Pilatus PC-12 NGX Pilot's Information Manual
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Pilatus PC-12 NGX Pilot's Information Manual

2001 and up
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PILOT'S INFORMATION MANUAL
PC-12/47E MSN 2001 AND UP

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Questions and answers

Steven
June 24, 2025

What would cause a epecs degraded message in the cas after engine start

0
DOMINIQUE AMPHIMAQUE
February 7, 2025

Good morning, I would like to know if the stick pusher/shaker on the PC12 NGX is inhibited on approach

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Summary of Contents for Pilatus PC-12 NGX

  • Page 1 PILOT‘S INFORMATION MANUAL PC-12/47E MSN 2001 AND UP...
  • Page 2 P .O. Box 992 6371 Stans, Switzerland Phone +41 41 619 67 00 +41 41 619 92 30 Certified to EN 9100/ISO 14001 standards info@pilatus-aircraft.com This Approval may be extended or withdrawn in writing by Pilatus at any time www.pilatus-aircraft.com...
  • Page 5 Table of Contents Front Matter Table of Contents Subject Page List of Effective Data Modules FM-1-1 Change Highlights FM-2-1 Log of Revisions FM-3-1 Issue 002 - Revision 00 - Dated: 14 October 2019 FM-3-1 Issue 003 - Revision 00 - Dated: 06 March 2020 FM-3-1 Issue 003 - Revision 01 - Dated: 18 December 2020 FM-3-1...
  • Page 6 Table of Contents This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page FM-0-2...
  • Page 7 List of Effective Data Modules List of Effective Data Modules All DMC are preceded with 12-C but for clarity this has been left out C = Changed data module N = New data module Data module code (DMC) Document title Issue date A15-00-0000-00A-002A-A List of Effective Data Modules...
  • Page 8 List of Effective Data Modules Data module code (DMC) Document title Issue date A15-40-0303-00A-141U-A Rejected Takeoff (Not engine related) 06.03.2020 A15-40-0304-00A-141U-A Engine Failure 18.12.2020 A15-40-0305-00A-141U-A Air Start 06.03.2020 A15-40-0306-00A-141A-A Engine Emergencies 06.03.2020 A15-40-0307-00A-141X-A Fire, Smoke or Fumes 06.03.2020 A15-40-0308-00A-141U-A Emergency Descent 06.03.2020 A15-40-0309-00A-141U-A Emergency Landing...
  • Page 9 List of Effective Data Modules Data module code (DMC) Document title Issue date A15-30-0415-00A-131A-A Balked Landing (Go-Around) 06.03.2020 A15-30-0416-00A-131A-A Landing 06.03.2020 A15-30-0417-00A-131A-A After Landing 06.03.2020 A15-30-0418-00A-131A-A Shutdown 06.03.2020 A15-30-0419-00A-131A-A Parking 06.03.2020 A15-30-0420-00A-131A-A Oxygen System 06.03.2020 A15-30-0421-00A-131A-A Noise Level 06.03.2020 A15-30-0422-00A-131A-A Automatic Flight Control System 06.03.2020 Operation...
  • Page 10 List of Effective Data Modules Data module code (DMC) Document title Issue date A15-60-0504-07A-030A-A Flight in Icing Conditions - Maximum 06.03.2020 Rate of Climb A15-60-0504-08A-030A-A Flight in Icing Conditions - Holding 06.03.2020 Endurance A15-60-0504-09A-030A-A Flight in Icing Conditions - Balked 06.03.2020 Rate of Climb A15-60-0504-10A-030A-A...
  • Page 11 List of Effective Data Modules Data module code (DMC) Document title Issue date A15-00-0726-00A-010A-A Primus APEX - Avionics Installation 06.03.2020 General A15-00-0727-00A-043A-A Primus APEX 06.03.2020 A15-00-0728-00A-043A-A Primus APEX - Attitude and Heading 06.03.2020 A15-00-0729-00A-043A-A Primus APEX - Communication and 06.03.2020 Navigation A15-00-0730-00A-043A-A Primus APEX - Situation Awareness...
  • Page 12 List of Effective Data Modules Data module code (DMC) Document title Issue date A15-20-1005-00A-043A-A Removal of Snow, Ice and Frost from 06.03.2020 the Aircraft A15-20-1006-00A-043A-A Operations from Prepared Unpaved 06.03.2020 Surfaces A15-20-1007-00A-043A-A Passenger Briefings 06.03.2020 * Authority Approved Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page FM-1-6...
  • Page 13 Change Highlights Change Highlights This change highlights section shows all changes to PC-12 Pilot’s Operating Handbook (POH) (No.02406), Issue 003 Revision 01, Dated 18 December 2020. All DMC are preceded with 12-C but for clarity this has been left out C = Changed data module.
  • Page 14 Change Highlights Data module code Type Reason for Update (RFU) Document title * A15-30-0427-00A-131A-A 21514 - Changed "SYS BRT" to "SVS BRT" SV Selection and Brightness (editorial). Control * A15-60-0503-08A-030A-A 21514 - Power-off Glide Distance graph X-axis Performance Data - Power-off updated (editorial).
  • Page 15 Log of Revisions Log of Revisions Issue 002 - Revision 00 - Dated: 14 October 2019 Re-issue of the PC-12/47E Pilot’s Operating Handbook to include technical changes and conversion of the manual to a new layout. The Issue 002 Revision 00 of the AFM ref. 02406 is approved under EASA approval number 10071186.
  • Page 16 Issue 003 - Revision 01 - Dated: 18 December 2020 Table 1-1-3: Issue 003 - Revision 01 - List of changes (continued from previous page) Section PTS Number Description of Change List of APEX 21999 Incorporated TR-11. Builds Remove and destroy TR 11 and record the removal in the Log of Temporary Revisions.
  • Page 17 Log of Temporary Revisions Log of Temporary Revisions Temporary Revision Title Date of Cancelled by Issue Fuel Anti-Icing Additive 28 Nov 2019 Issue 003 Revision 00 APEX Builds 10 Dec 2019 Issue 003 Revision 00 EX-6S-2 Placards 10 Dec 2019 Issue 003 Revision 00 Emergency Gear Extension 06 Dec 2019...
  • Page 18 Log of Temporary Revisions Temporary Revision Title Date of Cancelled by Issue Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page FM-4-2...
  • Page 19 List of Service Bulletins List of Service Bulletins This list of Service Bulletins provides the owner a means of recording the applicable SBs that are mentioned in the various Sections of the POH. It is not a complete list 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.
  • Page 20 List of Service Bulletins SB No. SB Title Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page FM-5-2...
  • Page 21 List of Service Bulletins SB No. SB Title Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page FM-5-3...
  • Page 22 List of Service Bulletins SB No. SB Title Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page FM-5-4...
  • Page 23 List of APEX Builds List of APEX Builds An overview of the various APEX builds, the corresponding Honeywell part number and the associated Electronic Checklist (ECL) version is given in the table below. APEX Build Honeywell part ECL version number ECL software number version Build 12...
  • Page 24 List of APEX Builds APEX Build Honeywell part ECL version number ECL software number version Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page FM-6-2...
  • Page 25 Section 0 - Introduction Table of Contents SECTION 0 Introduction Table of Contents Subject Page Introduction 0-1-1 General 0-1-1 Warnings, Cautions, and Notes 0-1-1 Data Modules 0-1-1 Revision Markings 0-1-1 Revision / Issue Dates 0-1-1 Revision Procedure 0-1-2 Supplements 0-1-3 Copyright and Legal Statement 0-1-3 Pilot's Operating Handbook...
  • Page 26 Section 0 - Introduction Table of Contents This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 0-0-2...
  • Page 27 To facilitate the most accurate and effective distribution of the latest information contained in this POH, Pilatus Aircraft Ltd. publishes the content of the POH from a collection of electronically stored publication components called Data Modules (DM). DMs contain various amounts of information depending on the subject they address.
  • Page 28 The Log of Revisions provides a brief description of each change that is introduced with a revision. Note The 5-digit Publication Task Sheet (PTS) number in the change column is for Pilatus internal use only. New or Revised Data Modules In accordance with the instructions of the LOADM, new or revised DMs must be incorporated into the POH and superseded DMs destroyed.
  • Page 29 Pilatus Aircraft Ltd. In connection with the use of this document, Pilatus does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose.
  • Page 30 Section 0 - Introduction Copyright and Legal Statement This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 0-1-4...

  • Page 31: Table Of Contents

    Section 1 - General Table of Contents SECTION 1 General Table of Contents Subject Page General 1-1-1 Introduction 1-2-1 Top Level Illustrations 1-3-1 Descriptive Data 1-4-1 1-4-1 Engine 1-4-1 1-4-2 5-Bladed Propeller 1-4-1 1-4-3 Fuel 1-4-1 1-4-4 1-4-2 1-4-5 Maximum Weights 1-4-2 1-4-6 Typical Airplane Weights...
  • Page 32 Section 1 - General Table of Contents This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 1-0-2...

  • Page 33: General

    Section 1 - General General General This section contains basic data and information of general interest to the pilot. It also contains definitions and explanations of symbols, abbreviations, and terminology that is used throughout this POH. Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 1-1-1...
  • Page 34 Section 1 - General General This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 1-1-2...

  • Page 35: Introduction

    Section 1 - General Introduction Introduction This POH includes the material required to be furnished by the Federal Aviation Regulations and additional information provided by the manufacturer and constitutes the: − EASA Approved Airplane Flight Manual − FAA Approved Airplane Flight Manual for operation in the U.S. in accordance with FAR 21.29.
  • Page 36 Section 1 - General Introduction This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 1-2-2...

  • Page 37: Top Level Illustrations

    Section 1 - General Top Level Illustrations Top Level Illustrations NOTE: WINGSPAN DIMENSION IS IN A FULLY FUELED CONDITION 5 ft 6 in (1,69 m) 53 ft 6 in 17 ft 1 in (16,31 m) (5,20 m) 14 ft 6 ft (4,26 m) (1,83 m) 11 ft 5 in...
  • Page 38 Section 1 - General Top Level Illustrations ICN-12-C-A150103-A-S4080-00114-A-001-01 Figure 1-3-2: Airplane - Ground Turning Clearance - NWS only (No Braking) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 1-3-2...
  • Page 39 Section 1 - General Top Level Illustrations ROTATION POINT (MEASUREMENT POINT) NOTE: Ground turning radius using nosewheel steering, inside brake and partial power. A . WING TIP RADIUS 35' 7" 10,864 m B . NOSEWHEEL RADIUS 14' 10" 4,513 m C .
  • Page 40 Section 1 - General Top Level Illustrations This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 1-3-4...

  • Page 41: Descriptive Data

    Section 1 - General Descriptive Data Descriptive Data 1-4-1 Engine Number of Engines Engine Manufacturer Pratt & Whitney Canada Engine Model Number PT6E-67XP Engine Type This airplane incorporates a twin shaft turboprop engine with 4 axial and 1 centrifugal compressor stages, an annular combustion chamber, and a 3 stage turbine where one stage drives the compressor and two stages power the propeller.

  • Page 42: Oil

    Section 1 - General 1-4-4 Oil Grade or Specification − Any oil specified in Section 2, Limitations, Power Plant Limitations, of this POH. Oil Quantity − Total Oil Capacity 3.6 US gal (13.6 liters) − Drain and Refill Quantity 2.0 US gal (7.6 liters) −...

  • Page 43: Specific Loadings

    Section 1 - General Specific Loadings - Cabin 326 ft (9.23 m 1-4-8 Specific Loadings Wing Loading 37.6 lb/sq ft (183.7 kg/sq m) Power Loading 8.71 lb/shp (3.95 kg/shp) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 1-4-3...
  • Page 44 Section 1 - General Specific Loadings This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 1-4-4...

  • Page 45: Symbols, Abbreviations, And Terminology

    Section 1 - General Symbols, Abbreviations, and Terminology Symbols, Abbreviations, and Terminology 1-5-1 General Airspeed Terminology and Symbols Calibrated Airspeed means the indicated airspeed of an aircraft, corrected for position and instrument error. Calibrated Airspeed is equal to True Airspeed in standard atmosphere at sea level. Ground Speed is the speed of an airplane relative to the ground.

  • Page 46: Meteorological Terminology

    Section 1 - General Meteorological Terminology Best Rate of Climb Speed is the airspeed which delivers the greatest gain of altitude in the shortest possible time. 1-5-2 Meteorological Terminology Indicated Altitude The number actually read from an altimeter when the barometric subscale has been Pressure set to 29.92 in hg (1013.2 mbar).

  • Page 47: Power Terminology

    Section 1 - General Power Terminology 1-5-3 Power Terminology Cruise Climb Power The power recommended to operate the airplane in a cruise climb (a continuous, gradual climb) profile. Flight Idle Power The power required to run an engine, in flight, at the lowest speed that will ensure satisfactory engine and systems operation and airplane handling characteristics.

  • Page 48: Airplane Performance And Flight Planning Terminology

    Section 1 - General Airplane Performance and Flight Planning Terminology Propeller Feather This is a propeller pitch condition which produces minimum drag in a flight condition (engine shutdown). Propeller Speed Control Propeller speed control is the principle operating mode of the Mode propeller control system while the aircraft is operating in flight.

  • Page 49: General Abbreviations And Symbols

    Section 1 - General General Abbreviations and Symbols Datum An imaginary vertical plane from which all horizontal distances are measured for balance purposes. Maximum Landing Weight Maximum weight approved for the landing touchdown. (MLW) Maximum Ramp Weight Maximum weight approved for ground maneuver. It includes (MRW) weight of start, taxi, and run-up fuel.

  • Page 50: Conversion Information

    Section 1 - General Conversion Information Nautical Mile Not Applicable Pounds per Square Inch Revolutions Per Minute Second Shaft Horsepower Statute Mile To Be Determined Time Between Overhauls Visual Flight Rules ° Degrees Feet " Inches Note Refer to Section 7, Airplane and Systems Descriptions, Primus APEX - Avionics Installation for Avionic acronyms and abbreviations.
  • Page 51 Section 1 - General Conversion Information Kilograms (kg) = Pounds (lb) x 0.454 Bar = psi x 0.069 1-5-8.3 Metric to Standard Inches (in) = Millimeters (mm) x 0.039 Inches (in) = Centimeters (cm) x 0.393 Feet (ft) = Meters (m) x 3.281 Yards (yd) = Meters (m) x 1.094 Statute Miles (sm) = Kilometers (km) x 0.621 Nautical Miles (nm) = Kilometers (km) x 0.54...
  • Page 52 Section 1 - General Conversion Information This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 1-5-8...
  • Page 53 Section 2 - Limitations (EASA Approved) Table of Contents SECTION 2 Limitations (EASA Approved) Table of Contents Subject Page General 2-1-1 Airspeed Limitations 2-2-1 Airspeed Indication Markings 2-3-1 Power Plant Limitations 2-4-1 2-4-1 Engine 2-4-1 2-4-2 2-4-1 2-4-3 Oil Quantity 2-4-1 2-4-4 Engine Operating Limits...
  • Page 54 Section 2 - Limitations (EASA Approved) Table of Contents Subject Page 2-15 Kinds of Operation Equipment List 2-15-1 2-16 Fuel Limitations 2-16-1 2-17 Maximum Operating Altitude Limits 2-17-1 2-18 Outside Air Temperature Limits 2-18-1 2-19 Cabin Pressurization Limits 2-19-1 2-20 Maximum Passenger Seating Limits 2-20-1 2-21...
  • Page 55 Section 2 - Limitations (EASA Approved) Table of Contents Subject Page 2-22 Other Limitations 2-22-1 2-22-1 All Passenger Seats 2-22-1 2-22-2 Luggage Limitations 2-22-1 2-22-3 Cargo Limitations 2-22-1 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...
  • Page 56 Section 2 - Limitations (EASA 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...

  • Page 57: General

    Section 2 - Limitations (EASA Approved) General General This section contains the EASA approved operating limitations, instrument markings, color coding, and basic placards necessary for the operation of the airplane, its engine, systems, and equipment. Compliance with approved limitations is mandatory. Limitations associated with systems or equipment which require POH Supplements are included in Section 9, Supplements.
  • Page 58 Section 2 - Limitations (EASA Approved) General This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-1-2...

  • Page 59: Airspeed Limitations

    Section 2 - Limitations (EASA Approved) Airspeed Limitations Airspeed Limitations Table 2-2-1: Airspeed Limitations AIRSPEED KIAS SIGNIFICANCE Maximum operating speed Do not exceed this speed in any operations. Maximum speed at or below 16,300 ft. 0.49 Refer to V schedule for maximum speed above 16,300 ft.
  • Page 60 Section 2 - Limitations (EASA Approved) Airspeed Limitations MAXIMUM OPERATING SPEED 30000 25000 20000 15000 10000 5000 KIAS ICN-12-C-A150202-A-S4080-00116-A-001-01 Figure 2-2-1: VMO / MMO Schedule Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-2-2...

  • Page 61: Airspeed Indication Markings

    Section 2 - Limitations (EASA Approved) Airspeed Indication Markings Airspeed Indication Markings Table 2-3-1: Airspeed Indication Markings INDICATION KIAS VALUE OR RANGE REMARKS Red/White Barber Pole 240 or 0.49 M whichever is Maximum operating limit across and upwards on right lower side of tape Red (high speed) strip on...
  • Page 62 Section 2 - Limitations (EASA Approved) Airspeed Indication Markings This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-3-2...

  • Page 63: Power Plant Limitations

    Section 2 - Limitations (EASA Approved) Power Plant Limitations Power Plant Limitations 2-4-1 Engine Number of Engines Engine Manufacturer Pratt & Whitney Canada Engine Model Number PT6E-67XP 2-4-2 Approved oils are: − AeroShell Turbine Oil 500 − AeroShell Turbine Oil 560 (ASTO 560) −...

  • Page 64: Engine Operating Limits

    Section 2 - Limitations (EASA Approved) Engine Operating Limits 2-4-4 Engine Operating Limits The limits presented in each column shall be observed. The limits presented do not necessarily occur simultaneously. Refer to the Pratt & Whitney Engine Maintenance Manual for specific action if limits are exceeded.

  • Page 65: Fuel

    Section 2 - Limitations (EASA Approved) Fuel Engine inlet condition limits for the operation of the engine are: − Altitude range: Sea level to 30,000 ft − Temperature: 57.2 °C (135 °F) at the engine inlet connection. The torque limit is in the propeller operation range of 1000 to 1700 RPM. At less than 1000 RPM the torque limit is 23.92 psi.

  • Page 66: Anti-Icing Additive

    Section 2 - Limitations (EASA Approved) Anti-Icing Additive Table 2-4-2: Approved Fuels (continued from previous page) APPROVED FUEL SPECIFICATION JP-8 (F-34) DEF STAN 91-87 MIL-DTL-83133 F-35 MIL-DTL-83133 JP-8+100 (F-37) Jet A-50 MSN 1720, 2001 - 2040 Post SB 28-013, and MSN 2041 and up GOST 10227-86 GSTU 320.00149943.007-97 TS-1...

  • Page 67: Propeller

    Section 2 - Limitations (EASA Approved) Propeller Table 2-4-3: Anti-Icing Additive ADDITIVE SPECIFICATION MAXIMUM CONCENTRATION Diethylene Glycol ATSM D4171 Type II 0.15% by volume Monomethyl Ether (DieGME) MIL-DTL-85470 Liquid I GOST 8313 0.30% by volume Liquid I-M 50/50 blend of TU-6-10-1458 0.30% by volume Liquid I with Methyl Alcohol...

  • Page 68: Starter

    Section 2 - Limitations (EASA Approved) Starter 2-4-8 Starter The engine starting cycle shall be limited to the following intervals: − Sequence, 60 seconds OFF − Sequence, 60 seconds OFF − Sequence, 30 minutes OFF. Note A dry motoring cycle is to be counted as a sequence. In case of start abort and automatic dry motoring commanded by EPECS, wait for an additional 10 minutes before a new start is attempted.

  • Page 69: Power Plant Window Markings

    Section 2 - Limitations (EASA Approved) Power Plant Window Markings Power Plant Window Markings Table 2-5-1: Power Plant Window Markings RED MARK AMBER GREEN ARC AMBER ARC RED MARK Min. Limit MARK Norm Ops. Caution Max. Limit Caution Indication Torque (psi) 0 to 40.63 40.63 44.84...
  • Page 70 Section 2 - Limitations (EASA Approved) Power Plant Window Markings This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-5-2...

  • Page 71: Miscellaneous Instrument Markings

    Section 2 - Limitations (EASA Approved) Miscellaneous Instrument Markings Miscellaneous Instrument Markings Table 2-6-1: Miscellaneous Instrument Markings Instrument RED RADIAL YELLOW GREEN ARC YELLOW Min. Limit Norm Ops. RAD/DIA Caution Caution Max. Limit Oxygen 1850 to 2000 Pressure (psi) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-6-1...
  • Page 72 Section 2 - Limitations (EASA Approved) Miscellaneous Instrument Markings This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-6-2...

  • Page 73: Weight Limits

    Section 2 - Limitations (EASA Approved) Weight Limits Weight Limits Maximum Ramp Weight 10,495 lb (4760 kg) Maximum Takeoff Weight 10,450 lb (4740 kg) Maximum Landing Weight 9921 lb (4500 kg) Maximum Zero Fuel Weight 9039 lb (4100 kg) Maximum Baggage Weight 400 lb (180 kg) Maximum Floor Loading: - On Seat Rails...
  • Page 74 Section 2 - Limitations (EASA Approved) Weight Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-7-2...

  • Page 75: Center Of Gravity Limits

    Section 2 - Limitations (EASA Approved) Center of Gravity Limits Center of Gravity Limits Table 2-8-1: Center of Gravity Limits Weight Forward Limit Aft Limit Pounds (kilograms) A.O.D.: in (m) A.O.D.: in (m) 10,450 (4740) 232.20 (5.898) 240.43 (6.107) 9921 (4500) 232.20 (5.898) 240.94 (6.120) 8158 (3700)
  • Page 76 Section 2 - Limitations (EASA Approved) Center of Gravity Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-8-2...

  • Page 77: Maneuver Limits

    Section 2 - Limitations (EASA Approved) Maneuver Limits Maneuver Limits This airplane is certificated in the Normal Category. The normal category is applicable to aircraft intended for non-aerobatic operations. These include any maneuvers incidental to normal flying, stalls (except whip stalls), lazy eights, chandelles, and turns in which the bank angle does not exceed 60°.
  • Page 78 Section 2 - Limitations (EASA Approved) Maneuver Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-9-2...

