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4-21

Noise Level

The noise levels stated below have been verified and approved by FOCA in noise level test
flights conducted on the PC-12/47E. The PC-12/47E model is in compliance with all ICAO
Annex 16 and Swiss VEL noise standards applicable to this type.

No determination has been made by EASA (FOCA) for the FAA that the noise levels of this
airplane are or should be acceptable or unacceptable for operation at, into, or out of, any
airport.

ICAO Annex 16, Chapter 10

77.0 dB(A)

Swiss VEL

77.0 dB(A)

FAR Part 36 Appendix G

77.0 dB(A).

Section 4 - Normal Procedures (EASA Approved)

Noise Level

Pilot's Operating Handbook

Report No: 02406

Issue date: Mar 06, 2020

Page 4-21-1

12-C-A15-30-0421-00A-131A-A

FOR

GENERAL

AND

FAMILIARIZATION

PURPOSES

ONLY

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Содержание PC-12 NGX

Страница 1: ...PILOT S INFORMATION MANUAL PC 12 47E MSN 2001 AND UP...

Страница 2: ...liarization purposes only This Pilot s Information Manual does NOT meet FAA FOCA or any other civil aviation authority regulations for operation of ANY Aircraft This Pilot s Information Manual is a re...

Страница 3: ...F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P U R P O S E S O N L Y...

Страница 4: ...F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P U R P O S E S O N L Y...

Страница 5: ...3 1 2 Issue 003 Revision 00 Dated 06 March 2020 FM 3 1 3 Issue 003 Revision 01 Dated 18 December 2020 FM 3 1 Log of Temporary Revisions FM 4 1 List of Service Bulletins FM 5 1 List of APEX Builds FM...

Страница 6: ...of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page FM 0 2 F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P U R P O S E S O...

Страница 7: ...laneous Instrument Markings 06 03 2020 A15 10 0207 00A 043A A Weight Limits 06 03 2020 A15 10 0208 00A 043A A Center of Gravity Limits 06 03 2020 A15 10 0209 00A 043A A Maneuver Limits 06 03 2020 A15...

Страница 8: ...8 0302 00A 014A A CAS Advisories 06 03 2020 A15 48 0303 00A 141A A CAS Status C 18 12 2020 A15 48 0304 00A 014U A Primary Altimeter Diverge by 200 ft or More 06 03 2020 A15 48 0305 00A 141U A Loss of...

Страница 9: ...rmance Data Climb Performance 06 03 2020 A15 60 0503 04A 030A A Performance Data Cruise Performance 06 03 2020 A15 60 0503 05A 030A A Performance Data Specific Air Range 06 03 2020 A15 60 0503 06A 030...

Страница 10: ...705 00A 043A A Baggage Compartment 06 03 2020 A15 00 0706 00A 043A A Cargo Tie Downs 06 03 2020 A15 00 0707 00A 043A A Seats Restraint Systems 06 03 2020 A15 00 0708 00A 043A A Doors Windows and Exits...

Страница 11: ...C 18 12 2020 A15 00 0739 00A 043A A Primus APEX Optional LPV LP Approach 06 03 2020 A15 00 0740 00A 043A A Lightweight Data Recorder If Installed 06 03 2020 A15 20 0801 00A 010A A General 06 03 2020 A...

Страница 12: ...043A A Operations from Prepared Unpaved Surfaces 06 03 2020 A15 20 1007 00A 043A A Passenger Briefings 06 03 2020 Authority Approved List of Effective Data Modules Pilot s Operating Handbook Report No...

Страница 13: ...043A A Maximum Passenger Seating Limits C 21999 Incorporated TR 07 Remove and destroy TR 07 and record the removal in the Log of Temporary Revisions A15 10 0221 00A 043A A Systems and Equipment Limits...

Страница 14: ...l C 21631 Updated Fuel Filter Replace status message description A15 00 0713 00A 043A A Electrical C 21513 PGDS Emergency Operation Condition figures updated removed Hydr Pwr from figures A15 00 0730...

Страница 15: ...6 03 2020 Table 1 1 2 Issue 003 Revision 00 List of changes Section PTS Number Description of Change All 20936 PC 12 Pilot s Operating Manual Issue 003 Revision 00 TR 01 thru 06 are integrated in this...

Страница 16: ...10 21514 Updated location of LDG CTL SEC circuit breaker 3 17 21298 Updated ACS Low Inflow procedure 21495 Updated ECS CB location to LE2 Section 4 4 10 21514 Updated Note editorial 4 27 21514 Change...

Страница 17: ...Dec 2019 Issue 003 Revision 00 04 Emergency Gear Extension 06 Dec 2019 Issue 003 Revision 00 05 EPECS Update 14 Feb 2020 Issue 003 Revision 00 06 Feather Inhibit option 10 Feb 2020 Issue 003 Revision...

Страница 18: ...f Issue Cancelled by Log of Temporary Revisions Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page FM 4 2 12 C A15 00 0000 00A 002B A F O R G E N E R A L A N D F A M I L I A R I Z...

Страница 19: ...st of SBs The purpose is to show the modification status of the aircraft to assist the pilot in the correct understanding of the procedures and the system description SB No SB Title List of Service Bu...

Страница 20: ...e List of Service Bulletins Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page FM 5 2 12 C A00 00 0000 00A 930A A F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P U R P O...

Страница 21: ...e List of Service Bulletins Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page FM 5 3 12 C A00 00 0000 00A 930A A F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P U R P O...

Страница 22: ...e List of Service Bulletins Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page FM 5 4 12 C A00 00 0000 00A 930A A F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P U R P O...

Страница 23: ...t number ECL version number ECL software version Build 12 EB60003299 0115 1212 00 PC1200101 ecl Build 12 6 1 EB60003299 0116 1212 01 PC1200102 ecl Build 12 6 1 EB60003299 0116 1212 02 PC1200103 ecl Li...

Страница 24: ...rsion number ECL software version List of APEX Builds Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page FM 6 2 12 C A15 00 0001 00A 030A A F O R G E N E R A L A N D F A M I L I A...

Страница 25: ...1 1 4 Revision Markings 0 1 1 5 Revision Issue Dates 0 1 1 6 Revision Procedure 0 1 2 7 Supplements 0 1 3 8 Copyright and Legal Statement 0 1 3 Section 0 Introduction Table of Contents Pilot s Operati...

Страница 26: ...uction Table of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 0 0 2 F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P U R P...

Страница 27: ...formation depending on the subject they address However when any of the content inside a DM changes the entire DM is up issued and distributed as the sum total of or as a portion of a POH revision Eac...

Страница 28: ...ions which DM needs to be inserted in new DM replaced changed DM or deleted from the POH with the applicable revision 6 2 Change Highlights The Change Highlights provides a dedicated overview of the c...

Страница 29: ...number A list of available Supplements at the release date of the POH is given in Section 9 of the POH All applicable Supplements are to be inserted in this Section 9 of the POH Section 1 of the Suppl...

Страница 30: ...Legal Statement This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 0 1 4 12 C A15 00 0010 00A 018A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 31: ...tions and Terminology 1 5 1 1 5 1 General Airspeed Terminology and Symbols 1 5 1 1 5 2 Meteorological Terminology 1 5 2 1 5 3 Power Terminology 1 5 3 1 5 4 Engine Controls and Instruments Terminology...

Страница 32: ...ral Table of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 1 0 2 F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P U R P O...

Страница 33: ...efinitions and explanations of symbols abbreviations and terminology that is used throughout this POH Section 1 General General Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 1...

Страница 34: ...al This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 1 1 2 12 C A15 00 0101 00A 010A A F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P...

Страница 35: ...order to achieve maximum utilization as an operating guide for the pilot This POH is divided into numbered sections which are separated by tabs Section 3 Emergency Procedures is further highlighted by...

Страница 36: ...ction This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 1 2 2 12 C A15 00 0102 00A 018A A F O R G E N E R A L A N D F A M I L I A R I Z A T I O...

Страница 37: ...NOTE WINGSPAN DIMENSION IS IN A FULLY FUELED CONDITION ICN 12 C A150103 A S4080 00113 A 001 01 Figure 1 3 1 Airplane Three view Diagram and Dimensions Section 1 General Top Level Illustrations Pilot...

Страница 38: ...11 68 m 47 3 14 41 m B A E D A B E D ROTATION POINT MEASUREMENT POINT C C NOTE ICN 12 C A150103 A S4080 00114 A 001 01 Figure 1 3 2 Airplane Ground Turning Clearance NWS only No Braking Section 1 Gene...

Страница 39: ...1 E INSIDE MAIN GEAR RADIUS 0 5 m 19 5 C E E B B D D ROTATION POINT MEASUREMENT POINT ICN 12 C A150103 A S4080 00115 A 001 01 Figure 1 3 3 Airplane Ground Turning Clearance NWS and Braking Section 1...

Страница 40: ...ustrations This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 1 3 4 12 C A15 00 0103 00A 030A A F O R G E N E R A L A N D F A M I L I A R I Z A T...

Страница 41: ...el Number HC E5A 31A NC10245B Number of Blades 5 Propeller Diameter 105 2 67 m Propeller Type The propeller assembly consists of a hub unit and five composite blades and is a hydraulically actuated co...

Страница 42: ...pty Weight approx 6173 lb 2800 kg Useful Load 4277 lb 1940 kg Empty weight of standard airplane with standard interior 9 passenger seats and cabin floor covering 1 4 7 Cabin and Entry Dimensions Maxim...

Страница 43: ...183 7 kg sq m Power Loading 8 71 lb shp 3 95 kg shp Section 1 General Specific Loadings Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 1 4 3 12 C A15 00 0104 00A 030A A F O R...

Страница 44: ...oadings This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 1 4 4 12 C A15 00 0104 00A 030A A F O R G E N E R A L A N D F A M I L I A R I Z A T I...

Страница 45: ...ximum speed at which an airplane can be safely flown with the landing gear extended VLO Maximum Landing Gear Operating Speed is the maximum speed at which the landing gear can be safely extended or re...

Страница 46: ...ables on the charts of this AFM are to be understood as the headwind or tailwind components of the reported winds ELEV Geographical altitude of landing field Icing Conditions Can exist when the Outsid...

Страница 47: ...he Np Beta sensor and beta ring position to calculate blade angle which is controlled and commanded by the PCL Below flight regime i e aft of the idle detent the Propeller Control Unit PCU limits the...

Страница 48: ...climb to the horizontal distance traversed in the same time interval Demonstrated Crosswind Velocity The demonstrated crosswind velocity is the velocity of the crosswind component for which adequate c...

Страница 49: ...fuselage usually given in terms of distance from the reference datum Tare Weight The weight indicated by a scale before it is loaded Unusable Fuel Fuel which may not be considered usable for flight p...

Страница 50: ...1 General Fahrenheit F C x 1 8 32 Celsius C F 32 x 0 556 Statute Mile sm Nautical Mile nm x 1 151 Nautical Mile nm Statute Mile sm x 0 869 Jet Fuel JET A Standard Weights at 15 C Relative Density 0 8...

Страница 51: ...Kilometers km x 0 621 Nautical Miles nm Kilometers km x 0 54 US Gallons US gal Liters x 0 264 Imperial Gallons IMP gal Liters x 0 22 Pounds lb Kilograms kg x 2 205 psi Bar x 14 504 Section 1 General...

Страница 52: ...nformation This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 1 5 8 12 C A15 00 0105 00A 005A A F O R G E N E R A L A N D F A M I L I A R I Z A T...

Страница 53: ...Feather Inhibit optional 2 4 6 2 5 Power Plant Window Markings 2 5 1 2 6 Miscellaneous Instrument Markings 2 6 1 2 7 Weight Limits 2 7 1 2 8 Center of Gravity Limits 2 8 1 2 9 Maneuver Limits 2 9 1 2...

Страница 54: ...l System 2 21 2 2 21 12 Primus Apex Flight Management System 2 21 3 2 21 13 RVSM 2 21 6 2 21 14 Primus Apex TCAS 2 21 6 2 21 15 Primus Apex Transponder 2 21 7 2 21 16 Primus Apex ADAHRS 2 21 7 2 21 17...

Страница 55: ...22 1 2 22 4 Structural Limitations 2 22 2 2 22 5 Smoking 2 22 2 2 22 6 Portable Electronic Devices 2 22 2 2 23 Placards 2 23 1 Section 2 Limitations EASA Approved Table of Contents Pilot s Operating H...

Страница 56: ...ASA Approved Table of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 2 0 4 F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P...

Страница 57: ...cuit breakers on the Essential Bus and if not detailed otherwise in procedures all tripped open circuit breakers are not allowed to be reset in flight Circuit breakers on the Essential Bus if tripped...

Страница 58: ...ved General This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 1 2 12 C A15 10 0201 00A 010A A F O R G E N E R A L A N D F A M I L I A R I Z A...

Страница 59: ...54 8380 lb 3800 kg 148 7940 lb 3600 kg 144 7500 lb 3400 kg 140 7060 lb 3200 kg 136 6610 lb 3000 kg 132 6170 lb 2800 kg 127 5730 lb 2600 kg 123 Maximum flap extended speed VFE Do not exceed this speed...

Страница 60: ...CN 12 C A150202 A S4080 00116 A 001 01 Figure 2 2 1 VMO MMO Schedule Section 2 Limitations EASA Approved Airspeed Limitations Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 2...

Страница 61: ...gear extended only Labeled Placards on right side of tape 180 VLO 165 VFE 15 130 VFE 30 40 Maximum flap operating and extended speed VFE 15 30 40 and maximum landing gear operating speed VLO Red low...

Страница 62: ...ed Indication Markings This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 3 2 12 C A15 10 0203 00A 043A A F O R G E N E R A L A N D F A M I L I...

Страница 63: ...mitted Note The oils listed are approved to MIL PRF 23699 Type II 2 4 3 Oil Quantity Total Oil Capacity 3 6 US gal 13 6 liters Drain and Refill Quantity 2 0 US gal 7 6 liters Oil Quantity Operating Ra...

Страница 64: ...F 7 10 1200 44 84 850 104 1700 90 to 135 15 to 110 MAX CLIMB 7 1200 44 84 825 104 1700 90 to 135 15 to 105 CRUISE 7 1100 40 63 820 104 1700 90 to 135 15 to 105 MIN IDLE 8 750 64 5 60 MIN 40 to 110 STA...

Страница 65: ...ature ITT is 5 seconds 7 Engine oil temperature must be 15 C or above prior to setting takeoff power on ground Engine oil temperature must be 10 C or above when operating with anti icing additives 8 F...

Страница 66: ...ided periodic fuel nozzle inspections are found acceptable by P WC 3 Not allowed for use when cloud point is lower than 5 C 4 Shall not contain a biodiesel component 5 Unless otherwise specified inter...

Страница 67: ...gine components Refer to Section 8 Handling Servicing and Maintenance Fuel Anti Ice Additive for blending instructions 2 4 7 Propeller Propeller Manufacturer Hartzell Propeller Model Number HC E5A 31A...

Страница 68: ...P 450 AMP Maximum load permitted for a 2 minute period per each one hour of operation 2 4 10 Power Control Lever Operation Power Control Lever operation aft of the idle detent is prohibited during fli...

Страница 69: ...84 ITT C N A N A 400 to 820 820 850 Engine Speed Ng N A 60 60 to 103 5 104 104 3 Oil Temperature C N A 15 15 to 105 105 110 Oil Pressure psi 60 90 90 to 135 N A 135 Section 2 Limitations EASA Approve...

Страница 70: ...Plant Window Markings This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 5 2 12 C A15 10 0205 00A 043A A F O R G E N E R A L A N D F A M I L I...

Страница 71: ...Ops YELLOW ARC Caution RED RAD DIA Max Limit Oxygen Pressure psi N A N A N A N A 1850 to 2000 Section 2 Limitations EASA Approved Miscellaneous Instrument Markings Pilot s Operating Handbook Report N...

Страница 72: ...eous Instrument Markings This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 6 2 12 C A15 10 0206 00A 043A A F O R G E N E R A L A N D F A M I L...

Страница 73: ...00 kg Maximum Baggage Weight 400 lb 180 kg Maximum Floor Loading On Seat Rails 205 lb ft2 1000 kg m2 On Cabin Floor 125 lb ft2 600 kg m2 Section 2 Limitations EASA Approved Weight Limits Pilot s Opera...

Страница 74: ...Weight Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 7 2 12 C A15 10 0207 00A 043A A F O R G E N E R A L A N D F A M I L I A R I Z...

Страница 75: ...aight line variation between points given The datum is 118 in 3 0 m forward of firewall It is the responsibility of the pilot to ensure that airplane is loaded properly See Section 6 Weight and Balanc...

Страница 76: ...er of Gravity Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 8 2 12 C A15 10 0208 00A 043A A F O R G E N E R A L A N D F A M I L I A...

