, paragraph 2.a.3 of Annex IV to Article 8(essential requirements for air operations) of the Basic Regulation also allows the use of a MinimumEquipment List (MEL) where compliance with certain equipment requirements is not necessary in the interestsof safety under all operating conditions. Experience has shown that with the various levels of redundancydesigned into aircraft, operation of every system or installed items may not be necessary when the remainingoperative equipment can provide an acceptable level of safety.
Purpose and limitationsThis Master Minimum Equipment List (MMEL) is developed by the applicant and holders of (Supplemental)Type Certificate and approved by the European Aviation Safety Agency to improve aircraft use and therebyproviding more convenient and economic air transportation for the public. This MMEL includes those itemsrelated to airworthiness, air operations, airspace requirements and other items the Agency finds may beinoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does notcontain obviously required items such as wings, flaps, and rudders. In order to maintain an acceptable level ofsafety, the MMEL establishes limitations on the duration of and conditions for operation with inoperative items.
Unless specifically allowed by this MMEL, an inoperative item may not be removed from the aircraft.
UtilisationThe MMEL is the basis for the development of individual operator’s MEL which take into consideration theoperator’s particular aircraft equipment configuration and operational conditions. An operator’s MEL may differin format from the MMEL, but shall not be less restrictive than the MMEL. The individual operator’s MEL,when approved, allows operation of the aircraft with inoperative items of equipment for a certain period of timeuntil rectification can be accomplished.
The MEL must not deviate from Airworthiness Directives, or any other additional mandatory requirements. It isimportant to remember that all items related to the airworthiness and the operational regulations of the aircraftnot listed on the MMEL must be operative.
In association with this MMEL, the Type Certificate Holder has prescribed suitable conditions and limitations inthe form of recommended placarding, (M) maintenance procedures, (O) crew operating procedures and otherrestrictions, that shall be specified in the operator’s MEL procedures document (i.e.: Dispatch DeviationGuide (DDG)), to ensure that an acceptable level of safety is maintained. As these are recommended by theOEM, it is important that during any operator MEL optimization, the intent of these be maintained.
When an item is discovered to be inoperative, it is reported by making an entry in the continuing airworthinessrecord system or the operator’s technical log, as applicable. Following sufficient fault identification, the item isthen either rectified or deferred following the MEL or other approved means of compliance acceptable to thecompetent authority and the Agency prior to further operation. Rectification shall be accomplished at theearliest opportunity. MEL conditions and limitations do not relieve the operator from determining that theaircraft is in a condition for safe operation with items inoperative.
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PREAMBLE(Cont'd)
The (M) procedures identified herein, are required to be performed once prior to dispatching with MEL relief. Ifthere is a further requirement to perform the procedure more frequently, such as “prior to each flight” forexample, then this is clearly stated in the provisos. The same principal applies to the (O) procedures. Prior tooperation with any item inoperative, acceptance by the crew is required in accordance with the continuingairworthiness management procedures.
Operators shall establish a controlled and sound rectification programme including the parts, personnel,facilities, procedures and schedules to ensure timely rectification. This program should identify the actions forMaintenance discrepancy messages.
Operators should include guidance in the MEL to deal with any failures which occur between thecommencement of the flight and the start of the take-off.
When developing the MEL, compliance with the stated intent of the preamble, definitions and theconditions and limitations specified in this MMEL is required.
Multiple inoperative itemsOperators are responsible for exercising the necessary operational control to ensure that an acceptable levelof safety is maintained. The exposure to additional failures during continued operation with inoperative itemsshall also be considered. Wherever possible, account has been taken in this MMEL of multiple inoperativeitems. However, it is unlikely that all possible combinations of this nature have been accounted for. Therefore,when operating with multiple inoperative items, the inter-relationships between those items and the effect onaircraft operation and crew workload shall be considered.
Rectification interval extensionThe operator may be permitted, by its competent authority, to extend the rectification intervals of the MEL.
This MMEL has been evaluated taking into account a one-time extension of the rectification intervals ofcategory B, C, and D.
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 21-1
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
21 – AIR CONDITIONING 4. Remarks or Exceptions
20-1 Heat Exchanger Fan(Footwarmer-Demist)(600, 601, 601-3A)
C 1 0
24-1 Cockpit DisplaysCooling ExhaustFan(604, 605, 650)
C 1 0 (M) May be inoperative provided both ACUs areoperative.
NOTE : During ground operations at ambienttemperatures above 40ºC (104° F),operation of electrical/avionics equipmentmust be limited to 30 minutes unless atleast one ACU is operating and cabindoors are closed.
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30-1 EmergencyPressurizationSystem(600, 601, 601-3A)
C 1 0 (O) May be inoperative provided aircraft is operatedunpressurized.
30-2 Cabin AltitudeWarning System(600, 601, 601-3A,601-3R)
1) Visual(CABIN PRESSLOW light)
C 1 0 (O) May be inoperative provided Cabin Altitude AuralWarning System is operative.
C 1 0 (O) May be inoperative provided airplane is operatedunpressurized.
2) Aural (Horn)***
D 1 0 (O) May be inoperative provided Cabin Altitude VisualWarning System is operative.
C 1 0 May be inoperative provide aircraft is operated at orbelow 10,000 feet MSL.
C 1 0 May be inoperative provided aircraft is operatedunpressurized.
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AIRCRAFT REVISION No: 1 Page
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
21 – AIR CONDITIONING 4. Remarks or Exceptions
30-3 Cabin AltitudeIndicator (600, 601,601-3A, 601-3R)
C 1 0 (O) May be inoperative provided:a) Cabin Differential Pressure Indicator is
operative, andb) A chart is provided to convert cabin differential
pressure to cabin altitude.
D 1 0 (O) May be inoperative provided aircraft is operatedunpressurized.
30-4 Cabin DifferentialPressure Indicator(600, 601,601-3A,601-3R)
C 1 0 (O) May be inoperative provided:a) Cabin Altitude Indicator is operative, andb) A chart is provided to convert cabin altitude to
cabin differential pressure.
D 1 0 (O) May be inoperative provided aircraft is operatedunpressurized.
30-5 Cabin Rate of ClimbIndicator(600, 601, 601-3A, 601-3R)
C 1 0 May be inoperative provided:a) Cabin Altitude Indicator is operative,b) Cabin Differential Pressure Indicator is
operative, andc) Cabin Pressurization Control System
Automatic Mode is operative.
C 1 0 (O) May be inoperative provided aircraft is operatedunpressurized.
30-6 CabinPressurization PanelEMER DEPRESS“ON” Switch Light(light function only)(604, 605, 650)
C 1 0 (O) May be inoperative provided the EMER DEPRESScaution message is verified operative.
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AIRCRAFT REVISION No: 1 Page
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
21 – AIR CONDITIONING 4. Remarks or Exceptions
31-1 CabinPressurizationControl System
1) Automatic andManual Modes
C 2 0 (O) Both may be inoperative provided:a) Aircraft is operated unpressurized, andb) Aircraft is not operated in extended overwater
operations.
NOTE 1: (604, 605, 650)During ground operations at ambienttemperatures above 40ºC (104ºF),operation of electrical/avionics equipmentmust be limited to thirty minutes unless atleast one ACU/Pack is operating andcabin doors are closed as per AFM.
NOTE 2: (600, 601, 601-3A, 601-3R)During ground operations at ambienttemperatures above 45ºC (113ºF),operation of electrical/avionics equipmentmust be limited to thirty minutes unless atleast one ACU/Pack is operating andcabin doors are closed as per AFM.
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2) Automatic Mode(600, 601, 601-3A, 601-3R)
C 1 0 (O) May be inoperative provided:a) Cabin Pressurization Control System Manual
Mode is operative,b) Autopilot is operative, andc) Aircraft is not operated more than 60 minutes
from a suitable airport.
C 1 0 (O) May be inoperative provided:a) Total fuel carried includes at least 50% more
than the fuel load required for the planned flight,and
b) Aircraft speed is limited to 300 KIAS when at orbelow 12,500 feet.
(Cont’d)
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AIRCRAFT REVISION No: 1 Page
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
21 – AIR CONDITIONING 4. Remarks or Exceptions
31-1 CabinPressurizationControl System(Cont'd)
3) Automatic Mode(604, 605, 650)
C 1 0 May be inoperative provided:a) Cabin Pressurization Control System Manual
Mode is operative,b) Autopilot is operative, andc) Aircraft is not operated more than 60 minutes
from a suitable airport.
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4) Manual Mode C 1 0 May be inoperative provided:a) Cabin Pressurization Control System Automatic
Mode is operative,b) Aircraft is not operated more than 60 minutes
from a suitable airport, andc) Aircraft is not operated in extended overwater
operations.
32-1 OutflowValve/Safety Valves
C 2 0 (M)(O) One or both may be inoperative provided:a) Affected Valve(s) are secured OPEN,b) Airplane is operated unpressurized at or below
10,000 feet MSL,c) Extended overwater operations are prohibited,
and,d) Takeoffs and landings must not be conducted
on runways that may lead to imminent ditching.
33-1 Cabin PressureAcquisition Module(CPAM)
1) (604) C 1 0 (O) May be inoperative provided:a) Aircraft is operated unpressurized, andb) Aircraft is not operated in extended overwater
operations.
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AIRCRAFT REVISION No: 1 Page
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
21 – AIR CONDITIONING 4. Remarks or Exceptions
33-1 Cabin PressureAcquisition Module(CPAM)(Cont’d)
2) (605, 650) C 2 1 May be inoperative provided:a) Automatic Mode of the Pressurization Control
System is operative, andb) Aircraft is not operated more than 60 minutes
from a suitable airport.
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C 2 0 (O) May be inoperative provided:a) Aircraft is operated unpressurized, andb) Aircraft is not operated in extended overwater
operations.
33-2 Standby CabinAltimeter (604)
C 1 0 (O) May be inoperative provided flight planning allowsfor descent to unpressurized flight altitudes in the eventof a CPAM failure.
51-1 Air ConditioningUnits (ACUs)(600, 601, 601-3A, 601-3R)
C 2 1 One may be inoperative provided:a) Ram Air Vent Valve is operative,b) Associated cowl anti-ice is selected ON when
aircraft is operated above FL 400, andc) Aircraft is not operated more than 60 minutes
from a suitable airport.
C 2 1 One may be inoperative provided:a) Total fuel carried includes at least 50% more
than the fuel load required for the plannedflight; and
b) Aircraft speed is limited to 300 KIAS when ator below 12, 500 ft.
(Cont’d)
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
21 – AIR CONDITIONING 4. Remarks or Exceptions
51-1 Air ConditioningUnits (ACUs)(600, 601, 601-3A, 601-3R)(Cont’d)
C 2 0 (O) Both may be inoperative provided:a) Ram Air Vent Valve is operative, andb) Aircraft is operated unpressurized.
NOTE : During ground operations at ambienttemperatures above 45oC (113oF) operation ofelectrical / avionics equipment must be limitedto 30 minutes unless at least one ACU isoperating and cabin doors are closed as perAFM.
51-2 Air ConditioningPacks(604, 605, 650)
C 2 1 One may be inoperative provided:a) Ram Air Vent Valve is operative,b) Associated cowl anti-ice is selected ON when
aircraft is operated above FL 400, andc) Aircraft is not operated more than 60 minutes
from a suitable airport.
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C 2 0 (O) Both may be inoperative provided:a) Ram Air Vent Valve is operative, andb) Aircraft is operated unpressurized.
NOTE : During ground operations at ambienttemperatures above 40ºC, (104ºF) operationof electrical / avionics equipment must belimited to 30 minutes unless at least onepack is operating and cabin doors are closedas per AFM.
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
21 – AIR CONDITIONING 4. Remarks or Exceptions
51-3 Air ConditioningPack “L/R FAIL”Switchlight(light function only)(604, 605, 650)
C 2 0
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51-4 CabinPressurization Panel“FAIL/MANUAL”Switchlight(light function only)(604, 605, 650)
B 1 0 (O) May be inoperative provided the manual andautomatic mode are verified operative on EICAS.
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52-1 Ram Air Vent Valve C 1 0 (M) May be inoperative CLOSED provided:a) Valve is deactivated closed, andb) Both ACUs / Packs are operative.
C 1 0 (M) May be inoperative OPEN provided:a) Valve is deactivated open,b) RH ACU/Pack is operative,c) LH ACU/Pack is selected OFF,d) Associated cowl anti-ice is selected ON when
aircraft is operated above FL 400, ande) Aircraft is not operated more than 60 minutes
from a suitable airport.
53-1 Right FootwarmerDe-Mist PressureRegulating andShut-Off Valve(600, 601, 601-3A)
C 1 0
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21 – AIR CONDITIONING 4. Remarks or Exceptions
61-1 TemperatureControl System
1) Cockpit Modes(NORMAL,STANDBY,MANUAL)
C 3 1
C 3 0 Any or all may be inoperative provided all Cabin modesare operative.
2) Cabin Modes(NORMAL,STANDBY,MANUAL)
C 3 1
C 3 0 Any or all may be inoperative provided all CockpitModes are operative.
61-2 Cabin TemperatureIndicator(600, 601, 601-3A, 601-3R)
C 1 0
61-3 EICAS “CABINTEMP” Indication(604, 605, 650)
C 1 0
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61-4 Cockpit HeatSystem(601-3R, 604)
C 1 0 (M) May be inoperative provided the system isdeactivated.
61-5 Pilots Heated Mats(605, 650)
C 4 0 (M) Any or all may be inoperative provided heated matsare deactivated. |
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
22 – AUTO FLIGHT 4. Remarks or Exceptions
10-1 Autopilot System1) 600, 601 B 1 0 (M)(O) Except when enroute operations or approach
procedures require its use, may be inoperativeprovided:
a) Autopilot is deactivated after Mach Trim test isverified operative once each flight day, and
b) Any increase in crew workload caused by theaffected autopilot has been considered forintended operation.
a) Roll axischannel
C 2 1 (O) May be inoperative provided the opposite rollchannel and roll monitor is verified operative prior toeach flight.
b) Pitch axischannel
C 2 1 (O) May be inoperative provided the opposite pitchchannel is verified operative prior to each flight.
2) 601-3A, 601-3R(AFCS)
C 2 1 (M) Except where enroute operations or approachprocedures require dual autopilot systems, may beinoperative provided:
a) Affected system is deactivated, andb) Autopilot and Transponder use same ADC
data for RVSM Operations.
B 2 0 (M) Except when enroute operations or approachprocedures require its use both may be inoperativeprovided:
a) Both systems are deactivated, andb) Any increase in crew workload caused by the
affected autopilot has been considered forintended operation.
3) 604, 605, 650(AFCS)
C 2 1 Except where enroute operations or approachprocedures require dual autopilot systems, may beinoperative provided:
a) Alternate AFCS is selected, andb) Autopilot and Transponder use same ADC
data for RVSM Operations.
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(Cont’d)
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1. 2. Number InstalledSystem & Sequence No Item
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22 – AUTO FLIGHT 4. Remarks or Exceptions
10-1 Autopilot System(Cont’d)
3) 604, 605, 650(AFCS)(Cont’d)
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B 2 0 (O) Except when enroute operations or approachprocedures require its use both may be inoperativeprovided:
a) Both systems are deactivated, andb) Any increase in crew workload caused by the
affected autopilot has been considered forintended operation.
a) VNAV ModeSwitch
C 1 0 May be inoperative provided enroute operations orapproach procedures are not dependent on its use.
10-2 Flight Directors1) 600, 601,
601-3A,601-3R
C 2 1 (O) May be inoperative provided:a) Approach minimums or operating procedures
are not dependent on its use,b) Flight Director and Transponder must use
same ADC data for RVSM Operations, andc) Associated TOGA switch is considered
inoperative.
B 2 0 (O) Except where enroute operations or approachprocedures require its use, both may be inoperativeprovided:
a) Associated TOGA switches is consideredinoperative, and
b) Autopilot is considered inoperative.
2) 604, 605, 650(FCC channels)
C 4 3 One may be inoperative provided associated autopilot(AFCS 1 or 2) is considered inoperative.
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C 4 2 (O) Two may be inoperative provided AFCS 1 or 2 isoperative.
(Cont’d)
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1. 2. Number InstalledSystem & Sequence No Item
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22 – AUTO FLIGHT 4. Remarks or Exceptions
10-2 Flight Directors(Cont’d)
2) 604, 605, 650(FCC channels)(Cont’d)
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B 4 1 (O) Except for RVSM Operations, three may beinoperative provided:
a) AFCS 1 and 2 are considered inoperative,b) One Yaw Damper is verified operative, andc) Approach minimums or operating procedures
are not dependent on their use.
11-1 Autopilot DisconnectSwitches (ControlWheel Buttons)
C 2 1 One may be inoperative provided:a) Pusher of the stall protection system can be
disengaged using the control wheel disconnectbutton,
b) With autopilot engaged the pilot controlling theaircraft has an operative disconnect switch,and
c) Autopilot is not engaged below 1500 feet AGL.
C 2 0 Both may be inoperative provided:a) Pusher of the stall protection system can be
disengaged using both control wheeldisconnect buttons, and
b) Autopilot system is not used.
11-2 Touch ControlSteering (TCS)Switches(600, 601, 601-3A, 601-3R)
C 2 0
11-3 AP/FD SyncSwitches(604, 605, 650)
C 2 0
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22 – AUTO FLIGHT 4. Remarks or Exceptions
11-4 Take-Off/Go-Around(TOGA) Switches
C 2 1 One may be inoperative provided:a) Approach procedures do not require its use,
andb) Pilot flying has the operative buttons.
C 2 0 Both may be inoperative provided:a) Both Thrust Levers are operated manually for
take-off and go-around, andb) Autopilot and Flight Director are not used at
less than 1500 feet AGL.
11-5 Flight GuidanceComputers(601-3A, 601-3R)
C 2 1 One may be inoperative provided aircraft is notoperated more than 60 minutes from a suitable airport.
NOTE: Each FGC provides Mach Trim, Yaw Damper,Autopilot and Flight Director functionsindependent of the other FGC. Failure of thesecond FGC after dispatch will result in thecomplete loss of these functions and AFMrestrictions will apply.
12-1 V-Speed Auto-SynchronizationSystem(604, 605, 650)
C 1 0 May be inoperative provided V Speed settings aremade manually by each pilot.
NOTE: “SPEED REFS INDEP” status message will bedisplayed on EICAS if selected speeds aredifferent.
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13-1 Input/OutputConcentrator (IOC)(Integrated AvionicsProcessing System)(604, 605, 650) |
1) (604(withoutAutothrottleSystem)
C 4 3 (M)(O) One IAPS IOC may be inoperative provided:a) Remaining IOCs are verified operative before
the first flight of the day,b) RTU 2 is operative, andc) Lightning Detection System (if installed)
is considered inoperative if the failed IOC is the2A quadrant.
NOTE : "IAPS DEGRADED" status message willbe displayed on EICAS.
(Cont'd)
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1. 2. Number InstalledSystem & Sequence No Item
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22 – AUTO FLIGHT 4. Remarks or Exceptions
13-1 Input/OutputConcentrator (IOC)(Integrated AvionicsProcessing System)(604, 605, 650)(Cont’d)
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2) (604 withAutothrottleSystem)
C 4 3 (M)(O) One IAPS IOC may be inoperative provided:a) Remaining IOCs are verified operative before
the first flight of the day,b) RTU 2 is operative,c) Lightning Detection System (if installed)
is considered inoperative if the failed IOC is the2A quadrant, and
d) The Autothrottle system is consideredinoperative if the failed IOC is the 1A quadrant.
NOTE : "IAPS DEGRADED" status message will bedisplayed on EICAS.
3) (605, 650) C 4 3 (M)(O) One IAPS IOC may be inoperative provided:
a) Remaining IOCs are verified operative beforethe first flight of the day,
b) CDU 2 radio tuning function is operative,
c) The Autothrottle system is consideredinoperative if the failed IOC is the 1A quadrant,and
d) Lightning Detection System (if installed)is considered inoperative if the failed IOC is the2A quadrant.
e) The Integrated Flight Information System (IFIS)File Server Unit (FSU) is consideredinoperative if the failed IOC is the 1A quadrant.
NOTE : "IAPS DEGRADED" status message will bedisplayed on EICAS.
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(Cont'd)
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1. 2. Number InstalledSystem & Sequence No Item
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22 – AUTO FLIGHT 4. Remarks or Exceptions
20-1 Mach Trim System C 1 0 May be inoperative provided autopilot is engaged inflight.
C 1 0 May be inoperative provided airspeed is limited to 250KIAS/0.7 Mach when the autopilot is not engaged.
