Pilatus Pc-12 Sample Ops Manual Draft

Operations Manual – Pilatus PC12/45 Nxxxxxx (S/N xxx) 4/11/2023

Table of Contents

Table of Contents.............................................................................................................................................11. Purpose.....................................................................................................................................................32. Pilot-In-Command Qualification.............................................................................................................4

2.1 Initial Instruction..............................................................................................................................42.2 Recurrent Instruction.......................................................................................................................42.3 Emergency training..........................................................................................................................42.4 Logging Requirements.....................................................................................................................52.5 Familiarization with aircraft systems...............................................................................................5

3. Aircraft Requirements..............................................................................................................................63.1 Certification Requirements..............................................................................................................63.2 Minimum Equipment List Compliance...........................................................................................63,3 Weight and Balance Documentation...............................................................................................63.4 Inspection Compliance.....................................................................................................................63.5 Safety and AD Compliance.............................................................................................................63.7 Electronic Navigation Databases.....................................................................................................73.8 Other Requirements – Over Water & International flight...............................................................7

4. Planning Procedures.................................................................................................................................84.1 Pilot Readiness/Fitness....................................................................................................................84.2 Flight Planning.................................................................................................................................84.3 Weather Considerations...................................................................................................................8

4.3.1 Departure..................................................................................................................................84.3.2 En-route....................................................................................................................................94.3.3 Destination...............................................................................................................................9

4.4 Fuel..................................................................................................................................................94.5 Weight and Balance.........................................................................................................................94.6 Field Length/Surface Analysis.......................................................................................................104.7 Pilot-in-command Authority..........................................................................................................10

5. Aircraft Operations................................................................................................................................115.1 Pre-Flight.......................................................................................................................................11

5.1.1 Aircraft Inspection.................................................................................................................115.1.2 Flight Data and Info...............................................................................................................115.1.3 Cockpit Check........................................................................................................................115.1.4 Passenger Briefing.................................................................................................................115.1.5 Cockpit Briefing.....................................................................................................................12

5.2 Start & Taxi...................................................................................................................................125.3 Take Off.........................................................................................................................................135.4 Climb..............................................................................................................................................135.5 Cruise.............................................................................................................................................135.6 Descent...........................................................................................................................................145.7 Terminal Procedures......................................................................................................................155.8 Landing..........................................................................................................................................155.9 Missed Approach Procedures........................................................................................................16

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5.10 Post-Landing..................................................................................................................................165.11 Parking and Shut Down.................................................................................................................165.12 Over Night Storage........................................................................................................................165.13 Post-Flight Analysis.......................................................................................................................16

Appendix 1 – Minimum Equipment List.......................................................................................................17Appendix 2 - Flight Data Card.......................................................................................................................92Appendix 3 - Weight and Balance Calculation form……………………………………………………….93Appendix 4 - Accident/Incident Reporting Section…………………...……………………………………95

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1. Purpose

The purpose of this manual is to express guidelines for normal single pilot operation of the Pilatus PC12, from planning a flight, through shut-down upon completion of the flight. This is not meant to be either a replacement for, or supplement to, the Pilot Operating Handbook. Pilots flying this aircraft are expected to familiarize themselves with the guidelines contained herein and apply them as appropriate to flight operations.

This operations manual is not intended to supersede or replace the FARs or any manufacturer’s operating handbook. Some redundancy may exist, however, in order to stress operational procedures or regulatory limitations.

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2. Pilot-In-Command Qualification

Operation of the aircraft may only be conducted by appropriate qualified and approved pilots. Approval may be granted (pending insurance approval) by the Owner based on the following minimum requirements:

Private Pilot Rating – Airplane Single Engine LandInstrument Flight RatingHigh Altitude Operating EndorsementClass III MedicalExperience Requirements

Current Instrument Proficiency1500 Hours Total Time100 Hours in previous 12 months500 Hours Turbine time50 Hours Make and Model

2.1 Initial Instruction

Pilots must demonstrate successful completion of SimCom’s Initial PC-12 training.

2.2 Recurrent Instruction

Pilots must attend SimCom Recurrent PC-12 or insurance approved equivalent training once in every 12 month period. At least one in three recurrent training sessions should include actual flight time.

Pilots shall complete an approved Safety and Flight Training seminar once in every 12 month period, not less than 4 months, nor more than 8 months, after the SimCom training.

2.3 Emergency training

Part 91 does not contain a detailed requirement for flight crew emergency training. However, FAR Section 135.331 requires each training program to include emergency training for each aircraft type, model and configuration, each crew member and each kind of operation conducted for each crew member. While SimCom training addresses basic emergency procedures for the PC-12, pilots should familiarize themselves with the following topics:

Instruction in emergency assignments and procedures, including coordination among crew members

Individual instruction in the location, function and operation of emergency equipment, including:

o Equipment used in ditching and evacuation o First aid equipment and its proper use o Portable fire extinguishers, with emphasis on the type of extinguisher to be used on

different classes of fires

Instruction in the handling of emergency situations including:

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o Rapid decompression o Fire in flight or on the surface and smoke control procedures with emphasis on electrical

equipment and related circuit breakers o Ditching and evacuation o Illness, injury, or other abnormal situations involving passengers or crew members o Hijacking and other unusual situations

Altitude chamber training is recommended for those pilots operating above 25,000-feet mean sea level (MSL) (Note: Altitude chamber training does not meet the high altitude training, which is required under FAR Section 61.31(f).)

Emergency procedures as described in the aircraft's manual

2.4 Logging Requirements

All flight experience shall be logged in written form as soon as practical upon completion of flight. Logged information shall include date of flight, origin, destination, time as PIC, number and type of landings, number and type of instrument approaches (if any), aircraft type, aircraft category, aircraft registration, and shall be available for inspection with on reasonable notice.

2.5 Familiarization with aircraft systems

The PC-12 S/N xxx has an extensive array of navigation and flight control equipment designed to improve safety, pilot flight awareness and reduce work load. These systems include:

Honeywell KLN90B Approach Certified GPS Honeywell EFIS King KFC-325 3-Axis autopilot King KMD-850 Multi-function display with moving map, radar, StormScope. Enhanced Ground

Proximity Warning System (E-GPWS), DataLink Weather, and Traffic Information System for collision avoidance

Dual Attitude and Heading Reference Systems (AHRS) Dual Transponders Dual Heated Pitot-Static reference systems

Manuals for all these systems are available on-board the aircraft for in-flight reference. Pilots should familiarize themselves with these systems prior to flight.

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3. Aircraft Requirements

3.1 Certification Requirements

Minimum legal certification requirements shall be maintained at all times, based on the local, state and federal requirements dictated by the home operating location of the aircraft. A written record of the current certification status shall be kept and shall be available for inspection on reasonable request. This record will include:

Date and flight hours of last Annual InspectionDate and flight hours of last 100 hour InspectionDate of last Pitot-Static testDate of last Transponder testDate of next ELT battery replacementDate, location, type of check, facility name, observed error for VOR check

3.2 Minimum Equipment List Compliance

The Minimum Equipment List – MEL - as developed by the Manufacturer shall be the overriding MEL for determining if the aircraft is legal for flight operation. In the event that the MEL is not met, the local responsible FSDO shall be contacted to provide necessary permission for ferry flight to maintenance.

3,3 Weight and Balance Documentation

Weight and Balance Documentation specific to the aircraft shall be maintained and copies kept with the aircraft. As changes are made to configuration, Weight and Balance baselines shall be recomputed and shall become the new baseline for pre-flight calculation.

Weight and Balance shall be verified every 5 years by weighing the aircraft in conformance with the Manufacturer’s approved procedure.

3.4 Inspection Compliance

Aircraft shall be maintained according to Pilatus suggested maintenance intervals. For aircraft S/N xxx, maintenance intervals shall be 100 hours, with a 10% excess allowance; however, any excess shall be subtracted from the next 100 hour interval. FAA required annual inspections shall qualify as 100 hour inspections, and restart the inspection cycle.

3.5 Safety and AD Compliance

All Airworthiness Directives will be complied with within the specified period, or the aircraft shall not be flown until compliance is achieved. All Service Bulletins and Service Letters shall be assessed for their safety impact, and all such Bulletins and Letters of a safety of-operation-nature shall be complied with as soon as practical. All such Bulletins and Letters of a Mandatory nature (per manufacturer’s statements) shall be complied with as soon as practical.

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3.7 Electronic Navigation Databases

The owner maintains subscriptions for electronic navigation databases used for the on-board GPS systems and Multi-function Display, as well as for Destination Direct flight planning software used in flight operations. The pilot-in-command should familiarize themselves with the locations and status of each electronic database prior to each flight.

3.8 Other Requirements – Over Water & International flight

All over-water flights of greater than 40 miles require marine survival equipment on board. This minimally will include a life jacket for each passenger and crew member, a raft with a capacity suitable for the full passenger and crew load, a hand held battery powered aviation frequency radio transceiver and batteries, a hand held battery powered GPS receiver and batteries, and a battery powered flashlight and batteries.

International operations shall be accomplished with caution in mind toward the safety and security of the aircraft while unattended on the ground.

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4. Planning Procedures

4.1 Pilot Readiness/Fitness

Before undertaking any flight, the pilot-in-command must assess their readiness for flight taking into account their physiological and mental health to perform flight operations.

Physiological health is impacted by a number of factors including lack of sleep, inadequate exercise, time elapsed since the last meal and consumption of alcohol. Pilots are responsible for assessing these and other factors in evaluating their suitability for flight operations.

Mental health is critical to maintain a high level of alertness and awareness of flight operations. Pilots should not conduct flight operations when under high levels of stress or fatigue.

4.2 Flight Planning

The success of every flight begins with thorough flight planning. Pilots should ensure that adequate time is set aside for flight planning well in advance of planned flight operations. Weather conditions and forecasts should be monitored at least 2 days in advance of planned long-distance flights so that a complete picture of weather conditions can be built in the mind of the pilot. Pilots should use all available weather resources including the Weather Channel and services such as DUATS, DTN Weather Services etc. as well as FAA Weather Briefing facilities via FSS or the Internet.

Flights will be conducted under FAR part 91 for day/night VFR/IFR operations taking into account the recommendations below. Flights to unfamiliar locations or to locations in areas of intensive air traffic (such as the Los Angeles Basin) should be planned and conducted under IFR flight plans. Flights to locations over 200 miles distant from the point of departure should be planned and conducted under IFR flight plans regardless of weather conditions.

Flights will be planned using a current weather briefing and Destination Direct flight planning software, which should be used to print out a detailed navigation log and planned weight & balance manifest prior to each flight.

4.3 Weather Considerations

4.3.1 Departure

Weather at the point of departure should always provide adequate minimums for a return to the airport using an FAA approved Instrument Approach Procedure (IAP) as available. Before takeoff, the pilot-in-command should insure that one of the EFIS navigation pointers is set to the departure point in case an emergency immediately after takeoff requires expedited return for landing.

Departure from airports without an approved FAA IAP should only be made when weather conditions at the point of departure meet VFR minimums (1000’ ceiling and 3 mile visibility).

4.3.2 En-route

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Flight planning should take into account the “big” picture. Prior to flight, the PIC should familiarize with current and forecast en-route weather with consideration of “what-if” planning. What-if planning should consider location of areas of VFR weather, mountainous regions and areas of intense weather activity. Flight planning should be performed with a backup plan in mind should weather or other situations require a change in flight path or destination.

Flights should be planned to avoid areas of reported or forecast severe turbulence, icing or convective activity.

The PIC must be familiar with the operation of weather detection and avoidance equipment including radar, StormScope, and DataLink weather reporting systems. Cruising altitudes should be chosen so that to the maximum extent possible the aircraft should travel above weather systems.

4.3.3 Destination

Weather minimums at the planned destination should be forecast to be at least 300’ above FAA published minimums for the IAP to be used at the destination for the period one hour before arrival to one hour after arrival. When forecast weather is less than 2000’ ceiling, 3 miles visibility within the period one hour before arrival to one hour after arrival, an alternate airport must be planned and filed. Weather at the planned alternate must also be forecast to be 300’ above the minimums required by the FAA for the airport to be designated as an alternate.

