328JET QRH.pdf

Issue: May 05/99

328JET

Model Dornier 328300

328JETQuick Reference HandbookMain Table of Contents

May 05/99

EFFECTIVITY: ALL MAIN TABLE OF CONTENTS Page 1

MAIN TABLE OF CONTENTS

TitleMain Table of ContentsList of Effective PagesRecord of RevisionsMaster Index

NORMAL PROCEDURES CHECKLISTEMERGENCY PROCEDURESABNORMAL PROCEDURES

328JETQuick Reference HandbookMain Table of Contents

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328JETQuick Reference HandbookList of Effective Pages

LIST OF EFFECTIVE PAGES

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May 05/99

LIST OF EFFECTIVE PAGES Page 1

EFFECTIVITY: ALL

Title 1 May 05/99

Main Table of Contents 1 May 05/99Main Table of Contents 2 May 05/99

List of Effective Pages 1 May 05/99List of Effective Pages 2 May 05/99List of Effective Pages 3 May 05/99List of Effective Pages 4 May 05/99

Record of Revisions 1 May 05/99Record of Revisions 2 May 05/99

Master Index 1 May 05/99Master Index 2 May 05/99Master Index 3 May 05/99Master Index 4 May 05/99

CHECK LIST 01 May 05/99CHECK LIST 02 May 05/99

Check List 1 May 05/99Check List 2 May 05/99Check List 3 May 05/99Check List 4 May 05/99Check List 5 May 05/99Check List 6 May 05/99Check List 7 May 05/99Check List 8 May 05/99Check List 9 May 05/99Check List 10 May 05/99Check List 11 May 05/99Check List 12 May 05/99

EMERGENCY 01 May 05/99EMERGENCY 02 May 05/99

Emergency 1 May 05/99Emergency 2 May 05/99Emergency 3 May 05/99Emergency 4 May 05/99Emergency 5 May 05/99Emergency 6 May 05/99Emergency 7 May 05/99Emergency 8 May 05/99Emergency 9 May 05/99Emergency 10 May 05/99Emergency 11 May 05/99Emergency 12 May 05/99

Emergency 13 May 05/99Emergency 14 May 05/99Emergency 15 May 05/99Emergency 16 May 05/99Emergency 17 May 05/99Emergency 18 May 05/99Emergency 19 May 05/99Emergency 20 May 05/99Emergency 21 May 05/99Emergency 22 May 05/99Emergency 23 May 05/99Emergency 24 May 05/99Emergency 25 May 05/99Emergency 26 May 05/99Emergency 27 May 05/99Emergency 28 May 05/99Emergency 29 May 05/99Emergency 30 May 05/99Emergency 31 May 05/99Emergency 32 May 05/99

ABNORMAL 01 May 05/99ABNORMAL 02 May 05/99

ECS/OXY Abnormal 101 May 05/99ECS/OXY Abnormal 102 May 05/99

ECS/OXY Abnormal 11 May 05/99ECS/OXY Abnormal 12 May 05/99ECS/OXY Abnormal 13 May 05/99ECS/OXY Abnormal 14 May 05/99ECS/OXY Abnormal 15 May 05/99ECS/OXY Abnormal 16 May 05/99

Auto Flight Abnormal 201 May 05/99Auto Flight Abnormal 202 May 05/99

Auto Flight Abnormal 21 May 05/99Auto Flight Abnormal 22 May 05/99Auto Flight Abnormal 23 May 05/99Auto Flight Abnormal 24 May 05/99

Electric Abnormal 301 May 05/99Electric Abnormal 302 May 05/99

Electric Abnormal 31 May 05/99Electric Abnormal 32 May 05/99Electric Abnormal 33 May 05/99Electric Abnormal 34 May 05/99

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Electric Abnormal 35 May 05/99Electric Abnormal 36 May 05/99Electric Abnormal 37 May 05/99Electric Abnormal 38 May 05/99Electric Abnormal 39 May 05/99Electric Abnormal 310 May 05/99Electric Abnormal 311 May 05/99Electric Abnormal 312 May 05/99Electric Abnormal 313 May 05/99Electric Abnormal 314 May 05/99Electric Abnormal 315 May 05/99Electric Abnormal 316 May 05/99

Fire Protection Abnormal 401 May 05/99Fire Protection Abnormal 402 May 05/99

Fire Protection Abnormal 41 May 05/99Fire Protection Abnormal 42 May 05/99

Flight Controls Abnormal 501 May 05/99Flight Controls Abnormal 502 May 05/99

Flight Controls Abnormal 51 May 05/99Flight Controls Abnormal 52 May 05/99Flight Controls Abnormal 53 May 05/99Flight Controls Abnormal 54 May 05/99Flight Controls Abnormal 55 May 05/99Flight Controls Abnormal 56 May 05/99Flight Controls Abnormal 57 May 05/99Flight Controls Abnormal 58 May 05/99Flight Controls Abnormal 59 May 05/99Flight Controls Abnormal 510 May 05/99Flight Controls Abnormal 511 May 05/99Flight Controls Abnormal 512 May 05/99Flight Controls Abnormal 513 May 05/99Flight Controls Abnormal 514 May 05/99Flight Controls Abnormal 515 May 05/99Flight Controls Abnormal 516 May 05/99Flight Controls Abnormal 517 May 05/99Flight Controls Abnormal 518 May 05/99Flight Controls Abnormal 519 May 05/99Flight Controls Abnormal 520 May 05/99Flight Controls Abnormal 521 May 05/99Flight Controls Abnormal 522 May 05/99Flight Controls Abnormal 523 May 05/99Flight Controls Abnormal 524 May 05/99

Fuel Abnormal 601 May 05/99

Fuel Abnormal 602 May 05/99

Fuel Abnormal 61 May 05/99Fuel Abnormal 62 May 05/99Fuel Abnormal 63 May 05/99Fuel Abnormal 64 May 05/99Fuel Abnormal 65 May 05/99Fuel Abnormal 66 May 05/99Fuel Abnormal 67 May 05/99Fuel Abnormal 68 May 05/99Fuel Abnormal 69 May 05/99Fuel Abnormal 610 May 05/99Fuel Abnormal 611 May 05/99Fuel Abnormal 612 May 05/99Fuel Abnormal 613 May 05/99Fuel Abnormal 614 May 05/99

Hydraulics Abnormal 701 May 05/99Hydraulics Abnormal 702 May 05/99

Hydraulics Abnormal 71 May 05/99Hydraulics Abnormal 72 May 05/99Hydraulics Abnormal 73 May 05/99Hydraulics Abnormal 74 May 05/99Hydraulics Abnormal 75 May 05/99Hydraulics Abnormal 76 May 05/99Hydraulics Abnormal 77 May 05/99Hydraulics Abnormal 78 May 05/99Hydraulics Abnormal 79 May 05/99Hydraulics Abnormal 710 May 05/99Hydraulics Abnormal 711 May 05/99Hydraulics Abnormal 712 May 05/99Hydraulics Abnormal 713 May 05/99Hydraulics Abnormal 714 May 05/99Hydraulics Abnormal 715 May 05/99Hydraulics Abnormal 716 May 05/99Hydraulics Abnormal 717 May 05/99Hydraulics Abnormal 718 May 05/99Hydraulics Abnormal 719 May 05/99Hydraulics Abnormal 720 May 05/99Hydraulics Abnormal 721 May 05/99Hydraulics Abnormal 722 May 05/99Hydraulics Abnormal 723 May 05/99Hydraulics Abnormal 724 May 05/99Hydraulics Abnormal 725 May 05/99Hydraulics Abnormal 726 May 05/99Hydraulics Abnormal 727 May 05/99Hydraulics Abnormal 728 May 05/99

328JETQuick Reference HandbookList of Effective Pages




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Ice Protection Abnormal 801 May 05/99Ice Protection Abnormal 802 May 05/99

Ice Protection Abnormal 81 May 05/99Ice Protection Abnormal 82 May 05/99Ice Protection Abnormal 83 May 05/99Ice Protection Abnormal 84 May 05/99Ice Protection Abnormal 85 May 05/99Ice Protection Abnormal 86 May 05/99Ice Protection Abnormal 87 May 05/99Ice Protection Abnormal 88 May 05/99

Indicating/Recording Abnormal 901 May 05/99Indicating/Recording Abnormal 902 May 05/99

Indicating/Recording Abnormal 91 May 05/99Indicating/Recording Abnormal 92 May 05/99Indicating/Recording Abnormal 93 May 05/99Indicating/Recording Abnormal 94 May 05/99Indicating/Recording Abnormal 95 May 05/99Indicating/Recording Abnormal 96 May 05/99Indicating/Recording Abnormal 97 May 05/99Indicating/Recording Abnormal 98 May 05/99Indicating/Recording Abnormal 99 May 05/99Indicating/Recording Abnormal 910 May 05/99Indicating/Recording Abnormal 911 May 05/99Indicating/Recording Abnormal 912 May 05/99

Landing Gear Abnormal 1001 May 05/99Landing Gear Abnormal 1002 May 05/99

Landing Gear Abnormal 101 May 05/99Landing Gear Abnormal 102 May 05/99Landing Gear Abnormal 103 May 05/99Landing Gear Abnormal 104 May 05/99Landing Gear Abnormal 105 May 05/99Landing Gear Abnormal 106 May 05/99Landing Gear Abnormal 107 May 05/99Landing Gear Abnormal 108 May 05/99Landing Gear Abnormal 109 May 05/99Landing Gear Abnormal 1010 May 05/99Landing Gear Abnormal 1011 May 05/99Landing Gear Abnormal 1012 May 05/99Landing Gear Abnormal 1013 May 05/99Landing Gear Abnormal 1014 May 05/99Landing Gear Abnormal 1015 May 05/99Landing Gear Abnormal 1016 May 05/99Landing Gear Abnormal 1017 May 05/99Landing Gear Abnormal 1018 May 05/99

Landing Gear Abnormal 1019 May 05/99Landing Gear Abnormal 1020 May 05/99Landing Gear Abnormal 1021 May 05/99Landing Gear Abnormal 1022 May 05/99Landing Gear Abnormal 1023 May 05/99Landing Gear Abnormal 1024 May 05/99

Navigation Abnormal 1101 May 05/99Navigation Abnormal 1102 May 05/99

Navigation Abnormal 111 May 05/99Navigation Abnormal 112 May 05/99Navigation Abnormal 113 May 05/99Navigation Abnormal 114 May 05/99Navigation Abnormal 115 May 05/99Navigation Abnormal 116 May 05/99Navigation Abnormal 117 May 05/99Navigation Abnormal 118 May 05/99Navigation Abnormal 119 May 05/99Navigation Abnormal 1110 May 05/99Navigation Abnormal 1111 May 05/99Navigation Abnormal 1112 May 05/99

