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Daher TBM 940, Pilot'S Information Manual


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Pilot's Operating Handbook

Section 2

Limitations

EASA Approved

Edition 0 - March 05, 2019
Rev. 0

Page 2.5.1

2.5

- Weight and C.G. limits

Weight limits

Maximum ramp weight (MRW) : 7430 lbs (3370 kg)

Maximum takeoff weight (MTOW) : 7394 lbs (3354 kg)

Maximum landing weight (MLW) : 7024 lbs (3186 kg)

Maximum zero fuel weight (MZFW) : 6032 lbs (2736 kg)

Maximum baggage weight :

-

in FWD compartment (non pressurized) : 110 lbs (50 kg)

>> With 6-seat accommodation

-

in rear part of pressurized cabin : 220 lbs (100 kg)

>> With 4-seat accommodation

-

in rear part of pressurized cabin : 396 lbs (180 kg), with small or large net, see
sketch below

Figure 2.5.1 - Baggage limits

PIM - DO NOT USE FOR FLIGHT OPERATIONS

Summary of Contents for TBM 940

Page 1: ...ating Handbook The content of this document is the property of DAHER AEROSPACE It is supplied in confidence and commercial security of its contents must be maintained It must not be used for any purpo...

Page 2: ...019 Rev 0 Page 0 7 Table of contents Section General 1 Limitations 2 Emergency procedures 3 Normal procedures 4 Performance 5 Weight and balance 6 Description 7 Airplane handling servicing and mainten...

Page 3: ...0 0 MAR 19 0 5 0 0 MAR 19 0 6 0 0 MAR 19 0 7 0 0 MAR 19 0 8 0 0 MAR 19 0 9 0 1 AUG 19 0 10 0 2 NOV 19 0 11 0 2 NOV 19 0 12 0 2 NOV 19 0 13 0 2 NOV 19 0 14 0 3 MAY 20 0 15 0 3 MAY 20 0 16 0 3 MAY 20 0...

Page 4: ...MAR 19 2 5 2 0 0 MAR 19 2 6 1 0 0 MAR 19 2 6 2 0 3 MAY 20 2 6 3 0 3 MAY 20 2 6 4 0 3 MAY 20 2 6 5 0 3 MAY 20 2 6 6 0 0 MAR 19 2 6 7 0 0 MAR 19 2 6 8 0 0 MAR 19 2 6 9 0 0 MAR 19 2 6 10 0 0 MAR 19 2 6 1...

Page 5: ...20 3 4 4 0 0 MAR 19 3 5 1 0 0 MAR 19 3 5 2 0 0 MAR 19 3 5 3 0 0 MAR 19 3 5 4 0 0 MAR 19 3 5 5 0 0 MAR 19 3 5 6 0 0 MAR 19 3 6 1 0 0 MAR 19 3 6 2 0 0 MAR 19 3 6 3 0 0 MAR 19 3 6 4 0 0 MAR 19 3 7 1 0 0...

Page 6: ...MAR 19 3 12 7 0 0 MAR 19 3 12 8 0 0 MAR 19 3 12 9 0 0 MAR 19 3 12 10 0 2 NOV 19 3 12 11 0 2 NOV 19 3 12 12 0 0 MAR 19 3 12 13 0 2 NOV 19 3 12 14 0 0 MAR 19 3 12 15 0 2 NOV 19 3 12 16 0 0 MAR 19 3 12...

Page 7: ...0 MAR 19 4 4 23 0 0 MAR 19 4 4 24 0 2 NOV 19 4 4 25 0 2 NOV 19 4 4 26 0 0 MAR 19 4 4 27 0 0 MAR 19 4 4 28 0 0 MAR 19 4 4 29 0 0 MAR 19 4 4 30 0 0 MAR 19 4 4 31 0 0 MAR 19 4 4 32 0 0 MAR 19 4 4 33 0 0...

Page 8: ...AR 19 5 0 1 0 0 MAR 19 5 0 2 0 0 MAR 19 5 1 1 0 0 MAR 19 5 1 2 0 0 MAR 19 5 2 1 0 0 MAR 19 5 2 2 0 0 MAR 19 5 3 1 0 0 MAR 19 5 3 2 0 0 MAR 19 5 4 1 0 2 NOV 19 5 4 2 0 0 MAR 19 5 5 1 0 0 MAR 19 5 5 2 0...

Page 9: ...0 MAR 19 6 0 2 0 0 MAR 19 6 1 1 0 0 MAR 19 6 1 2 0 0 MAR 19 6 2 1 0 0 MAR 19 6 2 2 0 0 MAR 19 6 3 1 0 0 MAR 19 6 3 2 0 0 MAR 19 6 3 3 0 0 MAR 19 6 3 4 0 0 MAR 19 6 4 1 0 0 MAR 19 6 4 2 0 0 MAR 19 6 4...

Page 10: ...32 0 0 MAR 19 7 3 33 0 2 NOV 19 7 3 34 0 2 NOV 19 7 3 35 0 0 MAR 19 7 3 36 0 0 MAR 19 7 3 37 0 0 MAR 19 7 3 38 0 0 MAR 19 7 3 39 0 0 MAR 19 7 3 40 0 0 MAR 19 7 4 1 0 0 MAR 19 7 4 2 0 0 MAR 19 7 4 3 0...

Page 11: ...9 5 0 1 AUG 19 7 9 6 0 1 AUG 19 7 9 7 0 3 MAY 20 7 9 8 0 2 NOV 19 7 9 9 0 3 MAY 20 7 9 10 0 3 MAY 20 7 9 11 0 3 MAY 20 7 9 12 0 1 AUG 19 7 9 13 0 3 MAY 20 7 9 14 0 1 AUG 19 7 9 15 0 1 AUG 19 7 9 16 0...

Page 12: ...7 15 12 0 2 NOV 19 7 15 13 0 2 NOV 19 7 15 14 0 2 NOV 19 7 15 15 0 3 MAY 20 7 15 16 0 3 MAY 20 7 15 17 0 3 MAY 20 7 15 18 0 3 MAY 20 8 0 1 0 0 MAR 19 8 0 2 0 0 MAR 19 8 1 1 0 0 MAR 19 8 1 2 0 0 MAR 19...

Page 13: ...rch 05 2019 Rev 3 Page 0 27 8 9 3 0 0 MAR 19 8 9 4 0 3 MAY 20 8 9 5 0 3 MAY 20 8 9 6 0 3 MAY 20 8 9 7 0 3 MAY 20 8 9 8 0 3 MAY 20 8 9 9 0 0 MAR 19 8 9 10 0 2 NOV 19 8 9 11 0 0 MAR 19 8 9 12 0 0 MAR 19...

Page 14: ...Pilot s Operating Handbook Section 0 Page Edit Rev Rev Date Page Edit Rev Rev Date No No No No Edition 0 March 05 2019 Rev 3 Page 0 28 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 15: ...nd entry dimensions 1 3 4 Specific loadings 1 3 4 1 4 Abbreviations and terminology 1 4 1 Meteorological terminology 1 4 1 General airspeed terminology and symbols 1 4 1 Power terminology 1 4 2 Airpla...

Page 16: ...Pilot s Operating Handbook Section 1 General Edition 0 March 05 2019 Rev 0 1 0 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 17: ...ex optional systems are given in section 9 Supplements of the POH The installed ADS B OUT system has been shown to meet the equipment requirements of 14 CFR 91 227 The installed transponder system is...

Page 18: ...Pilot s Operating Handbook Section 1 General Edition 0 March 05 2019 Rev 0 Page 1 1 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 19: ...book Section 1 General Edition 0 March 05 2019 Rev 0 Page 1 2 1 1 2 Three view drawing Figure 1 2 1 1 2 Three view drawing Airplane on level field with fully extended FWD shock absorber PIM DO NOT USE...

Page 20: ...Pilot s Operating Handbook Section 1 General Edition 0 March 05 2019 Rev 0 Page 1 2 2 Figure 1 2 1 2 2 Three view drawing PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 21: ...type 1 gas generator turbine stage 2 power turbines stages Horsepower rating and propeller speed 850 SHP at 2000 RPM Propeller Number of propellers 1 Propeller manufacturer HARTZELL Propeller model n...

Page 22: ...AVGAS shall not be used for more than 150 cumulative hours during any period between engine overhaul periods NOTE Use of AVGAS to be recorded in engine module logbook US specification US French speci...

Page 23: ...ion NATO code 5cSt MIL PRF 23699G O 156 STD O 154 HTS Figure 1 3 2 Recommended engine oil types Reference Service Bulletin P W C No 14001 at the latest revision Maximum certificated weights Ramp 7430...

Page 24: ...aximum cabin height 4 ft 1 22 m Number of cabin entries 1 standard 1 pilot door if installed Entry width standard 3 ft 6 52 in 1 08 m Entry height standard 3 ft 10 85 in 1 19 m Pilot entry mean width...

Page 25: ...n set to 29 92 inches of mercury 1013 2 hPa General airspeed terminology and symbols KCAS Knots Calibrated Airspeed is the indicated airspeed expressed in knots corrected for position and instrument e...

Page 26: ...t possible horizontal distance VY Best Rate of Climb Speed is the airspeed which delivers the greatest gain in altitude in the shortest possible time Power terminology Recovery altitude Maximum altitu...

Page 27: ...eference datum Datum perpendicular to the longitudinal airplane centerline from which all distances are measured for balance purpose Arm Is the distance from the reference datum to the center of gravi...

Page 28: ...ght approved for landing touchdown General abbreviations A Ampere or Amber ABN Abnormal ADC Air Data Computer AGL Above ground level AIL TRIM Aileron TRIM ALT SEL Altitude selector ALTI Altimeter AMP...

Page 29: ...lity Protection ESS BUS TIE Essential BUS tie EXT LIGHTS Exterior lightings F Fahrenheit degree FCU Fuel control unit FD Flight director FL Flight level FOB Fuel On Board FPL Flight Plan ft Feet ft mi...

Page 30: ...not 1 nautical mile hr 1852 m hr kW Kilowatt l Litre L or L H Left l h Litre hour lb or lbs Pound s L D Lift to drag LDG Landing LDG GR Landing gear LDR Lightweight Data Recorder LFE Landing Field Ele...

Page 31: ...Weight msg Message MTOW Maximum Takeoff Weight MXCR Maximum Cruise MZFW Maximum Zero Fuel Weight NM Nautical mile NOCR Normal cruise recommended NORM Normal PFD Primary Flight Display PHF Plan Horizon...

Page 32: ...Under Speed Protection V Volt or Voltage WARN Warning W S Windshield YD Yaw damper Radio navigation abbreviations ADF Automatic Direction Finder System ADI Attitude Director Indicator ADS B Automatic...

Page 33: ...ment Landing System IMC Instrument Meteorological Conditions L NAV Lateral NAVigation LPV Localizer Precision Vertical MKR Marker Radio Beacon NAV Navigation Indicators or Receivers P RNAV Precision a...

Page 34: ...logical Conditions V NAV Vertical NAVigation VOR VHF Omnidirectional Range VOR LOC VHF Omnidirectional Range LOCalizer WAAS Wide Area Augmentation System WFDE WAAS Fault Detection and Exclusion WGS Wo...

Page 35: ...units Metric units to Imperial and U S units Multiply By To obtain Multiply By To obtain feet 0 3048 metre metre 3 2808 feet inch 25 4 mm mm 0 03937 Inch Imp Gal 4 546 litre litre 0 220 Imp Gal USG 3...

Page 36: ...Operating Handbook Section 1 General Edition 0 March 05 2019 Rev 0 Page 1 5 2 Figure 1 5 2 Feet versus metres metres 30000 20000 10000 0 feet 2500 5000 7500 10000 31000 PIM DO NOT USE FOR FLIGHT OPER...

Page 37: ...Pilot s Operating Handbook Section 1 General Edition 0 March 05 2019 Rev 0 Page 1 5 3 Figure 1 5 3 Inches versus millimetres mm 10 0 in 250 500 750 1000 20 30 40 PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 38: ...t s Operating Handbook Section 1 General Edition 0 March 05 2019 Rev 0 Page 1 5 4 Figure 1 5 4 Pounds versus kilograms 1000 2000 3000 2000 6000 4000 0 kg lb 4000 8000 PIM DO NOT USE FOR FLIGHT OPERATI...

Page 39: ...942 1 11 0 51 8 4000 875 0 7 0 44 6 6000 811 9 3 1 37 6 8000 752 6 0 8 30 5 10000 696 8 4 8 23 4 12000 644 3 8 7 16 2 14000 595 2 12 7 9 2 16000 549 1 16 6 2 2 18000 505 9 20 6 5 0 20000 465 6 24 6 12...

Page 40: ...2 987 29 15 988 29 18 989 29 20 990 29 23 991 29 26 992 29 29 993 29 32 994 29 35 995 29 38 996 29 41 997 29 44 998 29 47 999 29 50 1000 29 53 1001 29 56 1002 29 59 1003 29 62 1004 29 65 1005 29 68 10...

Page 41: ...2 2 6 Operation limits 2 6 1 Maneuver limits 2 6 1 Temperature limits 2 6 1 Flight load factor limits 2 6 1 Generator limits 2 6 2 GFC 700 autopilot limits 2 6 2 Autothrottle limits 2 6 2 HomeSafe em...

Page 42: ...g limitations 2 6 19 2 7 Miscellaneous limits 2 7 1 Seating limits C G 2 7 1 Baggage limits 2 7 1 Minimum crew 2 7 1 Maximum occupancy 2 7 1 Use of doors 2 7 1 Cargo net installation limits 2 7 1 Weat...

Page 43: ...ently kept in the airplane with the POH Departure into IMC is not authorized if the MD302 battery fails its initial capacity check with associated message WARNING INTERNAL BATTERY MAY PROVIDE LESS THA...

Page 44: ...Pilot s Operating Handbook Section 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 1 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 45: ...eed 160 158 Do not make abrupt or full control movements above this speed VFE Maximum flaps extended speed landing configuration takeoff configuration 120 180 122 178 Do not exceed these speeds depend...

Page 46: ...Pilot s Operating Handbook Section 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 2 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 47: ...TNEY CANADA Engine model number PT6A 66D Maximum power 100 at Np 2000 RPM Ng limitation 104 1 Np limitation 2000 RPM 40 RPM ITT limitations Takeoff 850 C Maximum climb cruise 840 C During start 840 C...

Page 48: ...r maximum 20 seconds Normal oil pressure is 105 to 135 psi Oil pressures under 105 psi are undesirable Under emergency conditions to complete a flight a lower oil pressure of 60 psi is permitted at re...

Page 49: ...ditive in accordance with specification MIL I 27686 or MIL I 85470 Additive concentrations EGME or DIEGME shall be comprised between a minimum of 0 06 and a maximum of 0 15 by volume Refer to section...

Page 50: ...3404C Grade F44 DERD 2452 Issue 2 Amdt 1 F44 with additive when utilization MIL DTL 83133 Grade JP 8 AIR 3405C Grade F34 DERD 2453 Issue 4 Amdt 1 F34 with additive S748 AIR 3404C Grade F43 DERD 2498 I...

Page 51: ...arter operation limits Starter operation sequence is limited as follows if Ng 30 30 seconds if Ng 30 60 seconds Should several sequences be necessary respect following spacing 1st sequence wait 1 minu...

Page 52: ...Pilot s Operating Handbook Section 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 4 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 53: ...54 kg Maximum landing weight MLW 7024 lbs 3186 kg Maximum zero fuel weight MZFW 6032 lbs 2736 kg Maximum baggage weight in FWD compartment non pressurized 110 lbs 50 kg With 6 seat accommodation in re...

Page 54: ...20 85 of m a c 187 in 4 752 m aft of datum at all weights above 7024 lbs 3186 kg 23 8 of m a c Aft limits 193 65 in 4 921 m aft of datum at 7394 lbs 3354 kg 35 of m a c 194 in 4 928 m aft of datum at...

Page 55: ...hich the angle of bank is no more than 60 WARNING Aerobatic maneuvers including spins are not approved Temperature limits Minimum temperature at start and takeoff 40 C 40 F Maximum temperature at star...

Page 56: ...e the autopilot in descent below 2000 ft 600 m AGL with a vertical speed in excess of 2000 ft min Autothrottle AT limits Do not engage autothrottle for taxi Do not engage autothrottle below 1000 ft 30...

Page 57: ...meSafe before taking control of the airplane The airplane must be inspected by maintenance personnel before further flight if HomeSafe completes a landing GNSS GPS SBAS navigation equipment approvals...

Page 58: ...lass II Navigation RNAV 10 RNP 10 GNSS FDE availability must be verified prior to flight Maximum predicted FDE unavailability is 34 minutes 1 Two GNSS systems requi red to be operational 2 FAA AC 90 1...

Page 59: ...uired to obtain ope rational approval to utilize RNP 2 performance Departure Arrival RNP 1 with and without RF legs At a minimum the flight director must be displayed and utilized when conducting proc...

Page 60: ...cedures with RF legs Vertical guidance is based on GPS SBAS and or Baro VNAV RF legs may be used in the initial and intermediate legs of the approach pro cedure or the final leg of the missed approac...

Page 61: ...GNSS GPS SBAS navigation system limitations Navigation database limitations The pilot must confirm at system initialization that the Navigation database is current If the AIRAC cycle will change duri...

Page 62: ...RNAV T routes should be loaded into the flight plan from the database in their entirety rather than loading route waypoints from the database into the flight plan individually Selecting and inserting...

Page 63: ...gation is prohibited When using the VOR LOC GS receivers to fly the final approach segment VOR LOC GS navigation data must be selected and presented on the CDI of the pilot flying Use of Baro VNAV to...

Page 64: ...ce The Ice Detection System is only an advisory system The pilot must activate manually the ice protection systems as a preventive prior to entering icing conditions or when icing conditions are ident...

Page 65: ...dling characteristics use of the autopilot is prohibited when any of the visual cues specified above exist or when unusual lateral trim requirements or autopilot trim warnings are encountered while th...

Page 66: ...night VFR and day night IFR operations when appropriate equipment is installed and operating correctly The type certification for each use requires the following equipment The equipment must be instal...

Page 67: ...strument 2 CAS warning and caution messages Oil pressure Low fuel pressure Fuel selector OFF Fuel auxiliary pump ON L H and R H fuel tank low level Non functioning of fuel timer Battery stop Main gene...

Page 68: ...ators Fuel gauge indicators 2 Voltmeter Ammeter Outside air temperature 6 Installations Fuel mechanical pump main Fuel electrical pump auxiliary Fuel shut off valve Fuel timer Starter generator Inerti...

Page 69: ...ude display indicator 3 Instrument lighting 4 Instrument panel lighting 5 Emergency lighting 6 Vertical speed indicator 7 Navigation lights 4 8 Anticollision lights 2 9 Landing light IFR 1 All equipme...

Page 70: ...control valve 5 Safety valve 6 Pressurization control 7 Maximum cabin altitude and pressure warning light Flight into icing conditions 1 All equipment required for IFR flight 2 Propeller deicing 3 L H...

Page 71: ...with applicable operating rules Each operator must ensure compliance with required crew training and operating practices and procedures Moreover the following equipment must be installed and operating...

Page 72: ...supplementary procedures for SSR mode S enhanced surveillance in designatedeuropean airspace The capability totransmit data parameters is shown in column 2 Parameter Available A Not available NA Magne...

Page 73: ...eans for navigation or flight guidance The airplane symbol is not to be used for conducting instrument approaches or departures and it should not be relied upon during low visibility taxi operations P...

Page 74: ...Pilot s Operating Handbook Section 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 6 20 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 75: ...tion at 128 in 3 250 m Minimum crew One pilot at L H front seat Maximum occupancy Thenumber of persons on board is limited by approved seating configurationinstalled but must not exceed six including...

Page 76: ...019 Rev 0 Page 2 7 2 Weather radar limitation Weather radar can be displayed on PFD 1 PFD 2 MFD with different indications of mode Example PFD 1 SBY MODE MFD SBY MODE PFD 2 ACTIVE MODE CAUTION The rad...

Page 77: ...arking KIAS Value or range Significance Red strip Below 65 White strip 65 122 Full flap operating range Lower limit is maximum weight VSO in landing configuration Green strip 122 266 Normal operating...

Page 78: ...2 to 230 F 0 to 104 C 32 to 219 2 F 110 C 230 F Oil pressure 60 psi 60 to 105 psi 105 to 135 psi 135 psi red line normal limit Generator RPM Ng 103 to 104 51 to 103 104 Propeller RPM Np 1950 to 2050...

Page 79: ...Handbook Section 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 9 1 2 9 Placards 1 Under L H front side window 2 On pressurized baggage compartment partition wall PIM DO NOT USE FOR...

Page 80: ...ch 05 2019 Rev 2 Page 2 9 2 2 a For the small cargo net on the right lower upholstery panel 2 b For the large cargo net on R H side upholstery panel in the rear baggage compartment 2 c On FWD baggage...

Page 81: ...lot s Operating Handbook Section 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 3 Page 2 9 3 3 On pedestal console 4 On fuel selector 5 Near fuel tank caps PIM DO NOT USE FOR FLIGHT OPERATION...

Page 82: ...dition 0 March 05 2019 Rev 0 Page 2 9 4 6 On internal face of L H engine cowling Oil system capacity 12 l 12 7 qt 7 On landing gear emergency control access door 8 Under window at L H Intermediate sea...

Page 83: ...ection 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 9 5 10 Under R H control wheel 11 On nose gear door 12 On nose gear leg NOSE LANDING GEAR TIRE PRESSURE 6 5 bar 94 psi PIM DO NO...

Page 84: ...e 2 9 6 13 On main gear leg MAIN LANDING GEAR TIRE PRESSURE 8 96 bar 130 psi 14 On engine cowling in front of compartment door EXTERNAL POWER 28 VOLTS D C NOMINAL 800 AMP STARTING CAPACITY MIN DO NOT...

Page 85: ...ection 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 9 7 16 On access door External side 17 On outer fuselage skin aft of access door 18 In the cabin forward of access door PIM DO N...

Page 86: ...itations EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 9 8 19 On access door Internal side 20 On pilot door Internal side if installed 21 On emergency exit handle Marking on cover Marking on hand...

Page 87: ...ons EASA Approved Edition 0 March 05 2019 Rev 0 Page 2 9 9 22 Above emergency exit door 23 On last step of stairs 24 On rear passengers masks containers 25 On internal face of the oxygen cylinder serv...

Page 88: ...ce door 27 On emergency locator transmitter inspection door Airplane equipped with coat hanger Post MOD70 0641 25A 28 On the L H rear cargo compartment panel upper edge Airplane equipped with coat and...

Page 89: ...rating Handbook Section 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 3 Page 2 9 11 With HomeSafe emergency function Post MOD70 0650 34B 30 Above AFCS control unit PIM DO NOT USE FOR FLIGHT...

Page 90: ...Pilot s Operating Handbook Section 2 Limitations EASA Approved Edition 0 March 05 2019 Rev 3 Page 2 9 12 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 91: ...AME DEICE FAIL 3 11 1 AP ON YD OFF 3 12 20 APR DWNGRADE 3 12 25 AURAL WRN 1 CHNL 3 12 9 AURAL WRN FAIL 3 12 8 AUTO SEL 3 8 5 AUX BOOST PMP ON 3 8 3 BAT AMP 3 9 1 BAT OFF 3 9 1 CABIN ALTITUDE and USE O...

Page 92: ...8 GWX FAIL 3 12 35 HOMESAFE REQUEST 3 12 38 HS ABN BRAKES 3 7 17 HS CONFIG MODE 3 12 40 HS FUEL SHUTOFF 3 8 8 ICE DETECTED 3 11 8 ICE DETECTION FAIL 3 11 9 IGNITION 3 12 19 INERT SEP FAIL 3 11 3 INERT...

Page 93: ...14 6 PITOT NO HT L 3 11 6 PITOT NO HT R 3 11 6 PRESSU BACKUP 3 10 5 PRESSU OFF 3 10 1 PROP DEICE FAIL 3 11 2 PROP DEICE ON 7 14 4 STALL HEAT ON 7 14 6 STALL NO HEAT 3 11 7 STARTER Advisory TCAS FAIL 3...

Page 94: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 A 4 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 95: ...ailure before rotation 3 3 1 Engine failure after rotation 3 3 1 Engine failure in flight 3 3 3 OIL PRESS or OIL PRESS 3 3 4 Engine regulation discrepancy power loss throttle control loss 3 3 5 Govern...

Page 96: ...landing 3 7 2 FLAPS ASYM 3 7 3 Flaps malfunction 3 7 4 Landing with flaps malfunction 3 7 4 Landing gear retraction discrepancy 3 7 5 Landing gear extension discrepancy 3 7 6 Emergency gear extension...

Page 97: ...re blowout during landing 3 7 2 FLAPS ASYM 3 7 3 Flaps malfunction 3 7 4 Landing with flaps malfunction 3 7 4 Landing gear retraction discrepancy 3 7 5 Landing gear extension discrepancy 3 7 6 Emergen...

Page 98: ...FEATH FAULT 3 9 7 Bus bar 3 9 8 Total loss of electrical power 3 9 11 3 10 Pressurization and air conditioning 3 10 1 PRESSU OFF 3 10 1 GAS EVENT 3 10 3 GAS DEGRADED 3 10 4 PRESSU BACKUP 3 10 5 CABIN...