For operations at night or reduced (but still VFR) visibility, the PIC should plan and request an appropriate IAP at the destination airport; ILS approaches should be flown whenever possible (even in VFR conditions) as they provide both course and altitude guidance to the runway.

Circle to land approaches should only be used when the weather meets VFR minimums at the destination airport. Night time circle to land operations should be avoided.

Flights to airports served with only an ADF (no GPS overlay) approach should have weather minimums forecast to be at least 500’ higher than FAA published minimums and must be flown using the GPS for navigation.

4.4 Fuel

The PIC should plan to load the aircraft with adequate fuel for the planned flight operation considering FAA required fuel reserves appropriate to VFR or IFR flights, but not less than enough fuel to fly to the destination, fly the planned approach procedure, execute the missed approach procedure, climb to 10,000’ AGL, fly 150 miles to an alternative airport, and fly the approach procedure at that alternative airport. At airports with sufficient runway length (taking into account airport elevation), the PIC should load the maximum amount of fuel consistent with weight and balance limitations.

4.5 Weight and Balance

A weight and balance calculation should be performed before each flight taking into account fuel, number of passengers and baggage to be loaded onto the aircraft.

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4.6 Field Length/Surface Analysis

Prior to flight, the PIC should calculate the required takeoff and landing distances given the forecast weather and estimated weight of the aircraft at departure and arrival. The Pilatus POH should be used to facilitate this calculation. Runway length for either departure or landing should be at least 120% of the calculated distance for dry runway conditions and 130% for wet runway conditions.

Operations to non-paved runways should be avoided whenever practical. Landing distance requirements should be increased to 130% of the calculated landing distance for unimproved runways.

4.7 Pilot-in-command Authority

FAR Section 91.3 states that the pilot-in-command of an aircraft is directly responsible for, and is the final authority on, the operation of the aircraft. The pilot-in-command is vested with the final decision on whether or not to proceed with the flight.

The pilot-in-command must resist being pressured by passengers or their own desire to complete the flight into making a decision to proceed with the flight.

Pilot-in-command responsibilities include:

Ensuring compliance with FARs; Reviewing the correctness of all aspects of flight planning; Exercising command authority in routine and emergency situations.

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5. Aircraft Operations

All flight operations shall be conducted using an appropriate checklist. Copies of these checklists are located in the pilot chart holder.

The PIC should use noise canceling headsets and the aircraft intercom for all phases of flight. These headsets provide ear-protection against engine noise and ensure low noise communication.

5.1 Pre-Flight

5.1.1 Aircraft Inspection

A complete pre-flight inspection should be conducted by the PIC prior to each flight. The aircraft should be inspected to insure the removal of all protective flags and plugs and insure the operational readiness of the aircraft. Any discrepancies should be reviewed against the MEL to determine whether flight operations are appropriate or possible,

5.1.2 Flight Data and Info

Prior to flight, the PIC should verify that the navigation databases for the King KLN90B GPS units and the Honeywell KMD-850 MFD are valid and current.

5.1.3 Cockpit Check

Prior to engine start, the PIC should determine that all required charts and flight information are stowed within easy reach of the pilot and do not obstruct the controls, central pedestal or the glare shield.

5.1.4 Passenger Briefing

Prior to engine start, the PIC should determine that all passenger baggage is stowed and that there is clear access to doorways and the emergency exit.

Passengers need to be briefed on emergency exits, stations, and procedures. FAR Section 91.107 requires the pilot-in-command to ensure that the passengers have been notified to fasten their seat belt and shoulder harness, if installed. Additionally, the pilot-in-command should brief passengers on:

The fact that smoking is prohibited; Use of seat belts; The placement of seats, tray tables, equipment and stores before takeoff and landing; Prohibition on the use of cellular telephones and certain other portable electronic equipment

while in flight; Location and means for opening the passenger entry door and emergency exits; Location of survival equipment;

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Ditching and the use of required flotation equipment, if the flight involves extended over-water operations;

The normal and emergency use of oxygen, if the flight involves operations with cabin altitudes above 12,000-feet MSL;

Location and use of fire extinguishers.

Careful explanations and advance notice of operations that may seem unusual will help increase passenger comfort.

5.1.5 Cockpit Briefing

In the event that a passenger occupies the co-pilot seat, the PIC shall brief the passenger on the need to remain clear of all the controls and the importance of maintaining sterile cockpit procedures whenever the aircraft if below 10,000’ or on the ground.

5.2 Start & Taxi

Prior to start the PIC will complete the “Before Start” checklist items paying particular attention to verification of all annunciation systems and indicator lights.

During engine start, the PIC must pay careful attention to the engine operating limitations to insure that engine ITT limits are observed. Once the engine is running, engine parameters should be monitored to insure normal engine operation.

Departure airport weather information should be obtained from ATIS or ASOS prior to taxi. This information should be recorded on a Flight Data Card for easy reference. ATC should be contacted to obtain appropriate flight clearance and instructions and all necessary navigation equipment programmed and configured prior to beginning to taxi.

A pre-taxi announcement should be made to the passengers with a reminder not to distract the flight crew until further notice. For operations at night, the curtain behind the co-pilot seat should be pulled shut to minimize light glare into the cockpit.

As taxi operations begin, the PIC should verify the correct operation of the aircraft brakes before the aircraft achieves significant forward motion. As taxi continues, the PIC should monitor aircraft flight instruments to verify and confirm correct operation.

The PIC should maintain a sterile cockpit (only required flight crew, no communication unless necessary to the current flight operation) from the time that taxi operations begin until the aircraft is at least 10,000’ above the ground.

5.3 Take Off

Prior to takeoff, the PIC will insure that all navigation equipment is configured and programmed for the flight and that all necessary charts are to hand.

On departure, the PIC shall turn on all lights prior to beginning the takeoff roll. The PIC should commit the takeoff checklist to memory.

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After takeoff, the PIC should allow the aircraft to climb to 500’ before engaging the autopilot. Care should be used to guard the controls against possible autopilot malfunction.

Recognition lights should remain on for all aircraft operations below 10,000’ AGL.

5.4 Climb

Climb power should be set as soon as the aircraft passes through 1000’ AGL. Maximum power should be used for climb consistent with ATC speed restrictions and engine ITT limitations. The PIC should aim for approximately 36.9” TQ, not to exceed 720 degrees Celsius ITT during climb operations.

During climb the PIC should verify that the cabin is being pressurized by the ECS as shown by slowly climbing cabin altitude and increasing pressure differential being shown on the pressurization control panel.

The Pilot and Co-pilot altimeters should be cross checked during climb and both set to 29.92” no later than as the aircraft passes through 18,000’ MSL.

5.5 Cruise

Once the final cruising altitude has been reached, the PIC shall set cruise power not to exceed the parameters as determined by using the Pilatus POH Maximum Cruise Power table to calculate the appropriate torque setting given altitude and outside air temperature. After stabilized cruise for a minimum of 10 minutes, the PIC should capture engine trend data and log it into the aircraft Flight Data Card for that flight.

Engine trend information will be submitted bi-weekly to the Turbine Trend Group (or other facility as designated by Pratt & Whitney, Canada) for engine monitoring.

The PIC should turn off the seat belt light and advise the passengers that they may move about the cabin but that they should have their seat belts fastened when seated in case of unexpected turbulence.

During cruise operations, the PIC shall monitor en-route weather. In areas of cloud or precipitation, radar and the StormScope should be used to monitor for convective activity. Radar data shall be displayed in overlay mode on the pilot EFIS50 being used for primary navigation. Convective activity detected by the StormsScope is displayed on KMD-850 MFD. En-route weather can be further noted and verified against forecast by tracking the route of flight and monitoring ATIS/ASOS broadcast from airports along the route of flight, and by periodic updating of enroute conditions via weather data received via DataLink capabilities displayed on the KMD850 MFD. En-route updates should be made at least once an hour during flight.

At a point 175 miles from the proposed destination and preferqably prior to initial descent, the PIC should familiarize themselves with the IAP to be flown at the destination. A pre-approach briefing should be conducted observing the different phases of the approach and clearly specifying check points and reactions during the approach.

The landing distance should again be calculated given the expected aircraft arrival weight and weather expected at the destination and confirmed as appropriate.

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5.6 Descent

Descent should be planned to commence so that descent rates of no more than 1500 FPM are required during the descent unless requested by ATC. ATIS/ASOS information for the destination should be obtained as soon as practical to facilitate arrival planning.

Recognition lights should be turned on when the aircraft descents through 10,000’ AGL.

Descent planning should contemplate what weather conditions (precipitation, icing etc) are likely to be encountered during the descent. Wherever possible, plan to remain above or descend below regions of icing so as to minimize the amount of time the aircraft is exposed to icing conditions.

On reaching 10,000 AGL, the PIC should turn on the passenger seat belt light and advise passengers that the aircraft is approaching landing and to refrain from distracting the flight crew. Passengers should be asked to ensure that all baggage is stowed and that tray tables, seat backs, seat positions etc should be returned to their normal positions for landing.

5.7 Terminal Procedures

No IAP shall be begun unless the reported weather minimums are at least 200’ above the FAA published minimums. While this is not required by FAR Part 91, it is common sense and good practice. Weather below these limits shall cause the PIC to immediately plan for a missed approach, or to divert the aircraft to the planned or other suitable alternate destination.

When the aircraft is within 15 miles of the final approach fix, the aircraft should be slowed to 170 KIAS unless ATC requires a higher speed for traffic flow management.

Plan the extension of the landing gear while in unaccelerated flight prior to reaching the final approach fix on the IAP. With TQ set at approx. 15”, in level flight with gear extended, the aircraft will slow to approx. 140 KIAS.

Flaps shall be extended to 15 degrees before reaching the FAF, weather conditions permitting. The aircraft will slow to approx 120 KIAS, with little or no pitch change. Passing the FAF, Flaps of 30 degrees should be selected; minor pitch change will occur. Speed will decrease to approx. 100 KIAS.

Approaches should be flown coupled via the autopilot whenever possible. When hand flying, maintain course to within 1 dot maximum on the course direction indicator (CDI). Full scale left or right deflection on the CDI shall cause the PIC to immediately execute a missed approach.

Careful attention must be paid to approach speeds when in icing conditions. Pilots are cautioned to observe aircraft limitations of 15 degrees flaps (maximum) and to maintain a final approach speed of at least 120 KIAS while Pusher Ice mode is enabled on the Stick Pusher system (Inertial separator open and Propeller de-ice enabled).

5.8 Landing

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Final approach to landing should be made paying attention to the Angle of Attach indicator on the EFIS. The PIC should plan on flying the final approach to landing with the AOA centered unless other conditions dictate a higher approach speed. These include:

Landing with zero-flaps due to flap failure as the AOA indicator will not be accurate. Observe a final approach speed of 108 KIAS.

All landings should be planned with 40 degrees of flaps unless weather conditions require otherwise.

5.9 Missed Approach Procedures

A missed approach or go-around procedure should be executed if the approach or approach to landing cannot be continued with the aircraft performing normal maneuvers or if the runway is not visible at the decision height/missed approach point.

Go-around should be commanded on the autopilot and power smoothly advanced to either maximum torque or 720 degrees ITT. The aircraft should be established on a climb with 10 degree pitch up. Retract flaps to 15 degrees and then raise the landing gear. After the landing gear is up and airspeed is greater than 100 KIAS, retract the remaining flaps.

5.10 Post-Landing

After landing and taxiing clear of the runway, the PIC should follow the after landing checklist and clean up the aircraft configuration. Passengers should be cautioned to remain in their seats with their seat belts fastened until after the aircraft has been parked and the engine turned off.

5.11 Parking and Shut Down

After the aircraft has been taxied to its parking position, the PIC should follow the Shutdown checklist and secure the aircraft.

After completion of the shutdown, the PIC should complete the aircraft flight log noting the Hobbs time and record any aircraft or equipment issues on the Flight Data Card.