Pneumatic Abnormal 1201 May 05/99Pneumatic Abnormal 1202 May 05/99

Pneumatic Abnormal 121 May 05/99Pneumatic Abnormal 122 May 05/99

APU Abnormal 1301 May 05/99APU Abnormal 1302 May 05/99

APU Abnormal 131 May 05/99APU Abnormal 132 May 05/99APU Abnormal 133 May 05/99APU Abnormal 134 May 05/99

Doors Abnormal 1401 May 05/99Doors Abnormal 1402 May 05/99

Doors Abnormal 141 May 05/99Doors Abnormal 142 May 05/99

Engine Abnormal 1501 May 05/99Engine Abnormal 1502 May 05/99

Engine Abnormal 151 May 05/99Engine Abnormal 152 May 05/99Engine Abnormal 153 May 05/99

328JETFlight Crew Operating ManualList of Effective Pages




PAGE DATE

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EFFECTIVITY: ALL

Engine Abnormal 154 May 05/99Engine Abnormal 155 May 05/99Engine Abnormal 156 May 05/99Engine Abnormal 157 May 05/99Engine Abnormal 158 May 05/99

328JETQuick Reference HandbookRecord of Revisions

May 05/99

EFFECTIVITY: ALL RECORD OF REVISIONS Page 1

RECORD OF REVISIONS

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328JETQuick Reference HandbookRecord of Revisions

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EFFECTIVITY: ALL RECORD OF REVISIONS Page 2

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328JETQuick Reference HandbookMaster Index

MASTER INDEX

EMERGENCY & ABNORMAL PROCEDURES

May 05/99

MASTER INDEX Page 1

EFFECTIVITY: ALL

AAIRCONDITION SMOKEREMOVAL EMERGENCY 18ABNORMALAPU RESTART Abnormal 132ADC 1 FAIL Abnormal 119ADC 2 FAIL Abnormal 119AHRS 1 FAIL Abnormal 114AHRS 1 FAIL Abnormal 114AHRS 1 NO AUX Abnormal 114AHRS 2 NO AUX Abnormal 114AHRS 1 ON AUX Abnormal 114AHRS 2 ON AUX Abnormal 114AHRS 1 OVHT Abnormal 115AHRS 2 OVHT Abnormal 115AHRS 1 SLV FAIL Abnormal 115AHRS 2 SLV FAIL Abnormal 115AILERON CTRLSYSTEM JAMMED Emergency 15AILERON NORMALTRIM INOP Abnormal 52AIL DISCONNECT Abnormal 51AIL MISTRIM Abnormal 21AIRFOIL DEICE FAIL Abnormal 81ALT ANTISKID DEGR Abnormal 1018ALT ANTISKID FAIL Abnormal 1018ALT BRK FAIL Abnormal 1022APU LIMIT EXCEED Abnormal 133AOA MISCOMPARE Abnormal 99APU BLEED LEAK Abnormal 122APU FAIL Abnormal 131APU FIRE orSEVERE DAMAGE Emergency 4APU GEN FAIL Abnormal 33APU GEN OVHT Abnormal 33APU HOT START Abnormal 132ATT FAIL Abnormal 111AVIONIC FAN FAIL Abnormal 13

BBAT 1 OVHT Emergency 5BAT 2 OVHT Emergency 5BAT 1 FAIL Abnormal 31BAT 2 FAIL Abnormal 31BLEED SOV FAIL Abnormal 121BRK COV FAIL Abnormal 1023BRK MAINT Abnormal 1023BRK TEMP FAIL Abnormal 1021BRK TEMP HIGH Abnormal 1021BUS CTRL 1 FAIL Abnormal 98

BUS CTRL 2 FAIL Abnormal 98BUS Equipment List DC Busses Abnormal 37BUS Equipment List AC Busses Abnormal 316

CCAB ALT Emergency 7CAB DIFF PRSS Abnormal 16CHECK DU 1 thru 5 Abnormal 91COMPLETE HYDRAULICFAILURE Abnormal 725CONFIG MISMATCH Abnormal 98CPCS AUTO FAIL Abnormal 15CPCS MISCOMPARE Abnormal 14

DDAU 1A FAIL Abnormal 95DAU 2A FAIL Abnormal 95DAU 1B FAIL Abnormal 95DAU 2B FAIL Abnormal 95DC BUS 1 FAIL Abnormal 36DC BUS 2 FAIL Abnormal 36DISPLAY FAILURES Abnormal 92DOORS EMERGENCY 6DOORS SWITCH FAIL Abnormal 141DOUBLE DAU FAILURES Abnormal 96DOUBLE ENGINEFAILURE (> 20 000ft) MERGENCY 23DOUBLE ENGINEFAILURE (< 20 000ft) MERGENCY 24DU 1 OVHT Abnormal 94DU 2 OVHT Abnormal 94DU 3 OVHT Abnormal 94DU 4 OVHT Abnormal 94DU 5 OVHT Abnormal 94

EE/PBRK ACCU PRSS Abnormal 727EFIS FAN FAIL Abnormal 13EL MISTRIM NOSE UP Abnormal 21EL MISTRIM NOSE DN Abnormal 21EL TRIM FAIL Abnormal 22ELEVATOR DISCLOAD HI Abnormal 56ELECTRICAL SMOKEREMOVAL EMERGENCY 19ELEV DISCONNECT Abnormal 53ELEVATOR CTRL SYSTEMJAMMEND EMERGENCY 15

328JETFlight Crew Operating ManualMaster Index

MASTER INDEX


May 05/99

MASTER INDEX Page 2

EFFECTIVITY: ALL

ELEVATOR NORMALTRIM INOP Abnormal 55EMERGENCYDESCENT EMERGENCY 30EMERGENCYLANDING EMERGENCY 31ENGINE AIRSTART Abnormal 157ENG ANTIICE FAIL Abnormal 86ENGINE SURGE Abnormal 156ENGINE VIBRATION Abnormal 155ESS BUS FAIL Abnormal 34

FFDR FAIL Abnormal 910FGC DATA FAIL Abnormal 23FGC FAIL Abnormal 23FGC HDG HLD OFF Abnormal 23FGC LAT MODE OFF Abnormal 23FGC VERT MODE OFF Abnormal 23FLAP ASYM Abnormal 57FLAP CTRL FAIL Abnormal 58FLAPLESS LANDING Abnormal 59FMS DEGRAD MODE Abnormal 117FMS DR MODE Abnormal 117FORCEDLANDING EMERGENCY 25FUEL APU SOV FAIL Abnormal 614FUEL ASYM Abnormal 67FUEL CONN VLV OPEN Abnormal 61FUEL ELPMP FAIL Abnormal 61FUEL ELPMP ON Abnormal 62FUEL JETPMP FAIL Abnormal 62FUEL JETPMP ON Abnormal 62FUEL TANK TEMP Abnormal 63FUEL XFEED FAIL Abnormal 65FUEL XFEED PMP Abnormal 66FWC 1 FAIL Abnormal 912FWC 2 FAIL Abnormal 912FWC ANNUNCIATORon PFD Abnormal 911

GGND SPOIL NOT STOW Abnormal 522GND SPOIL FAIL Abnormal 523GND SPOILER ARMED Abnormal 524GROUNDEVACUATION EMERGENCY 31GROUND STARTNOITT AFTER 20 SECS Abnormal 151

HHX FAN FAIL Abnormal 13HYDRAULIC FUMES EMERGENCY 22HYD A PRSS HIGH Abnormal 76HYD B PRSS HIGH Abnormal 77HYD A PRSS LOW Abnormal 79HYD B PRSS LOW Abnormal 79HYD A QTY LOW Abnormal 711HYD B QTY LOW Abnormal 711HYD A QTY FAIL Abnormal 713HYD B QTY FAIL Abnormal 713HYD A TEMP HIGH Abnormal 715HYD B TEMP HIGH Abnormal 716HYD A PMP FAIL Abnormal 719HYD B PMP FAIL Abnormal 720HYD A PMP FAIL andHYD B PMP FAIL Abnormal 722HYD STBY PMP FAIL Abnormal 723

IIAC 1 INVALID Abnormal 116IAC 2 INVALID Abnormal 116IAC 1 OVHT Abnormal 116IAC 2 OVHT Abnormal 116IRS 1 ALN FAULT Abnormal 112IRS 2 ALN FAULT Abnormal 112IRS 1 COOL FAIL Abnormal 112IRS 2 COOL FAIL Abnormal 112IRS 1 FAIL Abnormal 113IRS 2 FAIL Abnormal 113IRS 1 NO AUX Abnormal 113IRS 2 NO AUX Abnormal 113IRS 1 ON AUX Abnormal 113IRS 2 ON AUX Abnormal 113INV 1 FAIL Abnormal 31INV 2 FAIL Abnormal 31INV BUS 1 FAIL Abnormal 36INV BUS 2 FAIL Abnormal 36

LLANDING GEAR RETRACTION FAILURE Abnormal 10!LANDING GEAR EXTENSION FAILURE Abnormal 103LANDING with ABNORMAL GEAR CONFIGURATION Abnormal 105LAV FIRE EMERGENCY 9L AC VOLT FAIL Abnormal 31L ALT FAIL Abnormal 32L ALT FAIL EMERGENCY 14

328JETQuick Reference HandbookMaster Index

MASTER INDEX


May 05/99

MASTER INDEX Page 3

EFFECTIVITY: ALL

L ALTIM ACCURACY Abnormal 910L AOA FAIL Abnormal 99L BLEED LEAK Abnormal 121L DC GEN FAIL EMERGENCY 11L DC GEN FAIL Abnormal 33L DC GEN OVHT Abnormal 32L DEICE PRSS LOW Abnormal 82LDG EMG ACTIVATED Abnormal 102L ELEV HEAT FAIL Abnormal 82L ENGINE FAIL Abnormal 152L ENG EXCEEDED Abnormal 151L FADEC FAULT Abnormal 152L FEEDTANK LOW Abnormal 611L FUEL CONTAMIN Abnormal 69L FUEL LOW FAIL Abnormal 610L FUEL PRSS LOW Abnormal 69L FUEL QTY FAIL Abnormal 610L FUEL SOV CLSD Abnormal 613L FUEL SOV FAIL Abnormal 613L FUEL TRANSFER Abnormal 610L PACK FAIL Abnormal 11LH ENG FIRE orSEVERE DAMAGE or ENGINEFAILURE before V1 EMERGENCY 1LH ENG FIRE orSEVERE DAMAGE or ENGINEFAILURE DURING TAKEOFFafter V1 and IN FLIGHT

EMERGENCY 2LH OIL PRS EMERGENCY 3LOOP FAIL Abnormal 41L SHAKER FAIL Abnormal 510

MMISCMPFUEL Abnormal 613MISCMPTRIM Abnormal 510

NNON ESS 1 FAIL Abnormal 36NON ESS 2 FAIL Abnormal 36NORM ANTISKID DEGR Abnormal 1017NORM ANTISKID FAIL Abnormal 1017NORM ANTISKID FAIL andALT ANTISKID FAIL Abnormal 1019NORM BRK FAIL Abnormal 1022NWS BYPASS FAIL Abnormal 1014NWS FAIL Abnormal 1012NWS HIGH Abnormal 1011NWS PWR UP FAUIL Abnormal 1013