  • Page 79: Flight Load Factor Limits

    Section 2 - Limitations (EASA Approved) Flight Load Factor Limits 2-10 Flight Load Factor Limits Flight load limits with flaps up +3.3 g -1.32 g Flight load limits with flaps down +2.0 g -0.0 g Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-10-1...
  • Page 80 Section 2 - Limitations (EASA Approved) Flight Load Factor Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-10-2...

  • Page 81: Flight Crew Limits

    Section 2 - Limitations (EASA Approved) Flight Crew Limits 2-11 Flight Crew Limits Minimum required flight crew is one pilot in the left hand seat. Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-11-1...
  • Page 82 Section 2 - Limitations (EASA Approved) Flight Crew Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-11-2...

  • Page 83: Kinds Of Operation

    Section 2 - Limitations (EASA Approved) Kinds of Operation 2-12 Kinds of Operation The Pilatus PC-12 is approved for the following types of operation when the required equipment is installed and operational: VFR Day. VFR Night. IFR Day incl. CAT 1 approaches, single pilot.
  • Page 84 Section 2 - Limitations (EASA Approved) Kinds of Operation This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-12-2...

  • Page 85: Pneumatic Deicing Boot System

    Section 2 - Limitations (EASA Approved) Pneumatic Deicing Boot System 2-13 Pneumatic Deicing Boot System The pneumatic de-ice boot system is required to be installed for all flights. Preflight function test required before takeoff and flight into known icing conditions. The system is required to function properly for flight into known icing conditions.
  • Page 86 Section 2 - Limitations (EASA Approved) Pneumatic Deicing Boot System This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-13-2...

  • Page 87: Icing Limitations

    Section 2 - Limitations (EASA Approved) Icing Limitations 2-14 Icing Limitations 2-14-1 Limitations Flight in icing conditions is only approved with all ice protection systems, generator 1 and generator 2 serviceable. Flight in icing conditions is prohibited when the Propeller De-ice caution is active. During flight in icing conditions, if there is a failure of any of the aircraft ice protection systems exit icing conditions.
  • Page 88 Section 2 - Limitations (EASA Approved) Severe Icing Conditions 2-14-3 Severe Icing Conditions Severe icing may result from environmental conditions outside of those for which the airplane is certificated. Flight in freezing rain, freezing drizzle, or mixed icing conditions (supercooled liquid water and ice crystals) may result in ice build-up on protected surfaces exceeding the capability of the ice protection system, or may result in ice forming aft of the protected surfaces.
  • Page 89 Section 2 - Limitations (EASA Approved) Kinds of Operation Equipment List 2-15 Kinds of Operation Equipment List This airplane is approved for operations under day and night VFR, day and night IFR and flight into known icing conditions when the required equipment is installed and operating properly.
  • Page 90 Section 2 - Limitations (EASA Approved) Kinds of Operation Equipment List Table 2-15-1: Kinds of Operation Equipment List (continued from previous page) SYSTEM / EQUIPMENT IFR DAY ICING RVSM NIGHT NIGHT Fire Detect System Engine and Propeller Electronic Control System Electrical: No.
  • Page 91 Section 2 - Limitations (EASA Approved) Kinds of Operation Equipment List Table 2-15-1: Kinds of Operation Equipment List (continued from previous page) SYSTEM / EQUIPMENT IFR DAY ICING RVSM NIGHT NIGHT Seat Restraints (each occupant) Firewall ACS Shutoff Valve Emergency Ram Air Scoop Negative Pressure Relief Valve Oxygen System...
  • Page 92 Section 2 - Limitations (EASA Approved) Kinds of Operation Equipment List This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-15-4...
  • Page 93 Section 2 - Limitations (EASA Approved) Fuel Limitations 2-16 Fuel Limitations Total Fuel Capacity 406.8 US gal, 2,736.5 lb (1,540 liters, 1,241.3 kg) Total Usable Fuel 402 US gal, 2,703.6 lb (1,521.5 liters, 1,226.4 kg) Total Unusable Fuel 4.8 US gal, 32.9 lb (18.5 liters, 14.9 kg) Maximum Fuel Imbalance 26.4 US gal, 178 lb (100 liters, 80.6 kg) (Maximum 3 segments on indicator)
  • Page 94 Section 2 - Limitations (EASA Approved) Fuel Limitations This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-16-2...
  • Page 95 Section 2 - Limitations (EASA Approved) Maximum Operating Altitude Limits 2-17 Maximum Operating Altitude Limits Maximum Operating Altitude 30,000 ft (9144 m) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-17-1...
  • Page 96 Section 2 - Limitations (EASA Approved) Maximum Operating Altitude Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-17-2...
  • Page 97 Section 2 - Limitations (EASA Approved) Outside Air Temperature Limits 2-18 Outside Air Temperature Limits Minimum Outside Air Temperature -55 °C (-67 °F) Maximum Outside Air Temperature +50 °C (122 °F) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-18-1...
  • Page 98 Section 2 - Limitations (EASA Approved) Outside Air Temperature Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-18-2...
  • Page 99 Section 2 - Limitations (EASA Approved) Cabin Pressurization Limits 2-19 Cabin Pressurization Limits Maximum cabin pressure differential is 5.75 psi (400 mbar). Pressurized landing is approved up to 0.7 psid. Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-19-1...
  • Page 100 Section 2 - Limitations (EASA Approved) Cabin Pressurization Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 2-19-2...
  • Page 101 For layouts EX-8S, EX-6S-STD-2S and EX-4S-STD-4S: Leave seats 5, 6, 7 and 8 vacant during takeoff and landing unless seat in front is occupied. Pilatus must be contacted to determine the modification work required to the aircraft, before any change to an interior configuration is made.
  • Page 102 Section 2 - Limitations (EASA Approved) Maximum Passenger Seating Limits This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 2-20-2...
  • Page 103 Section 2 - Limitations (EASA Approved) Systems and Equipment Limits 2-21 Systems and Equipment Limits 2-21-1 Stall Warning / Stick Pusher System Preflight function test required before takeoff. System is required to function properly in normal mode for all flights and in ice mode for flight into known icing conditions.
  • Page 104 Primus Apex The Pilots Guide for the Advanced Cockpit Environment (ACE ) (powered by Honeywell) for the Pilatus PC-12/47E must always be carried on board the aircraft. 2-21-11 Primus Apex - Automatic Flight Control System During autopilot operation, a pilot must be seated in a pilot position with seat belt fastened.
  • Page 105 Section 2 - Limitations (EASA Approved) Primus Apex - Flight Management System During normal operation: − Do not override the autopilot and Yaw Damper in any axis − Hold the throttle at the required position for at least 3 seconds if you intend to override the engaged AT system and confirm the AT disconnect by pressing the AT Quick- Disconnect button on the PCL −...
  • Page 106 Section 2 - Limitations (EASA Approved) Primus Apex - Flight Management System BARO-VNAV AMC 20-27 Airworthiness Approval and Operational Criteria for RNP Approach (RNP APCH) Operations including APV BARO- VNAV Operations. AC 90-105 Approval Guidance for RNP Operations and Barometric Vertical Navigation in the U.S. National Airspace System.
  • Page 107 Section 2 - Limitations (EASA Approved) Primus Apex - Flight Management System Instrument approaches must be conducted in the FMS approach mode and GPS integrity monitoring must be available at the Final Approach Fix. APP (approach active) mode indication must be displayed on the Primary Flight Display (PFD) at the Final Approach Fix (FAF).
  • Page 108 One (1) altitude reporting transponder KXP 2290. The ESIS does not meet RVSM performance requirements and 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 2-21-14.1 TCAS I...
  • Page 109 Section 2 - Limitations (EASA Approved) Primus Apex - Transponder 2-21-15 Primus Apex - Transponder The KXP 2290A ATC Transponder System with ADS-B Out (1090 MHz Extended Squitter ADS-B Out) supports the 1090ES equipment operating on the radio frequency of 1090MHz. The transponder system complies with the criteria of ICAO Doc 7030/4 Regional Supplementary Procedures for operations where enhanced surveillance is required.
  • Page 110 Section 2 - Limitations (EASA Approved) Yaw Damper 2-21-18 Yaw Damper Above FL155 (15,500 ft), when the yaw damper is not operating, the aircraft must be flown only in balanced flight (slip-skid indicator +/- 1 trapezoid). 2-21-19 Primus Apex - Electrionic Checklist The Electronic Checklist functionality allows implementation of a user defined Electronic Checklist database.
  • Page 111 Section 2 - Limitations (EASA Approved) Primus Apex - Weather Radar 2-21-23 Primus Apex - Weather Radar When the weather radar system is operated while the aircraft is on the ground, direct the nose of the aircraft so that the antenna scan sector is free of large metallic objects, such as hangars or other aircraft for a minimum distance of 15 feet (5 meters), and tilt the antenna fully upwards.
  • Page 112 Section 2 - Limitations (EASA Approved) Primus Apex - Terrain Database This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 2-21-10...
  • Page 113 Section 2 - Limitations (EASA Approved) Other Limitations 2-22 Other Limitations 2-22-1 All Passenger Seats For takeoff and landing the seat lap and shoulder belts must be fastened, the lap belt tightened, and the seat headrest positioned to support the head. 2-22-2 Luggage Limitations The luggage area maximum load is given in...
  • Page 114 Section 2 - Limitations (EASA Approved) Structural Limitations 2-22-4 Structural Limitations Refer to Chapter 4 of the PC-12/47E Aircraft Maintenance Manual, Pilatus Report Number 02436. 2-22-5 Smoking Smoking is not permitted in the cabin of aircraft equipped with a standard interior unless ashtrays are installed.
  • Page 115 Section 2 - Limitations (EASA Approved) Placards 2-23 Placards On exterior Passenger Door: PRESS HERE TO OPEN PULL HANDLE AND PULL DOOR OUT DO NOT OPEN DOOR WHEN ENGINE IS RUNNING UNLESS IN EMERGENCY ICN-12-C-A150223-A-S4080-00117-A-001-01 Figure 2-23-1: Placards - Exterior (Sheet 1 of 7) Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020...
  • Page 116 Section 2 - Limitations (EASA Approved) Placards On exterior Cargo Door: PRESS HERE TO OPEN PULL HANDLE AND PULL DOOR OUT DO NOT OPEN DOOR WHEN ENGINE IS RUNNING UNLESS IN EMERGENCY PULL TO OPEN ICN-12-C-A150223-A-S4080-00118-A-001-01 Figure 2-23-1: Placards - Exterior (Sheet 2 of 7) Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020...
  • Page 117 Section 2 - Limitations (EASA Approved) Placards Near Static Ports: STATIC PRESSURE KEEP CLEAR On left side Vertical Tail forward of Horizontal Stabilizer: On Rudder (each side): DO NOT PUSH ICN-12-C-A150223-A-S4080-00119-A-001-01 Figure 2-23-1: Placards - Exterior (Sheet 3 of 7) Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020...
  • Page 118 Section 2 - Limitations (EASA Approved) Placards On exterior Emergency Exit: (Not to Scale) EMERGENCY EXIT PUSH PUSH IN AFTER RELEASE Inside left Engine Cowling: ENGINE OIL TYPE USED, NOTE: The engine oil type used will be added to the placard prior to delivery of the aircraft. ICN-12-C-A150223-A-S4080-00120-A-001-01 Figure 2-23-1: Placards - Exterior (Sheet 4 of 7) Pilot's Operating Handbook...
  • Page 119 Section 2 - Limitations (EASA Approved) Placards On Nose Landing Gear (each side): On Nose Landing Gear: DO NOT TURN BEYOND RED MARKS Near Fuel Filler: JET-A-FUEL TOTAL CAPACITY 770 LTR. 203 US. GAL. SEE PILOT'S OPERATING HANDBOOK FOR APPROVED FUELS AND QUANTITY REFUELING BONDING POINT Near Fuel Vent: FUEL VENT...
  • Page 120 Section 2 - Limitations (EASA Approved) Placards On each side of Engine Lower Front Cowling: VERY HOT AREA DO NOT TOUCH On Forward Fuselage RH side Access Door: OXYGEN SERVICE POINT USE NO LUBRICANTS Note: When the optional larger oxygen bottle is installed, this placard is installed inside the battery compartment and outside on Rear Fuselage Bottom Access Door.
  • Page 121 Section 2 - Limitations (EASA Approved) Placards On Main Landing Gear Doors: MAIN LANDING GEAR SHOCK STRUT N2 CHARGE PRESSURE 1st. STAGE 141 psi (9,7 bar) 2nd. STAGE 1668 psi (115 bar) On Rear Fuselage Bottom Access Door: BATTERY COMPARTMENT INSTALLED INSIDE On Rear Fuselage Bottom LH side: 28 VOLT DC...
  • Page 122 Section 2 - Limitations (EASA Approved) Placards PLACARDS - COCKPIT On Cockpit LH and RH Rear Panels: (LH only) (LH only) (RH only) (RH only) EMERG AURAL CVFDR MAU DATA COM1 WARN SELECT TEST LOAD (Option) On Cockpit LH Side Panels near oxygen system controls: PASSENGER OXYGEN AUTO On Cockpit LH and RH Side Panels:...
  • Page 123 Section 2 - Limitations (EASA Approved) Placards On left Cockpit Side Panel and right Cockpit Side Panel (LH Shown, RH Opposite): 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. NO ACROBATIC MANEUVERS INCLUDING SPINS ARE APPROVED.
  • Page 124 Section 2 - Limitations (EASA Approved) Placards On the LH and RH Instrument Panel: (4740 KG) 166 KIAS (2600 KG) 123 KIAS 240 KIAS 0.49 M (UP TO 15°) 165 KIAS (ABOVE 15°) 130 KIAS Near Landing Gear Selector Handle: 180 KIAS 240 KIAS Near TS/MF Controller:...
  • Page 125 Section 2 - Limitations (EASA Approved) Placards On Cockpit LH Instrument Panel: Near optional Standby Magnetic Compass (if installed): STANDBY COMPASS FOR CORRECT READING SWITCH: GENERATORS & BATTERIES ON AVIONICS ON NAV & INSTRUMENT LIGHTS AS REQUIRED WINDSHIELD DE-ICE LH & RH OFF PROBES DE-ICE OFF ELECTRICAL HEAT/COOL SWITCH INHIBIT FOOT WARMER OFF (IF INST.)
  • Page 126 Section 2 - Limitations (EASA Approved) Placards On Center Console: FLAP POWER IDLE STABILIZED PROPELLER OPERATION ON GROUND (NOT FEATHERED) BETWEEN 350 AND 950 rpm IS PROHIBITED At aft end of Center Console: CAUTION PCL OPERATION AFT OF THE IDLE DETENT IS PROHIBITED WHEN IN FLIGHT ICN-12-C-A150223-A-S4080-00128-A-001-01 Figure 2-23-2: Placards - Cockpit (Sheet 5 of 6)
  • Page 127 Section 2 - Limitations (EASA Approved) Placards On the PCL: VHF1 TO/GA XFER AT DISC At rear of Center Console: FUEL EMER SOV HANDLE EMERGENCY GEAR EXTENSION ACS EMER SOV HANDLE On Fuel and ACS Firewall Shut off Valve and Emergency Gear Extension Handles: OPEN PRESS TO RELEASE...
  • Page 128 Section 2 - Limitations (EASA Approved) Placards PLACARDS - CABIN The following standard placards are installed in all aircraft. On Interior Passenger Door: EXIT DO NOT OPERATE IN FLIGHT CLOSED DO NOT OPEN DOOR WHEN ENGINE IS RUNNING UNLESS IN EMERGENCY ONLY ONE PERSON ON STAIRS AT ANY TIME PUSH BUTTON FOR...
  • Page 129 Section 2 - Limitations (EASA Approved) Placards On Interior Emergency Exit: EXIT On Interior Emergency Exit Handle: PULL On Interior Cargo Door Handle Cover: DO NOT REMOVE COVER IN FLIGHT On Interior Cargo Door Handle: LIFT LOCKING LEVER AND PULL HANDLE PUSH DOOR OUT On Interior Cargo Door: DO NOT OPEN DOOR WHEN ENGINE IS RUNNING...
  • Page 130 Section 2 - Limitations (EASA Approved) Placards On forward and rear Cargo Door Frame: MAX FREIGHT LOAD = 1500 kg / 3300 lb Max Load on Max Load on Seat Rails Floor Panels 1000 kg/m 600 kg/m 205 lb/ft 125 lb/ft CARGO MUST NOT OBSTRUCT ACCESS TO CABIN DOOR AND EMERGENCY EXIT...
  • Page 131 Section 2 - Limitations (EASA Approved) Placards PLACARDS - 9 SEAT CORPORATE COMMUTER (Interior Code STD-9S). The cabin placards plus the following additional placards are those required for this interior. On the rear of the left and right cockpit bulkheads, and on the rear of each seat: FOR TAKEOFF AND LANDING - SEAT BACK MUST BE FULLY UPRIGHT - ADJUST HEADREST TO SUPPORT HEAD...
  • Page 132 Section 2 - Limitations (EASA Approved) Placards PLACARDS - 6 SEAT EXECUTIVE (Interior Code EX-6S-2). The cabin placards plus the following additional placards are those required for this interior. On the rear of the left bulkhead: FIRE EXTINGUISHER LOCATED ON COCKPIT SIDE RH BULK- HEAD BEHIND CO-PILOT SEAT On the inside of the lavatory doors: NO SMOKING...
  • Page 133 Section 2 - Limitations (EASA Approved) Placards On each Passenger Oxygen Mask Cover: OXYGEN MASK INSIDE On the armrest near each Passenger Oxygen Mask: PULL TAPE FOR PULL TAPE FOR OXYGEN MASK OXYGEN MASK Near the optional coat rail in the baggage compartment: MAX COAT RAIL 5 kg / 11 lb On the forward cargo door frame: INTERIOR CODE:...
  • Page 134 Section 2 - Limitations (EASA Approved) Placards 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 Code EX-4S-STD-4S) The cabin placards, the 6 seat executive placards and the following replacement/additional placards are required for this interior.
  • Page 135 Section 2 - Limitations (EASA Approved) Placards PLACARDS - NO CABIN INTERIOR (OPTION) The following cockpit and cabin placards are required for this interior. On the overhead panel, covering the "NO SMOKING" and "SEAT BELTS" markings and on the instrument panel, covering the "CAB FLOOD" marking: INOP On the left rear side of the ferry flight compartment bulkhead: LIMITATIONS:...
  • Page 136 Section 2 - Limitations (EASA Approved) Placards On the first aid kit holder cover (left forward side of the ferry flight compartment bulkhead): On the right forward side of the ferry flight compartment bulkhead: FIRE EXTINGUISHER On the inside of the emergency exit: On the cargo door frame: MAX FREIGHT LOAD = 1500 kg / 3300 lb Max Load on...
  • Page 137 Section 3 - Emergency Procedures (EASA Approved) Table of Contents SECTION 3 Emergency Procedures (EASA Approved) Table of Contents Subject Page General 3-1-1 3-1-1 General 3-1-1 3-1-2 Crew Alerting System 3-1-2 3-1-3 Flight Alerting System 3-1-2 3-1-4 FAS Messages and Actions 3-1-2 Airspeeds for Emergency Operations 3-2-1...
  • Page 138 Section 3 - Emergency Procedures (EASA Approved) Table of Contents Subject Page 3-6-06 Engine Oil Press 3-6-3 3-6-07 Engine Oil Temp 3-6-4 3-6-07 Engine Oil Temp 3-6-4 3-6-08 Starter Engaged 3-6-4 3-6-09 Engine Oil Level 3-6-5 3-6-10 Engine Chip 3-6-6 3-6-11 EPECS Fail 3-6-6...
  • Page 139 Section 3 - Emergency Procedures (EASA Approved) Table of Contents Subject Page 3-11-01 Flaps 3-11-1 3-12 Stick Pusher Failure 3-12-1 3-12-01 Pusher 3-12-1 3-13 Inadvertent Pusher/Shaker Operation 3-13-1 3-13-01 Pusher 3-13-1 3-13-02 Shaker 3-13-2 3-14 Electrical Trim 3-14-1 3-14-01 Pitch Trim Runaway 3-14-1 3-14-02 Yaw Trim Runaway...
  • Page 140 Section 3 - Emergency Procedures (EASA Approved) Table of Contents Subject Page 3-15-18 Battery 2 Off 3-15-11 3-15-19 External Power 3-15-11 3-16 Fuel System 3-16-1 3-16-01 Fuel Pressure Low 3-16-1 3-16-02 Fuel PRESS SENS Fail 3-16-2 3-16-03 LH Fuel Low 3-16-2 3-16-03 RH Fuel Low...
  • Page 141 Section 3 - Emergency Procedures (EASA Approved) Table of Contents Subject Page 3-18-04 LH + RH Windshield Heat 3-18-4 3-18-05 Probes Off 3-18-4 3-18-06 AOA De Ice 3-18-5 3-18-07 Pitot 1 Heat 3-18-6 3-18-07 Pitot 2 Heat 3-18-6 3-18-08 Static Heat 3-18-6 3-18-09 Pusher...
  • Page 142 Section 3 - Emergency Procedures (EASA Approved) Table of Contents Subject Page 3-22-08 RH PFD CTRL Fail 3-22-6 3-22-09 LH+RH PFD CTRL Fail 3-22-6 3-22-10 Check Pilot PFD 3-22-6 3-22-11 Check Copilot PFD 3-22-6 3-22-12 Check Engine Display 3-22-7 3-22-13 ATT FAIL 3-22-7 3-22-14...
  • Page 143 Section 3 - Emergency Procedures (EASA Approved) Table of Contents Subject Page 3-22-39 FMS1-GPS2 Pos Misc 3-22-20 3-22-39 FMS2-GPS1 Pos Misc 3-22-20 3-22-39 FMS2-GPS2 Pos Misc 3-22-20 3-22-40 FMS1-GPS1+2 Pos Misc 3-22-20 3-22-40 FMS2-GPS1+2 Pos Misc 3-22-20 3-22-41 Unable FMS-GPS Mon 3-22-21 3-22-42 MMDR 1 Fail...
  • Page 144 Section 3 - Emergency Procedures (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...

  • Page 145: General

    Section 3 - Emergency Procedures (EASA Approved) General General 3-1-1 General The recommended action to be taken in case of failure or in emergency situations are contained in this section. Emergency procedures alone cannot protect against all situations. Good airmanship be used in conjunction with the emergency procedures to manage the emergency.

  • Page 146: Crew Alerting System

    Section 3 - Emergency Procedures (EASA Approved) Crew Alerting System 3-1-2 Crew Alerting System The Crew Alerting System (CAS) gives: − RED Warning messages which require immediate corrective action by the pilot. − AMBER Caution messages which requires the pilots attention but not an immediate action.