NOTE: Autopilot must be engaged during RVSMOperations.
20-2 Yaw DamperChannels
C 2 1 (O) One channel may be inoperative provided therudder is verified in the central position before flight.
20-3 Yaw Rate Gyros(600, 601, 601-3A,601-3R)
C 2 1 (O) One channel may be inoperative provided therudder is verified in the central position before flight.
30-1 Autothrottle System(604***, 605, 650)
C 1 0 (M) May be inoperative provided the autothrottlesystem is deactivated. |
D 1 0 (M) May be inoperative provided:
a) The autothrottle system is deactivated, andb) Routine procedures do not require its use.
1) AutothrottleDisconnectPushbuttonSwitch(On ThrustLever)(605, 650)
C 2 1 (O) May be inoperative provided theEngage/Disengage Pushbutton Switch is verifiedoperative.
|
C 2 0 May be inoperative provided the Autothrottle System isconsidered inoperative.
2) AutothrottleMode StatusDisplay(MSD)(605, 650)
C 2 1 May be inoperative on the non-flying pilot side andAutothrottle System is not used on that side.
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C 2 0 May be inoperative provided the Autothrottle System isconsidered inoperative.
(Cont'd)
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1. 2. Number InstalledSystem & Sequence No Item
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22 – AUTO FLIGHT 4. Remarks or Exceptions
30-1 Autothrottle System(604***, 605, 650)(Cont’d)
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3) AutothrottleN2 Sync PBA(605, 650)
C 1 0
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4) Engage LEDAnnunciator(605, 650)
C 2 1 .
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C 2 0 May be inoperative provided the Mode Status Display(MSD) on the flying pilot side is operative.
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23 – COMMUNICATIONS 4. Remarks or Exceptions
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
23 – COMMUNICATIONS 4. Remarks or Exceptions
11-1 CommunicationSystems(VHF, HF, etc)
1) VHF D - 2 Any in excess of those required by regulations may beinoperative provided:
a) VHF3 is operative (if installed), andb) It is not required for emergency purposes.
2) HF A - 1 (O) Any in excess of one may be inoperative for amaximum of 3 calendar days provided alternatecommunication procedures are established and used.
C - 1 (O) Any in excess of one may be inoperative provided:
a) SATCOM air-ground communications with AirTraffic Service Providers (ATSPs) are availablefor the intended flight route,
b) SATCOM Voice or Data transfer functions areoperative,
c) Prior to each flight, coordination with theappropriate Air Navigation Service Provider(s)is established where INMARSAT codes, orequivalent, are not available whilst usingSATCOM voice function, and
d) Alternate communication procedures areestablished and used.
D - - Any in excess of those required for the intended routemay be inoperative.
11-2 COMM Control Head #2 (COMM DigitalFrequency Selector/LEDDisplay Units)(601-3A, 601-3R)
C 1 0 May be inoperative provided the FMS CDU tuningcapability is operative.
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23 – COMMUNICATIONS 4. Remarks or Exceptions
11-3 Inflight TelephoneSystem***
D - 0
11-4 Datalink System(605, 650)***(IncludesCPDLCandADS-Cfunctions)***
C 1 0 (O) May be inoperative provided alternate proceduresare established and used. |
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D 1 0 May be inoperative provided routine procedures do notrequire its use.
1) Controller Pilot DataLink Communications(CPDLC)(WithSB 605-23-007, orSB 605-23-008, orSB 650-23-007orSB 650-23-008)
C 2 0 (O) May be inoperative where routine proceduresrequire its use provided alternate procedures areestablished and used.
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D 2 0 May be inoperative provided operating regulations donot require its use.
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a) CPDLC In-ComingMessage VisualAlerting(CDU and EICAS)
C 2 0 May be inoperative where routine procedures requireits use provided In-Coming Message Aural Alerting(chime) is operative.
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D 2 0 May be inoperative provided operating regulations androutine operations do not require the use of CPDLC.
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2) AutomaticDependentSurveillanceContract(ADS-C)***
C 2 0 (O) May be inoperative where routine proceduresrequire its use provided alternate procedures areestablished and used.
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D 2 0 May be inoperative provided operating regulations donot require its use.
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23 – COMMUNICATIONS 4. Remarks or Exceptions
21-1 Selective Call (SELCAL)System***
C - 0 (O) May be inoperative provided alternate proceduresare established and used.
D - 0 May be inoperative provided procedures do not requireits use.
1) Channels(604, 605, 650)
D 2 1|
C - 0 (O) May be inoperative provided alternate proceduresare established and used
D - 0 May be inoperative provided procedures do not requireits use.
21-2 SatelliteCommunications(SATCOM) Systems***
C - 0 (O) May be inoperative provided alternate proceduresare established and used.
D - 0 May be inoperative provided routine procedures do notrequire its use.
31-1 Public Address (PA)System***
D - - Any in excess of those required may be inoperativeprovided procedures do not require their use.
C - - (O) Any in excess of those required maybe inoperativeprovided alternate procedures are established andused.
B - 0 (O) May be inoperative provided:a) Alternate procedures are established and used,
andb) Flight crew compartment from and to cabin
interphone system (including audio and visualalerting system) is operative.
(Cont’d)
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1. 2. Number InstalledSystem & Sequence No Item
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
23 – COMMUNICATIONS 4. Remarks or Exceptions
41-1 Crew MemberInterphone System
C - - (O) Any in excess of those required may be inoperativeprovided alternate procedures are established andused.
D - - Any in excess of those required may be inoperativeprovided procedures do not require their use.
1) Flight CrewCompartment toCabin / Cabin toFlight CrewCompartmentInterphone
B 1 0 (O) May be inoperative provided:a) PA system is verified operative, andb) Alternate procedures are established and
used.
2) Alerting System(Chime/Light)
C - - (O) May be inoperative provided:a) Flight crew compartment call audio alerting
system is operative,b) Public Address system is operative, andc) Alternate procedures are established and
used.
3) FlightCompartment toGround /Ground to FlightCompartment
C 1 0 (O) May be inoperative provided alternate proceduresare established and used.
(Cont’d)
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1. 2. Number InstalledSystem & Sequence No Item
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23 – COMMUNICATIONS 4. Remarks or Exceptions
50-1 Headset D - - Any in excess of one headset (including boommicrophone) for each required crew member on flightcrew compartment duty may be inoperative or missing.
50-2 Cockpit Speakers C 2 0 (O) One or both may be inoperative provided:a) Aural alerts, messages and other
communication which are normally routedthrough the speakers are audible through theheadsets,
b) A headset is operative for each required crewmember on flight crew compartment duty, and
c) A spare operative headset is readily availablein the flight crew compartment for use by anyof the required crew member on flight crewcompartment duty.
50-3 Pre-recordedAnnouncement(Passenger Briefing)System***
C 1 0 (O) May be inoperative provided alternate proceduresare established and used.
50-4 Lavatory Speakers C - 0 (O) May be inoperative provided alternate proceduresare established and used.
51-1 Flight Deck HandMicrophones
C - 0 May be inoperative provided:a) Associated boom microphone operates
normally, andb) Each (Control Wheel) Press-To-Talk Switch is
operative.
D - - Any in excess of those required by regulation may beinoperative.
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
23 – COMMUNICATIONS 4. Remarks or Exceptions
51-2 Press-To-Talk (PTT)Switches(Control Wheel)(600, 601, 601-3A,601-3R)
B 2 0 (M) Any in excess of one for each required flight crewmember may be inoperative provided the affectedswitch is either verified failed open (non-transmitting) oris deactivated.
51-3 RT/IC Switches(Pilot / Co-Pilot)(604, 605, 650)
B 4 2 One or two may be inoperative provided:a) Switch is verified not failed in the transmit
mode, andb) One RT/IC switch operates normally for each
crew-member.
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51-4 Headsets D - - Any in excess of one headset (including boommicrophone) for each required crew member on flightcrew compartment duty may be inoperative or missing.
70-1 Flight CrewCompartment DoorSurveillance System***
D - 0 (O) May be inoperative provided alternate proceduresare established and used.
71-1 Cockpit VoiceRecorder (CVR)System***
A - 0 May be inoperative provided:
a) The aircraft does not exceed 8 furtherconsecutive flights with the cockpit voicerecorder inoperative,
b) A maximum of 72 hours have elapsed sincethe cockpit voice recorder was found to beinoperative, and
c) Any Flight Data Recorder required to becarried is operative.
D - - Any in excess of those required may be inoperative.
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23 – COMMUNICATIONS 4. Remarks or Exceptions
71-2 Electronic Checklist(604, 605, 650)***
D 1 0 (O) May be inoperative provided alternate proceduresare established and used. |
81-1 Radio Tuning Units(RTUs)(604)
C 2 1 (O) RTU 2 may be inoperative provided:a) Radio Tuning from at least one FMS unit is
verified operative,b) RTU 1 cross-side tuning is verified operative,
andc) RTU #2 is de-selected using its RTU INHIBIT
switch to ensure cross-side tuning by RTU #1,and
d) Operations do not require the use of HF.
NOTE 1: If RTU 1 fails, to restore ATC, the ATCselector switch, on the Reversionary/Inhibitpanel, must be selected from STBY to 1.
NOTE 2: Also, if RTU 1 fails, all RTU modeselections (COM 1 Squelch ON/OFF, NAVMarker sens. LO/HI, NAV DME-HOLD,ATC Altitude ON-OFF, ATC ID, ADF ANT,ADF BFO (ON/OFF),TCAS and HF) will belost, however, COM/NAV frequency tuningwill be available through FMS.
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1. 2. Number InstalledSystem & Sequence No Item
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24 – ELECTRICAL POWER 4. Remarks or Exceptions
21-1 Engine IntegratedDrive Generators(IDGs)1) (601-3A, 601-
3RwithoutSB 601-0568and604 withoutSB 604-49-006)
A 2 1 (M)(O) One may be inoperative provided:a) Inoperative generator GEN 1/2 switch is
selected to OFF,b) APU is operated continuously throughout flight
and the APU generator is verified operativeprior to flight,
c) APU generator is switched off throughout flight,d) Cross-side Hydraulic AC Motor Pump ACMP
(1B or 2B) is selected ON,e) APU AC Loadmeter is operative,f) Aircraft is operated in day VMC,g) Aircraft is operated at or below 10, 000 ft,h) Aircraft is not operated more than 60 minutes
from a suitable airport,i) If the operative IDG or APU generators have
P/Ns 720845, 720845A or 720845B, they musthave achieved an operational life in excess of150 operating hours, and
j) Repairs are made after one flight.
2) (604 withoutSB 604-49-006)
B 2 1 (M) One may be inoperative provided:a) Inoperative generator GEN 1/2 switch is
selected to OFF,b) APU is operated continuously throughout flight
and the APU generator is verified operativeprior to flight,
c) APU generator is switched off throughout flight,d) Cross-side Hydraulic AC Motor Pump ACMP
(1B or 2B) (29-11-1) is considered inoperative,e) APU AC Loadmeter is operative,f) Aircraft is operated in day VMC,g) Aircraft is operated at or below 10, 000 ft,h) Aircraft is not operated more than 60 minutes
from a suitable airport, andi) If the operative IDG or APU generators have
P/Ns 720845, 720845A or 720845B, they musthave achieved an operational life in excess of150 operating hours.
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24 – ELECTRICAL POWER 4. Remarks or Exceptions
21-1 Engine IntegratedDrive Generators(IDGs)Cont’d
3) (601-3A,601-3RwithSB 601-0568)
A 2 1 (M)(O) One may be inoperative provided:a) Inoperative generator GEN 1/2 switch is
selected to OFF,b) APU and its generator is operated continuously
throughout flight,c) Cross-side Hydraulic AC Motor Pump ACMP
(1B or 2B) is selected to ON,d) Aircraft is operated at or below FL 200,e) If the operative IDG or APU generators have
P/Ns 720845, 720845A or 720845B, they musthave achieved an operational life in excess of150 operating hours, and
f) Repairs are made after one flight.
4) (604 withSB 604-49-006andSB 604-24-020)
A 2 1 (M)(O) One may be inoperative provided:a) Inoperative generator GEN 1/2 switch is
selected to OFF,b) APU and its generator is operated continuously
throughout flight,c) Cross-side Hydraulic AC Motor Pump ACMP
(1B or 2B) is selected to ON,d) Aircraft is operated at or below FL 200,e) If the operative IDG or APU generators have
P/Ns 720845, 720845A or 720845B, they musthave achieved an operational life in excess of150 operating hours, and
f) Repairs are made after one flight.
(Cont’d)
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 24-3
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
24 – ELECTRICAL POWER 4. Remarks or Exceptions
21-1 Engine IntegratedDrive Generators(IDGs)(Cont’d)4) (604 with
SB 604-49-006andSB 604-24-020)(Cont’d)
B 2 1 (M) One may be inoperative provided:a) Inoperative generator GEN 1/2 switch is
selected to OFF,b) APU and its generator is operated continuously
throughout flight,c) Cross-side Hydraulic AC Motor Pump (ACMP)
(1B or 2B) is considered inoperative,d) Aircraft is operated at or below FL 200, ande) If the operative IDG or APU generators have
P/Ns 720845, 720845A or 720845B, they musthave achieved an operational life in excess of150 operating hours.
5) (605, 650) A 2 1 (O) One may be inoperative provided:a) Inoperative generator GEN 1/2 switch is
selected to OFF,b) APU and its generator is operated continuously
throughout flight,c) Cross-side Hydraulic AC Motor Pump ACMP
(1B or 2B) is selected to ON,d) Aircraft is operated at or below FL 200, ande) Repairs are made after one flight.
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B 2 1 One may be inoperative provided:a) Inoperative generator GEN 1/2 switch is
selected to OFF,b) APU and its generator is operated continuously
throughout flight,c) Cross-side Hydraulic AC Motor Pump (ACMP)
(1B or 2B) is considered inoperative, andd) Aircraft is operated at or below FL 200.
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 24-4
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
24 – ELECTRICAL POWER 4. Remarks or Exceptions
22-1 Auxiliary Power Unit(APU) ACLoadmeter1) Aircraft with IDG
P/Ns 720845,720845A,720845B
C 1 0 (M) May be inoperative provided:a) Any main generator with these P/Ns has more
than 150 operating hours,b) APU generator is not used, andc) APU generator switch is selected to
OFF/RESET.
2) Aircraft withother IDG P/Ns
C 1 0 May be inoperative provided:a) APU generator is not used, andb) APU generator switch is selected to
OFF/RESET.
22-2 Auxiliary Power Unit(APU) GeneratorSystem1) Aircraft with IDG
P/Ns 720845,720845A,720845B
C 1 0 (M) May be inoperative provided any main generatorwith these P/Ns has more than 150 operating hours.
2) Aircraft withother IDG P/Ns
C 1 0
23-1 Air Driven Generator(ADG) Auto-Deployment System
C 1 0 (M) May be inoperative provided the Auto-Deploymentsystem is deactivated.
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 24-5
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
24 – ELECTRICAL POWER 4. Remarks or Exceptions
30-1 Main AirplaneBattery (600, 601,601-3A, 601-3R)
D - 1 (M) Main Airplane Battery may be inoperative provided:a) Additional Main Airplane Battery and its
associated Charger are operative, andb) Affected Main Airplane Battery and its
associated Charger are isolated bydisconnecting and securing them.
30-2 Main AirplaneBattery Charger(600, 601, 601-3A,601-3R)
D - 1 (M) Main Airplane Battery Charger may be inoperativeprovided:
a) Additional Main Airplane Battery and itsassociated Charger are operative, and
b) Affected Main Airplane Battery and itsassociated Charger are isolated bydisconnecting and securing them.
30-3 APU AuxiliaryBattery(601-3A)(600,601)***
C - 0 (O) May be inoperative provided alternate proceduresare established and used.
D - 0 May be inoperative provided routine procedures do notrequire its use.
30-4 Refueling PanelBattery***
D 1 0 (M) May be inoperative provided Airplane Battery canbe used to fuel airplane.
30-5 Battery Ammeter***
D 1 0
31-1 TRU Cooling Fans1) 600, 601 C 3 1 (M) One or two may be inoperative provided:
a) ESS TRU Cooling Fan is operative, andb) Forward equipment doors are opened for
stationary ground operations at temps. >30 °C.
2) 601-3A, 601-3R,604, 605, 650
C 4 2 (M) One or two may be inoperative provided:a) ESS TRU 1 & 2 Cooling Fans are operative,
andb) Forward equipment doors are opened for
stationary ground operations at temps. >30 °C.
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EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 24-6
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
24 – ELECTRICAL POWER 4. Remarks or Exceptions
32-1 Main Battery1) (604) A 1 0 (M) May be inoperative provided:
a) APU Battery is operative,b) APU Battery Charger is operative,c) Boarding lights are considered inoperative,d) Service lights are considered inoperative,e) APR is selected off,f) Operations are conducted in accordance with
AFM APR inoperative performance data, andg) Repairs are made within one flight day.
2) (605, 650) A 1 0 (M)(O) May be inoperative provided:a) APU Battery is operative,b) APU Battery Charger is operative,c) Boarding lights are considered inoperative,d) Service lights are considered inoperative, ande) Repairs are made within one flight day
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32-2 Main BatteryCharger1) (604) A 1 0 (M) May be inoperative provided:
a) Main Battery is considered inoperative,b) APU Battery is operative,c) APU Battery Charger is operative,d) Boarding lights are considered inoperative,e) Service lights are considered inoperative,f) APR is selected off,g) Operations are conducted in accordance with
AFM APR inoperative performance data, andh) Repairs are made within one flight day.
2) (605, 650) A 1 0 (M)(O) May be inoperative provided:a) Main Battery is considered inoperative,b) APU Battery is operative,c) APU Battery Charger is operative,d) Boarding lights are considered inoperative,e) Service lights are considered inoperative, andf) Repairs are made within one flight day.
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EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 24-7
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
24 – ELECTRICAL POWER 4. Remarks or Exceptions
32-3 APU Battery(604, 605, 650)
A 1 0 (M) May be inoperative provided:a) Main Battery is operative,b) Main Battery Charger is operative,c) Both IDGs are operative, andd) Repairs are made within one flight day.
NOTE 1 : External DC power can be used to startAPU if required.
NOTE 2 : External DC power may be required forrefueling.
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32-4 APU BatteryCharger(604, 605, 650)
A 1 0 (M)(O) May be inoperative provided:a) APU Battery is considered inoperative after
APU is started,b) Main Battery is operative,c) Main Battery Charger is operative,d) Both IDGs are operative, ande) Repairs are made within one flight day.
NOTE 1 : External DC power can be used to startAPU if required.External
NOTE 2 : DC power may be required for refueling.
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32-5 Battery TemperatureMonitors***
D - 0
41-1 AC External PowerSystem
C 1 0
41-2 AC External Power“AVAIL / IN USE”Switch Lights(light function only)(604, 605, 650)
C 2 0
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42-1 DC External PowerSystem
C 1 0
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 24-8
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
24 – ELECTRICAL POWER 4. Remarks or Exceptions
42-2 DC Power Main BusSwitch Light(light function only)(604, 605, 650)
C 1 0
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42-3 DC External Power“IN USE” Light(604, 605, 650)
C 1 0
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42-4 AC/DC UTILITYSwitch light(light function only)(605, 650)
C 1 0
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EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-1
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
10-2 Chart Holders C - 0
1) IntegratedLights
C 2 0 May be inoperative provided cockpit lightingconfiguration is acceptable to the crewmembers.
11-1 Flight Crew Seats
1) PowerAdjustments***
D - 0 May be inoperative for each flight crew member.
2) ManualAdjustments
a) HorizontalAdjustments
- - Must be operative for each flight crew member.
b) Vertical andReclineAdjustments
B - 0 One or more may be inoperative provided theassociated power adjustment of the affected flight crewmember seat is operative.
B - 0 (M) One or more may be inoperative provided theaffected seat is secured or locked in a positionacceptable to the flight crew member.
c) OtherAdjustments
C - 0 (M) One or more may be inoperative provided theaffected seat is secured in a position acceptable to theflight crew member.
NOTE: If an inoperative armrest will hinder anemergency evacuation of any other flightduties it should be removed.
11-2 Cockpit Sunvisors C 2 0 May be inoperative or missing provided there are novisual restrictions to crewmembers.
11-3 GlareshieldRetractable Visors(604, 605, 650)
C 2 0 (M) May be inoperative or missing provided visor issecured in the retracted position or removed.
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EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-2
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
12-1 Observer Seat D 1 0 May be inoperative provided the affected seat is notoccupied and is correctly stowed.