Page 99: ...scellaneous 3 12 1 Unsuccessful AT disconnection 3 12 1 Trim runaway 3 12 2 Crack in cockpit window or window panel 3 12 3 Emergency exit use 3 12 4 Emergency beacon ELT use 3 12 5 Inadvertent spins 3...

Page 100: ...E 3 12 25 PIT in AP vertical mode during FD approach with vertical guidance 3 12 26 VDI or VDI on Approach 3 12 27 Left PFD failure 3 12 28 AHRS failure 3 12 29 ADC failure 3 12 31 MFD failure 3 12 32...

Page 101: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 3 0 6 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 102: ...r with standard emergency procedures Alarm system recall Main failure or state modification of the different systems are provided by warning or caution messages appearing on CAS display The color code...

Page 103: ...the L H instrument panel When either one lights up press it once to reactivate It will go out and is ready to signal in the event of another failure On the CAS display the corresponding failure messa...

Page 104: ...at must be executed quickly from memory without referring to POH or checklist CONDITIONAL STEPS Conditions are presented like this 1 With related actions to perform indented inside VALIDITY EFFECTIVIT...

Page 105: ...on as practical means land on the nearest suitable runway with convenient facilities CAS MESSAGES Indicated as displayed in the MFD CAS window FUEL PRESS means FUEL PRESS warning CAS message MAIN GEN...

Page 106: ...takeoff Engine failure at takeoff before rotation 1 THROTTLE Flight IDLE 2 Brakes As required If the airplane cannot be stopped on the runway 3 THROTTLE CUT OFF 4 FUEL TANK SELECTOR OFF 5 Crash lever...

Page 107: ...keoff for any other reason 1 THROTTLE Flight IDLE 2 Reverse As required 3 Brakes As required If the airplane cannot be stopped on the runway 4 THROTTLE CUT OFF 5 FUEL TANK SELECTOR OFF 6 Crash lever P...

Page 108: ...ly the airplane 1 MAN OVRD control Full forward If power recovery successful Fly the airplane using the MAN OVRD control for power 2 THROTTLE Flight IDLE Land as soon as possible End of procedure If p...

Page 109: ...o not unfasten seat belts before complete stop End of procedure If height allows to reach a suitable landing surface 11 LANDING GEAR lever DN 12 FLAPS lever As required Maintain airspeeds Flaps UP 105...

Page 110: ...wer Fly the airplane 1 FUEL TANK SELECTOR Switch tanks 2 AUX BP switch ON 3 AT AP Disconnect If power recovery successful 4 Remaining fuel Check Land as soon as possible End of procedure If power reco...

Page 111: ...sible 1 Oil pressure Monitor 2 TRQ Minimum necessary CAUTION Due to the oil pressure drop the propeller blade angle may go towards high pitch and therefore lead to a Np propeller rotation speed decrea...

Page 112: ...using autothottle End of procedure If AT is not engaged and discrepancy still occurant If circumstances and obtained minimum power allow CAUTION In manual override mode engine is neither protected ag...

Page 113: ...in short final CAUTION When MAN OVRD control is used the available power may not be sufficient to ensure a go around in landing configuration particularly if the weight is near the maximum weight Do...

Page 114: ...gine regulation discrepancy power loss throttle control loss 3 3 Continuing 18 Long final or ILS approach Establish At IAS 178 KIAS When runway is assured 19 THROTTLE CUT OFF 20 FLAPS lever LDG as req...

Page 115: ...the reverse efficiency might be lower than expected Repair before further flight End of procedure Excessive propeller rotation speed Fly the airplane 1 Reduce power and airplane speed to avoid propell...

Page 116: ...es not stop on ground If the engine does not stop when the THROTTLE is set to CUT OFF 1 FUEL TANK SELECTOR OFF 2 Wait for engine stop due to lack of fuel in the pipes 3 GENERATOR selector OFF 4 SOURCE...

Page 117: ...eoff normally When takeoff procedure is completed If AT is engaged 2 AT Disconnect 3 THROTTLE Reduce To get ITT 820 C NOTE Above 400 ft AGL autothrottle engine protection system will reduce power to g...

Page 118: ...arameters within the limitations NOTE Single engine indicator may switch to ITT or NG parameter depending on engine conditions 1 Check that AT reacts to reduce ITT 2 ITT decreasing Check Below 820 C N...

Page 119: ...parameters within the limitations During engine start 1 Starting procedure Abort Refer to procedure Engine start chapter 4 4 2 Cancel the flight Inform maintenance department End of procedure After en...

Page 120: ...3 13 CHIP Indicates that metallic chips have been detected in the engine oil In flight Fly the airplane Land as soon as practical Inform maintenance department End of procedure On ground Do not take...

Page 121: ...takeoff normally When takeoff procedure is completed If AT is engaged 2 AT Disconnect 3 THROTTLE Reduce To get Ng 103 NOTE Above 400 ft AGL autothrottle engine protection system will reduce power to g...

Page 122: ...and control the engine parameters within the limitations NOTE Single engine indicator has switched to NG parameter 1 Check that AT reacts to reduce Ng 2 Ng decreasing Check Below 103 NOTE Single engin...

Page 123: ...s more than 104 CAUTION Autothrottle engine protection system does not relieve the pilot s responsibility to monitor and control the engine parameters within the limitations 1 AT disengaged Check 2 TH...

Page 124: ...re Monitor End of procedure If the indicated temperature is not in the green sector Failure is confirmed you can expect an oil pressure failure shortly CAUTION Due to the oil pressure drop the propell...

Page 125: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 1 Page 3 3 18 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 126: ...0 March 05 2019 Rev 0 Page 3 4 1 3 4 Air start Air start envelope NOTE Air start may be attempted outside of the envelope However above 20000 ft or at lower speeds ITT tends to increase during start a...

Page 127: ...tch OFF 4 A C switch OFF 5 Electric consumption Reduce 6 FUEL TANK SELECTOR L or R 7 AUX BP switch ON NOTE Maintain AUX BP switch in ON position for the remainder of the flight 8 IGNITION switch AUTO...

Page 128: ...If starter has not turned off automatically 15 STARTER switch ABORT 16 THROTTLE Flight IDLE 17 THROTTLE As required 18 BLEED switch As required 19 Electrical equipment As required If necessary 20 Perf...

Page 129: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 4 4 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 130: ...Fire and smoke Engine fire on ground Symptoms ITT increasing ITT smoke 1 THROTTLE CUT OFF 2 BLEED switch OFF 3 A C switch OFF 4 Brakes As required 5 FUEL TANK SELECTOR OFF If necessary 6 Warn ground a...

Page 131: ...ion 0 March 05 2019 Rev 0 Page 3 5 2 Cabin fire on ground 1 THROTTLE CUT OFF 2 Brakes As required If necessary 3 Warn ground assistance 4 Crash lever Pull down 5 Cabin extinguisher As required Evacuat...

Page 132: ...WARNING No air start attempt after an engine fire Fly the airplane 1 Oxygen masks Use 2 THROTTLE CUT OFF 3 AUX BP switch OFF 4 FUEL TANK SELECTOR OFF 5 BLEED switch OFF 6 A C switch OFF If necessary...

Page 133: ...masks to 100 oxygen and the control knob to EMERGENCY to breathe oxygen at positive pressure 3 BLEED switch OFF WARNING The cabin pressurization system is inoperative and the cabin altitude increases...

Page 134: ...or fire persists 13 GENERATOR selector OFF 14 Left hand DISPLAY BACKUP pushbutton Press 15 ESS BUS TIE switch EMER WARNING If the cause of the smoke is an unextinguished fire maintain OFF for the BLE...

Page 135: ...16 Crash lever Pull down 17 Use the standby instrument MD302 for attitude airspeed altitude heading NOTE The internal battery will provide power to the MD302 for one hour If smoke or fire stops 18 Cra...

Page 136: ...nimum airspeed according to conditions and flaps configuration Normal conditions Icing conditions Flaps UP 105 135 Flaps TO 100 115 Flaps LDG 85 95 23 Land normally When airplane is stopped 24 THROTTL...

Page 137: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 TR30 July 2023 Page 3 5 8 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 138: ...and goggles Use If the origin is known 2 Defective equipment breaker Pull 3 Cabin extinguisher Use If the origin is unknown 4 A C switch OFF 5 All unnecessary equipment OFF 6 Perform procedure Emergen...

Page 139: ...goggles Use 2 BLEED switch OFF 3 A C switch OFF 4 DUMP switch Actuate 5 Wait until the differential pressure drops 6 EMERGENCY RAM AIR control knob Pull If smoke decreases Land as soon as possible End...

Page 140: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 5 6 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 141: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 6 1 3 6 Emergency descents Emergency descents profiles PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 142: ...rate descent 1 THROTTLE Flight IDLE 2 Oxygen masks Use 3 Pitch attitude 10 to 20 If smooth air 4 FLAPS and LANDING GEAR levers UP 5 Airspeed VMO 266 KIAS If rough air or in case of structure problem...

Page 143: ...M AIR control knob Pull If VMC and non icing conditions are possible 7 ESS BUS TIE switch EMER 8 Prepare for Forced landing Refer to chapter 3 7 End of procedure If VMC and non icing conditions are no...

Page 144: ...nuing 19 AP TRIMS OFF 20 DIMMER CABIN ACCESS OFF If icing conditions 21 PITOT L R STALL HTR switch ON 22 WINDSHIELD switch ON 23 Airspeed Above 135 KIAS Configuration flaps UP If time permits 24 PLUGS...

Page 145: ...peed Maintain 120 KIAS Until favorable ground approach 8 ESS BUS TIE switch NORM To have GEAR and FLAPS available If landing surface is suitable 9 LANDING GEAR lever DN If landing surface is not suita...

Page 146: ...0 March 05 2019 Rev 0 Page 3 7 2 Tire blowout during landing 1 Control direction with brakes and nose wheel steering 2 Reverse As required 3 Stop airplane to minimize damages 4 Perform procedure Shut...

Page 147: ...prevents further operation of the flaps Fly the airplane 1 FLAPS breaker Pull 2 FLAPS lever UP Land as soon as possible 3 Maintain airspeeds IAS 178 KIAS for deflections between UP and TO positions I...

Page 148: ...d TO positions IAS 122 KIAS for deflections greater than TO position 4 For landing refer to procedure Landing with flaps malfunction Refer to procedure hereafter End of procedure Landing with flaps ma...

Page 149: ...t flashing and 3 green lights are OFF 1 Airspeed Maintain below 150 KIAS 2 LDG GEAR breaker Pull If GEAR UNSAFE CAS msg and GEAR UNSAFE red warning light are OFF 3 The flight may be continued without...

Page 150: ...ymptoms have to be considered at the end of the sequence Symptoms GEAR UNSAFE CAS msg and GEAR UNSAFE red warning light are ON or amber light flashing and 0 to 3 green lights are OFF 1 Airspeed Mainta...

Page 151: ...ed compared to a clean airplane because of the drag This should be taken into account when calculating the airplane range 1 Airspeed Maintain below 150 KIAS 2 LANDING GEAR lever DN 3 LDG GEAR breaker...

Page 152: ...tside icing conditions Continue flight at airspeed 178 KIAS Land as soon as practical End of procedure If GEAR UNSAFE red warning light is ON and GEAR UNSAFE is ON and 0 to 3 green lights are ON 9 LDG...

Page 153: ...lock Push 13 Wait one minute 14 LANDING GEAR lever UP At airspeed 150 KIAS 15 Perform landing gear extension attempts in the normal mode while applying positive load factors during the maneuver as wel...

Page 154: ...2 BLEED switch OFF 3 DUMP switch Actuate 4 FUEL TANK SELECTOR Maintain on defective LDG gear side To lighten corresponding wing maximum fuel imbalance 15 USG 5 Choose a runway with headwind or crosswi...

Page 155: ...HROTTLE CUT OFF 13 Crash lever Pull down 14 FUEL TANK SELECTOR OFF 15 Evacuate after airplane comes to a stop End of procedure If landing gear does not drag during landing 16 Preferably do not use rev...

Page 156: ...cessary 1 Transfer passengers to the rear 2 Perform a normal approach 3 FLAPS lever LDG 4 Airspeed Maintain 90 KIAS 5 AT AP Disconnect Before 200 ft 6 Land with nose up attitude Keep nose high 7 THROT...

Page 157: ...inal approach 2 FLAPS lever LDG 3 Airspeed Maintain 85 KIAS 4 BLEED switch OFF 5 DUMP switch Actuate 6 AT AP Disconnect Before 200 ft When runway is assured 7 THROTTLE CUT OFF 8 FUEL TANK SELECTOR OFF...

Page 158: ...land facing wind 1 AT AP Disconnect Before 200 ft 2 LANDING GEAR lever UP 3 FLAPS lever LDG 4 Airspeed Maintain above 85 KIAS 5 Maintain a descent rate as low as possible when approaching the water 6...

Page 159: ...ol 1 LANDING GEAR lever DN 2 FLAPS lever LDG 3 Airspeed Maintain 95 KIAS 4 TRQ As required To maintain airspeed according to an easy approach slope 300 ft min 5 Adjust elevator by using manual pitch t...

Page 160: ...LAPS and LANDING GEAR levers positions 1 Flaps and landing gear configuration Check 2 FLAPS lever Set to agree with flaps position 3 LANDING GEAR lever Set to agree with landing gear position Maximum...

Page 161: ...3 7 17 With HomeSafe emergency function Post MOD70 0650 34A HS ABN BRAKES Indicates that the HomeSafe auto brake servo is operating When possible and at the latest before 200 ft on final 1 AP TRIM DI...

Page 162: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 3 Page 3 7 18 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 163: ...3 AUX BP switch AUTO If FUEL PRESS remains ON 4 AUX BP switch ON 5 AUX BOOST PMP ON Check ON If pressure is normal again and FUEL PRESS is OFF Mechanical pump has failed 6 AUX BP switch Maintain ON L...

Page 164: ...March 05 2019 Rev 0 Page 3 8 2 2 2 FUEL PRESS Continuing If FUEL PRESS remains ON 8 Fullest tank Select 9 Avoid high power andrapidmovements of the THROTTLE 10 Altitude Below 18000 ft Land as soon as...

Page 165: ...X BP switch is in ON position Indication is normal End of procedure If AUX BP switch is in AUTO position 1 Reset AUX BP switch to ON 2 Then AUX BP switch AUTO If AUX BOOST PMP ON goes OFF 3 Continue t...

Page 166: ...the corresponding tank 1 Corresponding gage Check 2 Check the other tank has been automatically selected If other tank not automatically selected 3 FUEL SEL switch MAN 4 Select tank manually As requi...

Page 167: ...L Indicates that there is no more automatic control mode running Fly the airplane 1 FUEL SEL switch Check AUTO If FUEL SEL switch already on AUTO Failure is confirmed 2 FUEL SEL switch MAN 3 Select ta...

Page 168: ...ks are imbalanced by more than 15 USG for more than 30 seconds If FUEL SEL switch is on AUTO 1 Fullest tank Select By pressing the SHIFT push button If FUEL SEL switch is on MAN 2 Fullest tank Select...

Page 169: ...05 2019 Rev 0 Page 3 8 7 LOW LVL FAIL L R Indicates a failure of fuel low level sensor 1 Remaining fuel in tanks Check 2 Take decision If any doubt Land as soon as practical Fly the airplane On the gr...

Page 170: ...ead to an engine stop if the right fuel tank is selected 1 FUEL TANK SELECTOR L 2 AUX BP switch ON NOTE Maintain AUX BP switch in ON position for the remainder of the flight Land as soon as practical...

Page 171: ...normal CAUTION Do not take off if battery charge is over 50 A If this indication remains steady at a high value It may be due to a battery or generation system failure End of procedure BAT OFF Indicat...

Page 172: ...ERATOR RESET push button Press In case of failure Fly the airplane 3 Keep the following systems connected Autopilot system Deicing systems STROBE and NAV lights Cockpit emergency lights VHF 1 NAV GPS...

Page 173: ...arge Fly the airplane 3 Keep the following systems connected Autopilot system Deicing systems STROBE and NAV lights Cockpit emergency lights VHF 1 NAV GPS 1 BLEED LDG LIGHTS on short final This will a...

Page 174: ...y connected 3 Disconnect non essential systems 4 Voltmeter and ammeter Monitor Land as soon as possible End of procedure If MAIN GENERATOR not successfully connected 5 GENERATOR selector ST BY 6 ST BY...

Page 175: ...nly both ESS BUS bars and BATT BUS bar are directly supplied by the battery Land as soon as possible If use of other systems is required 12 ESS BUS TIE switch NORM End of procedure If VMC and non icin...

Page 176: ...FF A C OFF AUX BP OFF FUEL SEL MAN AP TRIMS OFF DIMMER CABIN ACCESS OFF If icing conditions 14 PITOT L R STALL HTR switch Check ON 15 WINDSHIELD switch ON 16 Maintain minimum recommended airspeeds int...

Page 177: ...on 0 March 05 2019 Rev 0 Page 3 9 7 ELEC FEATH FAULT Indicates a propeller feathering system malfunction Fly the airplane 1 FEATHER breaker Pull Land as soon as possible NOTE Auto ignition may turn on...

Page 178: ...Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 3 Page 3 9 8 Bus bar 1 3 Figure 3 9 1 1 3 Electrical distribution of bus bars PIM DO NOT USE FOR FLIGHT OPE...

Page 179: ...Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 2 Page 3 9 9 Bus bar 2 3 Figure 3 9 1 2 3 Electrical distribution of bus bars PIM DO NOT USE FOR FLIGHT OPE...

Page 180: ...Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 3 Page 3 9 10 Bus bar 3 3 Figure 3 9 1 3 3 Electrical distribution of bus bars PIM DO NOT USE FOR FLIGHT OPE...

Page 181: ...for attitude airspeed altitude and or heading Fly the airplane Land as soon as possible NOTE Airplane power is provided to the MD302 display for normal operation Operation of the basic system is autom...

Page 182: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 9 12 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 183: ...1 Oxygen masks Use 2 BLEED switch Check Correct If possible 3 TRQ Reduce Fly the airplane 4 BLEED switch OFF 5 BLEED switch AUTO If PRESSU OFF is still ON If altitude 10000 ft If necessary 6 Perform p...

Page 184: ...pproved Edition 0 March 05 2019 Rev 0 Page 3 10 2 PRESSU OFF 2 2 Continuing If on ground 8 BLEED switch OFF 9 Taxi back to apron 10 Perform procedure Shutdown Refer to chapter 4 3 Inform maintenance d...

Page 185: ...05 2019 Rev 0 Page 3 10 3 GAS EVENT Indicates a GASC system malfunction only displayed 45 sec after landing 1 Taxi back to the apron 2 Perform procedure Shutdown Refer to chapter 4 4 3 Inform maintena...

Page 186: ...cy procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 10 4 GAS DEGRADED Indicates a GASC system malfunction 1 Shorten the flight 2 Inform maintenance department before next flight End of pr...

Page 187: ...automatically set to 9800 ft default value as cabin altitude reference Fly the airplane 1 Continue the flight Inform maintenance department before next flight CAUTION When the airplane descends below...

Page 188: ...ude over 10000 ft 500 ft 1 Pressurization indicator Check If cabin altitude 10000 ft 500 ft 2 Oxygen masks Use Fly the airplane 3 BLEED switch Check AUTO 4 DUMP switch Check NORM Guarded 5 EMERGENCY R...

Page 189: ...d other AP modes are usable AT engages automatically and reduces power Indicates a cabin altitude over 10000 ft 500 ft 1 Pressurization indicator Check If cabin altitude 10000 ft 500 ft 2 Oxygen masks...

Page 190: ...CABIN DIFF PRESS Indicates a cabin pressure differential over 6 4 PSI 0 2 PSI 1 Pressurization indicator Check If P 6 4 PSI 0 2 PSI 2 BLEED switch OFF 3 Oxygen masks Use Fly the airplane If necessary...

Page 191: ...19 Rev 0 Page 3 10 9 Cabin not depressurized after landing If P cabin remains 0 1 DUMP switch Actuate 2 BLEED switch OFF If necessary 3 EMERGENCY RAM AIR control knob Pull 4 Wait for complete cabin de...

Page 192: ...Approved Edition 0 March 05 2019 Rev 0 Page 3 10 10 O2 CYL CLOSED Indicates that the oxygen cylinder isolation valve is closed WARNING Flight is prohibited with oxygen cylinder closed 1 Oxygen cylind...

Page 193: ...osition of the door s If DOOR is still ON 2 Do not take off End of procedure In flight Fly the airplane 3 Start a slow descent 4 Decrease cabin pressure differential By selecting a higher LFE LFE betw...

Page 194: ...vacuum may lead to malfunctioning of leading edge deicing and pressurization 1 Monitor the normal functioning of leading edge deicing and pressurization If necessary 2 Altitude Below 10000 ft 3 Retur...

Page 195: ...or Turn to the left 3 DE ICE SYSTEM mode switch MAN All deicing systems turn on 4 WINDSHIELD switch Check ON 5 INERT SEP switch As required 6 AIRFRAME DE ICE switch As required 7 PROP DE ICE switch As...

Page 196: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 10 14 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 197: ...oms failure on one of the two pneumatic deicing pulses ice on wing outboard sections or ice on wing inboard sections and stabilizers AIRFRAME DE ICE status light lit in red Leave icing conditions as s...

Page 198: ...PROP DE ICE status light lit in red propeller vibrations 1 AT Disconnect 2 TRQ Reduce Fly the airplane 3 THROTTLE Actuate To vary RPM within operating range Leave icing conditions as soon as possible...

Page 199: ...ymptoms INERT SEP ON does not appear within 50 seconds following INERT SEP switch setting ON inertial separator is not retracted after 50 seconds following INERT SEP switch setting OFF INERT DE ICE br...

Page 200: ...ice no perception of heat when touching deiced section If symptoms result from overheat 1 DE ICE SYSTEM mode switch MAN All deicing systems turn on 2 WINDSHIELD switch OFF ON When necessary In case of...

Page 201: ...ms on 5 INERT SEP switch As required 6 AIRFRAME DE ICE switch As required 7 PROP DE ICE switch As required If unsuccessful to get sufficient visibility 8 HOT AIR FLOW distributor Fully turn to the lef...

Page 202: ...running If PITOT NO HT L Icing conditions may alter airspeed indications provided by ADC1 1 Avoid icing conditions Fly the airplane If not possible 2 Perform moderate descent or climb attitudes VMO ov...

Page 203: ...g vane heating has failed or PITOT L R STALL HTR switch is not ON while the engine is running Correct operation of the aural stall warning may be altered by severe or prolonged icing 1 Airspeed Monito...

Page 204: ...by the ice detector and all deicing systems have been automatically activated NOTE ICE DETECTED will only be displayed in AUTO mode 1 DE ICE SYSTEM mode switch MAN 2 All deicing systems Check ON When...

Page 205: ...E ICE SYSTEM panel printed circuit 1 DE ICE SYSTEM mode switch MAN All deicing systems turn on NOTE In case of failure of the DE ICE SYSTEM panel printed circuit INERT SEP AIRFRAME DE ICE PROP DE ICE...

Page 206: ...Pilot s Operating Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 11 10 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 207: ...unsuccessfull to disconnect AT using AP TRIM DISC push button 3 THROTTLE Move back To disengage AT by forcing the THROTTLE lever Move forward to manage power manually If unsuccessfull to disconnect A...

Page 208: ...switch OFF 3 AP TRIM DISC push button Release 4 Pitch trim may be used manually If necessary 5 Airspeed Reduce To reduce control forces In case of pitch trim runaway 6 AP TRIMS switch AP OFF Thepitch...

Page 209: ...ures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 12 3 Crack in cockpit window or window panel Fly the airplane 1 Descend slowly 2 Cabin P Reduce By setting Landing Field Elevation to 10000 ft E...

Page 210: ...holstery panel of the emergency exit Pull it firmly through the access area to the opening handle Refer to paragraph Emergency exit in chapter 7 3 All 3 Lift up the opening handle 4 Pull emergency exi...

Page 211: ...Check that the anti theft safety pin has been removed 2 Lift up the opening handle 3 Pull emergency exit assembly towards oneself to release it from its recess 4 Put the emergency exit door inside fus...

Page 212: ...2019 Rev 0 Page 3 12 5 Emergency beacon ELT use Before a forced landing If possible 1 Transmit a MAY DAY signal on COM VHF 121 5 MHz or on a known ATC frequency After landing 2 ELT remote control swi...

Page 213: ...untary spins are prohibited 1 AP TRIM DISC push button Press and Hold until recovery 2 Control wheel Neutral Pitch and roll axis 3 Rudder Fully opposed to the spin 4 THROTTLE Flight IDLE 5 FLAPS lever...

Page 214: ...e simultaneously with stall warning aural alert 1 Fly the airplane wings levelled and nose down until stall warning stops 2 TRQ As required 3 Return to the desired flight path End of procedure USP ACT...

Page 215: ...Page 3 12 8 AURAL WRN FAIL Indicates that no aural warning alerts are available CAUTION No aural stall warning No aural overspeed warning No landing gear warning 1 Maintain airspeeds Flaps UP 105 KIAS...

Page 216: ...ection 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 12 9 AURAL WRN 1 CHNL NOTE System switches automatically on the remaining valid aural channel End of procedure PIM DO N...

Page 217: ...peed and AoA protections are inoperative Autothrottle including engine protection system may also be inoperative Fly the airplane 1 Maintain the airplane inside the flight envelope Flaps UP 105 KIAS 2...