The PIC should open the passenger door and supervise the passengers as they deplane from the aircraft.

5.12 Over Night Storage

Prior to leaving the aircraft, the PIC should insure that all protective plugs and covers have been installed and that arrangements have been made to insure the physical security of the aircraft. Overnight storage should be arranged in a secure hangar when possible and particularly when weather forecasts include ice or snow prior to the day of departure.

5.13 Post-Flight Analysis

After the completion of the flight, the PIC should review the flight as flown and assess any variances from the pre-flight plan and any errors made during the flight.

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Pilots are encouraged to file NASA ACRS reports whenever a significant error has been made during the flight regardless of whether FAA regulatory deviations have occurred. Review of errors should be made not for self-castigation to as a learning exercise to determine how, when and why the error occurred and what could be done in the future to prevent reoccurrence.

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Appendix 1 – Minimum Equipment List

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 21-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Environmental C ¦ 1 ¦ 0 ¦ May be inoperative provided flight ¦¦ Control System ¦ ¦ ¦ is conducted unpressurized and ¦¦ (ECS) ¦ ¦ ¦ at or below 10,000 feet MSL. ¦¦ ¦ ¦ ¦ ¦¦ 2. Emergency Dump C ¦ 1 ¦ 0 ¦ (O) May be inoperative provided ¦¦ Function ¦ ¦ ¦ flight is conducted unpressurized. ¦¦ ¦ ¦ ¦ ¦¦ 3. Safety Valve C ¦ 1 ¦ 0 ¦ (M) May be inoperative provided: ¦¦ ¦ ¦ ¦ a) The aircraft remains ¦¦ ¦ ¦ ¦ unpressurized, and ¦¦ ¦ ¦ ¦ b) The Safety Valve and/or the ¦¦ ¦ ¦ ¦ Outflow Valve remains open. ¦¦ ¦ ¦ ¦ ¦¦ 4. Outflow Valve C ¦ 1 ¦ 0 ¦ (M) May be inoperative provided: ¦¦ ¦ ¦ ¦ a) The aircraft remains ¦¦ ¦ ¦ ¦ unpressurized, and ¦¦ ¦ ¦ ¦ b) The Safety Valve and/or the ¦¦ ¦ ¦ ¦ Outflow Valve remains open. ¦¦ ¦ ¦ ¦ ¦¦ 5. Outflow Valve C ¦ 1 ¦ 0 ¦ May be inoperative provided flight ¦¦ Controller ¦ ¦ ¦ is conducted unpressurized. ¦¦ ¦ ¦ ¦ ¦¦ 6. Cabin Differential C ¦ 1 ¦ 0 ¦ May be inoperative provided the ¦¦ Pressure Gauge ¦ ¦ ¦ flight is conducted unpressurized. ¦¦ ¦ ¦ ¦ ¦¦ 7. Cabin Altitude C ¦ 1 ¦ 0 ¦ May be inoperative provided the ¦¦ Warning System ¦ ¦ ¦ flight is conducted below 10,000 ¦¦ (CAWS) ¦ ¦ ¦ feet MSL, MEA and MOCA allowing. ¦¦ ¦ ¦ ¦ ¦¦ 8. Temperature C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ Control Sytem ¦ ¦ ¦ Temperature Control Sytem Manual ¦¦ (Auto Mode) ¦ ¦ ¦ Mode is operative. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 9. Temperature C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ Control System ¦ ¦ ¦ Temperature Control System Auto ¦¦ (Manual Mode) ¦ ¦ ¦ Mode is operative. ¦

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¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 21-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 10. Vapor Cycle C ¦ 1 ¦ 0 ¦ ¦¦ *** Cooling System(VCCS) ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 11. Cabin Temperature C ¦ 1 ¦ 0 ¦ ¦¦ Indicator ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 12. Auxiliary Electric C ¦ 1 ¦ 0 ¦ ¦¦ Cabin Heat System ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 13. Cabin Altimeter C ¦ 1 ¦ 0 ¦ May be inoperative provided the ¦¦ ¦ ¦ ¦ flight is conducted unpressurized. ¦¦ ¦ ¦ ¦ ¦¦ 14. Cabin Vertical C ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦¦ Speed Indicator ¦ ¦ ¦ a) Automatic Cabin Pressure | ¦¦ ¦ ¦ ¦ Control System is operative, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ b) Cabin Altimeter is | ¦¦ ¦ ¦ ¦ operative. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Aircraft is operated in an | ¦¦ ¦ ¦ ¦ unpressurized configuration, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ b) Aircraft is operated at or | ¦¦ ¦ ¦ ¦ below 10,000 feet MSL. | ¦¦ ¦ ¦ ¦ ¦¦ 15. CAB PRESS C ¦ 1 ¦ 0 ¦ May be inoperative provided the ¦¦ Annunciator ¦ ¦ ¦ flight is conducted below 10,000 ¦¦ ¦ ¦ ¦ feet MSL, MEA and MOCA allowing. ¦¦ ¦ ¦ ¦ ¦¦ 16. ECS C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided ¦¦ Annunciator ¦ ¦ ¦ flight is conducted unpressurized ¦¦ (CAWS) ¦ ¦ ¦ and at or below 10,000 feet MSL. ¦¦ ¦ ¦ ¦ ¦¦ 17. COOL Annunciator C ¦ 1 ¦ 0 ¦ (M) ¦¦ *** ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 21-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 18. Auxiliary Electric C ¦ 2 ¦ 0 ¦ (M) May be inoperative provided | ¦¦ Heat System ¦ ¦ ¦ underfloor heat system is | ¦¦ ¦ ¦ ¦ operative. | ¦¦ ¦ ¦ ¦ ¦¦ 19. Auxiliary Electric C ¦ 1 ¦ 0 ¦ | ¦¦ *** Battery Heater ¦ ¦ ¦ | ¦¦ System ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 20. Auxiliary Electric C ¦ 1 ¦ 0 ¦ | ¦¦ *** Engine Heater ¦ ¦ ¦ | ¦¦ System ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 21. Electric Foot C ¦ 1 ¦ 0 ¦ | ¦¦ *** Warmer System ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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Page 22


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 22-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Autopilot C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided | ¦¦ ¦ ¦ ¦ operations do not require its use. | ¦¦ ¦ ¦ ¦ ¦¦ 2. Autopilot Disconnect C ¦ 2 ¦ - ¦ May be inoperative provided the | ¦¦ ¦ ¦ ¦ autopilot is not utilized at less | ¦¦ ¦ ¦ ¦ than initial approach altitude. | ¦¦ ¦ ¦ ¦ ¦¦ 3. A/P DISENG C ¦ 1 ¦ - ¦ May be inoperative provided | ¦¦ Annunciator (CAWS) ¦ ¦ ¦ autopilot is not used. | ¦¦ ¦ ¦ ¦ ¦¦ 4. A/P TRIM C ¦ 1 ¦ - ¦ May be inoperative provided | ¦¦ Annunciator (CAWS) ¦ ¦ ¦ autopilot is not used. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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Page 24


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 23-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Communications C ¦ 2 ¦ 0 ¦ Any in excess of those required by | ¦¦ Equipment (VHF, ¦ ¦ ¦ FAR may be inoperative provided it | ¦¦ UHF) ¦ ¦ ¦ is not powered by an Emergency | ¦¦ ¦ ¦ ¦ Power Supply. | ¦¦ ¦ ¦ ¦ ¦¦ 2. Cockpit Speakers C ¦ 2 ¦ - ¦ As required by FAR. ¦¦ ¦ ¦ ¦ ¦¦ 3. Audio Amplifiers ¦ ¦ ¦ ¦¦ 1) Normal System B ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ ¦ ¦ ¦ alternate system is operative. ¦¦ ¦ ¦ ¦ ¦¦ 2) Alternate B ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ System ¦ ¦ ¦ normal system is operative. ¦¦ ¦ ¦ ¦ ¦¦ 4. Voice Activated C ¦ 1 ¦ 0 ¦ ¦¦ Interphone system ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 5. Boom Microphones C ¦ - ¦ - ¦ Any in excess of those required by | ¦¦ ¦ ¦ ¦ FAR may be inoperative. | ¦¦ ¦ ¦ ¦ ¦¦ 6. Control Yoke Press C ¦ 2 ¦ 0 ¦ May be inoperative provided ¦¦ To Talk Switches ¦ ¦ ¦ hand mike on affected side is ¦¦ ¦ ¦ ¦ operative. ¦¦ ¦ ¦ ¦ ¦¦ 7. Static Wicks ¦ - ¦ 0 ¦ May be inoperative provided no ¦¦ (SN 100- 180 without ¦ ¦ ¦ communication equipment is required ¦¦ SB 23-001) ¦ ¦ ¦ for the flight, otherwise: ¦¦ ¦ ¦ ¦ ¦¦ 1) Left Winglet C ¦ 3 ¦ 2 ¦ ¦¦ 2) Right Winglet C ¦ 3 ¦ 2 ¦ ¦¦ 3) Rudder C ¦ 4 ¦ 3 ¦ ¦¦ 4) Stinger C ¦ 1 ¦ 1 ¦ ¦¦ 5) Left Elevator C ¦ 3 ¦ 2 ¦ ¦¦ 6) Right Elevator C ¦ 3 ¦ 2 ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ NOTE: The outermost wick must be ¦¦ ¦ ¦ ¦ installed and undamaged on each ¦¦ ¦ ¦ ¦ control surface. ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 23-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 7. Static Wicks(cont) ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ (SN 181 and up and ¦ ¦ ¦ All may be inoperative or missing ¦¦ SN 100- 180 with ¦ ¦ ¦ provided no communication ¦¦ SB 23-001) ¦ ¦ ¦ equipment is required for the ¦¦ ¦ ¦ ¦ flight, otherwise: ¦¦ ¦ ¦ ¦ ¦¦ 1) Left Winglet C ¦ 2 ¦ 1 ¦ ¦¦ 2) Right Winglet C ¦ 2 ¦ 1 ¦ ¦¦ 3) Rudder C ¦ 3 ¦ 1 ¦ ¦¦ 4) Stinger C ¦ 1 ¦ 1 ¦ ¦¦ 5) Left Elevator C ¦ 2 ¦ 1 ¦ ¦¦ 6) Right Elevator C ¦ 2 ¦ 1 ¦ ¦¦ ¦ ¦ ¦ ¦¦ 8. Passenger Address C ¦ 1 ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ System ¦ ¦ ¦ a) PA not required by FAR, and | ¦¦ ¦ ¦ ¦ b) Alternate, Normal and | ¦¦ ¦ ¦ ¦ Emergency Procedures | ¦¦ ¦ ¦ ¦ and/or operating | ¦¦ ¦ ¦ ¦ restrictions are established | ¦¦ ¦ ¦ ¦ and used. | ¦¦ ¦ ¦ ¦ NOTE: Any station that | ¦¦ ¦ ¦ ¦ operates normally may | ¦¦ ¦ ¦ ¦ be used. | ¦¦ ¦ ¦ ¦ ¦¦ 1) Cargo D ¦ 1 ¦ 0 ¦ May be inoperative unless | ¦¦ Configuration ¦ ¦ ¦ procedures require its use. | ¦¦ ¦ ¦ ¦ ¦¦ 9. Cockpit Voice ¦ ¦ ¦ ¦¦ *** Recorder ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1) With Flight A ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦¦ Recorder (FDR) ¦ ¦ ¦ a) Flight Data Recorder (FDR) | ¦¦ Installed ¦ ¦ ¦ operates normally, and | ¦¦ ¦ ¦ ¦ b) Repairs are made within | ¦¦ ¦ ¦ ¦ three flight days. | ¦¦ ¦ ¦ ¦ ¦¦ 2) Without Flight A ¦ 1 ¦ 0 ¦ May be inoperative provided | ¦

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¦ Data Recorder ¦ ¦ ¦ repairs are made within three | ¦¦ (FDR) Installed ¦ ¦ ¦ flight days. | ¦-------------------------------------------------------------------------------

