Hawker Beechcraft Hawker 850XP Flight Manual

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Serials 258750 thru 258788, 258795 and 258802

Serials 258789 thru 258794, 258796 thru 258801, 258803 and After

Airplane Flight Manual

AIRPLANES EQUIPPED WITH COLLINS PRO LINE 21 AVIONICS

Airplane Serial Number:...................................................

Airplane Registration Number:..........................................

Original Issue: Feb 28, 2006

Revision A3: Apr 26, 2007

When Kit 140-1702 is Installed

FAA Approved

For Training Purposes Only

and

P/N 140-590035-0005

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Page 1 Airplane Flight Manual AIRPLANES EQUIPPED WITH COLLINS PRO LINE 21 AVIONICS Airplane Serial Number:........... Airplane Registration Number:.......... © Copyright 2007 Hawker Beechcraft Corporation. All rights reserved. Original Issue: Feb 28, 2006 P/N 140-590035-0005 Revision A3: Apr 26, 2007 For Training Purposes Only...
Page 2 NOTE Raytheon Aircraft Company, which has been renamed Hawker Beechcraft Corporation, is now owned by Hawker Beechcraft, Inc. Neither Hawker Beechcraft, Inc. nor Hawker Beechcraft Corporation are affiliated any longer with Raytheon Company. Any Raytheon marks contained in this document are owned by Raytheon Company and are employed pursuant to a limited license granted by Raytheon Company.
Page 3 Airplane Flight Manual LIST OF EFFECTIVE PAGES FAA Approved Airplane Flight Manual P/N 140-590035-0005 Revision A3: April 26, 2007 This List of Effective Pages contains all current pages issued to this manual. It should be used to ensure the manual is complete and up-to-date. Section &...
Page 4 Airplane Flight Manual LIST OF EFFECTIVE PAGES (continued) Section & Page Revision & Date Section & Page Revision & Date Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Revision A1: Mar 6, 2007 Original Issue: Feb 28, 2006 Revision A1: Mar 6, 2007 Original Issue: Feb 28, 2006...
Page 5 Airplane Flight Manual LIST OF EFFECTIVE PAGES (continued) Section & Page Revision & Date Section & Page Revision & Date Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006...
Page 6 Airplane Flight Manual LIST OF EFFECTIVE PAGES (continued) Section & Page Revision & Date Section & Page Revision & Date Section - 5 PERFORMANCE Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006...
Page 7 Airplane Flight Manual LIST OF EFFECTIVE PAGES (continued) Section & Page Revision & Date Section & Page Revision & Date Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006...
Page 8 Airplane Flight Manual LIST OF EFFECTIVE PAGES (continued) Section & Page Revision & Date Section & Page Revision & Date Sub-section 5.40 EN-ROUTE DATA Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006...
Page 9: Faa Approved Revision A3: Apr
Airplane Flight Manual LIST OF EFFECTIVE PAGES (continued) Section & Page Revision & Date Part 2 Revision A3: Apr 26, 2007 Revision A3: Apr 26, 2007 Section - 7 SUPPLEMENTS Original Issue: Feb 28, 2006 Original Issue: Feb 28, 2006 See LOG OF SUPPLEMENTS Page 7 of 7 FAA Approved...
Page 10: Sub-Section
LOG OF TEMPORARY CHANGES FAA Approved Airplane Flight Manual P/N 140-590035-0005 Issue Date: February 28, 2011 Active Temporary Changes must be inserted into this manual for all flight operations. Part Number Subject Date 140-590035-0005TC1 Instructions regarding erroneous EGPWS Feb 28, 2006 announcements during approach or landing.
Page 11 FAA Approved Airplane Flight Manual LOG OF TEMPORARY CHANGES (continued) Part Number Subject Date NOTE: Temporary Changes TC9, TC10 and TC11 not issued. 140-590035-0005TC12 Revised text with additional information and Dec 23, 2010 procedures for AIRFRAME ICE PROTECTION SYSTEM MALFUNCTIONS. Sub-section 4.05 - ABNORMAL PROCEDURES, Page 39.