20-1 Passenger Seats D - 0 (M) One or more may be inoperative provided:a) Inoperative seat does not block an emergency
exit,b) Inoperative seat does not restrict any
passenger from access to the main aircraftaisle, and
c) Affected seat(s) are blocked and placarded"DO NOT OCCUPY”.
NOTE: A seat with an inoperative or missingoccupant restraint system (seat belt, safetyharness, as applicable) is consideredinoperative.
1) ReclineFunctions
C - - One or more may be inoperative and the affected seatoccupied provided the seat back is immovable in thetake-off and landing position.
D - - (M) One or more may be inoperative and the affectedseat occupied provided the seat is secured in the take-off and landing position.
2) UnderseatBaggageRestrainingBars
D - - (O) May be inoperative or missing provided:a) Baggage is not stowed under associated seat,b) Associated seat is placarded ‘DO NOT STOW
BAGGAGE UNDER THIS SEAT’,c) Restraining bar does not restrict any
passenger from access to the main aircraftaisle, and
d) Procedures are established and used to alertcabin crew of inoperative restraining bars.
(Cont’d)
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-3
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
20-1 Passenger Seats(Cont’d)
3) Passenger SeatArmrests withRecline ControlMechanism
D - - (M) May be inoperative, damaged or missing and theaffected seat occupied provided:
a) The affected armrest does not block anemergency exit,
b) The affected armrest is not in such a positionthat it restricts any passengers from access tothe aircraft aisle, and
c) If armrest is missing, seat is secured in the fullupright position.
4) Passenger seatarmrests withoutrecline controlmechanism
D - - May be inoperative, damaged or missing, and theaffected seat occupied provided:
a) The affected armrest does not block anemergency exit, and
b) The affected armrest is not in such a positionthat it restricts any passengers from access tothe aircraft aisle.
5) Swivel/TravelMechanism***
C - - One or more may be inoperative and the affected seatoccupied provided the affected seat is immovable intake-off and landing position.
D - - (M) One or more may be inoperative and the affectedseat occupied provided:
a) Affected seat is secured in take-off and landingposition,
b) Affected seat does not block an emergencyexit, and
c) Affected seat does not restrict any passengerfrom access to the main aircraft aisle.
(Cont’d)
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-4
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
20-2 Cabin Seat StorageDoor (Under Seat)***
D - 0 (M)(O) May be inoperative or missing provided:a) If missing, contents must be relocated,b) If inoperative, door must be closed and
secured and contents relocated, andc) If contents contain emergency equipment, the
equipment must be relocated and accessiblefor the passenger or the seat must beconsidered inoperative. If the relocatedemergency equipment is an approved meansof flotation, it must be accessible to thepassenger while seated.
20-3 Divan Seat BerthingBelt***
D - 0 May be inoperative or missing provided divan seat isnot used for berthing.
20-5 Cabin Gasper Vents D - 0
29-1 Cabin Power Outlet D - 0 (M) May be inoperative provided affected outlet isdeactivated.
30-1 StorageBin(s)/Cabin,Galley, and LavatoryStorageCompartment/Closets
C - - (M) May be inoperative provided:a) Procedures are established to secure the
affected bin, compartment, or closet in theclosed position,
b) Affected bin, compartment or closet isprominently placarded DO NOT USE,
c) Any emergency equipment located in theaffected compartment is consideredinoperative and,
d) Affected bin, compartment, or closet is notused for storage of any items except for thosepermanently affixed.
NOTE: An inoperative lid/door latch renders thedoor inoperative
(Cont’d)
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-5
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
30-1 StorageBin(s)/Cabin,Galley, and LavatoryStorageCompartment/Closets(Cont’d)
C - - (M)(O) May be inoperative provided:a) For non-retractable doors, affected door is
removed,b) For retractable doors, affected door is removed
or secured in the retracted (fully open) position,c) Affected bin, compartment or closet is not used
for storage of any items, except thosepermanently affixed,
d) Affected bin, compartment or closet isprominently placarded DO NOT USE,
e) Procedures are established and used to alertcrew members and passengers of inoperativebins, compartments or closets and
f) Passengers are briefed that affected bin,compartment or closet is not used.
NOTE 1 : Any emergency equipment located in theassociated compartment (permanentlyaffixed) is available for use.
NOTE 2 : An inoperative lid/door latch renders thelid/door inoperative.
40-2 Exterior LavatoryDoor Ashtrays
A - 0 One or more may be inoperative or missing providedrepairs are made within three consecutive calendardays.
A - - One or more may be inoperative or missing provided:a) One operative exterior lavatory door ashtray
can be readily seen and accessed from theaffected lavatory door, and
b) Repairs are made within ten consecutivecalendar days.
(Cont’d)
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-6
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
40-2 Exterior LavatoryDoor Ashtrays(Cont’d)
D - 0 (M)(O) May be inoperative provided:a) The affected lavatory door is locked closed and
placarded to prohibit passengers’ entrance,and,
b) The affected lavatory is used only by crewmembers.
D - 0 One or more may be inoperative or missing providedflight is non-smoking.
40-3 Interior LavatoryDoor Ashtrays
B - 0 One or more may be inoperative or missing providedassociated lavatory fire-extinguishing system, wheninstalled, is operative.
D - 0 (M)(O) One or more may be inoperative or missingprovided:
a) The affected lavatory door is locked closed andplacarded to prohibit passengers’ entrance,and
b) The affected lavatory is used only by crewmembers.
50-1 Cargo RestraintSystems
C - - May be inoperative or missing provided baggagecompartment remains empty.
C - - All cargo is secured by an alternate approved method.
60-1 Protective BreathingEquipment (PBE)
D - - (M)(O) Any in excess of those required may beinoperative or missing provided:
a) Required distribution is maintained,
b) Inoperative PBE and its installed location areplacarded inoperative,
c) Inoperative PBE unit is secured out of sight inan approved stowage, and
d) Procedures are established and used to alertcrew members of inoperative or missingequipment.
NOTE: Inoperative PBE units may be subject todangerous goods requirements.
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-7
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
60-2 Airshow CockpitMonitor System***
D 1 0 (M) May be inoperative provided system is deactivated.
60-3 Security System***
D 1 0
60-4 IndependentPortable Lights
C - - May be inoperative or missing provided each requiredcrew member has an operative independent portablelight readily available when seated at designatedstation.
60-6 Emergency VisionAssurance System(EVAS)***
D 2 0
60-7 “FASTEN SEATBELT WHILESEATED” sign orplacard
C - - One or more signs or placards may be illegible ormissing provided a legible sign or placard is readablefrom each occupied passenger seat.
60-8 Megaphone***
D - 0 May be inoperative.
60-10 Life Rafts D - - (O) May be inoperative or missing provided:a) Extended overwater flights are not conducted,
and
b) Procedures are established and used to alertcrew members of inoperative or missingequipment.
60-11 Emergency MedicalKit (EMK)***
A - - The required emergency medical kits may beincomplete for flight to a destination where repairs orreplacements can be made but not to exceed amaximum of two calendar days.
D - - Any in excess of those required may be incomplete ormissing.
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-8
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
61-1 Crash Axes andCrowbars
D - - Any in excess of those required may be inoperative ormissing.
62-1 First Aid Kits A - - If more than one is required, only one of the requiredfirst-aid kits may be incomplete for two calendar days.
D - - Any in excess of those required may be incomplete ormissing.
63-1 Emergency LocatorTransmitter (ELT)
1) AutomaticEmergencyLocatorTransmitter
A 1 0 May be inoperative for a maximum of 6 flights or 25flight hours, whichever occurs first.
C - 1 Any in excess of one may be inoperative.
D - - Any in excess of those required may be inoperative.
2) SurvivalEmergencyLocatorTransmitter(ELT S)
D - - (M)(O) Any in excess of those required may beinoperative or missing provided:
a) Inoperative equipment and its installed locationare placarded inoperative,
b) Inoperative equipment is secured out of sight,and
c) Procedures are established and used to alertcrew members of inoperative or missingequipment.
64-1 Life jackets D - - (M)(O) Any in excess of those required may beinoperative or missing, provided:
a) Required distribution is maintained,b) Inoperative life jacket and its installed location
are placarded inoperative,,c) Inoperative life jacket is secured out of sight,
andd) Procedures are established and used to alert
crew members of inoperative or missingequipment.
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-9
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
70-1 Galley WasteReceptacles AccessDoors/Covers
C - - (M)(O) May be inoperative provided:a) The container is empty and the access is
secured to prevent waste introduction into thecompartment, and
b) Procedures are established to ensure thatsufficient galley/cabin waste receptacles areavailable to accommodate all waste that maybe generated on a flight.
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 25-10
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
25 – EQUIPMENT/ 4. Remarks or Exceptions FURNISHINGS
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EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 26-1
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
26 – FIRE PROTECTION 4. Remarks or Exceptions
10-1 APU Fire DetectionSystem1) (600, 601,
601-3A,601-3R)
C 1 0 (M) May be inoperative provided:a) If both main generators have P/Ns 720845,
720845A and 720845B they must have morethan 150 operating hours, and
b) APU is not used.
C 1 0 (M) May be inoperative provided:a) If both main generators have P/Ns 720845,
720845A and 720845B they must have morethan 150 operating hours,
b) APU is used on ground for engine start only,
c) APU is not used after engine start,d) APU external control system is operative, ande) Both IDGs are operative.
2) (604, 605, 650) C 1 0 (M) May be inoperative provided:a) APU is used on ground for engine start only,
b) APU is not used after engine start, andc) APU external control system is operative.
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C 1 0 May be inoperative provided APU is not used.
10-2 Lavatory SmokeDetection Systems***
C - 0 May be inoperative.
10-3 BaggageCompartment FireDetection /Suppression System***
C - 0 May be inoperative provided the baggage compartmentis empty.
(Cont’d)
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 26-2
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
26 – FIRE PROTECTION 4. Remarks or Exceptions
14-1 Main Landing GearBay OverheatDetection System
C 1 0 (M)(O) May be inoperative provided:a) Brakes are inspected prior to each flight and
are cool to the touch,b) After take-off the landing gear is left extended
for ten minutes,c) Takeoff performance is in accordance with the
AFM (Flight with Landing Gear Down), andd) Take-off is not conducted in icing conditions.
NOTE: In case of engine failure after V1,performance is the prime consideration andthe landing gear should be retracted normallyuntil performance penalty with gear down isnot a problem. Pilots must consider theeffects associated with delayed rising oflanding gear or lowering landing gear duringoperation from contaminated runways in icingconditions.
20-1 Lavatory WasteReceptacle FireExtinguisher System***
C - 0 May be inoperative.
20-2 Fuselage FireExtinguishingSystem (TotalFlood)***
C - 0 (M) May be inoperative provided the system is secured.
20-3 BaggageCompartmentSmoke DetectionSystem
C 1 0 For Class B,C or E Baggage compartments, thesystem may be inoperative provided the compartmentis empty.
NOTE: Unit Load Devices (ULD’s) may be carried inthe associated compartment provided no cargois carried on or in these devices. For ballastpurposes, use of bags (made of glass fibre orkevlar) or sand or ingots of non-magneticmetals (such as lead) is acceptable.
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 26-3
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
26 – FIRE PROTECTION 4. Remarks or Exceptions
20-4 Galley FireExtinguishingSystem***
C 1 0 May be inoperative provided:a) The galley is not used for any purpose, andb) Any waste receptacles are empty.
20-5 APU FireExtinguishingSystem1) (600, 601,
601-3A,601-3R)
C 1 0 (M) May be inoperative provided:a) If both main generators have P/Ns 720845,
720845A and 720845B they must have morethan 150 operating hours, and
b) APU is not used.
C 1 0 (M) May be inoperative provided:a) If both main generators have P/Ns 720845,
720845A and 720845B they must have morethan 150 operating hours,
b) APU is used on ground for engine start only,and
c) APU is not used after engine start.
d) APU external control system is operative, and
e) Both IDGs are operative.
C 1 0 May be inoperative provided APU is not used.
2) (604, 605, 650) C 1 0 (M) May be inoperative provided:a) APU is used on ground for engine start only,
b) APU is not used after engine start.c) APU external control system is operative, andd) Both IDGs are operative.
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C 1 0 May be inoperative provided APU is not used.
(Cont'd)
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 26-4
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
26 – FIRE PROTECTION 4. Remarks or Exceptions
20-6 APU FIREX BottleLow Pressure Switch1) (600, 601,
601-3A,601-3R)
C 1 0 (M)(O) May be inoperative provided:a) If both main generators have P/Ns 720845,
720845A and 720845B they must have morethan 150 operating hours,
b) The APU is used for ground operations only,c) Firex bottle charge pressure is visually verified
at bottle pressure gauge prior to each APUstart,
d) APU fire detection system is operative,e) APU external control system is operative,f) APU is not used after engine start, andg) Both IDGs are operative.
2) (604, 605, 650) C 1 0 (M) (O) May be inoperative provided:a) The APU is used for ground operations onlyb) Firex bottle charge pressure is visually verified
at bottle pressure gauge prior to each APUstart,
c) APU fire detection system is operative,d) APU external control system is operative ande) APU is not used after engine start.
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24-1 Hand FireExtinguishers
D - - (M)(O) Any of excess of those required may beinoperative or missing provided:
a) The inoperative hand fire extinguisher isremoved from the aircraft and its installedlocation is placarded inoperative; or it isremoved from the installed location, securedout of sight, and the hand fire extinguisher andits installed location are placarded inoperative,
b) Required distribution of operative units ismaintained throughout the aircraft, and
c) Procedures are established to alertcrewmembers of missing portable fireextinguisher.
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1. 2. Number InstalledSystem & Sequence No Item
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27 – FLIGHT CONTROLS 4. Remarks or Exceptions
05-1 Control SurfacePosition IndicatingSystems
1) FLT SPLR L/RAILERON L/RELEVATOR L/RRUDDER(600, 601, 601-3A, 601-3R)
C 7 0 (M)(O) Any or all indicator(s) may be inoperativeprovided:
a) Affected indicator is clearly identified asinoperative or covered, and
b) Affected control surface is visually checked forfull, free and correct movement prior to eachflight.
2) EICASIndications (FLTSPLR, AIL,RUDDER)(604, 605, 650)
C 5 0 (O) Any or all may be inoperative provided affectedControl Surface is visually checked for full, free andcorrect movement prior to each flight.
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3) EICASIndications(ELEV)(604, 605, 650) |a) L/H C 1 0 (O) May be inoperative provided:
a) Affected Control Surface is visually checked forfull, free and correct movement prior to eachflight, and
b) Autopilot is not engaged below 1500 feet AGL.
b) R/H D 1 0 (O) May be inoperative provided affected controlsurface is visually checked for full, free and correctmovement prior to each flight.
05-2 Ground SpoilerControl SurfaceIndications(LH & RH)(604, 605, 650)
C 2 0 (M) One or both may be inoperative provided:a) “ARM” mode is operative,b) Ground Spoilers switch is selected to AUTO,
andc) Ground spoilers are verified stowed before
each take-off.NOTE: “PROX SYS FAULT” status message appears
with “GND SPLRS” caution message.
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27 – FLIGHT CONTROLS 4. Remarks or Exceptions
05-3 Servo MonitorSystem(600, 601, 601-3A,6013R)
C 1 0 (M)(O) May be inoperative provided:a) All Powered Control Units (PCUs) are checked
prior to take-off to ensure correct operationusing each hydraulic system, and
b) Parking Brake SOV is open.
05-4 LH/RH Flight SpoilerIndication(Glareshield)(600, 601, 601-3A,601-3R)
C 2 0 (O) Both may be inoperative provided:a) Flight Spoiler Control Surface Position
Indication is operative,b) Flight Spoiler Indication on center pedestal is
verified operative prior to each flight,c) Flight Spoilers are verified stowed before take-
off, andd) Flight Spoilers are not used during approach.
12-1 Aileron Trim System B 1 0 May be inoperative provided:a) Autopilot is operative,b) Aileron Trim System is centered, andc) Main fuel tanks left and right are balanced prior
to take-off.
35-1 Stall Warning SwitchLights(light function only)(604)
C 2 1 One may be inoperative provided the shaker and thepusher are checked operative prior to each flight.
40-1 Trim Indicators(Ailerons, Rudder)
C 2 1 (O) One may be inoperative provided the affectedcontrol surface is checked visually as being in theappropriate take-off position prior to each take-off.
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27 – FLIGHT CONTROLS 4. Remarks or Exceptions
50-1 Flap Power DriveUnit (PDU) Motors
C 2 1 (M) May be inoperative provided:a) Affected motor is deactivated, andb) Operations are conducted in accordance with
AFM Supplement 14, Operations with AirplaneSystems Inoperative.(600, 601, 601-3A, 601-3R)
c) Operations are conducted in accordance withAFM Supplement 8, Operations with AirplaneSystems Inoperative.(604, 605, 650) |
NOTE 1: With only one motor operational, the flapswill operate at half speed.
NOTE 2: FLAPS MOTOR OVHT status messagewill be posted when a flap PDU isdeactivated.
52-1 Rudder PedalAdjustmentMechanism
C 2 0 (M)(O) May be inoperative provided:a) Rudder pedals can be secured in a position
acceptable to affected crewmember, andb) Rudder and brake pedals are checked for full
and unrestricted movement at both pilotstations.
NOTE: Full range of operation must be available tothe crewmember in seated position.
60-1 Ground SpoilerManual ArmingSwitchA/C withSB 600-0452SB 601-0113A/C 3060 & subs(604, 605, 650)
C 1 0 (O) May be inoperative provided the ground spoilerautomatic deployment is verified operative before eachflight.
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27 – FLIGHT CONTROLS 4. Remarks or Exceptions
60-2 Flight Spoiler LightsFlashing FeatureA/C withSB 600-0385SB 601-0040A/C 3013 &3018 to 3990
B 2 0 May be inoperative provided:a) Flight Spoilers are not used below 700 ft AGL,b) Flight spoilers are not used when flaps are
extended, andc) All flight spoilers indications are operative.
67-1 Ground SpoilerSystem1) 600, 601 C 1 0 (M) May be inoperative provided:
a) System is selected to OFF,b) Ground spoilers are verified in the retracted
position prior to each flight, andc) AFM Performance Chart entitled “Landing
Distance (Without Ground Spoilers)” is used.
NOTE: Service Bulletin 600-0368 must be installed onthe 600, or Service Bulletin 601-0020 must beinstalled on the 601.
2) 601-3A, 601-3R C 1 0 (M) May be inoperative provided:a) System is selected to OFF,b) Ground spoilers are verified in the retracted
position prior to each flight, andc) AFM Performance Chart entitled “Landing
Distance (Without Ground Spoilers)” is used.
3) 604, 605, 650 C 1 0 (M) May be inoperative provided:a) System is selected to DISARM,b) Ground spoilers are verified in the retracted
position prior to each flight, andc) Operations are conducted in accordance with
AFM Supplement 8 (Operations with AirplaneSystems inoperative).
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28 – FUEL 4. Remarks or Exceptions
11-1 Aux Tank FuelPanel with DrainValve
A 1 0 (M) May be inoperative (leaking) provided:a) Aux and Tail fuel tanks are verified empty prior
to the first flight each day and remain empty,b) Powered Crossfeed is considered inoperative
and not used,c) Aux and Tail fuel tank quantity indication or
EICAS readout is operative, andd) Repairs are made within 350 flight hours or at
the next A check, whichever occurs first.
NOTE: The Wing Tank Fuel Panel with Drain Valve isinterchangeable with the Aux Tank Fuel Panelwith Drain Valve. Refer to AMM.
D 1 0 (M) May be inoperative (leaking) provided panel withdrain valve is replaced with a blank panel.
11-2 Water Drain Valves C - 5 May be inoperative provided:a) One drain valve at each wing tank, lowest level
point is operative,b) One drain valve in the center tank is operative,c) Main Boost Pump drain valves are operative,
andd) There is no evidence of leakage.
13-1 Tail Cone Fuel TankSystem(601, 601-3A, ***)(601-3R)
C 1 0 (M) May be inoperative provided:a) Tail Cone fuel tank refuel / defuel SOVs are
verified in the closed position, andb) Tail cone fuel tank is empty.
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28 – FUEL 4. Remarks or Exceptions
13-2 Tail Tank FuelSystem (includingSaddle Tanks)(604, 605, 650)
C 1 0 (M) May be inoperative provided:a) Tail tank refuel / defuel SOVs are verified in the
closed position,b) Tail tank is empty,c) Aux tank is fueled as per AMM Chapter 12,
andd) CG load for the fuel distribution of all fuel
added is calculated to be aft of the Take-OffLimit Line (ref. AFM).