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 23-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 10. High Frequency D ¦ - ¦ - ¦ Any in excess of those required | ¦¦ *** (HF) Communication ¦ ¦ ¦ by FAR may be inoperative. | ¦¦ System ¦ ¦ ¦ | ¦¦ C ¦ - ¦ - ¦ (O)May be inoperative while | ¦¦ ¦ ¦ ¦ conducting operations that | ¦¦ ¦ ¦ ¦ require two LRCS provided: | ¦¦ ¦ ¦ ¦ a) SATCOM (High or Low Gain) | ¦¦ ¦ ¦ ¦ Data Link Operates normally, | ¦¦ ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ b) SATCOM Data Link | ¦¦ ¦ ¦ ¦ communication operates | ¦¦ ¦ ¦ ¦ normally over the intended | ¦¦ ¦ ¦ ¦ route of flight. | ¦¦ ¦ ¦ ¦ ¦¦ 11. Hand Microphones C ¦ 2 ¦ - ¦ Any in excess of those required | ¦¦ ¦ ¦ ¦ by FAR may be inoperative. | ¦¦ ¦ ¦ ¦ ¦¦ 12. Oxygen Mask C ¦ - ¦ - ¦ Any in excess of those required | ¦¦ Microphones ¦ ¦ ¦ by FAR may be inoperative. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 24-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. INVERTER C ¦ 1 ¦ 0 ¦ (O)May be inoperative for VMC ¦¦ Annunciation ¦ ¦ ¦ provided both inverters are ¦¦ ¦ ¦ ¦ verified to be operative prior to ¦¦ ¦ ¦ ¦ each takeoff. ¦¦ ¦ ¦ ¦ NOTE: Monitor RMI flag or Yaw Rate ¦¦ ¦ ¦ ¦ Sensor for indication of Inverter ¦¦ ¦ ¦ ¦ failure. ¦¦ ¦ ¦ ¦ ¦¦ 2. Emergency Power C ¦ 1 ¦ 0 ¦ May be inoperative except for FAR | ¦¦ *** System (EPS) ¦ ¦ ¦ 135 IFR passenger carrying | ¦¦ ¦ ¦ ¦ operations. | ¦¦ ¦ ¦ ¦ ¦¦ 3. Standby Power ¦ ¦ ¦ Renamed Emergency Power System, | ¦¦ *** Supply ¦ ¦ ¦ Revision 1. | ¦¦ ¦ ¦ ¦ ¦¦ 4. Second Generator C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦¦ ¦ ¦ ¦ a) Flight is conducted VFR, ¦¦ ¦ ¦ ¦ and ¦¦ ¦ ¦ ¦ b) Flight is not conducted in ¦¦ ¦ ¦ ¦ known or forecast icing ¦¦ ¦ ¦ ¦ conditions. ¦¦ ¦ ¦ ¦ ¦¦ 5. Battery C ¦ 2 ¦ 1 ¦ (M) May be inoperative provided | ¦¦ (Two Battery ¦ ¦ ¦ Main Battery (BAT 1) and both | ¦¦ option) ¦ ¦ ¦ generators operate normally. | ¦¦ ¦ ¦ ¦ ¦¦ 6. Inverters B ¦ 2 ¦ 1 ¦ One may be inoperative provided | ¦¦ ¦ ¦ ¦ autopilot is not required. | ¦¦ ¦ ¦ ¦ Note: Autopilot may be used. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 25-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Cockpit Shoulder C ¦ - ¦ - ¦ Right side may be inoperative ¦¦ Harness ¦ ¦ ¦ provided seat is not occupied. ¦¦ ¦ ¦ ¦ ¦¦ 2. Passenger Seat C ¦ - ¦ 0 ¦ (O) All may be inoperative | ¦¦ ¦ ¦ ¦ provided: | ¦¦ ¦ ¦ ¦ a) Seat does not block an | ¦¦ ¦ ¦ ¦ Emergency Exit, | ¦¦ ¦ ¦ ¦ b) Seat does not restrict any | ¦¦ ¦ ¦ ¦ passenger from access to the | ¦¦ ¦ ¦ ¦ main aircraft aisle, and | ¦¦ ¦ ¦ ¦ c) Affected seat(s) are | ¦¦ ¦ ¦ ¦ blocked and placarded | ¦¦ ¦ ¦ ¦ "DO NOT OCCUPY" | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ NOTE 1: A seat with an inoperative ¦¦ ¦ ¦ ¦ seatbelt or shoulder ¦¦ ¦ ¦ ¦ harness is considered ¦¦ ¦ ¦ ¦ inoperative. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ NOTE 2: Affected seat(s) may | ¦¦ ¦ ¦ ¦ include the seat(s) behind | ¦¦ ¦ ¦ ¦ and/or adjacent outboard | ¦¦ ¦ ¦ ¦ seats. | ¦¦ ¦ ¦ ¦ ¦¦ 1) Recline C ¦ - ¦ - ¦ May be inoperative and seat | ¦¦ Mechanism ¦ ¦ ¦ occupied provided seat is secured | ¦¦ ¦ ¦ ¦ in the up-right position. | ¦¦ ¦ ¦ ¦ ¦¦ 2) Underseat C ¦ - ¦ - ¦ (O) May be inoperative provided: | ¦¦ Baggage ¦ ¦ ¦ a) Baggage is not stowed under | ¦¦ Restraining Bars ¦ ¦ ¦ seat with inoperative | ¦¦ ¦ ¦ ¦ Restraining Bar, | ¦¦ ¦ ¦ ¦ b) Associated seat is | ¦¦ ¦ ¦ ¦ placarded "DO NOT STOW | ¦¦ ¦ ¦ ¦ BAGGAGE UNDER THIS SEAT", | ¦¦ ¦ ¦ ¦ and, | ¦¦ ¦ ¦ ¦ c) Procedures are established | ¦¦ ¦ ¦ ¦ to alert crew members of the | ¦¦ ¦ ¦ ¦ inoperative Restraining Bar. | ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 25-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 3. Passenger ¦ - ¦ 0 ¦ Passenger convenience items, as ¦¦ Convenience ¦ ¦ ¦ expressed in the MMEL, are those ¦¦ Item(s) ¦ ¦ ¦ related to passenger convenience, ¦¦ ¦ ¦ ¦ comfort or entertainment such as, ¦¦ ¦ ¦ ¦ but not limited to, galley ¦¦ ¦ ¦ ¦ equipment, movie equipment, ash ¦¦ ¦ ¦ ¦ trays, stereo equipment, overhead ¦¦ ¦ ¦ ¦ reading lamps, etc. Items ¦¦ ¦ ¦ ¦ addressed elsewhere in this ¦¦ ¦ ¦ ¦ document shall not be included. ¦¦ ¦ ¦ ¦ (M) and (O) procedures may be ¦¦ ¦ ¦ ¦ required and included in the air ¦¦ ¦ ¦ ¦ carrier's appropriate document. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ NOTE: EXTERIOR LAVATORY DOOR ASH | ¦¦ ¦ ¦ ¦ TRAYS ARE NOT CONSIDERED | ¦¦ ¦ ¦ ¦ CONVENIENCE ITEMS. | ¦¦ ¦ ¦ ¦ ¦¦ 4. ELT C ¦ 1 ¦ 0 ¦ As required by FAR. ¦¦ ¦ ¦ ¦ ¦¦ C ¦ 1 ¦ 0 ¦ May be inoperative for published ¦¦ ¦ ¦ ¦ scheduled flights in scheduled air ¦¦ ¦ ¦ ¦ carrier service. ¦¦ ¦ ¦ ¦ ¦¦ 5. Flotation D ¦ - ¦ - ¦ Any in excess of those required by ¦¦ Equipment ¦ ¦ ¦ FAR may be inoperative or missing. ¦¦ ¦ ¦ ¦ ¦¦ 6. Emergency Medical D ¦ - ¦ - ¦ Any in excess of those required by | ¦¦ Equipment ¦ ¦ ¦ FAR may be inoperative or missing | ¦¦ ¦ ¦ ¦ provided required distribution is | ¦¦ ¦ ¦ ¦ maintained. | ¦¦ ¦ ¦ ¦ ¦¦ 7. Pilot Seat C ¦ 1 ¦ 0 ¦ May be inoperative provided seat is ¦¦ Vertical Adjustment ¦ ¦ ¦ secured in a position acceptable to ¦¦ ¦ ¦ ¦ the pilot before flight. (No ¦¦ ¦ ¦ ¦ additional cushions acceptable) ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 25-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 8. Pilot Seat Fore C ¦ 1 ¦ 0 ¦ May be inoperative provided seat ¦¦ and Aft Adjustment ¦ ¦ ¦ is secured in a position acceptable ¦¦ ¦ ¦ ¦ to the pilot before flight (no ¦¦ ¦ ¦ ¦ additional cushions acceptable). ¦¦ ¦ ¦ ¦ NOTE: Rudder pedal adjustment must ¦¦ ¦ ¦ ¦ be operative. ¦¦ ¦ ¦ ¦ ¦¦ 9. Cabin Storage C ¦ - ¦ - ¦ (M) May be inoperative provided: | ¦¦ Compartment/Bins/ ¦ ¦ ¦ a) Procedures are established | ¦¦ Closets ¦ ¦ ¦ to secure the compartment | ¦¦ ¦ ¦ ¦ closed, | ¦¦ ¦ ¦ ¦ b) Compartment is not used | ¦¦ ¦ ¦ ¦ for storage of any | ¦¦ ¦ ¦ ¦ Emergency Equipment, and | ¦¦ ¦ ¦ ¦ c) Affected compartment is not | ¦¦ ¦ ¦ ¦ used for storage of any | ¦¦ ¦ ¦ ¦ item(s) except for those | ¦¦ ¦ ¦ ¦ permanently affixed. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ NOTE: If no partitions are | ¦¦ ¦ ¦ ¦ installed, the entire | ¦¦ ¦ ¦ ¦ compartment is considered one | ¦¦ ¦ ¦ ¦ bin. ¦¦ ¦ ¦ ¦ ¦¦ 10. Cargo Restraint C ¦ - ¦ - ¦ (M) May be inoperative, or missing | ¦¦ System ¦ ¦ ¦ such that the effect is that the | ¦¦ ¦ ¦ ¦ item must be considered inop- | ¦¦ ¦ ¦ ¦ ertive, provided acceptable cargo | ¦¦ ¦ ¦ ¦ loading limits from an approved | ¦¦ ¦ ¦ ¦ source, i.e., an Approved Cargo | ¦¦ ¦ ¦ ¦ Loading Manual, or Weight and | ¦¦ ¦ ¦ ¦ Balance Document are observed. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ - ¦ May be inoperative or missing such | ¦¦ ¦ ¦ ¦ that the effect is that the item | ¦¦ ¦ ¦ ¦ must be considered inoperative, | ¦¦ ¦ ¦ ¦ provided the Cargo Compartment | ¦¦ ¦ ¦ ¦ remains empty. | ¦