Page 12: Revision A3: April
Airplane Flight Manual LOG OF REVISIONS FAA Approved Airplane Flight Manual P/N 140-590035-0005 Revision A3: April 26, 2007 Section & Page Description Title Page Updated for Revision A3. Logo Page Aligned "Published By" text, no technical change. List of Effective Pages Updated for Revision A3.
Page 13 Airplane Flight Manual LOG OF REVISIONS (continued) Section & Page Description Page 2 of 2 For Training Purposes Only...
Page 14 Revised title page to reflect the new Hawker Beechcraft logo. Changed the copyright statement to reflect Hawker Beechcraft Corporation. Revised the header on the logo page to reflect Hawker Beechcraft Corporation. Added the Hawker Beechcraft, Inc. owner statement to logo page.
Page 15: Revision A1: Mar
Hawker 850XP Pro Line 21 Airplane Flight Manual LOG OF REVISIONS FAA Approved Airplane Flight Manual P/N 140-590035-0005 Revision A1: Mar 6, 2006 Section & Page Description Title Page Corrected airplane serial number effectivity. Logo Page Aligned GAMA logo, no technical change.
Page 16 Hawker 850XP Pro Line 21 Airplane Flight Manual LOG OF REVISIONS FAA Approved Airplane Flight Manual P/N 140-590035-0005 Original Issue: February 28, 2006 Section & Page Description All Sections Original Issue. Refer to the LIST OF EFFECTIVE PAGES. Pages Page 1 of 1...
Page 17: Table Of Contents
Hawker 850XP Pro Line 21 Airplane Flight Manual SECTION 1 GENERAL Table of Contents Page INTRODUCTION .....................3 IMPORTANT NOTICE...................3 USE OF THE AIRPLANE FLIGHT MANUAL..........4 REVISING THE AIRPLANE FLIGHT MANUAL ..........5 TEMPORARY CHANGES ................5 INSTRUCTION SHEET ................6 REVISION SERVICE ..................6 SUPPLEMENTS ...................6...
Page 18 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Section - 1 FAA Approved Page 2 GENERAL Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 19: Introduction
It contains the information required by 14 CFR Part 25 for safe operation of the Hawker 850XP airplane equipped with Collins Pro Line 21 avionics and winglets. It shall be the responsibility of the owner/operator to make sure the latest revisions of publications referenced in this Airplane Flight Manual are utilized during operation, servicing and maintenance of the airplane.
Page 20: Use Of The Airplane Flight Manual
Hawker 850XP Pro Line 21 Airplane Flight Manual WARNING: USE ONLY GENUINE RAYTHEON AIRCRAFT OR RAYTHEON AIRCRAFT APPROVED PARTS OBTAINED FROM RAYTHEON APPROVED SOURCES, IN CONNECTION WITH THE MAINTENANCE AND REPAIR OF HAWKER AIRPLANES. GENUINE RAYTHEON AIRCRAFT PARTS ARE PRODUCED AND INSPECTED UNDER RIGOROUS PROCEDURES TO MAKE SURE AIRWORTHINESS AND SUITABILITY FOR USE IN HAWKER AIRPLANE APPLICATIONS.
Page 21: Revising The Airplane Flight Manual
Hawker 850XP Pro Line 21 Airplane Flight Manual REVISING THE AIRPLANE FLIGHT MANUAL The Airplane Flight Manual is designed to facilitate maintaining the documents necessary for the safe and efficient operation of the airplane. The manual has been prepared in loose-leaf form for ease of maintaining and incorporates quick-reference tabs imprinted with the title for each section.
Page 22: Instruction Sheet
Hawker 850XP Pro Line 21 Airplane Flight Manual INSTRUCTION SHEET An INSTRUCTION SHEET will be provided for each reissue or revision of the Airplane Flight Manual. The heading of the INSTRUCTION SHEET identifies the publication action and part number of the affected Airplane Flight Manual. The body of the INSTRUCTION SHEET lists all effected pages of the reissue or revision with instructions for incorporating the action.
Page 23: Airplane Flight Manual Supplements Revision Record