NOTE: It it is necessary to add fuel to the Aux tanks,precautions should be taken to keep theaircraft CG in the safe limits at all times.
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13-3 Turbulator Vanes(Fuel Jettison Mast,Tail Tank FuelSystems)
C 2 0 One or both turbulator vanes may be damaged ormissing provided the Tail Cone Fuel Tank System(601, 601-3A, 601-3R) or Tail Tank Fuel System (604,605, 650) as applicable is declared inoperative. |
15-1 Transfer Ejectors(Aux Tank)
B 2 1 One may be inoperative provided Aux Tank (and TailTank if installed) remains empty.
15-2 Crossfeed ShutoffValves(600, 601, ***)(601-3A, 601-3R)
1) Left to RightRight to Left
C 2 0 One or both may be inoperative closed provided:a) All Fuel Quantity Indications or EICAS
Readouts are operative, andb) Aircraft is operated in accordance with AFM
procedures if fuel crossfeed is required.
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28 – FUEL 4. Remarks or Exceptions
15-3 Tail Tank TransferBoost Pumps(604, 605, 650) |
1) Primary A 1 0 (M) May be inoperative provided:a) Pump is deactivated,b) Secondary pump is operative,c) Fuel jettison system is verified operative before
each flight, andd) Repairs are made within three flight days.
2) Secondary A 1 0 (M) May be inoperative provided:a) Pump is deactivated,b) Primary pump is operative,c) Fuel jettison system is verified operative before
each flight, andd) Repairs are made within three flight days.
15-4 Crossflow ShutoffValves1) Left to Aux
Right to Aux(604, 605, 650)
C 2 0 One or both may be inoperative closed provided:a) All Fuel Quantity Indications or EICAS
Readouts are operative, andb) Aircraft is operated in accordance with AFM
procedures if fuel crossflow is required.
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28 – FUEL 4. Remarks or Exceptions
23-1 Fuel (Boost) Pumps
1) 600,601,601-3A,601-3R
A 2 1 (M)(O) One may be inoperative provided:
a) Affected fuel (boost) pump is selected off anddeactivated,
b) Crossfeed (Left to Right, Right to Left) SOVsare operative,
c) Both fuel feed line check valves are verifiedoperative prior to the first flight,
d) If left boost pump is inoperative, APU isoperated continuously throughout flight andAPU generator is verified operative prior toflight, and
e) Repairs are made within one flight day.
2) 604, 605, 650 A 2 1 (M)(O) One may be inoperative provided:a) Affected fuel (boost) pump is selected off and
deactivated,b) Crossflow (Left to Aux, Right to Aux) SOVs are
operative,c) Both fuel feed line check valves are verified
operative prior to the first flight,d) If left boost pump is inoperative, APU is
operated continuously throughout flight andAPU generator is verified operative prior toflight, and
e) Repairs are made within one flight day.
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23-2 Fuel Boost Pump“INOP/ON” SwitchLights (light functiononly)(604, 605, 650)
C 2 0
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28 – FUEL 4. Remarks or Exceptions
25-1 APU Fuel Pump C 1 0 (M) May be inoperative provided:a) APU is operated for a maximum of 10 minutes
from start-up to shutdown,b) APU is only used to start one engine,c) APU generator adapter temperature is below
40oC, or warm to the touch, prior to enginestart,
d) APU is started with the left fuel boost pump,and
e) APU is shutdown and considered inoperative inflight.
C 1 0 May be inoperative provided APU is consideredinoperative and is not used.
25-2 APU Fuel ShutoffValves
C 2 0 (M) One or both may be inoperative closed providedAPU is not used.
25-3 APU Negative GFeed Check Valve.
C 1 0 (O) May be inoperative open provided flight operationsare not dependent on use of the APU.
27-1 Single PointPressure RefuelingSystem
C 1 0 (O) May be inoperative provided alternate proceduresare established and used.
1) ExternalRefuel/DefuelControl Panel
C 1 0 May be inoperative provided the internal Refuel/Defuelcontrol panel is operative.
2) InternalRefuel/DefuelControl Panel***
D 1 0
a) FuelQuantityDisplay
D 1 0 (O) May be inoperative provided alternate means isused to determine the amount of fuel.
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28 – FUEL 4. Remarks or Exceptions
27-2 Refuel / DefuelShut-Off Valves1) Left, Right, Aux C 3 0 (O) May be inoperative provided:
a) Alternate refueling procedures are establishedand used,
b) Ensure that the calculated static aircraft CGwith full mission fuel load is aft of the fwdaircraft Take-off Limit Line (ref. AFM), and
c) Fuel Quantity Indication Systems (cockpit) areoperative.
2) Tail C 2 0 (O) May be inoperative closed provided Aux and TailFuel Tanks remain empty.
C 2 0 (O) May be inoperative open provided:a) Alternate refueling procedures are established
and used,b) Ensure that the calculated static aircraft CG
with full mission fuel load is aft of the fwdaircraft Take-off Limit Line (ref. AFM), and
c) Left, Right, Aux Refuel/Defuel SOVs areclosed.
27-3 Refuel / DefuelAdapter Cap
C 1 0 (M) May be inoperative (missing) provided:a) Refuel / defuel adapter is visually checked for
contamination prior to each refueling,b) Adapter poppet is visually checked closed after
each refueling,c) No leakage can be detected after refueling is
complete, andd) All Refuel/Defuel Shut-off valves are verified
closed after each refueling.
40-1 EICAS Bulk FuelTemperatureIndication(604, 605, 650)
C 1 0 (M)(O) May be inoperative provided:a) Bulk fuel is verified to be > -200C before
dispatch, andb) Total air Temperature is not < -500C
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28 – FUEL 4. Remarks or Exceptions
41-1 Fuel QuantityIndicating Systems(Cockpit)(600, 601, 601-3A,601-3R)
1) Main Fuel TanksLeft and Right
C 2 1 (M) (O) One may be inoperative provided:
a) Alternate gravity refueling procedures areestablished and used,
b) Both main tanks are visually confirmed full,c) Total fuel carried includes 5% more than the
required fuel load for the planned flight,d) Aux fuel Tank Quantity Indicator is operative or
the Aux Fuel Tank is empty,e) Fuel Flow Indicating Systems and associated
engine instruments are operative,f) Gravity Crossflow SOV is verified operative,g) Crossfeed SOVs (if installed) remain closed,h) Lateral fuel balance is maintained during flight,i) Fuel Totalizer is considered inoperative,j) After takeoff, power is set by matching fuel flow
indications on both engines, andk) An in-flight log of fuel burned is maintained.
2) Aux Fuel Tank(Without TailTank installed)
C 1 0 (M) May be inoperative provided the Aux Fuel Tankremains empty.
C 1 0 (O) May be inoperative provided:a) Aux tank is completely filled,b) Left and Right Main Fuel Tank Quantity
Indicators are operative,c) Fuel Flow Indicating Systems and associated
engine instruments are operative,d) After takeoff, power is set by matching fuel flow
indications on both engines, ande) An in-flight log of fuel burned is maintained.
(Cont’d)
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28 – FUEL 4. Remarks or Exceptions
41-1 Fuel QuantityIndicating Systems(Cockpit)(600, 601, 601-3A,601-3R)(Cont’d)2) Aux Fuel
Tank(WithoutTail Tankinstalled)Cont’d
C 1 0 (M)(O) May be inoperative provided:a) Aux Fuel Tank is defueled each refueling,b) Aux Fuel Tank is refueled with a known
quantity of fuel,c) Required Aux Fuel Tank fuel is increased by
5%,d) Left and Right Main Fuel Tank Quantity
Indicators are operative,e) Fuel Flow Indicating Systems and associated
engine instruments are operative,f) Aux Fuel Tank is verified to empty at the
appropriate time,g) After takeoff, power is set by matching fuel flow
indications on both engines, andh) An in-flight log of fuel burned is maintained.
3) Aux Fuel Tank(With Tail Tankinstalled)
C 1 0 (M) May be inoperative provided the Aux and Tail FuelTanks remain empty.
4) Fuel Totalizer C 1 0
41-2 EICAS Aux andTotal Fuel TankQuantity Readouts(604, 605, 650)
C 2 0 (M) Both may be inoperative provided the Aux and Tailtanks remain empty.
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41-3 EICAS Tail Tankand Total FuelQuantity Readouts(604, 605, 650)
C 2 0 (M) Both may be inoperative provided:a) Tail tank remains empty,b) Aux tank is fueled as per AMM Chapter 12,
andc) Ensure that the calculated static aircraft CG
with full mission fuel load is aft of the fwdaircraft Take-off Limit Line (ref. AFM).
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28 – FUEL 4. Remarks or Exceptions
41-4 Fuel ComputerChannels(604, 605, 650)
B 2 1 One may be inoperative provided:a) Both Transfer Ejectors are operative,b) Both Crossflow SOVs are operative,c) Both Fuel Flow Readouts are operative,d) Fuel Used on FMS is operative, ande) Opposite IRS is operative.
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28 – FUEL 4. Remarks or Exceptions
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29 – HYDRAULIC POWER 4. Remarks or Exceptions
11-1 Hydraulic AC MotorPump (ACMP)(Systems 1 and 2)
1) ACMP 1B(604, 605, 650)
C 1 0 (M) May be inoperative provided:a) All other hydraulic pumps are operative,b) Affected pump is deactivated and selected
OFF,c) Nosewheel Steering is operative,d) Both Thrust Reverser Systems are operative,
ande) Operations are conducted in accordance with
AFM Supplement (Operations with AirplaneSystems Inoperative).
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2) ACMP 2B(604, 605, 650)
C 1 0 (M) May be inoperative provided:a) All other hydraulic pumps are operative,b) Affected pump is deactivated and selected
OFF,c) Ground Spoilers are operative,d) Nosewheel Steering is operative,e) Both Thrust Reverser Systems are operative,f) Both Anti-Skid System Channels are operative,g) Take-off or landing is not conducted from a
contaminated runway, andh) Operations are conducted in accordance with
AFM Supplement (Operations with AirplaneSystems Inoperative).
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11-2 HydraulicAccumulatorPressure Gauges(Systems 1, 2 and 3)
C 3 0 (M) All may be inoperative provided accumulatorprecharge is checked using a suitable gauge before thefirst flight of each day.
11-3 HydraulicAccumulators(Systems 1, 2 and 3)
B 3 1 Systems 1 and/or System 2 accumulator(s) may beinoperative.
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29 – HYDRAULIC POWER 4. Remarks or Exceptions
11-4 Hydraulic HeatExchanger CoolingFan(600, 601, 601-3A,601-3R)
C 1 0 May be inoperative provided ground operation ofhydraulic systems 1 and 2 is limited to 30 minuteswhen OAT is above 45 deg C.
11-5 Engine DrivenHydraulic Pumps(604, 605, 650)
B 2 1 (M) One may be inoperative provided:a) All other hydraulic pumps are operative,b) Hydraulic AC Motor Pump (ACMP) 1B and 2B
are selected ON before each flight,c) Both Integrated Drive Generators (IDG) are
operative,d) Affected pump is mechanically removed and a
blanking plate is installed, ande) Operations are conducted in accordance with
AFM Supplement (Operations with AirplaneSystems Inoperative).
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11-6 Hydraulic “AUTO”Switches(Electric Pumps)(604, 605, 650)
C 3 0 Any or all may be inoperative provided the affectedpumps are manually selected on before take-off andlanding.
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11-7 Return ManifoldFilter – DifferentialPressure Indications
A 3 0 (M) Any or all may be inoperative provided:a) Filter element is verified free of any
contaminant, andb) Repairs are made within three flight days.
12-1 Hydraulic AC MotorPump (ACMP) 3A
C 1 0 May be inoperative provided:a) 3B pump is operated continuously throughout
the flight, andb) All other hydraulic pumps (engine driven and
electrical) are operative.
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29 – HYDRAULIC POWER 4. Remarks or Exceptions
31-1 Hydraulic PressureIndicators (Cockpit)(600, 601, 601-3A,601-3R)
C 3 2 One may be inoperative provided:a) All four Electric Motor Driven Hydraulic Pumps
are operative,b) Associated Hydraulic Pump Low Pressure
(ELECT PUMP or L/R ENG PUMP) CautionLights are operative,
c) Associated Hydraulic Pump HI TEMP CautionLight is operative, and
d) Brake Pressure Indicator is operative.
31-2 Hydraulic ReservoirQuantity Indicators(Systems 1, 2 and 3)(Cockpit)(600, 601, 601-3A,601-3R)
C 3 0 One or more may be inoperative provided:a) Affected reservoir quantity is confirmed within
limits prior to each flight,b) Associated Hydraulic Pressure Indicator is
operative,c) Associated Hydraulic Pump Low Pressure
(ELEC PUMP or L/H ENG PUMP) CautionLights are operative, and
d) Associated Hydraulic HI TEMP Caution Light isoperative.
31-3 EICAS HydraulicPressure ReadoutIndications(604, 605, 650)
C 3 0 (O) Any or all may be inoperative provided theassociated pressure switches are operative.
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32-1 EICAS HydraulicReservoir QuantityReadouts(Systems 1, 2 and 3)(604, 605, 650)
C 3 0 (M) Any or all may be inoperative provided the quantityin the associated reservoir(s) is checked on thereservoir sight glass prior to each flight.
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29 – HYDRAULIC POWER 4. Remarks or Exceptions
34-1 Hydraulic Pump LowPressure Switches
C 6 3 One in each system may be inoperative providedassociated Hydraulic Pressure and Quantity IndicatingSystems are operative.
35-1 Hydraulic HI TEMPCaution Lights(Systems 1, 2 and 3)(600, 601, 601-3A,601-3R)
C 3 2 (M) One may be inoperative provided:a) Associated Hydraulic Pressure Indicator is
operative,b) Associated Hydraulic Reservoir Quantity
Indicator is operative, andc) Hydraulic Heat Exchanger Cooling Fan is
operative.
37-1 Hydraulic Pump LowPressure CautionLights (light functiononly) (ELEC PUMP,L ENG PUMP, RENG PUMP) (600,601, 601-3A,601-3R)
C 6 3 One per system may be inoperative provided:a) Associated Hydraulic Pressure Indicator is
operative,b) Associated Hydraulic Reservoir Quantity
Indicator is operative, andc) Associated Hydraulic HI TEMP Caution Light is
operative.
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30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
12-1 Wing Anti-ice System
1) Auto Control(600)
C 1 0 (M) May be inoperative provided Wing Anti-ice SystemManual Control is operative.
B 1 0 May be inoperative provided:a) Both Ice Detection Systems are operative, andb) Flight is not conducted in known or forecast
icing conditions.
2) Manual Control(600)
C 1 0 May be inoperative provided Wing Anti-ice SystemAuto Control is operative.
B 1 0 May be inoperative provided:a) Both Ice Detection Systems are operative, andb) Flight is not conducted in known or forecast
icing conditions.
3) Normal Control(601)(601-3A, 601-3Rwith SB 601-0575)(604 with SB604-30-002 andaircraft S/N 5583and subsequent)(605, 650)
C 1 0 (M) May be inoperative provided Wing Anti-ice SystemStandby Control is operative.
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C 1 0 May be inoperative provided:a) Both Ice Detection Systems are operative, andb) Flight is not conducted in known or forecast
icing conditions.4) Normal Control
(601-3A,601-3R without SB601-0575)
(604 without SB604-30-002)
(Cont'd)
B 1 0 May be inoperative provided:a) Both Ice Detection Systems are operative, andb) Flight is not conducted in known or forecast
icing conditions.
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
12-1 Wing Anti-iceSystem
(Cont'd)
5) Standby Control(601, 601-3A,601-3R, 604,605, 650)
C 1 0 May be inoperative provided Wing Anti-ice SystemNormal Control is operative.
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B 1 0 May be inoperative provided:a) Both Ice Detection systems are operative, andb) Flight is not conducted in known or forecast
icing conditions.
12-2 Wing Anti-iceSystem Modulatingand Shut-off Valves
B 2 0 One or both may be inoperative CLOSED provided:a) Both Ice Detection Systems are operative, andb) Flight is not conducted in known or forecast
icing conditions.
12-3 Lower Bleed AirIsolation Valve(600)
C 1 0 May be inoperative OPEN.
B 1 0 May be inoperative CLOSED provided:a) Both Ice Detection Systems are operative, andb) Flight is not conducted in known or forecast
icing conditions.
12-4 14th Stage EngineBleed Air IsolationValve(601, 601-3A,601-3R, 604, 605,650)
C 1 0 May be inoperative OPEN.
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B 1 0 May be inoperative CLOSED provided:a) Both Ice Detection Systems are operative, andb) Flight is not conducted in known or forecast
icing conditions.
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
20-1 Engine Cowl Anti-Ice PressureRegulating andShutoff Valves
B 2 1 (M) One may be inoperative provided:a) Affected valve is secured closed,b) Both Ice Detection Systems are operative,c) Associated ACU is selected ON above FL 400,
andd) Flight is not conducted in known or forecast
icing conditions.
20-2 Engine Cowl Anti-Ice Pressure ReliefBlow-off Valves1) (601, 601-3A,
601-3R)C 2 1 One may be inoperative OPEN provided:
a) Associated Thrust Reverser is operative,b) Associated Bleed Air 14th Stage SOV is
operative, andc) Operations are conducted in accordance with
AFM Supplement 14, Operations with AirplaneSystems Inoperative.
2) (604, 605, 650) C 2 1 One may be inoperative OPEN provided:a) Associated Thrust Reverser is operative,b) Associated Bleed Air 14th Stage SOV is
operative, andc) Operations are conducted in accordance with
AFM Supplement 8, Operations with AirplaneSystems Inoperative.
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31-1 Probe Heaters
1) Pitot Probes B 2 1 (M) Except for RVSM Operations, one may beinoperative provided:
a) Both Ice Detection Systems are operative,b) Flight is not conducted in known or forecast
icing conditions or visible moisture,c) Aircraft is operated in day VMC only, andd) Standby Pitot Probe Heater is operative.
(Cont'd)
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30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
31-1 Probe Heaters(Cont’d)
2) Static Probes B 2 1 (M) Except for RVSM Operations, one may beinoperative provided:
a) Both Ice Detection Systems are operative,b) Flight is not conducted in known or forecast
icing conditions or visible moisture, andc) Aircraft is operated in day VMC only.
3) Standby PitotProbe(604, 605, 650)
C 1 0 (M) Except for RVSM Operations, may be inoperativeprovided:
a) Both Ice Detection Systems are operative,b) Flight is not conducted in known or forecast
icing conditions or visible moisture,c) Aircraft is operated in day VMC only, andd) Both Pitot Probes Heaters are operative.
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4) TAT Probe B 1 0 (M) May be inoperative provided:a) Both Ice Detection Systems are operative,b) Flight is not conducted in known or forecast
icing conditions or visible moisture, andc) Aircraft is operated in day VMC only.
5) Angle of AttackVanes
B 2 1 (M) One may be inoperative provided:a) Both Ice Detection Systems are operative,b) Flight is not conducted in known or forecast
icing conditions or visible moisture, andc) Aircraft is operated in day VMC only.
6) AUX Angle ofAttack VaneHeater(604, 605, 650)
B 1 0 (M) May be inoperative provided:a) Both Ice Detection Systems are operative,b) Flight is not conducted in known or forecast
icing conditions or visible moisture, andc) Aircraft is operated in day VMC only.
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3. Number Required For Dispatch
30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
31-2 Speed CommandAttitude Thrust(SCAT) VaneHeaterSTC SA4770SW***
C 1 0 (M) May be inoperative provided:a) SCAT Vane Heater is deactivated, andb) Airplane is not operated in known or forecast
icing conditions.
41-1 Windshield and SideWindow Anti-IceControllers
C 4 3 One may be inoperative provided:a) Operations are not conducted in known or
forecast icing conditions, andb) Pilot’s (Left) side window heating is operative.
C 4 2 Two may be inoperative provided:a) Operations are not conducted in known or
forecast icing conditions,b) Pilot’s (Left) side window heating is operative,
andc) Both Ice Detection Systems are operative.
41-2 Enhanced VisionSystem - IceProtection(605 withSB 605-31-002 andSB 605-34-010) ***(650 withSB 650-31-002 andSB 650-34-006) ***1) EVS Fairing & IR
Window heat DE-ICE / ANTI-ICEfunctions
C 2 0 (M)(O) One or both may be inoperative provided:a) EVS Ice Protection is deactivated,b) Operations are not conducted in known or
forecast icing conditions,c) One ice detection system is operative, andd) If installed, the EVS is not used when the image
is affected.