Page 218: ...Page 3 12 11 ESP DEGRADED IAS Indicates high speed protection is inoperative Autothrottle including engine protection system may also be inoperative Fly the airplane 1 Maintain IAS below 266 KIAS 2 C...

Page 219: ...Page 3 12 12 ESP DEGRADED AOA Indicates AoA protection at low speed is inoperative Fly the airplane 1 Maintain airspeed above 1 3Vs Flaps UP 105 KIAS 266 Flaps TO 100 KIAS 178 Flaps LDG 85 KIAS 122 2...

Page 220: ...raw it out of the stowage cup and uncoil tube totally 2 Press on the red side vanes to inflate the harness 3 Put the mask onto the face If no smokes 4 3 position selector NORMAL 100 as required In cas...

Page 221: ...oved Edition 0 March 05 2019 Rev 0 Page 3 12 14 Oxygen use 2 2 Continuing For rear passengers 1 Take a mask 2 Uncoil tube totally 3 Pull on the lanyard cord to take out the lanyard pin 4 Put the mask...

Page 222: ...cation in flight 1 PITOT L R STALL HTR switch Check ON If symptoms persist 2 ALTERNATE STATIC SOURCE selector Pull thoroughly 3 Use standby instrument only If symptoms persist as well as on the electr...

Page 223: ...it severe icing conditions by changing the route or the altitude 2 Avoid any sudden maneuver on flight controls Do not engage the autopilot If the autopilot is engaged 3 Hold the control wheel firmly...

Page 224: ...ition 0 March 05 2019 Rev 0 Page 3 12 17 CARGO DOOR Indicates that front cargo door is open On ground 1 Check and close the door In flight Fly the airplane 2 Airspeed Reduce To minimum available Land...

Page 225: ...ed Edition 0 March 05 2019 Rev 0 Page 3 12 18 GPU DOOR Indicates that GPU door is open On ground 1 Check and close the door In flight Fly the airplane 2 Airspeed Reduce To minimum available Land as so...

Page 226: ...arch 05 2019 Rev 0 Page 3 12 19 IGNITION Indicates that ignition exciter is running 1 IGNITION switch Check position If weather permits 2 IGNITION switch AUTO Fly the airplane NOTE IGNITION switch may...

Page 227: ...ition 0 March 05 2019 Rev 0 Page 3 12 20 AP ON YD OFF Indicates that the autopilot is ON while Yaw Damper is OFF so no automatic rudder trim is available 1 Yaw Damper status Check If necessary 2 Yaw D...

Page 228: ...ch trim malfunction hold the control wheel firmly Up to 30 pounds of force on the control wheel may be necessary to hold the airplane level 1 AP TRIM DISC push button Press and hold NOTE When AP TRIM...

Page 229: ...etobedisplayed with a ghosted airplane icon in the center and an amber DR overwriting the icon Airplane position will be based upon the last valid GPS position then estimated by Dead Reckoning methods...

Page 230: ...nd the last known GPS position to estimate the airplane s current position DR information will be available for a maximum of 20 minutes MAP TRAFFIC MAP display is not dependent on GPS information The...

Page 231: ...Handbook Section 3 Emergency procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 12 24 ABORT APR Indicates a loss of GPS navigation Perform a go around End of procedure PIM DO NOT USE FOR F...

Page 232: ...cated by an annunciation change on the HSI 1 System will automatically downgrade to LNAV VNAV or LNAV 2 Update minimums as appropriate NOTE In some cases the approach may be downgraded without APR DWN...

Page 233: ...icates the loss of vertical integrity signal during LPV or LNAV VNAV This may be indicated by an annunciation change on the HSI Symptoms AP mode from GP flashing 5 seconds to PIT VDI is flagged and in...

Page 234: ...Approved Edition 0 March 05 2019 Rev 0 Page 3 12 27 VDI VDI or on Approach Symptoms VDI amber or VDI white at bottom of VDI window Fly the airplane If possible 1 Use LNAV minimums If not Perform a go...

Page 235: ...ures EASA Approved Edition 0 March 05 2019 Rev 0 Page 3 12 28 Left PFD failure Fly the airplane 1 L H DISPLAY BACKUP Engage TAS system is lost 2 XFR button on AFCS Press to right side then left side E...

Page 236: ...opilot AP Systems still operative Flight Director FD when engaged again Autothrottle remains engaged or may be engaged Actions Autopilot is not operative 1 AHRS1 and or AHRS2 breaker Check pushed If B...

Page 237: ...IT and or ROL gooff refer to following condition If BOTH ON AHRS1 or BOTH ON AHRS2 annunciation not associated to HDG and or PIT and or ROL annunciation s 6 PFD1 and PFD2 SENSOR softkeys Press 7 AHRS1...

Page 238: ...1 ADC 1 and or ADC 2 breaker Check pushed If BOTH ON ADC1 or BOTH ON ADC2 annunciation is associated to IAS and or ALT annunciation s 2 No action required End of procedure If all annunciations IAS ALT...

Page 239: ...ion 0 March 05 2019 Rev 0 Page 3 12 32 MFD failure NOTE If PFD2 is in fullscreen mode it will be splitted a few seconds after MFD failure Lost system MFD Actions 1 L H DISPLAY BACKUP button Press 2 MF...

Page 240: ...e airplane If transponder 2 or transponder 1 is available 1 Set transponder 2 or transponder 1 as active 2 Continue flight 3 Inform maintenance department If transponder 2 or transponder 1 is unavaila...

Page 241: ...her functions may remain available Fly the airplane If transponder 2 or transponder 1 is available 1 RestoreADS BOUTfunctionbysettingtransponder2 or transponder 1 as active 2 Continue flight 3 Inform...

Page 242: ...2 35 GWX FAIL Indicates that GWX weather radar is inoperative NOTE No real time weather data available Fly the airplane 1 WXR breaker Check pushed 2 Continue flight by using other weather data source...

Page 243: ...0 March 05 2019 Rev 0 Page 3 12 36 TCAS FAIL Indicates that Traffic Advisory System is inoperative NOTE No active traffic available but ASDB IN traffic may still be displayed Fly the airplane 1 Infor...

Page 244: ...0 March 05 2019 Rev 0 Page 3 12 37 TRAFFIC FAIL Indicates that Traffic Advisory System is inoperative NOTE No active traffic available but ASDB IN traffic may still be displayed Fly the airplane 1 Inf...

Page 245: ...50 34A HOMESAFE REQUEST Indicates that HomeSafe is active and will take control and declare an emergency in 15 seconds If the pilot wants to cancel the HomeSafe request 1 AP TRIM DISC push button Pres...

Page 246: ...Safe deactivation is not recommended on final approach 1 AP TRIM DISC push button Press twice AT and AP also disengage CAUTION MFD reconfiguration can take up to 1 minute During this time engine instr...

Page 247: ...5 2019 Rev 3 Page 3 12 40 With HomeSafe emergency function Post MOD70 0650 34A HS CONFIG MODE Indicates that HomeSafe is still in configuration mode after a maintenance operation 1 Do not start the en...

Page 248: ...Before taxiing 4 3 7 Before line up 4 3 8 Takeoff with high OAT ISA 30 C 4 3 9 Normal takeoff 4 3 10 Short takeoff 4 3 11 After takeoff 4 3 12 Climb 4 3 13 Cruise 4 3 14 Before descent 4 3 15 Approac...

Page 249: ...cedures 4 5 1 Flight into known icing conditions 4 5 1 Flight into severe icing conditions 4 5 5 Flight under heavy precipitations 4 5 6 Utilization on runways covered with water 4 5 6 Utilization on...

Page 250: ...rocedures for the conduct of normal operation of TBM airplane The first part of this section lists the normal procedures required as a check list The amplified procedures are developed in the second p...

Page 251: ...Pilot s Operating Handbook Section 4 Normal procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 4 1 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 252: ...climb speed VY Landing gear and flaps UP 124 KIAS Best angle of climb speed Vx Landing gear and flaps UP 100 KIAS Maximum speed Flaps TO 178 KIAS Flaps LDG 122 KIAS Maximum airspeed with landing gear...

Page 253: ...Pilot s Operating Handbook Section 4 Normal procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 4 2 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 254: ...sed Locked 2 Baggage Stowed 3 EMERGENCY EXIT pin Removed 4 Seat pedals harness Adjust Lock 5 PASSENGER OXYGEN STBY 6 OXYGEN ON 7 Crew oxygen masks Test 8 EXT LIGHTS All OFF 9 INT LIGHTS All OFF 10 Cra...

Page 255: ...EED OFF 24 HOT AIR FLOW Fully turned to the right 25 MAN OVRD Full backward notched 26 THROTTLE CUT OFF 27 FUEL TANK SELECTOR Open L or R 28 ALTERNATE STATIC SOURCE Pushed 29 EMERGENCY RAM AIR Pushed...

Page 256: ...arance As required 4 SOURCE BATT or GPU 5 GENERATOR MAIN 6 TEST Press 7 INERT SEP Check OFF 8 LANDING GEAR LIGHTS CHECK DOWN Test 9 MFD Initialize 10 Fuel on board Check 11 Residual ITT Check If resid...

Page 257: ...ch 05 2019 Rev 0 Page 4 3 4 Motoring if residual ITT 150 C 1 IGNITION OFF 2 AUX BP ON 3 AUX BOOST PMP ON Check ON 4 Propeller area Clear 5 STARTER ON 2 sec then OFF After 30 seconds maximum 6 STARTER...

Page 258: ...4th new engine start 1 IGNITION AUTO 2 AUX BP ON 3 AUX BOOST PMP ON Check ON 4 Propeller area Clear 5 STARTER ON 2 sec then OFF When Ng around 13 6 THROTTLE LO IDLE 7 ITT Ng OIL C and OIL PSI Monitor...

Page 259: ...R Check OFF End of procedure After engine start 1 THROTTLE LO IDLE Flight IDLE 2 Ng Check 70 2 3 OIL C and OIL PSI Check 4 AUX BP AUTO 5 FUEL SEL AUTO 6 SHIFT Test 7 AP TRIMS ON If BATT 80 amps 8 GENE...

Page 260: ...ge 4 3 7 Before taxiing 1 Stand by instruments Check 2 DE ICE SYSTEM Test 3 INERT SEP ON 4 Flight controls Check 5 TRIMS Test 6 FLAPS UP 7 MFD FPL Set LFE Set Check WX RADAR STBY 8 THROTTLE Feather tw...

Page 261: ...EL AUTO 7 DE ICE SYSTEM As required 8 INERT SEP ON 9 PITOT L R STALL HTR ON 10 TRIMS TO 11 FLAPS TO 12 A C As required 13 BLEED AUTO or MAX DIFF 14 LFE Check 15 FUEL gages Check imbalance 16 BATT Chec...

Page 262: ...3 9 Takeoff with high OAT ISA 30 C 1 BLEED OFF 2 INERT SEP OFF 3 AT disengaged Check 4 Perform procedure Normal takeoff or Short takeoff Maintaining AT disengaged until 1000 ft AGL After takeoff 5 TR...

Page 263: ...10 Normal takeoff 1 ADI HSI headings Check 2 AT As required 3 PROP RPM Green sector 4 Brakes Release 5 TRQ 100 6 Rotation airspeed 7 Attitude 10 Up When vertical speed is positive 8 Brakes Apply 9 LAN...

Page 264: ...gs Check 2 AT As required 3 PROP RPM Green sector 4 TRQ 100 5 Brakes Release 6 Rotation airspeed Weight 6579 lbs 2984 kg 7 Attitude 15 Up Weight 6579 lbs 2984 kg 8 Attitude 12 5 Up When vertical speed...

Page 265: ...A Approved Edition 0 March 05 2019 Rev 1 Page 4 3 12 After takeoff 1 LANDING GEAR Check UP 2 FLAPS Check UP 3 TRQ Check max 100 4 EIS Check 5 CAS Check 6 DE ICE SYSTEM As required 7 INERT SEP As requi...

Page 266: ...Altimeters setting As required 3 AP Check 4 AT As required 5 TRQ adjustment ITT Ng Check 6 EIS Check 7 CAS Check 8 WX RADAR As required 9 Pressurization Check 10 FUEL gages Check 11 AMPS VOLTS Check...

Page 267: ...Altimeters setting Check 2 AP Check 3 AT As required 4 TRQ adjustment ITT Ng Check 5 EIS Check 6 CAS Check 7 Pressurization Check 8 FUEL gages Check 9 AMPS VOLTS Check 10 DE ICE SYSTEM As required 11...

Page 268: ...05 2019 Rev 1 Page 4 3 15 Before descent 1 Briefing before approach Completed 2 Altimeters setting Check 3 Pressurization Check 4 LFE Check 5 FUEL gages Check 6 AMPS VOLTS Check 7 DE ICE SYSTEM As re...

Page 269: ...age 4 3 16 Approach 1 Altimeters setting QNH Set Check 2 Minimums Set Check 3 COM NAV GPS Set Check 4 Pressurization Check 5 LFE Check 6 FUEL gages Check 7 AMPS VOLTS Check 8 DE ICE SYSTEM As required...

Page 270: ...on 4 Normal procedures EASA Approved Edition 0 March 05 2019 Rev 1 Page 4 3 17 Final approach in GS or downwind leg VMC 1 LDG lights ON 2 LANDING GEAR DN Check 3 green 3 FLAPS TO End of procedure PIM...

Page 271: ...Section 4 Normal procedures EASA Approved Edition 0 March 05 2019 Rev 1 Page 4 3 18 Short final 500 ft 1 LANDING GEAR Check DN and 3 green 2 FLAPS LDG 3 AP YD AT Disconnect End of procedure PIM DO NOT...

Page 272: ...dition 0 March 05 2019 Rev 1 Page 4 3 19 Runway clear 1 TAXI light ON 2 NAV As required 3 STROBE As required 4 DE ICE SYSTEM As required 5 TRIMS Reset to TO 6 FLAPS UP 7 A C As required 8 XPDR Check 9...

Page 273: ...E Flight IDLE For 2 min 11 THROTTLE LO IDLE For 15 sec 12 THROTTLE CUT OFF 13 INERT SEP OFF 14 AUX BOOST PMP ON Check ON 15 AUX BP OFF 16 GENERATOR OFF When inertial separator is retracted after appro...

Page 274: ...tems and parts attachments deflections leaks cracks deteriorations non obstructions nicks numbers free movements position In cold weather remove even small accumulations of frost ice or snow from wing...

Page 275: ...0 March 05 2019 Rev 0 Page 4 4 2 Preflight inspection 2 16 Continuing WARNING Remove tie downs Refer to section 8 for quantities products and specifications of products and materials currently used Fi...

Page 276: ...is normally stowed in the front cargo compartment with the towing bar and the blanking covers 5 Flight controls deflections Check 6 PARK BRAKE ON 7 LANDING GEAR lever DN 8 DUMP switch NORM Guarded 9 B...

Page 277: ...or In place NOTE By pass selector must be pushed at its maximum stop so as to have the door in place 17 ALTERNATE STATIC SOURCE selector Pushed 18 EMERGENCY RAM AIR control knob Pushed 19 Breakers pan...

Page 278: ...INT LIGHTS panel All OFF 31 EXT LIGHTS panel All OFF 32 OXYGEN switch OFF 33 PASSENGER OXYGEN switch STBY 34 Emergency lighting Check CAUTION Before selecting source check position of ignition and sta...

Page 279: ...hours at a temperature below 10 C 14 F If GPU source CAUTION Low voltage around 24 5 V may indicate that only the battery is powering the airplane and not the pair GPU battery Make sure that a GPU is...

Page 280: ...witches OFF 47 ICE LIGHT switch ON 48 From outside the airplane check operation of all lights and stall warning alert Reentering the airplane 49 EXT LIGHTS panel All OFF 50 CAS display Check 51 Left a...

Page 281: ...ON 58 PITOT L R STALL HTR switch OFF 59 Crash lever Pull down Cabin II 60 Cabin fire extinguisher Pressure Attachment 61 Seats belts Check 62 Windows General condition No crack 63 Emergency exit Close...

Page 282: ...ied down to prevent rotation without oil pressure When the airplane is stored for extended periods of time a thorough preflight inspection is recommended Particular attention shouldbe paid to possible...

Page 283: ...of rain on ground and to avoid fuel loss in flight 76 Fuel tank air vent Unobstructed NOTE Air vent is not likely to be obstructed by ice or water as it is located in a wing lower surface recess 77 Le...

Page 284: ...rations relative to fuel additives L H main LANDING GEAR 83 Shock absorber Check 84 Doors Check 85 Tire Check 86 Wheel well Check NOTE If airplane has been used from muddy airfields or in snow check w...

Page 285: ...s extended red collar visible the flight is not authorized 91 Filter contamination indicator clogging indicator Check 92 L H exhaust stub Condition No cracks NOTE Inspect if possible pressure port loc...

Page 286: ...ing system two rectangular grilles located forward of the circular grille 100 Propeller and spinner No nicks cracks or oil leaks Attachment NOTE In case of operation from contaminated runways it is ne...

Page 287: ...rain two on each wing Drain Fuel free of water and contamination R H main LANDING GEAR 107 Shock absorber Check 108 Doors Check 109 Tire Check 110 Wheel well Check 111 Wing deicer boots Condition Atta...

Page 288: ...sible through an inspection door located on R H side of fuselage rear section 127 Static pressure ports Clean 128 Ventral fins Condition Attachments NOTE Ventral fins are made of two parts one fixed p...

Page 289: ...spection 16 16 Continuing 132 Static dischargers Condition 133 Vertical stabilizer deicer boots Condition Attachments 134 Rudder and trim Condition Trim position 135 Static dischargers Condition 136 T...

Page 290: ...sing in low and intermediate positions Pilot seat and R H front seat if occupied Adjust NOTE Adjust seats and harnesses so as to permit access to flight controls The pilot at L H station must be able...

Page 291: ...meSafe language is set in accordance with passengers language All 10 PASSENGER OXYGEN switch STBY 11 OXYGEN switch ON NOTE Make sure to set on STBY the PASSENGER OXYGEN switch before setting the OXYGE...

Page 292: ...GNITION switch is normally selected to AUTO This ensures ignition whenever the starter is activated 23 AUX BP switch OFF 24 FUEL SEL switch MAN 25 AP TRIMS switch OFF 26 A C switch OFF 27 SEATS HTRS M...

Page 293: ...t start 36 MAN OVRD control Full backward notched CAUTION When the engine is shut down the THROTTLE must not be moved into the reverse area 37 THROTTLE CUT OFF 38 FUEL TANK SELECTOR Open L or R 39 ALT...

Page 294: ...Start clearance As required 5 SOURCE selector BATT battery start or GPU GPU start If one screen L or R PFD or MFD is missing 6 SOURCE selector OFF 7 Wait for 30 seconds 8 SOURCE selector BATT battery...

Page 295: ...GEAR light CHECK DOWN Test 21 MFD Initialize 22 Fuel onboard Check Quantity Check FUEL TANK SELECTOR L or R 23 Residual ITT Check If residual ITT 150 C 24 Perform procedure Motoring Refer to this chap...

Page 296: ...05 2019 Rev 0 Page 4 4 23 Before starting engine 3 3 Continuing 28 PARK BRAKE Check ON NOTE PARK BRAKE appearance does not indicate that parking brake is set For that press on brake pedals before turn...

Page 297: ...BP switch ON 5 AUX BOOST PMP ON Check ON 6 FUEL PRESS Check OFF 7 Propeller area Clear CAUTION If 5 seconds after having positioned the STARTER switch in ON position there is no start interrupt starti...

Page 298: ...f fuel inside the combustion chamber before ignition NOTE In case of starting with high residual ITT an ITT decrease below 150 C within starter operation limits may allow to stay within the allowed IT...

Page 299: ...g 30 after 30 seconds of starter use Ng 50 after 60 seconds of starter use 13 THROTTLE CUT OFF 14 IGNITION switch OFF or AUTO When ITT 850 C 15 STARTER switch ABORT End of procedure ITT When Ng 50 and...

Page 300: ...utdown in high OAT above 35 C 95 F environment it is recommended to perform a 30 second dry motoring run It is possible that no trace of drainage be observed under engine due to the drainage collector...

Page 301: ...N 2 sec then OFF Simultaneously 11 Timer clock Start 12 STARTER Check ON 13 Motor For 15 sec max 14 STARTER switch ABORT Then OFF 15 STARTER Check OFF To cool engine following shutdown in high tempera...

Page 302: ...oved Edition 0 March 05 2019 Rev 0 Page 4 4 29 Motoring 3 3 Continuing 23 STARTER switch ABORT Then OFF 24 STARTER Check OFF FUEL panel 25 AUX BP switch OFF 26 AUX BOOST PMP ON Check OFF 27 FUEL PRESS...

Page 303: ...re This procedure will conserve the battery by taking advantage of first Ng acceleration Engine controls 1 MAN OVRD control Full backward notched CAUTION When the engine is shut down the THROTTLE must...

Page 304: ...ec max 1000 C for 5 sec max NOTE No action is required for the following conditions ITT from 850 C to 870 C limited to 20 seconds ITT from 870 C to 1000 C limited to 5 seconds 18 Ng 19 Oil pressure 20...

Page 305: ...5 AUX BOOST PMP ON Check OFF Electric power 26 MAIN GEN Check OFF Reset if necessary NOTE MAIN GEN normally goes off as soon as STARTER goes off If MAIN GEN does not go off 27 Ng Increase over 70 To s...

Page 306: ...y goes off as soon as STARTER goes off If MAIN GEN does not go off 7 Ng Increase over 70 To start main generator 8 Generator and battery AMPS Check charge On EIS of MFD 9 Battery and ESS bus VOLTS Che...

Page 307: ...switch ON This initializes the AP and AT systems 8 PFD 1 MFD and PFD 2 NORMAL mode Perform generator test 9 BLEED switch OFF To unload the generator circuit 10 GENERATOR selector Check MAIN 11 AMPS V...

Page 308: ...Flight Deck Pilot s Guide 18 Brightness Adjust 19 DISPLAY BACKUP push button Check Then return to NORMAL mode 20 CAS Check Check engine parameters 21 A C switch As required NOTE A good cabin temperatu...

Page 309: ...gen percent using the chart figure 4 4 2 Figure 4 4 2 Usable oxygen 4 Determine the oxygen duration in minutes by multiplying the values read on table figure 4 4 3 by the percent obtained with the cha...

Page 310: ...ular procedures of this section 2 DE ICE SYSTEM mode switch MAN All deicing systems turn on 3 INERT SEP switch OFF 4 PROP DE ICE system Check ON Check illumination in green of the status light NOTE Il...

Page 311: ...ON Check illumination in green of the status light 10 Visually check functioning of deicer boots during 1 total cycle NOTE The cycle lasts 67 seconds Check both inflation impulses the first impulse i...

Page 312: ...FD flight management 23 Weight computing Set Check 24 FOB fuel on board synchronization Set If requested 25 FPL Set 26 LFE selection Done Landing Field Elevation selection is done on the touchscreen c...

Page 313: ...taxiing 4 4 Continuing 32 THROTTLE FEATHER twice Flight IDLE to LO IDLE then Flight IDLE twice 33 EIS Check 34 CAS display Check 35 Passenger briefing As required 36 TAXI lights ON 37 PARK BRAKE OFF M...

Page 314: ...F and cause damage to the propeller 1 TAXI lights Check ON 2 THROTTLE As required NOTE After initial acceleration THROTTLE may be in the TAXI range sector avoiding excessive movements in order to keep...

Page 315: ...NAV switch ON 6 STROBE switch ON 7 IGNITION As required AUTO or ON 8 AUX BP switch AUTO 9 FUEL SEL switch AUTO DE ICE SYSTEM panel 10 INERT SEP switch ON 11 AIRFRAME DE ICE switch As required 12 PROP...

Page 316: ...proper operation from stop to stop full deflection 21 A C switch As required 22 BLEED switch AUTO The MAX DIFF mode is available through the GTC 23 LFE Check 24 FUEL gages Check quantity and imbalance...

Page 317: ...Instruments departure setting Check 31 SID Set 32 ALT SEL Set 33 XPDR Set 34 VHF VOR GPS XPDR Adjust Check 35 Stormscope TAS TAWS ADF if installed Adjust Check 36 Radar Adjust Check On ground maintain...

Page 318: ...Rotation airspeed VR Check 41 Pilot s Passengers belts Check 42 Passengers table Stowed 43 Engine instruments Check All engine parameters must be in green range except propeller RPM which will be abou...

Page 319: ...tle engine protection system is inhibited below 400 ft AGL 1 BLEED switch OFF 2 INERT SEP switch OFF 3 AT disengaged Check 4 Perform procedure Normal takeoff or Short takeoff Maintaining AT disengaged...

Page 320: ...tions 1 ADI HSI headings Check 2 Horizon Check attitude 2 NOTE Horizon has been set so as to indicate a 2 nose up attitude when airplane center of gravity is at a middle average 3 HSI Heading Stand by...

Page 321: ...n airspeed 13 Attitude 10 Up When vertical speed is positive 14 Brakes Apply Briefly 15 LANDING GEAR lever UP Airspeed 150 KIAS NOTE During the sequence The amber caution light flashes It indicates th...

Page 322: ...ch 05 2019 Rev 1 Page 4 4 49 Normal takeoff 3 3 Continuing In case of initial climb at Vx WARNING It is recommended not to retract FLAPS to UP before 500 ft AGL 17 Airspeed 100 KIAS When airspeed abov...