Hawker 850XP Pro Line 21 Airplane Flight Manual AIRPLANE FLIGHT MANUAL SUPPLEMENTS REVISION RECORD Section 7, SUPPLEMENTS, contains FAA-approved Airplane Flight Manual Supplements, headed by a LOG OF SUPPLEMENTS page. On the LOG page is a listing of the FAA-approved Supplemental Equipment available for installation on the airplane.
Page 24: Section 1 - General
Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Section - 1 FAA Approved Page 8 GENERAL Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 25: Section 2 - Limitations
Hawker 850XP Pro Line 21 Airplane Flight Manual CONTENTS SECTION 1 - GENERAL This section provides manual introduction, contents and general information of the Hawker 850XP airplane equipped with Collins Pro Line 21 avionics and winglets. SECTION 2 - LIMITATIONS This section provides FAA-approved limitations necessary for the safe operation of the Hawker 850XP airplane equipped with Collins Pro Line 21 avionics.
Page 26 Hawker 850XP Pro Line 21 Airplane Flight Manual Annunciators Throughout the procedural sections of this Airplane Flight Manual, annunciators are provided as shown below: EMERGENCY ADVISORY ABNORMAL OIL 1 HYD 1 AUX FUEL LO PRESS LO PRESS • MWS annunciators located on the overhead roof panel are provided on the left side of the page.
Page 27: Section 4 - Abnormal/Normal Procedures
SECTION 5 - PERFORMANCE The performance information provided in this section relates to a Hawker 850XP airplane equipped with Collins Pro Line 21 avionics and powered by two Allied-Signal TFE731-5BR-1H turbofan engines with an Automatic Power Reserve system (APR). It is the responsibility of the operator to observe the limiting conditions specified.
Page 28: Section 6 - Weight & Balance
Hawker 850XP Pro Line 21 Airplane Flight Manual SECTION 6 - WEIGHT & BALANCE The data within this section is intended to make sure that the airplane is operated within the appropriate weight and center of gravity limitations. The "Basic Empty Weight and Balance - As Licensed"...
Page 29: Abbreviations And Acronyms
Hawker 850XP Pro Line 21 Airplane Flight Manual ABBREVIATIONS and ACRONYMS The use of capital letters in the text, apart from normal grammatical usage, indicates the actual markings of equipment, gauges, controls and control positions on the airplane. Abbreviations and acronyms used in this manual have the following meanings: AC or ac.........Alternating Current...
Page 30 Hawker 850XP Pro Line 21 Airplane Flight Manual EAS........Equivalent Air Speed EGPWS......... Enhanced Ground Proximity Warning System EGT........Exhaust Gas Temperature ENG ........Engine EPNdB ........Effective Perceived Noise decibel ESIS........Electronic Standby Instrument System FD ......... Flight Director F/DK........
Page 31 Hawker 850XP Pro Line 21 Airplane Flight Manual MPH or mph ......Miles Per Hour ........Rough Air Mach Number MSG ........Message MWS........Master Warning System NAV ........Navigation ..........Engine LP Shaft Speed (%) ........Engine LP Shaft Reference Speeds (%) 1 REF ..........Engine HP Shaft Speed (%) OAT ........Outside Air Temperature...
Page 32 Hawker 850XP Pro Line 21 Airplane Flight Manual US Gal(s) ......US Gallon(s) V or v........Volt(s) VFR........Visual Flight Rules VHF........Very High Frequency VLV ........Valve VNAV ........Vertical Navigation VOR ........VHF Omnidirectional Radio Range VSI ........Vertical Speed Indication ........
Page 33: Definitions
Hawker 850XP Pro Line 21 Airplane Flight Manual DEFINITIONS NOTE: Definitions of terms used primarily in performance calculations are given in Section 5, Sub-section 5.05. The indicated airspeed is the reading obtained on a pitot static airspeed indicator having no instrument calibration error.
Page 34: International Standard Atmosphere (Isa)