NOTE : With IR Window heat inoperative, theimage may degrade in high humidityconditions, to the point of disappearance,as IR Window misting increases. The EVSmust not be used if the image is affected.
(Cont’d)
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1. 2. Number InstalledSystem & Sequence No Item
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30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
41-2 Enhanced VisionSystem - IceProtection(605 withSB 605-31-002 andSB 605-34-010) ***(650 withSB 650-31-002 andSB 650-34-006) ***(Cont’d)
1) EVS Fairing & IRWindow heat DE-ICE / ANTI-ICEfunctions(Cont’d)
D 2 0 (M)One or both may be inoperative provided:a) The IR Window and EVS fairing are removed
as an assembly and replaced with an approvedblanking plate, and
b) If installed, the EVS system (STC) isconsidered inoperative.
2) IR Window -DE-MISTfunction
C 1 0 May be inoperative provided EVS image (if installed) isnot affected.
NOTE : The image may degrade in high humidityconditions, to the point of disappearance,as IR Window misting increases. The EVSmust not be used if the image is affected.
D 1 0 May be inoperative provided:a) if installed, the EVS system (STC) is
considered inoperative,b) The EVS system de-ice and anti-ice functions
operate normally, andc) Routine procedures do not require the use of
EVS system.
(Cont’d)
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1. 2. Number InstalledSystem & Sequence No Item
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30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
41-2 Enhanced VisionSystem - IceProtection(605 withSB 605-31-002 andSB 605-34-010) ***(650 withSB 650-31-002 andSB 650-34-006) ***(Cont’d)
2) IR Window -DE-MISTfunction(Cont’d)
D 1 0 (M) May be inoperative provided:a) The IR Window and EVS fairing are removed
as an assembly and replaced with an approvedblanking plate, and
b) If installed, the EVS system (STC) isconsidered inoperative.
3) EVS FairingTemperatureSensors
D 2 1 One may be inoperative.
C 2 0 (M)(O) Both may be inoperative provided:
a) EVS Ice Protection is deactivated,b) Operations are not conducted in known or
forecast icing conditions, andc) One ice detection system is operative.
D 2 0 (M) Both may be inoperative provided:a) The IR Window and EVS fairing are removed
as an assembly and replaced with an approvedblanking plate, and
b) If installed, the EVS system (STC) isconsidered inoperative.
(Cont’d)
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
41-2 Enhanced VisionSystem - IceProtection(605 withSB 605-31-002 andSB 605-34-010) ***(650 withSB 650-31-002 andSB 650-34-006) ***(Cont’d)
4) IR WindowTemperatureSensors
D 2 1 One may be inoperative.
C 2 0 (M)(O) Both may be inoperative provided:a) EVS Ice Protection is deactivated,b) Operations are not conducted in known or
forecast icing conditions,c) One ice detection system is operative, andd) If installed, the EVS is not used when the
image is affected.
NOTE : With IR Window heat inoperative, theimage may degrade in high humidityconditions, to the point of disappearance,as IR Window misting increases. The EVSmust not be used if the image is affected.
D 2 0 (M) Both may be inoperative provided:a) The IR Window and EVS fairing are removed
as an assembly and replaced with an approvedblanking plate, and
b) If installed, the EVS system (STC) isconsidered inoperative.
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30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
80-1 Ice DetectionSystems
C 2 1 (M) One may be inoperative provided:a) Affected ice detector is deactivated.b) Anti-ice systems are turned ON when icing
conditions exist as defined in AFM.
A 2 0 Both may be inoperative provided:a) Flight is not conducted in known or forecast
icing conditions, andb) Repairs are made within one flight day.
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30 – ICE AND RAIN 4. Remarks or Exceptions PROTECTION
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
14-1 Master WarningSwitch Lights(Glareshield)(light function only)(604)
C 2 1
14-2 Master Caution SwitchLights (Glareshield)(light function only)(604)
C 2 1
14-3 MasterWarning/CautionPushbuttonAnnunciators(Glareshield)(605, 650)
C 2 1
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1) Warning Lights(light functiononly)
C 2 1
2) Caution Lights(light functiononly)
C 2 1
21-1 Clock C - 0 May be inoperative provided an accurate timepiece isoperative in the flight crew compartment indicating thetime in hours, minutes and seconds.
1) Universal TimeCo-ordinationDisplay (UTC)(605, 650)
C 1 0
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2) Flight Time (FT)(605, 650)
C 1 0|
3) Chronometer(CHR)(605, 650)
C 1 0 (O) May be inoperative provided alternate proceduresare established and used to determine elapsed time.
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4) LCD DisplaySegments / Mode(Annuns.)(605, 650)
C - - Individual segments or annunciations may beinoperative provided flight crews can readily determinemode of operation.
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1. 2. Number InstalledSystem & Sequence No Item
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31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
31-1 Flight DataRecorder (FDR)
A - 0 May be inoperative provided:a) The aircraft does not exceed 8 further
consecutive flights with the FDR inoperative,and
b) A maximum of 72 hours have elapsed since theFDR was found to be inoperative, and
c) Any Cockpit Voice Recorder required to becarried is operative.
NOTE: The flight data recorder is considered to beinoperative when any of the followingconditions exist:(i) Loss of the flight recording function is
evident to the flight crew during the pre-flight check, e.g. by means of a systemstatus monitor; or
(ii) The need for maintenance has beenidentified by the system monitors, whereavailable, and the failure origin has notbeen identified; or
(iii) Analyses of recorded data ormaintenance actions have shown thatmore than 5 % of the total number ofindividual parameters (variable anddiscrete) required to be recorded for theparticular aircraft, are not beingrecorded properly.
A - 0 Up to 5% of the required parameters may beinoperative for a maximum of 90 calendar days or untilthe next maintenance inspection, whichever occursfirst.
D - - Any in excess of those required may be inoperativeprovided the FDR parameters are not required formonitoring purpose.
(Cont’d)
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31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
40-1 Cursor Control Panel(CCP)(605, 650)
C 2 1 (O) Right side may be inoperative.
|1) Joystick C 2 1
C 2 0 May be inoperative provided:a) Maintenance Diagnostic Computer is
considered inoperative,b) If installed, Graphical Weather function is
considered inoperative, andc) If installed, Electronic Charts are considered
inoperative.
2) JSTKPushbuttons
C 2 0
3) MEMPushbuttons
D 6 0
4) CHARTPushbuttons
C 2 1
C 2 0 May be inoperative provided Electronic Charts, ifinstalled, are considered inoperative.
5) ZOOMPushbuttons
C 2 1
C 2 0 May be inoperative provided:a) Maintenance Diagnostic Computer is
considered inoperative,b) If installed, Graphical Weather function is
considered inoperative, andc) If installed Electronic Charts are considered
inoperative.
(Cont’d)
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3. Number Required For Dispatch
31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
40-1 Cursor Control Panel(CCP)(605, 650) |
6) OrientPushbuttons(located under theCHARTpushbutton)
C 2 1
C 2 0 May be inoperative provided:a) Maintenance Diagnostic Computer is
considered inoperative,b) If installed, Graphical Weather function is
considered inoperative, andc) If installed, Electronic Charts are considered
inoperative.
7) LWR FRMTPushbuttons
C 2 0
8) UPR MENUPushbuttons
C 2 1
9) LWR MENUPushbuttons
C 2 1 (O) One may be inoperative.
10) ESC Pushbuttons C 2 0
11) PUSH SELECTPushbuttons(Menu)
C 2 1
12) MENU ADV knobs C 2 1
13) DATA knobs(Menu)
C 2 1
14) TFC Pushbuttons
C 2 0
15) TR/WXPushbuttons
C 2 0
(Cont’d)
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31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
40-1 Cursor Control Panel(CCP)(605, 650)(Cont'd)
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16) SUMRYPushbuttons
C 2 0
17) AC ELECPushbuttons
C 2 0
18) HYD Pushbuttons C 2 0
19) DC ELECPushbuttons
C 2 0
20) FLTPushbuttons
C 2 0
21) CAS Pushbuttons C 2 1 Right side may be inoperative
22) RADIOPushbuttons
C 2 1
23) FREQPushbuttons
C 2 1
24) 1/2 Pushbuttons
C 2 1
25) DME-HPushbuttons
C 2 1
26) IDENTPushbuttons
C 2 1
27) ATCPushbuttons
C 2 1
(Cont’d)
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31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
40-1 Cursor Control Panel(CCP)(605, 650)(Cont'd)
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28) PUSH SELECTPushbuttons(Radio)
C 2 1
29) RADIO ADVknobs
C 2 1
30) DATA knobs(Radio)
C 2 1
41-1 EICAS Control Panel(ECP) DiscreteButtons(604)1) Without
SB 604-34-033a) CKLST B 1 0b) RCL B 1 0c) EMER B 1 0d) HYD B 1 0e) ELEC B 1 0f) UP B 1 0g) DN B 1 0h) SKP B 1 0i) F/CTL B 1 0j) Joystick B 1 0 May be inoperative provided UP and DN Discrete
Buttons are operative.
(Cont’d)
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31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
41-1 EICAS ControlPanel (ECP)Discrete Buttons(604)(Cont’d)2) With
SB 604-34-033a) CKLST B 1 0b) RCL B 1 0c) EMER B 1 0d) HYD B 1 0e) ELEC B 1 0f) UP/PLAN B 1 0g) DN/SIDE B 1 0h) SKP/3D B 1 0i) F/CTL B 1 0j) Joystick B 1 0 May be inoperative provided UP/PLAN and DN/SIDE
Discrete Buttons are operative.
41-2 Data ConcentrationUnit (DCU)(604)
C - 2 (O) Any in excess of two may be inoperative provided:a) Associated AUDIO WARNING DISABLE
switch is selected, andb) Two separate audio warning channels are
verified operative before each flight.
NOTE 1 : In the event of a DCU 1 failure, both pilots’Master Warning and Master Caution lightswill not test during the lamp 1 test.
NOTE 2 : In the event of a DCU 2 failure, both pilots’Master Warning and Master Caution lightswill not test during the lamp 2 test.
NOTE 3 : Aircraft without SB 604-31-003 installed:In the event of either a DCU 1 or 2 failure, asubsequent TRU 2 failure will generate one"HOT" icon ITT engine indication. This iconshould be disregarded and the ITTmonitored.
(Cont’d)
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31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
50-1 Auto CB Fail Light(10-ChannelAnnunciator)(600, 601, 601-3A,601-3R)
B 1 0 May be inoperative provided the BRT / DIM function onthe 10-channel annunciator panel is confirmedoperative prior to each flight.
50-2 Voice AdvisorySystem(600, 601, 601-3A, 601-3R) ***
C - 0 (M)(O) May be inoperative provided:a) System is secured, andb) Alternate procedures are established and
used.
D - 0 (M) May be inoperative provided:a) System is secured, andb) Routine procedures do not require its use.
50-3 Angle of AttackIndication System(Speed CueIndexer)(600, 601, 601-3A,601-3R)***
C - 0 (M)(O) May be inoperative provided:a) System is deactivated, andb) Alternate procedures are established and
used.
50-4 Speed CommandAttitude Thrust(SCAT) System(600, 601, 601-3A,601-3R)***
C - 0 (O) May be inoperative provided alternate proceduresare established and used.
D - 0 (M) May be inoperative provided:
a) System is secured, andb) Routine procedures do not require its use.
50-5 Canadian MarconiCorp Omega NavStatus DisplaySystem WARNINGRepeater lights(600)***
D 2 1 (M) May be inoperative provided:a) Light is not illuminated, andb) All individual warning lights are operative.
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31 – INDICATING/ 4. Remarks or ExceptionsRECORDING SYSTEMS
61-1 Display Units
1) (604)A/C withoutSB 604-34-031)
B 6 5 EICAS display unit 1 or 2 may be inoperative providedthe display reversionary mode selector switches areoperative.
2) (604)For A/C 5500and up or withSB 604-34-031installed
B 6 5 (O) EICAS display unit 1 or 2 may be inoperativeprovided the display reversionary mode selectorswitches are operative.
61-2 Adaptive FlightDisplays(AFD)(605, 650)
B 4 3 (O) Right Inboard Display may be inoperative provided:a) Two Control Display Units are operative, andb) Unaffected displays reversion capabilities are
verified operative before the first flight of theday.
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
32 – LANDING GEAR 4. Remarks or Exceptions
30-1 Landing Gear SelectorHandle Anti-RetractionMechanism
C 1 0 (M) May be inoperative in the LOCKED position (down)provided the downlock release mechanism is operative.
30-2 Landing GearRetraction System(604, 605, 650)
A 1 0 (M) May be inoperative provided:a) Operations are conducted in accordance with
AFM Supplement 6 (Flight with Landing GearDown)
b) Operations are not conducted in known orforecast icing conditions,
c) Ground lock pins are installed to ensure allthree landing gears are locked downthroughout flight,
d) In-flight performance information given in theFlight Crew Operating Manual (FCOM), isused,
e) Extended overwater operations areprohibited,
f) Both pilot headsets are worn,g) Flight Compartment and Cabin Interphone
Systems are operative,h) Both Flap Power Drive Units (27-50-1) are
Operative,i) CAT II operations are prohibited, andj) Repairs are made within one flight day.
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43-1 Brake AccumulatorPressure Gauges
C 2 0 (M) One or both may be inoperative provided theaccumulator pre-charge pressure is checked using asuitable pressure gauge before the first flight of eachday.
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32 – LANDING GEAR 4. Remarks or Exceptions
43-2 Brake PressureIndications(600, 601, 601-3A,601-3R)
C 2 0 (M) One or both may be inoperative provided:a) Brake accumulator(s) nitrogen pressure is
checked prior to the first flight of each day,b) Capability of brake accumulators to retain
adequate hydraulic fluid for brakes is verifiedprior to the first flight of each day, and
c) Hydraulic Pressure Indication is operative.
44-1 Anti-Skid SystemChannels(604, 605, 650)
B 2 1 (M) Either the inboard or the outboard channel may beinoperative provided:
a) Inoperative channel is deactivated,b) Anti-skid is selected ON for take-off and
landing,c) Nosewheel Steering is operative,d) Ground Spoilers are operative,e) Both Thrust Reversers are operative,f) Operations are conducted in accordance with
AFM Supplement 8, Operations with AirplaneSystems Inoperative.
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45-1 Parking Brake Light(600, 601, 601-3A,601-3R)
C 1 0 (O) May be inoperative provided the amber anti-skidfail lights INBD FAIL and OUTBD FAIL illuminate as theparking brake is set.
47-1 EICAS Brake PressureIndications(604, 605, 650)
C 2 0 (M) One or both may be inoperative provided:a) Brake accumulator(s) nitrogen pressure is
checked prior to the first flight of the day,b) Capability of brake accumulators to retain
adequate hydraulic fluid for brakes is verifiedprior to the first flight of the day, and
c) Hydraulic Pressure Indication is operative.
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32 – LANDING GEAR 4. Remarks or Exceptions
50-1 Nosewheel SteeringSystem
C 1 0 (M) May be inoperative provided:a) Nosewheel steering system is selected off,b) Nose landing gear solenoid selector valve is
not failed open,c) Nosewheel is confirmed to be in a free-
castoring mode,d) Crosswind limit is 20 kts for take-off and
landing,e) Take-off and accelerate-stop distances are
increased by 2 %,f) Accelerate-stop distance available and runway
length available are reduced by 2 % whendetermining the AFM fields length limited take-off weight and V1 speed, and
g) Take-off or landing is not conducted on acontaminated runway.
NOTE 1 : Care should be taken when operating incongested areas, or on contaminatedsurfaces when using asymmetric thrust.
NOTE 2 : Excessive use of brakes may lead to fuseplug failure(s).
50-2 Remote Nose GearDoor ReleaseMechanism(Additional Handleand cablemechanism)***
D 1 0 (M) May be inoperative in the “DOOR CLOSED”position provided:
a) Mechanism is verified to be in the “DOORCLOSED” position, and
b) Actuator arm is secured in the “DOORCLOSED” position.
D 1 0 (M) May be inoperative in the “DOOR CLOSED”position provided:
a) Mechanism is verified to be in the “DOORCLOSED” position, and
b) Actuator arm is removed from the nose wheelwell fitting.
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3. Number Required For Dispatch
32 – LANDING GEAR 4. Remarks or Exceptions
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3. Number Required For Dispatch
33 – LIGHTS 4. Remarks or Exceptions
12-1 Lighting ControlPanels(Center Pedestal &L/R Facia Panels)(600, 601)1) Floodlight
System
a) BRT/DIMSystems
C 3 0 Any or all may be inoperative provided:a) BRT/DIM switch is selected to OFF position,
andb) Brightening System is operative.
C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
b) BrighteningSystems
C 3 0 Any or all may be inoperative provided the associatedBRT/DIM system is operative.
C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
2) InstrumentBrighteningSystems
C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
3) Floor LightSystems
C 2 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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3. Number Required For Dispatch
33 – LIGHTS 4. Remarks or Exceptions
12-2 Lighting ControlPanels(Center Pedestal &L/R Facia Panels)(601-3A, 601-3R)
1) FloodlightSystem
a) BRT/DIMSystems
C 3 0 Any or all may be inoperative provided:a) BRT/DIM switch is selected to OFF position,
andb) Brightening System is operative.
C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
b) BrighteningSystems
C 3 0 Any or all may be inoperative provided the associatedBRT/DIM system is operative.
C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
2) InstrumentBrighteningSystems
C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
(Cont'd)
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3. Number Required For Dispatch
33 – LIGHTS 4. Remarks or Exceptions
12-2 Lighting ControlPanels(Center Pedestal &L/R Facia Panels)(601-3A, 601-3R)(Cont’d)
3) DigitsBrighteningSystem
C 1 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
4) Floor LightSystems
C 2 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
12-3 PBA BRT/DIMSystem(10-ChannelAnnunciator Panel)(600, 601,601-3A,601-3R)
C 1 0 May be inoperative provided the DIM mode is operativefor night operations.
C 1 0 May be inoperative provided the BRT mode isoperative for day operations.
12-4 OverheadInstrument PanelBrightening System
C 1 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
flight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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3. Number Required For Dispatch
33 – LIGHTS 4. Remarks or Exceptions
12-5 Lighting ControlPanels(Center Pedestal)(604, 605, 650) |
1) FloodlightBrighteningSystems(604, 605, 650)
C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
flight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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2) IntegratedBrighteningSystems(604, 605, 650)
C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
flight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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3) DisplayBrighteningSystems
a) (604) C 3 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
flight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
b) PFD/MFDBrighteningSystems(605, 650)
C 4 0 May be inoperative provided:
a) Cockpit lighting and intensity is sufficient forflight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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(Cont'd)
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33 – LIGHTS 4. Remarks or Exceptions
12-5 Lighting ControlPanels(Center Pedestal)(604, 605, 650)(Cont'd)
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4) Floor LightSystems(604, 605, 650)
C 2 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
flight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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5) Circuit BreakerPanel BrighteningSystem(604)
C 1 0 May be inoperative provided:
a) Cockpit lighting and intensity is sufficient forflight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
6) Circuit BreakerLighting ON/OFFSwitch(605, 650)
C 1 0 May be inoperative provided:
a) Cockpit lighting and intensity is sufficient forflight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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12-6 Indicator (PBA)Lighting BRT/DIMSystem(604, 605, 650)
C 1 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
flight crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
33 – LIGHTS 4. Remarks or Exceptions
13-1 Cockpit andInstrument PanelLighting Systems(Excluding EFIS)
C - - Individual lights may be inoperative provideda) Sufficient lighting is operative to make each
required instrument, control, and other devicefor which it is provided easily readable, and
b) Sufficient flight crew compartment emergencylighting is operative, and
c) Lighting configuration at dispatch is acceptableto the flight crew.
14-1 Map Reading Lights
1) 600, 601,601-3A 601-3R,604
C 2 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
2) 605, 650 C 4 0 May be inoperative provided:a) Cockpit lighting and intensity is sufficient for
crewmembers to perform their dutiesthroughout flight, and
b) Ensure that direct rays are shielded from flightcrewmember’s eyes.
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20-1 PassengerCompartmentLighting
C - - Individual lights may be inoperativeprovided:
a) Lighting is acceptable for the crew located inthe cabin to perform their required duties, and
b) Inoperative lights are not part of the cabinemergency lighting.
D - 0 May be inoperative provided passengers are notcarried.