Page 323: ...en set so as to indicate a 2 nose up attitude when airplane center of gravity is at a middle average 3 HSI Heading Stand by instrument heading Check 4 OFF TAXI LDG switch LDG 5 AT As required 6 Engine...

Page 324: ...pply Briefly 16 LANDING GEAR lever UP Airspeed 150 KIAS NOTE During the sequence The amber caution light flashes It indicates that the landing gear pump is running It goes off when the 3 landing gears...

Page 325: ...ch 05 2019 Rev 1 Page 4 4 52 Short takeoff 3 3 Continuing In case of initial climb at Vx WARNING It is recommended not to retract FLAPS to UP before 500 ft AGL 18 Airspeed 100 KIAS When airspeed above...

Page 326: ...2019 Rev 1 Page 4 4 53 After takeoff 1 LANDING GEAR lever Check UP 2 FLAPS lever Check UP 3 TRQ Check 100 max 4 Climb airspeed 124 KIAS 5 EIS Check 6 CAS display Check 7 DE ICE SYSTEM panel As requir...

Page 327: ...100 at high altitude according to the tables during the final climb reaching the maximum permitted Ng 104 is possible and the ITT will be approximately constant giving a particular value of ITT For a...

Page 328: ...lector Adjust 12 FUEL gages Check Verify fuel quantity and imbalance correct if necessary 13 AMPS VOLTS Check CAUTION If heavy precipitation turn IGNITION and INERT SEP switches to ON 14 DE ICE SYSTEM...

Page 329: ...dex on the PFDs NOTE Engine operation tables chapter 5 8 give torque to be applied according to OAT in order not to exceed authorized maximum power When INERT SEP switch is OFF a more accurate setting...

Page 330: ...2019 Rev 1 Page 4 4 57 Cruise 2 2 Continuing CAUTION If heavy precipitation turn IGNITION and INERT SEP switches to ON 13 DE ICE SYSTEM panel As required Refer to chapter 4 5 14 INERT SEP switch As r...

Page 331: ...ON If heavy precipitation turn IGNITION and INERT SEP switches to ON 8 DE ICE SYSTEM mode switch As required Refer to chapter 4 5 9 Windshield misting protection system As required Prior to descent in...

Page 332: ...itch to ON 9 DE ICE SYSTEM mode switch As required Refer to chapter 4 5 10 Windshield misting protection system As required Prior to descent in moist conditions and to avoid canopy misting 11 HOT AIR...

Page 333: ...dicator lights Check ON 9 GEAR UNSAFE red warning light Check OFF 10 GEAR UNSAFE Check OFF 11 Amber light Check OFF NOTE During the sequence The amber caution light flashes It indicates that the landi...

Page 334: ...be extended in landing position before crossing the OUTER MARKER Without AP engaged 3 Approach airspeed 85 KIAS With AP engaged 4 Approach airspeed Above 85 KIAS NOTE This is to avoid any vertical dev...

Page 335: ...not to use reverse below 40 KIAS 2 Reverse As required Reverse may be applied as soon as the wheels touch the ground NOTE To avoid ingestion of foreign objects come out of the reverse range as speed...

Page 336: ...e 10 Up 4 FLAPS lever TO Weight below 6579 lbs 2984 kg If airspeed has been maintained at 80 KIAS or more and TRQ 100 select flaps to TO position as soon as the 10 Up attitude has been attained When t...

Page 337: ...EASA Approved Edition 0 March 05 2019 Rev 1 Page 4 4 64 Go around with AP OFF 2 2 Continuing When airspeed is at or above 115 KIAS 9 FLAPS lever UP 10 Climb airspeed As required All 11 TRQ As required...

Page 338: ...0 Up attitude has been attained When the vertical speed is positive and when airspeed is at or above 85 KIAS 4 LANDING GEAR lever UP All warning lights OFF When airspeed is at or above 110 KIAS 5 FLAP...

Page 339: ...he power to idle during the flare may induce a pronounced deceleration which may lead to a drop down of the airplane 1 Takeoff distances Checked Refer to chapter 5 9 2 Rotation airspeed VR Checked Aft...

Page 340: ...full flaps as airplane may lift off prematurely at low speed 5 THROTTLE T O power If normal takeoff 6 Attitude 10 Up If short takeoff Weight 6579 lbs 2984 kg 7 Attitude 15 Up Weight 6579 lbs 2984 kg 8...

Page 341: ...icing systems turn on 5 INERT SEP switch Check ON 6 AIRFRAME DE ICE switch OFF 7 PROP DE ICE switch OFF 8 WINDSHIELD switch As required 9 PITOT L R STALL HTR switch OFF 10 Trims Reset to takeoff posit...

Page 342: ...F 9 SEATS HTRS MASTER switch OFF 10 BLEED switch OFF 11 Check for cabin depressurization p 0 Psi 12 THROTTLE Flight IDLE For 2 min NOTE This allows the engine to stabilize at minimum obtainable ITT in...

Page 343: ...UEL TANK SELECTOR OFF 23 PARK BRAKE As required CAUTION In case of high OAT above 35 C 95 F it is required to perform 30 sec dry motoring run after shutdown to improve cooling of the bearing cavities...

Page 344: ...SA Approved Edition 0 March 05 2019 Rev 1 Page 4 4 71 Shutdown 3 3 Continuing 26 Turn the control knob to select POWER OFF on the menu and press the control knob to shut down the standby attitude modu...

Page 345: ...ition 0 March 05 2019 Rev 1 Page 4 4 72 Outside check after shutdown 1 Oxygen cylinder R H Karman Close NOTE Within 10 minutes following the engine shutdown check engine oil level Refer to chapter 8 7...

Page 346: ...tions exist when the OAT on the ground or in flight is 5 C or below and visible moisture in any form is present clouds fog with visibility of one mile 1 6 km or less rain snow sleet or ice crystals Ic...

Page 347: ...tatus light around AIRFRAME DE ICE switch If correct operation cannot be confirmed do not enter or leave as soon as possible icing conditions Perform emergency procedure Leading edges deicing failure...

Page 348: ...thickness on non deiced visible parts exceeds 15 mm or in This will avoid ice fragments coming from propeller spinner and being ingested by engine Procedures for holding approach and landing in icing...

Page 349: ...unt on one side the stall airspeed increase due to profile shape deterioration and on the other side the weight increase of the iced up airplane taking as a basis the airplane maximum weight when not...

Page 350: ...owing 1 Immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit the severe icing conditions in order to avoid extended exposure to flight con...

Page 351: ...d in highly improbable case of an engine flame out further to an important ingestion to ensure immediate restarting without action of the pilot 2 INERT SEP switch ON End of procedure Utilization on ru...

Page 352: ...y snow or ice from the wings stabilizers and movable surfaces landing gear wells and gear doors as well as flap tracks actuators and their fairings 2 Spray anti icing fluid on the wings stabilizers an...

Page 353: ...way condition The ground roll may be multiplied by 3 in some melting or not tamped snow cases 10 IGNITION switch ON 11 INERT SEP switch ON 12 INERT SEP ON Check ON Takeoff During takeoff run 13 Lightl...

Page 354: ...ilization on runways covered with melting or not tamped snow 3 3 Continuing Touch and Go WARNING Touch and Go is prohibited On the ramp after landing or taxiing 18 Do not use the parking brake to prev...

Page 355: ...nding gear wells and gear doors as well as flap tracks actuators and their fairings 2 Spray anti icing fluid on the wings stabilizers and movable surfaces upper and lower surfaces shortly before takeo...

Page 356: ...ly if necessary and very progressively by monitoring the airplane behaviour NOTE The engine torque tends to make the airplane turn to the left 16 Taxi airspeed Max 5 KIAS Use area of THROTTLE to adjus...

Page 357: ...to 25 C and very cold weather 25 C to 40 C NOTE The procedure hereafter supplements the normal procedures for the airplane use when operating under temperatures between 0 C and 40 C on ground Figure...

Page 358: ...icy or covered with tamped snow runways Refer to chapter 4 5 4 Carry out a complete rotation of the propeller to check its free rotation 5 Do not perform a fuel draining If the airplane is operating...

Page 359: ...ure Utilization on runways covered with melting or not tamped snow Refer to chapter 4 5 or 16 Perform procedure Utilization on icy or covered with tamped snow runways Refer to chapter 4 5 Landing Afte...

Page 360: ...K BRAKE Check OFF NOTE It is recommended not to use the parking brake by cold or very cold weather so that the brakes do not stick when cooling 22 Perform normal procedures defined in chapter s 4 3 an...

Page 361: ...d movable surfaces According to the condition of runways and taxiways 3 Perform procedure Utilization on runways covered with melting or not tamped snow Refer to chapter 4 5 or 4 Perform procedure Uti...

Page 362: ...heck OFF NOTE This enables to preheat spark igniters before starting the engine Before starting the engine 15 Perform normal procedures defined in Chapter s 4 3 and or 4 4 Engine start CAUTION The sta...

Page 363: ...E CUT OFF FUEL panel 22 AUX BP switch ON 23 AUX BOOST PMP ON Check ON 24 FUEL PRESS Check OFF 25 Propeller area Clear ENGINE START panel 26 IGNITION switch ON 27 IGNITION Check ON 28 STARTER switch ON...

Page 364: ...RT position of the STARTER switch 32 Starter Check OFF automatically 33 STARTER Check OFF 34 Engine parameters Check Ng 70 2 Oil pressure and ITT in green sector 35 SOURCE selector BATT 36 BAT OFF Che...

Page 365: ...ax warm 48 FAN speed selector 0 PRESSURIZATION panel 49 BLEED switch AUTO The MAX DIFF mode is available through the GTC As soon as the oil temperature is greater than 0 C 50 THROTTLE FEATHER twice Fl...

Page 366: ...lope 2 After engine start As soon as the current flow is lower than 100 A A C panel 2 A C switch PILOT 3 TEMP selector Max warm 4 FAN airspeed selector 0 PRESSURIZATION panel 5 BLEED switch AUTO The M...

Page 367: ...Envelope 3 2 2 Continuing Landing After landing Shutdown 10 Perform procedures defined for Envelope 1 NOTE If landing is foreseen by cold or very cold weather or in case of prolonged operation of the...

Page 368: ...Lateral control is not improved and flare phase is lengthened in time and in distance with increase of piloting difficulties and landing performance During approach with crosswind CAUTION Do not use o...

Page 369: ...touch this operation may provide pitch oscillations while increasing the yaw movement to the wind Do not deflect ailerons into wind while taxiing This will raise spoilers and have a detrimental effec...

Page 370: ...the condition of such a runway Particular directives Taxi Takeoff 1 INERT SEP switch ON 2 INERT SEP ON Check ON Do not use the reverse NOTE In fact on a flat runway with grass it is necessary to adopt...

Page 371: ...runway 2 2 Continuing NOTE Under 40 KIAS using the reverse makes a cloud of solid particles dusts sand gravels cut grass appear around the front face of the airplane This will damage the propeller and...

Page 372: ...o flight Check the systems availability requirements in the table 2 6 1 in section 2 GNSS GPS SBAS navigation equipment approvals depending on the planned navigation performance GPS flight plan In the...

Page 373: ...Pilot s Operating Handbook Section 4 Normal procedures EASA Approved Edition 0 March 05 2019 Rev 0 Page 4 5 28 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 374: ...Engine operation 5 8 1 Maximum climb power FL 200 124 KIAS 5 8 4 Maximum climb power FL 200 124 KIAS 5 8 5 Maximum climb power FL 200 170 KIAS M 0 40 5 8 6 Maximum climb power FL 200 170 KIAS M 0 40 5...

Page 375: ...performance after go around 5 10 9 Climb performance Flaps TO 5 10 10 5 11 Cruise performance 5 11 1 Maximum cruise 5 11 1 Normal cruise Recommended 5 11 9 Long range cruise 5500 lbs 2495 kg 5 11 17...

Page 376: ...Rev 0 Page 5 1 1 5 1 General This section provides all of the required and additional performance data for airplane operations The section 9 Supplements of the POH provides specific airplane performan...

Page 377: ...Pilot s Operating Handbook Section 5 Performance EASA Approved Edition 0 March 05 2019 Rev 0 Page 5 1 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 378: ...4 dB A ICAO Annex 16 Vol 1 6th edition Amdt 8 Chapter 10 Appendix 6 85 dB A 76 4 dB A Approved noise levels for TBM airplane are stated in EASA A 010 Type Certificate Data Sheet NOTE No determination...

Page 379: ...Pilot s Operating Handbook Section 5 Performance EASA Approved Edition 0 March 05 2019 Rev 0 Page 5 2 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 380: ...Flaps LDG LDG GR DN KIAS KCAS KIAS KCAS KIAS KCAS 125 150 175 200 225 250 266 128 154 179 205 230 255 271 70 80 90 100 120 140 160 69 80 90 101 121 141 162 60 70 80 90 100 110 120 58 68 78 88 98 108...

Page 381: ...1 124 149 174 199 224 249 270 70 80 90 100 120 140 160 70 80 90 100 120 139 159 60 70 80 90 100 110 120 59 69 79 90 100 110 120 MPH IAS MPH CAS MPH IAS MPH CAS MPH IAS MPH CAS 144 173 201 230 259 288...

Page 382: ...curve shows the minimum cabin altitude as a function of flight level corresponding to the maximum differential pressure The maximum differential pressure is limited by the pressurization system protec...

Page 383: ...Pilot s Operating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 4 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 384: ...02 07 08 17 18 27 28 6000 17 16 07 06 03 04 13 14 23 24 8000 21 20 11 10 01 00 09 10 19 20 10000 25 24 15 14 05 04 05 06 15 16 12000 29 28 19 18 09 08 01 02 11 12 14000 33 32 23 22 13 12 03 02 07 08...

Page 385: ...Pilot s Operating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 5 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 386: ...75 63 90 84 73 91 87 75 93 89 75 105 100 86 5512 lbs 2500 kg UP DN DN UP TO LDG 70 66 57 71 67 57 81 76 66 75 71 61 76 72 61 86 82 70 82 78 68 84 80 68 94 90 78 98 93 81 100 95 81 113 107 93 6579 lbs...

Page 387: ...Pilot s Operating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 6 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 388: ...ormance Edition 0 March 05 2019 Rev 0 Page 5 7 1 5 7 Wind components Figure 5 7 1 Wind components Example Angle between wind direction and flight path 50 Headwind 8 kts Crosswind 10 kts Wind speed 13...

Page 389: ...Pilot s Operating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 7 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 390: ...bles is the version 0719 14 or later This information is displayed on the MFD power up page upon system start CAUTION The TRQ setting must never exceed 100 When setting TRQ Ng must never exceed 104 Th...

Page 391: ...e maximum torque to be set Maximum climb power TRQ setting 83 for IAS 124 KIAS Add 0 5 of TRQ for each additional 10 KIAS on climb airspeed cf tables figures 5 8 1 and 5 8 1A Maximum cruise power TRQ...

Page 392: ...Pilot s Operating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 8 3 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 393: ...22 20 18 g 16 14 12 100 10 100 8 98 6 100 96 4 99 95 2 100 98 93 0 100 95 91 2 100 98 93 88 4 100 95 90 85 6 100 97 92 87 82 8 100 94 89 85 80 10 100 97 92 87 82 78 12 99 94 89 84 80 75 14 100 97 91...

Page 394: ...80 76 72 34 99 95 91 87 82 78 75 71 32 98 94 90 85 81 77 73 70 30 100 97 93 88 84 80 76 72 69 28 100 96 92 87 83 79 75 71 68 26 98 94 90 86 82 78 74 70 66 24 100 97 93 89 85 80 76 73 69 65 22 100 96...

Page 395: ...170 180 190 200 24 22 20 18 16 14 12 10 8 100 6 100 4 98 2 100 95 0 100 98 92 2 100 95 90 4 100 97 92 87 6 99 94 90 85 8 100 97 92 87 82 10 99 94 89 84 79 12 100 96 91 86 81 77 14 100 98 93 88 83 79...

Page 396: ...86 82 78 73 34 99 94 89 85 81 76 72 32 97 93 88 84 79 75 71 30 100 96 91 87 82 78 74 70 28 99 95 90 86 81 77 73 69 26 98 94 89 84 80 76 72 68 24 100 97 92 88 83 79 75 71 66 22 100 96 91 86 82 77 73 69...

Page 397: ...I msg ON T C Flight level FL OAT 100 110 120 130 140 150 160 170 180 190 200 24 22 20 18 16 14 12 10 8 6 4 2 0 2 100 4 98 6 100 95 8 98 92 10 100 95 89 12 100 97 92 87 14 99 94 89 84 16 100 97 91 86 1...

Page 398: ...1 86 82 32 100 95 90 85 80 30 98 93 88 84 79 28 97 92 87 82 78 26 100 95 90 85 81 76 24 99 94 89 84 79 74 22 97 92 87 82 77 72 20 100 96 90 85 80 75 70 18 99 94 88 83 78 73 68 16 100 97 92 86 81 76 71...

Page 399: ...190 200 24 22 20 18 16 14 12 10 8 6 4 100 2 99 0 100 96 2 99 94 4 100 96 91 6 99 93 88 8 100 95 90 85 10 100 98 92 87 82 12 100 95 89 84 79 14 100 97 92 86 81 77 16 99 94 89 84 79 18 100 96 91 86 81...

Page 400: ...81 76 30 99 94 89 84 79 75 28 97 92 87 82 78 73 26 100 96 91 86 81 76 72 24 99 94 89 84 79 74 70 22 100 97 92 87 82 77 72 68 20 100 95 90 85 80 75 70 66 18 98 93 88 83 78 73 68 64 16 100 96 91 86 81 7...

Page 401: ...Pilot s Operating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 8 12 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 402: ...A 30 C refer to procedure Normal takeoff or Short takeoff in Section 4 4 For OAT ISA 30 C refer to procedure Takeoff with high OAT ISA 30 C in Section 4 4 In SL ISA conditions nominal Np is of 1985 RP...

Page 403: ...5 850 1340 905 1415 4000 800 1260 885 1380 935 1460 990 1545 6000 880 1375 965 1505 1025 1595 1090 1690 8000 965 1500 1060 1645 1140 1765 1220 1880 Pressure altitude ft ISA 10 C ISA 20 C ISA 30 C ISA...

Page 404: ...85 1820 1355 1915 4000 1215 1725 1325 1875 1400 1975 1475 2075 6000 1320 1865 1445 2030 1545 2160 1645 2305 8000 1435 2020 1600 2240 1715 2400 1850 2570 Pressure altitude ft ISA 10 C ISA 20 C ISA 30 C...

Page 405: ...770 2445 1860 2560 4000 1685 2325 1820 2505 1910 2630 2045 2785 6000 1810 2500 1970 2710 2130 2930 2290 3135 8000 1960 2695 2220 3045 2410 3265 2590 3490 Pressure altitude ft ISA 10 C ISA 20 C ISA 30...

Page 406: ...2830 2810 2795 2775 4000 2840 2820 2805 2785 2765 2750 6000 2810 2790 2770 2750 2735 2710 8000 2775 2755 2735 2710 2690 2665 6594 lbs 2991 kg SL 2440 2425 2410 2400 2380 2365 2000 2415 2400 2385 2365...

Page 407: ...0 2 250 2 220 2 190 6000 2 305 2 270 2 235 2 205 2 170 2 140 8000 2 260 2 225 2 190 2 155 2 120 2 085 6594 lbs 2991 kg SL 2 075 2 050 2 025 2 000 1 975 1 955 2000 2 045 2 015 1 990 1 965 1 935 1 910 4...

Page 408: ...1 8 2 8 4 6000 02 15 11 9 3 0 4 02 30 13 10 3 5 5 03 00 16 12 4 1 6 8000 03 00 15 12 3 9 6 03 30 18 14 4 6 7 04 00 21 16 5 5 8 10000 03 30 18 14 4 9 8 04 15 22 17 5 7 9 05 00 26 20 6 8 11 12000 04 15...

Page 409: ...9 2 9 4 6000 02 15 12 9 3 1 5 02 30 14 11 3 6 5 03 00 16 13 4 3 6 8000 03 00 15 12 4 1 6 03 30 18 14 4 8 7 04 00 21 17 5 7 9 10000 03 45 19 15 5 0 8 04 15 22 18 5 9 10 05 15 27 21 7 0 11 12000 04 30...

Page 410: ...4 6 000 02 15 12 9 3 2 5 02 30 14 11 3 8 6 03 00 17 13 4 5 7 8 000 03 00 16 12 4 2 7 03 30 19 15 5 0 8 04 15 22 17 5 9 9 10 000 03 45 20 15 5 2 8 04 30 23 18 6 2 10 05 15 28 22 7 3 12 12 000 04 30 23...

Page 411: ...9 3 1 6 6000 02 30 13 10 3 5 7 03 00 15 12 4 0 8 03 30 18 14 4 7 10 8000 03 30 17 14 4 6 10 04 00 20 16 5 4 11 04 30 23 18 6 2 13 10000 04 15 22 17 5 7 12 05 00 25 20 6 7 15 05 45 29 23 7 7 17 12000...

Page 412: ...10 3 3 7 6000 02 30 14 11 3 6 8 03 00 16 13 4 2 9 03 30 19 15 4 9 10 8000 03 30 18 14 4 8 10 04 00 21 17 5 6 12 04 45 25 19 6 5 14 10000 04 30 23 18 6 0 13 05 15 26 21 7 0 16 06 00 31 24 8 1 18 12000...

Page 413: ...3 5 7 6000 02 45 14 11 3 8 8 03 00 17 13 4 5 9 03 30 20 15 5 2 11 8000 03 30 19 15 5 1 11 04 15 22 18 5 9 13 05 00 26 20 6 9 15 10000 04 30 24 19 6 3 14 05 15 28 22 7 4 17 06 15 33 26 8 6 19 12000 05...

Page 414: ...4000 1585 1545 1525 1500 1480 1455 1435 6000 1555 1515 1490 1465 1440 1420 1395 8000 1520 1480 1455 1430 1400 1375 1345 Conditions Landing gear DN and flaps LDG IAS 95 KIAS Airplane weight Pressure al...

Page 415: ...4000 2265 2245 2230 2215 2200 2180 2165 6000 2250 2225 2210 2190 2175 2155 2135 8000 2235 2205 2185 2165 2145 2130 2110 Conditions Landing gear UP and flaps TO IAS 115 KIAS Airplane weight Pressure al...

Page 416: ...g Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 11 1 5 11 Cruise performance Maximum cruise 7100 lbs 6300 lbs Figure 5 11 1 Cruise performance Maximum cruise PIM DO NOT USE FOR F...

Page 417: ...0 262 230 261 229 260 15000 34 100 265 208 70 1 226 276 225 275 224 275 18000 40 100 256 201 67 7 223 285 222 285 221 284 20000 44 100 251 197 66 2 221 292 220 291 219 290 21000 46 100 248 195 65 6 22...

Page 418: ...9 265 228 265 228 264 15000 24 100 268 210 70 8 224 280 223 279 222 278 18000 30 100 259 203 68 4 221 289 220 288 219 287 20000 34 100 253 199 66 9 219 296 218 295 217 294 21000 36 100 251 197 66 2 21...

Page 419: ...8 267 227 266 227 265 15000 19 100 269 211 71 2 223 282 222 281 222 280 18000 25 100 260 204 68 7 220 291 219 290 218 289 20000 29 100 254 200 67 2 218 298 217 297 216 296 21000 31 100 252 198 66 5 21...

Page 420: ...27 268 227 268 226 267 15000 14 100 271 213 71 5 222 283 222 283 221 282 18000 20 100 261 205 69 0 219 293 219 292 218 291 20000 24 100 256 201 67 6 217 300 216 299 215 297 21000 26 100 253 199 66 9 2...

Page 421: ...226 270 226 269 225 269 15000 9 100 272 214 72 0 221 285 221 284 220 283 18000 15 100 263 206 69 4 218 295 218 294 217 293 20000 19 100 257 202 67 9 216 302 216 301 215 299 21000 21 100 254 200 67 2 2...

Page 422: ...226 272 225 271 224 270 15000 4 100 274 215 72 3 221 287 220 286 219 285 18000 10 100 264 207 69 7 218 297 217 296 216 294 20000 14 100 258 203 68 3 216 303 215 302 214 301 21000 16 100 256 201 67 6...

Page 423: ...76 5 224 275 224 274 223 273 15000 6 100 276 217 73 0 219 290 218 289 217 288 18000 0 100 266 209 70 4 216 300 215 299 214 298 20000 4 100 261 205 69 0 214 307 213 306 212 304 21000 6 100 258 203 68 3...

Page 424: ...ating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 11 9 Normal cruise Recommended 7100 lbs 6300 lbs Figure 5 11 9 Cruise performance Recommended cruise PIM DO NOT USE FOR FLIGHT...

Page 425: ...73 3 230 262 230 261 229 260 15000 34 100 265 208 70 1 226 276 225 275 224 275 18000 40 100 256 201 67 7 223 285 222 285 221 284 20000 44 100 251 197 66 2 221 292 220 291 219 290 21000 46 100 248 195...

Page 426: ...74 2 229 265 228 265 228 264 15000 24 100 268 210 70 8 224 280 223 279 222 278 18000 30 100 259 203 68 4 221 289 220 288 219 287 20000 34 100 253 199 66 9 219 296 218 295 217 294 21000 36 100 251 197...