Hawker 850XP Pro Line 21 Airplane Flight Manual International Standard Atmosphere (ISA) For the relationship between air temperature and pressure altitude in the International Standard Atmosphere, refer to Sub-section 5.05, Figure 5.05.16 ISA TEMPERATURES. Standard Mean Chord (SMC) Wing area...
Page 35 Hawker 850XP Pro Line 21 Airplane Flight Manual GENERAL DIMENSIONS 9 FT 2 IN (2.79M) TRACK 54 FT 4 IN (16.55M) 51 FT 1.64 IN (15.59 M) OVERALL LENGTH) 20 FT (6.10M) TAIL SPAN 17 FT 5 IN (5.31 M) OVERALL HEIGHT 21 FT 0.5IN (6.41M)
Page 36 Hawker 850XP Pro Line 21 Airplane Flight Manual SECTION 2 LIMITATIONS Table of Contents Page KINDS OF OPERATION..................5 WEIGHT LIMITATIONS ..................5 PERFORMANCE LIMITATIONS ............... 5 Take-off Weight................... 5 Landing Weight ..................5 Take-off Field Length .................. 6 OPERATIONAL LIMITATIONS................6 Altitude ......................
Page 37 Hawker 850XP Pro Line 21 Airplane Flight Manual Page FUEL LIMITATIONS ..................15 Fuel Specifications ..................15 Fuel Additives ................... 16 Maximum Fuel Temperature ..............17 Minimum Fuel Temperature ..............17 Fuel Quantity..................... 17 Fuel Loading ..................... 18 Pressure Refueling ................... 18 Fuel System Management ................
Page 38 Hawker 850XP Pro Line 21 Airplane Flight Manual Page MISCELLANEOUS LIMITATIONS..............27 Air Brakes ....................27 Cabin Emergency Overwing Exit .............. 27 Cabin High Datum ..................27 Crew Seats ....................27 Ditching..................... 27 Inter-compartment Door................27 Lift Dump ....................27 Maneuvering Load Factor Limitations............
Page 39 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Section - 2 FAA Approved Page 4 Original Issue: Feb 28, 2006 LIMITATIONS For Training Purposes Only...
Page 40: Kinds Of Operation
Hawker 850XP Pro Line 21 Airplane Flight Manual KINDS OF OPERATION This airplane is eligible for certification in the Transport Category and is approved for the following kinds of operation when the appropriate instruments and equipment required by the airworthiness and/or operating certificate are installed and approved and are in operable condition.
Page 41: Take-Off Field Length
Hawker 850XP Pro Line 21 Airplane Flight Manual Take-off Field Length The take-off weight shall not exceed the maximum permitted by field length considerations as described in Sub-section 5.20 for the restricted range of conditions listed. When complying with the above, the following conditions shall be met: •...
Page 42: Runway Slope
Hawker 850XP Pro Line 21 Airplane Flight Manual Runway Slope The maximum effective runway slopes for takeoff are 2% uphill and 2% downhill. Airplane Configurations The airplane configurations as stated in Sub-section 5.05 must be observed. COMPARTMENT LOADING LIMITATIONS The airplane must be loaded in accordance with Section 6 - WEIGHT & BALANCE of this Airplane Flight Manual and as provided on placards in the Baggage/Stowage Compartments.
Page 43: Pounds/Feet
Hawker 850XP Pro Line 21 Airplane Flight Manual LOADING and FLIGHT ENVELOPE - POUNDS/FEET PERCENT STANDARD MEAN CHORD (SMC) 29,000 MAXIMUM RAMP WEIGHT 28,120 lb MAXIMUM TAKE-OFF WEIGHT 28,000 lb 28,000 27,000 ZONE A 26,000 USABLE ONLY WITH VENTRAL TANK FUEL...
Page 44: Kilograms/Meters
Hawker 850XP Pro Line 21 Airplane Flight Manual LOADING and FLIGHT ENVELOPE - KILOGRAMS/METERS PERCENT STANDARD MEAN CHORD (SMC) MAXIMUM RAMP WEIGHT 12,755 kg 12,900 MAXIMUM TAKE-OFF WEIGHT 12,701 kg 12,400 11,900 ZONE A USABLE ONLY WITH VENTRAL TANK FUEL...
Page 45 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Section - 2 FAA Approved Page 10 Original Issue: Feb 28, 2006 LIMITATIONS For Training Purposes Only...