Страница 77: ...mal flying stalls except whip stalls lazy eights chandelles and turns in which the bank angle does not exceed 60 Aerobatic maneuvers including spins are not approved Section 2 Limitations EASA Approve...

Страница 78: ...Maneuver Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 9 2 12 C A15 10 0209 00A 043A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 79: ...ad limits with flaps down 2 0 g 0 0 g Section 2 Limitations EASA Approved Flight Load Factor Limits Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 10 1 12 C A15 10 0210 00A 0...

Страница 80: ...t Load Factor Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 10 2 12 C A15 10 0210 00A 043A A F O R G E N E R A L A N D F A M I L I...

Страница 81: ...t in the left hand seat Section 2 Limitations EASA Approved Flight Crew Limits Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 11 1 12 C A15 10 0211 00A 043A A F O R G E N E R...

Страница 82: ...ight Crew Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 11 2 12 C A15 10 0211 00A 043A A F O R G E N E R A L A N D F A M I L I A R...

Страница 83: ...3 IFR Day incl CAT 1 approaches single pilot 4 IFR Night incl CAT 1 approaches single pilot 5 Flight into known icing conditions Section 2 Limitations EASA Approved Kinds of Operation Pilot s Operatin...

Страница 84: ...nds of Operation This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 12 2 12 C A15 10 0212 00A 043A A F O R G E N E R A L A N D F A M I L I A R...

Страница 85: ...manent damage to the boots The wing and tail leading edge pneumatic de icing boot system must be activated at the first sign of ice formation anywhere on the aircraft The wing and tail leading edge pn...

Страница 86: ...ic Deicing Boot System This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 13 2 12 C A15 10 0213 00A 043A A F O R G E N E R A L A N D F A M I L...

Страница 87: ...is not approved The aircraft must be clear of all deposits of snow ice and frost adhering to the lifting and control surfaces immediately prior to takeoff In the event of a balked landing go around w...

Страница 88: ...determined by the following visual cues If one or more of these visual cues exists immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to exit th...

Страница 89: ...has been authorized by the appropriate regulatory agency Table 2 15 1 Kinds of Operation Equipment List SYSTEM EQUIPMENT VFR DAY VFR NIGHT IFR DAY IFR NIGHT ICING RVSM PRIMUS APEX Pilot PFD 1 1 1 1 1...

Страница 90: ...1 1 1 1 1 Instrument and Panel Lighting 0 AR AR AR AR AR Audio System 1 1 1 1 1 1 Cockpit Speaker 1 1 1 1 1 1 Cabin Speaker 1 1 1 1 1 1 De ice Boot Timer 0 0 0 0 1 0 AOA Heater LH 1 1 1 1 1 1 AOA Heat...

Страница 91: ...ing RH 1 1 1 1 1 1 De ice Boot Outer Wing RH 1 1 1 1 1 1 De ice Boot Tail LH 1 1 1 1 1 1 De ice Boot Tail RH 1 1 1 1 1 1 Fuel Control Monitoring System 1 1 1 1 1 1 For Pressurized Flight ACS 1 1 1 1 1...

Страница 92: ...Operation Equipment List This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 15 4 12 C A15 10 0215 00A 043A A F O R G E N E R A L A N D F A M I...

Страница 93: ...Maximum Fuel Imbalance 26 4 US gal 178 lb 100 liters 80 6 kg Maximum 3 segments on indicator Note Usable fuel can be safely used during all Normal Category airplane maneuvers Section 2 Limitations EA...

Страница 94: ...uel Limitations This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 16 2 12 C A15 10 0216 00A 043A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 95: ...000 ft 9144 m Section 2 Limitations EASA Approved Maximum Operating Altitude Limits Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 17 1 12 C A15 10 0217 00A 043A A F O R G E...

Страница 96: ...perating Altitude Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 17 2 12 C A15 10 0217 00A 043A A F O R G E N E R A L A N D F A M I...

Страница 97: ...utside Air Temperature 50 C 122 F Section 2 Limitations EASA Approved Outside Air Temperature Limits Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 18 1 12 C A15 10 0218 00A...

Страница 98: ...Air Temperature Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 18 2 12 C A15 10 0218 00A 043A A F O R G E N E R A L A N D F A M I L...

Страница 99: ...ssurized landing is approved up to 0 7 psid Section 2 Limitations EASA Approved Cabin Pressurization Limits Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 19 1 12 C A15 10 02...

Страница 100: ...Pressurization Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 2 19 2 12 C A15 10 0219 00A 043A A F O R G E N E R A L A N D F A M I L I...

Страница 101: ...given below Corporate Commuter Interior Code STD 9S nine standard seats Executive Interior Code EX 6S 2 six executive seats Executive Interior Code EX 8S eight executive seats Executive Interior Code...

Страница 102: ...assenger Seating Limits This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 2 20 2 12 C A15 10 0220 00A 043A A F O R G E N E R A L A N D F A M I L...

Страница 103: ...itions at least one heating zone of the windshield on the side of the pilot in command must function properly 2 21 5 Fire Detection System Preflight Function Test is required for takeoff System must f...

Страница 104: ...with seat belt fastened The Autopilot AP and Yaw Damper YD must be OFF during takeoff and landing The Autothrottle AT must be OFF during landing Minimum engagement height after takeoff is 400 ft Abov...

Страница 105: ...rminal and En Route Area Navigation RNAV Operations B RNAV AMC 20 4 Guidance Material on Airworthiness Approval and Operational Criteria for the use of navigation Systems in European Airspace Designat...

Страница 106: ...System FMS second GPS and Cursor Control Device CCD are installed This does not constitute an operational approval RNP 4 RNP 10 AC20 138D The APEX FMS and KGS200 GNSSU complies with the requirements...

Страница 107: ...ordance with the operational approval Dead reckoning mode of navigation based on AHRS is not available in the high latitude regions approximately north of 82 north latitude and south of 82 south latit...

Страница 108: ...shall only be used for emergency procedures The RVSM option in the PRIMUS APEX option file has to be activated Contact Pilatus customer support for further proceeding 2 21 14 Primus Apex TCAS 2 21 14...

Страница 109: ...s displayed then the system accuracy does not allow VOR VOR DME and NDB non precision approaches The flight crew must use GPS VOR DME or GPS NDB overlay approaches LNAV or LNAV VNAV approaches RNAV GP...

Страница 110: ...PS sensor failure The aircraft symbol is not in scale with the APEX Electronic Charts The APEX Electronic Charts do not replace approved published paper or approved electronic systems for aeronautical...

Страница 111: ...ed LPV LP approach will not be available Use of NAV preview functionality will cause an amber LPV UNVL or LP UNVL message to be displayed Additional limitations for operation within EGNOS coverage are...

Страница 112: ...Apex Terrain Database This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 2 21 10 12 C A15 10 0221 00A 043A A F O R G E N E R A L A N D F A M I L...

Страница 113: ...tion of the net At least 340 mm forward of frame 34 when the net floor attachments are placed at frame 34 2 22 3 Cargo Limitations Maximum Freight Load 3300 lbs 1500 kg Cargo must be arranged to permi...

Страница 114: ...ding Change 1 Section 4 Back door coupling susceptibility was tested in accordance with DO 307 including Change 1 Section 3 There are no restrictions resulting from DO 307 testing therefore it is in t...

Страница 115: ...ESS IN EMERGENCY ICN 12 C A150223 A S4080 00117 A 001 01 Figure 2 23 1 Placards Exterior Sheet 1 of 7 Section 2 Limitations EASA Approved Placards Pilot s Operating Handbook Report No 02406 Issue date...

Страница 116: ...Y PULL TO OPEN ICN 12 C A150223 A S4080 00118 A 001 01 Figure 2 23 1 Placards Exterior Sheet 2 of 7 Section 2 Limitations EASA Approved Placards Pilot s Operating Handbook Report No 02406 Issue date D...

Страница 117: ...izontal Stabilizer On Rudder each side DO NOT PUSH Figure 2 23 1 Placards Exterior Sheet 3 of 7 Section 2 Limitations EASA Approved Placards Pilot s Operating Handbook Report No 02406 Issue date Dec 1...

Страница 118: ...used will be added to the placard prior to delivery of the aircraft ENGINE OIL TYPE USED PUSH Figure 2 23 1 Placards Exterior Sheet 4 of 7 Section 2 Limitations EASA Approved Placards Pilot s Operatin...

Страница 119: ...60 psi 4 1 bar TYRE PRESSURE 60 psi 4 1 bar JET A FUEL TOTAL CAPACITY 770 LTR 203 US GAL SEE PILOT S OPERATING HANDBOOK FOR APPROVED FUELS AND QUANTITY Near Fuel Vent FUEL VENT ICN 12 C A150223 A S40...

Страница 120: ...y compartment and outside on Rear Fuselage Bottom Access Door OXYGEN SERVICE POINT USE NO LUBRICANTS NOSE LANDING GEAR SHOCK STRUT N2 CHARGE PRESSURE 1st STAGE 50 psi 3 5 bar 2nd STAGE 834 psi 57 5 ba...

Страница 121: ...psi 115 bar On Rear Fuselage Bottom Access Door On Rear Fuselage Bottom LH side BATTERY COMPARTMENT INSTALLED INSIDE Figure 2 23 1 Placards Exterior Sheet 7 of 7 Section 2 Limitations EASA Approved Pl...

Страница 122: ...T ONLY ONE HEADSET OXYGEN MASK MIC RH only LH only RH only MAU DATA LOAD Option EMERG COM1 AURAL WARN MIC SELECT CVFDR TEST ICN 12 C A150223 A S4080 00124 A 001 01 Figure 2 23 2 Placards Cockpit Sheet...

Страница 123: ...ICE BOOTS 0 FLAP OPERATIONAL LIMITATIONS THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS MARKINGS AND MANUALS...

Страница 124: ...30 KIAS V L0 180 KIAS V LE 240 KIAS TOTAL USABLE CAPACITY 1521 LTR 402 US GAL 2704 LBS JET A1 On LH Crosspanel optional COM 3 ICN 12 C A150223 A S4080 00126 A 001 01 Near AFCS Control Panel if AT not...

Страница 125: ...D WINDSHIELD DE ICE LH RH OFF PROBES DE ICE OFF ELECTRICAL HEAT COOL SWITCH INHIBIT FOOT WARMER OFF IF INST A P DISC INOP On Cockpit LH Instrument Panel ELT ON CKLST When optional electronic checklist...

Страница 126: ...LIZED PROPELLER OPERATION ON GROUND NOT FEATHERED BETWEEN 350 AND 950 rpm IS PROHIBITED G R O U N D R E V E R S E Figure 2 23 2 Placards Cockpit Sheet 5 of 6 Section 2 Limitations EASA Approved Placar...

Страница 127: ...EMERGENCY SHUT OFF ACS PULL EMERGENCY SHUT OFF PRESS TO RELEASE PULL FUEL PULL OPEN AT DISC VHF1 XFER TO GA Behind Crew Seats SMOKE GOGGLE PULL Figure 2 23 2 Placards Cockpit Sheet 6 of 6 Section 2 Li...

Страница 128: ...N The following standard placards are installed in all aircraft PUSH BUTTON FOR COCKPIT DOME LIGHT ICN 12 C A150223 A S4080 00130 A 001 01 Figure 2 23 3 Placards Cabin Sheet 1 of 3 Section 2 Limitatio...

Страница 129: ...rgo Door DO NOT OPEN DOOR WHEN ENGINE IS RUNNING UNLESS IN EMERGENCY On Cabin to Baggage Area Step KEEP GRILL CLEAR ICN 12 C A150223 A S4080 00131 A 001 01 Figure 2 23 3 Placards Cabin Sheet 2 of 3 Se...

Страница 130: ...EMERGENCY EXIT Max Load on Seat Rails Max Load on Floor Panels 1000 kg m 205 lb ft 600 kg m 125 lb ft 2 2 2 2 MAX BAGGAGE LOAD 180 kg 400 lb or On lower Cargo Door Frame ICN 12 C A150223 A S4080 00132...

Страница 131: ...nd Cover OXYGEN On the forward Cargo Door Frame The cabin placards plus the following additional placards are those required for this interior On the rear of each seat except seat No 5 FOR TAKEOFF AND...

Страница 132: ...E PULL HERE Right cabinet Left cabinet Upper Lower WEIGHT LIMIT 4 5 kg 10 lb WEIGHT LIMIT 11 5 kg 25 lb Upper Lower OXYGEN MASK INSIDE PULL TAPE FOR OXYGEN MASK Near each executive seat FOR TAKEOFF AN...

Страница 133: ...6S 2 SEE AFM POH SECTION 6 PULL TAPE FOR OXYGEN MASK PULL TAPE FOR OXYGEN MASK or ICN 12 C A150223 A S4080 00135 A 001 01 Figure 2 23 5 Placards 6 Seat executive Interior code EX 6S 2 Sheet 2 of 2 Se...

Страница 134: ...PE FOR OXYGEN MASK or or PLACARDS 8 SEAT EXECUTIVE Interior Code EX 8S 6 SEAT EXECUTIVE AND 2 SEAT CORPORATE COMMUTER Interior Code EX 6S STD 2S 4 SEAT EXECUTIVE AND 4 SEAT CORPORATE COMMUTER Interior...

Страница 135: ...PILOT SEAT LIMITATIONS NOPERSON S ALLOWEDINCABIN BAGGAGEORLUGGAGEINTHECABINMUST BETIEDDOWNASDEFINEDINTHEAFM POH CAUTION EXTREMECAUTIONMUSTBEAPPLIEDNOTTO CONTACTTHESIDEWALLSASNOPROTECTIVE INTERIORSHELL...

Страница 136: ...AND EMERGENCY EXIT MAX FREIGHT LOAD 1500 kg 3300 lb On the cargo door handle On cabin to baggage area step KEEP GRILL CLEAR On the ferry plate left side Frame 34 On the ferry plate right side Frame 34...

Страница 137: ...3 4 03 Engine failure after rotation Landing gear up 3 4 2 3 4 04 Engine Failure in Flight Total Power Loss 3 4 2 3 4 05 Engine Surging 3 4 3 3 5 Air Start 3 5 1 3 5 01 Air Start Envelope 3 5 1 3 5 02...

Страница 138: ...3 9 1 3 9 02 Forced Landing 3 9 1 3 9 03 Landing with Main Landing Gear Unlocked 3 9 2 3 9 04 Landing with Nose Landing Gear Unlocked 3 9 3 3 9 05 Landing with Gear Up 3 9 4 3 9 06 Landing without El...

Страница 139: ...vionics 2 Bus 3 15 2 3 15 05 Main Bus 3 15 2 3 15 06 Generator 1 Bus 3 15 3 3 15 07 Generator 2 Bus 3 15 3 3 15 08 Standby Bus 3 15 4 3 15 09 Non Essential Bus 3 15 4 3 15 10 Bus Tie 3 15 4 3 15 11 Ge...

Страница 140: ...ted 3 16 8 3 16 11 Fuel IMP Bypass 3 16 9 3 16 12 Fuel Filter Blocked 3 16 10 3 16 13 Fuel TEMP 3 16 11 3 17 Cabin Environment Failures 3 17 1 3 17 01 Cabin Pressure 3 17 1 3 17 02 Cabin Pressure 3 17...

Страница 141: ...1 3 22 APEX Failures 3 22 1 3 22 01 All APEX display units indicate a red X or blank 3 22 1 3 22 02 Check DU 1 3 22 2 3 22 02 Check DU 2 3 22 2 3 22 02 Check DU 3 3 22 2 3 22 02 Check DU 4 3 22 2 3 22...

Страница 142: ...llaneous On Ground Only 3 22 12 3 22 25 MAU A Fail 3 22 12 3 22 26 MAU B Fail 3 22 13 3 22 27 Air Ground Fail 3 22 13 3 22 28 Aural Warning Fail 3 22 14 3 22 29 DME 1 Fail 3 22 14 3 22 30 Rad Alt 1 Fa...

Страница 143: ...22 48 ADS B Out 3 22 24 3 22 49 ASCB Fail 3 22 25 3 22 50 Automatic Flight Control System Failures 3 22 27 3 22 51 HSI1 is MAG TRK 3 22 30 3 22 51 HSI2 is MAG TRK 3 22 30 3 22 51 HSI1 2 is MAG TRK 3 2...

Страница 144: ...res EASA Approved Table of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 3 0 8 F O R G E N E R A L A N D F A M I L I A R I Z A T I...

Страница 145: ...r panel for CAS related CB status A Action Immediate and subsequent actions guided by airmanship and given checklist procedures The emergency procedures use the terms Land as soon as possible and Land...

Страница 146: ...ailures once the failure is identified 3 1 3 Flight Alerting System Flight Alerting System FAS messages are given when necessary on the pilot s PFD to warn of a condition that requires immediate actio...