Page 427: ...74 5 228 267 227 266 227 265 15000 19 100 269 211 71 2 223 282 222 281 222 280 18000 25 100 260 204 68 7 220 291 219 290 218 289 20000 29 100 254 200 67 2 218 298 217 297 216 296 21000 31 100 252 198...

Page 428: ...3 74 9 227 268 227 268 226 267 15000 14 100 271 213 71 5 222 283 222 283 221 282 18000 20 100 261 205 69 0 219 293 219 292 218 291 20000 24 100 256 201 67 6 217 300 216 299 215 297 21000 26 100 253 19...

Page 429: ...24 75 3 226 270 226 269 225 269 15000 9 100 272 214 72 0 221 285 221 284 220 283 18000 15 100 263 206 69 4 218 295 218 294 217 293 20000 19 100 257 202 67 9 216 302 216 301 215 299 21000 21 100 254 20...

Page 430: ...225 75 7 226 272 225 271 224 270 15000 4 100 274 215 72 3 221 287 220 286 219 285 18000 10 100 264 207 69 7 218 297 217 296 216 294 20000 14 100 258 203 68 3 216 303 215 302 214 301 21000 16 100 256 2...

Page 431: ...290 227 76 5 224 275 224 274 223 273 15000 6 100 276 217 73 0 219 290 218 289 217 288 18000 0 100 266 209 70 4 216 300 215 299 214 298 20000 4 100 261 205 69 0 214 307 213 306 212 304 21000 6 100 256...

Page 432: ...203 119 205 19000 39 42 149 32 148 22 147 12 145 2 143 37 4 37 9 38 4 38 7 38 9 111 196 113 199 114 202 115 203 116 204 20000 39 44 150 34 148 24 147 14 146 4 144 37 0 37 3 37 9 38 4 38 7 110 201 111...

Page 433: ...3 106 225 26 000 43 56 151 46 150 36 148 26 146 16 145 34 6 35 1 35 4 35 6 36 2 103 223 104 226 105 228 106 230 108 233 27 000 45 57 152 47 151 37 150 27 148 17 147 34 6 35 1 35 7 36 0 36 5 103 228 10...

Page 434: ...7 125 209 19 000 43 42 156 32 154 22 152 12 151 2 150 40 0 40 3 40 7 41 3 41 9 119 205 120 207 121 209 123 211 124 214 20 000 43 44 154 34 153 24 151 14 150 4 149 38 9 39 5 39 9 40 5 41 1 116 206 117...

Page 435: ...5 111 226 26 000 45 56 152 46 150 36 148 26 147 16 146 35 9 36 2 36 6 37 2 37 8 107 224 108 226 109 228 111 232 112 235 27 000 47 57 154 47 152 37 150 27 148 17 147 36 2 36 5 36 9 37 2 37 8 107 231 10...

Page 436: ...7 135 220 19 000 49 42 160 32 159 22 158 12 157 2 156 42 0 42 6 43 3 44 0 44 6 125 210 127 213 129 217 131 219 133 222 20 000 49 44 160 34 159 24 157 14 156 4 155 41 4 42 1 42 5 43 2 43 9 123 214 125...

Page 437: ...1 118 232 26 000 51 56 153 46 151 36 150 26 149 16 148 37 4 37 9 38 5 39 2 39 8 111 226 113 228 114 231 117 235 118 238 27 000 52 57 155 47 153 37 151 27 149 17 148 37 7 38 1 38 5 39 0 39 6 112 232 11...

Page 438: ...23 7 8 48 24000 16 00 55 43 14 5 73 12 00 37 29 9 8 55 09 35 28 22 7 3 44 22000 14 40 51 40 13 4 66 11 00 34 27 9 1 50 08 50 26 20 6 8 40 20000 13 20 47 37 12 3 59 10 00 32 25 8 4 44 08 00 24 19 6 3...

Page 439: ...Pilot s Operating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 12 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 440: ...holding time Weight 5500 lbs 2495 kg Weight 6300 lbs 2858 kg 10 min 30 min 10 min 30 min l kg USG l kg USG l kg USG l kg USG SL 30 23 7 8 89 70 23 5 30 24 8 0 91 71 24 1 5000 26 21 6 9 79 62 20 8 27...

Page 441: ...Pilot s Operating Handbook Section 5 Performance Edition 0 March 05 2019 Rev 0 Page 5 13 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 442: ...and level runway In table headings GR Ground roll in ft D50 Landing distance clear to 50 ft in ft Corrections In case of wind apply the following corrections Reduce total distances by 10 every 10 kts...

Page 443: ...0 1805 2395 1940 2560 2035 2660 2135 2790 6000 1940 2560 2100 2725 2200 2855 2300 2955 8000 2100 2725 2265 2920 2360 3020 2495 3180 Pressure altitude ft ISA 10 C ISA 20 C ISA 30 C ISA 37 C GR D50 GR D...

Page 444: ...0 1180 2100 1280 2230 1345 2330 1410 2395 6000 1280 2230 1380 2360 1445 2460 1510 2525 8000 1380 2360 1475 2490 1540 2590 1610 2690 Pressure altitude ft ISA 10 C ISA 20 C ISA 30 C ISA 37 C GR D50 GR D...

Page 445: ...1000 2100 1080 2230 1150 2330 1200 2395 6000 1080 2230 1180 2360 1230 2460 1280 2525 8000 1180 2360 1245 2490 1310 2590 1360 2690 Pressure altitude ft ISA 10 C ISA 20 C ISA 30 C ISA 37 C GR D50 GR D5...

Page 446: ...alance 6 4 1 General 6 4 1 Utilization of weight and balance graph 6 4 2 Airplane loading form m kg 6 4 4 Example of airplane weight and balance report 6 4 6 Weight and balance form and diagram m kg 6...

Page 447: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 6 0 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 448: ...is properly loaded and the weight and balance limits are adhered to This airplane allows multiple cabin seat configurations between 2 seats and 6 seats as required by the operator refer to chapter 7...

Page 449: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 1 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 450: ...ne weighing procedures Refer to maintenance manual for the procedures to use NOTE Weighing carried out at the factory takes into account all equipment installed on the airplane The list of this equipm...

Page 451: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 2 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 452: ...ng the cabin from the baggage compartment is attached to frame C14 With other allowed seat accommodations There are two loading areas onein place of the 2removedrear seats with maximum loadingcapacity...

Page 453: ...green self adhesive labels affixed to the inside of the rail A placard indicates loading limits for each securing net Evenly distribute the load within the cargo zone and ensure that overall weight i...

Page 454: ...lations concerning transport of dangerous product and any other applicable regulation Baggage compartments loading must be done in accordance with the weight and balance limits of the airplane refer t...

Page 455: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 3 4 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 456: ...imits are adhered to The procedure requires the following data related to the basic characteristics of the empty airplane to be obtained from the last airplane weight and balance report the empty weig...

Page 457: ...formulas 6 Record the loaded fuel 6a and compute associated moment 6b 7 Compute ramp weight 7a and moment 7b as sum of zero fuel weight 3a loaded fuel 6a and moments 3b 6b 8 Check value 7a to be belo...

Page 458: ...and balance Edition 0 March 05 2019 Rev 0 Page 6 4 3 19 Check that all points are within the weight and balance limits and check that they are vertically aligned 20 Record these data on your navigati...

Page 459: ...kg 2a 4 534 2b Inter seats 15 4 kg per seat removed 2a 5 710 2b Pax 2a 2b Rear bench net 21 kg per seat removed 2a 6 785 2b Pax 2a 2b Cargo 80 kg 2a 2b Baggage AFT 100 kg 2a 7 695 2b Zero fuel weight...

Page 460: ...age 6 4 5 Item Weight kg Empty weight 1a Baggage FWD 50 kg 2a Front seats 2a Inter seats 15 4 kg per seat removed 2a Pax 2a Rear bench net 21 kg per seat removed 2a Pax 2a Cargo 80 kg 2a Baggage AFT 1...

Page 461: ...ch 05 2019 Rev 0 Page 6 4 6 Example of airplane weight and balance report NOTE Airplane original report shall be kept with airplane POH Figure 6 4 1 Example of weight and balance report and basic airp...

Page 462: ...balance Edition 0 March 05 2019 Rev 0 Page 6 4 7 NOTE Airplane original report shall be kept with airplane POH Figure 6 4 2 Example of weight and balance report and basic airplane characteristics in...

Page 463: ...CG MAC Empty weight kg Baggage FWD 50 kg 3 250 Front seats kg 4 534 Inter seats 15 4kgper seat removed 5 710 Pax Rear bench net 21 kg per seat removed 6 785 Pax Cargo 80 kg Baggage AFT 100 kg 7 695 Ze...

Page 464: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 4 9 Figure 6 4 3 Weight and balance diagram PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 465: ...AC Empty weight lbs Baggage FWD 110 lbs 128 0 Front seats lbs 178 5 Inter seats 34 lbs per seat removed 224 8 Pax Rear bench net 46 2 lbs per seat removed 267 1 Pax Cargo 176 lbs Baggage AFT 220 lbs 3...

Page 466: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 4 11 Figure 6 4 4 Weight and balance diagram PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 467: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 4 12 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 468: ...lation concerning your airplane refer to the diagram corresponding to its validity Fig 6 4 5 1 Airplane basic characteristics W Empty weight Moment Balance arm CG MAC 2 126 kg 10 073 m kg 4 738 m 22 9...

Page 469: ...15 4kgper seat removed 0 5 710 0 Pax 0 0 Rear bench net 21 kg per seat removed 0 6 785 0 Pax 160 1 086 Cargo 80 kg 0 0 Baggage AFT 100 kg 50 7 695 385 Zero fuel weight 2736 kg 2 536 4 910 12 451 34 3...

Page 470: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 4 15 Figure 6 4 5 Loading sample in kg and m PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 471: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 4 16 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 472: ...iagram corresponding to its validity Fig 6 4 6 1 Airplane basic characteristics W Empty weight Moment Balance arm CG MAC 4 638 lbs 864 173 in lbs 186 3 in 22 6 2 Foreseen loading FWD compartment 1 Pil...

Page 473: ...ed 0 224 8 0 Pax 220 49 456 Rear bench net 46 2 lbs per seat removed 92 4 267 1 24 680 Pax 0 0 Cargo 176 lbs 176 47 010 Baggage AFT 220 lbs 220 303 0 66 660 Zero fuel weight 6032 lbs 5 562 193 1 1 074...

Page 474: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 4 19 Figure 6 4 6 Loading samples in lbs and in PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 475: ...xcept those listed in this Chapter Use the chart below to compute new empty weight and corresponding balance if necessary Date Equipment or modification description Weight modification Basic empty wei...

Page 476: ...86 3 400 25 Equipment and furnishings partial A 0171 25 Generation 2008 cabinets Version A L H low cabinet 9 48 4 300 203 74 5 175 Version B R H low cabinet 9 48 4 300 203 74 5 175 Version C Removabl...

Page 477: ...back to or in flight direction 34 06 15 45 224 65 5 706 S 0588 25 R H Intermediate seat with heaters system back to or in flight direction 34 06 15 45 224 65 5 706 Double chair S 0588 25 L H Seat with...

Page 478: ...List of equipment The list of equipment is available in manufacturer Report reference NAV No 34 90 RJ App 8 located at the end of this POH A separate list of equipment of items installed at the facto...

Page 479: ...Pilot s Operating Handbook Section 6 Weight and balance Edition 0 March 05 2019 Rev 0 Page 6 5 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 480: ...nterface panel Post MOD70 0650 34B 7 3 18 Doors windows and emergency exit 7 3 18 Seats belts and harnesses 7 3 26 Baggage compartments 7 3 32 Use of cargo nets 7 3 35 7 4 Flight controls 7 4 1 Roll 7...

Page 481: ...ons 7 7 1 AT engagement and disengagement 7 7 3 Engine start or engine air start 7 7 4 Taxi 7 7 4 Takeoff 7 7 4 Climb 7 7 4 Cruise 7 7 5 Descent 7 7 8 Approach 7 7 8 Go around 7 7 9 Landing 7 7 9 FD v...

Page 482: ...ystem ECS 7 10 6 7 11 Emergency oxygen system 7 11 1 Flight above 15000 ft with possible emergency descent 7 11 4 When required to remain above 15000 ft due to minimum enroute altitude 7 11 5 Flight b...

Page 483: ...7 15 2 GPS 7 15 2 Weather radar 7 15 3 Emergency locator transmitter 7 15 6 Lightweight data recorder LDR 1000 7 15 7 ADS B OUT function 7 15 8 Flight deck information system FS 510 7 15 8 Data collec...

Page 484: ...d herein is optional and may not be installed in the airplane Complete description and operation of the GARMIN integrated flight deck are detailed in the GARMIN Pilot s Guide References to this guide...

Page 485: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 1 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 486: ...equipped with a retractable tricycle landing gear The pressurized cabin is equipped on the left side of fuselage with a one piece access door and folding stairs comprising a hand rail allowing pilot...

Page 487: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 2 2 Figure 7 2 1 Cabin arrangement 6 seat accommodation PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 488: ...lot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 2 3 Figure 7 2 1A Cabin arrangement 4 seat accommodation with large securing net PIM DO NOT USE FOR FLIGHT OPERATION...

Page 489: ...lot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 2 4 Figure 7 2 1B Cabin arrangement 4 seat accommodation with small securing net PIM DO NOT USE FOR FLIGHT OPERATION...

Page 490: ...ed on the trailing edge of left side aileron is electrically activated by a trim switch through an actuator Wing flaps see figure 7 2 2 The wing flaps are large span slotted flaps with a single rotati...

Page 491: ...Description Edition 0 March 05 2019 Rev 0 Page 7 2 6 Figure 7 2 2 1 2 Wing flaps 1 Geared motor 2 Internal actuator 3 Intermediate bearings 4 Wing flap 5 External actuator 6 Rods 7 Control selector P...

Page 492: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 2 7 Figure 7 2 2 2 2 Wing flaps PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 493: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 2 8 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 494: ...MFD refer to the GARMIN Pilot s Guide for detailed description Apart from the GARMIN flight deck system equipment listed below complete the instrument panel Left area instrument panel includes see fi...

Page 495: ...ar on the MFD CAS window to alert crew about monitored systems discrepancies As a message appears a chime is heard Refer to the GARMIN Pilot s Guide to know all possible CAS messages A MASTER WARNING...

Page 496: ...escription of the other aural warning alerts Cockpit overhead panel see figure 7 3 2 This panel includes following elements the loud speaker of GMA the TEST push button the emergency lighting rheostat...

Page 497: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 4 Figure 7 3 1 Instrument panel assembly Typical arrangement PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 498: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 5 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 499: ...4 Instrument panel emergency lighting switches rheostats 5 R H cockpit floodlight 6 ELT remote control switch 7 AP TRIMS switch 8 FUEL control panel see figure 7 7 3 9 ENGINE START switches see figur...

Page 500: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 7 Figure 7 3 2 2 2 Upper panel and cockpit overhead panel PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 501: ...Alternate station reception micro jack 9 L H station rudder pedals adjusting handle 10 Left station reception micro jacks 11 Adjustable air outlet 12 Flight conditions and instruction placard 13 AP TR...

Page 502: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 3 9 Figure 7 3 3 2 2 Left instrument panel Typical arrangement PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 503: ...1 2 Central instrument panel 1 BARO knob 2 Micro LDR 3 AFCS control unit 4 LVL push button With HomeSafe emergency function Post MOD70 0650 34B 5 HomeSafe activation button All 6 Registration 7 MFD 8...

Page 504: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 3 11 Figure 7 3 4 2 2 Central instrument panel Typical arrangement PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 505: ...7 AP TRIM DISC push button 8 Adjustable air outlet 9 Circuit breakers panel postlight 10 R H station rudder pedals adjusting handle 11 Right station reception micro jacks 12 USB servicing plugs 13 Cre...

Page 506: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 13 Figure 7 3 5 2 2 Right instrument panel Typical arrangement PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 507: ...nsole 1 THROTTLE 2 FLAPS lever 3 THROTTLE and MAN OVRD friction adjustment 4 Manual FUEL TANK SELECTOR see figure 7 7 2 5 Roll trim tab control 6 MAN OVRD emergency fuel regulation lever 7 Pitch trim...

Page 508: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 15 Figure 7 3 6 2 2 Pedestal console Typical arrangement PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 509: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 16 Figure 7 3 7 Circuit breakers panel PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 510: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 17 Figure 7 3 8 General alarms warning lights PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 511: ...to extend CAUTION Retract stairs before closing access door and make sure door deflection area is clear To retract stairs press on locking pin located on stairs front string board see detail 1 raise r...

Page 512: ...he door from outside the airplane press on knob on outside fuselage at the right side of the door The door driven by a geared motor tilts downwards up to a position near the complete closing Push the...

Page 513: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 20 Figure 7 3 9 Cabin access door PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 514: ...TION Retract footstep before closing access door Fold and tilt footstep upwards To close the door from inside the airplane pull the door until it aligns with fuselage and lock it by moving inside hand...

Page 515: ...t is maintained in the up position by a compensation rod Two interlocking type latches ensure itsclosing andit is equipped with a lock same key as for the accessdoor andthe pilotdoor ifinstalled When...

Page 516: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 23 Figure 7 3 9A Cockpit access door pilot door PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 517: ...by a safety pin provided with a flag marker The handle is then inoperable WARNING Taxiing and flying with thief proof safety pin installed is forbidden To open the emergency exit pull one of the two...

Page 518: ...s one inside and the other outside each located on the upper frame When the airplane is parked the closing system may be locked by a safety pin provided with a flag marker The handle is then inoperabl...

Page 519: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 25 Figure 7 3 10 Emergency exit PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 520: ...34D r Il Pilot s Operating Handbook Pre MOD70 0793 25 1 Upholstery panel 2 Opening handle 1 1 t f I Step 1 t 1 j 1 t 1 L t f 0 1 l 0 0 00 7 0 Step 2 0 Figure 7 3 1 OA Removal of the upholstery panel o...

Page 521: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 TR29 July 2022 Page 7 3 25B Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 522: ...ng element in the cushion and one heating element in the backrest of each seat The SEATS HTRS MASTER switch located on the instrument panel HI OFF LOW three positions switch located on each cockpit an...

Page 523: ...ment in the cushion and one heating element in the backrest of each seat The SEATS HTRS MASTER switch located on the instrument panel HI OFF LOW three positions switch located on each cockpit and cabi...

Page 524: ...ription Edition 0 March 05 2019 Rev 0 Page 7 3 27 Figure 7 3 11 Heated seat 1 SEATS HTRS MASTER switch 2 Backrest surface heating 3 Seat surface heating 4 HI OFF LOW three position switch 5 Tactile ma...

Page 525: ...ng the switch to the right In this position the seat heats at its maximum capacity LOW position is obtained by positioning the switch to the left In this position the seat heats less than HI position...

Page 526: ...sts of two individual seats installed back to the flight direction mounted on the same rails as the front seats The seat back angle is adjusted by pulling up side handle two rear seats arranged as a b...

Page 527: ...ility of seat configuration Cargo zone ONLY zone B and zone C can be modified for seat configurations For the MID Seat zone B ONLY the Middle Seats can be installed in MID Seat Zone This zone accepts...

Page 528: ...X X C6 X X X C7 X X C8 X X C9 2 X X C10 1 X C11 X X X C12 2 X X C13 X X C14 X X C15 1 X C16 X X C17 X C18 X C19 2 X C20 1 Zone B Zone C 1 This configuration accepts small net or large net 2 With seat...

Page 529: ...6 seat accommodation There are two baggage compartments An AFT compartment located in the pressurized cabin between rearpassenger seats and rear pressure bulkhead A FWD compartment non pressurized loc...

Page 530: ...aw concerning transport of dangerous materials and any other applicable regulation With 4 seat accommodation Two cargo nets are available for the pilot to safely secure and transport baggage the small...

Page 531: ...s affixed on R H side upholstery panel in the rear baggage compartment Maximum loads allowable in the baggage compartments depend on airplane equipment refer to section 6 Weight and balance WARNING An...

Page 532: ...on tensioning strap strap must mandatorily be discarded and replaced webbing frayed or cut on less than 30 of its surface reduce maximum load by 50 seam of vertical net tensioning straps damaged on l...

Page 533: ...Front seat s back rest tilt control 10 Drawer for pilot s piddle pak if installed front side new bags rear side used bags 11 Intermediate seat s back rest tilt control 12 Rear bench seat s back rest...

Page 534: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 37 Figure 7 3 12 2 2 Seats PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 535: ...ront passenger seat 2 L H pilot seat 3 R H intermediate passenger seat facing flight direction 4 L H intermediate passenger seat facing flight direction 5 Front seat s longitudinal shift control 6 Fro...

Page 536: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 39 Figure 7 3 12A 2 2 Seats PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 537: ...ot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 3 40 All Figure 7 3 13 Front and rear seat belts with movable straps and harnesses PIM DO NOT USE FOR FLIGHT OPERATIO...

Page 538: ...is deflected upwards and remains in wing profile when the aileron is deflected downwards Control wheel movement is transmitted through rods to fuselage roll lever located under the floor The movement...

Page 539: ...Description Edition 0 March 05 2019 Rev 0 Page 7 4 2 Figure 7 4 1 1 2 Roll 1 Pedestal assembly 2 Control wheels 3 Fuselage roll lever 4 Spoiler 5 Aileron 6 Aileron control in wing 7 Spoiler control P...

Page 540: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 4 3 Figure 7 4 1 2 2 Roll PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 541: ...Description Edition 0 March 05 2019 Rev 0 Page 7 4 4 Figure 7 4 2 1 2 Lateral trim 1 Roll trim tab 2 Aileron 3 Adjustable rods 4 Actuator 5 Trim tab control wiring 6 Trim switch on pedestal console P...

Page 542: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 4 5 Figure 7 4 2 2 2 Lateral trim PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 543: ...tick shaker and the stall warning A spring actuator creates a nose down artificial force which allows a better static stability Each control surface is provided with an automatic anti tab automaticity...

Page 544: ...0 Page 7 4 7 Figure 7 4 3 1 2 Elevator 1 Control wheel assembly 2 Elevators 3 Lever assembly fuselage rear part 4 Elevator bellcrank 5 Rod with presseal connection 6 Lever assembly under floor 7 Pede...

Page 545: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 4 8 Figure 7 4 3 2 2 Elevator PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 546: ...iption Edition 0 March 05 2019 Rev 0 Page 7 4 9 Figure 7 4 4 1 2 Pitch trim 1 Cables 2 Pulleys 3 Pitch trim tabs 4 Actuating rods 5 Actuator 6 Pitch trim manual control wheel 7 Electric pitch trim con...

Page 547: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 4 10 Figure 7 4 4 2 2 Pitch trim PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 548: ...trument panel and a locking device on the rudder pedals This balllocking device allows selecting six different positions When landing gear is down rudder pedals are linked to nose gear steering system...

Page 549: ...March 05 2019 Rev 0 Page 7 4 12 Figure 7 4 5 1 2 Rudder 1 Roll rudder combination bellcrank installation 2 Rudder pedals assembly 3 Control cables 4 Pulleys 5 Rudder lever assembly 6 Rod 7 Rudder 8 N...

Page 550: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 4 13 Figure 7 4 5 2 2 Rudder PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 551: ...Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 4 14 Figure 7 4 6 1 2 Rudder trim 1 Trim switch on control wheel 2 Actuator 3 Rudder trim tab 4 Rods 5 Rudder trim control wiring PIM DO NOT...

Page 552: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 4 15 Figure 7 4 6 2 2 Rudder trim PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 553: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 4 16 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 554: ...ition nose wheel is automatically disconnected Actuating cylinders have a locking device integrated at both ends This device maintains landing gear in up or down position Landing gear doors two on the...

Page 555: ...ghts are OFF Down locked correct indication is when there are 3 green indicator lights ON the GEAR UNSAFE red warning light is OFF the GEAR UNSAFE is OFF and the amber caution light is OFF All other c...

Page 556: ...n 0 March 05 2019 Rev 0 Page 7 5 3 Figure 7 5 1 Control panel and landing gear indicating 1 Green indicator light 2 Red warning light 3 LANDING GEAR lever 4 CHECK DOWN push button 5 LIGHT TEST push bu...

Page 557: ...nd TO position Takeoff and landing gear is not down locked NOTE If one of above conditions exists and airplane is in stall configuration the Stall landing gear aural warning alert sounds and the contr...

Page 558: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 5 5 Figure 7 5 2 Emergency landing gear extension control PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 559: ...20 Steering may be increased up to 28 by applying differential braking to each side Airplane may be towed by attaching a steering or towing bar on nose gear refer to chapter 8 6 for operation In that...

Page 560: ...rating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 5 7 Figure 7 5 3 Minimum turn diameter Full rudder pedals travel without using differential braking PIM DO NOT USE FOR FLIGHT...

Page 561: ...perating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 5 8 Figure 7 5 4 Minimum turn diameter Full rudder pedals travel by using differential braking PIM DO NOT USE FOR FLIGHT OP...

Page 562: ...ayed in the CAS window if the servo motor is operating All Parking brake see figures 7 5 5 7 5 5A and 7 5 6 Parking brake control consists of a control knob located on pilot s side lower instrument pa...

Page 563: ...ut HomeSafe emergency function Pre MOD70 0650 34A Figure 7 5 5 1 2 Brake system 1 Reservoir 2 Vent 3 R H station master cylinders 4 PARK BRAKE control knob 5 PARK BRAKE valve 6 Drain 7 Pilot s station...