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¦ ¦ ¦ ¦ ¦¦ (CON'T.) ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 25-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 10. Cargo Restraint C ¦ - ¦ - ¦ May be inoperative or missing such | ¦¦ System ¦ ¦ ¦ that the effect is that the item | ¦¦ (CON'T.) ¦ ¦ ¦ must be considered inoperative, | ¦¦ ¦ ¦ ¦ provided pallet with inoperative | ¦¦ ¦ ¦ ¦ lock(s) is removed. | ¦¦ ¦ ¦ ¦ ¦¦ 11. Cockpit Sun Visors C ¦ - ¦ - ¦ May be inoperative or missing | ¦¦ ¦ ¦ ¦ provided there is no field of | ¦¦ ¦ ¦ ¦ vision restriction for the flight | ¦¦ ¦ ¦ ¦ crew. ¦¦ ¦ ¦ ¦ ¦¦ 12. Exterior Lavatory A ¦ 1 ¦ - ¦ One may be missing provided it is | ¦¦ Door Ashtray ¦ ¦ ¦ replaced within 3 calendar days. | ¦¦ ¦ ¦ ¦ ¦¦ 13. "Fasten Seat Belt C ¦ - ¦ - ¦ One or more signs or placards may | ¦¦ While Seated" Sign ¦ ¦ ¦ be illegible or missing provided | ¦¦ or Placard ¦ ¦ ¦ a legible sign or placard is | ¦¦ ¦ ¦ ¦ visible from each occupied | ¦¦ ¦ ¦ ¦ passenger seat. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 26-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 26 FIRE PROTECTION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Portable Fire C ¦ - ¦ 0 ¦ Any in excess of those required by ¦¦ Extinguisher(s) ¦ ¦ ¦ FAR may be inoperative or missing ¦¦ ¦ ¦ ¦ provided: ¦¦ ¦ ¦ ¦ a) The inoperative fire ¦¦ ¦ ¦ ¦ extinguisher is tagged ¦¦ ¦ ¦ ¦ inoperative, removed from ¦¦ ¦ ¦ ¦ the installed location and ¦¦ ¦ ¦ ¦ placed out of sight so it ¦¦ ¦ ¦ ¦ can not be mistaken for a ¦¦ ¦ ¦ ¦ functional unit, and ¦¦ ¦ ¦ ¦ b) The required distribution is ¦¦ ¦ ¦ ¦ maintained. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 27-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 27 FLIGHT CONTROLS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Flap Position C ¦ 1 ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ Indicator ¦ ¦ ¦ a) Prior to each flight, flaps ¦¦ ¦ ¦ ¦ are verified to operate ¦¦ ¦ ¦ ¦ normally, ¦¦ ¦ ¦ ¦ b) Prior to each takeoff, flaps ¦¦ ¦ ¦ ¦ are visually checked for ¦¦ ¦ ¦ ¦ proper position, and ¦¦ ¦ ¦ ¦ c) Stall Warning/Stick Shaker ¦¦ ¦ ¦ ¦ system is verified to ¦¦ ¦ ¦ ¦ function properly. ¦¦ ¦ ¦ ¦ ¦¦ 2. Electric Trim B ¦ 1 ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ Annunciator "STAB ¦ ¦ ¦ a) Triple Trim Indicator is ¦¦ TRIM"(CAWS) ¦ ¦ ¦ operative, and ¦¦ ¦ ¦ ¦ b) Stab pointer is visually ¦¦ ¦ ¦ ¦ checked before each takeoff ¦¦ ¦ ¦ ¦ to be in the proper ¦¦ ¦ ¦ ¦ position. ¦¦ ¦ ¦ ¦ ¦¦ 3. Aileron Trim C ¦ 1 ¦ - ¦ May be inoperative provided | ¦¦ ¦ ¦ ¦ aileron trim tab is set to neutral. | ¦¦ ¦ ¦ ¦ ¦¦ 4. Triple Trim C ¦ 1 ¦ - ¦ (O) May be inoperative provided: | ¦¦ Indicator ¦ ¦ ¦ a) Prior to each flight all | ¦¦ ¦ ¦ ¦ flight control trim tabs are | ¦¦ ¦ ¦ ¦ verified to operate | ¦¦ ¦ ¦ ¦ normally, and | ¦¦ ¦ ¦ ¦ b) Prior to each takeoff, trim | ¦¦ ¦ ¦ ¦ tabs are visually checked | ¦¦ ¦ ¦ ¦ for proper position. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 28-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 28 FUEL ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Fuel Quantity B ¦ 2 ¦ 1 ¦ (O)One indicator(L or R) may be ¦¦ Indicator(L/R) ¦ ¦ ¦ inoperative provided: ¦¦ ¦ ¦ ¦ a) The triple trim indicator is ¦¦ ¦ ¦ ¦ operative, ¦¦ ¦ ¦ ¦ b) The aileron trim is ¦¦ ¦ ¦ ¦ operative, and ¦¦ ¦ ¦ ¦ c) If autopilot is used it must ¦¦ ¦ ¦ ¦ be disconnected every 20 ¦¦ ¦ ¦ ¦ minutes to detect any ¦¦ ¦ ¦ ¦ possible fuel imbalance. ¦¦ ¦ ¦ ¦ ¦¦ 2. Low Fuel C ¦ 2 ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ Annunciator ¦ ¦ ¦ a) All fuel quantity indicating | ¦¦ R FUEL LOW/ ¦ ¦ ¦ systems operate normally, | ¦¦ L FUEL LOW (CAWS) ¦ ¦ ¦ and | ¦¦ ¦ ¦ ¦ b) Fuel Flow and Fuel Used | ¦¦ ¦ ¦ ¦ systems operate normally. | ¦¦ ¦ ¦ ¦ ¦¦ 3. Fuel Flow/ Fuel C ¦ 1 ¦ - ¦ (O) May be inoperative provided: | ¦¦ Used System ¦ ¦ ¦ a) All fuel quantity systems | ¦¦ ¦ ¦ ¦ operate normally, and | ¦¦ ¦ ¦ ¦ b) Low Fuel Annunciator (CAWS) | ¦¦ ¦ ¦ ¦ operates normally. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 30-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 30 ICE AND RAIN ¦ ¦ ¦ ¦¦ PROTECTION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Propeller Deice C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦¦ System ¦ ¦ ¦ a) Flight is not conducted in ¦¦ ¦ ¦ ¦ known or forecast icing ¦¦ ¦ ¦ ¦ conditions, and ¦¦ ¦ ¦ ¦ b) Stall Warning/Stick Pusher ¦¦ ¦ ¦ ¦ system is verified to ¦¦ ¦ ¦ ¦ function properly in the ¦¦ ¦ ¦ ¦ Normal mode. ¦¦ ¦ ¦ ¦ ¦¦ 2. Surface Deice C ¦ 1 ¦ 0 ¦ May be inoperative provided flight ¦¦ System ¦ ¦ ¦ is not operated in known or ¦¦ ¦ ¦ ¦ forecast icing conditions. ¦¦ ¦ ¦ ¦ ¦¦ 3. Inertial Separator C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided ¦¦ ¦ ¦ ¦ separator is verified open and ¦¦ ¦ ¦ ¦ switch is verified in ON position. ¦¦ ¦ ¦ ¦ ¦¦ 4. Probes Heat C ¦ 2 ¦ 0 ¦ May be inoperative provided: ¦¦ ¦ ¦ ¦ a) Flight is not conducted in ¦¦ ¦ ¦ ¦ known or forecast icing ¦¦ ¦ ¦ ¦ conditions, and ¦¦ ¦ ¦ ¦ b) Flight is conducted VMC. ¦¦ ¦ ¦ ¦ ¦¦ 5. Pitot and Static C ¦ 2 ¦ - ¦ May be inoperative provided: | ¦¦ Heat ¦ ¦ ¦ a) Not required by FAR, and | ¦¦ ¦ ¦ ¦ b) Flight is not conducted into | ¦¦ ¦ ¦ ¦ known or forecast icing | ¦¦ ¦ ¦ ¦ conditions. | ¦¦ ¦ ¦ ¦ ¦¦ 6. Windshield B ¦ - ¦ - ¦ (M)May be inoperative for IFR | ¦¦ Heating ¦ ¦ ¦ flight, except for flight in known | ¦¦ ¦ ¦ ¦ or forecast icing conditions, | ¦¦ ¦ ¦ ¦ provided one heating zone of the | ¦¦ ¦ ¦ ¦ left hand windshield is verified | ¦¦ ¦ ¦ ¦ to be operative. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 31-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 31 INDICATING/RECORDING ¦ ¦ ¦ ¦¦ SYSTEMS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Clock with sweep C ¦ 1 ¦ 0 ¦ May be inoperative for VFR. ¦¦ second hand, or ¦ ¦ ¦ ¦¦ electric digital ¦ ¦ ¦ ¦¦ clock. ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 2. Hourmeter C ¦ 1 ¦ 0 ¦ (O) ¦¦ *** ¦ ¦ ¦ ¦¦ 3. Flight Data C ¦ - ¦ - ¦ Any in excess of those required by | ¦¦ *** Recorder (FDR) ¦ ¦ ¦ FAR may be inoperative. | ¦¦ System. ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 32-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 32 LANDING GEAR ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Parking Brake C ¦ 1 ¦ 0 ¦ (O) ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 33-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 33 LIGHTS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Cockpit and C ¦ - ¦ - ¦ Individual lights may be ¦¦ Instrument Light ¦ ¦ ¦ inoperative provided remaining ¦¦ System ¦ ¦ ¦ lights are: ¦¦ ¦ ¦ ¦ a) Sufficient to clearly ¦¦ ¦ ¦ ¦ illuminate all required ¦¦ ¦ ¦ ¦ instruments, controls, ¦¦ ¦ ¦ ¦ and other devices for which ¦¦ ¦ ¦ ¦ it is provided, ¦¦ ¦ ¦ ¦ b) Positioned so that direct ¦¦ ¦ ¦ ¦ rays are shielded from ¦¦ ¦ ¦ ¦ flight crewmembers eyes, and ¦¦ ¦ ¦ ¦ c) Lighting configuration and ¦¦ ¦ ¦ ¦ intensity is acceptable to ¦¦ ¦ ¦ ¦ the flight crew. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 2. Cabin Lights C ¦ - ¦ - ¦ May be inoperative provided ¦¦ ¦ ¦ ¦ lighting configuration at dispatch ¦¦ ¦ ¦ ¦ is acceptable to the flight crew. ¦¦ ¦ ¦ ¦ ¦¦ 3. Anti-Collisison C ¦ 1 ¦ 0 ¦ ¦¦ *** Beacon Light System ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 4. Strobe Light C ¦ 1 ¦ 0 ¦ May be inoperative for day ¦¦ System ¦ ¦ ¦ operations. ¦¦ ¦ ¦ ¦ NOTE: This is certified as the ¦¦ ¦ ¦ ¦ anti-collision light system. ¦¦ ¦ ¦ ¦ ¦¦ 5. Landing Lights C ¦ 2 ¦ 0 ¦ May be inoperative for day ¦¦ ¦ ¦ ¦ operations. ¦¦ ¦ ¦ ¦ ¦¦ C ¦ 2 ¦ 1 ¦ One may be inoperative for night ¦¦ ¦ ¦ ¦ operations. ¦¦ ¦ ¦ ¦ ¦¦ C ¦ 2 ¦ - ¦ May be inoperative if Recognition | ¦¦ ¦ ¦ ¦ Lights are installed and | ¦¦ ¦ ¦ ¦ operative. | ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 33-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 33 LIGHTS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 6. Position Lights C ¦ 3 ¦ 0 ¦ May be inoperative for day ¦¦ ¦ ¦ ¦ operations. ¦¦ ¦ ¦ ¦ ¦¦ 7. Taxi Light C ¦ 1 ¦ 0 ¦ May be inoperative for day ¦¦ ¦ ¦ ¦ operations. ¦¦ ¦ ¦ ¦ ¦¦ C ¦ 1 ¦ 0 ¦ May be inoperative for night ¦¦ ¦ ¦ ¦ operations provided at least one ¦¦ ¦ ¦ ¦ landing light is operative. ¦¦ ¦ ¦ ¦ ¦¦ 8. Wing Illumination C ¦ 1 ¦ 0 ¦ (O) May be inoperative provided a | ¦¦ Light ¦ ¦ ¦ portable lamp/light of adequate | ¦¦ ¦ ¦ ¦ capacity for wing and/or control | ¦¦ ¦ ¦ ¦ surface inspection is available | ¦¦ ¦ ¦ ¦ for night operations in icing | ¦¦ ¦ ¦ ¦ conditions. | ¦¦ ¦ ¦ ¦ ¦¦ 9. Fasten Seat Belt C ¦ 1 ¦ 0 ¦ (O) May be inoperative provided | ¦¦ *** and No Smoking ¦ ¦ ¦ alternate procedures are | ¦¦ Signs ¦ ¦ ¦ established and used for briefing | ¦¦ ¦ ¦ ¦ passengers. | ¦¦ ¦ ¦ ¦ ¦¦ 10. Cockpit Dome C ¦ 2 ¦ - ¦ One may be inoperative for night | ¦¦ Lighting ¦ ¦ ¦ operations and both may be | ¦¦ ¦ ¦ ¦ inoperative for day operations. | ¦¦ ¦ ¦ ¦ ¦¦ 11. Recognition C ¦ - ¦ 0 ¦ | ¦¦ *** Light ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 12. Logo Lights C ¦ - ¦ 0 ¦ | ¦¦ *** ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Altimeters, B ¦ - ¦ 1 ¦ May be inoperative on right side ¦¦ adjustable for ¦ ¦ ¦ for operations not requiring a ¦¦ barometric pressure ¦ ¦ ¦ second in command. ¦¦ ¦ ¦ ¦ ¦¦ 2. Airspeed Indicators B ¦ - ¦ 1 ¦ May be inoperative on right side ¦¦ ¦ ¦ ¦ for operations not requiring a ¦¦ ¦ ¦ ¦ second in command. ¦¦ ¦ ¦ ¦ ¦¦ 3. Attitude Heading C ¦ - ¦ 1 ¦ ¦¦ Reference System ¦ ¦ ¦ ¦¦ (AHRS) ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1) Standard PC-12 C ¦ - ¦ 1 ¦ One may be inoperative provided ¦¦ (MTOW 4100 kg) ¦ ¦ ¦ a second AHRS is installed and ¦¦ ¦ ¦ ¦ operative. ¦¦ 2) PC-12/45 C ¦ - ¦ 1 ¦ Both AHRS or one AHRS and a Yaw ¦¦ (MTOW 4500 kg) ¦ ¦ ¦ Rate Sensor must be operative for ¦¦ ¦ ¦ ¦ IFR operatons and flight in icing ¦¦ ¦ ¦ ¦ conditions. ¦¦ ¦ ¦ ¦ ¦¦ 4. Standby Attitude C ¦ 1 ¦ 0 ¦ May be inoperative for day or night ¦¦ Indicator ¦ ¦ ¦ VFR, or ¦¦ C ¦ 1 ¦ 0 ¦ May be inoperative for all ¦¦ ¦ ¦ ¦ operations provided a second AHRS ¦¦ ¦ ¦ ¦ is installed and both are ¦¦ ¦ ¦ ¦ operative. ¦¦ ¦ ¦ ¦ ¦¦ 5. Vertical Speed B ¦ 2 ¦ 0 ¦ Must be operative on left side for ¦¦ Indicators ¦ ¦ ¦ IFR passenger carrying operations. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 6. ATC Transponders C ¦ - ¦ - ¦ May be inoperative provided: | ¦¦ and Automatic ¦ ¦ ¦ a) Enroute Operations do not | ¦¦ Altitude Reporting ¦ ¦ ¦ require its use, and | ¦¦ System(s) ¦ ¦ ¦ b) Prior to flight, approval | ¦¦ ¦ ¦ ¦ is obtained from ATC | ¦¦ ¦ ¦ ¦ facilities having | ¦¦ ¦ ¦ ¦ jurisdiction over the | ¦¦ ¦ ¦ ¦ planned route of flight. | ¦¦ ¦ ¦ ¦ ¦¦ D ¦ - ¦ 1 ¦ Any in excess of those required by | ¦¦ ¦ ¦ ¦ FAR may be inoperative. | ¦¦ ¦ ¦ ¦ ¦¦ 7. Navigation C ¦ - ¦ - ¦ As required by FAR. ¦¦ Equipment (VOR/ILS, ¦ ¦ ¦ ¦¦ Loran, Omega/VLF, ¦ ¦ ¦ ¦¦ INS, Doppler, GPS, ¦ ¦ ¦ ¦¦ MLS) ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 8. Weather Radar/ C ¦ 1 ¦ 0 ¦ As required by FAR. ¦¦ *** Thunderstorm ¦ ¦ ¦ ¦¦ Detection Equipment ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 9. Marker Beacon C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ ¦ ¦ ¦ approach procedure does not ¦¦ ¦ ¦ ¦ require its use. ¦¦ ¦ ¦ ¦ ¦¦ 10. Radar Altimeter C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ (PC-12/45) ¦ ¦ ¦ autopilot is disengaged at 1000 ¦¦ ¦ ¦ ¦ feet AGL. ¦¦ ¦ ¦ ¦ ¦¦ *** (PC-12) D ¦ 1 ¦ 0 ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 11. Distance Measuring D ¦ 1 ¦ 0 ¦ Any in excess of those required by | ¦¦ Equipment (DME) ¦ ¦ ¦ FAR may be inoperative. | ¦¦ Systems ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 12. ADF C ¦ 1 ¦ 0 ¦ As required by FAR. ¦