  • Page 147: Airspeeds For Emergency Operations

    Section 3 - Emergency Procedures (EASA Approved) Airspeeds for Emergency Operations Airspeeds for Emergency Operations 3-2-1 Airspeeds for Emergency Operations All airspeeds shown are with airplane in clean configuration under ISA conditions. Operating Maneuvering Speed (V Aircraft Mass Airspeed 10450 lb (4740 kg) 166 KIAS 9921 lb (4500 kg) 161 KIAS...
  • Page 148 Section 3 - Emergency Procedures (EASA Approved) Airspeeds for Emergency Operations This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-2-2...

  • Page 149: Rejected Takeoff (Not Engine Related)

    Section 3 - Emergency Procedures (EASA Approved) Rejected Takeoff (Not engine related) Rejected Takeoff (Not engine related) Rejected Takeoff (Not engine related) 3-3-01 PCL..........Idle Braking........As required Reverse........As required CAUTION If any further taxiing is required soft brake pedals and/or wheel fusible plugs release may occur due to overheating.
  • Page 150 Section 3 - Emergency Procedures (EASA Approved) Rejected 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...

  • Page 151: Engine Failure

    Section 3 - Emergency Procedures (EASA Approved) Engine Failure Engine Failure Engine failure before rotation 3-4-01 PCL..........Idle Braking........As required If runway overrun or collision is likely, then: Engine switch......FUEL EMERG shut off....Press latch down and pull lever up MASTER POWER switch....

  • Page 152: Engine Failure After Rotation - Landing Gear Up

    Section 3 - Emergency Procedures (EASA Approved) Engine Failure Engine failure after rotation - Landing gear up 3-4-03 If total power loss: Landing gear....... Down, if landing site allows, otherwise keep landing gear up Flaps........... 40º Aircraft......... Final Approach Speed for 10450 lb (4740 kg), not below DSB (1.3 V Speed Flap setting...

  • Page 153: Engine Surging

    Section 3 - Emergency Procedures (EASA Approved) Engine Failure Engine Failure in Flight - Total Power Loss 3-4-04 continued Aircraft......... Proceed to nearest airfield or landing site avoiding high terrain Remaining fuel......Check If no mechanical damage suspected and time permits: Aircraft.........
  • Page 154 Section 3 - Emergency Procedures (EASA Approved) Engine Failure This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 3-4-4...

  • Page 155: Air Start

    Section 3 - Emergency Procedures (EASA Approved) Air Start Air Start Air Start Envelope 3-5-01 ALTITUDE - AIRSPEED ENVELOPE 25,000 20,000 15,000 10,000 ENGINE RELIGHT POSSIBLE with Starter Assistance 5,000 0,000 AIRSPEED - KIAS ICN-12-C-A150305-A-S4080-00001-A-001-01 Figure 3-5-1: Engine Relight ---------- END ----------- Air Start - With starter 3-5-02 WARNING...
  • Page 156 Section 3 - Emergency Procedures (EASA Approved) Air Start Air Start - With starter 3-5-02 continued NG..........Check NG < 5% EEC CH A (Essential Bus PULL circuit breaker......EEC CH B (Avionic 1 Bus PULL circuit breaker......EEC CH A (Essential Bus PUSH, wait for 1 second circuit breaker......
  • Page 157 Section 3 - Emergency Procedures (EASA Approved) Air Start Air Start - With starter 3-5-02 continued If no air start: WARNING DO NOT ATTEMPT MORE THAN ONE AIR START. REPEATED AIR START ATTEMPTS COULD DISCHARGE THE BATTERY TO A LEVEL THAT WOULD NOT BE ABLE TO SUPPORT ESSENTIAL ELECTRICAL SERVICES.
  • Page 158 Section 3 - Emergency Procedures (EASA Approved) Air Start This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-5-4...

  • Page 159: Engine Emergencies

    Section 3 - Emergency Procedures (EASA Approved) Engine Emergencies Engine Emergencies Propeller Low Pitch 3-6-01 Propeller Low Pitch warning and voice callout “Propeller Low Pitch”. PCL..........Ensure forward of idle detent If it is not possible to maintain speed and height: Engine switch......

  • Page 160: Engine Ng

    Section 3 - Emergency Procedures (EASA Approved) Engine Emergencies Engine Np Engine Np 3-6-02 continued WARNING THE ENGINE WILL BE COMMANDED TO FEATHER/IDLE IF NP EXCEEDS 1845 RPM. ---------- END ----------- Engine Ng Engine Ng 3-6-03 NG..........Check NG % indication If NG is above 104%: PCL..........

  • Page 161: Engine Itt

    Section 3 - Emergency Procedures (EASA Approved) Engine Emergencies Engine Torque Engine Torque 3-6-04 continued If torque above 44.3 psi: PCL..........Reduce power Engine Torque Engine Torque remains: Aircraft......... Land as soon as possible, using minimum power. If possible always retain glide capability, to the selected landing airfield, in case of total engine failure ---------- END -----------...

  • Page 162: Engine Oil Temp

    Section 3 - Emergency Procedures (EASA Approved) Engine Emergencies Engine Oil Temp Engine Oil Temp 3-6-07 On ground: Oil..........Check OIL T °C indication If oil temperature is high: Aircraft......... Position into wind PCL..........Increase power If oil temperature does not return to normal: ELECTRICAL HEAT/COOL INHIBIT switch..........

  • Page 163: Engine Oil Level

    Section 3 - Emergency Procedures (EASA Approved) Engine Emergencies Starter Engaged 3-6-08 continued STARTER circuit breaker PULL (Essential Bus L1)..... EXT PWR (if available)....BAT 1 and BAT 2 switches..Aircraft......... Maintenance action required --- END --- In flight (following an air start): BUS TIE circuit breaker Pull (Electrical Power Management...

  • Page 164: Engine Chip

    Section 3 - Emergency Procedures (EASA Approved) Engine Emergencies Engine Chip 3-6-10 On ground: Before engine start: Do not start engine...... Maintenance required --- END --- On ground: After engine start or after landing: Aircraft......... Return to parking area Engine......... Shut down engine.

  • Page 165: Epecs Degraded

    Section 3 - Emergency Procedures (EASA Approved) Engine Emergencies EPECS Degraded 3-6-12 On ground: Engine......... Do not start engine, shut down engine when possible Engine......... Do an aircraft power reset If fault remains: Engine......... Maintenance required --- END --- In flight: Aircraft.........
  • Page 166 Section 3 - Emergency Procedures (EASA Approved) Engine Emergencies This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-6-8...

  • Page 167: Fire, Smoke Or Fumes

    Section 3 - Emergency Procedures (EASA Approved) Fire, Smoke or Fumes Fire, Smoke or Fumes Fire Detector 3-7-01 A fault in the Fire detection system has occurred. On ground Engine....... Do not start engine, shut down engine Engine....... Maintenance action required --- END --- In flight...
  • Page 168 Section 3 - Emergency Procedures (EASA Approved) Fire, Smoke or Fumes Engine Fire 3-7-02 continued Parking brake.... OFF (if possible) Aircraft....... Evacuate Fire......Extinguish --- END --- In flight Engine power.... Reduce to minimum acceptable according to flight situation ACS EMER shut off... PULL Main OXYGEN lever.
  • Page 169 Section 3 - Emergency Procedures (EASA Approved) Fire, Smoke or Fumes Engine Fire 3-7-02 continued Vent valve (if smoke Open goggles worn).... PASSENGER OXYGEN selector..Systems MFD PAX Confirm ON OXY advisory... Passengers....Instruct to don masks 10. Aircraft....... Check fire If confirmed that fire exists: 11.

  • Page 170: Cockpit/Cabin Fire, Smoke Or Fumes, Smoke Evacuation

    Section 3 - Emergency Procedures (EASA Approved) Fire, Smoke or Fumes Cockpit/Cabin Fire, Smoke or Fumes, Smoke 3-7-03 Evacuation Main OXYGEN lever. Confirm ON Crew oxygen masks and smoke goggles (if equipped)....Note Procedure to don the crew oxygen masks: Remove the normal headset.
  • Page 171 Section 3 - Emergency Procedures (EASA Approved) Fire, Smoke or Fumes Cockpit/Cabin Fire, Smoke or Fumes, Smoke 3-7-03 Evacuation continued Aircraft....... Proceed to nearest Airfield If smoke evacuation is required: 10. ACS EMER shut off... PULL 11. CABIN PRESSURE DUMP switch......
  • Page 172 Section 3 - Emergency Procedures (EASA Approved) Fire, Smoke or Fumes Cockpit/Cabin Fire, Smoke or Fumes, Smoke 3-7-03 Evacuation continued WARNING DO NOT PULL THE FOLLOWING CIRCUIT BREAKERS ASSOCIATED WITH THE AUXILIARY HEATING SYSTEM: − COND HTR CTL − CABIN FAN −...
  • Page 173 Section 3 - Emergency Procedures (EASA Approved) Fire, Smoke or Fumes Cockpit/Cabin Fire, Smoke or Fumes, Smoke 3-7-03 Evacuation continued 22. GEN 1 switch..... OFF 23. BAT 1 switch....OFF If smoke/fumes still persist and source is suspected electrical: 24. MASTER POWER EMERGENCY OFF switch......
  • Page 174 Section 3 - Emergency Procedures (EASA Approved) 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...

  • Page 175: Emergency Descent

    Section 3 - Emergency Procedures (EASA Approved) Emergency Descent Emergency Descent General 3-8-01 The type of emergency descent will depend on the kind of failure and the aircraft situation. Two types of descent are considered: Engine failure, aircraft flown for maximum range. Engine running, maximum descent rate.
  • Page 176 Section 3 - Emergency Procedures (EASA Approved) Emergency Descent Maximum Range Descent - After Engine Fail 3-8-02 continued CAUTION If landing gear and/or flaps are extended glide range will be severely reduced. Retracting landing gear and flaps will reduce battery endurance significantly and may prejudice subsequent flaps lowering.

  • Page 177: Maximum Rate Descent

    Section 3 - Emergency Procedures (EASA Approved) Emergency Descent Maximum Range Descent - After Engine Fail 3-8-02 continued CAUTION Monitor BAT 1 and BAT 2 amps. If one indication is positive, switch OFF affected battery. After 5 minutes battery can be switched ON again. If indication still positive switch battery OFF.
  • Page 178 Section 3 - Emergency Procedures (EASA Approved) Emergency Descent Maximum Rate Descent 3-8-03 continued Crew oxygen masks....Prepare. Put on before cabin altitude exceeds 10,000 ft Note Procedure to don the crew oxygen masks: Remove the normal headset. Put the oxygen mask on. Check 100%. Put the smoke goggles on.
  • Page 179 Section 3 - Emergency Procedures (EASA Approved) Emergency Descent EMERGENCY DESCENT PROFILES 30,000 MAXIMUM RATE DESCENT 25,000 20,000 MAXIMUM RANGE DESCENT 15,000 10,000 5,000 DISTANCE - NM ICN-12-C-A150308-A-S4080-00002-A-001-01 Figure 3-8-1: Emergency Descent Profiles Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-8-5...
  • Page 180 Section 3 - Emergency Procedures (EASA Approved) Emergency Descent Emergency Descent 3-8-04 Emergency Descent Cabin Altitude are indicated on the CAS window and is displayed on the PFD. If above FL200 (EDM armed) and if autopilot is engaged, the Emergency Descent Mode (EDM) will be triggered by a Cabin Altitude warning.

  • Page 181: Emergency Landing

    Section 3 - Emergency Procedures (EASA Approved) Emergency Landing Emergency Landing Glide Distance and Speed 3-9-01 (Refer to Fig. 3-8-1) Configuration: Landing gear....... Flaps........... 0° Airspeed........Best glide speed: Airspeed Aircraft Mass 119 KIAS 10450 lb (4740 kg) 116 KIAS 9920 lb (4500 kg) 110 KIAS 9040 lb (4100 kg)

  • Page 182: Landing With Main Landing Gear Unlocked

    Section 3 - Emergency Procedures (EASA Approved) Emergency Landing Forced Landing 3-9-02 continued Seat backs........Upright Seat belts........Fastened. Tighten lap straps Passengers......... Brief. Instruct to sit upright ELT..........Set to ON If landing site allows: Landing gear....... DOWN If landing site not suitable for gear down landing: Landing gear.......

  • Page 183: Landing With Nose Landing Gear Unlocked

    Section 3 - Emergency Procedures (EASA Approved) Emergency Landing Landing with Main Landing Gear Unlocked 3-9-03 continued Final approach speed....85 KIAS for 9921 lb (4500 kg). Not below Dynamic Speed Bug (1.3 V Touchdown........Gently, avoid sideslip during touchdown Landing........

  • Page 184: Landing With Gear Up

    Section 3 - Emergency Procedures (EASA Approved) Emergency Landing Landing with Gear Up 3-9-05 Fuel weight........Reduce Passengers......... Brief Approach........Standard Flaps........... 40° Final approach speed....85 KIAS for 9921 lb (4500 kg). Not below Dynamic Speed Bug (1.3 V CABIN PRESSURE switch..

  • Page 185: Landing With Immobilized Horizontal Stabilizer

    Section 3 - Emergency Procedures (EASA Approved) Emergency Landing Landing without Elevator Control 3-9-06 continued WARNING STALLS ARE NOT PROTECTED WITH THE STICK PUSHER INOPERATIVE. STALLS MUST BE AVOIDED WHEN THE STICK PUSHER IS INOPERATIVE. EXCESSIVE WING DROP AND ALTITUDE LOSS MAY RESULT DURING STALL WITH FLAPS DOWN AND/OR WHEN POWER IS APPLIED.

  • Page 186: Ditching

    Section 3 - Emergency Procedures (EASA Approved) Emergency Landing Ditching 3-9-09 Landing gear....... CAUTION Heavy swell with light wind, ditch parallel to the swell. Strong wind, ditch into the wind. Passengers......... Brief ELT..........Set to ON Flaps........... 40° Final approach speed....88 KIAS for 9921 lb (4500 kg).

  • Page 187: Landing Gear System Failure

    Section 3 - Emergency Procedures (EASA Approved) Landing Gear System Failure 3-10 Landing Gear System Failure Landing Gear Fails to Retract 3-10-01 All Landing Gear Indicator Lights do not change to UP. Airspeed........Below 180 KIAS Note To cycle the landing gear for troubleshooting is not recommended. However, if during landing gear retraction moderate turbulence and/or considerable G-load was present, the pilot may consider cycling the landing gear once, at his own discretion.

  • Page 188: Gear Actuator Cntl

    Section 3 - Emergency Procedures (EASA Approved) Landing Gear System Failure Emergency Gear Extension 3-10-02 continued To lock the nose landing gear: Airspeed........Reduce power to idle and airspeed to minimum safe airspeed If 3 green lights illuminated: Aircraft......... Land as soon as practical Aircraft.........

  • Page 189: Invalid Gear Config

    Section 3 - Emergency Procedures (EASA Approved) Landing Gear System Failure Invalid Gear Config 3-10-04 On ground: Aircraft......... Do not take off Aircraft......... Maintenance required ---------- END ----------- Gear Power Fail 3-10-05 On ground: LDG CTL SEC circuit breaker Check. Do not reset unless tripped (Essential Bus A2).....
  • Page 190 Section 3 - Emergency Procedures (EASA Approved) Landing Gear System Failure This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 3-10-4...

  • Page 191: Flaps Failure

    Section 3 - Emergency Procedures (EASA Approved) Flaps Failure 3-11 Flaps Failure Flaps 3-11-01 On ground: FLAP circuit breaker (LH Rear Check circuit breaker P4)..........If tripped: FLAP circuit breaker (LH Rear Wait 5 minutes, reset circuit breaker P4)..........(max. 2 attempts) and continue normal operation if Flaps goes off...
  • Page 192 Section 3 - Emergency Procedures (EASA Approved) Flaps Failure Flaps 3-11-01 continued In flight - With potential flap asymmetry: Flaps shortly followed by Pusher Pusher Safe Mode illuminating. Flap system failed asymmetrically and stick pusher remains available in “safe” mode. CAUTION The approach speed must be increased for indicated flap position 12°...

  • Page 193: Stick Pusher Failure

    Section 3 - Emergency Procedures (EASA Approved) Stick Pusher Failure 3-12 Stick Pusher Failure Pusher 3-12-01 On ground: Pusher Test......... Carry out Pusher caution persists: Aircraft......... No flight permitted. Maintenance required --- END --- In flight: Pusher Test......... Carry out If Shaker 1 and 2 active and Pusher caution extinguished:...
  • Page 194 Section 3 - Emergency Procedures (EASA Approved) Stick Pusher Failure This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-12-2...

  • Page 195: Inadvertent Pusher/Shaker Operation

    Section 3 - Emergency Procedures (EASA Approved) Inadvertent Pusher/Shaker Operation 3-13 Inadvertent Pusher/Shaker Operation Pusher 3-13-01 Non-commanded pusher operation, rapid nose pitch-down motion. Note Control wheel force to stop pusher operation is 60 to 65 pounds. Control wheel......Hold against pusher action PUSHER INTR switch....

  • Page 196: Shaker

    Section 3 - Emergency Procedures (EASA Approved) Inadvertent Pusher/Shaker Operation Pusher 3-13-01 continued WARNING APPROACHES TO STALLS ARE NOT WARNED AND NATURAL STALLS ARE NOT PREVENTED WITH THE STICK SHAKER INOPERATIVE. ---------- END ----------- Shaker 3-13-02 Non-commanded shaker operation. AOA..........Decrease IAS..........
  • Page 197 Section 3 - Emergency Procedures (EASA Approved) Inadvertent Pusher/Shaker Operation Shaker 3-13-02 continued WARNING APPROACHES TO STALLS ARE NOT WARNED AND NATURAL STALLS ARE NOT PREVENTED WITH THE STICK SHAKER INOPERATIVE. STALLS MUST BE AVOIDED WHEN THE STICK PUSHER IS INOPERATIVE. EXCESSIVE WING DROP AND ALTITUDE LOSS MAY RESULT DURING STALL WITH FLAPS DOWN AND/OR WHEN POWER IS APPLIED.
  • Page 198 Section 3 - Emergency Procedures (EASA Approved) Inadvertent Pusher/Shaker Operation This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-13-4...

  • Page 199: Electrical Trim

    Section 3 - Emergency Procedures (EASA Approved) Electrical Trim 3-14 Electrical Trim Pitch Trim Runaway 3-14-01 Pitch Trim Runaway warning and voice callout “Trim Runaway”. TRIM INTERRUPT switch... PITCH TRIM circuit breaker PULL (Essential Bus A1)..... TRIM INTERRUPT switch... If trim runaway continues: TRIM INTERRUPT switch...

  • Page 200: Trim Runaway

    Section 3 - Emergency Procedures (EASA Approved) Electrical Trim Trim Runaway 3-14-03 Non-commanded trim operation, rapidly increasing out of trim forces. TRIM INTERRUPT switch... Circuit breaker of failed trim:..PULL Circuit Breaker Location PITCH TRIM Essential Bus PITCH TRIM ALTN Main Bus AIL TRIM Essential Bus...

  • Page 201: Electrical System Failures

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures 3-15 Electrical System Failures Electrical Power Loss 3-15-01 MASTER POWER switch.... Check ON and guarded BAT and GEN switches....Check ON If indication remains: Aircraft......... Land as soon as possible ---------- END ----------- Essential Bus 3-15-02...

  • Page 202: Avionics 2 Bus

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Avionics 1 Bus 3-15-03 continued STBY BUS switch....... Confirm set to ON Note The systems connected to the Standby bus on the left rear circuit breaker panel will be operative. Aircraft.........

  • Page 203: Generator 1 Bus

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Main Bus 3-15-05 continued Aircraft......... At pilots discretion, continue flight without services of failed bus or land as soon as practical. Depart icing conditions to positive SAT atmosphere if possible. Do not fly in icing conditions.

  • Page 204: Standby Bus

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Standby Bus 3-15-08 Standby Bus voltage is below 22 V. AV 1 BUS and STBY BUS Confirm set to ON switches........AV STBY PWR circuit breaker Confirm set (LH Power Junction Box).... Aircraft.........

  • Page 205: Generators

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Bus Tie 3-15-10 continued BUS TIE circuit breaker Reset (max 1 attempt only) (overhead panel)......Aircraft......... Land as soon as possible CAUTION Buses are being powered only from a battery. Possible battery current caution.

  • Page 206: Generator 1 Off

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Generators 3-15-11 continued CAUTION The following buses are automatically load shed (no additional Cautions will be shown) and the systems connected to them will be inoperative: − Generator 1 bus (Left rear CB panel) −...

  • Page 207: Generator 2 Off

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Generator 1 Off 3-15-12 continued GEN 1 switch......RESET then ON If GEN 1 does not reset: Aircraft......... At pilots discretion, continue flight without the services of the load shed systems and buses CAUTION The following buses are automatically load shed (no additional Cautions will...

  • Page 208: Generator 1 Volts

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Generator 2 Off 3-15-13 continued CAUTION The following buses are automatically load shed (no additional Cautions will be shown) and the systems connected to them will be inoperative: − Generator 2 bus (Right rear CB panel) −...

  • Page 209: Generator 2 Volts

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Generator 1 Volts 3-15-14 continued CAUTION The following buses are automatically load shed (no additional Cautions will be shown) and the systems connected to them will be inoperative: − Generator 1 bus (Left rear CB panel) −...

  • Page 210: Battery 1 Hot

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Generator 2 Volts 3-15-15 continued CAUTION The following buses are automatically load shed (no additional Cautions will be shown) and the systems connected to them will be inoperative: − Generator 2 bus (Right rear CB panel) −...

  • Page 211: Battery 2 Hot

    Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures Battery 1 Hot Battery 2 Hot 3-15-16 Battery 1 + 2 Hot continued Aircraft......... Land as soon as possible Note Battery 1 Hot Battery 2 Hot warnings are inoperative on aircraft with lead acid batteries installed.
  • Page 212 Section 3 - Emergency Procedures (EASA Approved) Electrical System Failures This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-15-12...

  • Page 213: Fuel System

    Section 3 - Emergency Procedures (EASA Approved) Fuel System 3-16 Fuel System Fuel Pressure Low 3-16-01 Fuel Pressure Low or both green PUMP indications on the MFD Fuel Window are cycling on and off every 10 seconds. On ground: Fuel filter faults......Check Fuel temperature......