Page 564: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 5 11 Figure 7 5 5 2 2 Brake system PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 565: ...t MOD70 0650 34A Figure 7 5 5A 1 2 Brake system 1 Reservoir 2 Vent 3 HomeSafe braking servo actuator 4 HomeSafe master cylinder 5 R H station master cylinders 6 PARK BRAKE control knob 7 PARK BRAKE va...

Page 566: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 5 13 Figure 7 5 5A 2 2 Brake system PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 567: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 5 14 All Figure 7 5 6 Brake system PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 568: ...yed into combustion chamber by fuel nozzles The mixture is first ignited by two spark igniter plugs then combustion continues as a result of air fuel mixture flow Gases resulting from combustion expan...

Page 569: ...r governor 2 Exhaust stub 3 Axial compressors 4 Accessory gearbox 5 FCU Fuel Control Unit 6 Oil to fuel heater 7 Input coupling shaft 8 Air intake 9 Centrifugal impeller 10 Combustion chamber 11 Compr...

Page 570: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 6 3 Figure 7 6 1 2 2 Powerplant PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 571: ...wo levers located on pedestal console in cabin THROTTLE and its detent for reverse GA push button and AT DISC push button MAN OVRD control for emergency fuel regulation Thumbwheel for lever friction F...

Page 572: ...imum reverse the Beta valve to select the propeller pitch in reverse Return to idle position is accomplished by pushing the THROTTLE forward CAUTION Do not move the cockpit THROTTLE into the propeller...

Page 573: ...e the propeller is in feather position The THROTTLE can be positioned to CUT OFF idle LO IDLE or idle HI IDLE Change from idle HI IDLE to LO IDLEposition requiresmoving theTHROTTLE rearwards Change fr...

Page 574: ...the THROTTLE by an assembly of rods and levers permitting to link the GARMIN servo motor and the potentiometer The THROTTLE movements are defined by the servo motor The THROTTLE position is measured b...

Page 575: ...Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 6 8 Figure 7 6 4 Autothrottle 1 Pedestal assembly 2 Potentiometer 3 Servo motor 4 Rod 5 Lever PIM DO NOT USE FOR FLIGHT OP...

Page 576: ...hrottle is disconnected when the MAN OVRD lever is used Lever friction see figure 7 6 2 A thumbwheel located on right side of pedestal console allows the clamping of the THROTTLE lever and MAN OVRD le...

Page 577: ...tion The two other indications that do not have priority are displayed only in the form of a digital information There is only one arc displayed at a time with either TRQ NG or ITT At all times the di...

Page 578: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 6 11 Figure 7 6 6 Priority indication NG Figure 7 6 7 Priority indication ITT PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 579: ...uantity in system A visual oil sight glass located on engine left side allows a rapid checking of oil level NOTE For checking and oil filling up refer to section 8 Engine starting see figure 7 6 8 Ign...

Page 580: ...which drives powerplant STARTER lights on indicating that the starter generator is operating Starter operation is stopped automatically by the electrical power system once a sufficient starter genera...

Page 581: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 6 14 Figure 7 6 8 Engine starting PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 582: ...cally controlled by INERT SEP switch located on DE ICE SYSTEM panel When INERT SEP switch is set to ON an electric actuator activates vanes INERT SEP ON lights on when vanes have reached their maximum...

Page 583: ...essor turbine tacho generator Ng Compressor turbine tacho generator Ng is attached on accessory gearbox It supplies a voltage which is transmitted to the GARMIN system fordisplay onthe MFD under norma...

Page 584: ...nominal value of 2000 RPM Regulation is obtained through propeller blade pitch variation counterweights drive propeller blades toward high pitch low RPM whereas oil pressure delivered by governor dri...

Page 585: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 0 Page 7 6 18 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 586: ...6 Powerplant Single engine indicator and to GARMIN Pilot s Guide Engine Indication System EIS section AT engine and airspeed protections The AT function includes engine and airspeed protections to en...

Page 587: ...during extention or retraction of the inertial separator The engine will only require inspection maintenance if 110 torque is exceeded AT airspeed protections AT airspeed protections are complementar...

Page 588: ...tton on the THROTTLE lever Press the AP TRIM DISC push button on the control yoke AP FD will also be disengaged At AT standard disengagement an AT annunciation flashes during approximately 5 s and one...

Page 589: ...othrottle limits Takeoff Do not engage AT for takeoff if OAT ISA 30 C refer to section 2 6 2 Autothrottle limits If OAT ISA 30 C AT can be engaged for takeoff as follows When the aircraft is lined up...

Page 590: ...e FMS climb schedule Torque target display In MAN or FMS mode the Maximum Climb Torque index is displayed on the torque gauge when the inertial separator is OFF Its value corresponds to the Maximum Cl...

Page 591: ...d maintain the selected cruise schedule In FMS speed mode the AT takes speed constraints of the flight plan into account If the active leg of the flight plan has a speed constraint the speed constrain...

Page 592: ...lected Cruise Schedule Maximum Cruise No Speed Constraint AT mode MXCR Managed AT TRQ 100 IAS 200 kt maximum airspeed corresponding to torque value Examples with speed constraints Altitude 5 000 ft Se...

Page 593: ...nd maintain the target airspeed In MAN mode the target airspeedis themanually selectedairspeed InFMS mode the target airspeed is retrieved from the FMS descent schedule Then the target vertical speed...

Page 594: ...lateral and vertical modes become active With the AT disengaged if the GA push button is pressed only the FD GA lateral and vertical modes become active The AT remains disengaged NOTE With AT engaged...

Page 595: ...FD vertical modes and AT modes depending on the MAN FMS mode Active FD Vertical Mode Corresponding AT Mode MAN Corresponding AT Mode FMS PIT SPD XXXKT SPD XXXKT LVL ALT ALTS ALTV SPD XXXKT RCR MXCR LR...

Page 596: ...f the unit It is fitted with a by pass valve a clogging indicator and a drain valve With HomeSafe emergency function Post MOD70 0650 34A HomeSafe fuel shut off valve HomeSafe shuts down the engine aft...

Page 597: ...ump HP 6 Oil to fuel heater 7 Low pressure switch 8 Fuel jet 9 Main mechanical boost pump 10 Electric boost pump 11 Fuel filter 12 Filter clogging by pass valve 13 Filter clogging indicator 14 Fuel un...

Page 598: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 8 3 Figure 7 8 1 2 2 Fuel system PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 599: ...uel heater 7 Low pressure switch 8 Fuel jet 9 Main mechanical boost pump 10 Electric boost pump 11 Fuel filter 12 Filter clogging by pass valve 13 Filter clogging indicator 14 Fuel unit 15 Filter drai...

Page 600: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 8 5 Figure 7 8 1A 2 2 Fuel system PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 601: ...e fuel unit selector on the selected tank The sequencer controls the time during which the selected tank will operate This time varies depending on airplane conditions Airplane on ground tank is chang...

Page 602: ...arance of AUTO SEL AUTO SEL also lights on when order given by the sequencer has not been executed after 12 seconds Electric boost pump AUX BP Electric boost pump is an auxiliary pump located between...

Page 603: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 8 8 Figure 7 8 2 Manual selector of fuel tanks PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 604: ...s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 8 9 Figure 7 8 3 Fuel control panel 1 AUX BP switch 2 FUEL SEL switch 3 SHIFT push button PIM DO NOT USE FOR FLIGHT OPER...

Page 605: ...side fuel level gage is equipped with a low level detector which leads to fuel low level CAS messages appearance when usable fuel quantity remaining in the concerned fuel tank is under about 9 USG 34...

Page 606: ...d prior to the first flight of the day and after each tank refueling using a sampler to pick off fuel at the two drain valves of each tank and at the filter vent valve A red filter bypass flag on the...

Page 607: ...on 0 March 05 2019 Rev 3 Page 7 8 12 Figure 7 8 4 Fuel system draining points and clogging indicator 1 Lighting switch 2 Mirror door 3 Clogging indicator 4 Central access door 5 Filter drain 6 Tank dr...

Page 608: ...ver is positioned in theUP position SOURCE selector in the OFF position the battery supplies the electrical power system through the BATT BUS A Power Up Built In Test P BIT of the EPS internal functio...

Page 609: ...he power required for starting when no ground power unit is available and is a power supply source when engine driven generators are stopped The battery is always connected to BATT BUS bus bar except...

Page 610: ...catedonR H sidepanel see figure 7 9 4 In caseof overloadof asystem the breaker triggers and switches the system off CAUTION If a breaker corresponding to a non essential system trips do not reset in f...

Page 611: ...ich are not essential for flight safety for that set ESS BUS TIE switch to EMER position In this configuration only ESS BUS 1 ESS BUS 2 and BATT BUS bars are supplied NOTE Supplying BUS 1 BUS 2 BUS 3...

Page 612: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 9 5 Figure 7 9 1 Electrical diagram PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 613: ...attery UP BATT MAIN NORM Battery MAIN Battery MAIN Battery MAIN Battery MAIN UP BATT ST BY NORM Battery ST BY Battery ST BY Battery ST BY Battery ST BY UP OFF MAIN NORM MAIN MAIN MAIN MAIN UP OFF ST B...

Page 614: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 9 7 Figure 7 9 3 1 3 Electrical distribution of bus bars PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 615: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 2 Page 7 9 8 Figure 7 9 3 2 3 Electrical distribution of bus bars PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 616: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 9 9 Figure 7 9 3 3 3 Electrical distribution of bus bars PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 617: ...res torque propeller AIRFRAME 1 ENGINE Powerplant cont protection Ng flowmeter ITT AIRFRAME 2 FUEL GAGE 1 L H fuel gage protection FUEL GAGE 2 R H fuel gage protection ESS BUS 2 ESS BUS 2 Essential bu...

Page 618: ...ency function protection Post MOD70 0650 34A BUS 2 ICE DETEC Ice detector protection PROP DE ICE Propeller deicing protection ICE LIGHT L H wing leading edge lighting and lighting test protection FLAP...

Page 619: ...elector timer protection AUX BP Electrical fuel pump protection ADF ADF protection if installed TAXI LIGHT Taxi light protection LH LDG LIGHT L H landing light protection RH LDG LIGHT R H landing ligh...

Page 620: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 3 Page 7 9 13 Figure 7 9 4 4 4 Breaker panel Typical arrangement PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 621: ...systems protection in case of overvoltage short circuits In case of disconnection of starter generator or stand by generator following a failure MAIN or ST BY reset can be done by pressing correspond...

Page 622: ...k Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 9 15 Figure 7 9 5 Electrical control 1 MAIN reset knob 2 ST BY reset knob 3 Crash lever 4 SOURCE selector 5 GENERATOR selector PIM DO NOT U...

Page 623: ...nglets and located in leading edges They are controlled by setting to TAXI a switch located on upper panel Navigation lights and strobe lights Two strobe and navigation lights are installed in the win...

Page 624: ...nation of the FWD compartment is controlled by the switch located in the upper section of the door frame Fuel unit compartment light The lighting of the fuel unit compartment allows improving the visi...

Page 625: ...escription Edition 0 March 05 2019 Rev 1 Page 7 9 18 Figure 7 9 6 External lighting controls 1 Taxi and landing light switch 2 Pulselite system switch 3 Navigation lights switch 4 Strobe lights switch...

Page 626: ...the crash lever is down access lighting is automatically cut out after 3 minutes If the crash lever is up there is no access lighting automatic cut out Cabin lighting Cabin lighting consists of two in...

Page 627: ...ostat located on the cockpit overhead panel controls emergency lighting operation and intensity Forward rotation of control knob allows changing from OFF position to minimum lighting then increasing l...

Page 628: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 9 21 Figure 7 9 7 2 2 Internal lighting controls PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 629: ...Edition 0 March 05 2019 Rev 1 Page 7 9 22 115V Plug The 115V plug permits to connect external equipments max power 250 W The plug is located on the right aft side of the cabin compartment in the stor...

Page 630: ...m Dual zones Environmental Control System which includes heating andcooling functions These sub systems are managed by a single digital controller the GASC which receives information from the sensors...

Page 631: ...ng the P2 5 port The Inlet Pressure Port Sensor IPPS measures the pressure at the P2 5 port and sends the value to the GASC which manages the ports switching on condition with the Shut Off Valve SOV A...

Page 632: ...C controls the modulation of the Outflow Valve OFV in order to reach the computed cabin altitude System operation See figure 7 10 3 The BLEED switch allows to activate the pressurization system Either...

Page 633: ...itude rate of change in order to land with a cabin altitude equal to LFE minus 200 ft The pilot selects LFE on the touchscreen controller automatically by setting a destination airport in the flight p...

Page 634: ...total loss of pressurization or that the heating system is degraded GAS EVENT is displayed 45 seconds after landing if a fault on the Overheat Thermal Switch was detected by the GASC during flight MA...

Page 635: ...ted in the cockpit cabin zones depending on the demand The air is distributed into the cockpit zone through ports located on pedestal sides ports under each seat or the demisting outlets into the cabi...

Page 636: ...ASC to 23 C After GASC software evolution Post MOD70 0689 21 The system maintains the cabin air inlet temperature previously selected The pilot can modulate this temperature by using the TEMP selector...

Page 637: ...volution Post MOD70 0689 21 When the HOT AIR FLOW distributor is set in defog position fully turned to the left the bleed air system automatically switches from the P2 5 to the P3 bleed port to increa...

Page 638: ...our fans are supplied by BUS 4 bar and protected respectively by following breakers COND FAN CAB FAN CKPT FAN and GND FAN The system includes an automatic load shedding feature which when MAIN GEN is...

Page 639: ...gement select Air temperature expectations Cockpit panel selection Cabin panel selection Cockpit area Warm Cabin area Hot Results Mixed Bleed Air Circuit Warm air is distributed to both cockpit and ca...

Page 640: ...ve as no TEMP selector is set in the blue arc FANS select 0 Selecting a FAN speed will reduce cabin air temperature Cockpit area Warm Cabin area Cool Results Mixed Bleed Air Circuit Warm air is distri...

Page 641: ...resultingin bothcockpit andcabin air conditioning systems supplying their respective area Cockpit and cabin FANS Select 1 or more to circulate the cooled air Cockpit area Cool Cabin area Warm Results...

Page 642: ...used by the GASC for air temperature management Air temperature expectations Cockpit panel selection Cabin panel selection Cockpit area Warm Cabin area Results Mixed Bleed Air Circuit Warm air is dis...

Page 643: ...arc the Hot Air Distributor discharges the mixed bleed air below the floor towards the cold air circuit fans and evaporators to reduce the air to the desired temperature Cold Air Circuit Cockpit TEMP...

Page 644: ...ckpit panel selection Cabin panel selection Cockpit area Cabin area Results Mixed Bleed Air Circuit Air is distributed to the windshields and cockpit side windows at a fixed temperature regardless of...

Page 645: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 2 Page 7 10 16 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 646: ...orts 6 Cabin control panel 7 Global air system controller GASC 8 Out flow valve OFV 9 Safety valve SFV 10 Condenser fan 11 Condenser 12 High pressure switch 13 Drier filter 14 Cabin fan 15 Cabin evapo...

Page 647: ...ck valve 30 MFD unit 31 Ground safety microswitch 32 Differential pressure switch 33 By pass valve BPV 34 Cabin altitude alarm switch 35 Emergency air supply system EMERGENCY RAM AIR 36 Main heat exch...

Page 648: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 2 Page 7 10 19 Figure 7 10 2 3 3 GAS PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 649: ...9 Rev 2 Page 7 10 20 Figure 7 10 3 1 2 GAS controls 1 A C switch 2 FAN speed selector cockpit cabin 3 TEMP selector cockpit cabin 4 DUMP switch 5 HOT AIR FLOW distributor 6 BLEED switch 7 FAN speed se...

Page 650: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 2 Page 7 10 21 Figure 7 10 3 2 2 GAS controls PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 651: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 2 Page 7 10 22 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 652: ...es are maximum pressure 1850 PSIG 127 bars at 70 F 21 C Evolution of this pressure according to the outside temperature is given in section 8 figure 8 7 4 as well as on a placard on the inside of the...

Page 653: ...ing Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 11 2 Figure 7 11 1 Emergency oxygen system 1 MICRO MASK switch 2 OXYGEN switch 3 PASSENGER OXYGEN switch PIM DO NOT USE FOR FLIG...

Page 654: ...front seats Permanently connected to the oxygen system they are equipped with a micro controlled by the MICRO MASK switch under cover located on the instrument panel near the pilot s control wheel Th...

Page 655: ...ach pilot at 10000 ft Number of occupants Outside temperature Cockpit Cabin 110 F 43 C 90 F 32 C 70 F 21 C 50 F 10 C 30 F 1 C 10 F 12 C 10 F 23 C 1 0 631 614 597 580 563 546 529 1 1 759 736 713 691 66...

Page 656: ...F 1 C 10 F 12 C 10 F 23 C 1 0 618 602 585 569 552 536 520 1 1 842 816 789 763 736 710 685 1 2 1067 1029 992 955 918 882 846 1 3 1513 1240 1192 1144 1097 1050 1004 1 4 1513 1452 1392 1333 1275 1217 116...

Page 657: ...0 F 1 C 10 F 12 C 10 F 23 C 1 0 618 602 585 569 552 536 520 1 1 961 929 896 864 833 801 770 1 2 961 929 896 864 833 801 770 1 3 961 929 896 864 833 801 770 1 4 961 929 896 864 833 801 770 2 0 992 958...

Page 658: ...ped with a system that detects when a communication is made operating one of the push to talk buttons It activates a noise reduction system that attenuates the oxygen flow noise in the headsets Noise...

Page 659: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 11 8 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 660: ...plying the standby attitude module and air data computers Static pressure systems Primary systems Two dual static ports one on either side of the fuselage tail part supply a dual system routed towards...

Page 661: ...the standby attitude module and one ADC The second one supplies the other ADC Both lines incorporate a drain plug located in the root of L H and R H wings Pitot heating Pitot heating is controlled by...

Page 662: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 12 3 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 663: ...Standby Instrument 4 ADC 5 ADC 6 FWD pressure bulkhead 7 Static system drain 8 Static system drain 9 Static system drain 10 Emergency static system drain 11 Emergency static valve Normal alternate 12...

Page 664: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 12 5 Figure 7 12 1 2 2 Air data system PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 665: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 12 6 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 666: ...tch installed in the system indicates the failure by causing VACUUM LOW to light on Standby attitude module MD302 The Mid Continent Instrument and Avionics MD302 Standby Attitude Module consists of tw...

Page 667: ...7 Description Edition 0 March 05 2019 Rev 1 Page 7 13 2 Figure 7 13 1 1 2 Vacuum system 1 Pressure regulator 2 Ejector 3 Valve 4 Regulating and relief valve 5 Pressure switch 6 Failure CAS message PI...

Page 668: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 13 3 Figure 7 13 1 2 2 Vacuum system PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 669: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 1 Page 7 13 4 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 670: ...ne air inlet deice systems INERT SEP Deicing check and control panel is located on the lower L H side of the instrument panel Ice Detection System CAUTION Ice Detection System is only an advisory syst...

Page 671: ...by pressing the DE ICE SYSTEM mode switch When MAN mode is selected all deicing systems turn on see figure 7 14 3 In MAN mode all the ice protection systems can be activated deactivatedindividually Fi...

Page 672: ...atically cycles when AIRFRAME DE ICE system is activated either manually or automatically The 67 second cycle breaks down in two inflation cycles a first cycle induces inflation of leading edges deice...

Page 673: ...cycle is 180 seconds long The cycles continue as long as the system is activated The table hereafter gives the CAS messages and the status light colors corresponding to the state of the system System...

Page 674: ...ches 45 C 113 F the controllers cut the electrical supply to the heating resistors and resume supply when the temperature falls below 30 C 86 F The cycle continues as long as the system is activated I...

Page 675: ...en during flight into non icing conditions The system condition messages PITOT NO HT L or PITOT NO HT R PITOT HT ON L or PITOT HT ON R STALL HEAT ON or STALL NO HEAT are displayed on the MFD CAS windo...

Page 676: ...than 5 knots above the stall in all configurations Simultaneously the control wheel vibrates through the stick shaker The stall warning system should be checked during the preflight inspection by mom...

Page 677: ...but it is possible to encounter severe precipitation static conditions which might cause the loss of radio signals even with static dischargers installed Whenever possible avoid known severe precipita...

Page 678: ...ather information can be displayed on PFD1 PFD2 and MFD Refer to section 2 Limitations of this POH and to GARMIN Pilot s Guide for further details The controls for the weather radar are located on the...

Page 679: ...n 0 March 05 2019 Rev 2 Page 7 15 4 Figure 7 15 1 1 2 Weather radar display and controls 1 MFD 2 Radar mode 3 Area of weather display 4 Antenna stabilization status 5 Touchscreen controllers 6 Scale f...

Page 680: ...Pilot s Operating Handbook Section 7 Description Edition 0 March 05 2019 Rev 2 Page 7 15 5 Figure 7 15 1 2 2 Weather radar display and controls PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 681: ...rom the locator transmitter by setting its ARM OFF control switch to ON automatically in case of shock when remote control switch is set to ARM OFF and locator transmitter switch is set to ARM OFF A r...

Page 682: ...e intended to be used after an accident or an incident The lightweight data recorder system includes a cockpit microphone located on instrument panel between the standby instrument and the autopilot c...

Page 683: ...data can be transmitted via transponder 1 or transponder 2 if installed If the transponder 1 2 detects any internal fault or failure with the ADS B OUT functionality the following CAS message XPDR1 A...

Page 684: ...mpartment and does not require a pilot input to operate The data collection and transmission system is powered from the BATT BUS and protected by the REC circuit breaker GARMIN Integrated Flight Deck...

Page 685: ...as long as a system is configured to support barometric VNAV for approach If SBAS integrity is available it will be used to provide vertical guidance During execution of a GPS approach with LNAV VNAV...

Page 686: ...d Baro VNAV systems Outside of this temperature range LNAV VNAV minimums shall not be used with uncompensated Baro VNAV systems The GARMIN Approach Baro VNAV system is automatically temperature compen...

Page 687: ...e published approach waypoint altitudes on the active flight plan page and the minimum altitude The minimum altitude selection type changes to BARO if it was previously set to TEMP COMP Temperature co...

Page 688: ...If SBAS becomes unavailable on an RNAV LPV approach LPV will be shown in yellow but the CDI and VDI will continue to be shown At one minute to the FAF an APR DWNGRADE will be generated The VDI will b...

Page 689: ...plan or copied to a stored flight plan in the course of saving the active or standby flight plan CDI and VDI indications are equivalent to those of other GPS based approaches e g LPV or L VNAV The GI...

Page 690: ...cy Autoland function that isdescribed inthe GARMIN Pilot s Guide HomeSafe is an emergency autopilot function that is meant to be used in the case of pilot incapacitation i e in situations where the pi...

Page 691: ...of informational videos on the MFD related to the different phases of the HomeSafe function flight Set the transponder to the emergency code 7700 Communicate with Air Traffic Control Choose a destinat...

Page 692: ...ated and is able to fly the airplane he she must deactivate HomeSafe before taking control of the airplane HomeSafe can be stopped by any of the following actions Press twice the AP TRIM DISC push but...

Page 693: ...HomeSafe function is protected by the HOMESAFE breaker Optional equipment For optional equipment such as stormscope SVS or TAWS refer to section 9 Supplements Other optional equipment such as radio a...

Page 694: ...8 2 1 8 3 Publications 8 3 1 8 4 Inspection periods 8 4 1 8 5 Alterations or repairs 8 5 1 8 6 Ground handling 8 6 1 Towing 8 6 1 Parking 8 6 1 Tie down 8 6 2 Jacking 8 6 4 Leveling 8 6 4 Flyable sto...

Page 695: ...cleaning and care 8 8 1 Windshield and windows 8 8 1 Painted surfaces 8 8 1 Propeller care 8 8 2 Engine care 8 8 2 Interior care 8 8 2 8 9 Preparation of the airplane equipment and furnishings 8 9 1 8...

Page 696: ...of airplane Also included in this section arethe inspection and maintenance requirements which must befollowed if your airplane is to retain its performance and dependability It is recommendedthata p...

Page 697: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 1 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 698: ...ate Any correspondence regarding your airplane should include its serial number This number together with the model number type certificate number and production certificate number are stamped on the...

Page 699: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 2 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 700: ...RMIN Integrated Flight Deck Pilot s Guide and supplemental data covering optional equipment installed in the airplane refer to section 9 Supplements and pilot guides In addition the owner may get acce...

Page 701: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 3 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 702: ...regulations in force in the certification country for information concerning preventive maintenance to be carried out A maintenance manual must be obtained prior to performing any preventive maintena...

Page 703: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 4 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 704: ...1 8 5 Alterations or repairs It is essential that the airworthiness authorities be contacted prior to any alterations or repairs on the airplane to make sure that airworthiness of the airplane is not...

Page 705: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 5 2 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 706: ...ee figure 8 6 1 Parking When parking the airplane head it into the wind Do not set the parking brake when brakes are overheated or during cold weather when accumulated moisture may freeze the brakes C...

Page 707: ...tie the airplane down as outlined in the following paragraph Tie down Proper tie down procedure is the best protection against damage to the airplane by gusty or strong winds To tiedown the airplane s...

Page 708: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 6 3 Figure 8 6 1 Turning angle limits PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 709: ...ling Keep fuel tanks full to minimize condensation in the tanks Keep the battery fully charged to prevent the electrolyte from freezing in cold weather Close oxygen cylinder isolation valve Storage fr...