OOXY QTY FAIL Abnormal 16OXYGEN EMERGENCY 9

PPFD Abnormal 94PFD EMERGENCY 5PITCH TRIM ASYM Abnormal 510PITOT HEAT 1 FAIL Abnormal 83PITOT HEAT 2 FAIL Abnormal 83PITOT HEAT OFF Abnormal 83PITOT S HEAT FAIL Abnormal 83PRECAUTIONARY ENGINESHUTDOWN Abnormal 151PROXI ARINC FAIL Abnormal 71PROXI GNDSPLR FAIL Abnormal 521PROXI SYS FAIL Abnormal 74PROXI SYSA FAIL Abnormal 72PROXI SYSB FAIL Abnormal 72PUSH RESET FAIL Abnormal 511PUSHER FAIL Abnormal 511PUSHER NO ICE Abnormal 512

RR AC VOLT FAIL Abnormal 31R ALT FAIL EMERGENCY 14R ALT FAIL Abnormal 32R ALTIM ACCURACY Abnormal 910R AOA FAIL Abnormal 99R BLEED LEAK Abnormal 121R DC GEN FAIL EMERGENCY 11R DC GEN FAIL Abnormal 33R DC GEN OVHT Abnormal 32R DEICE PRSS LOW Abnormal 82R ELEV HEAT FAIL Abnormal 82R ENG EXCEEDED Abnormal 151R ENGINE FAIL Abnormal 152R FADEC FAULT Abnormal 152R FEED TANK LOW Abnormal 611R FUEL CONTAMIN Abnormal 611R FUEL LOW FAIL Abnormal 610R FUEL PRSS LOW Abnormal 69R FUEL QTY FAIL Abnormal 610R FUEL SOV CLSD Abnormal 613R FUEL SOV FAIL Abnormal 613R FUEL TRANSFER Abnormal 610R PACK FAIL Abnormal 11RH OIL PRS EMERGENCY 3R SHAKER FAIL Abnormal 510RAD ALT FAIL Abnormal 1110RAD ALT 12 FAIL Abnormal 1110

328JETFlight Crew Operating ManualMaster Index

MASTER INDEX


May 05/99

MASTER INDEX Page 4

EFFECTIVITY: ALL

RAPIDDECOMPRESSION EMERGENCY 29REJECTEDTAKEOFF EMERGENCY 1REC FAN FAIL Abnormal 13REV CTRL FAIL Abnormal 910RH ENG FIRE orSEVERE DAMAGE or ENGINEFAILURE before V1 EMERGENCY 1RH ENG FIRE orSEVERE DAMAGE or ENGINEFAILURE DURING TAKEOFFafter V1 and IN FLIGHT

EMERGENCY 2RMU 1 FAIL Abnormal 910RMU 2 FAIL Abnormal 910ROLL SPOILER JAMMED Abnormal 513RUDDER CTRLSYSTEM JAMMED Abnormal 517RUDDER LIMIT FAIL Abnormal 518RUDDER LIMITED Abnormal 518RUDDER NOT LIMITED Abnormal 519RUDDER NORMALTRIM INOP Abnormal 519

SSG 2 FAIL Abnormal 98SINGLE ENGINE OPERATIONApproach and Landing Abnormal 153GoAround Abnormal 154SMOKE EMERGENCY 17SMOKE LAV EMERGENCY 21SSEC 1 DISABLED Abnormal 118SSEC 2 DISABLED Abnormal 118

TTAT HEAT FAIL Abnormal 84TAT PROBE 1 FAIL Abnormal 84TAT PROBE 2 FAIL Abnormal 84TCAS FAIL Abnormal 1111TCAS OFF Abnormal 1111T/O CONFIG EMERGENCY 9TRIM SPEED FAST Abnormal 519TRIM SPEED SLOW Abnormal 519

UUNCOMMNDED ROLL Abnormal 514

W, X & YWSHLD HEAT FAIL Abnormal 85

XBLEED FAIL Abnormal 122YD OFF Abnormal 24

328JETQuick Reference HandbookNormal Procedures Checklist

May 05/99

EFFECTIVITY : ALL CHECK LIST Page 01

TABLE OF CONTENTS

SUBJECTPAGE

SECTION

GENERAL CHECK LIST 1Principles of normal procedure application CHECK LIST 1Normal checklist application CHECK LIST 1

Cockpit Preparation CHECK LIST 3Engine Start CHECK LIST 6After Engine Start CHECK LIST 7Taxi CHECK LIST 7Before Takeoff CHECK LIST 8After Takeoff (silent) CHECK LIST 8Climb (silent) CHECK LIST 8Cruise (silent) CHECK LIST 9Approach CHECK LIST 9Final Checks CHECK LIST 9After Landing (silent) CHECK LIST 10Engine Shutdown CHECK LIST 10Quick Turn Around CHECK LIST 11Securing CHECK LIST 12


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EFFECTIVITY : ALL CHECK LISTPage 02



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GENERAL

Principles of normal procedures applicationThis Section contains the normal routine operating procedures.

The checklist is used to verify that all steps of the preceding procedures havebeen accomplished. The procedures assume that all systems are operatingnormally and all safety aspects are covered. Additionally aspects of economicimportance may be included.Exterior lights, flight deck lighting and personal comfort items that have noobvious procedural requirements are not included in the checklists.

The normal checklist is applied after the appropriate procedure is completed.The Pilot Flying (PF) shall request reading of a checklist by announcing its title.All actions of a procedure are either required to operate the airplane safely inthe related phase of flight or to prepare the airplane for the following phase offlight. Each action is assigned to a specific crewmember to ensurecoordinated action. These assignments are guidance only and can bechanged as appropriate by the operator. The following crewmemberassignments are used:

LH seated pilot Captain (C) RH seated pilot First Officer (F) Pilot flying (PF) Pilot not flying (PNF)The Normal Checklist is read by the first officer when the airplane is on theground.The Normal Checklist is read by PNF when the airplane is in flight.

Normal checklist applicationNormal Checklists are two types:

1. CHALLENGE/RESPONSE:The appropriate pilot shall respond to the challenge after havingverified the existing configuration. The challenger shall wait for theresponse before proceeding with the checklist. Upon completion heshall announce: ......CHECKLIST COMPLETED.


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2. SILENT:Reading silently, PNF shall use the checklist as a reference to verifythat prescribed actions have been performed. Upon completion heshall announce: . . . . . CHECKLIST COMPLETED.

If the actual configuration is not in accordance with the checklist standard,corrective action shall be initiated. If corrective action is not possible, theresponse must be modified to reflect the actual situation (specific answer).


May 05/99


COCKPIT PREPARATION

Start selectors F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Gear lever F DOWN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Parking brake F PARK. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Thrust levers F CUT OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Emergency power supply F TEST. . . . . . . . . . . . . . . . . . . . . . . . . . . . Exterior check F COMPLETED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Emergency equipment F CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . Pubs and documents C ON BOARD. . . . . . . . . . . . . . . . . . . . . . . . Seat and rudder pedals C/F ADJUSTED. . . . . . . . . . . . . . . . . . . . . NWS tiller C CENTERED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Circuit breakers C/F CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Generators C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Batteries C ON (Check voltage). . . . . . . . . . . . . . . . . . . . . . . . . . . . DC Tie C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AC Tie C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Interior lights C/F AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . LAMP TEST C PERFORM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NAV lights C AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU Fire Test C PERFORM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU system page C SELECT ON MFD. . . . . . . . . . . . . . . . . . . . . . APU MASTER C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU C START. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU Generator C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine bleeds C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS packs C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS crossbleed C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU bleed C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS flow mode C AS DESIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . IRS panel(s) (if installed) C NAV. . . . . . . . . . . . . . . . . . . . . . . . . . . . FMS F PROGRAM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Oxygen, Mask flow C/F CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . . Smoke goggles C/F STOWED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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May 05/99



May 05/99


ENGINE START

engine start using APU air supply:

ELPMP AUTO C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AntiCollision lights C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . XBleed button C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS Packs C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU bleed C RECHECK ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Document hatch C CLOSE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . THRUST lever C IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine starts C COMPLETE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU bleed C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

engine start using external air supply (RH engine only):ELPMP AUTO C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AntiCollision lights C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . XBleed button C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS Packs C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXT BLEED button C EXT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . THRUST lever C IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine starts C COMPLETE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXT BLEED button C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . External bleed air C DISCONNECT/COVER. . . . . . . . . . . . . . . . .

CLOSED

engine start using engine cross bleed:

XBleed button C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU bleed button C OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BLEED (running engine) C ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . THRUST lever (running engine)C ADVANCE to 70%. . . . . . . . . . . THRUST lever C IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine starts C COMPLETE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . THRUST lever (first engine) C IDLE. . . . . . . . . . . . . . . . . . . . . . . . .


May 05/99


AFTER ENGINE START

HYD PWR STBY selector F AUTO. . . . . . . . . . . . . . . . . . . . . . . . . . Ground Crew C DISCONNECT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . DC Tie F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY Attitude Indicator F UNCAGED. . . . . . . . . . . . . . . . . . . . . . . . Hydraulic system pressure F CHECKED. . . . . . . . . . . . . . . . . . . . . Brake temp. indications F CHECKED. . . . . . . . . . . . . . . . . . . . . . . . NWS F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps F SET FOR T/O. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS Packs F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Bleeds F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU Bleed F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

before 1st flight of the day:GROUND SPOILERSYSTEM TEST C PERFORM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FLAP SYSTEM TEST C PERFORM. . . . . . . . . . . . . . . . . . . . . . . . .

TAXI

NAV Lights F AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TAXI Lights F AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NWS HIGH button F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Brakes and NWS C/F NORMAL RESPONSE. . . . . . . . . . . . . . . . . . Ice Protection F AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . WSHLD Heats F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PROBES 1, 2 and STBY button PNF ON. . . . . . . . . . . . . . . . . . . . . . Overhead Panel F NO FAIL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EICAS Display C/F CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flight Director F AS DESIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Attitudes and Headings C/F CHECKED. . . . . . . . . . . . . . . . . . . . . . T/O CONFIG Warning F TEST. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Briefing PF COMPLETE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cabin Report C/F RECEIVED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


May 05/99


BEFORE TAKEOFF

Transponder F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GUST LOCK F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flight Controls C/F FREE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

when cleared for takeoff:FMS F AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WX Radar C/F AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NWS HIGH button F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing Lights PNF ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Strobe Lights PNF ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

AFTER TAKEOFF (SILENT)

Landing Gear PNF UP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps PNF UP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FD/AP PF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Climb thrust PNF MAX CLIMB. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Taxi Lights PNF OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ice Protection PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . Signs PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU bleed PNF OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU Generator PNF OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU PNF STOP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU system page PNF SELECT ON MFD. . . . . . . . . . . . . . . . . . . . APU MASTER PNF OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

CLIMB (SILENT)

Altimeters PF/PNF SET. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing Lights PNF OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pressurization PNF CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Signs PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


May 05/99


CRUISE (SILENT)

Cruise power PNF SET. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pressurization PNF CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS Flow Mode PNF AS DESIRED. . . . . . . . . . . . . . . . . . . . . . . . . .