  • Page 214: Fuel Press Sens Fail

    Section 3 - Emergency Procedures (EASA Approved) Fuel System Fuel Pressure Low 3-16-01 continued Fuel pumps......... Monitor automatic switching Note When the system switches FUEL PUMPs automatically to ON at lower engine power, this is a result of degraded ejector pump performance. Fuel Pressure Low persists: FUEL PUMP switches....

  • Page 215: Fuel Balance Fault

    Section 3 - Emergency Procedures (EASA Approved) Fuel System LH Fuel Low RH Fuel Low 3-16-03 LH + RH Fuel Low continued LH Fuel Low RH Fuel Low is on: FUEL PUMP switch (fuller side).. Fuel state........Monitor If no fuel leak is suspected and both LH Fuel Low RH Fuel Low are on:...
  • Page 216 Section 3 - Emergency Procedures (EASA Approved) Fuel System Fuel Balance Fault Fuel Imbalance 3-16-04 continued CAUTION If there are 3 segments or more difference between left and right, possible aileron deflection required for wings level flight, especially at low speed. If fuel leak from one wing is suspected: Aircraft.........

  • Page 217: Suspected Fuel Leak

    Section 3 - Emergency Procedures (EASA Approved) Fuel System Fuel Balance Fault Fuel Imbalance 3-16-04 continued If difference cannot be balanced: Aircraft......... Land as soon as possible Note If a prompt landing is not possible, keep high IAS to nearest airfield and consider burning off fuel until the fuel imbalance is not greater than 5 segments for landing.

  • Page 218: Fuel Quantity Fault

    Section 3 - Emergency Procedures (EASA Approved) Fuel System Suspected Fuel Leak 3-16-05 continued If fuel imbalance persists: Aircraft......... Land as soon as practical Note If a prompt landing is not possible, keep high IAS to nearest airfield and consider burning off fuel until the fuel imbalance is not greater than 5 segments for landing.

  • Page 219: Lh Fuel Pump

    Section 3 - Emergency Procedures (EASA Approved) Fuel System Loss of Digital Fuel Quantity Indication 3-16-07 continued If Fuel Flow digital indication is invalid: Fuel state........Monitor analogue Fuel Quantity on Fuel window or the digital fuel indication on Systems Summary window Note Continued flight is possible without digital Fuel Quantity (QTY) providing analogue fuel quantity is operating correctly.

  • Page 220: Lh + Rh Fuel Pump

    Section 3 - Emergency Procedures (EASA Approved) Fuel System LH Fuel Pump RH Fuel Pump 3-16-08 continued If fuel imbalance with affected pump failed OFF and affected tank higher: Aircraft......... Land as soon as possible. Fuel imbalance correction not possible Note If a prompt landing is not possible, keep high IAS to nearest airfield and consider burning off fuel until the fuel imbalance is not greater than 5 segments for landing.

  • Page 221: Fuel Imp Bypass

    Section 3 - Emergency Procedures (EASA Approved) Fuel System Fuel Pump Failure (Unannunciated) 3-16-10 continued − Both fuel pumps on for more than 10 seconds with 2 or more segments difference between left and right and no Fuel Pressure Low and no Fuel PRESS SENS Fail...

  • Page 222: Fuel Filter Blocked

    Section 3 - Emergency Procedures (EASA Approved) Fuel System Fuel IMP Bypass 3-16-11 continued If fuel icing suspected: FUEL PUMP switches....AUTO Note Consider to retract landing gear if extended. A retracted landing gear helps to reduce oil cooling. Engine......... Decrease power to increase fuel temperature If failure is still present and fuel icing is suspected:...

  • Page 223: Fuel Temp

    Section 3 - Emergency Procedures (EASA Approved) Fuel System Fuel TEMP 3-16-13 On ground: If indicated fuel temperature low (less than 12 °C): Oil Temperature......Monitor increasing Fuel temperature......Monitor increasing Engine......... Increase power slightly if necessary to increase oil heating If indicated fuel temperature high (at or above 105 °C): Engine.........
  • Page 224 Section 3 - Emergency Procedures (EASA Approved) Fuel System This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-16-12...

  • Page 225: Cabin Environment Failures

    Section 3 - Emergency Procedures (EASA Approved) Cabin Environment Failures 3-17 Cabin Environment Failures Cabin Pressure 3-17-01 Cabin pressure differential of less than -0.25 psi or greater than 6.35 psi is exceeded. Systems MFD ENVIRONMENT Check ∆P psi indication window........If ∆P less than -0.25 psi: Aircraft.........

  • Page 226: Cabin Altitude

    Section 3 - Emergency Procedures (EASA Approved) Cabin Environment Failures Cabin Pressure 3-17-02 continued If unsuccessful: CABIN PRESSURE switch..DUMP ACS EMERG shut off....PULL Main OXYGEN lever....Confirm ON Crew oxygen masks....Note Procedure to don the crew oxygen masks: Remove the normal headset.

  • Page 227: Acs Low Inflow

    Section 3 - Emergency Procedures (EASA Approved) Cabin Environment Failures Cabin Altitude 3-17-03 continued Crew oxygen masks....Note Procedure to don the crew oxygen masks: Remove the normal headset. Put the oxygen mask on. Check 100%. Put the normal headset back on. Set MIC SELECT switch on the rear left panel to MASK.

  • Page 228: Cpcs Fault

    Section 3 - Emergency Procedures (EASA Approved) Cabin Environment Failures ACS Low Inflow 3-17-04 continued ACS EMERG shut off....PULL Main OXYGEN lever....Confirm ON Crew oxygen masks....Note Procedure to don the crew oxygen masks: Remove the normal headset. Put the oxygen mask on.
  • Page 229 Section 3 - Emergency Procedures (EASA Approved) Cabin Environment Failures CPCS Fault 3-17-05 continued In flight and if ∆P and CAB ALT indications are available: CPCS MODE switch....MANUAL for at least 1 sec then AUTO CAS..........Check CPCS Fault remains: CPCS MODE switch....

  • Page 230: Ecs Fault

    Section 3 - Emergency Procedures (EASA Approved) Cabin Environment Failures CPCS Fault 3-17-05 continued Prior to landing: CABIN PRESSURE switch..DUMP --- END --- In flight and if ∆P and Cabin Altitude not displayed: Main OXYGEN lever....Confirm ON Crew oxygen masks....Note Procedure to don the crew oxygen masks: Remove the normal headset.

  • Page 231: Uncontrolled Cabin Pressure

    Section 3 - Emergency Procedures (EASA Approved) Cabin Environment Failures ECS Fault 3-17-06 continued If ACS BLEED AIR switch is inhibited and aircraft altitude is > 10,000 ft: ACS EMER shut off..... PULL Aircraft......... Carry out Maximum Rate Descent - 3-8-03 procedure Aircraft.........
  • Page 232 Section 3 - Emergency Procedures (EASA Approved) Cabin Environment Failures Uncontrolled Cabin Pressure 3-17-07 continued Prior to landing: CABIN PRESSURE switch..DUMP (if not selected earlier) ---------- END ----------- Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 3-17-8...

  • Page 233: Deice Systems

    Section 3 - Emergency Procedures (EASA Approved) Deice Systems 3-18 Deice Systems Propeller De Ice 3-18-01 WARNING THE LOSS OF PROPELLER DEICE IN ICING CONDITIONS CAN CAUSE SEVERE DEGRADATION IN AIRCRAFT SPEED AND CLIMB PERFORMANCE. PROP LOW SPEED switch..Confirm OFF (if installed)........

  • Page 234: De Ice Boots

    Section 3 - Emergency Procedures (EASA Approved) Deice Systems De Ice Boots 3-18-02 De Ice Boots with BOOTS off WARNING A BOOT DEICE FAILURE IN ICING CONDITIONS CAN CAUSE DEGRADATION OF AIRCRAFT SPEED AND CLIMB PERFORMANCE AND A PREMATURE STALL. FLAP POSITION IS LIMITED TO 0° WITH THIS FAILURE.

  • Page 235: Inertial Seperator

    Section 3 - Emergency Procedures (EASA Approved) Deice Systems De Ice Boots 3-18-02 continued CAUTION On landing approach after boot failure (flaps 0°), the PFD dynamic speed bug will not be correct and should not be used as reference. CAUTION The total landing distance will be longer by up to 160%.

  • Page 236: Lh Windshield Heat

    Section 3 - Emergency Procedures (EASA Approved) Deice Systems Inertial Seperator 3-18-03 continued Aircraft......... DEPART ICING CONDITIONS to positive SAT atmosphere, if possible Aircraft......... Avoid further icing conditions If any attained performance degradation continues: Aircraft......... Land as soon as possible ---------- END ----------- LH Windshield Heat RH Windshield Heat...

  • Page 237: Aoa De Ice

    Section 3 - Emergency Procedures (EASA Approved) Deice Systems AOA De Ice 3-18-06 WARNING AN AOA PROBE DEICE FAILURE IN ICING CONDITIONS CAN CAUSE A FALSE ACTIVATION OF THE STALL PROTECTION SYSTEM. PROBES switch......Set to OFF and wait 3 minutes PROBES switch......

  • Page 238: Pitot 1 Heat

    Section 3 - Emergency Procedures (EASA Approved) Deice Systems Pitot 1 Heat Pitot 2 Heat 3-18-07 WARNING A PITOT AND STATIC DEICE FAILURE IN ICING CONDITIONS CAN CAUSE AN INCORRECT INDICATION ON THE ASI AND/OR ALTIMETER AND VSI. PROBES switch......Set to OFF then ON again LH PITOT DE-ICE circuit Check.

  • Page 239: Pusher

    Section 3 - Emergency Procedures (EASA Approved) Deice Systems Static Heat 3-18-08 continued RH STATIC DE-ICE circuit Check. Do not reset unless tripped breaker (Main Bus F2)....If caption returns to normal operation: Aircraft......... Continue flight and monitor system If caption stays in failure status: Autopilot........
  • Page 240 Section 3 - Emergency Procedures (EASA Approved) Deice Systems Pusher 3-18-09 continued PROP DE-ICE circuit breaker Check. Do not reset unless tripped (LH PJB)........INERT SEP circuit breaker Check. Do not reset unless tripped (Essential Bus F2)..... If captions return to normal operation within 30 seconds: Aircraft.........

  • Page 241: Boots Temp Limit

    Section 3 - Emergency Procedures (EASA Approved) Deice Systems Boots TEMP Limit 3-18-10 De ice boots switch has been inadvertently left in the ON position during climb or descent through the boots temperature limit, or the boots switch has been inadvertently switched ON without observing the boots temperature limits.
  • Page 242 Section 3 - Emergency Procedures (EASA Approved) Deice Systems This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-18-10...

  • Page 243: Passenger And Cargo Door

    Section 3 - Emergency Procedures (EASA Approved) Passenger and Cargo Door 3-19 Passenger and Cargo Door Passenger Door Cargo Door 3-19-01 Pax + Cargo Door On ground: Passenger and/or Cargo Door..Visually check for the correct locking of the door latches (green indicators visible) Passenger Door......
  • Page 244 Section 3 - Emergency Procedures (EASA Approved) 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...

  • Page 245: Cracked Window In Flight

    Section 3 - Emergency Procedures (EASA Approved) Cracked Window in Flight 3-20 Cracked Window in Flight Cracked Window in Flight 3-20-01 All occupants....... Check seat lap and shoulder belts are fastened and the lap belt tightened Airspeed........Reduce IAS to practical minimum Aircraft.........
  • Page 246 Section 3 - Emergency Procedures (EASA Approved) 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...

  • Page 247: Wheel Brake Failure

    Section 3 - Emergency Procedures (EASA Approved) Wheel Brake Failure 3-21 Wheel Brake Failure Wheel Brake Failure 3-21-01 Wheel brakes ineffective and/or pedal excessively soft when pressed. Landing + Taxi......Use reverse power, BETA and Nose Wheel steering ---------- END ----------- Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020...
  • Page 248 Section 3 - Emergency Procedures (EASA Approved) Wheel Brake Failure This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-21-2...

  • Page 249: Apex Failures

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures 3-22 APEX Failures All APEX display units indicate a red X or blank: 3-22-01 Primary flight information.... Use ESIS to control safe aircraft flight path continuation Autopilot........Use the autopilot (if available) with mode annunciations on the flight controller Note Basic autopilot operation is independent of display unit availability.

  • Page 250: Check Du 1

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures All APEX display units indicate a red X or blank: 3-22-01 continued Aircraft......... Refer to CAS captions to cross check that all issues are addressed If failure remains: Aircraft......... Land as soon as practical using minimum engine power to avoid exceeding engine limits Prior to landing:...

  • Page 251: Check Du 1+2+3+4

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures Check DU 1 AGM 1 Fail 3-22-03 Check DU 4 AGM 2 Fail continued If red X on display: Reversion Controller....For DU 1 set control knob to AGM 2 For Du 4 set control knob to AGM 1 ---------- END ----------- Check DU 1+2+3+4 3-22-04...

  • Page 252: Du 1 Overheat

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures DU 1 Overheat DU 2 Overheat 3-22-05 DU 3 Overheat DU 4 Overheat Note Or any other combination of 2 or 3 DU Overheat failure indications. Displays........Check relevant display and treat as suspect Reversion Controller....

  • Page 253: Lh Pfd Ctrl Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures DU 1+2+3+4 Overheat 3-22-06 continued Crew oxygen masks....Note Procedure to don the crew oxygen masks: Remove the normal headset. Put the oxygen mask on. Check 100%. Put the normal headset back on. Set MIC SELECT switch on the rear left panel to MASK.

  • Page 254: Rh Pfd Ctrl Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures RH PFD CTRL Fail 3-22-08 LH PFD Controller....... Push PFD button to operate RH PFD Note X PFD CTRL ACTIVE annunciation will be displayed in amber along bottom right of the ADI on copilot PFD (if installed). PFD CTRL INACTIVE will be displayed on pilot PFD.

  • Page 255: Check Engine Display

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures Check Engine Display 3-22-12 PFD engine data suspect. Display........Cross check pilot PFD data with copilot PFD data If data confirmed to be suspect: Reversion Controller....Set pilot PFD control knob to AGM2 If data remains suspect: Aircraft.........

  • Page 256: Airspeed Display Replaced With Red X

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures HDG FAIL 3-22-15 continued ADHRS pushbutton on PFD Press to bring the other ADAHRS Controller........channel Heading data onto PFD ---------- END ----------- Airspeed Display Replaced with Red X 3-22-16 Airspeed Tape data has become invalid. Airspeed data......

  • Page 257: Ias

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures IAS? ALT? 3-22-19 Airspeed and/or barometric Altitude miscompare between ADAHRS 1 and ADAHRS 2 by more than 10 KIAS / 200 feet. Note ADAHRS Channel A receives dynamic and static pressure information form the LH pitot static system, ADAHRS Channel B and the ESIS from he RH pitot static system.

  • Page 258: Hdg

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures IAS? ALT? 3-22-19 continued CAUTION The total landing distance will be longer by up to 71%. Refer to Section 5, Performance, Flight in Icing Conditions, Flight in Icing Conditions - Landing Performance for the exact landing distance calculation.

  • Page 259: Pitch

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures HDG? 3-22-20 continued If flight condition and pilot workload permit, attempt to realign the ADAHRS channels: Aircraft......... Fly straight and level for 2 minutes Note In regions where magnetic inclination (dip angle) exceeds 80°, erroneous magnetic heading indications may be experienced.

  • Page 260: Apex Miscellaneous - On Ground Only

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures APEX Miscellaneous - On Ground Only 3-22-24 Indication: − APM 1 Fail , or − APM 2 Fail , or − APM 1+2 Fail , or − CMS 1+2 Fail , or −...

  • Page 261: Mau B Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures MAU A Fail 3-22-25 continued Landing........Engine power may remain at flight idle. Reverse operation is not affected by this fault. ---------- END ----------- MAU B Fail 3-22-26 MAU CH. B1 circuit breaker Open, Wait 2 seconds and close (Standby Bus Z3).......

  • Page 262: Aural Warning Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures Aural Warning Fail 3-22-28 Note All aural warnings except TCAS and TAWS are inhibited, including FAS and CAS. Aural Warning Inhibit switch (left Check in ON position rear panel)........---------- END ----------- DME 1 Fail 3-22-29 PFD Controller......

  • Page 263: Adc A Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures ADC A Fail 3-22-31 Pilot PFD Controller....Press ADHRS button to select ADAHRS Pilots PFD Window..... Confirm ADAHRS 2 flag which indicates attitude, heading and air data same source as copilot PFD. Compare with Electronic Standby Instrument System (ESIS) CAUTION...

  • Page 264: Adc A+B Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures ADC B Fail 3-22-32 continued CAUTION The autopilot will disengage. Do not use VNAV function of the FMS. Autopilot........Re-engage, after PFD data displayed Altitude........Determine using ADAHRS 2 source Altitude........Cross-check aircraft altitude using ESIS.
  • Page 265 Section 3 - Emergency Procedures (EASA Approved) APEX Failures ADC A+B Fail 3-22-33 continued CAUTION The following services will be inoperative: − Autopilot (abnormal disengage) − Overspeed warning − Altitude Alert Monitor − Air data to other systems Do not use VNAV functions of the FMS. Cabin Altitude comes on: Main OXYGEN lever....

  • Page 266: Ahrs A Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures AHRS A Fail 3-22-34 Pilot PFD Controller....Press ADHRS button to select ADAHRS Pilot PFD window......Confirm ADAHRS 2 flag which indicates attitude, heading and air data same source as copilot PFD. Compare with Standby Instrument System CAUTION The autopilot will revert to roll and pitch mode.

  • Page 267: Flt Ctrl Ch A Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures AHRS A+B Fail 3-22-36 continued CAUTION The following services will be inoperative: − Autopilot (abnormal disengage) − INAV map. Do not use VNAV function of the FMS. If flight conditions and pilot workload permits, attempt to realign AHRS 1 and/or AHRS 2: ADHRS CH.

  • Page 268: Flt Ctrl Ch A+B Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures FLT CTRL Ch A+B Fail 3-22-38 Note FLT CTRL CAS messages are amber on the ground, but cyan in the air. Loss of both Flight Controller channels. CAUTION Loss of Autopilot. Loss of Flight Director.

  • Page 269: Unable Fms-Gps Mon

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures FMS1-GPS1+2 Pos Misc FMS2-GPS1+2 Pos Misc 3-22-40 continued CAUTION Loss of GPS or FMS navigation RAIM unavailable Note With dual FMS, if only one FMS shows a position miscompare, select the other FMS to avoid loss of navigation and RAIM functionality.

  • Page 270: Mmdr 1 Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures Unable FMS-GPS Mon 3-22-41 continued If GPS 2 is installed: GPS 2 Circuit Breaker (Avionic 2 Open, wait 2 seconds and close X1)........Unable FMS-GPS Mon remains and the DR flag is shown on the PFD: Aircraft (If in flight).......

  • Page 271: Mmdr 2 Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures MMDR 1 Fail 3-22-42 continued If COM 1, NAV 1 and ADF remain not available: COM and NAV......Use COM 2 and NAV 2 ---------- END ----------- MMDR 2 Fail 3-22-43 MMDR 2 PRI Circuit Breaker Reset (Main Bus...

  • Page 272: Mmdr 2 Overheat

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures MMDR 2 Overheat 3-22-46 Note MMDR 2 transmit capability is reduced because internal temperature of unit is too high. MMDR 2 may become operative again after a period of time. COM and NAV......Use COM 1, NAV 1 and ADF ---------- END ----------- MMDR 1+2 Overheat...

  • Page 273: Ascb Fail

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures ADS-B Out 3-22-48 continued Dual Transponder installation XPDR 1 Fail is on: PFD radio window....... Press bezel button adjacent to XPDR 1 window PFD Controller......Press DETAIL button XPDR detail page....... Press XPDR SEL bezel button to change to XPDR 2 XPDR 2 Fail...
  • Page 274 Section 3 - Emergency Procedures (EASA Approved) APEX Failures ASCB Fail 3-22-49 continued Displays........Monitor for remainder of flight --- END --- Dual ASCB Failure Displays suspect (Loss of Use Electronic Standby Instrument displayed data)......System (ESIS) If above 10,000 ft and ΔP and CAB ALT indications are suspect or lost: Main OXYGEN lever....

  • Page 275: Automatic Flight Control System Failures

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures Automatic Flight Control System Failures 3-22-50 AFCS uncommanded deviation from flight path Abrupt control and/or airplane motion Accomplish steps 1 and 2 simultaneously. Airplane Control Wheel....GRASP FIRMLY and regain aircraft control Autopilot Disengage switch..
  • Page 276 Section 3 - Emergency Procedures (EASA Approved) APEX Failures Automatic Flight Control System Failures 3-22-50 continued If no AFCS associated CAS messages: Aircraft......... Attempt to re-engage autopilot once Maximum Altitude losses due to autopilot malfunction: Configuration Altitude Loss Cruise, Climb, Descent 480 ft APR 3°...
  • Page 277 Section 3 - Emergency Procedures (EASA Approved) APEX Failures Automatic Flight Control System Failures 3-22-50 continued If failure persists: Aircraft......... At pilot's discretion continue flight without the yaw damper or land as soon as practical --- END --- Yaw damper is OFF above 15,500 ft: YD Off shows on the CAS window.

  • Page 278: Hsi1 Is Mag Trk

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures HSI1 is MAG TRK HSI2 is MAG TRK 3-22-51 HSI1+2 is MAG TRK The Primus APEX system has switched the long term reference source for the HSI heading from a gyro based magnetically corrected heading output to a magnetically compensated Track based display.