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3. Number Required For Dispatch
33 – LIGHTS 4. Remarks or Exceptions
20-2 Miscellaneous Lights
1) Boarding andDome Lights(604)
D - 0
2) Boarding andCabin Lights(605, 650)
D - 0
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20-3 Lavatory Vanity /Reading Lights
D - 0
20-4 Cabin Signs (‘FastenSeat Belt’, ‘NoSmoking’ Signs,Return to Cabin,NO PED)
C - - (M)/(O) One or more may be inoperative providedaffected passenger seats, crew member seats orlavatories from which at least one cabin sign is notreadily legible are blocked and placarded ‘DO NOTOCCUPY’.
C - - (O) One or more may be inoperative and the affectedpassenger seats, crew member seats or lavatories maybe occupied provided a procedure is used to notifypassengers as appropriate.
C - - May be inoperative provided passengers are notcarried.
1) Aural ToneFunction
C - 0 (O) May be inoperative provided a procedure isestablished and used to verify that visual indicationsare taken into account by passengers.
2) AutomaticFunction
C - 0 (O) May be inoperative provided:a) Manual control function is operative, andb) An alternate procedure is established and
used.
25-1 Push ButtonAnnunciators (Lightfunction only)(604, 605, 650)
B - - One lamp may be inoperative in each independentmodule provided the nomenclature remains legible
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33 – LIGHTS 4. Remarks or Exceptions
31-1 Service Lights D - 0
40-1 Position Lights(Navigation)1) Wing Tip Position
Light BulbsC 4 2 Two may be inoperative provided at least one bulb is
operative at each position.
C 4 0 All may be inoperative provided aircraft is not operatedat night.
2) Upper Aft PositionLight Bulb
C 1 0 May be inoperative provided Lower Aft Position Light isoperative.
C 1 0 May be inoperative provided aircraft is not operated atnight.
3) Lower Aft PositionLight Bulbsa) 600, 601,
601-3AC 2 1
C 2 0 Both may be inoperative provided Upper Aft PositionLight is operative.
C 2 0 Both may be inoperative provided aircraft is notoperated at night.
b) 601-3R,604, 605, 650
C 1 0 May be inoperative provided Upper Aft Position Light isoperative. |
C 1 0 May be inoperative provided aircraft is not operated atnight.
40-2 High Intensity orStrobe Light System
C 1 0 May be inoperative provided an approved Anti-CollisionBeacon Light System is installed and operative.
D - 0 May be inoperative provided aircraft is not operated atnight.
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33 – LIGHTS 4. Remarks or Exceptions
40-3 Pulselight LandingLight System1) (600, 601, 601-3A,
601-3R, 604)***
C 1 0 (M) May be inoperative provided affected system isdeactivated.
40-4 Logo LightSystem***
D - 0
40-5 Taxi / RecognitionLights1) 600, 601 C 2 0 One or both may be inoperative provided both Landing
Lights are operative.
C 2 0 May be inoperative provided aircraft is not operated atnight.
2) 601-3A, 601-3R,604, 605, 650
C 2 0 One or both may be inoperative provided at least threeLanding Lights are operative. |
C 2 0 May be inoperative provided aircraft is not operated atnight.
42-1 Anti-Collision LightSystem
1) Fuselage Lights(Beacon or StrobeType)
NOTE: If the fuselage anti-collision light isinoperative, alternate procedures areestablished and used when the aircraft is onthe ground with engine(s) running.
C - 1 (O) Either the upper or the lower fuselage lights may beinoperative provided all white wing-tip strobe lights areoperative.
C - 0 (O) May be inoperative for daylight operations providedall white wing-tip strobe lights are operative.
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33 – LIGHTS 4. Remarks or Exceptions
43-1 Wing IlluminationLight
B 2 0 (O) One or both may be inoperative provided a portablelamp/light of adequate capacity for wing and/or controlsurface inspection is available and used for nightoperations in icing conditions.
C 2 0 One or both may be inoperative provided operationsare not conducted at any time into known or forecasticing conditions.
C 2 0 One or both may be inoperative provided ground de-icing procedures do not require their use.
D 2 0 One or both may be inoperative for daylight operations.
44-1 Landing Lights1) 600, 601 B 2 1 One may be inoperative provided both Taxi /
Recognition Lights are operative.
C 2 0 One or both may be inoperative for daylight operations.
2) 601-3A, 601-3R,604, 605, 650
C 4 3|
B 4 1 Two or three may be inoperative provided both Taxi /Recognition Lights are operative.
C 4 0 All may be inoperative for daylight operations.
3) Pulse LightFunction(605, 650)
C 2 0 (M) May be inoperative provided Pulselight circuitbreaker is pulled and collared.
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50-1 Exterior EmergencyLights
B 4 0 Any may be inoperative for daylight operations.
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33 – LIGHTS 4. Remarks or Exceptions
50-2 Cabin EmergencyLighting1) Overhead
EmergencyLighting (eachaisle)
B - - A maximum of one in four consecutive overheademergency lights (or light assemblies) may beinoperative
2) EXIT MarkingSigns
C - - Up to 50% of the bulbs/LEDs may be inoperative in oneor more signs provided the sign remains legible.
3) EXIT LocatorSigns
C - - Up to 50% of the bulbs/LEDs may be inoperative in oneor more signs provided the sign remains legible.
4) Floor ProximityLighting (Electricalor photoluminescentsystems)***
a) IndividualLights/strips
B - - Individual lights/strips may be inoperative providedcompliance is shown with minimum acceptable lightingas required by certification documents.
b) EXIT Markers/Identifiers
C - - Up to 50% of the bulbs/LEDs may be inoperative in oneor more signs provided the sign remains legible.
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33 – LIGHTS 4. Remarks or Exceptions
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34 – NAVIGATION 4. Remarks or Exceptions
10-1 Metric Altimeter(600, 601, 601-3A601-3R, 604)***
D 1 0
12-1 Mach Indications(600, 601)
B 2 1 (M) Pilot’s Mach Indicator may be inoperative providedthe remaining functions, IAS, Vmo and overspeed(aural) warning, Mach Trim, and TAS (read-out on theTAS/SAT/TAT indicator) are operative.
B 2 1 (M) Copilot’s Mach Indicator may be inoperativeprovided both Mach trim and aural warnings areoperative.
B 2 0 Both Mach Indicators may be inoperative providedmaximum altitude is limited to FL 320 and maximumairspeed is limited to 250 KIAS.
12-2 Copilot’s AltimeterVibrator(600, 601)
B 1 0 May be inoperative for day VMC provided the ATCtransponder # 1 is used to transmit altitude data to AirTraffic Control Stations.
12-3 Vmo Indicator(Barber Pole)(600, 601)
A 2 1 (M) One may be inoperative provided:a) Both Mach airspeed indicators are operative,b) Inoperative Vmo indicator is on non-flying pilot
side,c) Airspeed aural warning (clacker) is operative,
andd) Repairs are made within ten flight hours.
12-4 Mach AirspeedIndicators (MASIs)(601-3A, 601-3R)
B 2 1 (M) Copilot’s (right) MASI may be inoperative providedthe Standby Airspeed Indicator is operative.
B 2 1 (M) Either MASI may be inoperative provided:a) Cross-side MASI is operative, andb) Air Data Computer is operative.
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34 – NAVIGATION 4. Remarks or Exceptions
12-4 Mach AirspeedIndicators (MASIs)(601-3A, 601-3R)(Cont’d)
B 2 0 Both MASIs may be inoperative provided:a) Maximum altitude is limited to
FL 320, andb) Maximum airspeed is limited to
250 KIAS.
12-5 Standby AirspeedIndicator(600, 601 ***)(601-3A, 601-3R,604)
B 1 0 May be inoperative for day VMC.
12-6 Standby Altimeter(601-3A, 601-3R)
B 1 0 May be inoperative provided:a) Radio Altimeter is operative, andb) Flight is conducted in day VMC.
12-7 Integrated StandbyInstrument System(ISIS)(600, 601, 601-3A, 601-3R, 604) ***(605, 650) |
1) Nav Function C 1 0
2) AttitudeFunction
B 1 0 (M) May be inoperative provided:a) Operations are conducted in day VMC, andb) Instrument attitude display is covered.
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34 – NAVIGATION 4. Remarks or Exceptions
13-1 True Airspeed(TAS), Static AirTemperature (SAT),Total AirTemperature (TAT),Indicating Systems(600, 601, 601-3A,601-3R)
1) TAS Indication C 1 0 May be inoperative provided other required systems(FMS, OMEGA, etc) do not depend on TAS data.
2) SAT Indication C 1 0 May be inoperative provided:a) TAT is operative,b) Other required systems (FMS, OMEGA, etc)
do not depend on SAT data, andc) TAT/SAT conversion method is provided.
3) TAT Indication C 1 0 May be inoperative provided SAT is operative.
13-2 Vertical SpeedIndicators (VSIs)(600, 601, 601-3A,601-3R)
C 2 1 One may be inoperative provided the operative VSI onthe pilot’s in command side.
C 2 1 One may be inoperative for operations under day VMCprovided procedures do not require its use.
17-1 Altitude AlertingSystem
1) (600, 601,601-3A,601-3R,)
B - 0 (O) May be inoperative provided:a) An autopilot with an altitude hold and altitude
capture is operative, andb) Alternate procedures are established and
used.
(Cont’d)
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34 – NAVIGATION 4. Remarks or Exceptions
17-1 Altitude AlertingSystem(Cont’d)2) (604, 605, 650) B 2 0 (O) Except where enroute operations require its use,
may be inoperative provided:a) Autopilot with altitude hold and altitude capture
operates normally,b) Each crewmember side has the altitude tape
operative on the displays, andc) Alternate procedures are established and
used.
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D 2 1 One may be inoperative.
3) Aural Alert(604, 605, 650)
C 1 0 May be inoperative provided:a) Visual alert operates normally, andb) Auto-pilot with altitude hold and altitude
capture operates normally,
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4) Visual Alert(604, 605, 650)
C 1 0 May be inoperative provided:a) Aural alert operates normally, andb) Auto-pilot with altitude hold and altitude
capture operates normally,
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5) Visual Alert(600, 601,601-3A,601-3R)
C 1 0 May be inoperative provided auto-pilot with altitudehold and altitude capture operates normally:
20-1 Attitude ReferenceSystem Sensors(excludes Standby)(600, 601 ***)
C - 2 Any in excess of two may be inoperative provided:a) Operations are conducted under VFR, andb) Independent attitude indicating system is
operative and available at each pilot’s station.
NOTE: A secondary/standby indication cannot satisfythe above condition (b).
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34 – NAVIGATION 4. Remarks or Exceptions
21-1 InstrumentComparator Monitor(601)
C 1 0 May be inoperative provided approach minimums arenot dependent on its use.
21-2 Non-EFIS ADIAnnunciators /Displays(600, 601)
1) GlideslopePointers
B 2 0 One or both may be inoperative provided GlideslopePointers are operative on the adjacent HSI.
B 2 0 One or both may be inoperative provided proceduresare not dependent on their use.
2) LocalizerPointers
B 2 0 One or both may be inoperative provided LocalizerPointers are operative on the adjacent HSI.
B 2 0 One or both may be inoperative provided proceduresare not dependent on their use.
3) Pitch and RollCommand Bars
B 2 0 One or both may be inoperative provided approachminimums are not dependent on their use.
4) Radio AltimeterDisplay
C - - May be inoperative provided weather minimums oroperating procedures are not dependent on its use.
NOTE: Category II operation prohibited in thisconfiguration.
5) Rate of TurnIndicators(600, 601)
C 2 0 Both may be inoperative provided:a) Associated Turn and Slip-Skid indicators are
operative andb) Standby Attitude Indicator is operative.
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34 – NAVIGATION 4. Remarks or Exceptions
21-3 Non-EFIS HSIAnnunciators /Displays (600, 601)
1) BearingPointers
C 2 1 May be inoperative provided:a) A stabilised direction indication is operative on
the pilot’s-in-command side, andb) Magnetic/standby compass is operative.
B 2 1 (O) May be inoperative provided:a) Operations are conducted under day VFR,b) The stabilised direction indication is displayed
at each required pilot’s station, andc) Magnetic/standby compass is operative.
2) DistanceMeasuringEquipment(DME) Displays
C 2 0 As required by regulations.
3) GlideslopePointers
B 2 0 One or both may be inoperative provided GlideslopePointers are operative on the adjacent ADI.
B 2 0 One or both may be inoperative provided proceduresare not dependent on their use.
4) HeadingDisplays
B 2 1 One may be inoperative provided:a) Standby Compass is operative, andb) Adjacent RMI is operative.
5) LocalizerPointers
B 2 0 One or both may be inoperative provided LocalizerPointers are operative on the adjacent ADI.
B 2 0 One or both may be inoperative provided proceduresare not dependent on their use.
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22-1 Electronic FlightInstrument System(EFIS)(600, 601 ***)(601-3A, 601-3R)
1) SymbolGenerators
C 3 2 (O) One may be inoperative provided:a) EFIS displays at pilot’s and co-pilot’s stations
are independent, andb) Procedures are established to provide for loss
of the associated Multi-Function Display(MFD).
2) Multi-FunctionDisplay
C 1 0 May be inoperative provided:a) Procedures are not dependent on its use, andb) Weather Radar information is available at each
pilot’s station or the Weather Radar Systemmust be considered inoperative.
22-2 Turn Slip/SkidIndication(600, 601, 601-3A,601-3R)
C 2 1 One may be inoperative provided the operativeslip/skid indication is on the pilot’s in- command station.
23-1 Vertical NavigationSystem (VNAV)(600,601)
C 1 0 Except for RVSM Operations may be inoperative.
23-2 Inertial ReferenceSystems (IRSs)
1) 600, 601 *** C - 0 Except when enroute or terminal operations require itsuse, may be inoperative provided:
a) Independent attitude indication is selected ateach pilot’s station, and
b) Independent directional compass indication isselected at each pilot’s station.
2) (601-3A,601-3R, 604)
C - 2 Any in excess of two may be inoperative provided:a) Independent attitude indication is available at
each pilot’s station, andb) Independent directional compass indication is
available at each pilot’s station.(Cont'd)
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34 – NAVIGATION 4. Remarks or Exceptions
23-2 Inertial ReferenceSystems (IRSs)(Cont’d)
3) (605, 650) C - 2 Any in excess of two may be inoperative provided:a) Independent attitude indication is available at
each pilot’s station,b) Independent directional compass indication is
available at each pilot’s station, andc) Autothrottle system (22-30-1) is considered
inoperative when the left Inertial ReferenceSystem is inoperative.
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23-3 Inertial DisplaySystem(601-3A, 601-3R)
1) Inertial SystemDisplay Unit(ISDU)***
D - 0 (O) May be inoperative provided alternate procedure isestablished and used.
2) Lasertrak -NavigationDisplay Unit(NDU)***
D - 0 (O) May be inoperative provided alternate procedure isestablished and used.
23-4 Emergency BatteryPacks for BackupCOMM / NAV***
D - 0
23-5 IRS Back-upBatteries
1) 600, 601 *** D - 0
2) 601-3A, 601-3R C - 1 Any in excess of one may be inoperative providedaircraft is not operated more than 60 minutes from asuitable airport.
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34 – NAVIGATION 4. Remarks or Exceptions
25-1 DirectionalCompass SystemSensors (excludesStandby)
C - 2 Any in excess of two may be inoperative provided:a) Independent directional compass indicating
system is operative and available at eachpilot’s station, and
b) Affected switches are not operated in flight.
27-1 Magnetic Compass(Standby)
B 1 0 May be inoperative provided any combination of threegyro or INS (IRU) stabilized compass system areoperative.
B 1 0 May be inoperative provideda) Any combination of two Gyro or INS (IRU)
stabilized compass system are operative, andb) Aircraft is operated:
1. With dual independent navigationcapability, and
2. Under positive radar control by ATC duringthe enroute flight phase, or one of thenavigation systems is a TSO’d GPS whichprovided track information.
C 1 0 (O) May be inoperative for flights that are entirely withinareas of magnetic unreliability provided at least twostabilized directional gyro systems are installed,operative and, an appropriate navigation technique isestablished and used.
28-1 Standby AttitudeIndicator
1) 600, 601 B 1 0 May be inoperative provided flight is conducted in dayVMC.
2) 601-3A, 601-3R, 604
B 1 0 May be inoperative provided:a) Flight is conducted in day VMC, andb) Independent attitude indication is available at
each pilot’s station.
32-1 Head-up GuidanceSystems***
D 1 0 (M) May be inoperative provided procedures are notdependent on its use.
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34 – NAVIGATION 4. Remarks or Exceptions
32-2 Enhanced VisionSystem (EVS)STC SA10-63***
D - 0 (M) May be inoperative provided EVS is deactivated.
NOTE: Where the EVS image is adversely affected,the system is to be considered inoperative.
1) EVS Yoke Switch D - 0 May be inoperative provided EVS is consideredinoperative.
34-1 Synthetic VisionSystem (SVS)(including Database)(605***, 650)
D 1 0 (O) May be inoperative provided SVS is deactivated.
NOTE: SVS is considered inoperative if associateddatabase is out of date.
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40-1 Windshear AlertSystem***
C - 0
(If not required byregulation)
D - 0 (O) May be inoperative provided alternate proceduresare established and used.
40-2 Stormscope System***
D - 0
40-3 Lightning DetectionSystem (LDS)***
D - 0
41-1 Weather RadarSystem
C 1 0 May be inoperative provided no thunderstorm or otherpotentially hazardous weather conditions, regarded asdetectable with the airborne weather detection system,are forecasted along the route.
NOTE: The route corresponds to any point on theroute including diversions to reach alternateaerodromes required by the operational rules.
41-2 Weather RadarControl Panel(600,601,601-3A 601-3R, 604)
C 1 0 May be inoperative provided no hazardous weatherconditions or thunderstorms are forecast in the area ofthe planned route.
D - 1
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34 – NAVIGATION 4. Remarks or Exceptions
42-1 Radio AltimeterSystems
C - 0 (O) May be inoperative provided:a) Radio altitude data is either available to, or not
required by other required systems, andb) Approach minimums or operating procedures
are not dependent on its use.
NOTE 1 : Radio altitude data is required for Autopilot,Flight Director System, TCAS, GPWS(TAWS) and Autothrottle System (ATS).
NOTE 2 : (605, 650) (604 with ATS) ATS retard modenot available when pilot’s radio altimeter isinoperative.
NOTE 3 : EFIS COMP INOP (Caution) message mightbe displayed.
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42-2 Terrain Awarenessand WarningSystem (TAWS)
1) GPWS/TAWS A 1 0 May be inoperative for a maximum of 6 flights or 2calendar days, whichever occurs first.
C - 0 Any in excess of those required may be inoperative.
a) Modes1 to 4
B 4 0 One or more mode may be inoperative provided FLTAand PDA functions are operative.
b) Test Mode A 1 0 May be inoperative for a maximum of 6 flights or 2calendar days, whichever occurs first.
c) GlideslopeDeviation(Mode 5)
B - 0 May be inoperative.
C - 0 May be inoperative for day VMC only.
d) AdvisoryCallouts(Mode 6)***
C - 0 (O) May be inoperative provided:a) Low visibility approaches requiring the use of
affected callouts are not performed, andb) Alternate procedures are established and used.
NOTE: Check Flight Manual limitations for approachminima.
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(Cont’d)
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34 – NAVIGATION 4. Remarks or Exceptions
42-2 Terrain Awarenessand WarningSystem (TAWS)(Cont’d)
e) WindshearReactiveMode(Mode 7)***
B 1 0 (O) May be inoperative provided alternate proceduresare established and used
NOTE: Operator’s alternate procedures shouldinclude reviewing windshear avoidance andwindshear recovery procedures.
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C 1 0 (O) May be inoperative provided:a) Alternate procedures are established and used,
andb) Windshear Detection and Avoidance System
(Predictive) is operative.
2) Terrain System– ForwardLooking TerrainAvoidance(FLTA) andPrematureDescent Alert(PDA) Functions***
B 1 0 May be inoperative provided:a) Mode 1-4 are operative, andb) Approach procedures do not require its use.
3) Terrain Displays C - 1
B - 0
4) RunwayAwareness andAdvisory System(RAAS)(Includes SmartRunway / SmartLanding (SR/SL)functions(605***, 650))
C 1 0 (O) May be inoperative provided the RAAS system isselected OFF.
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34 – NAVIGATION 4. Remarks or Exceptions
43-1 Traffic CollisionAvoidance System(TCAS)TCAS II(605)(600, 601, 601-3A,601-3R, 604)***(Including TCASfunction of theTraffic SurveillanceSystem (TSS)(650))
A - 0 (M)(O) May be inoperative for a maximum of 10calendar days provided:
a) TCAS is deactivated, andb) Operating procedures do not require its use.