Page 710: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 6 5 Figure 8 6 2 Control lock device PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 711: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 6 6 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 712: ...scosities or specifications of oil as their different chemical structure can make them incompatible Specification Nominal Viscosity Specification NATO Code 5cSt MIL PRF 23699G O 156 STD O 154 HTS Figu...

Page 713: ...may result in high consumption rate with the oil exiting through the accessory gearbox breather CAUTION When filler cap assembly is installed and locked no movement is allowed Fuel Total capacity eac...

Page 714: ...only AVGAS will not be used for more than 150 cumulative hours during any period between engine overhaul NOTE Use of AVGAS must be recorded in engine module logbook US Specification US French Specifi...

Page 715: ...d operators they do exist in certain areas of the world and consequently must be dealt with when encountered Therefore to alleviate the possibility of fuel icing occurring under these unusual conditio...

Page 716: ...using a differential refractometer It is imperative that the technical manual for the differential refractometer be followed explicitly when checking the additive concentration Fuel and fuel additives...

Page 717: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 7 6 Figure 8 7 3 Additive mixing ratio EGME or DIEGME PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 718: ...ck absorbers Fill with hydraulic fluid AIR 3520 B MIL H5606E inflate with nitrogen to 160 psi 11 bars Hydraulic system Check every 100 hours and service with AIR 3520 B MIL H5606E hydraulic fluid Brak...

Page 719: ...der is installed directly on the cylinder head It consists of a charging valve and of a pressure gage graduated from 0 to 2000 PSIG A chart see figure 8 7 4 located on the inside of the cylinder servi...

Page 720: ...Use no oil or grease with the oxygen replenishment equipment Always open shut off valve slowly to avoid generating heat and replenish the system slowly at a rate not exceeding 200 PSIG 13 7 bars per...

Page 721: ...ect it to the charging valve 7 Slowly pressurize the oxygen cylinder to the correct pressure 8 Close the oxygen supply and let the cylinder temperature become stable 9 Monitor the oxygen pressure on t...

Page 722: ...masks to deploy WARNING Masks shall be repacked in an area free of oil grease flammable solvents or other contaminants 1 Inspect and disinfect mask and deployment container with an aqueous solution o...

Page 723: ...2019 Rev 0 Page 8 7 12 4 Gently fold reservoir bag lengthwise into thirds outside edges folded inward over center of bag Do not crease bag 5 Fold reservoir bag away from breathing valves and into fac...

Page 724: ...into correct check valve for mask being installed Cross connected pins will result in passengers pulling lanyard cords only to initiate oxygen flow to another mask 8 Insert lanyard pin into correspond...

Page 725: ...down the crash lever 2 Pull the BATT BUS breaker located in the front cargo compartment 3 Remove the cap 1 4 Connect the BatteryMINDer charger connector plug 5 to the airplane connector 2 5 Connect t...

Page 726: ...Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 7 15 Figure 8 7 5 2 2 Removal Installation of BatteryMINDer charger PIM DO NOT USE FOR FLIGHT OPER...

Page 727: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 7 16 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 728: ...aning operation avoid wearing objects such as ring watch bracelet and exercise care to prevent buttons buckles and any hard objects from touching the windshield and the windows Adhesive tapes other th...

Page 729: ...ass and bug stains will assure long blade life Never use an alkaline cleaner on the blades remove grease and dirt Refer to maintenance manual for the procedures to follow Engine care Refer to maintena...

Page 730: ...accommodation and conversely However it can be used partly to remove or install an equipment item However the pilot must ensure that he gets all necessary authorizations from his regulatory authority...

Page 731: ...moving in rails f Open the floor hatch and clip the second loose connector to the holder located under floor panel Close the floor hatch g Hold the seat in tilted position and unscrew quick links 7 of...

Page 732: ...the seat in the rails to line up pads 23 with rail 24 apertures h Remove the seat i Install backrest bottom upholstery 25 CAUTION In order to prevent deflectors damage it is necessary to remove them 2...

Page 733: ...NOTE Position deflectors 34 as indicated on label according to future position of intermediate seat in order to optimize cabin cooling 2 Install intermediate seats NOTE If seats are installed facing...

Page 734: ...E Slide properly the carpet under doorstep 2 If necessary remove the baggage compartment partition net and install the small or large cargo net refer to section 7 3 Make sure the work area is clean an...

Page 735: ...g device and plug arrangements will need to be reconfigured in order to optimize the temperature conditioning system Subject changes should preferably be performed at a recognized service center D Ins...

Page 736: ...rest and lock it using backrest tilting handle 6 12 Slide properly the carpet under the seat 13 Remove protective covers G Reconditioning 1 Make sure the work area is clean and free from debris 2 Dete...

Page 737: ...Action Description operation Rear seat Removal Paragraph 1 C Installation Paragraph 2 F Intermediate seat Removal Paragraph 1 D Installation Paragraph 1 G Cargo net Installation Section 7 Table 1 1 S...

Page 738: ...Pilot s Operating Handbook Section 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 9 9 Figure 8 9 1 2 2 Removal installation of rear seat PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 739: ...ing and maintenance Edition 0 March 05 2019 Rev 2 Page 8 9 10 Figure 8 9 2 Removal installation of intermediate seat 21 Locking handle 22 Lock 23 Pad 24 Rail 25 Backrest bottom upholstery 26 Seats hea...

Page 740: ...ervicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 9 11 Figure 8 9 3 Cabin comfort Installation of blanking plugs and deflector 31 Blanking plug 32 Blanking plug 33 Blanking device assy 34...

Page 741: ...tion 8 Handling servicing and maintenance Edition 0 March 05 2019 Rev 0 Page 8 9 12 Figure 8 9 4 Cabin comfort Installation of deflector 34 Deflector 35 Deflector hole 36 Red mark 37 Color mark PIM DO...

Page 742: ...ngine cowlings seals as well as the leading edge deicers 2 Apply engine oil on the engine cowling latches 3 Inflate main landing gear shock absorbers to 247 psi 17 bars at a room temperature of 15 C 4...

Page 743: ...table 1 during operation in cold weather only OAT C 40 30 20 10 15 P r e s s u r e s psi bars Main landing gear shock absorber 189 13 196 13 5 203 14 218 15 247 17 Nose gear shock absorber 102 7 109 7...

Page 744: ...9 6 1 SUPPLEMENT WX 500 stormscope Table of contents Page 1 General 9 6 2 2 Limitations 9 6 2 3 Emergency procedures 9 6 3 4 Normal procedures 9 6 3 5 Performance 9 6 3 6 Weight and balance 9 6 4 7 De...

Page 745: ...airplane is equipped with the option WX 500 stormscope The WX 500 stormscope systems signal displays are not intended for the purpose of penetrating thunderstorm areas or areas of severe turbulence su...

Page 746: ...cedures of the airplane described in section 3 Emergency procedures of the basic POH SECTION 4 Normal procedures Normal operating procedures of the WX 500 stormscope are outlined in the WX 500 Pilot s...

Page 747: ...cribed in section 7 Description of the basicPOH whenthe airplaneis equippedwith theoption WX 500 stormscope The WX 500 series II stormscope weather mapping system provides a visual screen readout of t...

Page 748: ...1 SUPPLEMENT Engine fire detection system Table of contents Page 1 General 9 18 2 2 Limitations 9 18 2 3 Emergency procedures 9 18 3 4 Normal procedures 9 18 5 5 Performance 9 18 5 6 Weight and balan...

Page 749: ...ne fire detection system The general hereafter supplement or replace those of thestandard airplanedescribed in section 1 General of the basic POH when the airplane is equipped with the option Engine f...

Page 750: ...ok when the airplane is equipped with the option Engine fire detection system Engine fire on ground Symptoms ITT increasing ITT FIRE smoke 1 THROTTLE CUT OFF Airplane with G1000 or G1000 NXi Flight de...

Page 751: ...warning is not confirmed 1 Monitor the engine parameters ITT in particular 2 Look for smoke coming from engine cowls or from air conditioning system Land as soon as possible If the fire warning is co...

Page 752: ...with the option Engine fire detection system Before starting the engine Up to S N 1105 plus S N 687 on left side of left instrument panel FIRE TEST push button Press From S N 1106 on upper panel TEST...

Page 753: ...ic Pilot s Operating Handbook when the airplane is equipped with the option Engine fire detection system S R A O Item OPT70 or MOD70 Required R or Standard S or Optional A or O equipment Weight per un...

Page 754: ...ngine areas They consist of thermal switches detecting a temperature greater than 200 C Push button The push button enables the pilot to test the detection system by opening the grounding circuit It i...

Page 755: ...Pilot s Operating Handbook Supplement 18 Engine fire detection system Edition 3 December 31 2015 Rev 2 Page 9 18 8 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 756: ...cs Table of contents Page 1 General 9 45 2 2 Limitations 9 45 2 Internal placards 9 45 2 External placards 9 45 10 3 Emergency procedures 9 45 17 4 Normal procedures 9 45 17 5 Performance 9 45 17 6 We...

Page 757: ...uired by the relevant Certification Authorities limitations description and operations necessary to the operation of the TBM airplane SECTION 2 Limitations The limitations hereafter supplement or repl...

Page 758: ...2018 Rev 0 Page 9 45 3 For the small cargo net on R H side lower upholstery panel For the large cargo net on R H Side upholstery panel in the rear baggage compartment 2 Non pressurized FWD baggage com...

Page 759: ...45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 4 3 On rear passengers masks containers 4 On internal face of rear passengers masks containers doors 5 On rear passenger s table casing...

Page 760: ...ng Handbook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 5 6 Door internal side On access door On pilot door if installed 7 On emergency exit handle PIM DO NOT USE FOR FLI...

Page 761: ...ook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 6 8 Above emergency exit door 9 On landing gear emergency control access door 10 On cabinet drawer optional PIM DO NOT USE...

Page 762: ...0 Page 9 45 7 Airplane equipped with coat hanger Post MOD70 0557 25B 11 On the upper edge of the L H Passenger access door panel Airplane equipped with lavatory compartment Post MOD70 0505 25 12 On f...

Page 763: ...Handbook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 8 14 On access door cabin side and toilet side 15 Behind access door cabin side and toilet side PIM DO NOT USE FOR F...

Page 764: ...g Handbook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 9 16 Front face of lavatory compartment near opening closing switches 17 On the magazine rack PIM DO NOT USE FOR FL...

Page 765: ...ng Handbook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 10 All External placards 18 Under engine cowling and under each wing 19 Near fuel tank caps PIM DO NOT USE FOR FLI...

Page 766: ...5 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 11 20 Above brakes hydraulic fluid reservoir against firewall 21 On langing gear hydraulic fluid reservoir 22 On fuse box in engine cowlin...

Page 767: ...ng Handbook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 12 23 On internal face of L H engine cowling 24 On front lower portion of firewall L H side PIM DO NOT USE FOR FLI...

Page 768: ...g Handbook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 13 25 On engine cowling in front of compartment door 26 On nose gear door 27 On nose gear leg PIM DO NOT USE FOR FL...

Page 769: ...ook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 14 28 On main gear leg 29 On internal face of the oxygen cylinder service door 30 On the oxygen service door PIM DO NOT US...

Page 770: ...45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 15 31 Near air data system port 32 On external side of emergency locator transmitter inspection door 33 On emergency exit external side...

Page 771: ...45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 16 34 Door external side On pilot door On access door On outer fuselage skin aft of access door and in the cabin forward of access door...

Page 772: ...No specifics SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH S R A O Item...

Page 773: ...Handbook Supplement 45 Mexico specifics Edition 3 December 20 2018 Rev 0 Page 9 45 18 SECTION 7 Description No specifics SECTION 8 Handling servicing and maintenance No specifics PIM DO NOT USE FOR F...

Page 774: ...1 SUPPLEMENT GARMIN TAWS system Table of contents Page 1 General 9 49 2 2 Limitations 9 49 2 3 Emergency procedures 9 49 3 4 Normal procedures 9 49 4 5 Performance 9 49 6 6 Weight and balance 9 49 6...

Page 775: ...zontal navigation AC 2318 recommendation in order to avoid unwillingly warnings TAWS function must be inhibited for any landing on a terrain which is not mentioned in the data base The use of the terr...

Page 776: ...y procedures The emergency procedures hereafter supplement or replace those of the standard airplane described in section 3 Emergency procedures of the basic POH when the airplane is equipped with the...

Page 777: ...Heard End of procedure 4 1 Warnings of the TAWS function PULL UP voice alert PULL UP PFD MFD alert annunciation and PULL UP MFD pop up alert light ON 1 Level the wings 2 TRQ Maximum 3 Choose the opti...

Page 778: ...CLE or TOO LOW TERRAIN MFD pop up alerts light ON 1 Adjust airplane path in order to make the warning disappear End of procedure Don t sink voice alert TERRAIN PFD MFD alert annunciation and DON T SIN...

Page 779: ...e of the basic POH SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH when th...

Page 780: ...Controller Voice alerts inhibiting TAWS Alerts can be inhibited by the pilot selecting Inhibit TAWS on Touchscreens Controllers Discretion should be used when inhibiting alerts and the system should b...

Page 781: ...s annunciated when the projected vertical flight path is calculated to come within minimum clearance altitudes in table 9 49 1 Phase of flight Minimum Clearance Altitude Level Flight ft Minimum Cleara...

Page 782: ...p Reduced Required Obstacle Clearance Warning ROC Red PULL UP OBSTACLE PULL UP Obstacle Obstacle Pull up Pull up Imminent Obstacle Impact Warning IOI Red PULL UP OBSTACLE AHEAD PULL UP Obstacle Ahead...

Page 783: ...he destination airport PDA alerting ends when the airplane is either 0 5 Nm from the runway threshold or at an altitude of 125 feet AGL while within 1 0 Nm of the threshold Figure 9 49 1 PDA alerting...

Page 784: ...e purpose of the Excessive Descent Rate EDR alert is to provide suitable notification when the airplane is determined to be closing descending upon terrain at an excessive speed Figure 9 49 2 shows th...

Page 785: ...ve Climb Rate NCR After Takeoff alert also referred to as Altitude Loss After Takeoff is to provide suitable alerts to the pilot when the system determines that the airplane is loosing altitude closin...

Page 786: ...ustrate the NCR alerting parameters as defined by TSO C151b The NCR alert is issued when the altitude loss and height are within the range in the first figure or when the sink rate negative vertical s...

Page 787: ...avigation solution along with specific vertical accuracy minimums Should the navigation solution become degraded or if the airplane is out of the database coverage area the annunciation TAWS N A is ge...

Page 788: ...1 SUPPLEMENT GARMIN Synthetic Vision System Table of contents Page 1 General 9 50 2 2 Limitations 9 50 2 3 Emergency procedures 9 50 3 4 Normal procedures 9 50 4 5 Performance 9 50 5 6 Weight and bal...

Page 789: ...basic POH when the TBM airplane is equipped with the option GARMIN Synthetic Vision System The following document or any further edition applicable to the latter shall be readily available to the pilo...

Page 790: ...orth 75 latitude to South 60 latitude in all longitudes SECTION 3 Emergency procedures The emergency procedures hereafter supplement or replace those of the standard airplane described in Section 3 Em...

Page 791: ...ereafter supplement or replace those of the standard airplane described in section 4 Normal procedures of the basic POH when the TBM airplane is equipped with the option GARMIN Synthetic Vision System...

Page 792: ...ne is equipped with the option GARMIN Synthetic Vision System S R A O Item OPT70 or MOD70 Required R or Standard S or Optional A or O equipment Weight per unit lb kg Arm in m 34 Navigation A 0226 00 S...

Page 793: ...9 50 6 SECTION 8 Handling servicing and maintenance Installation and operation of GARMIN Synthetic Vision System do not change the basic handling servicing and maintenance procedures of the airplane d...

Page 794: ...1 SUPPLEMENT GARMIN GSR 56 weather datalink and satellite phone Table of contents Page 1 General 9 56 2 2 Limitations 9 56 2 3 Emergency procedures 9 56 4 4 Normal procedures 9 56 4 5 Performance 9 5...

Page 795: ...Deck Pilot s Guide mentioned in section 2 Limitations of the basic POH G1000 or G3000 as standard or of the POH supplement G1000 NXi retrofit as applicable or any further applicable edition shall be...

Page 796: ...to comply with the applicable operational regulation in terms of flight preparation especially with regard to the use of an approved weather and NOTAM sources during flight planning International tel...

Page 797: ...d in section 3 Emergency procedures of the basic POH SECTION 4 Normal procedures The normal procedures hereafter supplement or replace those of the standard airplane described in section 4 Normal Proc...

Page 798: ...OFF If rear passengers intend to take part in a phone call 2 CABIN button or PASS ICS button OFF 2 types of wording may exist for the same button If front passenger intends to take part in a phone cal...

Page 799: ...assengers intend to take part into a phone call In one of the GTC s NAV COM Intercom Page 2 Pilot Passenger Link Arrow OFF If front passenger intends to take part into a phone call In one of the GTC s...

Page 800: ...sic POH SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH when the airplane...

Page 801: ...be received and sent through the dedicated pages on the MFD The controls for the MFD are located on both the MFD bezel and the MFD control unit The telephone audio including the incoming callringing i...

Page 802: ...9 56 9 SECTION 8 Handling servicing and maintenance Installation and operation of GARMIN GSR 56 weather datalink and satellite phone do not change the basic handling servicing and maintenance procedur...

Page 803: ...Pilot s Operating Handbook Supplement 56 GARMIN GSR 56 weather datalink and satellite phone Edition 3 December 31 2015 Rev 3 Page 9 56 10 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 804: ...SUPPLEMENT Brazil specifics Table of contents Page 1 General 9 59 2 2 Limitations 9 59 2 3 Emergency procedures 9 59 14 4 Normal procedures 9 59 14 5 Performance 9 59 14 6 Weight and balance 9 59 15 7...

Page 805: ...ies limitations description and operations necessary to the operation of the TBM airplane SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane described...

Page 806: ...ith Brazilian IS 21 013A use of GNSS GPS is prohibited under IFR unless other means of navigation suitable and approved for the intended route are installed and operational It must be possible atany p...

Page 807: ...dition 3 February 15 2019 Rev 0 Page 9 59 4 For the small cargo net on frame C13bis For the large cargo net on R H side upholstery panel in the rear baggage compartment On FWD baggage compartment door...

Page 808: ...ook Supplement 59 Brazil specifics Edition 3 February 15 2019 Rev 0 Page 9 59 5 Near fuel tank caps On internal face of L H engine cowling CAPACIDAD E DE LEO 12 L Above passenger s table PIM DO NOT US...

Page 809: ...ruary 15 2019 Rev 0 Page 9 59 6 On nose gear door On engine cowling in front of compartment door TOMADA EXTERNA 28 VOLTS D C NOMINAL 800 AMPS CAPACIDADE M NIMA PARA PARTIDA N O EXCEDA 1000 AMPS On pil...

Page 810: ...ook Supplement 59 Brazil specifics Edition 3 February 15 2019 Rev 0 Page 9 59 7 On access door External side On outer fuselage skin aft of access door In the cabin forward of access door PIM DO NOT US...

Page 811: ...ics Edition 3 February 15 2019 Rev 1 Page 9 59 8 On access door Internal side Airplane equipped with MOD70 0619 11 version B Airplane equipped with MOD70 0619 11 version G All On pilot door Internal s...

Page 812: ...lement 59 Brazil specifics Edition 3 February 15 2019 Rev 1 Page 9 59 9 On emergency exit handle Marking on cover Marking on handle Above emergency exit door On rear passengers masks containers PIM DO...

Page 813: ...razil specifics Edition 3 February 15 2019 Rev 1 Page 9 59 10 On the oxygen service door Airplanes equipped with Lavatory compartment Post MOD70 0505 25 On fixed panel cabin side On fixed panel toilet...

Page 814: ...book Supplement 59 Brazil specifics Edition 3 February 15 2019 Rev 1 Page 9 59 11 On access door cabin side and toilet side Behind access door cabin side Behind access door toilet side PIM DO NOT USE...

Page 815: ...Rev 1 Page 9 59 12 Front face of lavatory compartment near opening closing switches On the magazine rack and on side wall of storage volume Airplane equipped with coat hanger Post MOD70 0641 25A On t...

Page 816: ...Page 9 59 13 Airplane equipped with coat and headset hanger Post MOD70 0783 25B On each coat and headset hanger Airplane equipped with extended large storage cabinet Post MOD70 0684 25 On the upper su...

Page 817: ...cifics Edition 3 February 15 2019 Rev 1 Page 9 59 14 Inside small internal drawer on side wall SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics SECTION 5 Performanc...

Page 818: ...e standard airplane described in section 6 Weight and balance of the basic POH S R A O Item OPT70 or MOD70 Required R or Standard S or Optional A or O equipment Weight per unit lb kg Arm in m 01 Speci...

Page 819: ...Pilot s Operating Handbook Supplement 59 Brazil specifics Edition 3 February 15 2019 Rev 1 Page 9 59 16 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 820: ...1 SUPPLEMENT Lavatory compartment Table of contents Page 1 General 9 63 2 2 Limitations 9 63 2 3 Emergency Procedures 9 63 7 4 Normal Procedures 9 63 8 5 Performance 9 63 8 6 Weight and Balance 9 63 8...

Page 821: ...llowing the installation of the lavatory compartment option SECTION 2 Limitations The information in this section supplements and or replaces the information in section 2 Limitations of the standard P...

Page 822: ...pplement 63 Lavatory compartment Edition 1 November 16 2016 Rev 2 Page 9 63 3 On fixed panel toilet side On access door cabin side and toilet side Behind access door cabin side and toilet side PIM DO...

Page 823: ...upplement 63 Lavatory compartment Edition 1 November 16 2016 Rev 2 Page 9 63 4 Inner face of toilet cover Front face of lavatory compartment near opening closing switches On the magazine rack PIM DO N...

Page 824: ...ment 63 Lavatory compartment Edition 1 November 16 2016 Rev 3 Page 9 63 5 From S N 1270 2 9 Placards On fixed panel cabin side On fixed panel toilet side On access door cabin side and toilet side PIM...

Page 825: ...Lavatory compartment Edition 1 November 16 2016 Rev 3 Page 9 63 6 Behind access door cabin side and toilet side Inner face of toilet cover Front face of lavatory compartment near opening closing switc...

Page 826: ...ion and air conditioning Pre v15 GARMIN software update Pre MOD70 0407 00 CABIN ALTITUDE Inform passengers to use emergency stowing of the divider and oxygen mask Post v15 GARMIN software update Post...

Page 827: ...deployed to allow communication with the crew in case of emergency SECTION 5 Performance The installation of the Lavatory compartment system does not change the performance of the airplane described...

Page 828: ...ued after the lavatory compartment option is installed which gives the new empty weight arm and CG for the weight and balance form Refer to POH section 6 4 using the weight and balance form procedure...

Page 829: ...toilet Electrically deployable separating panels divider Two 2 actuating switches DEPLOY STOW Two 2 emergency stowing buttons PUSH TO STOW accessible from inside or outside the lavatory compartment On...

Page 830: ...sible when the lavatory compartment structure is unscrewed from the floor and moved slightly aside to access the plug The circuit breaker for the power plug is only accessible when the lavatory compar...

Page 831: ...Pilot s Operating Handbook Supplement 63 Lavatory compartment Edition 1 November 16 2016 Rev 4 Page 9 63 12 Figure 9 63 3 1 2 Lavatory compartment PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 832: ...Pilot s Operating Handbook Supplement 63 Lavatory compartment Edition 1 November 16 2016 Rev 4 Page 9 63 13 Figure 9 63 3 2 2 Lavatory compartment PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 833: ...Page 9 63 14 SECTION 8 Handling Servicing and Maintenance The installation of the Lavatory compartment system does not change the handling servicing and maintenance of the airplane described in sectio...

Page 834: ...rplane Table of contents Page 1 General 9 71 2 2 Limitations 9 71 4 3 Emergency procedures 9 71 13 4 Normal procedures 9 71 13 5 Performance 9 71 14 6 Weight and balance 9 71 17 7 Description 9 71 17...

Page 835: ...lied except for matters revised or supplemented by this Supplement Model Basic Pilot s Operating Handbook TBM940 From S N 1272 Doc No DMKFM00EEN Table 1 Applicable coverage TC Holder DAHER AEROSPACE 2...

Page 836: ...DMKFM00EEN for details Weight and Center of Gravity Maximum certified weight and center of gravity range Refer to the JCAB TCDS No 99 and Pilot s Operating Handbook for TBM940 airplane Doc No DMKFM00...

Page 837: ...nt or replace those of the standard airplane described in section 2 Limitations of the basic POH General The limitations are the same as those in the basic EASA Approved Pilot s Operating Handbook exc...

Page 838: ...940 airplane Edition 0 June 26 2019 Rev 0 Page 9 71 5 1 b For the large cargo net on R H side upholstery panel in the rear baggage compartment 1 c On FWD baggage compartment door frame non pressurized...

Page 839: ...ing Handbook Supplement 71 JCAB Supplement for TBM940 airplane Edition 0 June 26 2019 Rev 0 Page 9 71 6 3 On pilot door External side if installed 4 On access door External side PIM DO NOT USE FOR FLI...