Страница 147: ...9040 lb 4100 kg 110 KIAS 8160 lb 3700 kg 105 KIAS 7280 lb 3300 kg 99 KIAS 6400 lb 2900 kg 93 KIAS Landing Approach Speeds with ice accretion on the airframe After failure of Minimum Approach Speed Pne...

Страница 148: ...eeds for Emergency Operations This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 2 2 12 C A15 40 0302 00A 043U A F O R G E N E R A L A N D F A...

Страница 149: ...and pull lever up 7 MASTER POWER switch EMERG OFF After the aircraft has stopped 8 Aircraft Evacuate CAUTION A rejected takeoff may cause overheating of wheel and brake assembly components The main wh...

Страница 150: ...ted Takeoff Not engine related This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 3 2 12 C A15 40 0303 00A 141U A F O R G E N E R A L A N D F A...

Страница 151: ...ircraft Land straight ahead turning only to avoid obstructions maximum recommended bank angle 30 L R 2 Flaps 40 3 Final Approach Speed for 10450 lb 4740 kg 88 KIAS Not below Dynamic Speed Bug 1 3 VS 4...

Страница 152: ...OFF After the aircraft has stopped 8 Aircraft Evacuate END Engine Failure in Flight Total Power Loss 3 4 04 1 Autopilot Use FLC best glide speed and HDG T or NAV mode Best glide propeller feathered we...

Страница 153: ...rical HEAT COOL switch INHIBIT If engine surge persists 4 PCL Set to IDLE and descent to denser air if required to 15 000 ft If engine surge persists and flight altitude cannot be maintained 5 ACS Ble...

Страница 154: ...oved Engine Failure This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 3 4 4 12 C A15 40 0304 00A 141U A F O R G E N E R A L A N D F A M I L I A...

Страница 155: ...G IF THE ENGINE RUNS AT FLIGHT IDLE WITH THE PROPELLER FEATHERED ABOVE FL200 KEEP ENGINE RUNNING UNTIL WITHIN AIR START ENVELOPE TO MINIMIZE EXPOSURE TIME WITHOUT BLEED AIR AND GENERATOR SUPPORT 1 Eng...

Страница 156: ...installed PUSH set to ON if not active 11 Engine switch RUN 12 FUEL EMERG shut off Full in 13 BAT 1 and BAT 2 switches ON 14 Air start envelope Check Refer to Fig 3 5 1 15 IGNITION switch ON 16 STARTE...

Страница 157: ...TO A LEVEL THAT WOULD NOT BE ABLE TO SUPPORT ESSENTIAL ELECTRICAL SERVICES 22 Aircraft Make a Forced Landing 3 9 02 END Section 3 Emergency Procedures EASA Approved Air Start Pilot s Operating Handboo...

Страница 158: ...pproved Air Start This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 5 4 12 C A15 40 0305 00A 141U A F O R G E N E R A L A N D F A M I L I A R...

Страница 159: ...n 3 Engine Shutdown as soon as possible If propeller RPM is above 1760 steady state 4 PCL IDLE 5 Engine Shutdown END In flight 1 NP Check PROP RPM If propeller RPM is below 1640 steady state 2 PCL Inc...

Страница 160: ...ected landing airfield in case of total engine failure END If NG is below 64 5 On ground 1 PCL IDLE Engine Shutdown END In flight 1 PCL Increase power 2 Aircraft speed Increase If engine does not resp...

Страница 161: ...possible using minimum power If possible always retain glide capability to the selected landing airfield in case of total engine failure END Engine Oil Press Engine Oil Press 3 6 06 1 Oil Check OIL P...

Страница 162: ...dy state until oil temperature is above 15 C END In flight 1 Oil Check OIL T C indication If oil temperature is high 2 PCL Reduce power If oil temperature does not return to normal 3 Landing gear Exte...

Страница 163: ...n ON 5 BUS TIE circuit breaker Electrical Power Management panel Reset If Starter Engaged remains 6 BAT 2 switch OFF 7 GEN 1 switch RESET then ON 8 BAT 1 switch Check ON Note Starter Engaged will rema...

Страница 164: ...n EPECS Fail conditions the system commands flight idle and feathers the propeller The engine continues to provide bleed air for cabin pressurization airframe anti de icing and generator power If engi...

Страница 165: ...Disconnect if active 3 PCL Do not make fast PCL movements 4 Torque If indication is invalid slowly reduce power to idle prior to further engine power changes 10 sec rate from MCP to IDLE If flight co...

Страница 166: ...ed Engine Emergencies This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 6 8 12 C A15 40 0306 00A 141A A F O R G E N E R A L A N D F A M I L I...

Страница 167: ...g and voice callout Fire Possible smoke and or fumes On ground 1 PCL Idle 2 Engine switch OFF 3 ACS EMER shut off PULL 4 FUEL EMER shut off Press latch down and pull lever up 5 Radio Emergency call 6...

Страница 168: ...te Procedure to don the crew oxygen masks 1 Remove the normal headset 2 Put the oxygen mask on 3 Put the smoke goggles on 4 Put the normal headset back on 5 Set MIC SELECT switch on rear left panel to...

Страница 169: ...ngine switch OFF If smoke evacuation is required 13 CABIN PRESSURE switch DUMP When cabin differential pressure is zero 14 DV window Open 15 FANS VENT switch LOW 16 Aircraft Carry out Emergency Descen...

Страница 170: ...nel to MASK 3 Crew Oxygen EMGCY 4 Vent valve if smoke goggles worn OPEN 5 PASSENGER OXYGEN selector ON 6 Systems MFD PAX OXY advisory Confirm ON 7 Passengers Instruct to don masks 8 Aircraft Initiate...

Страница 171: ...ow Open 13 VENT FANS LOW 14 Fire Extinguisher Use if required As soon as time permits and source is known electrical 15 Associated electrical equipment Off circuit breakers Continued on next page Sect...

Страница 172: ...8 BAT 2 switch OFF 19 CABIN HEATER circuit breaker 1 LHPJB PULL If smoke fumes still persist and source is suspected electrical 20 Aircraft Attempt to regain VMC conditions if possible 21 EPS switch C...

Страница 173: ...uspected electrical 24 MASTER POWER switch EMERGENCY OFF Refer to Emergency Gear Extension 3 10 02 END Section 3 Emergency Procedures EASA Approved Fire Smoke or Fumes Pilot s Operating Handbook Repor...

Страница 174: ...ed Fire Smoke or Fumes This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 7 8 12 C A15 40 0307 00A 141X A F O R G E N E R A L A N D F A M I L I...

Страница 175: ...nditions IMC VMC ICING 5 Minimum safe altitude 6 Fuel reserves The pilot must consider the situation and priorities and adjust his actions accordingly END Maximum Range Descent After Engine Fail 3 8 0...

Страница 176: ...he lap belt tightened 6 Main OXYGEN lever Confirm ON 7 Crew oxygen masks Prepare Put on before cabin altitude exceeds 10 000 ft Note Procedure to don the crew oxygen masks 1 Remove the normal headset...

Страница 177: ...ent Adjust to achieve cabin altitude of 10 000 ft before oxygen supply exhausted Below 10 000 ft 14 ACS EMER shut off PULL cabin ventilation 15 Aircraft Carry out Forced Landing 3 9 02 END Maximum Rat...

Страница 178: ...to MASK If cabin altitude exceeds 10 000 ft 7 PASSENGER OXYGEN selector ON Check contents Calculate Oxygen duration 8 Systems MFD PAX OXY advisory Confirm ON 9 Passengers Instruct to don masks CAUTION...

Страница 179: ...XIMUM RATE DESCENT ICN 12 C A150308 A S4080 00002 A 001 01 Figure 3 8 1 Emergency Descent Profiles Section 3 Emergency Procedures EASA Approved Emergency Descent Pilot s Operating Handbook Report No 0...

Страница 180: ...off will not be maintained If Cabin Altitude displayed 1 Aircraft Carry out Cabin Altitude 3 17 03 procedure To cancel EDM for manually flown descent or if Cabin Altitude is NOT displayed and cabin a...

Страница 181: ...d Shedding END Forced Landing 3 9 02 1 PCL IDLE 2 Engine switch OFF 3 FUEL EMERG shut off PULL 4 CABIN PRESSURE switch DUMP 5 Airspeed Best glide speed Airspeed Aircraft Mass 119 KIAS 10450 lb 4740 kg...

Страница 182: ...ding with Main Landing Gear Unlocked 3 9 03 1 Aircraft Confirm landing gear position by control tower or other aircraft CAUTION If one main landing gear is not down it is recommended to land with gear...

Страница 183: ...the aircraft before deficiency is rectified END Landing with Nose Landing Gear Unlocked 3 9 04 1 Fuel weight Reduce 2 Passengers Brief 3 Flaps 40 4 Final approach speed 85 KIAS for 9921 lb 4500 kg Not...

Страница 184: ...ithout Elevator Control 3 9 06 1 Passengers Brief 2 Landing gear Down 3 Flaps 40 4 Final approach speed 90 KIAS 5 Power Set power as necessary to maintain speed and 300 to 500 ft min rate of descent 6...

Страница 185: ...forces END Landing without Flaps 3 9 08 1 Aircraft Proceed as for normal approach 2 Landing gear DOWN 3 Final approach speed 120 KIAS for 9921 lb 4500 kg Not below Dynamic Speed Bug 1 3 VS 4 Landing...

Страница 186: ...tch AUTO CPCS SYSTEM MODE switch MANUAL MANUAL CONTROL switch Set and hold to DESCENT for 30 sec to close OFV 10 FUEL EMERG shut off Press latch down and pull lever up 11 Ditching Ditch with a low rat...

Страница 187: ...n 3 10 02 Incorrect Indication on landing gear indicator lights Red unlocked lights on and or green lights not illuminated 1 Airspeed 120 KIAS 2 Landing Gear Selector Select DN If 3 green lights not i...

Страница 188: ...Landing with Gear Up 3 9 05 END Gear Actuator Cntl 3 10 03 On ground 1 Aircraft Do not take off 2 Aircraft Maintenance required END In flight 1 Landing gear Do not cycle Before landing 2 Airspeed Bel...

Страница 189: ...sential Bus LA2 Check Do not reset unless tripped 2 LDG CTL PRI circuit breaker Essential Bus LB2 Check Do not reset unless tripped 3 LDG GEAR PWR circuit breaker RH PJB Check Do not reset unless trip...

Страница 190: ...nding Gear System Failure This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 3 10 4 12 C A15 40 0310 00A 141A A F O R G E N E R A L A N D F A M I...

Страница 191: ...tted 5 Aircraft Maintenance action required END In flight 1 FLAP circuit breaker LH Rear LP4 Check circuit breaker If tripped 2 FLAP circuit breaker LH Rear LP4 Wait 5 minutes reset circuit breaker ma...

Страница 192: ...osition 30 or greater 2 Aircraft Land as soon as practical with flaps at the failed position 3 Approach For indicated flaps position 12 or greater Approach at approximately 10 knots above AOA based Dy...

Страница 193: ...Flap setting Airspeed KIAS 0 120 15 101 30 90 40 88 WARNING STALLS MUST BE AVOIDED WHEN THE STICK PUSHER IS INOPERATIVE EXCESSIVE WING DROP AND ALTITUDE LOSS MAY RESULT DURING STALL WITH FLAPS DOWN AN...

Страница 194: ...d Stick Pusher Failure This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 12 2 12 C A15 40 0312 00A 141A A F O R G E N E R A L A N D F A M I L...

Страница 195: ...etting Airspeed KIAS 0 120 15 101 30 90 40 88 WARNING NATURAL STALLS ARE NOT PREVENTED WITH THE STICK PUSHER INOPERATIVE STALLS MUST BE AVOIDED WHEN THE STICK PUSHER IS INOPERATIVE EXCESSIVE WING DROP...

Страница 196: ...s LK3 PULL 4 STALL WARN 2 circuit breaker Main Bus RH3 PULL WARNING THE AIRCRAFT IS NOT STALL PROTECTED 5 Airspeed Not below 1 3 VS for 10450 lb 4740 kg Flap setting Airspeed KIAS 0 120 15 101 30 90 4...

Страница 197: ...TUDE LOSS MAY RESULT DURING STALL WITH FLAPS DOWN AND OR WHEN POWER IS APPLIED CAUTION Stall speeds in turns are higher Dynamic speed bug may not be reliable END Section 3 Emergency Procedures EASA Ap...

Страница 198: ...rtent Pusher Shaker Operation This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 13 4 12 C A15 40 0313 00A 141U A F O R G E N E R A L A N D F A...

Страница 199: ...sconnect when TRIM INTERRUPT is operated If main stabilizer trim has failed 8 Pitch trim Use ALTERNATE STAB TRIM END Yaw Trim Runaway 3 14 02 Yaw Trim Runaway warning and voice callout Trim Runaway 1...

Страница 200: ...as failed the autopilot is not operative The autopilot will disconnect when TRIM INTERRUPT is operated END No Main Stabilizer Trim 3 14 04 1 TRIM INTERRUPT Check OFF 2 ALTERNATE STAB TRIM Operate as r...

Страница 201: ...le Do not fly in icing conditions CAUTION There will be no normal landing gear operation Refer to Emergency Gear Extension 3 10 02 Note It is possible to verify the down position of the right main lan...

Страница 202: ...m set to ON 2 AV 2 circuit breaker RH Power Junction Box Confirm set 3 Aircraft At pilots discretion continue flight without services of failed bus or land as soon as practical CAUTION The systems con...

Страница 203: ...r land as soon as practical CAUTION The systems connected to the Generator 1 Bus on the left rear circuit breaker panel are inoperative END Generator 2 Bus 3 15 07 Generator 2 Bus voltage is below 22...

Страница 204: ...At pilots discretion continue flight without services of failed bus or land as soon as practical CAUTION The systems connected to the Non Essential Bus on the right forward circuit breaker panel are...

Страница 205: ...2 switch RESET then ON If generators do not reset Generators remains on 4 Systems MFD ELECTRICAL window Monitor BAT 1 and BAT 2 5 Aircraft Land as soon as possible Do not fly in icing conditions Note...

Страница 206: ...e Propeller de ice LH AOA plate heater RH AOA plate heater VCCS compressor Footwarmer optional system Logo lights optional system Note If further load reduction is desired to extend battery endurance...

Страница 207: ...ms are automatically load shed Cabin heater Under floor heater VCCS compressor Footwarmer optional system Logo lights optional system END Generator 2 Off 3 15 13 Generator 2 is OFF line and engine run...

Страница 208: ...armer optional system Logo lights optional system END Generator 1 Volts 3 15 14 GEN 1 voltage is low or high 1 Systems MFD ELECTRICAL window Confirm the failure 2 GEN 1 switch RESET then ON If Generat...

Страница 209: ...armer optional system Logo lights optional system END Generator 2 Volts 3 15 15 GEN 2 voltage is low or high 1 Systems MFD ELECTRICAL window Confirm the failure 2 GEN 2 switch RESET then ON If Generat...

Страница 210: ...attery 1 2 Hot Battery 2 Hot 3 15 16 Battery temperature is excessive 1 Systems MFD ELECTRICAL window Check battery 1 and 2 charge current If charge current high 2 BAT 1 or BAT 2 switch OFF Do not sel...

Страница 211: ...are normal 2 BAT 1 or BAT 2 switch OFF If indications are not normal 3 Aircraft Carry out Generator 1 Volts 3 15 14 or Generator 2 Volts 3 15 15 procedure END Battery 1 Off Battery 2 Off 3 15 18 1 BA...

Страница 212: ...ectrical System Failures This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 15 12 12 C A15 40 0315 00A 141A A F O R G E N E R A L A N D F A M I...

Страница 213: ...ded A retracted landing gear helps to reduce oil cooling 3 Engine Decrease power to increase fuel temperature 4 Aircraft Descend to warmer air 5 Engine oil temperature Monitor 6 Fuel state imbalance M...

Страница 214: ...as soon as possible If possible always retain glide capability to the selected airfield in case of total engine failure END Fuel PRESS SENS Fail 3 16 02 Fuel PRESS SENS Fail or both FUEL PUMPs on con...

Страница 215: ...round 1 Fuel L and R indications Check for difference WARNING IF THERE ARE 4 SEGMENTS OR MORE DIFFERENCE BETWEEN LEFT AND RIGHT DO NOT TAKE OFF If fuel pump on fuller side is not running 2 FUEL PUMP s...

Страница 216: ...ll the FUEL PUMP CB when Fuel Pressure Low was displayed with a large imbalance 6 Fuel state Monitor 7 Engine parameters Monitor If fuel is balanced 8 FUEL PUMP circuit breakers Essential Bus LJ1 and...