Page 46: Ice Protection Limitations
P/N 140-590035-0005TC7 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE SERIAL NUMBERS AFFECTED: All Hawker 850XP serial numbers. DESCRIPTION OF CHANGE: Revised criteria for in-flight icing. FILING INSTRUCTIONS: Insert this Temporary Change Page 1 of 1 into the Hawker 850XP FAA Approved Airplane Flight Manual to face Page 11 in Section 2 - LIMITATIONS.
Page 47: Airframe Icing
Hawker 850XP Pro Line 21 Airplane Flight Manual ICE PROTECTION LIMITATIONS Icing General Icing conditions exist when Outside Air Temperature (OAT) on the ground and during takeoff, is 10° C SAT or below, and visible moisture in any form is present (e.g. clouds, fog with visibility of 1 mile (1600 meters) or less, rain, snow, sleet and ice crystals).
Page 48: Severe Icing Conditions Limitations
Hawker 850XP Pro Line 21 Airplane Flight Manual SEVERE ICING CONDITIONS LIMITATIONS WARNING: SEVERE ICING MAY RESULT FROM ENVIRONMENTAL CONDITIONS OUT- SIDE 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...
Page 49: Engine Limitations
Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINE LIMITATIONS Engine Type Two Allied Signal TFE731-5BR-1H turbofan engines. Engine Limitations % RPM CONDITION MAX ITT °C TIME LIMIT Unrestricted Start or Relight * ---- ---- 10 Seconds over 996 5 Seconds...
Page 50: Approved Engine Oils
Hawker 850XP Pro Line 21 Airplane Flight Manual Approved Engine Oils Airplanes which have not accomplished Airplanes which have accomplished Honeywell Service Bulletin Honeywell Service Bulletin 72-3597 or 72-3662 72-3597 or 72-3662 Aeroshell/Royco Turbine Oil 500 Mobil 254 Aeroshell/Royco Turbine Oil 560...
Page 51: Thrust Reversers
Hawker 850XP Pro Line 21 Airplane Flight Manual Thrust Reversers • Deployment of either thrust reverser is restricted to ground operations only. • The thrust reverse levers must not be selected until the airplane is on the ground. • Engine starts with thrust reversers deployed are prohibited.
Page 52: Fuel Additives
Hawker 850XP Pro Line 21 Airplane Flight Manual Aviation wide-cut fuel to the current approved issue of the following specifications British DEF STAN 91-88 (D.E.R.D. 2454) American ASTM D1655/JET B MIL-T-5624/JP4 MIL-T-5624/JP5 Canadian CAN/CGSB 3.22/JET B Russian GOST 10227-86 T-2...
Page 53: Maximum Fuel Temperature
Hawker 850XP Pro Line 21 Airplane Flight Manual Maximum Fuel Temperature The maximum permissible fuel temperature is 57° C. Minimum Fuel Temperature To avoid the possibility of fuel freezing or exceeding engine limitations, the following ambient air and indicated fuel temperature limitations should be observed:...
Page 54: Fuel Loading
Hawker 850XP Pro Line 21 Airplane Flight Manual Fuel Loading Fuel tanks may be replenished in any sequence provided that the appropriate refueling instructions are observed and that the following preflight fuel loading conditions are achieved: 1. Fuel contained in the wing tanks shall be equally disposed between the two wing tanks.
Page 55: Avionics Limitations
Hawker 850XP Pro Line 21 Airplane Flight Manual AVIONICS LIMITATIONS General 1. The following documents must be carried onboard the airplane at all times: • Collins Pro Line 21 Avionics System for the Hawker 800XP Pilot’s Guide P/N 523-0780409, 1st Edition dated May 31, 2001 or latest revision.
Page 56 Hawker 850XP Pro Line 21 Airplane Flight Manual Flight Management System continued 3. During periods of dead reckoning, the FMS shall not be used for navigation. 4. All FMS navigation operations are approved within the U.S. National Airspace System and latitudes bounded by 60°...
Page 57 TEMPORARY CHANGE P/N 140-590035-0005TC4 P/N 140-590035-0005TC4 (Issue 2) Page 2 of 2 May 1, 2008 For Training Purposes Only...