Page 840: ...ent 71 JCAB Supplement for TBM940 airplane Edition 0 June 26 2019 Rev 0 Page 9 71 7 5 On outer fuselage skin aft of access door 6 In the cabin forward of access door 7 On access door Internal side PIM...

Page 841: ...B Supplement for TBM940 airplane Edition 0 June 26 2019 Rev 0 Page 9 71 8 8 On pilot door Internal side if installed 9 On emergency exit handle Marking on cover Marking on handle 10 Above emergency ex...

Page 842: ...the L H Rear cargo compartment panel upper edge Occupants limits Maximum Occupancy The number of persons on board is limited by approved seating configuration installed but must not exceed six includi...

Page 843: ...me specified in Article 66 of the Regulations under visual meteorological condition Visual flight other than flight under instrumental navigation Night operations Day operations Flight under icing met...

Page 844: ...Standards using GPS for the Instrumental Flight Method The installed GPS complies with the equipment requirements described in the JCAB Circular No 5 005 Operational lmplementation Standards using GPS...

Page 845: ...ith 14 CFR 91 225 and 91 227 CS ACNS D ADSB 1090 MHz Extended Squitter ADS B Out and CS ACNS D ELS EHS Mode S Elementary Enhanced Surveillance The standard GTX 345R is compliant with TSO C112e The opt...

Page 846: ...ndbook Supplement 71 JCAB Supplement for TBM940 airplane Edition 0 June 26 2019 Rev 0 Page 9 71 13 SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics PIM DO NOT USE F...

Page 847: ...s Operating Handbook ln Japan Compliance to the Noise Requirement is certified as a part of Airworthiness Certification Noise Certificate is not issued and Noise Characteristics are described in Pilo...

Page 848: ...A 66D HARTZELL HC E5N 3C NC8834K 9 Maximum takeoff mass 10 Maximum landing mass 11 Noise certification standard 3354 kg 7394 lbs 3186 kg 7024 lbs Chapter 10 12 Additional modifications incorporated fo...

Page 849: ...aircraft complies with the requirements of Civil Aeronautics Regulations Annex 3 Chapter 1 NOTE The fuel venting has been demonstrated under the ICAO Annex 16 Volume Il Third Edition Part Il Chapter...

Page 850: ...those of the standard airplane described in section 6 Weight and balance of the basic POH S R A O Item OPT70 or MOD70 Required R or Standard S or Optional A or O equipment Weight per unit lb kg Arm in...

Page 851: ...FM00EEN Pilot s Operating Handbook Basic Feb 18 2020 Edit 0 Rev 2 Nov 30 2020 DMJFM06EEN POH Supplement 6 WX 500 stormscope Feb 26 2018 Edit 3 Rev 2 Aug 08 2019 DMJFM18EEN POH Supplement 18 Engine fir...

Page 852: ...imeter 1 Note 2 Note 8 Rate of climb indicator 1 Airspeed indicator with anti icing device 1 Note 2 Ambient air temperature indicator 1 Clock with second indication 1 Airborne DME 1 Note 4 Direction f...

Page 853: ...n flight is conducted at altitude beyond 4 000 meters necessary oxygen quantity shall be as much as for all occupants to use for flight time related to the said flight 2 Aircraft with cabin pressuriza...

Page 854: ...to receive radio signals all through the flight from NDB VOR or TACAN stations However direction finder can be substituted with GNSS receiver Note 7 Aircraft of which maximum takeoff weight is equal a...

Page 855: ...perating Handbook Supplement 71 JCAB Supplement for TBM940 airplane Edition 0 June 26 2019 Rev 0 Page 9 71 22 APPENDIX C Table of TCD insertion Status Template Figure 1 1 1 PIM DO NOT USE FOR FLIGHT O...

Page 856: ...ating Handbook Supplement 71 JCAB Supplement for TBM940 airplane Edition 0 June 26 2019 Rev 0 Page 9 71 23 APPENDIX D Table of Supplemental Pilot s Operating Handbook Template PIM DO NOT USE FOR FLIGH...

Page 857: ...Pilot s Operating Handbook Supplement 71 JCAB Supplement for TBM940 airplane Edition 0 June 26 2019 Rev 0 Page 9 71 24 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 858: ...1 SUPPLEMENT France specifics Table of contents Page 1 General 9 72 2 2 Limitations 9 72 2 3 Emergency procedures 9 72 6 4 Normal procedures 9 72 6 5 Performance 9 72 6 6 Weight and balance 9 72 7 7...

Page 859: ...hers those required by the relevant Certification Authorities limitations description and operations necessary to the operation of the French registered TBM airplane SECTION 2 Limitations The limitati...

Page 860: ...specifics Edition 0 December 04 2019 Rev 1 Page 9 72 3 2 On access door Internal side Airplane equipped with MOD70 0619 11E Airplane equipped with MOD70 0619 11H All 3 On pilot door Internal side if...

Page 861: ...ng Handbook Supplement 72 France specifics Edition 0 December 04 2019 Rev 1 Page 9 72 4 4 On emergency exit handle Marking on cover Marking on handle 5 Above emergency exit door PIM DO NOT USE FOR FLI...

Page 862: ...ber 04 2019 Rev 1 Page 9 72 5 6 On rear passengers masks containers 7 On internal face of rear passengers masks containers doors Airplane equipped with lavatory compartment Post MOD70 0505 25 8 On acc...

Page 863: ...ics Edition 0 December 04 2019 Rev 1 Page 9 72 6 9 Behind access door cabin side and toilet side SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics SECTION 5 Performa...

Page 864: ...e standard airplane described in section 6 Weight and balance of the basic POH S R A O Item OPT70 or MOD70 Required R or Standard S or Optional A or O equipment Weight per unit lb kg Arm in m 01 Speci...

Page 865: ...Pilot s Operating Handbook Supplement 72 France specifics Edition 0 December 04 2019 Rev 0 Page 9 72 8 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 866: ...1 SUPPLEMENT Extended large storage cabinet Table of contents Page 1 General 9 73 2 2 Limitations 9 73 2 3 Emergency procedures 9 73 3 4 Normal procedures 9 73 3 5 Performance 9 73 4 6 Weight and bala...

Page 867: ...necessary for operation when the airplane is equipped with the Extended large storage cabinet option SECTION 2 Limitations The information in this section supplements and or replaces the information...

Page 868: ...procedures Installation and operation of the Extended large storage cabinet do not change the emergency procedures of the airplane described in section 3 Emergency procedures of the standard POH SECT...

Page 869: ...ndard POH when the airplaneis equippedwith the Extended large storage cabinet option 6 1 General WARNING It is the pilot s responsibility to ensure that the airplane is properly loaded and that the we...

Page 870: ...orm to determine the weight and balance of the airplane Refer to procedure Utilization of weight and balance graph in section 6 4 of the standard POH S R A O Item OPT70 or MOD70 Required R or Standard...

Page 871: ...weight kg Baggage FWD 50 kg 3 250 Front seats kg 4 534 Storage cabinet 30 kg 5 451 Inter seats 15 4 kg per seat removed 5 710 Pax Rear bench net 21 kg per seat removed 6 785 Pax Cargo 80 kg Baggage A...

Page 872: ...Pilot s Operating Handbook Supplement 73 Extended large storage cabinet Edition 0 February 14 2020 Rev 0 Page 9 73 7 Figure 9 73 1 Weight and balance diagram PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 873: ...pty weight lbs Baggage FWD 110 lbs 128 0 Front seats lbs 178 5 Storage cabinet 66 lbs 214 6 Inter seats 34 lbs per seat removed 224 8 Pax Rear bench net 46 2 lbs per seat removed 267 1 Pax Cargo 176 l...

Page 874: ...Pilot s Operating Handbook Supplement 73 Extended large storage cabinet Edition 0 February 14 2020 Rev 0 Page 9 73 9 Figure 9 73 2 Weight and balance diagram PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 875: ...pplements and or replaces the information in section 7 Description of the standard POH when the airplane is equipped with the Extended large storage cabinet option The Extended large storage cabinet i...

Page 876: ...of a large drawer One large drawer opens sideways into the aisle A small drawer is installed inside this large storage volume One large drawer opens rearward in front of the large door Figure 9 73 4 S...

Page 877: ...side the cabinet BUS 4 USB USB plug protection 115 VAC INVERTER 115 VAC inverter protection 115 VAC PLUG 115 VAC plug protection SECTION 8 Handling servicing and maintenance The information in this se...

Page 878: ...Supplement Garmin GDR66 CPDLC Table of contents Page 1 General 9 75 2 2 Limitations 9 75 3 3 Emergency procedures 9 75 4 4 Normal procedures 9 75 4 5 Performance 9 75 4 6 Weight and balance 9 75 5 7...

Page 879: ...on 1 General of the standard POH when the airplane is equipped with the GDR66 transceiver 1 1 General The datalink system formed by the addition of the GDR66 transceiver in the Garmin avionics is comp...

Page 880: ...l Radio navigation abbreviations CPDLC Controller Pilot Data Link Communications VDL VHF Data Link Section 2 Limitations The information in this section supplements and or replaces the information in...

Page 881: ...sceiver is inoperative or the data link is lost 1 Resume voice communication Select COM 1 or COM 2 2 Inform Air Traffic Control of the loss of CPDLC Section 4 Normal procedures Installation and operat...

Page 882: ...uipment Weight per unit lb kg Arm in m 23 Communications A 0722 23A or G Garmin GDR66 installation and CPDLC furnction of which GDR66 transceiver 4 87 2 21 201 1 5 108 VDL antenna 0 88 0 40 148 9 3 78...

Page 883: ...h G3000 Flight deck a COM3 channel in the 118 000 to 137 000 MHz VHF aviation communications band All CPDLC communications The CPDLC function allows efficient communications with Air Traffic Control w...

Page 884: ...t deck VHF COM3 communications NOTE COM1 and COM2 remain the primary means of communications The pilot can operate COM3 communications through the GTC It will be available as GDR audio channel Refer t...

Page 885: ...ing Handbook Supplement 75 Garmin GDR66 CPDLC Edition 0 March 15 2021 Rev 2 Page 9 75 8 Airplane with G3000 Flight deck Figure 9 75 2 Partial electrical distribution of BUS bars PIM DO NOT USE FOR FLI...

Page 886: ...ing Handbook Supplement 75 Garmin GDR66 CPDLC Edition 0 March 15 2021 Rev 2 Page 9 75 9 Airplane with G1000 Flight deck Figure 9 75 3 Partial electrical distribution of BUS bars PIM DO NOT USE FOR FLI...

Page 887: ...9 75 10 All Section 8 Handling servicing and maintenance Installation and operation of the GDR66 transceiver do not change the handling servicing and maintenance of the airplane described in section...

Page 888: ...1 Supplement Buckle positioner Table of contents Page 1 General 9 76 2 2 Limitations 9 76 2 3 Emergency procedures 9 76 2 4 Normal procedures 9 76 3 5 Performance 9 76 3 6 Weight and balance 9 76 4 7...

Page 889: ...or replaces the information in Section 2 Limitations of the standard POH when the airplane is equipped with the buckle positioner WARNING The buckle positioner does not serve as a fifth attach point...

Page 890: ...ion Ensure correct positioning of front seat occupiers safety belt buckles by using the buckle positioners NOTE Check for the correct locking of belt buckles for the pilot and passengers as well as au...

Page 891: ...25 Buckle positioner 0 11 0 05 170 6 4 334 Section 7 Description The information in this section supplements and or replaces the information in Section 7 Description of the standard POH when the airpl...

Page 892: ...21 Rev 0 Page 9 76 5 Figure 9 76 1 Correct pre positioning of the buckle WARNING The central buckle must be positioned so that the belt straps remain at hip level just below the center of gravity to p...

Page 893: ...Operating Handbook Supplement 76 Buckle positioner Edition 0 October 12 2021 Rev 0 Page 9 76 6 Figure 9 76 2 Front and rear seat belts with movable straps and harnesses PIM DO NOT USE FOR FLIGHT OPER...

Page 894: ...he seat belts on front seats 1 Fasten the belt straps 2 Fasten the buckle positioner in the buckle and adjust its length so that the belt straps remain at hip level 3 Adjust the belt straps 4 Fasten a...

Page 895: ...2 2021 Rev 0 Page 9 76 8 Section 8 Handling servicing and maintenance The buckle positioner does not change the handling servicing and maintenance of the airplane described in Section 8 Handling servi...

Page 896: ...Supplement Beacon lights Table of contents Page 1 General 9 80 2 2 Limitations 9 80 2 3 Emergency procedures 9 80 2 4 Normal procedures 9 80 2 5 Performance 9 80 2 6 Weight and balance 9 80 3 7 Descr...

Page 897: ...2 Limitations of the standard POH Section 3 Emergency procedures Installation of beacon lights does not change the emergency procedures of the airplane described in section 3 Emergency procedures of t...

Page 898: ...on in section 6 Weight and Balance of the standard POH when the airplane is equipped with beacon lights S R A O Item OPT70 or MOD70 Required R or Standard S or Optional A or O equipment Weight per uni...

Page 899: ...he top of the fuselage one on the bottom of the fuselage These lights are controlled by the BEACON switch located on the right side of the instrument panel The beacon lights are powered by the BUS 1 b...

Page 900: ...rpose other than that for which it is supplied nor may information contained in it be disclosed to unauthorized persons It must not be reproduced nor transmitted in any form in whole or in part withou...

Page 901: ...MAR 19 5 0 0 MAR 19 6 0 0 MAR 19 7 0 0 MAR 19 8 0 0 MAR 19 9 0 0 MAR 19 10 0 0 MAR 19 11 0 0 MAR 19 12 0 0 MAR 19 13 0 0 MAR 19 14 0 0 MAR 19 15 0 0 MAR 19 16 0 0 MAR 19 17 0 0 MAR 19 18 0 0 MAR 19 1...

Page 902: ...Pilot s Operating Handbook List of equipment Edition 0 March 05 2019 Rev 0 Page 0B Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 903: ...ot s Operating Handbook List of equipment Edition 0 March 05 2019 Rev 0 Page 0C List of amendments Revision 0 dated March 05 2019 Pages Description All pages Creation PIM DO NOT USE FOR FLIGHT OPERATI...

Page 904: ...Pilot s Operating Handbook List of equipment Edition 0 March 05 2019 Rev 0 Page 0D Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

Page 905: ...urnishings 13 ATA 26 Fire protection 16 ATA 27 Flight controls 17 ATA 28 Fuel system 18 ATA 30 Ice and rain protection 19 ATA 31 Indicating recording systems 21 ATA 32 Landing gears 22 ATA 33 Lights 2...

Page 906: ...ane file Columns showing weight in pounds and arm in inches provide the weight and center of gravity location for the equipment In the list of Required Standard or Optional equipment not restrictive a...

Page 907: ...P N Barometric altimeter GDC72B Air data computer GDU1250W Display 2 3 2 2 P N 011 03734 40 P N 011 04186 00 Autopilot Altitude Hold function GMC710 AFCS mode controller GIA64W Integrated Avionics Com...

Page 908: ...ion 0 March 05 2019 Rev 0 Page 4 S R A O Item OPT70 or MOD70 Required R or Standard S or Optional A or O equipment Weight per unit lb kg Arm in m 01 Specific optional equipment S 01026A Flight ceiling...

Page 909: ...6044A010001 4 06 0 840 153 54 3 900 S Bleed temperature switch 92244B010002 0 13 0 060 153 54 3 900 21 30 Pressurization control S Cabin altitude warn switch 214 C40 3 261 0 077 0 035 153 94 3 910 S C...

Page 910: ...108 27 2 750 S Non return valve 52704A010001 0 66 0 300 118 11 3 000 S Ground Fan 8031A020 3 95 1 790 90 55 2 300 S Ground Fan 8031A030 3 95 1 790 90 55 2 300 21 55 Vapor cycle cooling system S Compre...

Page 911: ...it lb kg Required R or Standard S or Optional A or O equipment Item OPT70 or MOD70 S Inlet temperature sensor 93276A010001 0 11 0 050 153 54 3 900 S Cockpit ventilated sensor 92279A010002 0 18 0 080 1...

Page 912: ...l servo GSA 81 Servo mount GSM 86 4 08 1 85 231 10 5 870 Yaw servo GSA 81 Servo mount GSM 86 4 08 1 85 253 70 6 444 Pitch trim servo GSA 81 Servo mount GSM 86 4 14 1 88 157 87 4 010 Trim adapter GTA 8...

Page 913: ...or 155 94 3 961 or 161 33 4 098 S Static dischargers 2 31 SCY Qty 2 Neglig S 0526 23A Static dischargers on flaps Neglig Static dischargers 2 5 SCY Qty 2 Neglig O 0287 23A Radio stereo headset A20 wit...

Page 914: ...28 8 694 Power amplifier 8 40 3 810 342 83 8 708 HF Antenna kit 1 74 0 790 324 80 8 250 A 0458 23B GDL 69A SXM XM Generation 4 interfaced with G3000 system 1 41 0 640 163 46 4 152 S 0563 23A Dual aud...

Page 915: ...ionics Unit 2 refer to ATA 34 28 VHF antenna above fuselage 16 21B P3 0 86 0 390 271 65 6 900 S 0564 31C G3000 COM 1 system Transceiver integrated in GIA 64W Integrated Avionics Unit 1 refer to ATA 34...

Page 916: ...4 Electric power system EPS 1408 1 1 14 330 6 500 128 15 3 255 R Stand by alternator ES10024B 5 13 000 5 897 104 84 2 663 R Starter generator MG94K 1 31 989 14 510 118 83 2 815 S 24002A Lead acid batt...

Page 917: ...tment A 25032 Front seats ease covers 2 756 1 250 183 78 4 668 A 0417 25 Support device for document on yoke one on each control wheel Version A Paper clips Neglig 166 00 4 220 Version B Mechanical pr...

Page 918: ...two 5 VDC servicing double plug units USB type 6430202 5 in the cabin R H and L H Intermediate seats S 0531 25A 13 8 VDC servicing plug unit of which 0 74 0 334 193 00 4 900 28 12 VDC converter 643012...

Page 919: ...98 22 67 185 86 4 721 S 0588 25A Front R H seat T700J2500005 with seat heaters system 49 98 22 67 185 86 4 721 25 60 Emergency equipment S Smoke goggles MXP 210 0 855 0 388 200 00 5 080 25 61 Emergen...

Page 920: ...lb kg Required R or Standard S or Optional A or O equipment Item OPT70 or MOD70 26 Fire protection A 0391 26 Portable fire extinguisher unit 74 00 Version A on R H Station R H Upholstering 4 89 2 220...

Page 921: ...700 02 1 543 0 700 395 27 10 040 S 0348 27 New control wheels S L H equipped control wheel 83912112 2 535 1 150 157 48 4 000 S R H equipped control wheel 83912113 2 535 1 150 157 48 4 000 27 30 Pitch...

Page 922: ...0 24 2 800 R Fuel unit L88A15 651 4 586 2 080 133 07 3 380 R A35 fuel sequencer unit 1 102 0 500 125 98 3 200 28 40 Fuel indication R 0158 28C Fuel gage amplifier in us gal 738574 1 0 1 08 0 49 278 74...

Page 923: ...02 inboard L H wing 5 732 2 600 173 23 4 400 S Deicer T700A3010001003 inboard R H wing 5 732 2 600 173 23 4 400 S Deicer T700A3010001004 middle L H wing 3 748 1 700 173 23 4 400 S Deicer T700A30100010...

Page 924: ...ight per unit lb kg Required R or Standard S or Optional A or O equipment Item OPT70 or MOD70 30 40 Windshield deicing S Windshield heater controllers Qty 2 L H R H TWH 93 01 1 984 0 900 149 61 3 800...

Page 925: ...ADRS CARS of which 5 659 2 567 256 50 6 515 Light Data Recorder 4 982 2 260 260 63 6 620 MK170 microphone 0 198 0 090 153 54 3 900 Support pre installed 0 478 0 217 260 63 6 620 S 0533 31A Digital hou...

Page 926: ...5 090 R 0190 32 R H main landing gear D23768001 53 79 24 400 200 39 5 090 32 20 Nose landing gear R 0134 32 Nose gear D23766000 53 57 24 300 93 70 2 380 32 30 Extension and retraction O 0334 32 Main...

Page 927: ...0PR 14 396 6 530 204 33 5 190 R Master cylinder 010 07802 0 882 0 400 145 67 3 700 O 0643 32 Nose tire 070 310 0 5 709 2 590 98 18 2 494 R Nose tire 5 00 5 10PR TL MICHELIN 5 600 2 540 89 57 2 275 GOO...

Page 928: ...hting S 0509 33 Leading edge ice detection LED light 01 0771904 00 0 25 0 113 172 00 4 371 S 0322 00 LED L H taxi and landing lights 01 0771674 01 1 400 0 635 181 10 4 600 S 0322 00 LED R H taxi and l...

Page 929: ...ard S or Optional A or O equipment Item OPT70 or MOD70 S Lights S L H navigation strobe recognition lights 01 0771170 02 0 499 0 227 184 29 4 681 S R H navigation strobe recognition lights 01 0771170...

Page 930: ...reference selector TB30 77010000 0 220 0 100 157 48 4 000 S 0160 34A Authorization to operate in RVSM area S 0423 34A Lift transducer and AoA computer installation of which 1 66 0 752 242 01 6 147 R...

Page 931: ...flight instrumentation system A 0226 00C Synthetic Vision System S 0549 00A Integrated Flight Deck System G3000 composed of PFD1 GDU 1250W 5 49 2 49 154 88 3 934 PFD2 GDU 1250W 5 49 2 49 154 88 3 934...

Page 932: ...rface watch unlock card Neglig 34 31 Marker O 0541 23A MARKER antenna 6216 82 00 0 990 0 450 121 00 3 065 34 41 Stormscope A 34056F Stormscope WX 500 G3000 coupled 4 94 2 24 232 28 5 900 Antenna NY163...

Page 933: ...82 5 812 Transmitting antenna S67 2002 0 300 0 136 182 09 4 625 and Receiving antenna S67 2002 0 300 0 136 205 83 5 228 34 44 Traffic advisory system A 0176 00F TAWS system Neglig A 0258 00G TAS syst...

Page 934: ...75 34D Transponder 1 GTX 33D Mode S with antenna diversity and extended squitter 3 39 1 54 147 68 3 751 Antenna KA 61 under fuselage 0 40 0 18 150 08 3 812 Antenna KA 61 above fuselage 0 40 0 18 193 2...

Page 935: ...ll Mode S enhanced surveillance capability without antenna diversity with extended squitter and ADS B IN acquisition without ethernet connection 2 90 1 32 147 20 3 738 34 57 Global Positioning System...

Page 936: ...per unit lb kg Required R or Standard S or Optional A or O equipment Item OPT70 or MOD70 35 Oxygen S 0207 00 Gaseous oxygen system with ZODIAC oxygen masks 22 73 10 31 226 77 5 760 O 0597 35A MC10 Sma...

Page 937: ...d R or Standard S or Optional A or O equipment Item OPT70 or MOD70 37 Vacuum S Air ejector valve 19E17 5A 0 661 0 300 116 14 2 950 S Regulator and relief valve 38E 96 2D 1 323 0 600 116 14 2 950 S Vac...

Page 938: ...4 S R A O Arm in m Weight per unit lb kg Required R or Standard S or Optional A or O equipment Item OPT70 or MOD70 46 Information system S 0545 46A Pdf viewer installation SD card Neglig S 0547 46C Fl...

Page 939: ...35 S R A O Arm in m Weight per unit lb kg Required R or Standard S or Optional A or O equipment Item OPT70 or MOD70 52 Doors O 0320 52B New Pilot door 45 607 20 687 173 23 4 400 S 0342 52 Additional l...

Page 940: ...on 0 March 05 2019 Rev 0 Page 36 S R A O Arm in m Weight per unit lb kg Required R or Standard S or Optional A or O equipment Item OPT70 or MOD70 56 Windows S 56001A Deiced R H windshield 1 764 0 800...

Page 941: ...5 2019 Rev 0 Page 37 S R A O Arm in m Weight per unit lb kg Required R or Standard S or Optional A or O equipment Item OPT70 or MOD70 57 Wings S 57001A Utilization on runways covered with melting snow...

Page 942: ...S or Optional A or O equipment Item OPT70 or MOD70 61 Propeller 61 10 Propeller assembly S 0345 61 Propeller 5 blade HC E5N 3C NC 8834 K spinner 104552P 171 08 77 60 43 11 1 095 61 20 Controls S Prope...

Page 943: ...l A or O equipment Item OPT70 or MOD70 71 Power plant R Turboprop engine PT6 A 66D 497 30 226 00 79 72 2 025 S Top silentblocks 95007 16 Qty 2 2 647 1 201 79 72 2 025 S Bottom silentblocks 95007 19 Qt...

Page 944: ...12 1 400 R 0328 77 Torque transducer APTE 438 1000 75D 0 473 0 215 54 84 1 393 S 0565 77 Engine Airframe Interface Units GEA 71B installation and Sandia conditioner and low pass filter removal of whic...

Page 945: ...d R or Standard S or Optional A or O equipment Item OPT70 or MOD70 79 Lubrication 79 20 Distribution R Oil cooler L8538233 10 472 4 750 90 55 2 300 79 30 Indicating R 0327 79A Oil pressure transmitter...

Page 946: ...Pilot s Operating Handbook List of equipment Edition 0 March 05 2019 Rev 0 Page 42 Intentionally left blank PIM DO NOT USE FOR FLIGHT OPERATIONS...

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