Страница 217: ...eaker on good side Essential Bus LJ1 or LH1 PULL 3 Fuel state Monitor If fuel state is more than 3 segments 4 FUEL PUMP switch on fuller side ON 5 FUEL PUMP switch on leaking side AUTO 6 FUEL PUMP cir...

Страница 218: ...digital Fuel Quantity indication If fuel imbalance is suspected Note To check fuel imbalance disengage the autopilot regularly to check for roll trim changes 2 Aircraft Land as soon as possible END Lo...

Страница 219: ...ial Bus LJ1 or Essential Bus LH1 Reset 3 FUEL PUMP switch on affected side ON After 10 seconds 4 FUEL PUMP switch on affected side AUTO 5 Fuel state Monitor If fuel imbalance with affected pump failed...

Страница 220: ...ssential Bus LH1 PULL 3 Fuel state Monitor If fuel pumps failed OFF 4 Aircraft Land as soon as possible Fuel imbalance correction not possible Note If a prompt landing is not possible keep high IAS to...

Страница 221: ...fuel imbalance 6 Aircraft Carry out Fuel Balance Fault and or Fuel Imbalance 3 16 04 procedure END Fuel IMP Bypass 3 16 11 On ground If engine started with cold fuel below 0 C 1 Oil temperature CHECK...

Страница 222: ...elow 12 C or Fuel Balance Fault 9 Engine Reduce power for balancing approx 300 LB H fuel flow END Fuel Filter Blocked 3 16 12 On ground 1 Engine Shut down 2 Aircraft Maintenance required END In flight...

Страница 223: ...ture 4 Aircraft Descend to warmer air if necessary If indicated fuel temperature remains low less than 12 C 5 CAS Window Check for fuel filter faults If indicated fuel temperature decreases and remain...

Страница 224: ...roved Fuel System This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 16 12 12 C A15 40 0316 00A 141A A F O R G E N E R A L A N D F A M I L I A...

Страница 225: ...adset back on 4 Set MIC SELECT switch on the rear left panel to MASK 8 PASSENGER OXYGEN selector AUTO or ON 9 Systems MFD PAX OXY advisory Confirm ON 10 Passengers Instruct to don masks 11 Aircraft Ca...

Страница 226: ...engers Instruct to don masks 10 Aircraft Carry out Maximum Rate Descent 3 8 03 procedure Prior to landing 11 CABIN PRESSURE switch DUMP if not selected earlier END Cabin Altitude 3 17 03 Note If above...

Страница 227: ...flight altitude to maintain cabin altitude below 10 000 ft If necessary 9 Aircraft Carry out Maximum Rate Descent 3 8 03 procedure Prior to landing 10 CABIN PRESSURE switch DUMP END ACS Low Inflow 3 1...

Страница 228: ...ure When cabin altitude below 10 000 ft 12 CABIN PRESSURE switch DUMP cabin ventilation END CPCS Fault 3 17 05 On ground 1 CPCS MODE switch MANUAL for at least 1 sec then AUTO 2 CAS Check If CPCS Faul...

Страница 229: ...4 Crew oxygen masks ON Note Procedure to don the crew oxygen masks 1 Remove the normal headset 2 Put the oxygen mask on Check 100 3 Put the normal headset back on 4 Set MIC SELECT switch on the rear...

Страница 230: ...Aircraft Descend below 10 000 ft or to minimum safe altitude if higher 7 Aircraft Land as soon as practical Prior to landing 8 CABIN PRESSURE switch DUMP END ECS Fault 3 17 06 1 ECS circuit breaker Es...

Страница 231: ...ocedure to don the crew oxygen masks 1 Remove the normal headset 2 Put the oxygen mask on Check 100 3 Put the normal headset back on 4 Set MIC SELECT switch on the rear left panel to MASK 5 PASSENGER...

Страница 232: ...UMP if not selected earlier END Section 3 Emergency Procedures EASA Approved Cabin Environment Failures Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 3 17 8 12 C A15 40 0317 0...

Страница 233: ...onds 6 PROPELLER switch Maintain ON together with INERT SEP OPEN to maintain PUSHER ICE MODE 7 Aircraft DEPART ICING CONDITIONS to positive SAT atmosphere if possible If propeller vibration occurs 8 P...

Страница 234: ...y in failure status 6 Aircraft DEPART ICING CONDITIONS to positive SAT atmosphere if possible 7 BOOTS switch Set to OFF 8 Aircraft Avoid large or sudden changes in aircraft directional longitudinal an...

Страница 235: ...PERFORMANCE AN INCREASE IN ITT AN INERTIAL SEPARATOR FAILURE DURING OPERATIONS IN FOREIGN OBJECT DAMAGE FOD ENVIRONMENTS MAY CAUSE LONG TERM ENGINE DETERIORATION AND SHOULD BE REPORTED FOR POST FLIGH...

Страница 236: ...ue flight and monitor system If caption stays in failure status and forward visibility through LH windshield is lost 6 Windshield Use RH windshield If total forward visibility is lost 7 Aircraft DEPAR...

Страница 237: ...if possible CAUTION Stick shaker may activate at higher speeds than normal If this occurs increase speed until shaker stops 9 Aircraft Avoid further icing conditions 10 Flap position Limited to 15 11...

Страница 238: ...9 Landing approach Keep speed as indicated by Dynamic Speed Bug 1 3 VS with PUSHER ICE MODE and flaps 15 CAUTION The total landing distance will be longer by up to 71 Refer to Section 5 Performance F...

Страница 239: ...ng Performance for the exact landing distance calculation END Pusher 3 18 09 WARNING A FAILURE OF THE STALL WARNING STICK PUSHER SYSTEM TO RE DATUM TO ICE MODE WHEN IN ICING CONDITIONS CAN LEAVE THE A...

Страница 240: ...ch for 9921 lb 4500 kg MLW Keep minimum landing approach speed above 105 KIAS CAUTION The total landing distance will be longer by up to 71 Refer to Section 5 Performance Flight in Icing Conditions Fl...

Страница 241: ...he deice timer controller allows deactivation of the deice boots in this initial 20 seconds dwell timer before inflation sequence starts this to prevent damage to the pneumatic de ice boots due to inf...

Страница 242: ...oved Deice Systems This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 18 10 12 C A15 40 0318 00A 141A A F O R G E N E R A L A N D F A M I L I A...

Страница 243: ...flight 1 All occupants Check seat lap and shoulder belts are fastened and the lap belt tightened 2 Airspeed Reduce IAS to practical minimum 3 Aircraft Start a slow descent to 10 000 ft or minimum saf...

Страница 244: ...Passenger and Cargo Door This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 19 2 12 C A15 40 0319 00A 141A A F O R G E N E R A L A N D F A M I...

Страница 245: ...fe altitude if higher 4 CPCS SYSTEM MODE AUTO 5 Aircraft Land as soon as practical Note When left hand front winshield is cracked and the visibility impaired use direct vision window for landing END S...

Страница 246: ...Cracked Window in Flight This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 20 2 12 C A15 40 0320 00A 141U A F O R G E N E R A L A N D F A M I...

Страница 247: ...d 1 Landing Taxi Use reverse power BETA and Nose Wheel steering END Section 3 Emergency Procedures EASA Approved Wheel Brake Failure Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 P...

Страница 248: ...d Wheel Brake Failure This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 21 2 12 C A15 40 0321 00A 141U A F O R G E N E R A L A N D F A M I L I...

Страница 249: ...elector AUTO or ON 6 Systems MFD PAX OXY Confirm ON 7 Passengers Instruct to don masks 8 Aircraft Descend below 10 000 ft or to minimum safe altitude if higher If required inform ATC ask for assistanc...

Страница 250: ...formatting If display unit indicates red X or blank 2 Reversion Controller Set DU control knob to OFF REV Note If the MFD swap button is used for DU 2 or 3 the optional single charts can only be acce...

Страница 251: ...itch on the rear left panel to MASK 4 PASSENGER OXYGEN selector AUTO or ON 5 Systems MFD PAX OXY Confirm ON 6 Passengers Instruct to don masks 7 Aircraft Descend below 10 000 ft or to minimum safe alt...

Страница 252: ...s used for DU 2 or 3 the optional single charts can only be accessed on the upper DU 2 not applicable if the Dual Charts option is installed 5 Displays Monitor for remainder of flight END DU 1 2 3 4 O...

Страница 253: ...t Land as soon as practical using minimum engine power to avoid exceeding engine limits Prior to landing 10 CABIN PRESSURE switch DUMP END LH PFD CTRL Fail 3 22 07 1 RH PFD Controller Push PFD button...

Страница 254: ...t PFD data suspect 1 Display Cross check pilot PFD data with copilot PFD data or with Electronic Standby Instrument System ESIS If data confirmed to be suspect 2 Reversion Controller Set pilot PFD con...

Страница 255: ...m ESIS 3 ADHRS pushbutton on PFD Controller Press to bring the other ADAHRS channel data onto PFD END RAD 3 22 14 Radar Altimeter data has become invalid Note Autothrottle does not disconnect automati...

Страница 256: ...e invalid 1 Altitude data Use Electronic Standby Instrument System ESIS 2 ADHRS pushbutton on PFD Controller Press to bring the other ADAHRS channel Altitude data onto PFD END Vertical Speed Replaced...

Страница 257: ...wrong 4 PCL Set maximum cruise power torque and cross check resulting IAS from Max cruise table See Section 5 3 4 Performance Data Cruise Performance against cockpit indications 5 ADAHRS pushbutton on...

Страница 258: ...ilot PFD miscompares more than 6 1 Heading Cross check with the magnetic heading indication on the Electronic Standby Instrument System ESIS 2 ADHRS pushbutton on PFD Controller If required press to b...

Страница 259: ...gle miscompares more than 6 1 Roll Cross check with Electronic Standby Instrument System ESIS Copilot PFD and Pilot PFD 2 ADHRS pushbutton on PFD Controller If required press to bring the other ADAHRS...

Страница 260: ...g LP approach if either Flight Director FD fails both the VNAV Pre Approach Pointer and the Vertical Deviation Pointer will be removed from the Vertical Deviation Information VDI scale scale remains V...

Страница 261: ...MAU Channel B cannot be reset Autopilot Flight Director Yaw Damper and XPDR 2 are not available for remainder of the flight For single FMS installations FMS is not available for the remainder of the f...

Страница 262: ...ker Avionic 1 bus LU1 Reset CAUTION Autopilot performance on coupled approaches will be reduced For autopilot limitations refer to Section 2 Primus Apex Automatic Flight Control System END Rad Alt 1 F...

Страница 263: ...e in additional contingency situations Repeat procedure each hour 6 Air Traffic Control Inform to facilitate a route or an altitude change to exit RVSM airspace Note Pilots should be aware of any nati...

Страница 264: ...mary altimetry systems END ADC A B Fail 3 22 33 Loss of primary altitude and airspeed data 1 Aircraft Use Electronic Standby Instrument System ESIS 2 Altitude Monitor and maintain assigned altitude by...

Страница 265: ...GEN selector AUTO or ON 9 Systems MFD PAX OXY Confirm ON 10 Passengers Instruct to don masks 11 CPCS MODE switch Confirm MANUAL 12 MANUAL CONTROL switch Push intermittently to DESCENT to reduce cabin...

Страница 266: ...ilot PFD window Confirm ADAHRS 1 flag which indicates attitude heading and air data same source as pilot PFD Compare with Standby Instrument System CAUTION The autopilot will revert to roll and pitch...

Страница 267: ...ttitude for 1 minute If realignment is successful 5 PFD Controller Push ADHRS button to select required ADHRS If realignment is not successful 6 Aircraft Land as soon as practical using Standby Instru...

Страница 268: ...oss of RNAV capability Note For dual GPS with a single GPS failure no loss of position will occur With single GPS sensor failed system goes to DEGRADE and then Dead Reckoning DR mode DEGRADE and DR mo...

Страница 269: ...her means of navigation If aircraft is SBAS capable and the GPS shows problems with the GPS GNSS reception 3 SBAS sensor page Swap to systems Select sensor pages on multipurpose window and select GPS...

Страница 270: ...a missed approach if required In flight during RNP operation 8 Aircraft Terminate and revert to other means of navigation In flight during RNAV operation 9 FMS information Cross check with VOR DME and...

Страница 271: ...Set to 121 5 MHz If communication not successful 4 XPDR Set to 7600 and follow national communication loss procedures If all VHF and ADF navigation capabilities are lost 5 Aircraft Continue flight wi...

Страница 272: ...d follow national communication loss procedures If all VHF and ADF navigation capabilities are lost 3 Aircraft Continue flight with FMS GPS END ADS B Out 3 22 48 ADS B Out or removed ADS B Out annunci...

Страница 273: ...1 2 Fail remains 9 Aircraft Proceed according to ATC instructions expect descent below controlled airspace or diversion to next suitable airfield END ASCB Fail 3 22 49 Note By checking available data...

Страница 274: ...back on 4 Set MIC SELECT switch on the rear left panel to MASK 4 PASSENGER OXYGEN selector AUTO or ON 5 Systems MFD PAX OXY Confirm ON 6 Passengers Instruct to don masks 7 Aircraft Descend below 10 00...

Страница 275: ...age switch PRESS to disengage the autopilot pilot or copilot yoke 3 Aircraft RETRIM manually as necessary 4 Aircraft If no AFCS associated CAS messages attempt to re engage autopilot once END CAS Caut...

Страница 276: ...mize side slip do not make abrupt or large rudder or aileron control deflections Keep the slip skid indicator centered to 1 trapezoid CAUTION Above 15 500 ft Fly smoothly and as soon as practical incr...

Страница 277: ...Airplane control wheel and rudder pedals Grasp and position feet to gain aircraft control 2 Aircraft Minimize side slip do not make abrupt or large rudder or aileron control deflections Keep the slip...

Страница 278: ...display Note The main difference is that the drift angle i e difference between aircraft heading and track is not shown The card shows actual track related to True North being made The autopilot will...

Страница 279: ...Mic detection If T is not removed and affected MMDR continues to transmit 2 Affected audio panel Select PA to disconnect PTT to MMDR 3 Other audio panel Use 2nd audio panel 2nd headset and 2nd PTT to...

Страница 280: ...oved APEX Failures This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3 22 32 12 C A15 40 0322 00A 141A A F O R G E N E R A L A N D F A M I L I A...

Страница 281: ...Autopilot Altitude Hold Function in RVSM Airspace 3A 5 1 3A 6 Flight Training 3A 6 1 3A 6 01 Emergency Gear Extension Lever Reset 3A 6 1 3A 7 Smartview 3A 7 1 3A 7 1 Smartview Procedures 3A 7 1 3A 7...

Страница 282: ...es EASA Approved Table of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 3A 0 2 F O R G E N E R A L A N D F A M I L I A R I Z A T I...

Страница 283: ...y effect on flight and where possible any actions that can be taken they are not readily adaptable to a checklist format In addition abnormal procedures are given for the following Primary Altimeter D...

Страница 284: ...pproved General This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3A 1 2 12 C A15 48 0301 00A 010A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 285: ...CSIO A Fail CSIO B Fail CSIO A B Fail Custom I O module A or B or A and B failed A single A or B failure will have no effect on flight an A and B failure will result in some invalid data on PFD MFD wi...

Страница 286: ...o off re engage autopilot ADAHRS reset can only be achieved in stable pitch and no bank condition also only light turbulence Only one reset attempt per flight If the CAS messages stay on or recur trim...

Страница 287: ...B Fail Single channel failure has no effect Dual channel failure results in loss of AP FD YD GPS 1 Fail GPS 2 Fail GPS 1 2 Fail GPS has no satellite signal reception or GPS unit failed If CAS message...

Страница 288: ...NAVAIL Required parameter levels not available leading to loss of Surface Traffic function TERR INHIB Active Terrain Inhibit selected by pilot G S INHIB Active Glide slope inhibited for EGPWF while fl...

Страница 289: ...ot prevent the aircraft from dispatching may impact mechanic s ability to diagnose and repair the aircraft in a timely manner ACMF Logs Full One or more of the Aircraft Condition Monitoring Function A...

Страница 290: ...oved CAS Advisories This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3A 2 6 12 C A15 48 0302 00A 014A A F O R G E N E R A L A N D F A M I L I A...

Страница 291: ...nd Possible Actions FCMU Fault The Fuel Control and Monitoring computer has a fault condition Automatic fuel balancing analog fuel quantity and low level indication may be suspect Low Lvl Sense Fault...

Страница 292: ...file for periodic maintenance analysis Crew Event Store Indicates that a crew initiated event has been recorded LH WOW Fault RH WOW Fault LH RH WOW Fault Indicates that the Modular Avionics Unit MAU h...

Страница 293: ...ates the propeller is feathered for maintenance purposes Wet Motoring Indicates that a wet motoring run is in progress Prop Feather Inhibit Indicates propeller feathering is inhibited during engine sh...