  • Page 279: Stuck Mic

    Section 3 - Emergency Procedures (EASA Approved) APEX Failures CAS Miscompare 3-22-53 continued Aircraft......... Ascertain the reason for the miscompare flag and take appropriate action, using the affected CAS message and Abnormal Procedures ---------- END ----------- Stuck Mic 3-22-54 Continuous transmit indication on one of the MMDRs and/or a “Stuck Mic” indication on the Radio Window.
  • Page 280 Section 3 - Emergency Procedures (EASA Approved) APEX Failures This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3-22-32...
  • Page 281 Section 3A - Abnormal Procedures (EASA Approved) Table of Contents SECTION 3A Abnormal Procedures (EASA Approved) Table of Contents Subject Page 3A-1 General 3A-1-1 3A-1-1 General 3A-1-1 3A-2 CAS Advisories 3A-2-1 3A-2-1 CAS Advisories 3A-2-1 3A-3 CAS Status 3A-3-1 3A-3-1 CAS Status 3A-3-1 3A-4...
  • Page 282 Section 3A - Abnormal Procedures (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...
  • Page 283 Section 3A - Abnormal Procedures (EASA Approved) General 3A-1 General 3A-1-1 General This section provides a description and any actions that can be taken for the Crew Alerting System (CAS) cyan advisory and white status messages. There are failures of system module or element parts that are not of an emergency nature.
  • Page 284 Section 3A - Abnormal Procedures (EASA Approved) General This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3A-1-2...
  • Page 285 Section 3A - Abnormal Procedures (EASA Approved) CAS Advisories 3A-2 CAS Advisories 3A-2-1 CAS Advisories This section provides a description and any actions that can be taken for the Crew Alerting system (CAS) cyan advisory messages. These cyan advisory messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL.
  • Page 286 Section 3A - Abnormal Procedures (EASA Approved) CAS Advisories CAS Advisory Message Meaning, Effects and Possible Actions YD Fail Yaw Damper has failed below 15,500 ft PA. Minimize sideslip by using rudder pedals and manual rudder trim. Above 15,500 ft PA, refer to the Automatic Flight Control System Failures - 3-22-50 procedure.
  • Page 287 Section 3A - Abnormal Procedures (EASA Approved) CAS Advisories CAS Advisory Message Meaning, Effects and Possible Actions FMS Synch Error FMS1 and FMS2 are operating independently (not synchronized). Non-coupled FMS will not receive any changes made to the flight plan. See Section 7-33, Synchronization, for a description of how to synchronize FMS1 and FMS2.
  • Page 288 Section 3A - Abnormal Procedures (EASA Approved) CAS Advisories CAS Advisory Message Meaning, Effects and Possible Actions EPECS Fault On ground: Engine data from one EEC channel is not available for display. In flight: Monitor engine parameters. Consider diversion to an airfield with appropriate maintenance capability.
  • Page 289 Section 3A - Abnormal Procedures (EASA Approved) CAS Advisories CAS Advisory Message Meaning, Effects and Possible Actions TSC Fail The Touch Screen Controller is turned off or has failed. Make sure that the TSC is turned on using the TSC dimming knob on the display reversionary control panel.
  • Page 290 Section 3A - Abnormal Procedures (EASA Approved) CAS Advisories This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3A-2-6...
  • Page 291 Section 3A - Abnormal Procedures (EASA Approved) CAS Status 3A-3 CAS Status 3A-3-1 CAS Status This section provides a description and any actions that can be taken for the Crew Alerting system (CAS) white status messages. These white status messages require maintenance action if they cannot be cleared before flight, or dispatch the aircraft under the provisos of an approved and permissible PC-12 aircraft MEL.
  • Page 292 Section 3A - Abnormal Procedures (EASA Approved) CAS Status On Ground CAS Status Meaning, Effects and Possible Actions Message Engine Exceedance Reminds on the ground that during flight a WARNING was displayed for an exceedance of one or more of the following engine parameters: −...
  • Page 293 Section 3A - Abnormal Procedures (EASA Approved) CAS Status On Ground CAS Status Meaning, Effects and Possible Actions Message EPECS TLD The engine is cleared for Time Limited Dispatch (TLD), follow the applicable time limits. Dry Motoring Indicates that a dry motoring run is in progress. Maintenance Feather Indicates the propeller is feathered for maintenance purposes.
  • Page 294 Section 3A - Abnormal Procedures (EASA Approved) CAS Status This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 3A-3-4...
  • Page 295 Section 3A - Abnormal Procedures (EASA Approved) Primary Altimeter Diverge by 200 ft or More 3A-4 Primary Altimeter Diverge by 200 ft or More If able to identify defective altimetry system Determine aircraft altitude using operating ADAHRS channel. Disengage autopilot and flight director. Select operating ADAHRS channel, using the flight director couple select switch (L/R).
  • Page 296 Section 3A - Abnormal Procedures (EASA Approved) Primary Altimeter 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...
  • Page 297 Section 3A - Abnormal Procedures (EASA Approved) Loss of Autopilot Altitude Hold Function in RVSM Airspace 3A-5 Loss of Autopilot Altitude Hold Function in RVSM Airspace 3A-5-1 Procedure: Loss of Autopilot Altitude Hold Function in RVSM Airspace Loss of Autopilot Altitude Hold Function in 3A-5-01 RVSM Airspace Autopilot........
  • Page 298 Section 3A - Abnormal Procedures (EASA Approved) Procedure: Loss of Autopilot 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...
  • Page 299 Section 3A - Abnormal Procedures (EASA Approved) Flight Training 3A-6 Flight Training Emergency Gear Extension Lever Reset 3A-6-01 If Emergency Gear Extension Lever has been pulled in flight: Landing Gear Selector....Emergency Gear Extension Press black release latch and push red Lever...........
  • Page 300 Section 3A - Abnormal Procedures (EASA Approved) Flight Training This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3A-6-2...
  • Page 301 Section 3A - Abnormal Procedures (EASA Approved) Smartview 3A-7 Smartview 3A-7-1 Smartview Procedures Smartview abnormal procedures 3A-7-01 If Smartview information is inconsistent with APEX primary flight indications: PFD..........Select OVRLY menu SV..........Note SV can be set to OFF by deselecting the checkmark “SVS ON”. PFD..........
  • Page 302 Section 3A - Abnormal Procedures (EASA Approved) Smartview status and failure indications 3A-7-2 Smartview status and failure indications Smartview related status and failure indications on the SV Status / Failure field: SV Indication Description Position and altitude used to position the synthetic scenery meets the integrity requirements.
  • Page 303 Section 3A - Abnormal Procedures (EASA Approved) LPV/LP Approach (Optional) 3A-8 LPV/LP Approach (Optional) If PRIMUS APEX avionics suite GPS navigation information is not available or invalid, utilize remaining operational navigation equipment as appropriate. Degradation of Approach Capability ( LPV UNVL LP UNVL ) in the terminal or initial approach phase of flight (prior to FAF).
  • Page 304 Section 3A - Abnormal Procedures (EASA Approved) 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...
  • Page 305 Section 3A - Abnormal Procedures (EASA Approved) Engine Dry Motoring 3A-9 Engine Dry Motoring Dry Motoring Run 3A-9-01 Note This procedure is used to remove internally trapped smoke, fuel and vapor within the engine gas path. Do a dry motoring cycle once the ITT has stabilized. Note A dry motoring run can always be aborted by setting the Master Power switch to EMERGENCY OFF.
  • Page 306 Section 3A - Abnormal Procedures (EASA Approved) Engine Dry Motoring Dry Motoring Run 3A-9-01 continued EXT PWR switch......For shutdown, refer to Section 4-18, Shutdown. ---------- END ----------- Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 3A-9-2...
  • Page 307 Section 4 - Normal Procedures (EASA Approved) Table of Contents SECTION 4 Normal Procedures (EASA Approved) Table of Contents Subject Page General 4-1-1 Airspeeds for Normal Operations 4-2-1 Preflight Inspection 4-3-1 4-3-01 Empennage 4-3-1 4-3-02 Right Wing Trailing Edge 4-3-2 4-3-03 Right Wing Leading Edge 4-3-2...
  • Page 308 Section 4 - Normal Procedures (EASA Approved) Table of Contents Subject Page 4-12-01 Cruise 4-12-1 4-12-02 Cruise within RVSM Airspace 4-12-1 4-13 Descent 4-13-1 4-13-01 Descent 4-13-1 4-14 Before Landing 4-14-1 4-14-01 Approach Check 4-14-1 4-14-02 Final Check 4-14-1 4-15 Balked Landing (Go-Around) 4-15-1 4-15-01...

  • Page 309: General

    Section 4 - Normal Procedures (EASA Approved) General General This section provides the normal operating procedures. All of the procedures required by regulation as well as those procedures which have been determined as necessary for the operation of this airplane are provided. Normal operating procedures associated with optional systems or equipment which require supplements are contained in Section 9, Supplements, General.
  • Page 310 Section 4 - Normal Procedures (EASA Approved) General This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-1-2...

  • Page 311: Airspeeds For Normal Operations

    Section 4 - Normal Procedures (EASA Approved) Airspeeds for Normal Operations Airspeeds for Normal Operations Airspeeds for normal operations are listed below. Unless otherwise noted, all airspeeds are based on a maximum takeoff weight of 10,450 lb (4740 kg) at sea level under ISA standard day conditions.
  • Page 312 Section 4 - Normal Procedures (EASA Approved) Airspeeds for Normal Operations Balked Landing (Go-Around): TO/Pwr, Flaps 15º, LG down 98 KIAS TO/Pwr, Flaps 30º, LG down 89 KIAS TO/Pwr, Flaps 40º, LG down 85 KIAS TO/Pwr, Flaps 15º, LG down, Pusher Ice 105 KIAS Mode Maximum Demonstrated Crosswind for Takeoff and Landing (not a limitation):...

  • Page 313: Preflight Inspection

    Section 4 - Normal Procedures (EASA Approved) Preflight Inspection Preflight Inspection Empennage 4-3-01 Luggage........CHECKED and SECURED Cargo (Combi Interior)....CHECK that cargo is located against retainer angles installed on seat rails Tie Down Straps (Combi Interior) CHECK fittings properly inserted into seat rails and that the straps are tight Cargo Door.........

  • Page 314: Right Wing Leading Edge

    Section 4 - Normal Procedures (EASA Approved) Preflight Inspection Empennage 4-3-01 continued Power junction box circuit CHECK IN breakers........Steering bar........ STOWED and SECURED Battery......... CONNECTED Battery compartment....CHECK CLOSED ---------- END ----------- Right Wing Trailing Edge 4-3-02 Flaps........... CHECK CONDITION Aileron and flettner tab....

  • Page 315: Nose Section

    Section 4 - Normal Procedures (EASA Approved) Preflight Inspection Nose Section 4-3-04 Service Bay (right) (If a standard oxygen system is installed): Oxygen Press......CHECK Oxygen and ECS Doors....CLOSED Oxygen rupture disc....INTACT --- END --- Engine Area: Cowling RH......... CHECK and SECURE Propeller - Blade Anchor.....

  • Page 316: Left Wing Leading Edge

    Section 4 - Normal Procedures (EASA Approved) Preflight Inspection Nose Section 4-3-04 continued WARNING DO NOT TOUCH OUTPUT CONNECTORS OR COUPLING NUTS OF IGNITION EXCITER WITH BARE HANDS. Oil Quantity......... CHECK SIGHT GLASS AND DIPSTICK FOR SECURITY (green markings aligned) Check oil level in green range of sight glass within 10 to 20 minutes after engine shut down.

  • Page 317: Left Wing Trailing Edge

    Section 4 - Normal Procedures (EASA Approved) Preflight Inspection Left Wing Leading Edge 4-3-05 continued Nav/Strobe light......CHECK CONDITION General condition......CHECK ---------- END ----------- Left Wing Trailing Edge 4-3-06 Static discharge wicks....CHECK SECURITY and CONDITION Fuel tank vents (three)....CLEAR of OBSTRUCTIONS Aileron and trim tab.....

  • Page 318: Cockpit

    Section 4 - Normal Procedures (EASA Approved) Preflight Inspection Cockpit 4-3-08 Note Items marked thus: * only necessary on first flight of day. Flight Control Lock...... REMOVED and placed in STOWAGE POINT EMERG COM 1 switch....NORM Aural Warning Inhibit Switch..* LH MASK/MIC switch....
  • Page 319 Section 4 - Normal Procedures (EASA Approved) Preflight Inspection Cockpit 4-3-08 continued PASSENGER WARNING switches........EPS switch........MASTER POWER switch.... ON and GUARDED. Check condition of guard BAT 1, BAT 2, STBY BUS... CHECK OFF EXT PWR........CHECK CENTER AV 2 BUS, CABIN BUS, AV 1 CHECK ON BUS, GEN 1, GEN 2....
  • Page 320 Section 4 - Normal Procedures (EASA Approved) Preflight Inspection This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-3-8...

  • Page 321: Before Starting Engine

    Section 4 - Normal Procedures (EASA Approved) Before Starting Engine Before Starting Engine Before Starting Engine 4-4-01 Preflight inspection...... COMPLETE STBY BUS switch....... ON wait until MFD powers up (30 secs) prior to switching batteries on Display reversion control panel... PILOTS PFD NORM, CO-PILOTS PFD NORM (if installed) Adjust lower MFD brightness and set...
  • Page 322 Section 4 - Normal Procedures (EASA Approved) Before Starting Engine Before Starting Engine 4-4-01 continued FIRE WARN test switch....PUSH. (CAS Engine Fire and Fire Detector annunciations ON while switch is pushed, callout heard if powered from GPU) LAMP test switch......PUSH.

  • Page 323: Engine Starting

    Section 4 - Normal Procedures (EASA Approved) Engine Starting Engine Starting Engine Start (With or Without External Power) 4-5-01 External lights......AS REQUIRED Note Avoid prolonged use of the beacon and logo lights (if installed), as this can cause a decrease in battery power and affect the engine starting. Propeller area......
  • Page 324 Section 4 - Normal Procedures (EASA Approved) Engine Starting Engine Start (With or Without External Power) 4-5-01 continued ITT..........MONITOR − MAXIMUM 1000 °C − 900 - 1000 °C for max 5 sec. − 850 - 900 °C for max 20 sec. If there is a rapid increase in ITT towards 1000 °C and the start is not automatically aborted, then: STARTER switch......

  • Page 325: Before Taxiing

    Section 4 - Normal Procedures (EASA Approved) Before Taxiing Before Taxiing Before Taxiing 4-6-01 Flaps Lever......... 15° If icing conditions expected or first flight of the day: ICE PROTECTION switches..Set all on for 1 minute (windshield heavy) CAS window........ No cautions.
  • Page 326 Section 4 - Normal Procedures (EASA Approved) Before Taxiing Before Taxiing 4-6-01 continued PFD Engine Window....Check T1 Note Engine takeoff power is calculated based on displayed T1. ---------- END ----------- Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-6-2...

  • Page 327: Taxiing

    Section 4 - Normal Procedures (EASA Approved) Taxiing Taxiing Taxiing 4-7-01 EXTERNAL LIGHTS switches..AS REQUIRED PASSENGER WARNING switches (if installed)....Parking Brake......RELEASE Brakes......... CHECK PCL..........CHECK beta is available, return to IDLE Display units........ Compare ADIs, speeds, Altitude, Heading and check no flags CAUTION To avoid possible propeller damage, do not allow stabilized propeller...
  • Page 328 Section 4 - Normal Procedures (EASA Approved) Taxiing This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-7-2...

  • Page 329: Before Takeoff

    Section 4 - Normal Procedures (EASA Approved) Before Takeoff Before Takeoff Before Departure 4-8-01 Takeoff power setting....CALCULATED Engine instruments..... CHECK Flaps........... 15° (for reduced takeoff distance flap 30° may be used) Trim..........SET GREEN range If CG is 236 inches (6 meters) or SET GREEN DIAMOND further aft of datum......
  • Page 330 Section 4 - Normal Procedures (EASA Approved) Before Takeoff This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-8-2...

  • Page 331: Takeoff

    Section 4 - Normal Procedures (EASA Approved) Takeoff Takeoff Takeoff 4-9-01 ACS BLEED AIR switch....INHIBIT (If static takeoff torque is below flat rating and additional torque should be achieved.) POWER CONTROL LEVER..SET to T/O (EPECS sets power to ambient conditions) CAUTION Monitor for exceedances.
  • Page 332 Section 4 - Normal Procedures (EASA Approved) Takeoff This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-9-2...

  • Page 333: Flight Into Known Icing Conditions

    Section 4 - Normal Procedures (EASA Approved) Flight into Known Icing Conditions 4-10 Flight into Known Icing Conditions Flight into Known Icing Conditions 4-10-01 WARNING FLIGHT IN ICING CONDITIONS IS PROHIBITED IF THERE IS A KNOWN FAILURE OF ANY OF THE ICE PROTECTION SYSTEMS. WARNING DURING FLIGHT IN ICING CONDITIONS OR FLIGHT WITH ANY VISIBLE ICE ACCRETION ON THE AIRFRAME, THE FOLLOWING FLAP EXTENSION LIMITS...
  • Page 334 Section 4 - Normal Procedures (EASA Approved) Flight into Known Icing Conditions Flight into Known Icing Conditions 4-10-01 continued MFD ICE PROTECTION window MONITOR for correct function of ice protection systems WARNING IF ANY OF THE AIRCRAFT ICE PROTECTION SYSTEMS FAIL DURING FLIGHT IN ICING CONDITIONS, EXIT ICING CONDITIONS.

  • Page 335: Climb

    Section 4 - Normal Procedures (EASA Approved) Climb 4-11 Climb Climb 4-11-01 Ice Protection System....AS REQUIRED Autopilot........AS REQUIRED FMS Auto speed (if selected)..Verify and confirm correct POWER CONTROL LEVER..SET to MCP (EPECS sets power to ambient conditions) CAUTION Monitor for exceedances.
  • Page 336 Section 4 - Normal Procedures (EASA Approved) Climb This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-11-2...

  • Page 337: Cruise

    Section 4 - Normal Procedures (EASA Approved) Cruise 4-12 Cruise Cruise 4-12-01 Cabin Pressurization....Monitor POWER CONTROL LEVER..SET as required Engine instruments..... MONITOR Fuel state........MONITOR Note On longer flights the digital fuel quantity value can be updated to the actual fuel content by pressing the FUEL RESET soft key, on Systems MFD FUEL window.
  • Page 338 Section 4 - Normal Procedures (EASA Approved) Cruise This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-12-2...

  • Page 339: Descent

    Section 4 - Normal Procedures (EASA Approved) Descent 4-13 Descent Descent 4-13-01 ATIS / Briefing......RECEIVED / PERFORMED Ice Protection System....AS REQUIRED POWER CONTROL LEVER..SET to desired torque FMS Auto speed (if selected)..Verify and confirm correct CPCS system window....CHECK landing field elevation set Passengers.........
  • Page 340 Section 4 - Normal Procedures (EASA Approved) Descent This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-13-2...

  • Page 341: Before Landing

    Section 4 - Normal Procedures (EASA Approved) Before Landing 4-14 Before Landing Approach Check 4-14-01 Altimeter........Ice Protection system....AS REQUIRED Inertial Separator......OPEN, if operating on unprepared surface or for birdstrike protection Fuel Quantity....... CHECK Landing Gear......DOWN (below 180 KIAS) Taxi and Landing Lights....
  • Page 342 Section 4 - Normal Procedures (EASA Approved) Before Landing Final Check 4-14-02 continued Speed.......... REDUCE to Dynamic Speed Bug (1.3 V and STABILIZED Boot failure........130 KIAS AOA Deice or PUSHER ICE 105 KIAS MODE failure......Cabin Pressurization....Diff Pressure below 0.7 psi decreasing AP, AT (if installed), YD (prior to DISENGAGED (use red AP QD button on landing)........

  • Page 343: Balked Landing (Go-Around)

    Section 4 - Normal Procedures (EASA Approved) Balked Landing (Go-Around) 4-15 Balked Landing (Go-Around) Balked Landing (Go-Around) 4-15-01 Go Around switch (if Autopilot PRESS engaged)........POWER CONTROL LEVER..SET to T/O (EPECS sets power to ambient conditions) CAUTION Monitor for exceedances. EPECS will not protect against all possibilities of exceedance.
  • Page 344 Section 4 - Normal Procedures (EASA Approved) Balked Landing (Go-Around) This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-15-2...

  • Page 345: Landing

    Section 4 - Normal Procedures (EASA Approved) Landing 4-16 Landing Normal 4-16-01 Aircraft......... Touch down main wheels first Aircraft......... Do not flare with high pitch angle Power Control Lever....IDLE DETENT Braking........AS REQUIRED ---------- END ----------- Short Field 4-16-02 Aircraft.........
  • Page 346 Section 4 - Normal Procedures (EASA Approved) Landing This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-16-2...

  • Page 347: After Landing

    Section 4 - Normal Procedures (EASA Approved) After Landing 4-17 After Landing After Landing 4-17-01 When runway vacated: Flaps........... Trims........... SET GREEN RANGE External Lights......AS REQUIRED Ice Protections switches..... OFF or as required Transponder........ STBY or check GND WX Radar........STBY ---------- END ----------- Pilot's Operating Handbook...
  • Page 348 Section 4 - Normal Procedures (EASA Approved) After Landing This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-17-2...

  • Page 349: Shutdown

    Section 4 - Normal Procedures (EASA Approved) Shutdown 4-18 Shutdown Shutdown 4-18-01 WARNING IN CASE OF ENGINE FIRE, DO THE PROCEDURE. ENGINE FIRE - 3-7-02 Note − Allow ITT to stabilize at least two minutes at ground idle − Monitor compressor deceleration after shutdown for possible engine damage −...
  • Page 350 Section 4 - Normal Procedures (EASA Approved) Shutdown Shutdown 4-18-01 continued CAS Feather Inhibit status..CHECK (if installed and activated)... Feather Inhibit switch....Release (if installed and activated)... External Lights switches..... PASS-Warning switches (if installed)........Main OXYGEN lever....Engine Oil Level (60 sec.

  • Page 351: Parking

    Section 4 - Normal Procedures (EASA Approved) Parking 4-19 Parking Parking 4-19-01 Flight Control Lock...... INSTALLED Wheel Chocks......AS REQUIRED Tail Stand........AS REQUIRED Note Install the tail stand when the aircraft is parked outside and wet snow fall is expected.
  • Page 352 Section 4 - Normal Procedures (EASA Approved) Parking This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-19-2...