Page 59


¦ ¦ ¦ ¦ ¦¦ 13. RMI C ¦ 1 ¦ 0 ¦ ¦-------------------------------------------------------------------------------

Page 60


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-3 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 14. Altitude Alerter/ C ¦ 1 ¦ 0 ¦ ¦¦ Pre-select ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 15. Altitude Alerting A ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ System ¦ ¦ ¦ a) Autopilot with Altitude | ¦¦ ¦ ¦ ¦ Hold is operative, | ¦¦ ¦ ¦ ¦ b) Enroute operations do not | ¦¦ ¦ ¦ ¦ require its use, and | ¦¦ ¦ ¦ ¦ c) Repairs are made within | ¦¦ ¦ ¦ ¦ three flight days. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ May be inoperative provided it is | ¦¦ ¦ ¦ ¦ not required by FAR. | ¦¦ ¦ ¦ ¦ ¦¦ 16. Multifunction C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ *** Display(MFD) ¦ ¦ ¦ weather radar is not required by ¦¦ ¦ ¦ ¦ FAR. ¦¦ ¦ ¦ ¦ ¦¦ 17. EADI/EHSI Display C ¦ 2 ¦ 0 ¦ May be inoperative for operations ¦¦ Unit(Copilot side) ¦ ¦ ¦ not requiring a second in ¦¦ ¦ ¦ ¦ command. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 62


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-4 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 18. Nonstabilized B ¦ 1 ¦ 0 ¦ May be inoperative provided any ¦¦ Magnetic ¦ ¦ ¦ combination of three gyro or INS ¦¦ Compass ¦ ¦ ¦ (IRU) stabilized compass systems ¦¦ ¦ ¦ ¦ are operative. ¦¦ ¦ ¦ ¦ ¦¦ B ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦¦ ¦ ¦ ¦ a) Any combination of two gyro ¦¦ ¦ ¦ ¦ or INS stabilized compass ¦¦ ¦ ¦ ¦ systems are operative, and ¦¦ ¦ ¦ ¦ b) Aircraft is operated with ¦¦ ¦ ¦ ¦ dual independent naviga- ¦¦ ¦ ¦ ¦ tion capability and under ¦¦ ¦ ¦ ¦ positive radar control by ¦¦ ¦ ¦ ¦ ATC on the enroute portion ¦¦ ¦ ¦ ¦ of the flight. ¦¦ ¦ ¦ ¦ ¦¦ B ¦ 1 ¦ 0 ¦ May be inoperative for flights ¦¦ ¦ ¦ ¦ that are entirely within areas of ¦¦ ¦ ¦ ¦ magnetic unreliability provided at ¦¦ ¦ ¦ ¦ least two stabilized directional ¦¦ ¦ ¦ ¦ gyro systems are installed, ¦¦ ¦ ¦ ¦ operative, and used in conjunction ¦¦ ¦ ¦ ¦ with approved free gyro navigation ¦¦ ¦ ¦ ¦ techniques. ¦¦ ¦ ¦ ¦ ¦¦ 19. Windshear Warning C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ *** and Flight ¦ ¦ ¦ a) Alternate procedures are | ¦¦ Guidance System ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Windshear Detection and | ¦¦ ¦ ¦ ¦ Avoidance System Operates | ¦¦ ¦ ¦ ¦ normally. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Takeoffs and landings are | ¦¦ ¦ ¦ ¦ not conducted in known or | ¦¦ ¦ ¦ ¦ forecast windshear | ¦

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¦ ¦ ¦ ¦ conditions. | ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 64


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-5 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 20. Windshear C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ *** Detection and ¦ ¦ ¦ a) Alternate procedures are | ¦¦ Avoidance System ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Windshear Warning and | ¦¦ ¦ ¦ ¦ Guidance System Operates | ¦¦ ¦ ¦ ¦ normally. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Takeoffs and landings are | ¦¦ ¦ ¦ ¦ not conducted in known or | ¦¦ ¦ ¦ ¦ forecast windshear | ¦¦ ¦ ¦ ¦ conditions. | ¦¦ ¦ ¦ ¦ ¦¦ 21. Traffic Alert and B ¦ 1 ¦ 0 ¦ (M)(O) May be inoperative provided: | ¦¦ *** Collision Avoidance ¦ ¦ ¦ a) System is deactivated and | ¦¦ System (TCAS I) ¦ ¦ ¦ secured, and | ¦¦ ¦ ¦ ¦ b) Enroute or approach | ¦¦ ¦ ¦ ¦ procedures do not require | ¦¦ ¦ ¦ ¦ its use. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ (M)(O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Not required by FAR, | ¦¦ ¦ ¦ ¦ b) System is deactivated and | ¦¦ ¦ ¦ ¦ secured, and | ¦¦ ¦ ¦ ¦ c) Enroute or approach | ¦¦ ¦ ¦ ¦ procedures do not require | ¦¦ ¦ ¦ ¦ its use. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

Page 65


¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 66


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-6 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 22. Traffic Alert and B ¦ 1 ¦ 0 ¦ (M)(O) May be inoperative provided: | ¦¦ *** Collision Avoidance ¦ ¦ ¦ a) System is deactivated and | ¦¦ System (TCAS II) ¦ ¦ ¦ secured, and | ¦¦ ¦ ¦ ¦ b) Enroute or approach | ¦¦ ¦ ¦ ¦ procedures do not require | ¦¦ ¦ ¦ ¦ its use. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ (M)(O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Not required by FAR, | ¦¦ ¦ ¦ ¦ b) System is deactivated and | ¦¦ ¦ ¦ ¦ secured, and | ¦¦ ¦ ¦ ¦ c) Enroute or approach | ¦¦ ¦ ¦ ¦ procedures do not require | ¦¦ ¦ ¦ ¦ its use. | ¦¦ ¦ ¦ ¦ ¦¦ 1) Combined Traffic C ¦ 2 ¦ 1 ¦ May be inoperative on the non- | ¦¦ Alert (TA) and ¦ ¦ ¦ flying pilot side provided: | ¦¦ Resolution ¦ ¦ ¦ a) TA and RA visual display is | ¦¦ Advisory (RA) ¦ ¦ ¦ operative on the flying | ¦¦ Dual Display ¦ ¦ ¦ pilot side, and | ¦¦ System(s) ¦ ¦ ¦ b) TA and RA audio function is | ¦¦ ¦ ¦ ¦ operative on the flying | ¦¦ ¦ ¦ ¦ pilot side. | ¦¦ ¦ ¦ ¦ ¦¦ 2) Resolution C ¦ 2 ¦ 1 ¦ May be inoperative on the non- | ¦¦ Advisory (RA) ¦ ¦ ¦ flyingf pilot side. | ¦¦ Display Systems ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Traffic Alert (TA) visual | ¦¦ ¦ ¦ ¦ display and audio functions | ¦¦ ¦ ¦ ¦ are operative, | ¦¦ ¦ ¦ ¦ b) TA only mode is selcted by | ¦¦ ¦ ¦ ¦ the crew, and | ¦¦ ¦ ¦ ¦ c) Enroute or approach | ¦¦ ¦ ¦ ¦ procedures do not require | ¦¦ ¦ ¦ ¦ its use. | ¦¦ ¦ ¦ ¦ ¦

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¦ ¦ ¦ ¦ ¦¦ (CON'T.) ¦ ¦ ¦ | ¦-------------------------------------------------------------------------------