Страница 294: ...proved CAS Status This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 3A 3 4 12 C A15 48 0303 00A 141A A F O R G E N E R A L A N D F A M I L I A R...

Страница 295: ...ncy of primary altimeters If unable to determine accuracy of either altimetry system perform appropriate national RVSM contingency procedures for loss of all primary altimetry systems Note 1 The copil...

Страница 296: ...timeter Diverge by 200 ft or More This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3A 4 2 12 C A15 48 0304 00A 014U A F O R G E N E R A L A N D...

Страница 297: ...is disengaged 2 Altitude Maintain assigned altitude manually 3 Appropriate national RVSM contingency procedure for loss of altitude hold capability Perform END Section 3A Abnormal Procedures EASA Appr...

Страница 298: ...pilot Altitude Hold Function in RVSM Airspace This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3A 5 2 12 C A15 48 0305 00A 141U A F O R G E N E...

Страница 299: ...ear Extension Lever Press black release latch and push red lever down 3 Emergency Gear Extension Lever cover Close END Section 3A Abnormal Procedures EASA Approved Flight Training Pilot s Operating Ha...

Страница 300: ...ved Flight Training This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3A 6 2 12 C A15 48 0306 00A 141U A F O R G E N E R A L A N D F A M I L I A...

Страница 301: ...er X Ptr After approximately 2 5 minutes the SV is displayed automatically and the pilot can reselect the preferred flight director mode on the FCS tab Example Indication Check DU 1 Condition Pilot PF...

Страница 302: ...position integrity error was detected SV FPS SV is selected but not being displayed due to the Flight Path Symbol FPS being invalid SV TER SV is selected but not being displayed due to a terrain rend...

Страница 303: ...played If below LNAV minimum initiate a Go Around and follow published standard missed approach procedure as long as DGRD message is not displayed If DGRD message is displayed avoid obstacles with rem...

Страница 304: ...LPV LP Approach Optional This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3A 8 2 12 C A15 48 0308 00A 141U A F O R G E N E R A L A N D F A M I...

Страница 305: ...le 7 STARTER switch PUSH momentarily less than 2 seconds To crank for a pilot determined amount of time hold the push button for longer than 2 seconds 8 CAS window CHECK Dry Motoring comes on 9 Engine...

Страница 306: ...Section 4 18 Shutdown END Section 3A Abnormal Procedures EASA Approved Engine Dry Motoring Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 3A 9 2 12 C A15 48 0309 00A 141A A F...

Страница 307: ...4 5 Engine Starting 4 5 1 4 5 01 Engine Start With or Without External Power 4 5 1 4 6 Before Taxiing 4 6 1 4 6 01 Before Taxiing 4 6 1 4 7 Taxiing 4 7 1 4 7 01 Taxiing 4 7 1 4 8 Before Takeoff 4 8 1...

Страница 308: ...4 20 01 Oxygen System 4 20 1 4 21 Noise Level 4 21 1 4 22 Automatic Flight Control System Operation 4 22 1 4 23 Crosswind Operation 4 23 1 4 24 Flight in Icing Conditions 4 24 1 4 25 Severe Icing Con...

Страница 309: ...ith these procedures to become proficient in the normal operation of the airplane It is recommended that these procedures be followed for the normal operation of the aircraft When the aircraft has bee...

Страница 310: ...proved General This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 1 2 12 C A15 30 0401 00A 010A A F O R G E N E R A L A N D F A M I L I A R I Z...

Страница 311: ...KIAS Maximum Operating Maneuvering Speed VO 10 450 lb 4740 kg 166 KIAS Maximum Flaps Extended VFE Flaps 15 15 165 KIAS Flaps 30 40 15 130 KIAS Maximum Landing Gear Extension VLO 180 KIAS Retraction V...

Страница 312: ...ed Crosswind for Takeoff and Landing not a limitation Flaps 0 30 kts Flaps 15 25 kts Flaps 30 20 kts Flaps 40 landing only 15 kts Section 4 Normal Procedures EASA Approved Airspeeds for Normal Operati...

Страница 313: ...ensure that no foreign matter is found within the static port orifice 7 Tail tie down DISCONNECTED 8 External Power Door CLOSED AS REQUIRED 9 Oxygen rupture disc INTACT if a larger capacity oxygen sys...

Страница 314: ...Strobe light CHECK CONDITION 2 Fuel quantity and filler cap CHECK and SECURE 3 Pitot probe COVER REMOVED and CHECKED 4 AOA probe COVER REMOVED and CHECK FREE MOVEMENT 5 Wing tie down wheel chocks DIS...

Страница 315: ...4 Propeller De icing Boots CHECK GENERAL CONDITION 5 Propeller Spinner CHECK 6 Air Inlet and Exhaust Covers REMOVED and STOWED 7 Air Inlets CHECK ENGINE AIR INTAKE OIL COOLER ECS and GENERATOR for OB...

Страница 316: ...security may be conducted from the RH cowling 14 General Condition CHECK 15 Cowling LH CHECK and SECURE 16 Windshield CHECK CLEAN END Service Bay left 1 Service Bay Doors CLOSED END Left Wing Leading...

Страница 317: ...nd luggage SECURED STOWED 3 Passenger Seat CHECK backrests in upright position for takeoff and landing 4 Passenger Seat Belts FASTENED 5 Overwing Emergency Exit LOCK PIN REMOVED EXIT CHECKED and LOCKE...

Страница 318: ...SK MIC switch CHECK MIC 14 RH Circuit Breakers CHECK IN 15 TRIM INTERRUPT switch Check OFF 16 FLAP INTERRUPT switch Check NORM GUARDED 17 POWER CONTROL LEVER IDLE DETENT 18 Flap Lever 0 19 Cockpit Ins...

Страница 319: ...T 2 STBY BUS CHECK OFF 31 EXT PWR CHECK CENTER 32 AV 2 BUS CABIN BUS AV 1 BUS GEN 1 GEN 2 CHECK ON END Section 4 Normal Procedures EASA Approved Preflight Inspection Pilot s Operating Handbook Report...

Страница 320: ...Preflight Inspection This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 3 8 12 C A15 30 0403 00A 131A A F O R G E N E R A L A N D F A M I L I...

Страница 321: ...BAT 1 and BAT 2 switches ON 14 Red EPS ON indicator Check OFF 15 BAT 1 and BAT 2 indicators CHECK 24 VDC min External power if available 16 External power unit ON Check 28 VDC 17 External power unit...

Страница 322: ...n pressure gage CHECK 1 850 psi MAX 25 PASSENGER OXYGEN selector AUTO SET switch to OFF if no passengers on board 26 Direct Vision Window CLOSED and LOCKED 27 Radios Avionics SET as required ESIS alig...

Страница 323: ...an engine start if any of the following cases occur ITT exceedance Hung start No light off The starter switch is pushed during the starting sequence In this event the EPECS will immediately command a...

Страница 324: ...ow 50 and the start is not automatically aborted 12 STARTER switch PUSH momentarily If NG stable 13 Starter sequence COMPLETED 14 Engine instruments STABLE in green range 15 GEN 1 and GEN 2 Check volt...

Страница 325: ...2 sec Break for 1 sec Pusher Shaker CHECK correct operation 11 ICE PROTECTION PUSHER ICE MODE advisory CHECK ON When pusher operates 12 PUSHER INTR switch control wheel PRESS and HOLD check pusher in...

Страница 326: ...er is calculated based on displayed T1 END Section 4 Normal Procedures EASA Approved Before Taxiing Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 6 2 12 C A15 30 0406 00A 13...

Страница 327: ...N Do not leave the PCL stationary for more than 30 seconds in the beta range aft of idle detent to avoid an EPECS Degraded message on the CAS window Note If operating conditions allow use the beta ran...

Страница 328: ...proved Taxiing This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 7 2 12 C A15 30 0407 00A 131A A F O R G E N E R A L A N D F A M I L I A R I Z...

Страница 329: ...If greater than 30 amps is indicated delay takeoff until indications are at or below 30 amps 8 Flight controls FULL FREE and CORRECT 9 Radios Navigation FD clearance SET and checked 10 Departure and...

Страница 330: ...ved Before Takeoff This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 8 2 12 C A15 30 0408 00A 131A A F O R G E N E R A L A N D F A M I L I A R...

Страница 331: ...uments MONITOR Torque ITT Ng Oil Temp Pressure 4 Aircraft Rotate at VR initial climb at VX or VY as required After lift off and positive rate of climb 5 Brakes PRESS to stop wheel rotation 6 Landing G...

Страница 332: ...proved Takeoff This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 9 2 12 C A15 30 0409 00A 131A A F O R G E N E R A L A N D F A M I L I A R I Z...

Страница 333: ...OOTS ON and 3 MIN or 1 MIN as required Note A deice boots failure indication can occur at low power settings while in high pressure altitudes Refer to De Ice Boots 3 18 02 Emergency Procedure for syst...

Страница 334: ...airframe ice 7 PROP Maintain ON 8 INERT SEP Maintain OPEN Note This ensures that the stick shaker pusher system is maintained in PUSHER ICE MODE 9 BOOTS ON and 3 MIN or 1 MIN as required 10 LH and RH...

Страница 335: ...MONITOR max 825 9 Ng MONITOR max 104 When passing transition altitude 10 Baro SET STD and cross check CAUTION If autothrottle is installed and engaged and FD AP is set to OFF monitor for engine torqu...

Страница 336: ...pproved Climb This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 11 2 12 C A15 30 0411 00A 131A A F O R G E N E R A L A N D F A M I L I A R I Z...

Страница 337: ...heck altimeters Maximum differences 200 feet 1 2 Altimeters Record indicated altitudes 2 3 Autopilot Altitude Hold Verify altitude hold within 65 feet 3 Note 1 Ensure matched altimeter baro settings S...

Страница 338: ...proved Cruise This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 12 2 12 C A15 30 0412 00A 131A A F O R G E N E R A L A N D F A M I L I A R I Z...

Страница 339: ...and confirm correct 5 CPCS system window CHECK landing field elevation set 6 Passengers Brief 7 Passenger Warning Switches if installed ON END Section 4 Normal Procedures EASA Approved Descent Pilot...

Страница 340: ...proved Descent This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 13 2 12 C A15 30 0413 00A 131A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 341: ...Note If the optional TAWS Class A or RAAS are installed activate FLAP OVRD for approaches and landing where flap settings are intentionally at less than 40 to avoid an aural flaps annunciation during...

Страница 342: ...DISENGAGED use red AP QD button on the yoke Note For minimum Autopilot heights refer to Systems and Equipment Limits For crosswind information refer to Airspeeds for Normal Operations and Section 5 P...

Страница 343: ...peed Boot failure 130 KIAS 6 Landing Gear Selector Up with positive rate of climb 7 Yaw Damper ON 8 Flaps Normal AS REQUIRED Flaps With residual airframe ice Maintain at 15 Flaps Boot failure Maintain...

Страница 344: ...lked Landing Go Around This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 15 2 12 C A15 30 0415 00A 131A A F O R G E N E R A L A N D F A M I L...

Страница 345: ...Aircraft Touch down main wheels first 2 Aircraft Do not flare with high pitch angle 3 Power Control Lever REVERSE 4 Braking FIRM 5 Power Control Lever IDLE END Section 4 Normal Procedures EASA Approve...

Страница 346: ...proved Landing This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 16 2 12 C A15 30 0416 00A 131A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 347: ...rotections switches OFF or as required 5 Transponder STBY or check GND 6 WX Radar STBY END Section 4 Normal Procedures EASA Approved After Landing Pilot s Operating Handbook Report No 02406 Issue date...

Страница 348: ...ved After Landing This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 17 2 12 C A15 30 0417 00A 131A A F O R G E N E R A L A N D F A M I L I A R...

Страница 349: ...ake SET PEDALS PUSH 3 ICE PROTECTION switches OFF 4 Inertial Separator OPEN if operating on unprepared surface 5 Feather Inhibit switch if installed PUSH and HOLD if desired refer to note Note After 9...

Страница 350: ...ec minimum after shutdown CHECK Refill engine with an approved oil 13 CPCS CHECK cabin depressurized 14 STBY BUS switch OFF 15 EPS switch OFF 16 Battery 1 and 2 switches OFF 17 Crew oxygen masks CHECK...

Страница 351: ...ler anchor is properly installed to prevent possible engine damage due to windmilling with zero oil pressure Note Make sure that the rudder nose wheel is centered 5 Propeller Anchor INSTALLED 6 Extern...

Страница 352: ...proved Parking This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 19 2 12 C A15 30 0419 00A 131A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 353: ...apacity to obtain the available oxygen duration in minutes 0 500 1 000 1 500 2 000 2 500 02 GAGE PRESSURE PSIG 10 20 30 40 50 60 70 80 PERCENT OF USEABLE CAPACITY OXYGEN AVAILABLE WITH PARTIALLY FULL...

Страница 354: ...70 42 47 24 2 47 32 35 21 3 35 26 28 18 4 28 22 23 16 5 23 19 20 14 6 20 17 17 13 7 17 15 16 12 8 16 13 14 11 9 14 12 13 10 Table 4 20 2 Oxygen Duration with Full Bottle Large Capacity Oxygen System N...

Страница 355: ...ask on Oxygen Duration Pax plus 2 Crew Mask on Diluter Demand min 100 min Diluter Demand min 100 min 6 68 57 57 44 7 57 51 54 41 8 54 44 47 37 9 47 41 44 34 END Section 4 Normal Procedures EASA Approv...

Страница 356: ...ved Oxygen System This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 20 4 12 C A15 30 0420 00A 131A A F O R G E N E R A L A N D F A M I L I A R...

Страница 357: ...ade by EASA FOCA for the FAA that the noise levels of this airplane are or should be acceptable or unacceptable for operation at into or out of any airport ICAO Annex 16 Chapter 10 77 0 dB A Swiss VEL...

Страница 358: ...oved Noise Level This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 21 2 12 C A15 30 0421 00A 131A A F O R G E N E R A L A N D F A M I L I A R...

Страница 359: ...lected PFD left right At power up the default setting is L pilot side PFD A brief description of the AFCS is given in Section 7 of this POH Refer to the Pilot s Guide for the Advanced Cockpit Environm...

Страница 360: ...Flight Control System Operation This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 22 2 12 C A15 30 0422 00A 131A A F O R G E N E R A L A N D F...

Страница 361: ...rated crosswind for takeoff and landing for all flap configurations is shown in Section 4 2 Airspeeds for Normal Operations For further information on crosswind operation refer to Section 10 3 Operati...

Страница 362: ...Crosswind Operation This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 23 2 12 C A15 30 0423 00A 131A A F O R G E N E R A L A N D F A M I L I...

Страница 363: ...be shed and it may seriously degrade performance and control of the aircraft Flight in severe icing conditions should be avoided as this may exceed the capabilities of the aircraft ice protection sys...

Страница 364: ...ng Go Around Flaps 15 LG down Pusher Ice Mode 105 Balked Landing Go Around Boot failure Flaps 0 LG down Pusher Ice Mode 130 Flight in icing conditions is only permitted with full operational status of...

Страница 365: ...s fails when selected then either the CAS caption Pitot 1 Heat or Pitot 2 Heat will be illuminated and an aural gong will sound If the static ports fail a CAS Static Heat caption will be illuminated a...

Страница 366: ...le and unprotected areas of the aircraft are observed as being free of ice This protects the engine from possible ice ingestion and maintains the stick shaker pusher computer in PUSHER ICE MODE theref...

Страница 367: ...red severe icing you should apply the procedures as given in Section 4 Normal Procedures Severe Icing Conditions In case of a balked landing go around after an icing encounter the climb speeds defined...

Страница 368: ...ght in Icing Conditions This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 24 6 12 C A15 30 0424 00A 131A A F O R G E N E R A L A N D F A M I L...

Страница 369: ...8 degrees Celsius increased vigilance is warranted at temperatures around freezing with visible moisture present If the visual cues specified in Section 2 Limitations Icing Limitations for identifying...

Страница 370: ...evere Icing Conditions This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 25 2 12 C A15 30 0425 00A 131A A F O R G E N E R A L A N D F A M I L...

Страница 371: ...altitude will increase to maintain max Dp The following Table gives the aircraft altitude for a selected LFE from which upwards the maximum pressure differential of 5 75 psid will be reached and main...

Страница 372: ...Low Cabin Mode Operation This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 4 26 2 12 C A15 30 0426 00A 131A A F O R G E N E R A L A N D F A M I...

Страница 373: ...ntrol Device CCD or Touch Screen Controller TSC rotary knobs MF Controller scroll wheel to set the brightness ICN 12 C A150427 A S4080 00393 A 001 01 Figure 4 27 1 PFD OVRLY Menu Note When pointing di...

Страница 374: ...ction and Brightness Control This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 4 27 2 12 C A15 30 0427 00A 131A A F O R G E N E R A L A N D F A...