  • Page 353: Oxygen System

    Section 4 - Normal Procedures (EASA Approved) Oxygen System 4-20 Oxygen System Oxygen System 4-20-01 Oxygen Pressure Gauge.... NOTE READING Outside Air Temperature..... NOTE READING Percentage of Full Bottle..... DETERMINE (refer to Fig. 4-20-1) COMPUTE........Oxygen Duration in minutes − Determine the Oxygen Duration in minutes for a full bottle for the number of connected passenger oxygen masks and pilots from the "Oxygen Duration with Full Bottle"...
  • Page 354 Section 4 - Normal Procedures (EASA Approved) Oxygen System Oxygen System 4-20-01 continued Passenger Oxygen control valve Insert the connector of each mask into an outlet and verify proper oxygen flow to the mask. For flights above 10,000 feet leave the masks connected to the outlets and turn the Oxygen Control Valve to AUTO.
  • Page 355 Section 4 - Normal Procedures (EASA Approved) Oxygen System Oxygen System 4-20-01 continued Table 4-20-2: Oxygen Duration with Full Bottle (Large Capacity Oxygen System) (continued from previous page) No. of Pax Oxygen Duration Oxygen Duration Oxygen Pax plus 1 Crew Mask Pax plus 2 Crew Mask Masks Connected...
  • Page 356 Section 4 - Normal Procedures (EASA Approved) Oxygen System This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-20-4...
  • Page 357 Section 4 - Normal Procedures (EASA Approved) Noise Level 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.
  • Page 358 Section 4 - Normal Procedures (EASA Approved) Noise Level This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-21-2...
  • Page 359 A brief description of the AFCS is given in Section 7 of this POH. Refer to the Pilot’s Guide for the Advanced Cockpit Environment (ACE ) (powered by Honeywell) for the Pilatus PC-12/47E for complete information on the description and operation of the AFCS.
  • Page 360 Section 4 - Normal Procedures (EASA Approved) Automatic 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...
  • Page 361 Section 4 - Normal Procedures (EASA Approved) Crosswind Operation 4-23 Crosswind Operation CAUTION On runways with pools of standing water and/or poor braking action it may not be possible to maintain centerline and/or the correct alignment of the aircraft on the runway in conditions of strong crosswind.
  • Page 362 Section 4 - Normal Procedures (EASA Approved) Crosswind Operation This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-23-2...
  • Page 363 Section 4 - Normal Procedures (EASA Approved) Flight in Icing Conditions 4-24 Flight in Icing Conditions Icing conditions can exist when: − The Outside Air Temperature (OAT) on the ground and for takeoff, or Static Air Temperature (SAT) in flight, is 10°C or colder, and visible moisture in any form is present (such as clouds, fog or mist with visibility of one mile or less, rain snow, sleet and ice crystals).
  • Page 364 Section 4 - Normal Procedures (EASA Approved) Flight in Icing Conditions The procedures for selection of the ice protection systems are provided in Section 4, Normal Procedures, Flight into Known Icing Conditions. During all icing encounters or times with visible ice accretion on any part of the airframe the flaps must not be extended beyond certain limits.
  • Page 365 Section 4 - Normal Procedures (EASA Approved) Flight in Icing Conditions The wing and horizontal tail de-ice boots are activated from the ICE PROTECTION switch panel by the switch labeled BOOTS being pushed to either 3MIN or 1MIN. 3MIN is to be selected in icing conditions with moderate ice accretion rates as judged by the aircrew.
  • Page 366 Section 4 - Normal Procedures (EASA Approved) Flight in Icing Conditions During the icing encounter the pneumatic de-ice boots will operate continuously in either 3min or 1min cycle mode as selected by the aircrew. During this time the aircrew should frequently monitor the continual shedding of ice from the wing leading edge and the airframe for ice accretion on all visible surfaces that could affect aircraft controllability.
  • Page 367 Section 4 - Normal Procedures (EASA Approved) Flight in Icing Conditions Of note, the tailplane may have residual ice that is not visible to the pilot. The speeds listed as minimum recommended speeds for icing encounters should be adhered to and recognized as MINIMUM recommended speeds following any icing encounter where there is even the slightest suspicion that the airframe may have residual ice.
  • Page 368 Section 4 - Normal Procedures (EASA Approved) Flight in Icing Conditions This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-24-6...

  • Page 369: Severe Icing Conditions

    Section 4 - Normal Procedures (EASA Approved) Severe Icing Conditions 4-25 Severe Icing Conditions Severe icing may result from environmental conditions outside of those for which the airplane is certificated. Flight in freezing rain, freezing drizzle, or mixed icing conditions (supercooled liquid water and ice crystals) may result in ice build-up on protected surfaces exceeding the capability of the ice protection system, or may result in ice forming aft of the protected surfaces.
  • Page 370 Section 4 - Normal Procedures (EASA Approved) Severe Icing Conditions This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 4-25-2...
  • Page 371 Section 4 - Normal Procedures (EASA Approved) CPCS Low Cabin Mode Operation 4-26 CPCS Low Cabin Mode Operation A semi-automatic mode called ‘Low Cabin’ is available, whereby the pilot can use Landing Field Elevation (LFE) as the target cabin altitude. The targeted cabin altitude can be the automatic LFE value from the FMS or the manually entered LFE.
  • Page 372 Section 4 - Normal Procedures (EASA Approved) CPCS 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...
  • Page 373 Section 4 - Normal Procedures (EASA Approved) SV Selection and Brightness Control 4-27 SV Selection and Brightness Control If installed, SV is automatically activated at start-up. SV can be turned ON/OFF by selecting or deselecting the “SVS ON” checkbox from the OVRLY menu, which is located just above the HSI on the outboard side of either PFD (Refer Fig.
  • Page 374 Section 4 - Normal Procedures (EASA Approved) SV Selection and Brightness Control This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 4-27-2...
  • Page 375 4-28-1 Introduction Normal operating procedures for LPV/LP Approach are described in the Pilot’s Guide for the Advanced Cockpit Environment (ACE ) (powered by Honeywell) for the Pilatus PC-12/47E. 4-28-2 Operating Procedures for Approach to LPV Minimum − Retrieve approach chart for the RNAV approach −...
  • Page 376 Section 4 - Normal Procedures (EASA Approved) Flight Director/Autopilot Coupled Operation − Verify NAV and VGP are the active autopilot modes (if required) − LPV Approach: Continue approach to LPV minimum by using lateral and vertical deviation pointers − LP Approach: Continue approach to LP minimum by using lateral deviation pointer and baro altitude to comply with published approach procedure (vertical deviation pointer is advisory only) −...
  • Page 377 Section 5 - Performance (EASA Approved) Table of Contents SECTION 5 Performance (EASA Approved) Table of Contents Subject Page Standard Tables 5-1-1 5-1-1 General 5-1-1 5-1-2 Standard Tables 5-1-3 NOT USED 5-2-0 5-3-1 Performance Data 5-3-1-1 5-3-1 Performance Data - Stall Speeds 5-3-1-1 5-3-2 Performance Data - Takeoff Performance...
  • Page 378 Section 5 - Performance (EASA 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...
  • Page 379 Section 5 - Performance (EASA Approved) Standard Tables Standard Tables 5-1-1 General This section contains all of the required and complementary performance data for airplane operation. Aircraft performance associated with optional equipment and systems which require supplements is provided in Section 9, Supplements. The performance information presented in this section is derived from actual flight test data corrected to standard day conditions and analytically expanded for the different parameters such as weight, altitude, and temperature, etc.
  • Page 380 Section 5 - Performance (EASA Approved) General The formulas for the conversion of standard format to metric equivalent and vice versa are given in Section 1, Conversion Information. Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-2...
  • Page 381 Section 5 - Performance (EASA Approved) Standard Tables 5-1-2 Standard Tables FAHRENHEIT TO CELSIUS CONVERSION EXAMPLE: DEGREES FAHRENHEIT 34 F DEGREES CELSIUS DEGREES ~ F ICN-12-C-A150501-A-S4080-00235-A-001-01 Figure 5-1-1: Performance - Fahrenheit to Celsius Conversion Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-3...
  • Page 382 Section 5 - Performance (EASA Approved) Standard Tables ICN-12-C-A150501-A-S4080-00236-A-001-01 Figure 5-1-2: Performance - ISA Conversion Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-4...
  • Page 383 Section 5 - Performance (EASA Approved) Standard Tables ICN-12-C-A150501-A-S4080-00237-A-001-01 Figure 5-1-3: Performance - U.S. Gallons to Liters Conversion Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-5...
  • Page 384 Section 5 - Performance (EASA Approved) Standard Tables ICN-12-C-A150501-A-S4080-00238-A-001-01 Figure 5-1-4: Performance - Feet to Meters Converion Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-6...
  • Page 385 Section 5 - Performance (EASA Approved) Standard Tables ICN-12-C-A150501-A-S4080-00239-A-001-01 Figure 5-1-5: Performance - Pounds to Kilograms Conversion Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-7...
  • Page 386 Section 5 - Performance (EASA Approved) Standard Tables ICN-12-C-A150501-A-S4080-00240-A-001-01 Figure 5-1-6: Performance - Inches to Millimeters Conversion Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-8...
  • Page 387 Section 5 - Performance (EASA Approved) Standard Tables ICN-12-C-A150501-A-S4080-00241-A-001-01 Figure 5-1-7: Performance - Wind Components Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-9...
  • Page 388 Section 5 - Performance (EASA Approved) Standard Tables ICN-12-C-A150501-A-S4080-00242-A-001-01 Figure 5-1-8: Performance - Airspeed Calibration Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-10...
  • Page 389 Section 5 - Performance (EASA Approved) Standard Tables ICN-12-C-A150501-A-S4080-00243-A-001-01 Figure 5-1-9: Performance - Altimeter Correction Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-11...
  • Page 390 Section 5 - Performance (EASA Approved) Standard Tables This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-1-12...
  • Page 391 Section 5 - Performance (EASA Approved) Performance Data - Stall Speeds 5-3-1 Performance Data - Stall Speeds See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00245-A-001-01 Figure 5-3-1-1: Performance - Stall Speeds KIAS - Flight Idle Power (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020...
  • Page 392 Section 5 - Performance (EASA Approved) Performance Data - Stall Speeds See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00246-A-001-01 Figure 5-3-1-2: Performance - Stall Speeds KIAS - Flight Idle Power (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-1-2...
  • Page 393 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance 5-3-2 Performance Data - Takeoff Performance ICN-12-C-A150503-A-S4080-00247-A-001-01 Figure 5-3-2-1: Performance - Static Takeoff Torque Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-1...
  • Page 394 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance S TATIC TAKEOFF TORQUE ACS INHIBIT P ROP ELLER S P EED: 1700 RP M ICE P ROTECTION: P ROBES ON / WINDS HIELD ON INERTIAL S EP ERATOR OP ERATION: EXAMP LE: HAS NO EFFECT ON TORQUE P RES S URE ALTITUDE...
  • Page 395 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00249-A-001-01 Figure 5-3-2-3: Performance - Accelerate-Stop Distance - Flaps 30° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-3...
  • Page 396 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00250-A-001-01 Figure 5-3-2-4: Performance - Accelerate-Stop Distance - Flaps 30° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-4...
  • Page 397 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00253-A-001-01 Figure 5-3-2-5: Performance - Takeoff Ground Roll - Flaps 30° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-5...
  • Page 398 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00254-A-001-01 Figure 5-3-2-6: Performance - Takeoff Ground Roll - Flaps 30° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-6...
  • Page 399 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00255-A-001-01 Figure 5-3-2-7: Performance - Takeoff Ground Roll - Flaps 30° - ACS OFF (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-7...
  • Page 400 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00256-A-001-01 Figure 5-3-2-8: Performance - Takeoff Ground Roll - Flaps 30° - ACS OFF (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-8...
  • Page 401 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00257-A-001-01 Figure 5-3-2-9: Performance - Takeoff Total Distance - Flaps 30° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-9...
  • Page 402 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00258-A-001-01 Figure 5-3-2-10: Performance - Takeoff Total Distance - Flaps 30° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-10...
  • Page 403 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00259-A-001-01 Figure 5-3-2-11: Performance - Takeoff Total Distance - Flaps 30° - ACS OFF (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-11...
  • Page 404 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00260-A-001-01 Figure 5-3-2-12: Performance - Takeoff Total Distance - Flaps 30° - ACS OFF (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-12...
  • Page 405 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00261-A-001-01 Figure 5-3-2-13: Performance - Accelerate-Stop Distance - Flaps 15° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-13...
  • Page 406 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00262-A-001-01 Figure 5-3-2-14: Performance - Accelerate-Stop Distance - Flaps 15° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-14...
  • Page 407 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00265-A-001-01 Figure 5-3-2-15: Performance - Takeoff Ground Roll - Flaps 15° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-15...
  • Page 408 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00266-A-001-01 Figure 5-3-2-16: Performance - Takeoff Ground Roll - Flaps 15° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-16...
  • Page 409 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00267-A-001-01 Figure 5-3-2-17: Performance - Takeoff Ground Roll - Flaps 15° - ACS OFF (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-17...
  • Page 410 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00268-A-001-01 Figure 5-3-2-18: Performance - Takeoff Ground Roll - Flaps 15° - ACS OFF (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-18...
  • Page 411 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00269-A-001-01 Figure 5-3-2-19: Performance - Takeoff Total Distance - Flaps 15° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-19...
  • Page 412 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00270-A-001-01 Figure 5-3-2-20: Performance - Takeoff Total Distance - Flaps 15° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-20...
  • Page 413 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00271-A-001-01 Figure 5-3-2-21: Performance - Takeoff Total Distance - Flaps 15° - ACS OFF (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-21...
  • Page 414 Section 5 - Performance (EASA Approved) Performance Data - Takeoff Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00272-A-001-01 Figure 5-3-2-22: Performance - Takeoff Total Distance - Flaps 15° - ACS OFF (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-2-22...
  • Page 415 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance 5-3-3 Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00273-A-001-01 Figure 5-3-3-1: Performance - Maximum Climb Torque Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-1...
  • Page 416 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00274-A-001-01 Figure 5-3-3-2: Performance - Maximum Rate Of Climb - Flaps 30° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-2...
  • Page 417 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00275-A-001-01 Figure 5-3-3-3: Performance - Maximum Rate Of Climb - Flaps 30° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-3...
  • Page 418 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00276-A-001-01 Figure 5-3-3-4: Performance - Maximum Rate Of Climb - Flaps 15° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-4...
  • Page 419 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00277-A-001-01 Figure 5-3-3-5: Performance - Maximum Rate Of Climb - Flaps 15° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-5...
  • Page 420 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00278-A-001-01 Figure 5-3-3-6: Performance - Maximum Rate Of Climb - Flaps 0° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-6...
  • Page 421 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00279-A-001-01 Figure 5-3-3-7: Performance - Maximum Rate Of Climb - Flaps 0° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-7...
  • Page 422 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00280-A-001-01 Figure 5-3-3-8: Performance - Rate Of Climb - Cruise Climb (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-8...
  • Page 423 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00281-A-001-01 Figure 5-3-3-9: Performance - Rate Of Climb - Cruise Climb (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-9...
  • Page 424 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00282-A-001-01 Figure 5-3-3-10: Performance - Time To Climb - Cruise Climb (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-10...
  • Page 425 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00283-A-001-01 Figure 5-3-3-11: Performance - Time To Climb - Cruise Climb (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-11...
  • Page 426 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00284-A-001-01 Figure 5-3-3-12: Performance - Fuel Used To Climb - Cruise Climb (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-12...
  • Page 427 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00285-A-001-01 Figure 5-3-3-13: Performance - Fuel Used To Climb - Cruise Climb (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-13...
  • Page 428 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00286-A-001-01 Figure 5-3-3-14: Performance - Distance To Climb - Cruise Climb (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-14...
  • Page 429 Section 5 - Performance (EASA Approved) Performance Data - Climb Performance ICN-12-C-A150503-A-S4080-00287-A-001-01 Figure 5-3-3-15: Performance - Distance To Climb - Cruise Climb (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-3-15...
  • Page 430 Section 5 - Performance (EASA Approved) Performance 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...
  • Page 431 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance 5-3-4 Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00288-A-001-01 Figure 5-3-4-1: Performance - Maximum Cruise Power (Sheet 1 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-1...
  • Page 432 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00289-A-001-01 Figure 5-3-4-1: Performance - Maximum Cruise Power (Sheet 2 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-2...
  • Page 433 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00290-A-001-01 Figure 5-3-4-1: Performance - Maximum Cruise Power (Sheet 3 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-3...
  • Page 434 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00291-A-001-01 Figure 5-3-4-1: Performance - Maximum Cruise Power (Sheet 4 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-4...
  • Page 435 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00292-A-001-01 Figure 5-3-4-2: Performance - Long Range Cruise (Sheet 1 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-5...
  • Page 436 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00293-A-001-01 Figure 5-3-4-2: Performance - Long Range Cruise (Sheet 2 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-6...
  • Page 437 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00294-A-001-01 Figure 5-3-4-2: Performance - Long Range Cruise (Sheet 3 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-7...
  • Page 438 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00295-A-001-01 Figure 5-3-4-2: Performance - Long Range Cruise (Sheet 4 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-8...
  • Page 439 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00296-A-001-01 Figure 5-3-4-3: Performance - Maximum Endurance Cruise (Sheet 1 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-9...
  • Page 440 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00297-A-001-01 Figure 5-3-4-3: Performance - Maximum Endurance Cruise (Sheet 2 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-10...
  • Page 441 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00298-A-001-01 Figure 5-3-4-3: Performance - Maximum Endurance Cruise (Sheet 3 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-11...
  • Page 442 Section 5 - Performance (EASA Approved) Performance Data - Cruise Performance ICN-12-C-A150503-A-S4080-00299-A-001-01 Figure 5-3-4-3: Performance - Maximum Endurance Cruise (Sheet 4 of 4) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-4-12...
  • Page 443 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range 5-3-5 Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00300-A-001-01 Figure 5-3-5-1: Performance - Specific Air Range (7000 lb) (Sheet 1 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-1...
  • Page 444 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00301-A-001-01 Figure 5-3-5-1: Performance - Specific Air Range (7000 lb) (Sheet 2 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-2...
  • Page 445 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00302-A-001-01 Figure 5-3-5-1: Performance - Specific Air Range (7000 lb) (Sheet 3 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-3...
  • Page 446 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00303-A-001-01 Figure 5-3-5-2: Performance - Specific Air Range (8000 lb) (Sheet 1 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-4...
  • Page 447 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00304-A-001-01 Figure 5-3-5-2: Performance - Specific Air Range (8000 lb) (Sheet 2 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-5...
  • Page 448 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00305-A-001-01 Figure 5-3-5-2: Performance - Specific Air Range (8000 lb) (Sheet 3 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-6...
  • Page 449 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00306-A-001-01 Figure 5-3-5-3: Performance - Specific Air Range (9000 lb) (Sheet 1 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-7...
  • Page 450 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00307-A-001-01 Figure 5-3-5-3: Performance - Specific Air Range (9000 lb) (Sheet 2 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-8...
  • Page 451 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00308-A-001-01 Figure 5-3-5-3: Performance - Specific Air Range (9000 lb) (Sheet 3 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-9...
  • Page 452 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00309-A-001-01 Figure 5-3-5-4: Performance - Specific Air Range (10,000 lb) (Sheet 1 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-10...
  • Page 453 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00310-A-001-01 Figure 5-3-5-4: Performance - Specific Air Range (10,000 lb) (Sheet 2 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-11...
  • Page 454 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00311-A-001-01 Figure 5-3-5-4: Performance - Specific Air Range (10,000 lb) (Sheet 3 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-12...
  • Page 455 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00312-A-001-01 Figure 5-3-5-5: Performance - Specific Air Range (10,400 lb) (Sheet 1 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-13...
  • Page 456 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00313-A-001-01 Figure 5-3-5-5: Performance - Specific Air Range (10,400 lb) (Sheet 2 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-14...
  • Page 457 Section 5 - Performance (EASA Approved) Performance Data - Specific Air Range ICN-12-C-A150503-A-S4080-00314-A-001-01 Figure 5-3-5-5: Performance - Specific Air Range (10,400 lb) (Sheet 3 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-5-15...
  • Page 458 Section 5 - Performance (EASA Approved) Performance 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...
  • Page 459 Section 5 - Performance (EASA Approved) Performance Data - Holding Time and Fuel 5-3-6 Performance Data - Holding Time and Fuel ICN-12-C-A150503-A-S4080-00315-A-001-01 Figure 5-3-6-1: Performance - Holding Time and Fuel Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-6-1...
  • Page 460 Section 5 - Performance (EASA Approved) Performance 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...
  • Page 461 Section 5 - Performance (EASA Approved) Performance Data - Descend Performance 5-3-7 Performance Data - Descend Performance TIME TO DESCEND ASSOCIATED CONDITIONS: LANDING GEAR RETRACTED, FLAPS UP POWER AS REQUIRED TO EXAMPLE: DESCEND AT 2000 FPM ALTITUDE 12000 FT AIRSPEED: MACH 0.48 OR 240 KIAS, TIME 6 MIN WHICHEVER IS LOWER...
  • Page 462 Section 5 - Performance (EASA Approved) Performance Data - Descend Performance ICN-12-C-A150503-A-S4080-00317-A-001-01 Figure 5-3-7-2: Performance - Fuel Used To Descend (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-7-2...
  • Page 463 Section 5 - Performance (EASA Approved) Performance Data - Descend Performance ICN-12-C-A150503-A-S4080-00318-A-001-01 Figure 5-3-7-3: Performance - Fuel Used To Descend (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-7-3...
  • Page 464 Section 5 - Performance (EASA Approved) Performance Data - Descend Performance ICN-12-C-A150503-A-S4080-00319-A-001-01 Figure 5-3-7-4: Performance - Distance to Descend Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-7-4...
  • Page 465 Section 5 - Performance (EASA Approved) Performance Data - Power-off Glide Performance 5-3-8 Performance Data - Power-off Glide Performance ICN-12-C-A150503-A-S4080-00320-A-001-01 Figure 5-3-8-1: Performance - Power-off Glide Time (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 5-3-8-1...
  • Page 466 Section 5 - Performance (EASA Approved) Performance Data - Power-off Glide Performance ICN-12-C-A150503-A-S4080-00321-A-001-01 Figure 5-3-8-2: Performance - Power-off Glide Time (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 5-3-8-2...
  • Page 467 Section 5 - Performance (EASA Approved) Performance Data - Power-off Glide Performance OUTSIDE AIR TEMPERATURE ~ °C ICN-12-C-A150503-A-S4080-00322-A-002-01 Figure 5-3-8-3: Performance - Power-off Glide Distance Pilot's Operating Handbook Report No: 02406 Issue date: Dec 18, 2020 Page 5-3-8-3...
  • Page 468 Section 5 - Performance (EASA Approved) Performance Data - 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...
  • Page 469 Section 5 - Performance (EASA Approved) Performance Data - Balked Landing Performance 5-3-9 Performance Data - Balked Landing Performance ICN-12-C-A150503-A-S4080-00323-A-001-01 Figure 5-3-9-1: Performance - Balked Landing Torque Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-9-1...
  • Page 470 Section 5 - Performance (EASA Approved) Performance Data - Balked Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00324-A-001-01 Figure 5-3-9-2: Performance - Rate Of Climb - Balked Landing (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-9-2...
  • Page 471 Section 5 - Performance (EASA Approved) Performance Data - Balked Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00325-A-001-01 Figure 5-3-9-3: Performance - Rate Of Climb - Balked Landing (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-9-3...
  • Page 472 Section 5 - Performance (EASA Approved) Performance Data - 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...
  • Page 473 Section 5 - Performance (EASA Approved) Performance Data - Landing Performance 5-3-10 Performance Data - Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00326-A-001-01 Figure 5-3-10-1: Performance - Landing Total Distance - Flaps 40° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020...
  • Page 474 Section 5 - Performance (EASA Approved) Performance Data - Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00327-A-001-01 Figure 5-3-10-2: Performance - Landing Total Distance - Flaps 40° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-10-2...
  • Page 475 Section 5 - Performance (EASA Approved) Performance Data - Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00328-A-001-01 Figure 5-3-10-3: Performance - Landing Ground Roll - Flaps 40° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-10-3...
  • Page 476 Section 5 - Performance (EASA Approved) Performance Data - Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00329-A-001-01 Figure 5-3-10-4: Performance - Landing Ground Roll - Flaps 40° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-3-10-4...
  • Page 477 Section 5 - Performance (EASA Approved) Performance Data - Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00330-A-001-01 Figure 5-3-10-5: Performance - Landing Total Distance with the use of Reverse Thrust - Flaps 40° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020...
  • Page 478 Section 5 - Performance (EASA Approved) Performance Data - Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00331-A-001-01 Figure 5-3-10-6: Performance - Landing Total Distance with the use of Reverse Thrust - Flaps 40° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020...
  • Page 479 Section 5 - Performance (EASA Approved) Performance Data - Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00332-A-001-01 Figure 5-3-10-7: Performance - Landing Ground Roll with the use of Reverse Thrust - Flaps 40° (standard units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020...
  • Page 480 Section 5 - Performance (EASA Approved) Performance Data - Landing Performance See FLIGHT IN ICING CONDITIONS para for info on effect of icing ICN-12-C-A150503-A-S4080-00333-A-001-01 Figure 5-3-10-8: Performance - Landing Ground Roll with the use of Reverse Thrust - Flaps 40° (metric units) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020...
  • Page 481 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - General 5-4-1 Flight in Icing Conditions - General The following section presents performance information related to the operation in or into known icing conditions. This information was derived analytically from actual wind tunnel tests with natural ice.
  • Page 482 Section 5 - Performance (EASA Approved) Flight in 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...
  • Page 483 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Flaps 5-4-2 Flight in Icing Conditions - Flaps When operating in or into known icing conditions, the use of Flaps 30° or 40° is prohibited. When operating in or into known icing conditions with fully operational pneumatic de-ice boots, the flap position is limited to a maximum of 15°.
  • Page 484 Section 5 - Performance (EASA Approved) Flight in 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...
  • Page 485 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Stall Speeds 5-4-3 Flight in Icing Conditions - Stall Speeds When operating in STICK PUSHER ICE MODE the stick pusher computer automatically reduces the shaker and pusher settings as measured by the angle of attack vanes, by 8°. With operational pneumatic de-ice boots, this results in an increase of the stall speed at the maximum takeoff weight of 12 kts with flaps set to 0°...
  • Page 486 Section 5 - Performance (EASA Approved) Flight in Icing 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...
  • Page 487 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Engine Torque 5-4-4 Flight in Icing Conditions - Engine Torque When the engine inlet inertial separator is open and during flight, the maximum torque available can be reduced by up to 2.2 psi in non-icing conditions, and up to 2.8 psi in icing conditions.
  • Page 488 Section 5 - Performance (EASA Approved) Flight in Icing 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...
  • Page 489 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Takeoff Performance 5-4-5 Flight in Icing Conditions - Takeoff Performance The flaps must be set to 15° for takeoff. The use of flaps 30° for takeoff is prohibited. When de-icing / anti-icing fluids are applied to the aircraft before departure, and/or when the stick pusher is in ICE mode: The takeoff reference speeds must be adjusted to the values indicated by the corresponding correction table.
  • Page 490 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Takeoff Performance Table 5-4-5-1: Icing Corrections to Takeoff Total Distance - Altitude Correction (Table A) Table A Takeoff Weight (kg (lb)) Altitude 2900 3300 3700 4100 4500 4740 Correction (6393) (7275) (8157)
  • Page 491 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Takeoff Performance Takeoff Ground Roll Analogically, the takeoff ground roll is derived correcting the distances obtained from Fig. 5-3-2-15 (standard units), Fig. 5-3-2-16 (metric units), Fig. 5-3-2-17 (ACS OFF, standard units) or Fig.
  • Page 492 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Takeoff Performance Table 5-4-5-4: Icing Corrections to Takeoff Ground Roll - Altitude Correction (Table A) Table A Takeoff Weight (kg (lb)) Altitude 2900 3300 3700 4100 4500 4740 Correction (6393) (7275) (8157)
  • Page 493 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Takeoff Performance Example: − Pressure Altitude = 6000 ft − Outside Air Temperature = -10 °C − Weight = 3500 kg − Headwind Component = 8 kt − Uphill Component = 1% −...
  • Page 494 Section 5 - Performance (EASA Approved) Flight in Icing 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...
  • Page 495 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Accelerate-Stop Performance 5-4-6 Flight in Icing Conditions - Accelerate-Stop Performance The flaps must be set to 15° for takeoff. The use of flaps 30° for takeoff is prohibited. The maximum speed for power chop is assumed to be 10 kt higher than that for non-icing conditions.
  • Page 496 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Accelerate-Stop Performance Table 5-4-6-1: Icing Corrections to Accelerate-Stop Distance - Altitude Correction (Table A) Table A Takeoff Weight (kg (lb)) Altitude 2900 3300 3700 4100 4500 4740 Correction (6393) (7275) (8157) (9039)
  • Page 497 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Maximum Rate of Climb 5-4-7 Flight in Icing Conditions - Maximum Rate of Climb The use of Flaps 30° is prohibited in or into known icing conditions. After icing encounters, and with visible ice accretion on the airframe, a climb is performed with the flaps retracted and a climb speed based on the schedule as given in Table...
  • Page 498 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Maximum Rate of Climb Table 5-4-7-3: Icing Corrections to Maximum Rate of Climb with Pneumatic De-ice Boots Inop- erative Rate of Climb Correction (feet per minute) Takeoff Weight (kg (lb)) Altitude (ft) 2900 (6393) 3500 (7716)
  • Page 499 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Holding Endurance 5-4-8 Flight in Icing Conditions - Holding Endurance During holding flight in icing conditions, a higher engine torque is required to maintain level flight. Table 5-4-8-1 Table 5-4-8-2 give the increases in fuel flow with respect to non-icing conditions.
  • Page 500 Section 5 - Performance (EASA Approved) Flight in Icing 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...
  • Page 501 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Balked Rate of Climb 5-4-9 Flight in Icing Conditions - Balked Rate of Climb The use of Flaps 30° or Flaps 40° is prohibited in or into known icing conditions. After icing encounters and with visible ice accretion on the airframe, a balked landing climb is performed with Flaps 15°...
  • Page 502 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - 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...
  • Page 503 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance 5-4-10 Flight in Icing Conditions - Landing Performance The flaps must be set to 15° for landing. The use of Flaps 30° or 40° for landing is prohibited. With pneumatic de-ice boots failed;...
  • Page 504 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-1: Landing in Icing Conditions - Overview (continued from previous page) Pneumatic Landing Reverse Flap Non-icing Icing Correction De-ice Performance Thrust Setting Figure No. Table Boots Information Table 5-4-10-23 Landing Ground...
  • Page 505 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-2: Icing Corrections to Landing Total Distance - Flaps 15° - No Reverse Thrust - Altitude Correction (Table A) Table A Landing Weight (kg (lb)) Altitude 2900 3300 3700...
  • Page 506 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-5: Icing Corrections to Landing Ground Roll - Flaps 15° - No Reverse Thrust - Al- titude Correction (Table A) Table A Landing Weight (kg (lb)) Altitude 2900 3300...
  • Page 507 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-8: Icing Corrections to Landing Total Distance - Flaps 0° - No Reverse Thrust - Altitude Correction (Table A) Table A Landing Weight (kg (lb)) Altitude 2900 3300 3700...
  • Page 508 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-11: Icing Corrections to Landing Ground Roll - Flaps 0° - No Reverse Thrust - Al- titude Correction (Table A) Table A Landing Weight (kg (lb)) Altitude 2900 3300...
  • Page 509 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-14: Icing Corrections to Landing Total Distance - Flaps 15° - With Reverse Thrust - Altitude Correction (Table A) Table A Landing Weight (kg (lb)) Altitude 2900 3300 3700...
  • Page 510 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-17: Icing Corrections to Landing Ground Roll - Flaps 15° - With Reverse Thrust - Altitude Correction (Table A) Table A Landing Weight (kg (lb)) Altitude 2900 3300 3700...
  • Page 511 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-20: Icing Corrections to Landing Total Distance - Flaps 0° - With Reverse Thrust - Altitude Correction (Table A) Table A Landing Weight (kg (lb)) Altitude 2900 3300 3700...
  • Page 512 Section 5 - Performance (EASA Approved) Flight in Icing Conditions - Landing Performance Table 5-4-10-23: Icing Corrections to Landing Ground Roll - Flaps 0° - With Reverse Thrust - Altitude Correction (Table A) Table A Landing Weight (kg (lb)) Altitude 2900 3300 3700...
  • Page 513 Section 5 - Performance (EASA Approved) Flight Planning Example 5-5-1 Flight Planning Example 5-5-1-1 General This section gives an example of flight planning for aircraft with a five bladed propeller. Before performance calculations can begin, it will be necessary to determine the aircraft loading. Refer to Section 6, Weight and Balance to calculate the actual aircraft loading.
  • Page 514 Section 5 - Performance (EASA Approved) Flight Planning Example Table 5-5-1-4: Time, Fuel and Distance to climb from Departure Airport to Cruise Altitude Climb Time Fuel Distance From S.L. to 28000 ft 21 min 190 lb 68 nm From S.L. to 2 min 30 lb 6 nm...
  • Page 515 Section 5 - Performance (EASA Approved) Flight Planning Example Cruise power setting By assuming an average cruise weight of 8500 lb, Maximum Cruise Power setting for 28000 ft. at ISA +10°C yields 275 KTAS at 378 lb/hr. Ground speed Cruise speed ±...
  • Page 516 Section 5 - Performance (EASA Approved) Flight Planning Example This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 5-5-1-4...
  • Page 517 Section 6 - Weight and Balance (EASA Approved) Table of Contents SECTION 6 Weight and Balance (EASA Approved) Table of Contents Subject Page General 6-1-1 Preparations for Airplane Weighing 6-2-1 Airplane Weighing with Load Plates 6-3-1 6-3-1 Leveling 6-3-1 6-3-2 Weighing 6-3-1 Airplane Weighing with Jacks and Load Cells...
  • Page 518 Section 6 - Weight and Balance (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...