Page 68


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-7 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 22. Traffic Alert and ¦ ¦ ¦ | ¦¦ *** Collision Avoidance ¦ ¦ ¦ | ¦¦ System (TCAS II) ¦ ¦ ¦ | ¦¦ (CON'T.) ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 3) Traffic Alert C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ Display System(s) ¦ ¦ ¦ a) RA Visual display and audio | ¦¦ ¦ ¦ ¦ functions are operative, and | ¦¦ ¦ ¦ ¦ b) Enroute or approach | ¦¦ ¦ ¦ ¦ procedures do not require | ¦¦ ¦ ¦ ¦ its use. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

Page 69


¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 70


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-8 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 23. Navagation ¦ ¦ ¦ | ¦¦ Databases ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 1) Flight C ¦ - ¦ - ¦ (O) May be out of currency | ¦¦ Management ¦ ¦ ¦ provided: | ¦¦ System ¦ ¦ ¦ a) Current Aeronautical Charts | ¦¦ ¦ ¦ ¦ are used to verify Navigation | ¦¦ ¦ ¦ ¦ Fixes prior to dispatch, | ¦¦ ¦ ¦ ¦ b) Procedures are established | ¦¦ ¦ ¦ ¦ and used to verify status and | ¦¦ ¦ ¦ ¦ suitibility of Navigation | ¦¦ ¦ ¦ ¦ Facilities used to define | ¦¦ ¦ ¦ ¦ route of flight, and | ¦¦ ¦ ¦ ¦ c) Approach Navigation Radios | ¦¦ ¦ ¦ ¦ are manually tuned and | ¦¦ ¦ ¦ ¦ identified. | ¦¦ ¦ ¦ ¦ ¦¦ 2) Navigation C ¦ - ¦ - ¦ (O) May be out of currency | ¦¦ Management ¦ ¦ ¦ provided: | ¦¦ System ¦ ¦ ¦ a) Current Aeronautical Charts | ¦¦ ¦ ¦ ¦ are used to verify Navigation | ¦¦ ¦ ¦ ¦ Fixes prior to dispatch, | ¦¦ ¦ ¦ ¦ b) Procedures are established | ¦¦ ¦ ¦ ¦ and used to verify status and | ¦¦ ¦ ¦ ¦ suitibility of Navigation | ¦¦ ¦ ¦ ¦ Facilities used to define | ¦¦ ¦ ¦ ¦ route of flight, and | ¦¦ ¦ ¦ ¦ c) Approach Navigation Radios | ¦¦ ¦ ¦ ¦ are manually tuned and | ¦¦ ¦ ¦ ¦ identified. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

Page 71


¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 72


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-9 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 24. Terrain Awareness A ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ and Warning ¦ ¦ ¦ a) Alternate procedures are | ¦¦ System (GPWS) ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Repairs are made within two | ¦¦ ¦ ¦ ¦ flight days. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) It is not required by | ¦¦ ¦ ¦ ¦ FAR, and | ¦¦ ¦ ¦ ¦ b) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦¦ ¦ ¦ ¦ ¦¦ 1) Modes 1-4 A ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Repairs are made within two | ¦¦ ¦ ¦ ¦ flight days. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) It is not required by | ¦¦ ¦ ¦ ¦ FAR, and | ¦¦ ¦ ¦ ¦ b) Alternate procedures are | ¦¦ ¦ ¦ ¦ and used. | ¦¦ ¦ ¦ ¦ ¦¦ 2) Test Mode A ¦ 1 ¦ 0 ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) GPWS is considered | ¦¦ ¦ ¦ ¦ inoperative, and | ¦¦ ¦ ¦ ¦ b) Repairs are made within | ¦¦ ¦ ¦ ¦ two flight days. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) It is not by FAR, and | ¦¦ ¦ ¦ ¦ b) GPWS is considered | ¦¦ ¦ ¦ ¦ inoperative. | ¦¦ ¦ ¦ ¦ ¦¦ 3) Glideslope B ¦ 2 ¦ 0 ¦ | ¦¦ Deviation ¦ ¦ ¦ | ¦¦ (Mode 5) ¦ ¦ ¦ | ¦

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¦ ¦ ¦ ¦ ¦¦ (CON'T.) ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 74


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-10 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 24. Terrain Awareness ¦ ¦ ¦ | ¦¦ and Warning ¦ ¦ ¦ | ¦¦ System (GPWS) ¦ ¦ ¦ | ¦¦ (CON'T.) ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 4) Advisory C ¦ - ¦ 0 ¦ (O) May be inoperative provided | ¦¦ *** Callouts ¦ ¦ ¦ alternate procedures are | ¦¦ ¦ ¦ ¦ established and used. | ¦¦ ¦ ¦ ¦ ¦¦ *** 5) Windshear Mode C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Windshear Detection and | ¦¦ ¦ ¦ ¦ Avoidance System operates | ¦¦ ¦ ¦ ¦ normally. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ 0 ¦ (O) May be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Alternate procedures are | ¦¦ ¦ ¦ ¦ established and used, and | ¦¦ ¦ ¦ ¦ b) Takeoffs and Landings are | ¦¦ ¦ ¦ ¦ not conducted in known or | ¦¦ ¦ ¦ ¦ forecast windshear | ¦¦ ¦ ¦ ¦ conditions. | ¦¦ ¦ ¦ ¦ ¦¦ 6) TAWS C ¦ - ¦ 0 ¦ | ¦¦ *** ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

Page 75


¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 76


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 34-11 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 34 NAVIGATION ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 25. Automatic Dependent D ¦ - ¦ 0 ¦ May be inoperative provided it is | ¦¦ *** Surveillance - ¦ ¦ ¦ not required by FAR. | ¦¦ Broadcast System ¦ ¦ ¦ | ¦¦ (ADS-B) ¦ ¦ ¦ NOTE: If ADS-B is installed in lieu | ¦¦ ¦ ¦ ¦ of, or as a replacement for, 14 CFR | ¦¦ ¦ ¦ ¦ required equipment the repair | ¦¦ ¦ ¦ ¦ catagory in the operator's MEL will | ¦¦ ¦ ¦ ¦ be the same as that of the 14 CFR | ¦¦ ¦ ¦ ¦ required equipment. | ¦¦ ¦ ¦ ¦ ¦¦ 1) Link and Display D ¦ - ¦ 0 ¦ | ¦¦ Processor Unit ¦ ¦ ¦ NOTE: Cockpit Display Traffic | ¦¦ (LDPU) ¦ ¦ ¦ Information (CDTI) display of data | ¦¦ ¦ ¦ ¦ from other aircraft systems may be | ¦¦ ¦ ¦ ¦ used. | ¦¦ ¦ ¦ ¦ ¦¦ 2) Cockpit Display D ¦ - ¦ 0 ¦ | ¦¦ and Traffic ¦ ¦ ¦ NOTE: ADS-B data transmissions | ¦¦ Information ¦ ¦ ¦ may continue. | ¦¦ (CDTI) ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 3) CDTI Control D ¦ - ¦ 0 ¦ May be inoperative provided: | ¦¦ Panel ¦ ¦ ¦ a) Flight ID can be set, and | ¦¦ ¦ ¦ ¦ b) Screen display is | ¦¦ ¦ ¦ ¦ acceptable to the Flight | ¦¦ ¦ ¦ ¦ Crew. | ¦¦ ¦ ¦ ¦ ¦¦ 4) Data Link D ¦ - ¦ 0 ¦ | ¦¦ Transmitter(s) ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 5) Data Link D ¦ - ¦ 0 ¦ | ¦¦ Receiver(s) ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 26. Moving Map Display C ¦ 1 ¦ 0 ¦ | ¦¦ *** (i.e. Argus) ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ 27. GPS Cooling Fan C ¦ - ¦ 0 ¦ May be inoperative provided GPS is | ¦¦ *** ¦ ¦ ¦ considered inoperative. | ¦

Page 77


¦ ¦ ¦ ¦ (See 34-7) | ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 78


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 35-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 35 OXYGEN ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Passenger C ¦ - ¦ - ¦ Individual masks or dispensers may ¦¦ Oxygen ¦ ¦ ¦ be inoperative or missing provided ¦¦ ¦ ¦ ¦ the associated seat is ¦¦ ¦ ¦ ¦ unoccupied. ¦¦ ¦ ¦ ¦ ¦¦ 2. External Oxygen C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦¦ Pressure Gauge ¦ ¦ ¦ cockpit oxygen pressure gauge ¦¦ ¦ ¦ ¦ is operative. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 80


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 38-2 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 38 WATER/WASTE ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 2. Lavatory Waste C ¦ - ¦ - ¦ (M) Individual components may be | ¦¦ Systems ¦ ¦ ¦ inoperative provided: | ¦¦ ¦ ¦ ¦ a) Associated components are | ¦¦ ¦ ¦ ¦ deactivated or isolated and, | ¦¦ ¦ ¦ ¦ b) Associated System components | ¦¦ ¦ ¦ ¦ are verified to not have any | ¦¦ ¦ ¦ ¦ leaks. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ NOTE: Any portion of the system | ¦¦ ¦ ¦ ¦ which operates normally may | ¦¦ ¦ ¦ ¦ be used. | ¦¦ ¦ ¦ ¦ ¦¦ C ¦ - ¦ - ¦ (M) Associated Lavatory system(s) | ¦¦ ¦ ¦ ¦ may be inoperative provided: | ¦¦ ¦ ¦ ¦ a) Associated components are | ¦¦ ¦ ¦ ¦ deactivated or isolated to | ¦¦ ¦ ¦ ¦ prevent leaks, and | ¦¦ ¦ ¦ ¦ b) Lavatory door is secured | ¦¦ ¦ ¦ ¦ closed and placarded, | ¦¦ ¦ ¦ ¦ "INOPERATIVE - DO NOT ENTER" | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ NOTE: The provisions are not | ¦¦ ¦ ¦ ¦ intended to prohibit inspections | ¦¦ ¦ ¦ ¦ by crewmembers. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 82


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 52-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 52 DOORS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. PASS DOOR C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Annunciator ¦ ¦ ¦ a) A flight crewmember ¦¦ ¦ ¦ ¦ confirms by visual ¦¦ ¦ ¦ ¦ inspection that the door is ¦¦ ¦ ¦ ¦ latched prior to each ¦¦ ¦ ¦ ¦ departure, and that ¦¦ ¦ ¦ ¦ b) The locking pin at the ¦¦ ¦ ¦ ¦ handle is verified to be ¦¦ ¦ ¦ ¦ engaged by ground crew. ¦¦ ¦ ¦ ¦ ¦¦ 2. CAR DOOR C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: ¦¦ Annunciator ¦ ¦ ¦ a) A flight crewmember ¦¦ ¦ ¦ ¦ confirms by visual ¦¦ ¦ ¦ ¦ inspection that the door is ¦¦ ¦ ¦ ¦ latched prior to each ¦¦ ¦ ¦ ¦ departure. ¦¦ ¦ ¦ ¦ ¦¦ 3. Cargo Door C ¦ 1 ¦ 0 ¦ ¦¦ *** Driving Opening ¦ ¦ ¦ ¦¦ Mechanism ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 4. Cabin Door Seal C ¦ 1 ¦ 0 ¦ May be inoperative provided flight | ¦¦ ¦ ¦ ¦ is conducted unpressurized and at | ¦¦ ¦ ¦ ¦ or below 10,000 feet MSL. | ¦¦ ¦ ¦ ¦ ¦¦ 5. Cargo Door Seal C ¦ 1 ¦ 0 ¦ May be inoperative provided flight | ¦¦ ¦ ¦ ¦ is conducted unpressurized and at | ¦¦ ¦ ¦ ¦ or below 10,000 feet MSL. | ¦¦ ¦ ¦ ¦ ¦¦ 6. Emergency Exit Seal C ¦ 1 ¦ 0 ¦ May be inoperative provided flight | ¦¦ ¦ ¦ ¦ is conducted unpressurized and at | ¦¦ ¦ ¦ ¦ or below 10,000 feet MSL. | ¦¦ ¦ ¦ ¦ ¦¦ 7. Door Key Locks D ¦ 2 ¦ - ¦ (M) May be inoperative provided | ¦¦ ¦ ¦ ¦ lock is in the unlocked position | ¦¦ ¦ ¦ ¦ secured. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