APPROACH

Ice Protection PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . Landing Lights, PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . Taxi Lights PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pressurization PNF CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing Elevation PNF CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . . Ref Data PNF SET. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DH/MDA PNF SET. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Briefing PF COMPLETE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FMS Arrival PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . Signs PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cabin Report PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . . . Airspeed indicators PNF XCHECKED. . . . . . . . . . . . . . . . . . . . . . . Altimeters PF/PNF SET/XCHECKED. . . . . . . . . . . . . . . . . . . . . . .

FINAL CHECKS

Landing Gear PF/PNF DOWN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps PF/PNF SET. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GND SPOILER PNF AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . EICAS Display PF/PNF CHECKED. . . . . . . . . . . . . . . . . . . . . . . . . . Parking Brake PNF OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AP/YD PNF OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NWS HI button PNF OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


May 05/99


AFTER LANDING (SILENT)

Thrust Levers F IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flaps F 0. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WX Radar F CHECK STBY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Transponder F STBY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Landing Lights F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Strobe Lights F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WSHLD Heats F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Probes F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ice Protection F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ELPMP AUTO F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DC Tie F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start Selectors F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

If desired:LH Engine Bleed F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ECS Cross Bleed F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LH Power Lever F GI. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

ENGINE SHUTDOWN

Parking Brake F PARK. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Thrust Levers C IDLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Taxi Lights F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY HYD PWR F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . If external DC power is desired:APU BLEED F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GEN APU F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU F STOP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . External power F ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU MASTER F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DC Tie F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Emergency Lights F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Bleeds F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Contd next page ===>>>


May 05/99



May 05/99


SECURING

STBY Attitude Indicator F CAGED. . . . . . . . . . . . . . . . . . . . . . . . . IRS Panel(s) (if installed) F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . GEN APU F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APU F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . External Power F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Batteries F OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

CHECKLIST COMPLETED

328JETQuick Reference HandbookEmergency Procedures

May 05/99

EFFECTIVITY : ALL EMERGENCY Page 01

TABLE OF CONTENTS

SUBJECTPAGE

SECTION

REJECTED TAKEOFF EMERGENCY 1

LH or RH ENG FIRE or SEVERE DAMAGEor ENGINE FAILURE before V1 EMERGENCY 1

LH or RH ENG FIRE or SEVERE DAMAGEor ENGINE FAILURE DURING TAKEOFFafter V1 and IN FLIGHT EMERGENCY 2

LH or RH OIL PRS EMERGENCY 3

APU FIRE or SEVERE DAMAGE EMERGENCY 4

BAT 1 or BAT 2 OVHT EMERGENCY 5

PFD EMERGENCY 5

DOORS EMERGENCY 6

CAB ALT EMERGENCY 7

OXYGEN EMERGENCY 9

T/O CONFIG EMERGENCY 9

LAV FIRE EMERGENCY 9

L R DC GEN FAIL EMERGENCY 11

L R ALT FAIL EMERGENCY 14

AILERON CTRL SYSTEM JAMMED EMERGENCY 15

ELEVATOR CTRL SYSTEM JAMMED EMERGENCY 15

SMOKE EMERGENCY 17


May 05/99

EFFECTIVITY : ALL EMERGENCYPage 02

TABLE OF CONTENTS

SUBJECTPAGE

SECTION

AIRCONDITION SMOKE REMOVAL EMERGENCY 18

ELECTRICAL SMOKE REMOVAL EMERGENCY 19

SMOKE LAV EMERGENCY 21

HYDRAULIC FUMES EMERGENCY 22

DOUBLE ENGINE FAILURE (above 20 000 ft) EMERGENCY 23DOUBLE ENGINE FAILURE (below 20 000 ft) EMERGENCY 24FORCED LANDING EMERGENCY 25

RAPID DECOMPRESSION EMERGENCY 29

EMERGENCY DESCENT EMERGENCY 30

EMERGENCY LANDING EMERGENCY 31

GROUND EVACUATION EMERGENCY 31


May 05/99


REJECTED TAKEOFF

Immediately and simultaneously: THRUST levers (both) IDLE. . . . . . . . . . . . GND SPOILER Check if not deployed. . . . . . . . . . . . . . . . . . .

manual deploy MAX BRAKING Apply until airplane. . . . . . . . . . . . . . . . . . .

is safely stopped

LH or RH ENG FIRE or SEVERE DAMAGEor ENGINE FAILURE before V1

1. Takeoff Reject. . . . . . . . . . . . . . . . . . . . . . . . . . After airplane has stopped:2. PARK BRAKE lever PARK. . . . . . . . . . . . . . . 3. THRUST lever (affected engine) CUT OFF. . .

In case of ENGINE FIRE:4. ENG FIRE button

(affected engine) LIFT security cover. . . . . . . . . . . . . . . . . . and PUSH

After 10 sec:5. Either illuminated BTL button PUSH. . . . . . .

Check DIS light Illuminated. . . . . . . . . . . . . . . . . . .

If ENG FIRE (WARNING) still persists after 30 sec:6. Other illuminated BTL button PUSH. . . . . . . .

Check DIS light Illuminated. . . . . . . . . . . . . . . . . . . 7. GROUND EVACUATION

procedure Apply IF REQUIRED. . . . . . . . . . . . . . . . . . . . . . . . END

In case of ENGINE FAILURE or SEVERE DAMAGE:4. GROUND EVACUATION

procedure Apply IF REQUIRED. . . . . . . .

END


May 05/99


LH or RH ENG FIRE or SEVERE DAMAGEor ENGINE FAILURE DURING TAKEOFF

after V1 and IN FLIGHTAt safe altitude:

1. THRUST lever (affected engine) IDLE then CUT OFF. . . 2. DC/AC TIE button On (closed). . . . . . . . . . . . . . . . 3. XBLEED button On. . . . . . . . . . . . . . . . .

In case of ENGINE FIRE:4. ENG FIRE button

(affected engine) LIFT security cover . . . . . . . . . . . . . . . . . . and PUSH

After 10 sec:5. Either illuminated BTL button PUSH. . . . . . .

Check DIS light Illuminated. . . . . . . . . . . . . . . . . . .

6. JETPMP button (affected engine) OFF. . .

If ENG FIRE (WARNING) still persists after 30 sec:7. Other illuminated BTL button PUSH. . . . . . . .

Check DIS light Illuminated. . . . . . . . . . . . . . . . . . . 8. Land at the nearest suitable airport9. SINGLE ENGINE OPERATION

procedure Apply. . . . . . . . . . . . . . . . . . . . . . . . END

In case of ENGINE SEVERE DAMAGE:4. Land at the nearest suitable airport5. SINGLE ENGINE OPERATION

procedure Apply. . . . . . . . . . . . . . . . . . . . . . . .

END

contd next page


May 05/99


contd

3. Land at the nearest suitable airport3. ENGINE AIRSTART procedureApply only if no engine or

FADEC damage isindicated or suspected

END

3.SINGLE ENGINE OPERATIONprocedure Apply. . . . . . . . . . . . . . . . . . . .

END

LH or RH OIL PRSIN FLIGHT

1. Oil pressure (affected engine) Check. . . . . . . If OIL PRESS in white range (36 110 PSI)

2. Normal thrust (affected engine) Maintain. . . . . . 3. Engine indications Monitor. . . . . . . . . . . . . . . . .

END

If OIL PRESS in amber range (20 36 PSI or 80 220 PSI)2. THRUST lever (affected engine) Reduce THRUST. . . . .

NOTE: If deemed necessary for safety reasons, the affected engine may be used.

3. Engine indications Monitor. . . . . . . . . . . . . . . . . END

If OIL PRESS below 20 PSI:2. THRUST lever (affected engine) IDLE then CUT OFF. . . . . 3. SINGLE ENGINE OPERATION



May 05/99


APU FIRE or SEVERE DAMAGE1. APU FIRE button LIFT security cover . . . . . . . . . . . . . . . . .

and PUSHNOTE: Activation of the APU FIRE button will also:

initiate an automatic APU shut down. close the APU fuel shut off valve. remove power from the APU (starter) generator. close the BLEED air load control valve (the BLEED air load.

control valve status can be checked on the APU page). cause the APU FAIL CAUTION to illuminate..

After 10 sec:2. Illuminated BTL button PUSH. . . . .

Check DIS light Illuminated. . . . . . . . . . . 3. APU MASTER button Off. . . . . .

If on ground:4. Order the ground crew to check the APU compartment

for fire.If the APU fire still exists:

5. GROUND EVACUATION procedure Apply. 6. Fire fighting (by ground crew) Initiate through the ground. . . . . .

fire fighting door or bypushing the APU FIREbutton on the APU groundcontrol panel

END

If in flight:4. Land at the nearest suitable airport

END


May 05/99


BAT 1 or BAT 2 OVHT1. BAT button (affected battery) OFF. . . . . . . .

If associated BAT OVHT light remains illuminated (after 2 min):2. Land at the nearest suitable airport

END

If associated BAT OVHT light extinguishes:

END

PFD1. Refer to STBY instruments

2. STBY instruments and PFDs Compare to determine. . . . . . . incorrect parameters

On Reversionary Mode Controller:3. Select the following reversions until the PFD WARNING

disappears: ATT/HDG: position 1 then NORM, then 2, then NORM again ADC: position 1 then NORM, then 2, then NORM again SG: position 1 then NORM, then 2, then NORM again

NOTE: If the PFD WARNING is replaced by an avionic relatedCAUTION, continue with the relevant procedure in 031000.

4. CREW AWARENESS of lost redundancy5. Continue to crosscheck STBY instruments


May 05/99


DOORS1. SEAT BELT / NO SMOKING

switches ON. . . . . . . . . . . . . . . . . . . . . 2. DOOR UNLOCKED Identify by OPEN WARNING. . . . . . . . . . .

on DOORS page if available3. Crew/Passengers Secure. . . . . . . . . . . . . 4. Airspeed Reduce to below . . . . . . . . . . . . . . . . . . . . .

150 KIAS5. Land at the nearest suitable airport Avoid descent rate

above 2500 FPM Keep positive DIFF PRSS


May 05/99


CAB ALT

1. Crew oxygen masks DON 100%. . . . . . . . . . 2. Oxygen mask mike Activateadjust speaker. . . . . . . . . . .

VOL or use headsetwith oxygen mask toestablish crewcommunication

3. SEAT BELT/ NO SMOKINGswitches ON. . . . . . . . . . . . . . . . . . . . .

4. CABIN ALTITUDE and RATE Check. . . 5. PRESSURIZATION

CONTROL MODE MAN. . . . . . . . . . . . . 6. MAN CAB ALT selector DN. . . . . . . .