  • Page 519: General

    Section 6 - Weight and Balance (EASA Approved) General General This section contains the information required to determine the Basic Empty Weight and Moment of the aircraft, adjust the B.E.W. & M as equipment is added or removed, and calculate aircraft loading for various flight operations. Sample loading forms are provided. To achieve the performance designed for the aircraft it must be flown with approved weight and center of gravity limits.
  • Page 520 Section 6 - Weight and Balance (EASA Approved) General This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-1-2...

  • Page 521: Preparations For Airplane Weighing

    Section 6 - Weight and Balance (EASA Approved) Preparations for Airplane Weighing Preparations for Airplane Weighing Make sure that all applicable items listed on the airplane equipment list are installed in their proper locations. Clean airplane. Remove dirt, excessive grease, water, and foreign items. Completely defuel the fuel tanks.
  • Page 522 Section 6 - Weight and Balance (EASA Approved) Preparations for Airplane Weighing This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-2-2...

  • Page 523: Airplane Weighing With Load Plates

    Section 6 - Weight and Balance (EASA Approved) Airplane Weighing with Load Plates Airplane Weighing with Load Plates 6-3-1 Leveling Open the cargo door and place a level across the seat tracks. Adjust the main gear tire pressure (do not exceed the recommended maximum tire pressure) until the airplane is laterally level.
  • Page 524 Section 6 - Weight and Balance (EASA Approved) Weighing Scale Position Scale Tare Net Weight Symbol Reading lb (kg) lb (kg) lb (kg) Nose Landing Gear Left Main Landing Gear Right Main Landing Gear TOTAL AIRCRAFT WEIGHT DATUM C.G. ARM 118 in.
  • Page 525 Section 6 - Weight and Balance (EASA Approved) Weighing Landing Symbol Dimension Average (b) Gear in (mm) Nose Left Main Right Main (L+R) / 2 NOSE GEAR Dimension (mm) (in) (mm) 111.90 2842 111.82 2840 111.74 2838 111.62 2835 111.54 2833 111.46 2831...
  • Page 526 Section 6 - Weight and Balance (EASA Approved) Weighing MAIN GEAR ARM Dimension (mm) (in) (mm) 254.78 6471 254.46 6463 254.07 6453 253.60 6441 253.04 6427 252.41 6411 251.71 6393 250.88 6372 249.97 6349 248.91 6322 247.73 6292 Dimension (b) is strut extension Calculate the airplane C.G.

  • Page 527: Airplane Weighing With Jacks And Load Cells

    Section 6 - Weight and Balance (EASA Approved) Airplane Weighing with Jacks and Load Cells Airplane Weighing with Jacks and Load Cells 6-4-1 Leveling Put the jacks in position below the wing and tail jacking points. The fuselage jacking points must not be used.

  • Page 528: Weighing

    Section 6 - Weight and Balance (EASA Approved) Weighing 6-4-2 Weighing With the airplane level, record the weight shown on each load cell in the appropriate section on Fig. 6-4-1, Airplane Weighing Form. Calculate airplane C.G. Arm and record on Fig.
  • Page 529 Section 6 - Weight and Balance (EASA Approved) Weighing 463.38 in (11770 mm) 216.75 in (5505.5 mm) LEFT MAIN JACKING POINT RIGHT MAIN JACKING POINT TAIL JACKING POINT Scale Scale Position Symbol Reading lb (kg) Tail Jacking Point Left Main Jacking Point Right Main Jacking Point TOTAL AIRCRAFT WEIGHT ICN-12-C-A150604-A-S4080-00145-A-001-01...
  • Page 530 Section 6 - Weight and Balance (EASA Approved) Weighing Model: Serial No: Registration No: Date: Item Weight C.G. Arm Moment lb-in 1. Airplane Weight, C.G. arm, and moment (As weighed in Figure 6-1) 2. Unusable Fuel 32.9 14.9 225.6 5.73 7422 85.39 3.
  • Page 531 Section 6 - Weight and Balance (EASA Approved) Weighing The Basic Empty Weight, C.G., and Useful Load are for the airplane as licensed at the factory. These figures are only applicable to the specific airplane serial number and registration number shown. Refer to Fig.
  • Page 532 Section 6 - Weight and Balance (EASA Approved) Weighing This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-4-6...