Page 58: Flight Management System
P/N 140-590035-0005TC4 (Issue 2) PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual P/N 140-590035-0005. AIRPLANE SERIAL NUMBERS AFFECTED: All Hawker 850XP serial numbers. DESCRIPTION OF CHANGE: Revised the P-RNAV equipment list to include DBU-5000. Remove and destroy existing Temporary Change 4 Pages 1...
Page 59: Autopilot
Hawker 850XP Pro Line 21 Airplane Flight Manual Flight Management System continued • Operation in European B-RNAV/RNP-5 airspace in accordance with AC 90-96 and AC 20- 130A. This does not constitute an operational approval. • Minimum Navigation Performance Specification (MNPS) airspace when equipped with...
Page 60: Vnav
Hawker 850XP Pro Line 21 Airplane Flight Manual Autopilot continued 5. Maximum airspeed for operation of the autopilot system must not exceed the airplane indicated maximum speed V 6. Operation of the autopilot system with a pitch trim malfunction is prohibited.
Page 61: Egpws
Hawker 850XP Pro Line 21 Airplane Flight Manual VNAV continued 6. VNAV approach guidance to a DA is not authorized if the reported surface temperature is below the Baro-VNAV minimum temperature limitation specified on the applicable RNAV approach procedure chart.
Page 62: Mode S Enhanced Surveillance Transponder
Hawker 850XP Pro Line 21 Airplane Flight Manual Mode S Enhanced Surveillance Transponder The installed Mode S system satisfies the data requirements of the International Civil Aviation Organization (ICAO) Doc. 7030/4, Regional Supplementary Procedures for SSR Mode S Enhanced Surveillance in designated European airspace.
Page 63: Airspeed Limitations
Hawker 850XP Pro Line 21 Airplane Flight Manual AIRSPEED LIMITATIONS Maximum Operating Speed ..........280 KIAS (Ventral fuel tank not empty, Flaps 0°) ..........335 KIAS (Ventral fuel tank empty, Flaps 0°) Sea Level to 12,000 ft, reducing by 1 kt per 680 ft to 310 KIAS at 29,000 ft.
Page 64: Air Brakes
Hawker 850XP Pro Line 21 Airplane Flight Manual Air Brakes Air Brakes (Flaps 0° Only) ......No Limit Landing Gear Extended/Operating Speed ......... 220 KIAS Bird Strike Speed Under normal conditions the maximum permissible airspeed to meet bird strike requirements is 280 KIAS up to 8000 ft.
Page 65: Miscellaneous Limitations
Hawker 850XP Pro Line 21 Airplane Flight Manual MISCELLANEOUS LIMITATIONS Air Brakes In flight, the air brakes must not be operated when the flaps are extended to any position. Cabin Emergency Overwing Exit The internal cabin emergency overwing exit locking pin, if installed, must be removed and stowed before each flight.
Page 66: Rudder Bias
Hawker 850XP Pro Line 21 Airplane Flight Manual Rudder Bias The rudder bias switches must be ON and the systems operative during each takeoff. Smoking When the airplane is being operated in the Transport Category (Passenger), smoking in the toilet compartment is prohibited.
Page 67 Hawker 850XP Pro Line 21 Airplane Flight Manual Table 1 - Take-off Weights for Wheel Brakes Waiting Period Temperature °C Field Pressure Altitude ft Take-off Weight 21,100 lb 20,500 lb 20,000 lb 19,500 lb 19,300 lb 19,100 lb 14,000 9570 kg...
Page 68 Hawker 850XP Pro Line 21 Airplane Flight Manual SECTION 3 EMERGENCY PROCEDURES Table of Contents Page ENGINES ENGINE FIRE, FAILURE or INADVERTENT THRUST REVERSER DEPLOYMENT DURING TAKEOFF Below V - Takeoff Aborted................3 ENGINE FIRE, FAILURE or INADVERTENT THRUST REVERSER DEPLOYMENT DURING TAKEOFF After V - Takeoff Continued ..............3...
Page 69 Hawker 850XP Pro Line 21 Airplane Flight Manual Page AVIONICS EGPWS WARNING (PULL UP MESSAGE ON PFD and/or PULL UP, or TERRAIN, TERRAIN PULL UP or OBSTACLE, OBSTACLE, PULL UP AURAL ALERT)......29 WINDSHEAR WARNING (RED WINDSHEAR MESSAGE ON PFD and/or WINDSHEAR, WINDSHEAR, WINDSHEAR AURAL ALERT) ....