7. Descent Initiate to 10 000 ft or. . . . . . . . . . . . . . . . . . . . . . minimum enroute altitude whichever is higher

If CABIN ALTITUDE can be controlled or CAB ALT Cautionextinguishes:8. PRESSURIZATION

CONTROL MODE Leave in MAN. . . . . . . . . . . . . 9. CPCS AUTO FAIL procedure Apply. . .

If CABIN ALTITUDE cannot be controlled:10. OXYGEN DROPOUT switch Unlatch MAN. . .

If DROPOUT unsuccessful:11. OXYGEN SEPARATION VALVE OPEN.

If flight is continued above 10 000 ft:12. Crew oxygen masks NORM. . . . . . . . . . . 13. Oxygen duration Check refer to the. . . . . . . . . . . . . .

OXYGEN CONSUMPTIONtables 1 and 2 below. Add theoxygen consumption requiredfor descent (table 1) to theoxygen consumption requiredfor 2 pilots at the altitude to beflown (table 2) When thisoxygen quantity is eachedproceed with step 14.

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May 05/99


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14. OXYGEN PAXSUPPLY button OFF (closed). . . . . 15. OXYGEN SEPARATION VALVE CLOSE. . . . . 16. Advise cabin attendant that only FIRST AID OXYGEN is

available.

OXYGEN CONSUMPTION (%) FOR FLIGHT CREW AND PASSENGERSIN DESCENT to 10 000 FTIN DESCENT to 10 000 FT

34% RESERVE INCLUDED CREW OXYGEN MASKS DEMAND REGULATORS IN NORM or 100% MODE

Descent rate (ft/min) 1 000 1 500 2 000 3 00031 000 98 82 69 56

28 000 88 68 58 48Initial

altitude 25 000 70 56 49 42(feet)

20 000 47 40 37 33

15 000 31 29 28 27

OXYGEN CONSUMPTION TABLE 1(77 cuft OXYGEN BOTTLE)

OXYGEN CONSUMPTION (% per hour) FOR 2 PILOTS AT CONSTANT ALTITUDE

Altitude (feet) 15 000 20 000 25 000 28000 31 000% per hour in NORM MODE 12 14 17 21 22

% per hour in 100% MODE 52 42 31 25 23

OXYGEN CONSUMPTION TABLE 2(77 cuft OXYGEN BOTTLE)


May 05/99


OXYGENNOTE: OXYGEN low pressure WARNING of the passenger

system is suppressed below 14 000 feet.1. Descent Initiate to 10 000 ft or. . . . . . . . . . . . . . . . . . . . . . . . . .

minimum enroute altitude whichever is higher

T/O CONFIG1. Airplane STOP. . . . . . . . . . . . . . . . . . . . . . . . . .

LAV FIRE1. Crew oxygen masks DON IF REQUIRED, check . . . . . . . . . . . . . . . . . . . . .

100%2. Oxygen mask mike Activate IF REQUIRED, . . . . . . . . . . . . . . . . . . . . . .

adjust speaker VOL or use headset with oxygen mask to establish crew communication

3. RECIRC FAN button OFF. . . . . . . . . . . . . . . 4. ECS FLOW MODE button HIGH. . . . . . . . . . 5. Fire source Locate and advise cabin. . . . . . . . . . . . . . . . . . . . . . .

attendant to extinguish fireIf fire cannot be eliminated:6. DESCENT AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . 7. CAB DUMP button DUMP if below 12 000 ft. . . . . . . . . . . . . . . . 8. Land at the nearest suitable airport

WARNING: WHETHER OR NOT SMOKE HAS DISSIPATED, IF IT CANNOT BE VISIBLY VERIFIED THAT THE FIRE HASBEEN EXTINGUISHED AFTER FOLLOWING THESE PROCEDURES LAND IMMEDIATELY AT THE NEAREST SUITABLE AIRPORT.


May 05/99




May 05/99


L R DC GEN FAIL1. Pilot flying LH seat. . . . . . . . . . . . . . . . . . . . . . . . 2. GENLH/RH buttons OFF then on (reset). . . . . . . . . . . . . . 3. DC TIE button ON then off (reset). . . . . . . . . . . . . . . . . . . . CAUTION: Do not attempt an inflight start of the APU with both

generators inoperative.If APU is running:

4. GENAPU button ON. . . . . . . . . . . . . . . . . 5. Ground cooling and RECIRC fan OFF. . . . 6. DC TIE button ON. . . . . . . . . . . . . . . . . . . . 7. Land at the nearest suitable airport

END

If APU is >not< running: If only one generator is restored:

4. L or R DC GEN FAIL procedure Apply. . . . . END

If both generators still failed:4. TRU switch Unlatch select L or R. . . . . . . . . . . . . . . . . . . . . . .

Confirm ESSENTIAL BUS is powered on ELECTR system pageCAUTION: Maximum flight time is 70 minutes because DC BUS 1

and 2 are powered by the batteries only.If TRU does not supply ESSENTIAL BUS:5. Autopilot Disengage. . . . . . . . . . . . . . . . . . . . . . . . . 6. Revert to STBY instrumentsCAUTION: If TRU power cannot be recovered, max flight time on

both batteries is 30 minutes, provided the battery loadis reduced by pulling c/bs.

7. BAT load Reduce by pulling the. . . . . . . . . . . . . . . . . . . . . . . . . following marked c/bswithin 5 minutes:

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May 05/99


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DAU CH 1B A08 IRS 2 AUX DAU CH 2B C27PFD1 A11 (if installed) A26 IRS 2 PRI orMFD1 A12 PFD 2 A27 AHRS 2 PRI C28EICAS A13 MFD 2 A28IAC1 A14 COM2 B 1ADC1 A15 FMS CDU B 4 LDG LTS RH1 E27

IAC 2 B27 LDG LTS RH2 E28ADC 2 B28 PITOT HEAT LH E13

TONE GEN 1 A17 ELPMP LH C14 TAT HEAT E21BACKUP BATT A18 ELPMP RH C25

NOTE: The PROBE switch lights on the overhead panel indicatecombined sensor heating functions. After completion of loadshedding the correct sensor heating functions can beconfirmed on the RMU backup page.

For remaining services refer to the end of procedure8. EMG LIGHTS switch OFF. . . . . . . . . . . . . . . 9. ENGINE START selectors OFF. . . . . . . . . .

10. HYD PWR STBY selector OFF. . . . . . . . . .

NOTE: Attain visual flight conditions as soon as possible.11. Land at the nearest suitable airport

Before starting the normal BEFORE LANDING procedure:12. PACK LH/RH buttons OFF. . . . . . . . . . . . . . 13. HYD PWR STBY selector AUTO. . . . . . . . . .

REMAINING SERVICES protected by resetable C/Bs:AVIONICS/FLIGHT INSTRUMENTS

RMU1 & 2 AOA and stall warning LHSTBY attitude indicator DAU 1A & 2ASTBY airspeed & altimeter Flight data recorderClearance delivery head Cockpit voice recorderClock 1

ELECTRICSInverter 1 Emergency power supplyTransformer rectifier unit DC TIE indicator

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May 05/99


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REMAINING SERVICES protected by resetable C/Bs:

COMMUNICATION / NAVIGATIONAudio panel 1 & 2 DME1COM1 ADF1ATC1 PAX adress systemNAV1

FLIGHT CONTROLSElevator trim STBY rudder trimAileron trim Trim indicationsRudder trim Rudder limiterSTBY elevator trim STBY rudder limiterSTBY aileron trim Flaps

FUELCrossfeed LH & RH Shut off valve LH & RHJetpump LH & RH

HYDRAULICS LANDING GEARAnti skid NORM & ALT HYD A & B pumpsNose wheel steering HYD STBY pump (all modes)Gear retraction & extension All HYD pressure indicationsProxi

LIGHTS / SIGNSNAV lights STBY instrument lightsAnti collision lights Red warning panelStrobe lights Boarding lightsWing inspection lights Emergency exit lightsLanding lights LH PAX & Lavatory signs

FIRE PROTECTIONTotal fire protection system

CPCS / OXYGENOxygen system Pressurization system

ENGINEIgnition LH & RH

Oil pressure indication LH & RH

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May 05/99


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REMAINING SERVICES protected by resetable C/Bs:

ECSEngine bleed valve LH & RH Pack LH & RHCross bleed ECS flow modeEngine bleed leak detectionLH & RH

Temperature control of flight and PAXcompartment

ICE PROTECTIONIce detector Windshield wipers LH & RHDeice pressure LH & RH Engine intake antiice LH & RHAirfoil deice single & cycle STBY pitot heat

Elevator & rudder horn deiceWindshield heat front and both sides

LAVATORYWater and waste

L R ALT FAILBOTH ALTERNATORS LOST

1. ALT LH and RH buttons OFF then ON (reset). . . . . . . . . . . . If one alternator is restored:

2. L or R ALT FAIL procedure Apply. . . . . . . . .

END

If both alternators still failed:2. Avoid icing conditions3. Land at the nearest suitable airport4. HYD A PMP FAIL and

HYD B PMP FAIL procedure Apply. . . . . . . . The following services are lost: HYD A PMP and HYD B PMP with associated systems Ice detector Windshield heating Horn deicing

END


May 05/99


AILERON CTRL SYSTEM JAMMED1. Autopilot Disconnect. . . . . . . . . . . . . . . . . . . . . . 2. Pilots (both) Apply a ROLL force in the. . . . . . . . . . . . . . . . . . .

same direction to openaileron disconnect unit

3. AIL DISCONNECT procedure Apply. . . . .

ELEVATOR CTRL SYSTEM JAMMED1. Autopilot Disconnect. . . . . . . . . . . . . . . . . . . . . . 2. Pilots (both) PUSH or PULL in the same. . . . . . . . . . . . . . . . . . .

direction to open elevator disconnect unit

3. ELEV DISCONNECT procedure Apply. . .


May 05/99




May 05/99


SMOKE

1. Crew oxygen masks DON check 100%. . . . . . . . . . . . . . . . . . 2. Smoke goggles DON IF REQUIRED, then. . . . . . . . . . . . . . . . . . . . . . .

oxygen mask EMERG3. Oxygen mask mike Activate adjust speaker VOL . . . . . . . . . . . . . . . . . . .

or use headset with oxygenmask to establish crewcommunication

4. Land at the nearest suitable airport5. SEAT BELT/NO SMOKING

switches ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6. RECIRCEFISAVIONIC FAN

buttons OFF. . . . . . . . . . . . . . . . . . . . . . . . . 7. ECS FLOW MODE button HIGH. . . . . . . . . 8. Smoke source Locate and extinguish fire. . . . . . . . . . . . . . . . . . . NOTE: If fire fighting is required, use protective breathing equipment

and hand fire extinguisher.