Страница 375: ...indicator will appear on PFD If the FAF is the active waypoint or the present position is within 5 nm from the FAF the vertical deviation pointer right hand side of the vertical deviation scale will b...

Страница 376: ...age autopilot below 200ft 4 28 3 Flight Director Autopilot Coupled Operation The LPV LP approach mode can be armed via the APR button on the Flight Guidance Panel as soon as the vertical deviation poi...

Страница 377: ...5 4 1 Flight in Icing Conditions 5 4 1 1 5 4 1 Flight in Icing Conditions General 5 4 1 1 5 4 2 Flight in Icing Conditions Flaps 5 4 2 1 5 4 3 Flight in Icing Conditions Stall Speeds 5 4 3 1 5 4 4 Fli...

Страница 378: ...ASA Approved Table of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 5 0 2 F O R G E N E R A L A N D F A M I L I A R I Z A T I O N P...

Страница 379: ...All performance data is limited to between the 55 C 67 F and 50 C 122 F outside air temperature limits Some tables presented in this section show data for temperatures below 55 C 67 F which is purely...

Страница 380: ...versa are given in Section 1 Conversion Information Section 5 Performance EASA Approved General Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 2 12 C A15 60 0501 00A 030A A...

Страница 381: ...FAHRENHEIT 34 F DEGREES CELSIUS 1 C ICN 12 C A150501 A S4080 00235 A 001 01 Figure 5 1 1 Performance Fahrenheit to Celsius Conversion Section 5 Performance EASA Approved Standard Tables Pilot s Opera...

Страница 382: ...rmance ISA Conversion Section 5 Performance EASA Approved Standard Tables Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 4 12 C A15 60 0501 00A 030A A F O R G E N E R A L A...

Страница 383: ...S Gallons to Liters Conversion Section 5 Performance EASA Approved Standard Tables Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 5 12 C A15 60 0501 00A 030A A F O R G E N...

Страница 384: ...ce Feet to Meters Converion Section 5 Performance EASA Approved Standard Tables Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 6 12 C A15 60 0501 00A 030A A F O R G E N E R...

Страница 385: ...Pounds to Kilograms Conversion Section 5 Performance EASA Approved Standard Tables Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 7 12 C A15 60 0501 00A 030A A F O R G E N...

Страница 386: ...ches to Millimeters Conversion Section 5 Performance EASA Approved Standard Tables Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 8 12 C A15 60 0501 00A 030A A F O R G E N...

Страница 387: ...mance Wind Components Section 5 Performance EASA Approved Standard Tables Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 9 12 C A15 60 0501 00A 030A A F O R G E N E R A L A...

Страница 388: ...nce Airspeed Calibration Section 5 Performance EASA Approved Standard Tables Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 10 12 C A15 60 0501 00A 030A A F O R G E N E R A...

Страница 389: ...ce Altimeter Correction Section 5 Performance EASA Approved Standard Tables Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 11 12 C A15 60 0501 00A 030A A F O R G E N E R A...

Страница 390: ...Standard Tables This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 1 12 12 C A15 60 0501 00A 030A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 391: ...1 01 Figure 5 3 1 1 Performance Stall Speeds KIAS Flight Idle Power standard units Section 5 Performance EASA Approved Performance Data Stall Speeds Pilot s Operating Handbook Report No 02406 Issue da...

Страница 392: ...2 Performance Stall Speeds KIAS Flight Idle Power metric units Section 5 Performance EASA Approved Performance Data Stall Speeds Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page...

Страница 393: ...1 Performance Static Takeoff Torque Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 2 1 12 C A15 60...

Страница 394: ...OR OPERATION HAS NO EFFECT ON TORQUE DE ICE ANTI ICE SYSTEMS CAN REDUCE TORQUE BY 0 5 PSI P R E S S U R E A L T I T U D E F T 6000 8000 MAX OAT LIMIT MIN OAT LIMIT 10000 2000 40 10 ICN 12 C A150503 A...

Страница 395: ...erformance Accelerate Stop Distance Flaps 30 standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 P...

Страница 396: ...Performance Accelerate Stop Distance Flaps 30 metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pa...

Страница 397: ...5 Performance Takeoff Ground Roll Flaps 30 standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pag...

Страница 398: ...6 Performance Takeoff Ground Roll Flaps 30 metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page...

Страница 399: ...rformance Takeoff Ground Roll Flaps 30 ACS OFF standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020...

Страница 400: ...erformance Takeoff Ground Roll Flaps 30 ACS OFF metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020...

Страница 401: ...Performance Takeoff Total Distance Flaps 30 standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pa...

Страница 402: ...Performance Takeoff Total Distance Flaps 30 metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pag...

Страница 403: ...ormance Takeoff Total Distance Flaps 30 ACS OFF standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 202...

Страница 404: ...formance Takeoff Total Distance Flaps 30 ACS OFF metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020...

Страница 405: ...erformance Accelerate Stop Distance Flaps 15 standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 P...

Страница 406: ...Performance Accelerate Stop Distance Flaps 15 metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pa...

Страница 407: ...5 Performance Takeoff Ground Roll Flaps 15 standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pag...

Страница 408: ...16 Performance Takeoff Ground Roll Flaps 15 metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page...

Страница 409: ...rformance Takeoff Ground Roll Flaps 15 ACS OFF standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020...

Страница 410: ...erformance Takeoff Ground Roll Flaps 15 ACS OFF metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020...

Страница 411: ...Performance Takeoff Total Distance Flaps 15 standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pa...

Страница 412: ...Performance Takeoff Total Distance Flaps 15 metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pag...

Страница 413: ...ormance Takeoff Total Distance Flaps 15 ACS OFF standard units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 202...

Страница 414: ...formance Takeoff Total Distance Flaps 15 ACS OFF metric units Section 5 Performance EASA Approved Performance Data Takeoff Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020...

Страница 415: ...1 Performance Maximum Climb Torque Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 1 12 C A15 60 05...

Страница 416: ...2 Performance Maximum Rate Of Climb Flaps 30 standard units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pag...

Страница 417: ...3 Performance Maximum Rate Of Climb Flaps 30 metric units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page...

Страница 418: ...4 Performance Maximum Rate Of Climb Flaps 15 standard units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pag...

Страница 419: ...5 Performance Maximum Rate Of Climb Flaps 15 metric units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page...

Страница 420: ...6 Performance Maximum Rate Of Climb Flaps 0 standard units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page...

Страница 421: ...limb Flaps 0 metric units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 7 12 C A15 60 0503 03A 030...

Страница 422: ...uise Climb standard units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 8 12 C A15 60 0503 03A 030...

Страница 423: ...ruise Climb metric units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 9 12 C A15 60 0503 03A 030A...

Страница 424: ...uise Climb standard units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 10 12 C A15 60 0503 03A 03...

Страница 425: ...ruise Climb metric units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 11 12 C A15 60 0503 03A 030...

Страница 426: ...Cruise Climb standard units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 12 12 C A15 60 0503 03A...

Страница 427: ...Cruise Climb metric units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 13 12 C A15 60 0503 03A 0...

Страница 428: ...Cruise Climb standard units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 14 12 C A15 60 0503 03A...

Страница 429: ...Cruise Climb metric units Section 5 Performance EASA Approved Performance Data Climb Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 15 12 C A15 60 0503 03A 0...

Страница 430: ...Data Climb Performance This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 3 16 12 C A15 60 0503 03A 030A A F O R G E N E R A L A N D F A M I...

Страница 431: ...ormance Maximum Cruise Power Sheet 1 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 1 12 C A1...

Страница 432: ...e Power Sheet 2 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 2 12 C A15 60 0503 04A 030A A...

Страница 433: ...e Power Sheet 3 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 3 12 C A15 60 0503 04A 030A A...

Страница 434: ...e Power Sheet 4 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 4 12 C A15 60 0503 04A 030A A...

Страница 435: ...Cruise Sheet 1 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 5 12 C A15 60 0503 04A 030A A F...

Страница 436: ...Cruise Sheet 2 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 6 12 C A15 60 0503 04A 030A A F...

Страница 437: ...Cruise Sheet 3 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 7 12 C A15 60 0503 04A 030A A F...

Страница 438: ...Cruise Sheet 4 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 8 12 C A15 60 0503 04A 030A A F...

Страница 439: ...Maximum Endurance Cruise Sheet 1 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 9 12 C A15 60...

Страница 440: ...aximum Endurance Cruise Sheet 2 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 10 12 C A15 60...

Страница 441: ...aximum Endurance Cruise Sheet 3 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 11 12 C A15 60...

Страница 442: ...aximum Endurance Cruise Sheet 4 of 4 Section 5 Performance EASA Approved Performance Data Cruise Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 4 12 12 C A15 60...

Страница 443: ...ance Specific Air Range 7000 lb Sheet 1 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 1 12 C...

Страница 444: ...ge 7000 lb Sheet 2 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 2 12 C A15 60 0503 05A 030A...

Страница 445: ...ge 7000 lb Sheet 3 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 3 12 C A15 60 0503 05A 030A...

Страница 446: ...ge 8000 lb Sheet 1 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 4 12 C A15 60 0503 05A 030A...

Страница 447: ...ge 8000 lb Sheet 2 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 5 12 C A15 60 0503 05A 030A...

Страница 448: ...ge 8000 lb Sheet 3 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 6 12 C A15 60 0503 05A 030A...

Страница 449: ...ge 9000 lb Sheet 1 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 7 12 C A15 60 0503 05A 030A...

Страница 450: ...ge 9000 lb Sheet 2 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 8 12 C A15 60 0503 05A 030A...

Страница 451: ...ge 9000 lb Sheet 3 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 9 12 C A15 60 0503 05A 030A...

Страница 452: ...e 10 000 lb Sheet 1 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 10 12 C A15 60 0503 05A 03...

Страница 453: ...e 10 000 lb Sheet 2 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 11 12 C A15 60 0503 05A 03...

Страница 454: ...e 10 000 lb Sheet 3 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 12 12 C A15 60 0503 05A 03...

Страница 455: ...e 10 400 lb Sheet 1 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 13 12 C A15 60 0503 05A 03...

Страница 456: ...e 10 400 lb Sheet 2 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 14 12 C A15 60 0503 05A 03...

Страница 457: ...e 10 400 lb Sheet 3 of 3 Section 5 Performance EASA Approved Performance Data Specific Air Range Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 15 12 C A15 60 0503 05A 03...

Страница 458: ...Data Specific Air Range This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 5 16 12 C A15 60 0503 05A 030A A F O R G E N E R A L A N D F A M...

Страница 459: ...1 Performance Holding Time and Fuel Section 5 Performance EASA Approved Performance Data Holding Time and Fuel Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 6 1 12 C A15 6...

Страница 460: ...Data Holding Time and Fuel This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 6 2 12 C A15 60 0503 06A 030A A F O R G E N E R A L A N D F A M...

Страница 461: ...00 FPM AIRSPEED MACH 0 48 OR 240 KIAS WHICHEVER IS LOWER TIME TO DESCEND ALTITUDE FT ICN 12 C A150503 A S4080 00316 A 001 01 Figure 5 3 7 1 Performance Time to Descend Section 5 Performance EASA Appro...

Страница 462: ...escend standard units Section 5 Performance EASA Approved Performance Data Descend Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 7 2 12 C A15 60 0503 07A 030A...

Страница 463: ...Descend metric units Section 5 Performance EASA Approved Performance Data Descend Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 7 3 12 C A15 60 0503 07A 030A A...

Страница 464: ...ce to Descend Section 5 Performance EASA Approved Performance Data Descend Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 7 4 12 C A15 60 0503 07A 030A A F O R...

Страница 465: ...rmance Power off Glide Time standard units Section 5 Performance EASA Approved Performance Data Power off Glide Performance Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 5 3 8...

Страница 466: ...ime metric units Section 5 Performance EASA Approved Performance Data Power off Glide Performance Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 5 3 8 2 12 C A15 60 0503 08A 03...

Страница 467: ...rformance Power off Glide Distance Section 5 Performance EASA Approved Performance Data Power off Glide Performance Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 5 3 8 3 12 C...

Страница 468: ...a Power off Glide Performance This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 5 3 8 4 12 C A15 60 0503 08A 030A A F O R G E N E R A L A N D F...

Страница 469: ...1 Performance Balked Landing Torque Section 5 Performance EASA Approved Performance Data Balked Landing Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 9 1 12 C...

Страница 470: ...rformance Rate Of Climb Balked Landing standard units Section 5 Performance EASA Approved Performance Data Balked Landing Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020...

Страница 471: ...erformance Rate Of Climb Balked Landing metric units Section 5 Performance EASA Approved Performance Data Balked Landing Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 P...

Страница 472: ...a Balked Landing Performance This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 3 9 4 12 C A15 60 0503 09A 030A A F O R G E N E R A L A N D F A...

Страница 473: ...01 01 Figure 5 3 10 1 Performance Landing Total Distance Flaps 40 standard units Section 5 Performance EASA Approved Performance Data Landing Performance Pilot s Operating Handbook Report No 02406 Iss...

Страница 474: ...Performance Landing Total Distance Flaps 40 metric units Section 5 Performance EASA Approved Performance Data Landing Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pag...

Страница 475: ...3 Performance Landing Ground Roll Flaps 40 standard units Section 5 Performance EASA Approved Performance Data Landing Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Pag...

Страница 476: ...4 Performance Landing Ground Roll Flaps 40 metric units Section 5 Performance EASA Approved Performance Data Landing Performance Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page...

Страница 477: ...ding Total Distance with the use of Reverse Thrust Flaps 40 standard units Section 5 Performance EASA Approved Performance Data Landing Performance Pilot s Operating Handbook Report No 02406 Issue dat...

Страница 478: ...nding Total Distance with the use of Reverse Thrust Flaps 40 metric units Section 5 Performance EASA Approved Performance Data Landing Performance Pilot s Operating Handbook Report No 02406 Issue date...

Страница 479: ...nding Ground Roll with the use of Reverse Thrust Flaps 40 standard units Section 5 Performance EASA Approved Performance Data Landing Performance Pilot s Operating Handbook Report No 02406 Issue date...

Страница 480: ...anding Ground Roll with the use of Reverse Thrust Flaps 40 metric units Section 5 Performance EASA Approved Performance Data Landing Performance Pilot s Operating Handbook Report No 02406 Issue date M...

Страница 481: ...utes holding in moderate icing conditions with ice accretion on the total airframe due to inoperative pneumatic de ice boots Besides these aerodynamic degradations performance losses to the aircraft s...

Страница 482: ...Icing Conditions General This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 4 1 2 12 C A15 60 0504 01A 030A A F O R G E N E R A L A N D F A M I...

Страница 483: ...ition is limited to a maximum of 15 When operating in or into known icing conditions with failed operational pneumatic de ice boots the flap position is limited to a maximum of 0 Section 5 Performance...

Страница 484: ...Icing Conditions Flaps This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 4 2 2 12 C A15 60 0504 02A 030A A F O R G E N E R A L A N D F A M I...

Страница 485: ...um takeoff weight of 10450 lb 4740 kg and with flight idle power are summarized in Table 5 4 3 1 Table 5 4 3 1 Stall Speeds in accordance with ICE Mode Set FLAPS STALL SPEED PUSHER ACTIVATION AT MTOW...

Страница 486: ...ng Conditions Stall Speeds This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 4 3 2 12 C A15 60 0504 03A 030A A F O R G E N E R A L A N D F A M...

Страница 487: ...reduced by up to 2 2 psi in non icing conditions and up to 2 8 psi in icing conditions Section 5 Performance EASA Approved Flight in Icing Conditions Engine Torque Pilot s Operating Handbook Report No...

Страница 488: ...ng Conditions Engine Torque This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 4 4 2 12 C A15 60 0504 04A 030A A F O R G E N E R A L A N D F A...

Страница 489: ...orrecting that distance for takeoff in or into known icing conditions by using the corrections in Table 5 4 5 1 Table 5 4 5 2 and Table 5 4 5 3 Icing correction A B C Note Due to the increased referen...

Страница 490: ...Correction Table B Table B Takeoff Weight kg lb Wind Correction 2900 4740 6393 10450 10 kts Tailwind 3 No Wind 0 10 kts Headwind 1 20 kts Headwind 3 30 kts Headwind 5 Table 5 4 5 3 Icing Corrections t...

Страница 491: ...Fig 5 3 2 18 ACS OFF metric units by using the corrections in Table 5 4 5 4 Table 5 4 5 5 and Table 5 4 5 6 Icing correction A B C Section 5 Performance EASA Approved Flight in Icing Conditions Takeof...

Страница 492: ...Correction Table B Table B Takeoff Weight kg lb Wind Correction 2900 4740 6393 10450 10 kt Tailwind 4 No Wind 0 10 kt Headwind 2 20 kt Headwind 5 30 kt Headwind 8 Table 5 4 5 6 Icing Corrections to T...