  • Page 533: Weight And Balance Determination For Flight

    Section 6 - Weight and Balance (EASA Approved) Weight and Balance Determination for Flight Weight and Balance Determination for Flight 6-5-1 General This section contains the crew seats, baggage, fuel load moments charts and C of G envelopes in LB-IN and KG-M. Refer to the Interior Configurations section for the passenger seat moments.
  • Page 534 Section 6 - Weight and Balance (EASA Approved) Combi Conversion 6-5-3 Combi Conversion A Combi Conversion can be made from the removal of cabin seats from a Corporate Commuter and the removal of cabin seats and furnishings from an Executive Interior aircraft. The Combi Interior consists of 2 crew seats and payload or a combination of seats and payload.
  • Page 535 Section 6 - Weight and Balance (EASA Approved) Combi Conversion Complete the remainder of the Loading Form as given above. When re-installing the passenger seats, return the seats to their original positions and verify the dimensions as shown in the Seat Location Chart for the aircraft configuration. Secure the arresting pin on the Corporate Commuter Seat(s) or install the locking needles on the Executive Seat(s).
  • Page 536 Section 6 - Weight and Balance (EASA Approved) Combi Conversion Table 6-5-4: Moment Chart - Rear Baggage Area Moments - Standard Net at Frame 34 (impe- rial) REAR BAGGAGE AREA MOMENTS ( LB-IN ) STANDARD NET AT FRAME 34 - ARM 371.0 IN WEIGHT MOMENT WEIGHT...
  • Page 537 Section 6 - Weight and Balance (EASA Approved) Combi Conversion Table 6-5-6: Moment Chart - Rear Baggage Area Moments - Extendable Net at Frame 32 (im- perial) REAR BAGGAGE AREA MOMENTS ( LB-IN ) EXTENDABLE NET AT FRAME 32 - ARM 361.0 IN WEIGHT MOMENT WEIGHT...
  • Page 538 Section 6 - Weight and Balance (EASA Approved) Combi Conversion Table 6-5-8: Moment Chart - Fuel Load Moments (imperial) FUEL LOAD MOMENTS (LB-IN) WEIGHT MOMENT WEIGHT MOMENT WEIGHT MOMENT WEIGHT MOMENT lb-in lb-in lb-in lb-in 22572 183555 1500 347656 2200 511463 45161 207111...
  • Page 539 Section 6 - Weight and Balance (EASA Approved) Combi Conversion PC-12/47E EXAMPLE LOADING FORM INTERIOR CODE: STD-9S ITEM WEIGHT ARM AFT OF MOMENT DATUM in lb-in Basic Empty Weight 5613 225.16 1263823 Combi Interior Conversion Pilot 160.27 27246 Copilot (Right Seat Passenger) 160.27 27246 210.35...
  • Page 540 Section 6 - Weight and Balance (EASA Approved) Combi Conversion PC-12/47E LOADING FORM INTERIOR CODE: STD-9S ITEM WEIGHT ARM AFT OF MOMENT DATUM in (m) lb-in (kg-m) Basic Empty Weight Combi Interior Conversion Pilot 160.27 (4.071) Copilot (Right Seat Passenger) 160.27 (4.071) Passenger 1 Passenger 2...
  • Page 541 Section 6 - Weight and Balance (EASA Approved) Combi Conversion ICN-12-C-A150605-A-S4080-00168-A-001-01 Figure 6-5-3: C. G. Envelope (Sheet 1 of 2) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-5-9...
  • Page 542 Section 6 - Weight and Balance (EASA Approved) Combi Conversion ICN-12-C-A150605-A-S4080-00169-A-001-01 Figure 6-5-3: C. G. Envelope (Sheet 2 of 2) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-5-10...
  • Page 543 6-5-4 Equipment List Refer to Pilatus Report No. 02047, Airplane equipment List, attached to the back of this report. The equipment list itemizes the installed equipment included in the Basic Empty Weight indicated in the Airplane Basic Empty Weight figure Fig.
  • Page 544 Section 6 - Weight and Balance (EASA Approved) Equipment List This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-5-12...
  • Page 545 Section 6 - Weight and Balance (EASA Approved) Weight and Balance Records Weight and Balance Records Fig. 6-6-1 Weight and Balance Record is a log of the modifications that occurred after the airplane was licensed at the factory. Any change to the permanently installed equipment or airplane modifications which effect the airplane Basic Empty Weight or Total Moment must be entered in Fig.
  • Page 546 Section 6 - Weight and Balance (EASA Approved) Weight and Balance Records ICN-12-C-A150606-A-S4080-00147-A-001-01 Figure 6-6-1: Weight and Balance Record (Sheet 1 of 2) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-6-2...
  • Page 547 Section 6 - Weight and Balance (EASA Approved) Weight and Balance Records ICN-12-C-A150606-A-S4080-00148-A-001-01 Figure 6-6-1: Weight and Balance Record (Sheet 2 of 2) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-6-3...
  • Page 548 Section 6 - Weight and Balance (EASA Approved) Weight and Balance Records This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 6-6-4...
  • Page 549 Section 6 - Weight and Balance (EASA Approved) General Loading Recommendations General Loading Recommendations 6-7-1 General The following general loading recommendation is intended as only a guide. Refer to Section 2, Limitations, Other Limitations for Seating and Cargo Limitations. The pilot in command must refer to the appropriate moment charts, loading form, and the C.G.
  • Page 550 Section 6 - Weight and Balance (EASA Approved) Hazardous Materials 48.4" 1.23 m 44.25" 1.13 m PASSENGER DOOR 12.6" 20.47" 12.6" 0.32 m 0.52 m 0.32 m CABIN CROSS-SECTION EMERGENCY EXIT CARGO NET ATTACHMENT 44.5" FRAME 24 1.13 m 153.5" 3.9 m CABIN AREA...
  • Page 551 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight Per Single Container (Without Special Equipment) 6-7-4 Maximum Allowable Weight Per Single Container (Without Special Equipment) The maximum allowable weight is based on the package dimensions, vertical c.g. and the number of seat rails used to secure the fore-aft tie-down straps.
  • Page 552 Is the cargo The Cargo Tie-Down Configuration lateral c.g. within centre Charts are not valid: 20% of width ? contact Pilatus for advice Max 67% 1. Place the cargo in the cabin with height the heavier end to the rear.
  • Page 553 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight Per Single Container (Without Special Equipment) Step Two Choose the correct Restraint Bar(s) based on the cargo width Cargo width between 14.5'' and 15.75'' (between 370 mm and 400 mm) Use a single, short Restraint Bar (525.25.12.072 or 525.25.12.171 or 525.25.12.276)
  • Page 554 The Cargo Tie-Down Is the cargo Configuration Charts Vertical c.g. below are not valid: contact 67% height ? Pilatus for advice mid-height or below above mid-height Where is the vertical c.g. of the cargo ? Use "Normal Use "High Centre of Cargo"...
  • Page 555 Is the Height/Length ratio less than or equal to 1.25 ? The Cargo Tie-Down Configuration Charts are not valid: contact Pilatus for advice Use Height/Length ratio to enter the Cargo Configuration Chart Is the Cargo weight less than or equal...
  • Page 556 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight Per Single Container (Without Special Equipment) 6-7-4.1 Restrain Cargo in Cabin Fit the Restraint Bars and the Load Carrier Assemblies to the aircraft. If there is more than one cargo item, try to place the heavier items forward of the lighter ones.
  • Page 557 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight Per Single Container (Without Special Equipment) 6-7-4.2 Example The cargo to be transported is shown below. Looking down, the c.g. is roughly in the centre of the box, but its height is unknown. WEIGHT 200 lb (90kg) 18'' (450mm) 36'' (900mm)
  • Page 558 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight Per Single Container (Without Special Equipment) Determine the cargo size and orientation The best orientation in the cabin is with the shortest side (18”) vertical and the longest side (36”) across the cabin width. Fig.
  • Page 559 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight Per Single Container (Without Special Equipment) CARGO SECURED LONGITUDINALLY TO TWO SEAT RAILS CARGO TOO HEAVY Max. 350 lb (160 kg) LIMIT: NORMAL CARGO CARGO WEIGHT ACCEPTABLE LIMIT: HIGH CENTER OF GRAVITY CARGO 0.25 0.75...
  • Page 560 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight Per Single Container (Without Special Equipment) CARGO SECURED LONGITUDINALLY TO TWO SEAT RAILS Max. 440 lb (200 kg) CARGO TOO HEAVY LIMIT: NORMAL CARGO CARGO WEIGHT ACCEPTABLE LIMIT: HIGH CENTER OF GRAVITY CARGO 0.25 0.75...
  • Page 561 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight Per Single Container (Without Special Equipment) INSTALLATION OF A CARGO NET FORWARD OF CARGO IS RECOMMENDED IF PASSENGERS ARE IN CABIN CARGO NET FRAME 24 FRAME 27 EXTENDABLE FRAME 32 LUGGAGE NET LUGGAGE NET FRAME 34...
  • Page 562 Section 6 - Weight and Balance (EASA Approved) Maximum Allowable Weight 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...
  • Page 563 Before making any changes to the interior configuration, contact Pilatus to make 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.
  • Page 564 Section 6 - Weight and Balance (EASA Approved) General SEAT TRACK SEAT TRACK FIRST SEAT TRACK LOCATING HOLE X = 183.13" (4,652 m) NOTE: CABIN SEAT LOCATION IS DEFINED AS THE DISTANCE FROM THE CENTER OF THE FIRST SEAT TRACK LOCATING HOLE TO THE CENTER OF THE CENTER ARRESTING PIN ON EACH SEAT.
  • Page 565 Section 6 - Weight and Balance (EASA Approved) Corporate Commuter Interior Code STD-9S 6-8-2 Corporate Commuter Interior Code STD-9S 6-8-2.1 General The basic Corporate Commuter Interior consisting of 9 standard passenger seats. The section contains the following information: − passenger seat location chart −...
  • Page 566 Section 6 - Weight and Balance (EASA Approved) Corporate Commuter Interior Code STD-9S CORPORATE COMMUTER INTERIOR CODE STD-9S SEAT LOCATIONS DISTANCE FROM CENTER OF FIRST 0.00" 26.00" 59.00" 92.00" 125.00" 158.00" SEAT TRACK 0.000 m 0.660 m 1.499 m 2.337 m 3.175 m 4.013 m LOCATING HOLE...
  • Page 567 Section 6 - Weight and Balance (EASA Approved) Corporate Commuter Interior Code STD-9S 6-8-2.2 Permitted Passenger Seat Part Numbers That Can Be Installed Table 6-8-1: STD-9S - Permitted Passenger Seat Part Numbers That Can Be Installed SEAT NO. SEAT PART NUMBER 1,3,5,7 959.30.01.445 (with literature pocket) 959.30.01.447 (without literature pocket)
  • Page 568 Section 6 - Weight and Balance (EASA Approved) Corporate Commuter Interior Code STD-9S 6-8-2.4 Passenger Seat Occupant Moment Charts (Standard and Metric Units) Table 6-8-3: STD-9S - Passenger Seat Occupant Moment Chart (imperial) PASSENGER SEAT OCCUPANT MOMENTS ( LB - IN ) WEIGHT PAX 1 PAX 2...
  • Page 569 Section 6 - Weight and Balance (EASA Approved) Corporate Commuter Interior Code STD-9S Table 6-8-4: STD-9S - Passenger Seat Occupant Moment Chart (metric) PASSENGER SEAT OCCUPANT MOMENTS ( KG - M ) WEIGHT PAX 1 PAX 2 PAX 3 PAX 4 PAX 5 PAX 6 PAX 7...
  • Page 570 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-2 6-8-3 Executive Interior Code EX-6S-2 6-8-3.1 General The basic Executive Interior consisting of 6 executive passenger seats. The section contains the following information: − passenger seat location chart −...
  • Page 571 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-2 EXECUTIVE INTERIOR CODE EX-6S-2 SEAT LOCATIONS TOILET PAX 6 CABINET DISTANCE FROM CENTER OF FIRST 0.00" 6.87" 28.71" 157.00" SEAT TRACK 0.000 m 0.174 m 0.729 m 3.988 m LOCATING HOLE 183.13"...
  • Page 572 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-2 6-8-3.2 Permitted Passenger Seat Part Numbers That Can Be Installed Table 6-8-5: EX-6S-2 - Permitted Passenger Seat Part Numbers That Can Be Installed SEAT NO. Seat Part Number 959.30.00.017 959.30.00.019 959.30.00.081...
  • Page 573 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-2 6-8-3.4 Passenger Seat Occupant Moment Charts (Standard and Metric Units) Table 6-8-7: EX-6S-2 - Passenger Seat Occupant Moment Chart (imperial) PASSENGER SEAT OCCUPANT MOMENTS ( LB - IN ) WEIGHT PAX 1/2 PAX 3/4...
  • Page 574 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-2 Table 6-8-8: EX-6S-2 - Passenger Seat Occupant Moment Chart (metric) PASSENGER SEAT OCCUPANT MOMENTS ( KG - M ) WEIGHT PAX 1/2 PAX 3/4 PAX 5 PAX 6 (kg) (5,899 m) (7,011 m)
  • Page 575 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-8S 6-8-4 Executive Interior Code EX-8S 6-8-4.1 General This configuration is a variation of the basic executive interior and consists of 8 executive passenger seats. It is the operator’s responsibility to check before using this configuration whether they require authorization by their regulatory authority.
  • Page 576 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-8S EXECUTIVE INTERIOR CODE EX-8S SEAT LOCATIONS TOILET CABINET DISTANCE FRO M 0.00" 6.87" 28.71" CENTER OF FIRST SEAT TRACK 0.000 m 0.174 m 0.729 m LOCATING HOLE 183.13" 190.00"...
  • Page 577 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-8S 6-8-4.2 Permitted Passenger Seat Part Numbers That Can Be Installed Table 6-8-9: EX-8S - Permitted Passenger Seat Part Numbers That Can Be Installed SEAT NO. PART NO. 959.30.00.017 959.30.00.019 959.30.00.081 959.30.00.083...
  • Page 578 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-8S 6-8-4.4 Passenger Seat Occupant Moment Charts (Standard and Metric Units) Table 6-8-11: EX-8S - Passenger Seat Occupant Moment Chart (imperial) PASSENGER SEAT OCCUPANT MOMENTS ( LB - IN ) WEIGHT PAX 1/2 PAX 3/4...
  • Page 579 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-8S Table 6-8-12: EX-8S - Passenger Seat Occupant Moment Chart (metric) PASSENGER SEAT OCCUPANT MOMENTS ( KG - M ) WEIGHT PAX 1/2 PAX 3/4 PAX 5/6 PAX 7/8 (kg) (5,899 m) (7,011 m)
  • Page 580 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-STD-2S 6-8-5 Executive Interior Code EX-6S-STD-2S 6-8-5.1 General This configuration is a variation of the basic Executive interior and consists of 6 executive passenger seats and 2 standard seats. It is the operator’s responsibility to check before using this configuration whether they require authorization by their regulatory authority.
  • Page 581 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-STD-2S SIX EXECUTIVE AND TWO STANDARD INTERIOR CODE EX-6S-STD-2S SEAT LOCATIONS LAVATORY/ WARDROBE CABINET DISTANCE FROM CENTER OF FIRST 0.00" 6.87" 28.71" 156.00" SEAT TRACK 0.000 m 0.174 m 0.729 m 3.962 m LOCATING HOLE...
  • Page 582 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-STD-2S 6-8-5.2 Permitted Passenger Seat Part Numbers That Can Be Installed Table 6-8-13: EX-6S-STD-2S - Permitted Passenger Seat Part Numbers That Can Be Installed SEAT NO. PART NO. 959.30.00.017 959.30.00.019 959.30.00.081 959.30.00.083...
  • Page 583 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-STD-2S When installing the extendable baggage net refer to Section 2, Limitations, Other Limitations for the Luggage Limitations. 6-8-5.4 Passenger Seat Occupant Moment Charts (Standard and Metric Units) Table 6-8-15: EX-6S-STD-2S - Passenger Seat Occupant Moment Chart (imperial) PASSENGER SEAT OCCUPANT MOMENTS ( LB - IN ) WEIGHT PAX 1/2...
  • Page 584 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-6S-STD-2S Table 6-8-16: EX-6S-STD-2S - Passenger Seat Occupant Moment Chart (metric) PASSENGER SEAT OCCUPANT MOMENTS ( KG - M ) WEIGHT PAX 1/2 PAX 3/4 PAX 5/6 PAX 7/8 (kg) (5,899 m) (7,011 m)
  • Page 585 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-4S-STD-4S 6-8-6 Executive Interior Code EX-4S-STD-4S 6-8-6.1 General This configuration is a variation of the basic Executive interior and consists of 4 executive passenger seats and 4 standard seats. It is the operator’s responsibility to check before using this configuration whether they require authorization by their regulatory authority.
  • Page 586 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-4S-STD-4S FOUR EXECUTIVE AND FOUR STANDARD INTERIOR CODE EX-4S-STD-4S SEAT LOCATIONS LAVATORY/ WARDROBE CABINET DISTANCE FROM CENTER OF FIRST 0.00" 6.87" 28.71" 125.00" 158.00" SEAT TRACK 0.000 m 0.174 m 0.729 m 3.175 m 4.013 m...
  • Page 587 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-4S-STD-4S 6-8-6.2 Permitted Passenger Seat Part Numbers That Can Be Installed Table 6-8-17: EX-4S-STD-4S - Permitted Passenger Seat Part Numbers That Can Be Installed SEAT NO. PART NO. 959.30.00.017 959.30.00.019 959.30.00.081 959.30.00.083...
  • Page 588 Section 6 - Weight and Balance (EASA Approved) Executive Interior Code EX-4S-STD-4S When installing the extendable baggage net refer to Section 2, Limitations, Other Limitations for the Luggage Limitations. 6-8-6.4 Passenger Seat Occupant Moment Charts (Standard and Metric Units) Table 6-8-19: EX-4S-STD-4S - Passenger Seat Occupant Moment Chart (imperial) PASSENGER SEAT OCCUPANT MOMENTS ( LB - IN ) WEIGHT PAX 1/2...
  • Page 589 Section 6 - Weight and Balance (EASA Approved) No Cabin Interior Configuration Table 6-8-20: EX-4S-STD-4S - Passenger Seat Occupant Moment Chart (metric) PASSENGER SEAT OCCUPANT MOMENTS ( KG - M ) WEIGHT PAX 1/2 PAX 3/4 PAX 5/6 PAX 7/8 (kg) (5,899 m) (7,011 m)
  • Page 590 Section 6 - Weight and Balance (EASA Approved) No Cabin Interior Configuration NO CABIN INTERIOR CONFIGURATION NOTE: INTERIOR CONFIGURATION PLACARD NOT REQUIRED ICN-12-C-A150608-A-S4080-02039-A-001-01 Figure 6-8-7: No Cabin Interior Configuration 6-8-7.2 Furnishings Weight and Moment Chart Table 6-8-21: No Cabin Interior Furnishings Weight and Moment Chart ITEM WEIGHT lb (kg) MOMENT lb-in (kg-m)
  • Page 591 Section 7 - Airplane and Systems Description Table of Contents SECTION 7 Airplane and Systems Description Table of Contents Subject Page General 7-1-1 Airframe 7-2-1 7-2-1 General 7-2-1 7-2-2 Fuselage 7-2-1 7-2-3 Empennage 7-2-1 7-2-4 Wings 7-2-1 Flight Controls 7-3-1 7-3-1 General 7-3-1...
  • Page 592 Section 7 - Airplane and Systems Description Table of Contents Subject Page 7-7-2 Seat Belts And Shoulder Harnesses 7-7-1 7-7-3 Restraint Systems for Children 7-7-5 Doors, Windows and Exits 7-8-1 7-8-1 Passenger Door 7-8-1 7-8-2 Cargo Door 7-8-1 7-8-3 Windows 7-8-2 7-8-4 Indication/Warning...
  • Page 593 Section 7 - Airplane and Systems Description Table of Contents Subject Page 7-12-4 Indication / Warning 7-12-3 7-13 Electrical 7-13-1 7-13-1 General 7-13-1 7-13-2 Description 7-13-1 7-13-3 Operation 7-13-6 7-13-4 Indication / Warning 7-13-8 7-14 Lighting 7-14-1 7-14-1 Interior 7-14-1 7-14-2 Exterior 7-14-1...
  • Page 594 Section 7 - Airplane and Systems Description Table of Contents Subject Page 7-20-1 General 7-20-1 7-20-2 Description 7-20-1 7-20-3 Indication / Warning 7-20-1 7-21 Stall Warning / Stick Pusher System 7-21-1 7-21-1 General 7-21-1 7-21-2 Description 7-21-1 7-21-3 Operation 7-21-2 7-21-4 Indication / Warning 7-21-3...
  • Page 595 Section 7 - Airplane and Systems Description Table of Contents Subject Page 7-27-7 Situation Awareness Multifunction Display 7-27-20 7-27-8 Systems Multifunction Display 7-27-20 7-27-9 Indication / Warning 7-27-23 7-28 Primus APEX - Attitude and Heading 7-28-1 7-28-1 General 7-28-1 7-28-2 Air Data and Attitude Heading Reference System (ADAHRS) 7-28-1 7-28-3...
  • Page 596 Section 7 - Airplane and Systems Description Table of Contents Subject Page 7-31-8 CAS Advisory Messages (CYAN) 7-31-12 7-31-9 CAS Status Messages (WHITE) 7-31-14 7-32 Primus APEX - Automatic Flight Control System 7-32-1 7-32-1 General 7-32-1 7-32-2 Description 7-32-2 7-32-3 Operation 7-32-5 7-32-4...
  • Page 597 Section 7 - Airplane and Systems Description Table of Contents Subject Page 7-38-1 General 7-38-1 7-38-2 Description 7-38-1 7-38-3 VNAV Modes 7-38-1 7-38-4 Pilot’s Display 7-38-2 7-38-5 VNAV Operation Description 7-38-10 7-38-6 Visual Approach (optional) 7-38-12 7-39 Primus APEX - Optional LPV/LP Approach 7-39-1 7-39-1 General...
  • Page 598 Section 7 - Airplane and Systems 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...

  • Page 599: General

    Section 7 - Airplane and Systems Description General General The airplane is a low wing, T-tail, single engine, retractable landing gear type designed to transport passengers, cargo, or various combinations of both passengers and cargo. Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 7-1-1...
  • Page 600 Section 7 - Airplane and Systems Description General This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 7-1-2...

  • Page 601: Airframe

    Section 7 - Airplane and Systems Description Airframe Airframe 7-2-1 General The aircraft construction is conventional semimonocoque, primarily incorporating aluminum alloy, but composite structures are used in certain areas. Flush riveting is used where appropriate to minimize drag. Access panels are installed to facilitate inspection and maintenance.
  • Page 602 Section 7 - Airplane and Systems Description Wings Each wing contains an integral fuel tank, aileron, flaps, de-ice boot, and main landing gear. The fuel tanks are located between ribs 3 and 16, forward of the main spar to the nose rib and between ribs 6 and 16 behind the main spar to the rear spar.

  • Page 603: Aileron

    Section 7 - Airplane and Systems Description Flight Controls Flight Controls 7-3-1 General Refer to Fig. 7-3-1. Flight Controls - General, for system controls and flap operation. The flight control system is conventional using push-pull rods and carbon steel cables. Electric trim systems are provided for the aileron, rudder, and elevator.

  • Page 604: Trim

    Section 7 - Airplane and Systems Description Trim 7-3-5 Trim The aileron, horizontal stabilizer and rudder trim are electrically operated. Aileron and horizontal stabilizer trim operation is controlled by a switch on the outboard yoke of each control wheel, rudder trim operation is controlled by a switch on the Engine Power Control Lever.

  • Page 605: Flaps

    Section 7 - Airplane and Systems Description Flaps A rotation sensor is installed on each of the outer flap screw actuators. These sense the rotation of the flexible shafts and give signals to the FCWU. The FCWU monitors these signals for asymmetrical flexible shaft rotation of more than 20 rotations (caused by a broken inner flap drive shaft).
  • Page 606 Section 7 - Airplane and Systems Description Indication / Warning 7-3-7 Indication / Warning Symbolic aircraft views of the trim positions for the aileron trim tab (roll), rudder trim tab (yaw) and horizontal stabilizer (pitch) are shown in the TRIM window of the systems MFD. In flight, the trim indications are shown in white.
  • Page 607 Section 7 - Airplane and Systems Description Indication / Warning GEAR FLAP Pitch Trim Runaway Yaw Trim Runaway Flaps Takeoff Configuration TRIM SYSTEM MFD AILERON AND AILERON AND HOZN STAB HOZN STAB TRIM SWITCH TRIM SWITCH TRIM TRIM ENGAGE ENGAGE SWITCH SWITCH CONTROL WHEEL...
  • Page 608 Section 7 - Airplane and Systems Description Indication / Warning This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 7-3-6...

  • Page 609: General

    Section 7 - Airplane and Systems Description Landing Gear Landing Gear 7-4-1 General Refer to Fig. 7-4-2. Landing Gear System, for system operation. The landing gear is a conventional tricycle configuration that is extended and retracted using electromechanical actuators. Landing gear operation is completely automatic upon pilot gear selection.
  • Page 610 Section 7 - Airplane and Systems Description Electromechanical Actuators 7-4-3 Electromechanical Actuators 7-4-3.1 Description Both nose landing gear and main landing gear actuators have the same functionality and are electromechanical, self-rigging type actuators. The actuator motor control and monitoring electronics are incorporated within the actuator. Control is provided by the landing gear selector handle and the landing gear control system (including the Gear Relay Unit).
  • Page 611 Section 7 - Airplane and Systems Description Indication/Warning Condition of left main gear, Color and Font Gear right main gear and nose Display gear Amber cross on black State is 'undetermined' background White UP with white box State is 'Gear Up' normal outline State is 'Gear Up' declutter Grey UP with grey box...
  • Page 612 Section 7 - Airplane and Systems Description Indication/Warning The Flight Alerting System (FAS) will initiate a Gear warning message on the Primary Flight Display (PFD) and an aural warning will sound if the landing gear is not down and locked whilst in the air with: −...
  • Page 613 Section 7 - Airplane and Systems Description Emergency Extension System 7-4-5 Emergency Extension System To manually extend the landing gear set the landing gear selector handle to DN with airspeed 120 KIAS. Open the Emergency Gear Extension Lever cover and pull the Emergency Lever. This will allow the landing gear to free fall.
  • Page 614 Section 7 - Airplane and Systems Description Emergency Extension System ICN-12-C-A150704-A-S4080-00004-A-002-01 Figure 7-4-2: Landing Gear System (Sheet 1 of 3) Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 7-4-6...
  • Page 615 Section 7 - Airplane and Systems Description Emergency Extension System GEAR Gear Actuator Cntl Invalid Gear Config Gear Control Fault PARKING BRAKE HANDLE CAS WINDOW EMERG GEAR CTL PRI CTL SEC GEAR EMERG CTL PRI CTL SEC LANDING GEAR SELECTOR HANDLE EMERGENCY LANDING LG CONTROL PANEL GEAR RELEASE...
  • Page 616 Section 7 - Airplane and Systems Description Emergency Extension System LDG GEAR NOSE RH UP LH UP PROX RH GEAR UP PROX PROX NOSE GEAR UP NOSE NOSE DOWN & LOCKED LOCK LH DW RH DW LOCK LOCK RH DOWN &...

  • Page 617: Brakes

    Section 7 - Airplane and Systems Description Air / Ground System 7-4-6 Air / Ground System The aircraft “in air” or “on ground” (AIR/GND) status is determined from a combination of aircraft systems interfaced to the MAU: − LH main gear proximity switch −...
  • Page 618 Section 7 - Airplane and Systems Description Brakes The brake system consists of a brake fluid reservoir, four brake master cylinders, a left and right shuttle valve, a parking brake valve, and two brake assemblies. If the pilot and copilot simultaneously apply pressure to the same side brake pedal, the one applying the greatest pressure will control the braking.
  • Page 619 Section 7 - Airplane and Systems Description Wheels and Tires 7-4-8 Wheels and Tires The wheels are split-hub type, the main wheels have three fusible plugs which melt when there is too much heat from the brakes. Tubeless tires are installed on the wheels and each wheel has a tire inflation valve and an overinflation safety plug.
  • Page 620 Section 7 - Airplane and Systems Description Wheels and Tires BRAKE FLUID RESERVOIR LEFT RIGHT LEFT RIGHT PILOT BRAKE/ COPILOT BRAKE/ MASTER CYLINDER MASTER CYLINDER ASSEMBLIES ASSEMBLIES LEFT RIGHT SHUTTLE SHUTTLE VALVE VALVE TO PARKING BRAKE T-HANDLE PARKING BRAKE VALVE (SHOWN WITH PARKING BRAKE NOT SET) NOT SET...

  • Page 621: General

    Section 7 - Airplane and Systems Description Baggage Compartment Baggage Compartment 7-5-1 General A baggage compartment is provided at the rear of the cabin and is accessible during flight. A standard luggage net is secured at twelve attachment points to secure the baggage. An extendible baggage net can be installed instead of the standard net, to secure baggage in front of and in the baggage compartment.
  • Page 622 Section 7 - Airplane and Systems Description General This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 7-5-2...
  • Page 623 Section 7 - Airplane and Systems Description Cargo Tie-Downs Cargo Tie-Downs 7-6-1 General Tie-down anchor points fit into the seat rails and lock into place by an over-center lever. Tie- down straps can be secured to these anchor points. Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 7-6-1...
  • Page 624 Section 7 - Airplane and Systems Description General This Page Intentionally Left Blank Pilot's Operating Handbook Report No: 02406 Issue date: Mar 06, 2020 Page 7-6-2...

  • Page 625: Seats

    Section 7 - Airplane and Systems Description Seats / Restraint Systems Seats / Restraint Systems 7-7-1 Seats 7-7-1.1 Crew Seats Refer to Fig. 7-7-1, Crew Seat - Controls The crew seats are adjustable fore and aft and vertically. They also have controls for recline, thigh support, back cushion lumbar support, armrests and headrest.

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Pc-12/47e 2001

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