IF SMOKE IS EVIDENT IN FLIGHT COMPARTMENT:9. MAN CAB ALT selector Turn gradually to the . . . . . . . . . . . .

UP position10. EMERGENCY DESCENT Initiate. . . . . . . . . .

Below 14 000 ft:11. MAN CAB ALT selector Full up. . . . . . . . . . . . 12. If BLEED source is suspected, proceed with AIRCONDITION

SMOKE REMOVAL procedure if time permits.If ELECTRICAL source is suspected, proceed withELECTRICAL SMOKE REMOVAL procedure if time permits.

END

IF SMOKE IS EVIDENT IN PAX COMPARTMENT:

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May 05/99


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9. Flight compartment door Ensure closed. . . . . . . . . 10. EMERGENCY DESCENT Initiate. . . . . . . . 11. CAB DUMP button DUMP if below 12 000 ft. . . . . . . . . . . . . . 12. If BLEED source is suspected, proceed with AIRCONDITION

SMOKE REMOVAL procedure if time permits.

If ELECTRICAL source is suspected, proceed withELECTRICAL SMOKE REMOVAL procedure if time permits.

END

AIRCONDITION SMOKE REMOVAL If smoke is primarily entering the flight compartment:

1. RH ECS BLEED button orAPU BLEED button (if used) OFF. . . . . .

2. XBLEED button On. . . . . . . . . . . . . . . . 3. GROUND EVACUATION

procedure Apply IF REQUIRED. . . . . . . . . . . . . . . . . . . . . . END

If smoke is primarily entering the PAX compartment:1. LH ECS BLEED button OFF. . . . . . . . . . . 2. XBLEED button On. . . . . . . . . . . . . . . . 3. GROUND EVACUATION

procedure Apply IF REQUIRED. . . . . . . . . . . . . . . . . . . . . . END


May 05/99


ELECTRICAL SMOKE REMOVALNOTE: When any one of the following steps eliminates the smoke, stop

procedure.1. Pilot flying LH seat. . . . . . . . . . . . . . . . . . . . . 2. DC TIE Confirm Off. . . . . . . . . . . . . . . . . . . . . . . . 3. NONESS BUS 1 button OFF. . . . . . . . . Wait to see if smoke source is eliminated if not:4. GENLH button OFF. . . . . . . . . . . . . . . . . 5. BAT 1 button OFF. . . . . . . . . . . . . . . . . . . Wait to see if smoke source is eliminated if not:6. BAT 1 button ON. . . . . . . . . . . . . . . . . . . 7. GENLH button ON. . . . . . . . . . . . . . . . . 8. NONESS BUS 1 button ON. . . . . . . . . 9. NONESS BUS 2 button OFF. . . . . . . . . Wait to see if smoke source is eliminated if not:10. TONE GEN 1 C/B (A17) PULL to eliminate nuisance . . . . . . . . . .

gear warning11. GENAPU button OFF IF USED. . . . . . . . . . . . . . . 12. GENRH button OFF. . . . . . . . . . . . . . . . . 13. BAT 2 button OFF. . . . . . . . . . . . . . . . . . .

NOTE: AUDIO panel 2 is inoperative as long as DC BUS 2 is withoutpower, no intercommunication on RH side available.

Wait to see if smoke source is eliminated if not:14. GENAPU button ON IF DESIRED. . . . . . . . . . . . . . . 15. BAT 2 button ON. . . . . . . . . . . . . . . . . . . 16. GENRH button ON. . . . . . . . . . . . . . . . . 17. TONE GEN 1 C/B (A17) PUSH. . . . . . . . . . 18. NONESS BUS 2 button ON. . . . . . . . . 19. INV 1 button OFF. . . . . . . . . . . . . . . . . . . . 20. INV 2 button OFF. . . . . . . . . . . . . . . . . . . .

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May 05/99


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Wait to see if smoke source is eliminated if not:21. INV 1 button ON. . . . . . . . . . . . . . . . . . . . . . 22. INV 2 button ON. . . . . . . . . . . . . . . . . . . . . . 23. AC TIE CHECK off. . . . . . . . . . . . . . . . . . . . . . . . . . . 24. ALT LH button OFF. . . . . . . . . . . . . . . . . . . . Wait to see if smoke source is eliminated if not:25. ALT LH button ON. . . . . . . . . . . . . . . . . . . . 26. ALT RH button OFF. . . . . . . . . . . . . . . . . . . . Wait to see if smoke source is eliminated if not:27. ALT RH button ON. . . . . . . . . . . . . . . . . . . . 28. Pilot flying RH seat IF DESIRED. . . . . . . . . . . . . . . . . . . . . . . . 29. MFD 2 switch Select EICAS. . . . . . . . . . . . . . . . . . . . . 30. SG switch SG 2. . . . . . . . . . . . . . . . . . . . . . . . 31. DAU switch DAU 2B. . . . . . . . . . . . . . . . . . . . . . . 32. TONE GEN 1 and 2 c/bs (A17/N2) PULL to eliminate. . .

nuisance gear warning33. Pull c/bs on the ESSENTIAL BUS until smoke source is

eliminated, or until all c/bs are pulled.NOTE: Pulling all c/bs on the ESSENTIAL BUS will not affect the

functionality of the copilots MFD and PFDIf smoke is eliminated:

If desired, reset individual c/bs for desired equipment, wait aminimum of one minute between resetting c/bs. If smoke startsagain pull c/b.The following initial order of restoring c/bs is recommended:

DAU 1A (A9) to restore LH engine indications AUDIO 1 (B26) to restore LH AUDIO panel OIL PRSS LH (D13) and OIL PRSS RH (D23) to restore oil

pressure indications ELEV TRIM (B9), AIL TRIM (B10) and RUDDER TRIM (B11) to

restore normal trims34. GROUND EVACUATION procedure Apply IF REQUIRED.

END


May 05/99


SMOKE LAV1. Crew oxygen masks DON IF REQUIRED, check. . . . . . . . . . . . .

100%2. Oxygen mask mike Activate IF REQUIRED,. . . . . . . . . . . . . .

adjust speaker VOL or useheadset with oxygen mask toestablish crew ommunication

3. RECIRC FAN button OFF. . . . . . . . . . . . . 4. ECS FLOW MODE button HIGH. . . . . . . . 5. Smoke source Locate and advise cabin. . . . . . . . . . . . . . . . . .

attendant to extinguish fireNOTE: If there is visible fire associated with smoke, fight the fire

using protective breathing equipment, fire gloves and handfire extinguisher.

If smoke cannot be eliminated:6. DESCENT AS REQUIRED. . . . . . . . . . . . . . . . . . . . . 7. CAB DUMP button DUMP if below 12 000 ft. . . . . . . . . . . . . . 8. Land at the nearest suitable airportWARNING: WHETHER OR NOT SMOKE HAS DISSIPATED, IF IT

CANNOT BE VISIBLY VERIFIED THAT THE FIRE HASBEEN EXTINGUISHED AFTER FOLLOWING THESEPROCEDURES LAND IMMEDIATELY AT THE NEARESTSUITABLE AIRPORT.


May 05/99


HYDRAULIC FUMES1. RECIRC FAN button OFF. . . . . . . . . . . . . 2. HYD PWR SYSTEM A and

SYSTEM B buttons OFF. . . . . . . . . . . . . . 3. HYD PWR STBY selector OFF. . . . . . . . NOTE: Rollspoilers will be inoperative resulting in reduced

ROLL performance.Before the normal BEFORE LANDING procedure:1. HYD PWR SYSTEM A and

SYSTEM B buttons ON. . . . . . . . . . . . . . 2. HYD PWR STBY selector AUTO. . . . . . . . 3. Continue normal operationAfter airplane has stopped:4. GROUND EVACUATION

procedure Apply IF REQUIRED. . . . . . . . . . . . . . . . . . . . . .


May 05/99


DOUBLE ENGINE FAILURE APU INOPERATIVE and ALL ALTITUDES or

APU NOT OPERATING and ABOVE 20 000 FEET

1. Airspeed Above 200 KIAS. . . . . . . . . . . . . . . . . . . . . . . . . . 2. THRUST levers (both) CUT OFF. . . . . . . . . . . . . .

Either Engine:3. WINDMILLING AIRSTART PERFORM. . . . . . . . . . . 4. Minimum safe altitude Observe. . . . . . . . . . . . . . 5. ATC/Transponde Notify / 7700. . . . . . . . . . . . . . . . . . .

2nd Engine:6. WINDMILLING AIRSTART or AIRSTART using

ENGINE CROSS BLEED air supply PERFORM. . .

If 2nd Engine AIRSTART is >not< successful:7. SINGLE ENGINE

OPERATION procedure Apply. . . . . . . . . . . . . . . . . . . . . .

END

If NEITHER Engine starts:8. THRUST levers (both) CUT OFF. . . . . . . . . . . 9. FORCED LANDING procedure Apply. . . .

(Note GLIDE RANGE table below)END

ALTITUDE (ft) RANGE (NM)30 00025 00020 00015 00010 000

5 000

837056422814

Conditions: Engines windmilling FLAPS 0, ISA, zero wind Weight: 13 500 kg (29 760 lb)

GLIDE RANGE 150 KIAS


May 05/99


DOUBLE ENGINE FAILUREAPU AVAILABLE and BELOW 20 000 FEET

1. Airspeed 150 KIAS. . . . . . . . . . . . . . . . . . . . . . . . 2. THRUST levers (both) CUT OFF. . . . . . . . . . . . 3. APU START Perform IF REQUIRED. . . . . . . . . . . . . . . . . . . . . .

If APU start is >not< successful:4. Airspeed Above 200 KIAS. . . . . . . . . . . . . . . . . . . . . . . . 5. WINDMILLING AIRSTART PERFORM. . . . . . . . .

END

If APU is running:Either Engine:4. STARTER ASSISTED AIRSTART using

APU BLEED air supply PERFORM. . . . . . . . . . . 5. Minimum safe altitude Observe. . . . . . . . . . . . 6. ATC/Transponder Notify / 7700. . . . . . . . . . . . . . . .

2nd Engine:7. WINDMILLING or

STARTER ASSISTED AIRSTART PERFORM. . . If 2nd Engine AIRSTART is >not< successful: 8. SINGLE ENGINE

OPERATION procedure Apply. . . . . . END

If NEITHER Engine starts: 8. THRUST levers (both) CUT OFF 9. FORCED LANDING procedure Apply

(Note GLIDE RANGE table on page before)END


May 05/99


FORCED LANDING1. Flight attendant Advise to prepare cabin for. . . . . . . . . . . . . . . . . . .

emergency landing2. Pilot flying LH seat. . . . . . . . . . . . . . . . . . . . . . . . 3. SEAT BELT/NO SMOKING switches ON.

IF LANDING is IMMINENT:In place of the normal APPROACH / LANDING procedures:4. CAB DUMP button DUMP. . . . . . . . . . . . . . . . 5. HYD PWR STBY selector CONT HYD B PRSS. . . . . . . . . .