Страница 493: ...ing Correction A B C 28 5 1 6 0 5 30 6 Takeoff Ground Roll in Icing Conditions 300 m 1 306 392 m Section 5 Performance EASA Approved Flight in Icing Conditions Takeoff Performance Pilot s Operating Ha...

Страница 494: ...Conditions Takeoff Performance This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 5 4 5 6 12 C A15 60 0504 05A 030A A F O R G E N E R A L A N D F...

Страница 495: ...ance in non icing conditions from Fig 5 3 2 13 standard units Fig 5 3 2 14 metric units and then correcting that distance for takeoff in or into known icing conditions by using the corrections in Tabl...

Страница 496: ...n Table B Table B Takeoff Weight kg lb Wind Correction 2900 4740 6393 10450 10 kts Tailwind 3 No Wind 0 10 kts Headwind 2 20 kts Headwind 3 30 kts Headwind 5 Table 5 4 6 3 Icing Corrections to Acceler...

Страница 497: ...its and then correcting the Rate of Climb in or into known icing conditions by using the corrections in Table 5 4 7 2 with operational pneumatic de ice boots or Table 5 4 7 3 with the pneumatic de ice...

Страница 498: ...0 30000 1940 1600 1210 1150 Example Pressure Altitude 5000 ft Outside Air Temperature 10 C Aircraft Weight 3800 kg Rate of Climb non icing 2400 fpm from Fig 5 3 3 7 Icing Correction 982 fpm interpolat...

Страница 499: ...l Flow Correction Altitude ft Aircraft Weight kg lb 2900 4740 6393 10450 0 29 5000 33 10000 37 15000 45 Table 5 4 8 2 Icing Conditions to Holding Fuel Flow with Pneumatic De ice Boots Inoperative Fuel...

Страница 500: ...Conditions Holding Endurance This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 4 8 2 12 C A15 60 0504 08A 030A A F O R G E N E R A L A N D F...

Страница 501: ...0 150 110 80 14000 150 110 80 After failure of the airframe pneumatic boots in icing conditions a balked landing climb is performed with Flaps 0 and a climb speed of 130 KIAS The total climb performan...

Страница 502: ...onditions Balked Rate of Climb This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 4 9 2 12 C A15 60 0504 09A 030A A F O R G E N E R A L A N D F...

Страница 503: ...Distance Fig 5 3 10 1 Fig 5 3 10 2 Table 5 4 10 2 A Table 5 4 10 3 B Table 5 4 10 4 C Landing Ground Roll Fig 5 3 10 3 Fig 5 3 10 4 Table 5 4 10 5 A Table 5 4 10 6 B Table 5 4 10 7 C Inoperative Flap...

Страница 504: ...Correction Table Landing Ground Roll Fig 5 3 10 5 Fig 5 3 10 6 Table 5 4 10 23 A Table 5 4 10 24 B Table 5 4 10 25 C Section 5 Performance EASA Approved Flight in Icing Conditions Landing Performance...

Страница 505: ...tion Table B Table B Landing Weight kg lb Wind Correction 2900 6393 3300 7275 3700 8157 4100 9039 4500 9921 10 kt Tailwind 5 5 5 5 5 No Wind 0 0 0 0 0 10 kt Headwind 3 3 3 3 3 20 kt Headwind 6 6 6 6 6...

Страница 506: ...on Table B Table B Landing Weight kg lb Wind Correction 2900 6393 3300 7275 3700 8157 4100 9039 4500 9921 10 kt Tailwind 7 7 6 5 5 No Wind 0 0 0 0 0 10 kt Headwind 6 5 4 4 4 20 kt Headwind 14 11 9 9 8...

Страница 507: ...ing Weight kg lb Wind Correction 2900 6393 3300 7275 3700 8157 4100 9039 4500 9921 10 kt Tailwind 12 11 11 11 11 No Wind 0 0 0 0 0 10 kt Headwind 7 6 6 6 6 20 kt Headwind 15 14 14 13 13 30 kt Headwind...

Страница 508: ...nding Weight kg lb Wind Correction 2900 6393 3300 7275 3700 8157 4100 9039 4500 9921 10 kt Tailwind 13 12 11 10 10 No Wind 0 0 0 0 0 10 kt Headwind 12 10 9 8 8 20 kt Headwind 26 22 19 18 17 30 kt Head...

Страница 509: ...aps 15 With Reverse Thrust Wind Correction Table B Table B Landing Weight kg lb Wind Correction 2900 4500 6393 9921 10 kt Tailwind 5 No Wind 0 10 kt Headwind 3 20 kt Headwind 6 30 kt Headwind 11 Table...

Страница 510: ...ion Table B Table B Landing Weight kg lb Wind Correction 2900 6393 3300 7275 3700 8157 4100 9039 4500 9921 10 kt Tailwind 7 7 7 6 6 No Wind 0 0 0 0 0 10 kt Headwind 5 5 4 4 4 20 kt Headwind 12 10 9 8...

Страница 511: ...ction Table B Table B Landing Weight kg lb Wind Correction 2900 6393 3300 7275 3700 8157 4100 9039 4500 9921 10 kt Tailwind 13 13 14 14 9 No Wind 0 0 0 0 0 10 kt Headwind 6 6 6 6 6 20 kt Headwind 14 1...

Страница 512: ...rrection Table B Table B Landing Weight kg lb Wind Correction 2900 6393 3300 7275 3700 8157 4100 9039 4500 9921 10 kt Tailwind 14 13 13 13 12 No Wind 0 0 0 0 0 10 kt Headwind 11 9 8 8 7 20 kt Headwind...

Страница 513: ...lable field length at the departure airport Apply the departure airport conditions to the Takeoff Power Chart to determine maximum torque to be applied before brake release 5 5 1 3 Climb Note The clim...

Страница 514: ...the destination airport to sea level Subtract the values for the destination airport from those for the cruise altitude The remaining values are the time fuel and distance to descend from the cruise...

Страница 515: ...the calculated aircraft weight to the appropriate landing performance charts and check that the corresponding distances are less than the available field length at the destination airport 5 5 1 7 Tota...

Страница 516: ...t Planning Example This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 5 5 1 4 12 C A15 60 0505 00A 043A A F O R G E N E R A L A N D F A M I L I A...

Страница 517: ...l Loading Recommendations 6 7 1 6 7 1 General 6 7 1 6 7 2 Cargo 6 7 1 6 7 3 Hazardous Materials 6 7 1 6 7 4 Maximum Allowable Weight Per Single Container Without Special Equipment 6 7 3 6 8 Interior C...

Страница 518: ...ce EASA Approved Table of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 6 0 2 F O R G E N E R A L A N D F A M I L I A R I Z A T I O...

Страница 519: ...formance will also be affected Loads that the aircraft was not designed for may be put on the structure particularly during landing The pilot should routinely determine the balance of the aircraft sin...

Страница 520: ...pproved General This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 6 1 2 12 C A15 30 0601 00A 010A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 521: ...in the neutral position 6 Place crew seats in the center position and make sure the cabin passenger seats are in the correct positions Refer to the relevant Interior Configuration Code Seat Location...

Страница 522: ...ations for Airplane Weighing This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 6 2 2 12 C A15 30 0602 00A 169A A F O R G E N E R A L A N D F A M...

Страница 523: ...ulate the arm of the nose gear A from the extension of the nose gear strut a using the table in Fig 6 3 2 Sheet 2 If the extension of the nose gear strut a is in between two values in the table the ar...

Страница 524: ...t Main Landing Gear Nose Landing Gear TOTAL AIRCRAFT WEIGHT R L N ICN 12 C A150603 A S4080 00142 A 001 01 Figure 6 3 1 Airplane Weighing Form Section 6 Weight and Balance EASA Approved Weighing Pilot...

Страница 525: ...7 2826 160 111 19 2824 180 111 07 2821 200 110 99 2819 220 110 91 2817 240 110 79 2814 Dimension a is strut extension NOSE GEAR ARM a ICN 12 C A150603 A S4080 00143 A 001 01 Figure 6 3 2 Airplane Weig...

Страница 526: ...In or m N x A L R x B T A Nose Landing gear arm B Main Landing gear arm N Nose Landing gear weight L Left main landing gear weight R Right main landing gear weight T Total weight of N L R Where ICN 12...

Страница 527: ...level across the seat tracks Place the level along the top of the inboard seat track and adjust the tail jack until the airplane is longitudinally level Refer to Section 8 Levelling of this Handbook f...

Страница 528: ...T 3 Adjust weight and moment for unusable fuel and optional equipment installed after airplane weighing to determine airplane Total Basic Empty Weight and Moment 4 Calculate Basic Empty Weight C G 5...

Страница 529: ...in Jacking Point Right Main Jacking Point T L R TOTAL AIRCRAFT WEIGHT ICN 12 C A150604 A S4080 00145 A 001 01 Figure 6 4 1 Airplane Weighing Form Section 6 Weight and Balance EASA Approved Weighing Pi...

Страница 530: ...if applicable 6 TOTAL BASIC EMPTY WEIGHT AND MOMENT Sum of 1 thru 5 lb kg lb kg lb kg Ramp Weight Ramp Weight Useful Load AIRPLANE USEFUL LOAD NORMAL CATEGORY OPERATION ICN 12 C A150604 A S4080 00146...

Страница 531: ...and registration number shown Refer to Fig 6 6 1 Weight and Balance Record when modifications to the airplane have been made Section 6 Weight and Balance EASA Approved Weighing Pilot s Operating Hand...

Страница 532: ...proved Weighing This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 6 4 6 12 C A15 30 0604 00A 169A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 533: ...ight and Moment of the airplane to determine the Zero Fuel Weight and Moment Divide the moment by the weight to determine the c g arm Locate this point in the C G Envelope Fig 6 5 3 If the point falls...

Страница 534: ...ple EX 6S 2 Conversion Seat 5 6 removed Frame 27 Cargo Net installed ITEM WEIGHT LB KG MOMENT LB IN KG M Passenger Seat 5 60 09 27 26 19764 40 227 70 Passenger Seat 6 60 09 27 26 20485 50 236 00 Frame...

Страница 535: ...0451 240 38465 Arm for center position only Adjust arm 0 69 inch for each hole from center position Maximum seat travel is 4 holes or 2 76 inches from center position Table 6 5 3 Moment Chart Crew Occ...

Страница 536: ...Moment Chart Rear Baggage Area Moments Standard Net at Frame 34 met ric REAR BAGGAGE AREA MOMENTS KG M STANDARD NET AT FRAME 34 ARM 9 420 M WEIGHT Kg MOMENT Kg m WEIGHT Kg MOMENT Kg m WEIGHT Kg MOMEN...

Страница 537: ...7 Moment Chart Rear Baggage Area Moments Extendable Net at Frame 32 metric REAR BAGGAGE AREA MOMENTS KG M EXTENDABLE NET AT FRAME 32 ARM 9 17 M WEIGHT Kg MOMENT Kg m WEIGHT Kg MOMENT Kg m WEIGHT Kg MO...

Страница 538: ...AD MOMENTS KG M WEIGHT Kg MOMENT Kg m WEIGHT Kg MOMENT Kg m WEIGHT Kg MOMENT Kg m WEIGHT Kg MOMENT Kg m 50 286 64 400 2337 14 750 4419 61 1100 6497 53 100 573 59 450 2635 13 800 4717 33 1150 6793 90 1...

Страница 539: ...ff Weight MTOW 10450 lb Sum of 19 23 ITEM WEIGHT lb ARM AFT OF DATUM in MOMENT lb in 5613 NA 170 170 170 170 170 170 170 170 170 170 170 215 225 16 NA 160 27 160 27 210 35 207 35 243 35 240 35 276 35...

Страница 540: ...u 18 20 Fuel 21 Ramp Weight MRW 10495 lb 4760 kg Sum of 19 20 22 Less Fuel for Ground Operations 23 Fuel at Takeoff Sum of 20 22 24 Takeoff Weight MTOW 10450 lb 4740 kg Sum of 19 23 ITEM WEIGHT lb ARM...

Страница 541: ...EIGHT MLW 9921 lb 10500 MAX TAKEOFF WEIGHT MTOW 10450 lb ICN 12 C A150605 A S4080 00168 A 001 01 Figure 6 5 3 C G Envelope Sheet 1 of 2 Section 6 Weight and Balance EASA Approved Combi Conversion Pilo...

Страница 542: ...740 kg 4500 MAX LANDING WEIGHT MLW 4500 kg ICN 12 C A150605 A S4080 00169 A 001 01 Figure 6 5 3 C G Envelope Sheet 2 of 2 Section 6 Weight and Balance EASA Approved Combi Conversion Pilot s Operating...

Страница 543: ...luded in the Basic Empty Weight indicated in the Airplane Basic Empty Weight figure Fig 6 4 2 of this Airplane Flight Manual Section 6 Weight and Balance EASA Approved Equipment List Pilot s Operating...

Страница 544: ...ved Equipment List This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 6 5 12 12 C A15 30 0605 00A 169A A F O R G E N E R A L A N D F A M I L I A...

Страница 545: ...Basic Empty Weight or Total Moment must be entered in Fig 6 6 1 Weight and Balance Record The last entry on the Weight and Balance Record will be the current airplane Basic Empty Weight and Total Mom...

Страница 546: ...lb kg Moment lb in 1000 mkg As Delivered ICN 12 C A150606 A S4080 00147 A 001 01 Figure 6 6 1 Weight and Balance Record Sheet 1 of 2 Section 6 Weight and Balance EASA Approved Weight and Balance Reco...

Страница 547: ...mkg Wt lb kg Moment lb in 1000 mkg ICN 12 C A150606 A S4080 00148 A 001 01 Figure 6 6 1 Weight and Balance Record Sheet 2 of 2 Section 6 Weight and Balance EASA Approved Weight and Balance Records Pi...

Страница 548: ...ight and Balance Records This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 6 6 4 12 C A15 30 0606 00A 169A A F O R G E N E R A L A N D F A M I L...

Страница 549: ...10 Fig 6 7 11 and Fig 6 7 12 for cargo weight calculation restraining bar installation and tie down strap installation Refer to Fig 6 7 13 for cargo net installation Refer to the Illustrated Parts Cat...

Страница 550: ...GAGE AREA CROSS SECTION PASSENGER DOOR 44 25 1 13 m 34 8 0 88 m HEIGHT WIDTH 4 5 1 35 m 2 0 0 61 m CARGO DOOR HEIGHT WIDTH 4 4 1 32 m 4 5 1 35 m COMPARTMENT VOLUME WITHIN DIMENSIONED AREAS CABIN BAGGA...

Страница 551: ...Figure 6 7 2 Cargo Dimensions The process to decide whether and how cargo can be tied down follows the following 4 steps 1 Determine the cargo size and orientation 2 Determine the correct restraint ba...

Страница 552: ...h the heavier end to the rear 2 Heavier cargo items should be placed in front of lighter ones Go to Step Two NO Cargo Width 20 Width C g in central 20 of Width Max 67 height Heavier end of cargo is pl...

Страница 553: ...aircraft Step Two Cargo width between 22 5 and 33 between 570 mm and 840 mm Use a single long Restraint Bar 525 25 12 073 or 525 25 12 172 or 525 25 12 277 in the centre of the aircraft ICN 12 C A1506...

Страница 554: ...charts for cargo straddling 4 seat rails Figure 6 12 or 6 14 YES mid height or below above mid height Use High Centre of Gravity Cargo curve Step Three MAXIMUM ALLOWABLE WEIGHT PER SINGLE CONTAINER WI...

Страница 555: ...argo is acceptable Cargo is too heavy to transport contact Pilatus for advice NO NO NO Step Four MAXIMUM ALLOWABLE WEIGHT PER SINGLE CONTAINER WITHOUT SPECIAL EQUIPMENT ICN 12 C A150607 A S4080 00154...

Страница 556: ...0 as shown in Fig 6 7 7 Additional straps may be placed laterally on cargo straddling the centre two seat rails if desired 10 TO ICN 12 C A150607 A S4080 00155 A 001 01 20 Figure 6 7 7 Fore aft Strap...

Страница 557: ...S4080 00155 A 001 01 Figure 6 7 8 Maximum Allowable Weight Per Single Container Without Special Equipment Section 6 Weight and Balance EASA Approved Maximum Allowable Weight Per Single Container With...

Страница 558: ...and curve 3 1 The front stop is attached to 4 seat rails but cargo tie down straps can only be fitted to the inner seat tracks This cargo straddles 2 seat rails The restraining Bars are angle shaped...

Страница 559: ...0 75 1 1 25 0 Weight lbf 100 Weight kg 150 100 50 250 300 350 200 300 400 500 600 700 CARGO SECURED LONGITUDINALLY TO FOUR SEAT RAILS Max 660 lb 300 kg CARGO TOO HEAVY LIMIT NORMAL CARGO LIMIT HIGH CE...