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C - - (M) Any in excess of those required may be inoperativeprovided it is deactivated.
1) CombinedTraffic Alert (TA)and ResolutionAdvisory (RA)Dual Displays
C 2 1 (O) May be inoperative on the pilot side monitoring’sside provided:
a) TA and RA elements and audio functions areoperative on the pilot flying’s side, and
b) TA and RA display indications are visible to thepilot monitoring.
2) RA DisplaySystems
C 2 1 (O) One may be inoperative on the pilot monitoringside.
C 2 0 (O) One or both may be inoperative provided:a) All Traffic Alert (TA) display elements and voice
command audio functions are operative,b) TA only mode is selected by the crew, andc) Operating procedures do not require its use.
3) TA DisplaySystem(s)
C - 0 (O) One or more may be inoperative provided:a) RA display and audio functions are operative,
andb) Operating procedures do not require its use.
TCAS I(600, 601, 601-3A,601-3R)***
1) TCAS DisplaySystem(s)
C - 0 May be inoperative provided all installed audiofunctions are operative.
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34 – NAVIGATION 4. Remarks or Exceptions
50-1 Long RangeNavigation Systems(OMEGA, LORAN,VLF, GPS, etc)(600, 601, 601-3A,601-3R, 604)***
C - - (O) One or more may be inoperative provided:a) The navigation systems required for each
segment of the intended flight route areoperative, and
b) Alternate procedures are established and used,where applicable.
50-2 Canadian MarconiONA-T16 StatusDisplay System(SDS)***
D - 0
51-1 VHF NavigationSystems (VOR /ILS)1) ILS B - 0 May be inoperative under IFR operations provided
approaches and missed approaches where navigationis based on ILS are not included in the flight plan.
D - 0 May be inoperative under VFR operations.
2) VOR C - - (O) One or more may be inoperative provided:a) The navigation systems required for each
segment of the intended flight route areoperative, and
b) Alternate procedures are established and used,where applicable.
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34 – NAVIGATION 4. Remarks or Exceptions
51-2 Marker BeaconSystems
C - 0 May be inoperative under IFR operations providedapproach procedures do not require marker fixes.
D - 0 May be inoperative under VFR operations.
51-3 NAV / COM / ADF /ATC System(600, 601 ***)(601-3A, 601-3R)1) Preselect Tuning C - 0 May be inoperative provided direct tuning mode is
operative.
2) MemoryChannels
C - 0 May be inoperative provided direct tuning mode isoperative.
51-4 Radio MagneticIndicators (RMIs)1) (600, 601) C 2 0 One or both may be inoperative provided both HSIs are
operative.
2) (601-3A, 601-3R)***
C - 0 May be inoperative provided both EHSIs are operative.
52-1 Automatic DirectionFinding (ADF)Systems
C - - (O) One or more may be inoperative provided:
a) The navigation systems required for eachsegment of the intended flight route areoperative, and
b) Alternate procedures are established andused, where applicable.
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34 – NAVIGATION 4. Remarks or Exceptions
53-1 Distance MeasuringEquipment (DME)Systems
C - - (O) One or more may be inoperative provided:a) The navigation systems required for each
segment of the intended flight route areoperative,
b) Alternate procedures are established andused, where applicable, and
c) FMS accuracy without DME update isacceptable for the intended operation(600, 601 ***)(601-3A, 601-3R, 604, 605, 650) |
53-2 DME RepeaterIndicators
D - 0
***
54-1 Air Traffic Control(ATC) Transponders)Mode A/C(Includes transponderfunction of TrafficSurveillance System(TSS)(650))
A - 0 May be inoperative for a maximum of 5 flights provided:a) Flight is conducted under VFR over routes
navigated by reference to visual landmarks,and
b) Permission is obtained from the Air NavigationService Provider(s) along the route or anyplanned diversion.
NOTE: Mode C function is required to be operative forRVSM operations.
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D - - Any excess of those required may be inoperative.
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34 – NAVIGATION 4. Remarks or Exceptions
54-2 ATC TransponderMode S(Includes transponderfunction of TrafficSurveillance System(TSS)(650))
C - 0 One or more may be inoperative provided permission isobtained from the Air Navigation Service Provider(s)when required for the intended flight route.
NOTE 1: An ATC transponder with an operativeMode S function is defined as atransponder which can provide, at least,Elementary Surveillance capability.
NOTE 2: Elementary Surveillance (ELS) capability(Mode S including Aircraft Identificationand Pressure Altitude Reporting) isrequired in European Mode S designatedairspace.
NOTE 3: Altitude reporting, provided by an ATCtransponder Mode S function, is requiredfor TCAS II operation. Refer to item 34-40for flight with TCAS II inoperative.
NOTE 4: Altitude reporting, provided by an ATCtransponder Mode S function, is requiredfor flight into RVSM airspace.
||||||
D - - Any in excess of those required for the intended flightroute, may be inoperative.
Note: An ATC transponder with an operative Mode Sfunction is defined as a transponder which can provide,at least, Elementary Surveillance capability.
1) EnhancedSurveillanceFunctionsa) Elementary
and EnhancedDownlinkAircraftParameters(604 withSB604-34-040 orSB604-34-041)(605, 650)
C - 0 One or more Downlinked Aircraft Parameters (DAPs),which provide Enhanced Surveillance, may beinoperative when required for the intended flight route.
NOTE: Mode C function is required to be operative forRVSM operations.
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34 – NAVIGATION 4. Remarks or Exceptions
54-2 ATC TransponderMode S(Cont’d)
1) EnhancedSurveillanceFunctions(Cont’d)
a) ElementaryandEnhancedDownlinkAircraftParameters(604 withSB604-34-040orSB604-34-041)(605, 650)(Cont’d)
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D - 0 One or more Downlinked Aircraft Parameters (DAPs),which provide Enhanced Surveillance, may beinoperative when not required for the intended flightroute.
2) Extended Squitter(ADS-B OUT)Transmissiona) ADS-B
SquitterTransmissions(604 withSB 604-34-058and605 withSB 605-34-013) orSB605-34-030)(650)
C - 0 One or more extended squitter transmissions may beinoperative when required for the intended flight route.
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(Cont’d)
D - 0 One or more extended squitter transmissions may beinoperative when not required for the intended flightroute.
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34 – NAVIGATION 4. Remarks or Exceptions
54-3 Remote TransponderIdent Buttons***
D - 0 (M) All may be inoperative provided:a) IDENT button had not faulted to the ON
condition, andb) IDENT button on Transponder Control Unit /
RTU is operative.
60-1 Datanav System***
D - 0
60-5 Global PositioningSystem (GPS)(605, 650)
C 2 0 (O) One or both may be inoperative provided:a) The navigation systems required for each
segment of the intended flight route areoperative, and
b) Alternate procedures are established and used,where applicable.
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D 2 0 May be inoperative provided:a) Operations are conducted under VFR, andb) Applicable airspace requirements are complied
with.
61-1 Flight ManagementSystems (FMS)
1) (600, 601)***
C - 0 (O) Except when operations require its use, may beinoperative provided alternate procedures areestablished and used.
2) (601-3A, 601-3R) C - 1 Except when enroute operations require dual FMS use,any in excess of one may be inoperative.
3) (604 withoutSB 604-34-031)
C - 1 Except when enroute operations require dual FMS use,any in excess of one may be inoperative.
NOTE: Autothrottle system is consideredinoperative when the FMS No. 1 isinoperative (604 with autothrottle system).
(Cont'd)
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34 – NAVIGATION 4. Remarks or Exceptions
61-1 Flight ManagementSystems (FMS)(Cont’d)
4) (604 withSB 604-34-031)
C - 1 (O) Except when enroute operations require dual FMSuse, any in excess of one may be inoperative.
NOTE 1: Autothrottle system is consideredinoperative when the FMS No. 1 isinoperative (604 with autothrottle system).
NOTE 2: When operating with a single FMSoperative, FMS-computed take off andapproach performance (FMS V speed)and FMS-computed N1 thrust data mustbe verified using applicable AFM data.
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5) (605, 650) |a) Flight
ManagementComputer(No. 1 and No. 2)
C 2 1 (O) Except when enroute operations require dual FMSuse, any in excess of one may be inoperative:
a) One GPS system is operative, andb) Autothrottle system is considered inoperative
when the FMS No. 1 is inoperative.
NOTE: When operating with a single FMS operative,FMS-computed take off and approachperformance (FMS V speed) and FMS-computed N1 thrust data must be verifiedusing applicable AFM data.
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b) ControlDisplayUnits(No. 1 and No. 2)
C 2 1 (O) CDU 2 may be inoperative provided:a) All Adaptive Flight Displays (AFD) are
operative,b) Associated Flight Management Computer is
considered inoperative,c) CDU 2 INHIB switch/light is pressed in, andd) Both Cursor Control Panels (CCP) are
operative.
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(Cont’d)
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34 – NAVIGATION 4. Remarks or Exceptions
61-1 Flight ManagementSystems (FMS)(Cont'd)
5) (605, 650) (Cont’d)
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c) CDU RadioTuningFunction(No. 1 and No. 2)
C 2 1 (O) CDU Radio Tuning No. 2 may be inoperativeprovided:
a) All Adaptive Flight Displays (AFD) areoperative,
b) Radio tuning reversion capabilities are verifiedoperative before each flight., and
c) CDU 2 INHIB switch/light is pressed ind) Both Cursor Control Panels (CCP) are
operative.
d) FlightManagementComputer(FMC)No. 3***
D 1 0
e) ControlDisplay Unit(CDU)No. 3***
D 1 0
(Cont’d)
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34 – NAVIGATION 4. Remarks or Exceptions
61-1 Flight ManagementSystems (FMS)(Cont'd)
6) NavigationDatabases
NOTE: A database which is out of date is consideredto be inoperative.
A - 0 (O) One or more may be out of date for a maximum of10 calendar days provided:
a) Area Navigation (RNAV/RNP) departure,arrival and approach procedures are checkednot to depend on the data amended in thecurrent database cycle or Conventional (Non-RNAV/RNP) or ANSP assistance are used asan alternative to RNAV/RNP procedures whichhave been amended in the current databasecycle,
b) Before each flight, current aeronauticalinformation is used to verify the databaseNavigation Fixes, the coordinates, frequencies,status (as applicable) and suitability ofNavigation Facilities required for the intendedflight route, and
c) Radio navigation aids, which are required to beflown for departure, arrival and approachprocedures and which have been amended inthe current database cycle, are manually tunedand identified.
C - 0 (O) One or more may be inoperative for the intendedflight route where conventional (non-RNAV/RNP)navigation is sufficient, provided:
a) Current aeronautical information (e.g. charts) isavailable for the entire route and for theaerodromes to be used,
b) Navigation database information isdisregarded, and
c) Radio navigation aids, which are required to beflown for departure, arrival and approachprocedures are manually tuned and identified..
(Cont’d)
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34 – NAVIGATION 4. Remarks or Exceptions
61-1 Flight ManagementSystems (FMS)(Cont'd)
C - 1 (O) Any in excess of one may be inoperative provided:a) The operative database must be up to date for
routes, departures, arrival and approachprocedures that require the use of navigationDatabase for RNAV/RNP,
b) The operative database is available and usedby the flight crew member(s) responsible fornavigation, and
c) Radio navigation aids, which are required to beflown for departure, arrival and approachprocedures are manually tuned and identified.
61-2 Flight ManagementSystem (FMS)Performance DataBase (604, 605, 650)
D - 0 (O) May be inoperative (not installed) providedalternate procedures are established and used.
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61-3 Data Base Unit (DBU)(604, 605, 650)
C 1 0|
61-4 Flight ManagementSystem (FMS) VspeedData Base(604, 605, 650)
D - 0 (O) May be inoperative (not installed) providedalternate procedures are established and used.
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61-5 Flight ManagementSystem (FMS) N1Thrust Data Base(604***, 605, 650)
D - 0 (O) May be inoperative (not installed) providedalternate procedures are established and used.
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35 – OXYGEN 4. Remarks or Exceptions
10-2 Crew OxygenPressure Gauge(600, 601, 601-3A,601-3R)
C 1 0 (M) May be inoperative provided both the fill pointgauge and the bottles mounted gauge are checkedprior to each flight.
12-1 Crew OxygenPressure(604, 605, 650) |
1) EICAS Readout C 1 0 (M) May be inoperative provided the Ground ServicePanel pressure gauge or the bottle pressure gauge isoperative and checked prior to each flight.
2) Ground ServicePanel PressureGauge
C 1 0 May be inoperative provided the EICAS Readout or thebottle pressure gauge is operative and checked prior toeach flight.
3) Bottle PressureGauge
C - 0 One or more may be inoperative provided theassociated flight crew compartment pressure indicationis operative.
20-1 Passenger OxygenSystem
B 1 0 (M)(O) May be inoperative provided:a) Maximum altitude is limited to 10 000 ft
pressure altitude,b) An adequate supply of fresh air is provided to
the cabin, andc) Passengers are appropriately briefed
B 1 0 (O) May be inoperative provided:a) Maximum altitude is limited to 25 000 ft
pressure altitude,b) Air conditioning packs are operative,c) All components of the pressurisation system
are operative,d) Aeroplane is able to descend within 4 minutes
to a cabin pressure altitude of 13 000 ft at allpoints along the route to be flown,
e) Portable oxygen units are available for allrequired cabin crew members,
(Cont’d)
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35 – OXYGEN 4. Remarks or Exceptions
20-1 Passenger OxygenSystem(Cont’d)
f) Sufficient oxygen quantity is available for atleast 10 % of the passengers for the entireflight time when the cabin pressure altitude isbetween 10 000 ft and 13 000 ft following adecompression event at the most critical pointof the intended flight route, and
g) Passengers are appropriately briefed.
20-2 Passenger OxygenSystem – AutomaticPresentationSystem1) (604, 605, 650) C 1 0 May be inoperative provided:
a) The manual deployment from the flight crewcompartment is operative, and
b) The maximum altitude is limited to 30 000 ftpressure altitude
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2) (600, 601,601-3A, 601-3R,604)
C 1 0 (O) May be inoperative provided:a) Maximum altitude is limited to 25 000 ft
pressure altitude, andb) Aeroplane is able to descend within 4 minutes
to a cabin pressure altitude of 13 000 ft at allpoints along the route to be flown.
20-3 Passenger ServiceUnits (PSUs)
B - - (M)(O) One or more may be inoperative provided:a) Affected seats are blocked and placarded to
prevent occupancy,b) Units are operative for all operative passenger
seats, toilet compartments and cabin crewlocations.
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35 – OXYGEN 4. Remarks or Exceptions
20-4 Lavatory OxygenSystem
C 1 0 May be inoperative provided:a) The lavatory is not used for any purpose, andb) The lavatory door is locked and placarded
“INOPERATIVE DO NOT ENTER”.
NOTE: This does not preclude storage of in-flightservice waste bags in the associatedlavatory.
C 1 0 May be inoperative provided the aircraft is not operatedabove FL250.
50-1 First-Aid Oxygen D - - (M)(O) Any portable oxygen dispensing unit in excessof those required may be inoperative or missingprovided:
a) Required distribution of operative units ismaintained throughout the aircraft,
b) The inoperative portable oxygen dispensingunit is placarded inoperative, and
c) Procedures are established and used to alertcrew members of inoperative or missingequipment.
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CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 35-4
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
35 – OXYGEN 4. Remarks or Exceptions
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 36-1
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
36 – PNEUMATICS 4. Remarks or Exceptions
10-1 Engine Bleed AirSOVs (14th Stage)(601, 601-3A, 601-3R, 604,605, 650)
C 2 1 (M) One may be inoperative provided:a) Affected valve is secured CLOSED,b) Both Ice Detection Systems are operative,c) Associated Thrust Reverser is deactivated,
stowed and locked in forward thrust position,d) Flight is not conducted in known or forecast
icing conditions,e) Aircraft is operated at or below
FL 400, andf) 14th Stage Engine Bleed Air Isolation Valve is
operative.
NOTE: Refer to MMEL Item 78-30-1.
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20-1 Bleed Air PressureIndicators (LH &RH)
1) 8th Stage(600)
C 2 1 (O) One may be inoperative provided procedures areused to ensure that the pressure is present at bothsides.
2) 10th Stage(601, 601-3A,601-3R)
C 2 1 (O) One may be inoperative provided procedures areused to ensure that the pressure is present at bothsides.
20-2 EICAS Bleed AirPressure Readout(604, 605, 650)
C 2 1 (O) One may be inoperative provided procedures areused to ensure that the pressure is present at bothsides. |
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36 – PNEUMATICS 4. Remarks or Exceptions
23-1 Bleed Air OverheatSensing Loops A andB
1) 600, 601, 601-3A,601-3R
C 2 1 Either loop A or B may be inoperative provided:a) Remaining loop is operative, andb) DUCT MON switch is selected to operative
loop position.
2) 604, 605, 650 C 2 1 (O) Either loop A or B may be inoperative providedneither loop is failed open.
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 38-1
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
38 – WATER/WASTE 4. Remarks or Exceptions
10-1 Potable WaterSystem
C - 0 (M) May be inoperative provided appropriateprocedures are established to deactivate applicablesystem components (i.e. tank drained) to prevent itsservicing, inspect system for leaks, and to provide forcrewmember inspection.
10-2 Lavatory WasteSystems1) If more than
one lavatory(IncludesWheelchairAccessibleLavatories)
C - 1 (M) (O) May be inoperative provided:a) Waste is drained and system is inspected for
leakage,b) Procedures are established to deactivate
system components, andc) Lavatory door is locked closed and placarded
“INOPERATIVE - DO NOT ENTER”.
D - - (M)(O) Individual components may be inoperativeprovided:
a) Associated components are deactivated orisolated, and
b) Associated system components are verified notto have leaks.
NOTE: Any portion of the system that operatesnormally may be used.
2) If one lavatory(IncludesWheelchairAccessibleLavatories)
C - 0 (M)(O) May be inoperative provided:a) Waste is drained and system is inspected for
leakage,b) Procedures are established to deactivate
system components, andc) Lavatory door is locked closed and placarded
“INOPERATIVE - DO NOT ENTER”.
NOTE 1 : The (O) procedure addresses other meansfor water provision for crew members aswell as the need to advise of system statusduring crew changes
(Cont’d)
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CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 38-2
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
38 – WATER/WASTE 4. Remarks or Exceptions
10-2 Lavatory WasteSystems(Cont’d)2) If one lavatory
(IncludesWheelchairAccessibleLavatories)(Cont’d)
D - - (M)(O) Individual components may be inoperativeprovided:
a) Associated components are deactivated orisolated, and
b) Associated system components are verified notto have leaks.
NOTE: Any portion of the system that operatesnormally may be used.
10-3 Lavatory ExternalService Cap
C 1 0 (M) May be inoperative or missing provided:a) The waste valve is verified closed prior to each
flight, andb) No leakage can be detected after each
servicing.
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45 – CENTRAL 4. Remarks or ExceptionsMAINTENANCE SYSTEMS
45-1 MaintenanceDiagnostic Computer(MDC)(604, 605, 650)
C 1 0 (O) May be inoperative provided:a) Electronic Checklists if installed is considered
inoperative, andb) Alternate procedures are established and
used.
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AIRCRAFT REVISION No: 1 Page
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45 – CENTRAL 4. Remarks or ExceptionsMAINTENANCE SYSTEMS
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1. 2. Number InstalledSystem & Sequence No Item
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46 –INFORMATION SYSTEMS 4. Remarks or Exceptions
10-1 Electronic FlightBags
C - 0 (M)(O) May be inoperative provided alternateprocedures are established and used where operatingprocedures require the use of the affected EFB.
1) Class 2 EFBa. Mounting
Device***
C - 1 (M)(O) Any in excess of one may be inoperativeprovided the affected EFB is secured by an alternativemeans.
C - 0 (M)(O) May be inoperative provided:a) The associated EFB is used in accordance with
Class 1 EFB stowage criteria, andb) Alternate procedures are established and used
where operating procedures require the use ofthe affected EFB.
b. DataConnectivity***
C - 1 (M)(O) Any in excess of one may be inoperativeprovided an alternative means of data connectivity isused.
C - 0 (M)(O) May be inoperative provided alternateprocedures are established and used where operatingprocedures require the use of the affected EFB.
2) PowerConnection forClass 1 andClass 2 EFB***
C - 1 (M)(O) Any in excess of one may be inoperativeprovided an alternative power source is available andcan be used for the planned duration of use of theaffected EFB.
C - 0 (M)(O) May be inoperative provided alternateprocedures are established and used.