HIGH Caution mayilluminate

6. Landing gear AS REQUIRED. . . . . . . . . . . . . . . . . . . . . 7. FLAPS 32. . . . . . . . . . . . . . . . . . . . . . . . . . . 8. Minimum approach airspeed VREF. . . . . . . . 9. LAND LH /RH lights switches AS REQUIRED. . . . . . . Before impact:10. ENG FIRE buttons (2) LIFT security cover and. . . . . . . . . . . . .

PUSH11. EMG LIGHTS switch ON. . . . . . . . . . . . . . . 12. Brace for impact ORDER. . . . . . . . . . . . . . . . . . 13. Shoulder harness (both) Tighten and LOCK. . . . . . . . . . . . During LDG up landing:14. HYD PWR STBY selector and ANTICOLL

light switch OFF . . . . . . . . . . . . . . . . . . . . . . . 15. HYD PWR SYSTEM A

and SYSTEM B button (both) OFF. . . . . . . After impact (when airplane has stopped):16. All Illuminated FIRE BTL buttons PUSH. . . . 17. GROUND EVACUATION


IF LANDING is >NOT< IMMINENT (more than 10 minutes totouchdown):

Conserve DC power:4. EMG LIGHTS switch OFF. . . . . . . .

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May 05/99


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5. LAND LH/RH lights switches OFF. . . . . . . . . . 6. ENGINE START selectors OFF. . . . . . . . . . . . 7. HYD PWR STBY selector OFF. . . . . . . . . . . . 8. ELPMP buttons (both) OFF. . . . . . . . . . . . . . . 9. ELPMP AUTO buttons (both) OFF. . . . . . . . . 10. Revert to STBY instruments11. Pull the following marked c/bs:

DAU CH 1B A8 IRS 2 AUX DAU CH 2B C27PFD1 A11 (if installed) A26 IRS 2 PRI orMFD1 A12 PFD 2 A27 AHRS 2 PRI C28EICAS A13 MFD 2 A28IAC1 A14 COM2 B 1ADC1 A15 FMS CDU B 4 LDG LTS RH1 D27

IAC 2 B27 LDG LTS RH2 D28ADC 2 B28 PITOT HEAT LH E13

TONE GEN 1 A17 ELPMP LH C14 TAT HEAT E23BACKUP BATT A18 ELPMP RH C25

12. EMERGENCY LANDING procedure Review. . . In place of the normal APPROACH / LANDING procedures:13. CAB DUMP button DUMP. . . . . . . . . . . . . . . . . . 14. HYD PWR STBY selector CONT HYD B PRSS. . . . . . . . . . . .

HIGH Caution mayilluminate

15. Landing gear AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . . 16. FLAPS 32. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17. Minimum approach airspeed VREF. . . . . . . . . . 18. LAND LH /RH lights switches AS REQUIRED. . . . . . . . . During LDG up landing:19. HYD PWR STBY selector and

ANTICOLL light switch OFF. . . . . . . . . . . . . . 20. HYD PWR SYSTEM A

and SYSTEM B button (both) OFF. . . . . . . . .

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May 05/99


contd

Before impact:21. ENG FIRE buttons (2) LIFT security cover. . . . . . . . . . . . . . .

and PUSH22. EMG LIGHTS switch ON. . . . . . . . . . . . . . . . . 23. Brace for impact ORDER. . . . . . . . . . . . . . . . . . . . After impact (when airplane has stopped):24. All Illuminated FIRE BTL buttons PUSH. . . . . . 25. GROUND EVACUATION

procedure Apply. . . . . . . . . . . . . . . . . . . . . . . . . .

END


May 05/99




May 05/99


RAPID DECOMPRESSION1. Crew oxygen masks DON 100%. . . . . . . . . . . . . . 2. Oxygen mask mike Activate adjust speaker VOL. . . . . . . . . . . . . . . . . .

or use headset with oxygen mask to establish crewcommunication

3. SEAT BELT/ NO SMOKINGswitches ON. . . . . . . . . . . . . . . . . . . . . . . . . . . .

4. EMERGENCY DESCENT Initiate IF REQUIRED . . . . . . . . . . . refer to EMERGENCY DESCENT procedure in this Subsection


May 05/99


EMERGENCY DESCENT1. SEAT BELT / NO SMOKING

switches ON. . . . . . . . . . . . . . . . . . . . . . . 2. THRUST levers IDLE. . . . . . . . . . . . . . . . . 3. Airspeed MMO/VMO. . . . . . . . . . . . . . . . . . . . . . CAUTION: If structural integrity is in doubt reduce airspeed

and avoid high maneuvering loads as appropriate.4. OXYGEN DROPOUT switch Unlatch MAN IF. . . . .

REQUIRED5. ATC/Transponder Notify / 7700. . . . . . . . . . . . . . . 6. Level off At 10 000 ft or minimum. . . . . . . . . . . . . . . . . . . . . . .

enroute altitude whichever is higher

If flight is continued above 10 000 ft:7. Crew oxygen masks NORM. . . . . . . . . . . . . 8. Oxygen duration Check refer to the. . . . . . . . . . . . . . . .

OXYGEN CONSUMPTIONtables 1 and 2 in this Section. Add the oxygen consumption required fordescent (table 1) to theoxygen consumption requiredfor 2 pilots at the altitude tobe flown (table 2).When this oxygen quantity isreached proceed with step 9.

9. OXYGEN PAXSUPPLY button OFF (closed). . . 10. OXYGEN SEPARATION VALVE CLOSE. . . 11. Advise cabin attendant that only FIRST AID OXYGEN is

available.


May 05/99


EMERGENCY LANDING1. Brief crew on type of emergency 2. Consider extreme situations after an emergency landing

e.g. airplane attitude after an unsafe gear landing3. Secure all loose items4. Notify ATC as appropriate5. Review desired actions and crew coordination including GROUND

EVACUATION procedure in this Section6. Check shoulder harness tight and locked

GROUND EVACUATION1. PARK BRAKE lever PARK. . . . . . . . . . . . 2. THRUST levers IDLE then CUT OFF. . . . . . . . . . . . . . . . 3. ATC Notify if time permits. . . . . . . . . . . . . . . . . . . . . . . . . . 4. EMG LIGHTS switch ON. . . . . . . . . . . 5. APU (if running) STOP. . . . . . . . . . . . . . . 6. CAB DUMP button DUMP. . . . . . . . . . . . 7. Evacuation Initiate in case of fire to. . . . . . . . . . . . . . . . . . .

nonaffected side only in case of ditching useexits above the waterlineonly

8. BAT1 and 2 buttons OFF just before leaving. . . . . . . . . . . . . airplane


May 05/99



328JETQuick Reference HandbookAbnormal Procedures

May 05/99

EFFECTIVITY : ALL ABNORMAL Page 01

TABLE OF CONTENTS

SUBJECTPAGE

SECTION

ECS / OXY ABNORMAL 10

AUTO FLIGHT ABNORMAL 20

ELECTRIC ABNORMAL 30

FIRE PROTECTION SYSTEM MALFUNCTION ABNORMAL 40

FLIGHT CONTROLS ABNORMAL 50

FUEL ABNORMAL 60

HYDRAULICS ABNORMAL 70

ICE PROTECTION ABNORMAL 80

INDICATING / RECORDING ABNORMAL 90

LANDING GEAR ABNORMAL 100

NAVIGATION ABNORMAL 110

PNEUMATIC ABNORMAL 120

AUXILIARY POWER UNIT (APU) ABNORMAL 130DOORS ABNORMAL 140

ENGINE ABNORMAL 150


May 05/99

EFFECTIVITY : ALL ABNORMALPage 02



May 05/99

EFFECTIVITY : ALL ECS / OXY ABNORMAL Page 1 01

TABLE OF CONTENTS

SUBJECTPAGE

SECTION

ECS / OXY

L or R PACK FAIL Caution 1 1AVIONIC FAN FAIL Caution 1 3EFIS FAN FAIL Caution 1 3HX FAN FAIL Caution 1 3REC FAN FAIL Caution 1 3CPCS MISCOMPARE Caution 1 4CPCS AUTO FAIL Caution 1 5CAB DIFF PRSS Caution 1 6OXY QTY FAIL Caution 1 6


May 05/99

EFFECTIVITY : ALL ECS / OXY ABNORMALPage 1 02



May 05/99


L or R PACK FAIL ECS OPERATION WITH MAIN ENGINE BLEED SUPPLY:

1. ECS BLEED button (affected side) OFF. . 2. PACK button (affected side) OFF. . . . . . . . If OVPRSS or OVHT is illuminated on the ECS page:

3. XBLEED button ON. . . . . . . . . . . . . . . . . . 4. PACK button (affected side) ON (reset after 2 minutes). . . . . . . .

If the PACK FAIL CAUTION extinguished:END

If the PACK FAIL CAUTION is not removed or reoccurs:5. PACK button (affected side) OFF. . . . 6. Maximum altitude 25 000 ft. . . . . . . . . . . . . 7. XBLEED button OFF. . . . . . . . . . . . . . 8. ECS FLOW MODE button HIGH confirm. . . . . .

END

ECS OPERATION WITH APU BLEED SUPPLY:NOTE: When using APU BLEED supply for ECS operation, a pack

overheat condition is the only cause to trigger the L or RPACK FAIL CAUTION.

1. PACK button (affected side) OFF . . . . . . . . wait 2 minutes, then on(reset)

If the PACK FAIL CAUTION extinguished:END

contd next page


May 05/99


contd

If the PACK FAIL CAUTION is not removed or reoccurs:2. PACK button (affected side) OFF. . . . 3. Maximum altitude 25 000 ft. . . . . . . . . . . . . 4. ECS FLOW MODE button HIGH. . . . . . 5. ECS BLEED button

(nonaffected side) ON confirm. . . . . . . . . . . . 6. APU BLEED button OFF. . . . . . . . . . . . 7. XBLEED button OFF. . . . . . . . . . . . . .

END


May 05/99


AVIONIC FAN FAIL1. AVIONIC FAN button OFF. . . . . . . . . . . . . . 2. ECS FLOW MODE button HIGH performance . . . . . . . . . .

permitting

EFIS FAN FAIL1. EFIS FAN button OFF. . . . . . . . . . . . . . . . . . 2. FLOW MODE button HIGH performance . . . . . . . . . . . . . . .

permitting

HX FAN FAILIf the affected HX FAN can be identified:

1. PACK button (affected side) OFF below 120 KIAS. . . . . . . . END

If the affected HX FAN >cannot< be identified:If L or R PACK FAIL CAUTION illuminates:1. PACK button (affected side) OFF. . . . . . . .

REC FAN FAIL1. ECS FLOW MODE button HIGH performance . . . . . . . . . .

permitting2. RECIRC FAN button OFF. . . . . . . . . . . . . . .


May 05/99


CPCS MISCOMPARE1. CABIN ALTITUDE Check if within. . . . . . . . . . . . . . . . .