Page 83


¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 84


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 56-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 56 WINDOWS ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. DV-Window Seal C ¦ 1 ¦ 0 ¦ May be inoperative provided flight | ¦¦ ¦ ¦ ¦ is conducted unpressurized and at | ¦¦ ¦ ¦ ¦ or below 10,000 feet MSL. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

Page 85


¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 86


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 77-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 77 ENGINE INDICATING ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Engine Trend D ¦ 1 ¦ - ¦ | ¦¦ Condition and ¦ ¦ ¦ | ¦¦ Monitoring System ¦ ¦ ¦ | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

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¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

Page 88


-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 79-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 79 ENGINE OIL ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. OIL QTY C ¦ 1 ¦ - ¦ (O) May be inoperative provided | ¦¦ Annunciator (CAWS) ¦ ¦ ¦ oil quantity is visually checked | ¦¦ ¦ ¦ ¦ before each flight. | ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦

Page 89


¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦-------------------------------------------------------------------------------

-------------------------------------------------------------------------------¦ U.S. DEPARTMENT OF TRANSPORTATION ¦¦ ¦¦ MASTER MINIMUM EQUIPMENT LIST ¦¦ FEDERAL AVIATION ADMINISTRATION ¦¦ --------------------------------------------------------------------------- ¦¦ AIRCRAFT: ¦ REVISION NO: 1 ¦ PAGE: ¦¦ PC-12 ¦ ¦ ¦¦ ¦ DATE: 04/16/2002 ¦ 80-1 ¦¦ --------------------------------------------------------------------------- ¦¦ 1. ¦ 2. NUMBER INSTALLED ¦¦ SYSTEM & ¦ -------------------------------------------- ¦¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦¦ NUMBERS ¦ ¦ --------------------------------------- ¦¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦¦ 80 STARTING ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ 1. Starter Generator C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦¦ Timer ¦ ¦ ¦ start cycle is interrupted when ¦¦ ¦ ¦ ¦ Ng obtains a minimum of 52% Ng. ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦ ¦¦ ¦ ¦ ¦

Page 90


Page 91


Appendix 2 – Flight Data Card

Signature: VOR Test:ZERO FUEL FUEL OUT TIME IN HOBBS IN STN ID FREQ

ENG/LDGFUEL OUT FUEL IN TIME OUT HOBBS OUT VOR1 RAD DME CYCLE:

RAMP WT FUEL USED FLT TIME HOBBS TOT VOR2 RAD DME

TREND DATA:HOBBS: IOAT IALT IAS ATQ AFF

WEIGHT: AOAT PALT CAS TAS

ISA DALT CIAS CTAS CTQ CFF

NP NG ITT OIL P OIL T Volt1/Volt2

Appendix 3: Weight and BalanceNxxx , S/N xxx, PC-12/45 LOADING FORM - 6 Seats

REF ITEM WEIGHT ARM AFT OF DATUM MOMENT (LB-IN)

Page 92


(LB) (IN)1 Basic Empty Weight 6179.20 230.48 1424186.50

2 Pilot 230.00 160.27 36862.10

3 Copilot (Right Seat Passenger) 160.27

4 LH Cabinet Stowage 12.00 212.09 2545.08

5 RH Cabinet Stowage 12.00 211.18 2534.16

6 Passenger 1 224.89






12 Rear Baggage (Max 400 lb) 371.00

13 Zero Fuel Weight (MZFW 9039 lb)

14 Fuel (Max 402 gal/2704 lb)

15 Ramp Weight (MRW 9965 lb)

16 Less Fuel for Ground Operations -44.00 232.00 -10208.00

17 Takeoff Weight (MTOW 9921 lb)


19 Landing Fuel

20 Landing Weight (MLW 9921 lb)

FUEL LOAD MOMENTSWT(LB

)ARM MOMENTS (LB-

IN)100 225.72 22572200 225.81 45161400 226.11 90443500 226.70 113351

1000 230.57 2305721200 231.20 2774411400 231.59 3242211600 231.92 3710791800 232.17 4179122000 232.37 4647462200 232.48 5114632500 232.58 5814502600 232.59 6047242704 232.62 629005

Appendix 3: Weight and BalanceNxxx , S/N xxx, PC-12/45 LOADING FORM - 5 Seats

REF ITEM WEIGHT (LB)

ARM AFT OF DATUM (IN)

MOMENT (LB-IN)

1 Basic Empty Weight ?????? ??????? ??????????

2 Pilot 230.00 160.27 36862.10

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3 Copilot (Right Seat Passenger) 160.27

4 LH Cabinet Stowage 12.00 212.09 2545.08

5 RH Cabinet Stowage 12.00 211.18 2534.16







12 Rear Baggage (Max 400 lb) 371.00


14 Fuel (Max 402 gal/2704 lb)

15 Ramp Weight (MRW 9965 lb)

16 Less Fuel for Ground Operations -44.00 232.00 -10208.00

17 Takeoff Weight (MTOW 9921 lb)


19 Landing Fuel

20 Landing Weight (MLW 9921 lb)

FUEL LOAD MOMENTSWT(LB

)ARM MOMENTS (LB-

IN)100 225.72 22572200 225.81 45161400 226.11 90443500 226.70 113351

1000 230.57 2305721200 231.20 2774411400 231.59 3242211600 231.92 3710791800 232.17 4179122000 232.37 4647462200 232.48 5114632500 232.58 5814502600 232.59 6047242704 232.62 629005

Aircraft Incident Procedure/Response

Introduction

The intent of this section is to outline the immediate considerations, steps and processes

for an effective response to an incident involving the Aircraft.

Page 94


The objective is to provide guidance concerning notification, steps to take and forms to

complete to properly handle the immediate consequences and requirements for

circumstances that by definition include serious personal injury, fatality or

substantial damage to an aircraft.

For accidents that include serious personal injury, fatality or substantial damage to an

aircraft, the procedures outlined in this section will escalate to the Aircraft

Accident Response Manual.

Aircraft Incident Procedure/Response

Definitions

For purposes of identifying the level of response required, it is important to define the

different categories of events. The following are industry standard definitions:

Aircraft

Pilatus PC-12 s/n xxx, Nxxx

Accident

An occurrence associated with the operation of an aircraft which takes place between

the time any person boards the aircraft with the intention of flight, until such time

as all persons have disembarked, and in which any persons suffer death, or

serious injury, as a result of being in or upon the aircraft, or by direct contact with

the aircraft or anything attached thereto, or in which the aircraft receives

substantial damage.

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Substantial Damage

Damage or structural failure which adversely affects the structural strength, performance

or flight characteristics of the aircraft, and which would normally require major

repair or replacement of the affected component.

NOTE: Engine failure (damage limited to an engine), bent fairing or cowling, dented

skin, small puncture holes in the skin or fabric, ground damage to rotor or

propeller blades, damage to landing gear, wheels, tires, flaps, engine accessories,

brakes, or wing tips are not considered “substantial damage” for the purposes of an

accident report.

Demolished

Includes destruction by fire

Fatal Injury

Any injury which results in death caused by the accident.

Serious Injury

Any injury which:

1. Requires hospitalization for more than 48 hours, commencing within seven days

from the date the injury was received

2. Results in a fracture of any bone (except simple fractures of fingers, toes, or nose).

3. Involves lacerations which cause severe hemorrhages, nerve muscle or tendon

damage.

4. Involves injury to any internal organ.

5. Involves second or third degree burns, or any burns affecting more than 5 percent

of the body surface.

6. Death

Page 96


Incident

1. Flight control system malfunction or failure.

2. Inability of any required flight crew member to perform their normal flight duties

as a result of injury or illness.

3. Turbine engine rotor failures excluding compressor blades and turbine buckets.

4. In-flight fire.

5. Aircraft collide in flight.

Overdue

Any aircraft which is overdue at a destination and is believed to be lost or to have been

involved in an accident.

Aircraft Incident Procedure/Response Section

On-Scene Procedures

The procedures noted below assume that an accident has occurred at a location away

from the flight operations base.

1. Get all persons clear of the aircraft.

2. Give whatever first aid is necessary and possible.

3. Provide medical attention as needed and possible. Obtain a copy of a medical

report, if possible.

4. Based on the definitions in this section, determine the level of incident or accident

and the response required.

5. Ensure that the aircraft and related equipment are guarded continuously and that

nothing is moved except to the extent necessary:

A. To remove persons injured or trapped.

B. To protect the aircraft or related equipment from further damage, or to protect the

public from injury.

6. Ensure that state and local police are notified.

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7. Notify nearest FAA general aviation district office, control tower or flight station

(listed under United Sates Government, Transportation Department, Federal

Aviation Administration). Report items with as asterisk (*) on the Information

Form. NTSB is automatically advised (NTSB Phone: 202-267-3333).

8. Notify Lance Toland Associates as soon as possible. Refer to the Lance Toland

Associates Home Office/Branch Personnel Office.

9. Make no statement and give no reports regarding estimates of damage, injuries,

or opinion of cause, except to appropriate authorities (e.g. NTSB, FAA, Insurance

representative).

A. If you are requested by an authorized representative of the FAA, the national

Transportation Safety Board, the Airport Police, or other state or local police to

give them a statement, make the following declaration as diplomatically as

possible: “ I am instructed not to make any comment related to the incident

until my insurance and legal counsel have arrived”. Remember, you are not

required to say anything that might tend to incriminate you and you are

entitled to legal counsel. You have these rights, whether or not the person

asking for the statement advises you of them. If you choose to assert these

rights, you should affirmatively state them, or they may be considered to have

been waived.

B. Attempt to satisfy all such requested by referring the requesting party to that person

contacted in the procedure listed under this section.

10. Preserve to the extent possible, the aircraft, related equipment and all records.

Additionally, records pertaining to the operation and maintenance of the aircraft

and related equipment, as well as records pertaining to the flight personnel

involved in the incident or accident.

11. Make sketches and descriptive notes. Photographs of the accident scene should

also be secured. Identify the location, including the position of the aircraft, if the

aircraft was moved, any significant impact marks and any damage to surrounding

property.

12. Obtain names, addresses and phone numbers of witnesses. Obtain written

statement, if possible.

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13. Obtain names and addresses of all federal, state and local investigators.

14. Ask the senior law enforcement official present to keep any spectators (including

news media) clear of the area until an official of the FAA or NTSB arrives and

takes charge. Request that all personnel in the area be identified as law

enforcement, medical, or official investigators.

Page 99


Aircraft Incident Procedure/Response Section

Information Form

Date_________________________

Name & Title of

reporter____________________________________________________

Location of report ________________________________________________________

Phone # of

reporter_________________________________________________________

FAA Registration

Number____________________________________________________

Make &

Model_____________________________________________________________

Owner ( if

known)__________________________________________________________

_______________________________________________________________________

__

Location of Accident:

Nature of accident:

_______________________________________________________________________

___

*Crew & Passengers Name Status Location

Pilot (in command) ___________________ ______________ ______________

Co-Pilot ( if any) ___________________ ______________ ______________

Passengers ___________________ ______________ ______________

Page 100


___________________ ______________ ______________

___________________ ______________ ______________

___________________ ______________ ______________

___________________ ______________ ______________

___________________ ______________ ______________

___________________ ______________ ______________

Page 101


*Date & Time of

Incident/Accident_____________________________________________

*Last Point of Departure & Point of Intended Landing of

Aircraft_____________________

_______________________________________________________________________

___

*Extent of Damage to the Aircraft, So Far as is

Known______________________________

_______________________________________________________________________

___

*Weather Conditions at Incident/Accident

Site____________________________________

_______________________________________________________________________

___

*Any Explosives, Radioactive Materials, or Other Dangerous Articles Carried

______________________________________________________________

_____________

_________________________________________________________________________________________________________________________________________________

Page 102

Documents

Pilatus Pc-12 Sample Ops Manual Draft