(Cont’d)
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CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 46-2
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
46 –INFORMATION SYSTEMS 4. Remarks or Exceptions
10-2 Integrated FlightInformation System(IFIS)(605, 650)***
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1) File Server Unit(FSU)***
C 1 0 (O) May be inoperative provided alternate proceduresare established and used.
D 1 0 May be inoperative provided routine procedures do notrequire its use.NOTE: Any function which operates normally may be
used.
2) Electronic ChartDisplays***
C 2 0 (O) May be inoperative provided alternate proceduresare established and used.
D 2 0 May be inoperative provided routine procedures do notrequire its use.
3) GraphicalWeatherFunction***
C 1 0 (O) May be inoperative provided alternate proceduresare established and used.
D 1 0 May be inoperative provided routine procedures do notrequire its use.
4) EnhancedMapOverlayFunction***
C 1 0 (O) May be inoperative on either or both MFDsprovided alternate procedures are established andused.
D 1 0 May be inoperative on either or both MFDs providedroutine procedures do not require its use.
20-1 Airborne FlightInformation System(AFIS)(600, 601, 601-3A, 601-3R, 604)***
D - 0 May inoperative provided routine procedures donot require its use.
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
49 – APU 4. Remarks or Exceptions
00-1 APU Bleed Air SOV(Load Control Valve)
C 1 0 May be inoperative closed.
00-2 Auxiliary Power Unit(APU)
1) Aircraft withGenerator P/Ns720845,720845A,720845B
C 1 0 (M) May be inoperative provided any main generatorwith these P/Ns has more than 150 operating hours.
2) Aircraft withother GeneratorP/Ns
C 1 0
00-3 APU Load ControlValve (APU LCV)Fail Switchlight(light function only)(604, 605, 650)
C 1 0
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00-4 APU Hour Meter C 1 0 (O) May be inoperative provided alternate means ofrecording is established.
1) (604, 605,650)***
D - 1|
00-5 APU / START /STOP / AVAIL(Light function only)(604, 605, 650)
C 1 0 (O) May be inoperative provided, APU parameters areused to confirm that the APU has started or stopped.
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 49-2
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
49 – APU 4. Remarks or Exceptions
61-1 Electronic ControlUnit (ECU)
1) With IDG P/Ns720845720845Aand 720845B
C 1 0 (M) May be inoperative provided any main generatorwith one of these P/Ns has more than 150 operatinghours
2) With Other IDGP/Ns
C 1 0
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52 – DOORS 4. Remarks or Exceptions
00-1 Exterior Door KeyLocks1. Passenger Door
Key LockD 1 0 May be inoperative or missing provided door opens
and closes normally.
2. Cargo/BaggageDoor Key Lock
D 1 0 May be inoperative or missing provided door opensand closes normally.
3. Aft-EquipmentCompartmentDoor Key Lock
D 1 0 May be inoperative or missing provided door opensand closes normally.
4. External ServiceDoors KeyLocks***
D - 0 May be inoperative or missing provided door opensand closes normally.
11-1 Passenger DoorManual Retract Handle
C 1 0 May be inoperative provided door is verified manuallyoperative (opens and closes) without any interference.
11-2 StorageCompartment Door(Main Entry Door)
C 1 0 (M) May be inoperative provided:a) Storage content is relocated, andb) Door is secured closed.
12-1 Main Cabin DoorPower AssistSystem(600, 601 ***)(601-3A, 601-3R,604, 605, 650)
C - 0 May be inoperative provided the door can be openedand closed manually without any interference.
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AIRCRAFT REVISION No: 1 Page
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1. 2. Number InstalledSystem & Sequence No Item
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52 – DOORS 4. Remarks or Exceptions
30-1 Baggage DoorCounterbalanceSystems (balancesprings)
C 2 0 (M) Both may be inoperative provided baggage door isverified closed, latched, locked and not used.
NOTE: Baggage compartment is accessible throughthe door located in the aft cabin.
70-1 Main Cabin DoorIndication System(600, 601, 601-3A,601-3R)
C 1 0 May be inoperative provided :a) All four latches are engaged as indicated by
witness marks,b) Inner Handle is verified stowed,c) External handle is verified stowed, andd) Airstair (CL-600 if installed) is properly stowed
and the actuator arming latch is disengaged.
NOTE: Canadair Service Bulletin 600-0621 or 601-0395 must be incorporated.
70-2 Passenger DoorIndication System(604, 605, 650)
B 1 0 (O) Any or all of the following caution messages:“PAX DOOR LATCH”“PAX DOOR STOW”“PAX DOOR OUT HNDL”may be either inoperative or malfunction provided:
a) Door is closed, latched and locked prior toeach flight,
b) Green marks on the two middle roll latches arealigned,
c) Green marks on the two upper roll latches arealigned,
d) Flag indicator indicates “LOCKED”,e) Inner knob is verified stowed,f) External handle is verified stowed, andg) External pressure vent flap is verified
operative.
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AIRCRAFT REVISION No: 1 Page
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1. 2. Number InstalledSystem & Sequence No Item
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52 – DOORS 4. Remarks or Exceptions
70-3 BAG DR UNSAFECaution Light(600, 601, 601-3A,601-3R)
C 1 0 May be inoperative provided the door is confirmedclosed and latched prior to each flight.
70-4 Baggage DoorIndication System(604, 605, 650)
C 1 0 Caution message “BAGGAGE DOOR” may beinoperative provided:
a) Associated door is closed, latched and locked,and
b) External handle is verified stowed prior to eachflight.
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70-5 Refueling PanelDoor Open CautionLight***
D - 0 All may be inoperative provided it can be determinedthat the door is closed and latched prior to each flight.
70-6 Hydraulic # 3Access Door OpenCaution Light***
D 1 0 May be inoperative provided access door is confirmedclosed and latched prior to each flight.
70-7 Lavatory ServicingOutlet Door OpenCaution Light***
D 1 0 May be inoperative provided outlet door is confirmedclosed and latched prior to each flight.
70-8 Aft Equipment BayDoor Open CautionLight***
D 1 0 May be inoperative provided door is confirmed closedand latched prior to each flight.
70-9 Nose Door (OxygenService) OpenCaution Light***
D 1 0 May be inoperative provided door is confirmed closedand latched prior to each flight.
70-10 Water Fill ControlAccess Door OpenCaution Light***
D 1 0 May be inoperative provided door is confirmed closedand latched prior to each flight.
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52 – DOORS 4. Remarks or Exceptions
70-11 DC Ground AccessDoor Open CautionLight***
D 1 0 May be inoperative provided door is confirmed closedand latched prior to each flight.
70-12 AC Ground AccessDoor Open CautionLight***
D 1 0 May be inoperative provided door is confirmed closedand latched prior to each flight.
70-13 APU Control andGround StartAccess Door OpenCaution Light***
D 1 0 May be inoperative provided door is confirmed closedand latched prior to each flight.
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 56-1
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For DispatchNombre d'articles à expédier
56 – WINDOWS 4. Remarks or ExceptionsRemarques ou exceptions
10-1 Windshield Face Ply(Acrylic or Glass Face Ply)
A 2 1 (M) The face ply of one windshield may be crackedprovided:
a) Vision is not impaired through remainingwindows,
b) Tape and face-ply is checked for integrity priorto each flight,
c) Visibility through the affected windshield isacceptable,
d) Affected windshield heater is consideredinoperative,
e) Pilot’s (Left) side window heater and at leastone additional windshield or side windowheater are operative,
f) Flight into known or forecast icing conditions,precipitation, thunderstorms or other conditionswhich could cause fogging or misting isprohibited,
g) Airspeed is limited to 280KIAS or less below8, 000 ft MSL, and
h) Repairs are made within 6 flights.
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56 – WINDOWS 4. Remarks or Exceptions
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AIRCRAFT REVISION No: 1 Page
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
71 – POWER PLANT 4. Remarks or Exceptions
70-1 Ecology TankEjector Pumps(600, 601, 601-3A)
C 2 1 (M) One may be inoperative provided the tank isdrained:
a) Prior to the first flight of each day,b) After three normal shutdowns, andc) After two false wet starts.
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71 – POWER PLANT 4. Remarks or Exceptions
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AIRCRAFT REVISION No: 1 Page
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73 – ENGINE FUEL & 4. Remarks or ExceptionsCONTROL
30-1 Fuel TemperatureIndicating Systems
C 2 1 One may be inoperative provided icing inhibitor isadded to the fuel.
31-1 Fuel Flow IndicatingSystems(600, 601, 601-3A,601-3R)
B 2 1 One may be inoperative provided:
a) Fuel Quantity Indicating System is operative,and
b) N1, N2 and ITT indications for the associatedengine are operative.
NOTE: Inoperative Fuel Flow Indicating System maycause Fuel Used Indicating System to beinoperative.
1) Left Vertical ScaleLamps
C 28 14 (O) May be inoperative provided:a) No two adjacent lamps on the affected scale
are inoperative.b) Engine parameters are monitored during flight.
2) Right VerticalScale Lamps
C 28 14 (O) May be inoperative provided:a) No two adjacent lamps on the affected scale
are inoperative.b) Engine parameters are monitored during flight.
3) Digital indications C 2 1 (M) May be inoperative provided:a) Associated vertical scale indicator is operativeb) The affected digital indicator is covered
31-2 EICAS Fuel Flow “FF”Readouts(604, 605, 650)
B 2 1 One may be inoperative provided:a) EICAS Fuel Tank quantity readouts are
operative,b) FMS Fuel Used Indication is considered
inoperative and not used, andc) FMS Fuel Remaining Indication is considered
inoperative and not used.
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AIRCRAFT REVISION No: 1 Page
CL 600\601\601-3A\601-3R\604\605\650 DATE: Feb 19/2016 73-2
1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
73 – ENGINE FUEL & 4. Remarks or ExceptionsCONTROL
31-3 Fuel Used IndicatingSystem***
C - 0 May be inoperative provided procedures are notdependent on its use.
31-4 Fuel Low PressureIndication
1) 600, 601, 601-3A, 601-3R
C 2 1 One Fuel LOW PRESS Light may be inoperativeprovided both fuel boost pumps are operative.
2) 604, 605, 650 C 2 1 One “L/R FUEL LO PRESS” EICAS caution messagemay be inoperative provided both fuel boost pumps areoperative.NOTE: The Fuel Fed Check Valve Test (First flight of
the day) is waived for the inoperative fuel lowpressure indication.
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74 – IGNITION 4. Remarks or Exceptions
10-1 Ignition Exciters(600)
B 4 2 One exciter per engine may be inoperative providedtake-off in heavy precipitation, or on a runway surfacecovered with standing water, slush or snow isprohibited.
10-2 Igniter Plugs(600)
B 4 2 One Igniter Plug per engine may be inoperativeprovided take-off in heavy precipitation, or on a runwaycovered with standing water, slush or snow isprohibited.
11-1 Ignition Systems(601, 601-3A, 601-3R, 604, 605, 650) |
1) A Systems B 2 1 One may be inoperative provided:a) Both B Systems are operative, andb) Take-off in heavy precipitation, or on a runway
surface covered with standing water, slush orsnow is prohibited.
2) B Systems B 2 0 One or both may be inoperative provided:a) Both A Systems are operative, andb) Take-off in heavy precipitation, or on a runway
surface covered with standing water, slush orsnow is prohibited.
11-2 Relight IgnitionSystem Switch(600, 601)
C 1 0 May be inoperative provided continuous ignitionsystems A and B modes for both engines areconfirmed operative prior to each flight.
C 1 0 May be inoperative provided In Flight Start Ignition isconfirmed operative on both engines and is used in lieuof relight switch.
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74 – IGNITION 4. Remarks or Exceptions
30-1 IGNITION A/B“ARM/ON” SwitchLights(light function only)(604, 605, 650)
C 2 0
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30-2 IGNITIONCONT”ON” SwitchLight(light function only)(604, 605, 650)
C 1 0
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76 – ENGINE CONTROL 4. Remarks or Exceptions
00-1 Engine SpeedControl Systems1) (601, 601-3A,
601-3R, 604)withoutAutothrottleSystem
C 2 0 (O) One or both may be inoperative provided:a) Both ENG SPEED CONTROL switches are
selected OFF,b) APR is selected OFF, andc) Operations are conducted in accordance with
AFM APR inoperative performance data,
2) (601, 601-3A,601-3R, 604)withAutothrottleSystem)(605, 650)
C 2 0 (O) One or both may be inoperative provided:a) Both ENG SPEED CONTROL switches are
selected OFF,b) APR is selected OFF,c) Operations are conducted in accordance with
AFM APR inoperative performance data, and
d) Autothrottle System is considered inoperative.
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10-1 Automatic PowerReserve (APR)System(601, 601-3A, 601-3R, 604, 605, 650)
C 1 0 May be inoperative in accordance with the performancerequirements defined in the AFM applicable to take-offwith the APR selected OFF.
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11-1 Engine SpeedSynchronizerSystem(600)
C 1 0 (O) May be inoperative provided the ENG SYNCCONTROL switch is selected OFF.
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76 – ENGINE CONTROL 4. Remarks or Exceptions
20-1 Engine OverspeedPickups (PrimaryOverspeedProtection System(600)
C 4 2 (O) One per engine may be inoperative provided theassociated engine(s) are shut down using the engineoverspeed procedure once each flight day.
20-2 Engine OverspeedPickups(Secondary)OverspeedProtection System)(Post ServiceBulletin ALF502L-76-0166)(600 ***)
C 2 0 (M)(O) One or both may be inoperative provided theassociated engine(s) are shutdown using the engineoverspeed procedure once each flight day.
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77 – ENGINE INDICATING 4. Remarks or Exceptions
10-1 N1 Vertical ScaleIndicators(600, 601, 601-3A,601-3R)
C 2 1 (O) One may be inoperative provided all other engineinstruments are operative.
1) Vertical ScaleLamps
a) Left C 28 14 (O) One or more lamps may be inoperative provided:a) No two adjacent lamps are inoperative,b) The lowest lamp in the red zone and the
highest lamp in the green zone are operative,c) Both amber lamps are operative,d) A test is conducted before each flight to
determine the inoperative lamps, ande) Engine parameters are monitored during flight.
b) Right C 28 14 (O) One or more lamps may be inoperative provided:a) No two adjacent lamps are inoperative,b) The lowest lamp in the red zone and the
highest lamp in the green zone are operative,c) Both amber lamps are operative,d) A test is conducted before each flight to
determine the inoperative lamps, ande) Engine parameters are monitored during flight.
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77 – ENGINE INDICATING 4. Remarks or Exceptions
10-2 N2 Vertical ScaleIndicators(600, 601,601-3A,601-3R)
C 2 1 (O) One may be inoperative provided all other engineinstruments are operative.
1) Vertical scalelamps(600)
a) Left C 28 14 (O) One or more lamps may be inoperative provided:a) No two adjacent lamps are inoperative,b) The two amber lamps adjacent to the green
zone (upper and lower sides) and the lowestlamp in the red zone are operative,
c) The top and bottom green lamps (adjacent tothe upper and lower amber zones) areoperative,
d) A test is conducted before each flight todetermine the inoperative lamps, and
e) Engine parameters are monitored during flight.
b) Right C 28 14 (O) One or more lamps may be inoperative provided:a) No two adjacent lamps are inoperative,b) The two amber lamps adjacent to the green
zone (upper and lower sides) and the lowestlamp in the red zone are operative,
c) The top and bottom green lamps (adjacent tothe upper and lower amber zones) areoperative'
d) A test is conducted before each flight todetermine the inoperative lamps, and
e) Engine parameters are monitored during flight.
(Cont'd)
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77 – ENGINE INDICATING 4. Remarks or Exceptions
10-2 N2 Vertical ScaleIndicators(600, 601, 601-3A,601-3R)(Cont'd)
2) Vertical scalelamps(601, 601-3A,601-3R)
a) Left C 28 14 (O) One or more lamps may be inoperative provided:a) No two adjacent lamps are inoperative,b) The highest lamp in the green zone, the yellow
lamp and the lowest lamp in the red zone areoperative,
c) A test is conducted before each flight todetermine the inoperative lamps, and
d) Engine parameters are monitored during flight.
b) Right C 28 14 (O) One or more lamps may be inoperative provided:a) No two adjacent lamps are inoperative,b) The highest lamp in the green zone, the yellow
lamp and the lowest lamp in the red zone areoperative,
c) A test is conducted before each flight todetermine the inoperative lamps, and
d) Engine parameters are monitored during flight.
EUROPEAN AVIATION SAFETY AGENCYMASTER MINIMUM EQUIPMENT LIST
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1. 2. Number InstalledSystem & Sequence No Item
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77 – ENGINE INDICATING 4. Remarks or Exceptions
20-1 ITT Indicators(600, 601, 601-3A,601-3R)
B 4 2 Either the digital or the vertical scale indicators, but notboth, may be inoperative for each engine.
NOTE:If starting with DC Electrical Power Only:
1. When the Right Engine Digital ITT Indication isinoperative, a Left Engine start must beaccomplished first.
2. When the Left Engine Vertical Scale ITTIndication is inoperative, a Right Engine startmust be accomplished first.
1) Vertical ScaleLamps
a) Left B 28 14 (O) One or more lamps may be inoperative provided:a) No two adjacent lamps may be inoperative,b) The highest lamp in the green zone, the yellow
lamps and the lowest lamp in the red zone areoperative,
c) A test is conducted before each flight todetermine the inoperative lamps, and
d) Engine parameters are monitored during flight.
b) Right B 28 14 (O) One or more lamps may be inoperative provided:a) No two adjacent lamps may be inoperativeb) The highest lamp in the green zone, the yellow
lamps and the lowest lamp in the red zone areoperative.
c) A test is conducted before each flight todetermine the inoperative lamps, and
d) Engine parameters are monitored during flight.
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77 – ENGINE INDICATING 4. Remarks or Exceptions
20-2 DGT OFF switch(600, 601, 601-3A,601-3R)
C 1 0 (M) May be inoperative in the ON position.
30-1 Engine VibrationMonitor
C 2 0 One or both may be inoperative provided:a) Flight is not conducted in known or forecast
icing conditions, andb) One Ice Detection System is operative.
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77 – ENGINE INDICATING 4. Remarks or Exceptions
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1. 2. Number InstalledSystem & Sequence No Item
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78 – EXHAUST 4. Remarks or Exceptions
30-1 Thrust ReverserSystems
C 2 1 (M) One may be inoperative provided:a) The affected thrust reverser does not have
structural damages other than cracks in thecascades.
b) Affected Thrust Reverser is deactivated andsecured in the forward thrust position,
c) Nosewheel Steering System is operative,d) For Take-off on wet or contaminated runways
and landing on contaminated runways,operations are conducted in accordance with:
(604, 605, 650)AFM Supplement 2 (Operations on Wet andContaminated Runways.)
(600, 601, 601-3A, 601-3R)AFM Supplement 2 (Operations onContaminated Runways.)
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NOTE: Cracks in the cascades must be repaired orthe cascades replaced before the affectedthrust reverser is activated.
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78 – EXHAUST 4. Remarks or Exceptions
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1. 2. Number InstalledSystem & Sequence No Item
3. Number Required For Dispatch
79 – OIL 4. Remarks or Exceptions
12-1 Oil ReplenishmentSystem(601, 601-3A, 601-3R, 604, 605, 650)
C 1 0 (M) One may be inoperative provided alternatemethods for checking engine oil levels and servicingengine oil are established.
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30-1 Oil PressureIndicators(600, 601, 601-3A,601-3R)
C 2 0 One or both may be partially inoperative to the extentthat every alternate segment of the indicator strip maybe inoperative provided:
a) Associated Low Pressure Warning Light isoperative, and
b) Associated Oil Temperature Indicator isoperative.
30-2 Oil PressureReadouts(604, 605, 650)
B 2 1 (M) One may be inoperative provided:a) Associated EICAS “ENG OIL PRESS” warning
message is operative,b) Oil quantity is checked prior to each flight, andc) Engine is operated at idle for 2 minutes prior to
each flight.
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30-3 Oil TemperatureIndicators(600, 601, 601-3A,601-3R)
C 2 0 One or both may be partially inoperative to the extentthat every alternate segment of the indicator strip maybe inoperative provided the associated oil pressureindicator is operative.
30-4 Oil Low PressureWarning Lights L orR LOP(600, 601, 601-3A,601-3R)
B 2 1 One may be inoperative provided:a) Indicator light is extinguished or blanked, andb) Associated oil pressure indicator is operative
and monitored.
30-5 Oil Low PressureSwitch(604, 605, 650)
B 2 1 One may be inoperative provided both oil pressurereadouts are operative.
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79 – OIL 4. Remarks or Exceptions
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