PRESSURIZATION SCHEDULE as given in the CPCS AUTO FAIL procedures:

2. CABIN RATE Check within limit:. . . . . . . . . . . . . . . . . . . . . 1 200 ft/min > CAB RATE > 1 500 ft/min

If CABIN ALTITUDE and RATE within limits:3. PRESSURIZATUION

CONTROL MODE Leave in AUTO. . . . . . . . . . . . . . . . . END

If CABIN ALTITUDE and RATE >not< within limits:3. PRESSURIZATION

CONTROL MODE MAN. . . . . . . . . . . . . . . . . END


May 05/99


CPCS AUTO FAIL1. DIFF PRSS and CABIN ALTITUDE Check and monitor. . 2. PRESSURIZATION

CONTROL MODE MAN. . . . . . . . . . . . . . . . . 3. MAN CAB ALT selector AS REQUIRED to follow. . . . . . . . . . . .

PRESSURIZATION SCHEDULE do not exceed a CABIN DIFF PRESS of 6.75 psi do not exceed a CABIN ALT of 8 000 ft

PRESSURIZATION SCHEDULEPRESSUREALTITUDE

CABINALTITUDE

DIFFERENTIALPRESSURE

5 000 feet 300 feet 2.54 PSI10 000 feet 1 300 feet 4.09 PSI15 000 feet 2 400 feet 5.31 PSI20 000 feet 3 700 feet 6.21 PSI25 000 feet 5 400 feet 6.63 PSI30 000 feet 7 500 feet 6.73 PSI31 000 feet 8 000 feet 6.75 PSI

If CPCS AUTO FAIL caution extinguishes:4. PRESSURIZATUION

CONTROL MODE Leave in MAN. . . . . . . . . . . . . . . . . NOTE: The CPCS should remain in MAN to prevent any increase in

cabin altitude when returning to AUTO at high flight levels.Prior to landing:5. MAN CAB ALT selector Full UP. . . . . . . . . . . . NOTE: LAND ELEV window info will be inoperative.


May 05/99


CAB DIFF PRSSOn ground:

1. Doors Keep closed. . . . . . . . . . . . . . . . . . . . . . . . . . . . 2. CAB DUMP button DUMP. . . . . . . . . . . . . . . .

CPCS AUTO FAIL CAUTION Illuminated. . . . . . 3. MAN CAB ALT selector Full UP. . . . . . . . . . . . 4. Doors Can be opened. . . . . . . . . . . . . . . . . . . . . . . . . . . .

In flight:1. PRESSURIZATION

CONTROL MODE MAN. . . . . . . . . . . . . . . . . 2. CPCS AUTO FAIL procedure Apply. . . . . . .

OXY QTY FAIL 1. OXY PAX SUPPLY button OFF. . . . . . . . . .

2. Descent Initiate Maximum altitude. . . . . . . . . . . . . . . . . . . . . . . . . . 10 000 ft or minimum enroute altitude whicheveris higher


May 05/99

EFFECTIVITY : ALL AUTO FLIGHT ABNORMAL Page 2 01

TABLE OF CONTENTS

SUBJECTPAGE

SECTION

AUTO FLIGHT

AIL MISTRIM Caution 2 1EL MISTRIM NOSE UP or DN Caution 2 1EL TRIM FAIL Caution 2 2FGC DATA FAIL Caution 2 3FGC FAIL Caution 2 3FGC HDG HLD OFF Caution 2 3FGC LAT MODE OFF Caution 2 3FGC VERT MODE OFF Caution 2 3YD OFF Caution 2 4


May 05/99

EFFECTIVITY : ALL AUTO FLIGHT ABNORMALPage 2 02



May 05/99


AIL MISTRIM1. Rudder trim Check ball centered. . . . . . . . . . . . . . . . . . . . . . . 2. Aileron trim Trim in direction of green. . . . . . . . . . . . . . . . . . . . . . .

command arrow until AIL MISTRIM CAUTIONdisappears but not morethan 25% deflection.

NOTE: ROLL forces opposite to the green command arrow can beexpected if the autopilot is disengaged.

EL MISTRIM NOSE UP or DN If EL MISTRIM NOSE UP is illuminated:

1. Autopilot Disconnect expect. . . . . . . . . . . . . . . . . . . . . . . . . PITCH force DOWN

2. Elevator trim Trim AS REQUIRED. . . . . . . . . . . . . . . . . . . . . . EL MISTRIM NOSE UP CAUTION Extinguished. . . . . . . . . . . . . . . . . . . . . . . .

3. Autopilot Reengage if desired. . . . . . . . . . . . . . . . . . . . . . . . . END

If EL MISTRIM NOSE DN is illuminated:1. Autopilot Disconnect expect. . . . . . . . . . . . . . . . . . . . . . . . .

PITCH force UP2. Elevator trim Trim AS REQUIRED. . . . . . . . . . . . . . . . . . . . . .

EL MISTRIM NOSE DN CAUTION Extinguished. . . . . . . . . . . . . . . . . . . . . . . .

3. Autopilot Reengage if desired. . . . . . . . . . . . . . . . . . . . . . . . . END


May 05/99


EL TRIM FAIL1. Autopilot Disconnect expect pitch . . . . . . . . . . . . . . . . . . . . . . . . .

force UP or DN2. Elevator trim Trim as required. . . . . . . . . . . . . . . . . . . . . . NOTE: After pilot actuated autopilot disconnect the FGC goes

through a reset phase (approx. 20 sec) and the FGC FAIL CAUTION and FD FAIL on the PFD are displayed duringthis time.

When FGC FAIL has disappeared:3. Autopilot Reengage if desired. . . . . . . . . . . . . . . . . . . . . . . . .


May 05/99


FGC DATA FAIL1. Autopilot Disconnect be aware of . . . . . . . . . . . . . . . . . . . . . . . . .

any mistrim condition

FGC FAILIf FGC FAIL CAUTION disappears (auto reset in approx. 20 secs):1. Autopilot Reengage if desired. . . . . . . . . . . . . . . . . . . . . . . . .

FGC HDG HLD OFFNOTE: The PFD mode annunciation is ROL.1. Heading information

(coupled side) Xcheck with opposite . . . . . . . . . . . . . . . . . . . . PFD and magnetic compass

On coupled pilots display controller:2. HDG selector Reselect desired HDG. . . . . . . . . . . . . . . . . . . . .

On flight guidance controller:3. HDG mode Engage if desired. . . . . . . . . . . . . . . . . . . . . . .

FGC LAT MODE OFF1. Lateral navigation source Confirm. . . . . . . . . . . 2. Desired LAT mode parameter Confirm / reset. . . . . . . 3. Desired LAT mode Reengage if desired. . . . . . . . . . . . . . . .

FGC VERT MODE OFF1. Vertical navigation source Confirm. . . . . . . . . . 2. Desired VERT mode parameter Confirm / reset. . . . . 3. Desired VERT mode Reengage if desired. . . . . . . . . . . . . . .


May 05/99


YD OFF1. Airplane retrim all axes2. Yaw damper Reengage if desired. . . . . . . . . . . . . . . . . . . . . .


May 05/99

EFFECTIVITY : ALL ELECTRIC ABNORMAL Page 301

TABLE OF CONTENTS

SUBJECTPAGE

SECTION

ELECTRIC

BATT 1 or BATT 2 FAIL Caution 3 1INV 1 or INV 2 FAIL Caution 3 1L or R AC VOLT FAIL Caution 3 1L or R ALT FAIL Caution 3 2L or R DC GEN OVHT Caution 3 2L or R DC GEN FAIL Caution 3 3APU GEN OVHT Caution 3 3APU GEN FAIL Caution 3 3ESS BUS FAIL Caution 3 4NON ESS 1 or NON ESS 2 FAIL Caution 3 6DC BUS 1 or DC BUS 2 FAIL Caution 3 6INV BUS 1 or INV BUS 2 FAIL Caution 3 6Bus Equipment List

DC Busses 3 7AC Busses 3 16


May 05/99

EFFECTIVITY : ALL ELECTRIC ABNORMALPage 302



May 05/99

EFFECTIVITY : ALL ELECTRIC ABNORMAL Page 3 1

BATT 1 or BATT 2 FAIL1. BAT button (affected battery) OFF. . . . . . . .

INV 1 or INV 2 FAIL1. INV button (affected inverter) OFF. . . . . . . If all other electrical indications are normal:2. INV button (affected inverter) ON (reset). . . . . . . If reset is unsuccessful:3. INV button (affected inverter) OFF. . . . . . .

L or R AC VOLT FAIL1. AC TIE ON. . . . . . . . . . . . . . . . . . . . . . . . . . 2. ALT button (affected alternator) OFF. . . . . 3. WSHLD heat 1 or 2 OFF. . . . . . . . . . . . . . . . 4. Icing conditions AVOID. . . . . . . . . . . . . . . . . . .

If the caution is extinguished:END

If the caution remains illuminated:Determine lost and/or degraded consumers by BUS EQUIPMENTLIST, located in this Subsection.

END


May 05/99


L or R ALT FAIL1. ALT button (affected alternator) OFF. . . . .

If all other electrical indications are normal:2. ALT button (affected alternator) ON (reset). . . . . If reset is unsuccessful:3. AC TIE ON. . . . . . . . . . . . . . . . . . . . . . . . . . 4. ALT button (affected alternator) OFF. . . . . 5. LR AC VOLT FAIL CAUTION Extinguished. . . . . CAUTION:IN CASE OF A SHORT CIRCUIT, THE REMAINING

ALTERNATOR WILL ALSO FAIL. IN THIS CASE SWITCHOFF THE AC TIE AND RESET THE ALTERNATOR.

L or R DC GEN OVHT1. DC TIE button ON . . . . . . . . . . . . . . . . . . . . 2. GEN button (affected generator) OFF. . . . . NOTE: Observe electrical load limitations in

Section 010000 LIMITATIONS for single generatoroperation till APU generator is selected.

3. Electrical load Check below 400 A. . . . . . . . . . . . . . . . . . . . .


May 05/99


L or R DC GEN FAIL1. GEN button (affected generator) OFF. . . . .

If all other electrical indications are normal:2. GEN button (affected generator) ON (reset). . . . .

If reset is unsuccessful:3. GEN button (affected generator) OFF. . . . . 4. DC TIE button ON. . . . . . . . . . . . . . . . . . . . NOTE: In case of a short circuit, the remaining generator would be

switched off by the protection logic. In this case switch off theDC TIE and reset the generator.

5. APU START Perform refer to . . . . . . . . . . . . . . . . . . . . . .

NOTE: Observe electrical load limitations in Section 010000 LIMITATIONS for single generatoroperation till APU generator is selected.

6. Electrical load Check below 400 A. . . . . . . . . . . . . . . . . . . . .

APU GEN OVHT1. GENAPU button OFF. . . . . . . . . . . . . . . . .

APU GEN FAIL1. GENAPU button OFF. . . . . . .

Documents

328JET QRH.pdf