Страница 560: ...100 Weight kg 150 100 50 250 300 350 200 300 400 500 600 700 CARGO SECURED LONGITUDINALLY TO FOUR SEAT RAILS CARGO TOO HEAVY LIMIT NORMAL CARGO 400 450 800 900 LIMIT HIGH CENTER OF GRAVITY CARGO CARG...

Страница 561: ...ATTACHMENT FITTINGS EXTENDABLE LUGGAGE NET FRAME 32 CARGO NET ICN 12 C A150607 A S4080 00161 A 001 01 Figure 6 7 13 Cargo and Luggage Restraint Installation Section 6 Weight and Balance EASA Approved...

Страница 562: ...Per Single Container Without Special Equipment This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 6 7 14 12 C A15 30 0607 00A 169A A F O R G E N...

Страница 563: ...e sure that any modification work or SB s are identified for embodiment The placard must then be changed to show the correct code for the new configuration It is possible for aircraft with the executi...

Страница 564: ...SEAT TRACK LOCATING HOLE SEAT TRACK SEAT TRACK ICN 12 C A150608 A S4080 00401 A 001 01 Figure 6 8 1 Interior Configurations First Seat Track Locating Hole Section 6 Weight and Balance EASA Approved G...

Страница 565: ...ings weight and moment chart standard and metric units passenger seat occupant moment charts standard and metric units All distances on the passenger seat locating chart are based on the first seat tr...

Страница 566: ...ISTANCE FROM CENTER OF FIRST SEAT TRACK LOCATING HOLE FUSELAGE STATION PAX 9 26 00 0 660 m 59 00 1 499 m 92 00 2 337 m 125 00 3 175 m 158 00 4 013 m 209 13 5 312 m 242 13 6 150 m 275 13 6 988 m 308 13...

Страница 567: ...3 6795 78 29 PASS SEAT 3 31 6 14 3 7933 91 40 PASS SEAT 4 31 6 14 3 7838 90 30 PASS SEAT 5 31 6 14 3 8975 103 41 PASS SEAT 6 31 6 14 3 8881 102 32 PASS SEAT 7 31 6 14 3 10018 115 42 PASS SEAT 8 31 6 1...

Страница 568: ...36762 40722 130 27345 26955 31635 31245 35925 35535 40215 39825 44115 140 29449 29029 34069 33649 38689 38269 43309 42889 47509 150 31552 31102 36502 36052 41452 41002 46402 45952 50902 160 33655 3317...

Страница 569: ...505 78 560 26 70 374 00 368 66 432 67 427 34 491 34 486 01 550 02 544 68 603 36 75 400 71 395 00 463 58 457 86 526 44 520 73 589 31 583 59 646 46 80 427 42 421 33 494 48 488 38 561 54 555 44 628 59 6...

Страница 570: ...weight and moment chart standard and metric units passenger seat occupant moment charts standard and metric units All distances on the passenger seat locating chart are based on the first seat track...

Страница 571: ...ACING SEAT CENTER OF ARRESTING PIN B B B DISTANCE FROM CENTER OF FIRST SEAT TRACK LOCATING HOLE DISTANCE FROM CENTER OF FIRST SEAT TRACK LOCATING HOLE 0 00 0 000 m CABIN SEAT LOCATION IS DEFINED AS TH...

Страница 572: ...Furnishings Weight and Moment Chart ITEM WEIGHT lb kg MOMENT lb in kg m PASS SEAT 1 OR 2 56 28 25 53 12682 9 146 1 PASS SEAT 3 OR 4 57 71 26 18 16327 188 1 PASS SEAT 5 57 71 26 18 18981 6 218 7 PASS...

Страница 573: ...425 36745 120 27867 33125 38645 40085 130 30189 35886 41866 43426 140 32511 38646 45086 46766 150 34834 41406 48306 50106 160 37156 44167 51527 53447 170 39478 46927 54747 56787 180 41800 49688 57968...

Страница 574: ...383 4 455 7 531 7 551 5 70 412 9 490 8 572 6 593 9 75 442 4 525 9 613 5 636 4 80 471 9 560 9 654 4 678 8 85 501 4 596 0 695 3 721 2 90 530 9 631 0 736 2 763 6 95 560 4 666 1 777 1 806 0 100 589 9 701...

Страница 575: ...ed passenger seat Part Numbers that can be installed passenger seats and furnishings weight and moment chart standard and metric units passenger seat occupant moment charts standard and metric units A...

Страница 576: ...IN SEAT LOCATION IS DEFINED AS THE DISTANCE FROM THE CENTER OF THE FIRST SEAT TRACK LOCATING HOLE TO THE CENTER OF THE ARRESTING PIN ON EACH SEAT CENTER OF ARRESTING PIN B B FWD ICN 12 C A150608 A S40...

Страница 577: ...ngs Weight and Moment Chart ITEM WEIGHT lb kg MOMENT lb in kg m PASS SEAT 1 OR 2 56 28 25 53 12682 9 146 1 PASS SEAT 3 OR 4 57 71 26 18 16327 0 188 1 PASS SEAT 5 OR 6 57 71 26 18 18173 68 209 4 PASS S...

Страница 578: ...33885 37405 120 27867 33125 36965 40805 130 30189 35886 40046 44206 140 32511 38646 43126 47606 150 34834 41406 46206 51006 160 37156 44167 49287 54407 170 39478 46927 52367 57807 180 41800 49688 5544...

Страница 579: ...65 383 4 455 7 508 6 561 4 70 412 9 490 8 547 7 604 6 75 442 4 525 9 586 8 647 8 80 471 9 560 9 625 9 691 0 85 501 4 596 0 665 1 734 2 90 530 9 631 0 704 2 777 3 95 560 4 666 1 743 3 820 5 100 589 9...

Страница 580: ...seat location chart permitted passenger seat Part Numbers that can be installed passenger seats and furnishings weight and moment chart passenger seat occupant moments standard and metric units All di...

Страница 581: ...ENTER OF ARRESTING PIN CABIN SEAT LOCATION IS DEFINED AS THE DISTANCE FROM THE CENTER OF THE FIRST SEAT TRACK LOCATING HOLE TO THE CENTER OF THE ARRESTING PIN ON EACH SEAT NOTE ICN 12 C A150608 A S408...

Страница 582: ...S 02415 6 8 5 3 Passenger Seats and Furnishings Weight and Moment Chart Table 6 8 14 EX 6S STD 2S Passenger Seats and Furnishings Weight and Moment Chart ITEM WEIGHT lb kg MOMENT lb in kg m PASS SEAT...

Страница 583: ...4844 27724 30361 100 23222 27604 30804 33735 110 25545 30365 33885 37108 120 27867 33125 36965 40482 130 30189 35886 40046 43855 140 32511 38646 43126 47229 150 34834 41406 46206 50602 160 37156 44167...

Страница 584: ...65 383 4 455 7 508 6 557 0 70 412 9 490 8 547 7 599 8 75 442 4 525 9 586 8 642 6 80 471 9 560 9 625 9 685 5 85 501 4 596 0 665 1 728 3 90 530 9 631 0 704 2 771 2 95 560 4 666 1 743 3 814 0 100 589 9...

Страница 585: ...seat location chart permitted passenger seat Part Numbers that can be installed passenger seats and furnishings weight and moment chart passenger seat occupant moments standard and metric units All di...

Страница 586: ...NTER OF ARRESTING PIN CABIN SEAT LOCATION IS DEFINED AS THE DISTANCE FROM THE CENTER OF THE FIRST SEAT TRACK LOCATING HOLE TO THE CENTER OF THE ARRESTING PIN ON EACH SEAT NOTE DISTANCE FROM CENTER OF...

Страница 587: ...MS 02415 6 8 6 3 Passenger Seats and Furnishings Weight and Moment Chart Table 6 8 18 EX 4S STD 4S Passenger Seats and Furnishings Weight and Moment Chart ITEM WEIGHT lb kg MOMENT lb in kg m PASS SEAT...

Страница 588: ...4844 27571 30541 100 23222 27604 30635 33935 110 25545 30365 33698 37328 120 27867 33125 36762 40722 130 30189 35886 39825 44115 140 32511 38646 42889 47509 150 34834 41406 45952 50902 160 37156 44167...

Страница 589: ...778 1 861 9 105 619 3 736 2 817 0 905 0 110 648 8 771 3 855 9 948 1 115 678 3 806 3 894 8 991 2 120 707 8 841 4 933 7 1034 3 6 8 7 No Cabin Interior Configuration 6 8 7 1 General The No Cabin Interior...

Страница 590: ...urnishings Weight and Moment Chart ITEM WEIGHT lb kg MOMENT lb in kg m FR 24 CARGO NET 3 6 1 65 941 10 96 FR 27 CARGO NET 3 6 1 65 941 10 96 FR 34 BAGGAGE NET 5 13 2 325 1341 15 44 Section 6 Weight an...

Страница 591: ...General 7 4 1 7 4 2 Description 7 4 1 7 4 3 Electromechanical Actuators 7 4 2 7 4 4 Indication Warning 7 4 2 7 4 5 Emergency Extension System 7 4 5 7 4 6 Air Ground System 7 4 9 7 4 7 Brakes 7 4 9 7 4...

Страница 592: ...l 7 10 11 7 10 6 Oil 7 10 11 7 10 7 Starting 7 10 14 7 10 8 Ignition 7 10 15 7 10 9 Accessories 7 10 15 7 10 10 Fire Detection 7 10 15 7 10 11 Automatic Limiting and Recovery 7 10 16 7 10 12 Engine In...

Страница 593: ...16 1 Description 7 16 1 7 16 2 Operation 7 16 1 7 17 Cabin Pressure Control System 7 17 1 7 17 1 General 7 17 1 7 17 2 Description 7 17 1 7 17 3 Operation 7 17 2 7 17 4 Indication Warning 7 17 5 7 18...

Страница 594: ...4 Combi Cargo Interior 7 24 2 7 25 Emergency Locator Transmitter 7 25 1 7 25 1 Kannad Integra ELT and ENAV Unit 7 25 1 7 25 2 Low Frequency Underwater Locator Beacon ULB if installed 7 25 2 7 26 Primu...

Страница 595: ...29 7 7 29 8 Distance Measuring Equipment DME 7 29 8 7 29 9 Transponder XPDR 7 29 8 7 29 10 Global Navigation Satellite Sensor Unit GNSSU 7 29 9 7 29 11 HF Communications System 7 29 17 7 29 12 Aerowav...

Страница 596: ...toring System ACMS 7 34 1 7 34 1 General 7 34 1 7 35 Primus APEX Aircraft Diagnostic and Maintenance System ADMS 7 35 1 7 35 1 General 7 35 1 7 35 2 Description 7 35 1 7 35 3 Maintenance Data Download...

Страница 597: ...l LPV LP Approach 7 39 1 7 39 1 General 7 39 1 7 39 2 Description 7 39 1 7 39 3 Pilot s Display 7 39 2 7 40 Lightweight Data Recorder If Installed 7 40 1 7 40 1 Description 7 40 1 7 40 2 Operation 7 4...

Страница 598: ...tems Description Table of Contents This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Dec 18 2020 Page 7 0 8 F O R G E N E R A L A N D F A M I L I A R I Z A T I O...

Страница 599: ...rt passengers cargo or various combinations of both passengers and cargo Section 7 Airplane and Systems Description General Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 7 1 1...

Страница 600: ...ription General This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 7 1 2 12 C A15 00 0701 00A 010A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 601: ...running the length of the center cabin and are accessible through quick release panels The cabin carry through spar attachment fittings are one piece machined aluminum Fuselage fairings are construct...

Страница 602: ...and associated linkages The wing trailing edges above the flaps are foam core covered with carbon laminate while the flap fairings are a carbon laminate with nomex honeycomb reinforcement strips A su...

Страница 603: ...They move in the opposite direction to the ailerons The left aileron trim tab is also operated electrically from the cockpit Refer to Trim system for more information 7 3 3 Elevator The elevator is a...

Страница 604: ...pped by lifting the switch guard and pressing the TRIM INTR switch located in front of the Engine Control quadrant on the center console 7 3 6 Flaps Each wing trailing edge has a single piece Fowler t...

Страница 605: ...ap screw actuators If a failure is detected the FCWU disconnects the power to the PDU and the CAS window will show a Flaps caution Additionally if flap asymmetry or twist is detected and the flap angl...

Страница 606: ...valid flap condition or status related to the flap position will be shown by an amber cross If the airspeed goes above the maximum limit for the current flap setting the Flight Alerting System FAS wil...

Страница 607: ...D HOZN STAB TRIM SWITCH TRIM ENGAGE SWITCH CONTROL WHEEL AILERON AND HOZN STAB TRIM SWITCH ICN 12 C A150703 A S4080 00003 A 002 01 Yaw Trim Runaway FLAP INTERUPT FLAP INTR NORM Figure 7 3 1 Flight Con...

Страница 608: ...n Indication Warning This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 7 3 6 12 C A15 00 0703 00A 043A A F O R G E N E R A L A N D F A M I L I A...

Страница 609: ...Proximity switches give the up or down signal to the Modular Avionics Unit MAU Both main landing gear are trailing link types A hydraulic fluid and nitrogen filled shock strut connects the trailing l...

Страница 610: ...with an electrical spring loaded solenoid which prevents it from moving to the retracted position when the airplane is on the ground The airplane on ground status is sensed by the MAU An emergency ge...

Страница 611: ...ith white box outline Grey UP with grey box outline White UP in red box Black DN with green background White hatched lines with black background White hatched lines with red background ICN 12 C A15070...

Страница 612: ...he Electric Landing Gear System Gear Actuator Cntl Indicates a failure reported by one of the landing gear actuators Gear should not be cycled unnecessarily Gear can be lowered if it is raised Mainten...

Страница 613: ...hree green indicators banking the airplane left and right to use the G load may assist the emergency extension of the main landing gear Reducing airspeed and engine power to reduce aerodynamic load ma...

Страница 614: ...1 FAULT 2 ENABLE UP DOWN COMMAND PRI UP DOWN STATUS SEC UP DOWN STATUS ACTUATOR POWER 30 SECONDS MLG CABLE ASSY ICN 12 C A150704 A S4080 00004 A 002 01 Figure 7 4 2 Landing Gear System Sheet 1 of 3 S...

Страница 615: ...LDG GEAR IND CB LDG EMERG REL POS CB LDG CTL PRI CB LDG CTL SEC CB EMERGENCY LANDING GEAR RELEASE ICN 12 C A150704 A S4080 00005 A 001 01 Figure 7 4 2 Landing Gear System Sheet 2 of 3 Section 7 Airpla...

Страница 616: ...GEAR HANDLE ENABLE LDG GEAR GEAR HANDLE UP LH GEAR UP GIO CHB GIO CHA ICN 12 C A150704 A S4080 00006 A 001 01 Figure 7 4 2 Landing Gear System Sheet 3 of 3 Section 7 Airplane and Systems Description...

Страница 617: ...rmination When the MAU determines that all monitors disagree it results in an invalid AIR GND state If the AIR GND state is invalid a Air Ground Fail will be shown on the CAS When Air Ground Fail show...

Страница 618: ...blies have steel friction surfaces and three retractors The retractors pull the pressure plate back when no hydraulic pressure is applied to the brake assembly When the system is pressurized and the r...

Страница 619: ...flation valve and an overinflation safety plug The main wheels have fairings on the outer hubs which make the wheels aerodynamically smooth when the landing gear is retracted Section 7 Airplane and Sy...

Страница 620: ...BRAKE VALVE SHOWN WITH PARKING BRAKE NOT SET PARKING BRAKE VALVE SHOWN WITH PARKING BRAKE SET KEY RESERVOIR BRAKE FLUID LEFT BRAKE SYSTEM RIGHT BRAKE SYSTEM ICN 12 C A150704 A S4080 00007 A 001 01 Fig...

Страница 621: ...can be installed instead of the standard net to secure baggage in front of and in the baggage compartment The floor attachments at the front of the net can be moved between Frames 32 and 34 Section 7...

Страница 622: ...ription General This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 7 5 2 12 C A15 00 0705 00A 043A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 623: ...center lever Tie down straps can be secured to these anchor points Section 7 Airplane and Systems Description Cargo Tie Downs Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 7...

Страница 624: ...ription General This Page Intentionally Left Blank Pilot s Operating Handbook Report No 02406 Issue date Mar 06 2020 Page 7 6 2 12 C A15 00 0706 00A 043A A F O R G E N E R A L A N D F A M I L I A R I...

Страница 625: ...assenger seats have a reclining backrest sliding headrest a folding inner armrest and a restraint system The executive seats are leather upholstered with swivel and forward rear inboard travel Seat tr...

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