Page 70: Engines
Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINES ENGINE FIRE, FAILURE or INADVERTENT THRUST REVERSER DEPLOYMENT DURING TAKEOFF Below V - Takeoff Aborted Thrust levers ............Close Brakes ..............Apply AIR BRAKES ............Deploy Thrust reversers ............Deploy Complete as applicable: ENGINE FIRE ON GROUND procedure - this section.
Page 71: Engine Fire In Flight
Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINE FIRE IN FLIGHT ENG 1 ENG 1 Fire Bell Sounds and FIRE FIRE ENG 2 ENG 2 Fire Bell Sounds and FIRE FIRE Thrust lever (affected engine)......Close If Fire Warning Persists HP COCK (affected engine)........Close...
Page 72: Engine Fire On Ground
Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINE FIRE ON GROUND ENG 1 ENG 1 Fire Bell Sounds and FIRE FIRE ENG 2 ENG 2 Fire Bell Sounds and FIRE FIRE START PWR switch (starting only) ..... PUSH FOR ABORT HP COCK (affected engine) .........
Page 73: Engine Shutdown Or Failure In Flight
Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINE SHUTDOWN or FAILURE IN FLIGHT Mechanical Failure, Malfunction, Separation or Inability to Maintain ITT or RPM Within Limits If failure occurs during initial climb, complete all of the following checks MAIN AIR VLVs 1 & 2 ............CLOSE F/DK VLV ...............CLOSE...
Page 74: Engine Failure In Landing Configuration
Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINE FAILURE IN LANDING CONFIGURATION If Landing Is Assured Thrust (operating engine)..........As required Airspeed...............V minimum HP COCK (affected engine).........Close LANDING CHECKS .............Complete If Landing Is Not Assured Thrust (operating engine)..........As required FLAP OVRD ..............Select FLAPS................Retract to 25°...
Page 75: Double Engine Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual DOUBLE ENGINE FAILURE NOTE: Headsets and hats must be removed before donning oxygen mask. ENG IGNITION 1 & 2 ........... ON Thrust levers............Close Crew oxygen ............Don masks if above 15,000 ft.
Page 76: Inadvertent Thrust Reverser Deployment In Flight
Hawker 850XP Pro Line 21 Airplane Flight Manual INADVERTENT THRUST REVERSER DEPLOYMENT IN FLIGHT UNLCK REVRS HP COCK (affected engine) ......... CLOSE If Thrust Reverser Does Not Stow AP & YD...............Disengage Airspeed...............Maintain 150 KIAS THRUST REVERSER POWER (affected engine) ..OFF Complete ENGINE SHUTDOWN or FAILURE IN FLIGHT procedure, this section.
Page 77 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Page 10 Section - 3 FAA Approved EMERGENCY PROCEDURES Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 78: Air Conditioning & Pressurization
Hawker 850XP Pro Line 21 Airplane Flight Manual AIR CONDITIONING & PRESSURIZATION DEPRESSURIZATION CABIN Horn sounds and ALTITUDE NOTE: Headsets and hats must be removed before donning oxygen mask. Crew oxygen ............Don masks Mic selector ............OXY- MIC If Cabin Depressurization Has Occurred MAIN AIR VLVs 1 &...
Page 79 Hawker 850XP Pro Line 21 Airplane Flight Manual DEPRESSURIZATION (continued) If Cabin Altitude Rising (Cabin Pressure Decreasing) or Cabin Altitude Fluctuating (Cabin Pressure Oscillating) Altitude ................35,000 ft or below No. 2 engine ..............Set high power MAIN AIR VLV 2.............CLOSE F/DK VLV ...............OPEN fully MAIN AIR VLV 1.............CLOSE...
Page 80: Rear Equipment Bay Overheat
Hawker 850XP Pro Line 21 Airplane Flight Manual REAR EQUIPMENT BAY OVERHEAT REAR BAY OVHT MAIN AIR VLVs 1 & 2..........CLOSE F/DK VLV ..............OPEN fully REAR BAY OVHT warning annunciator .......Check If Warning Annunciator Remains Illuminated NOTE: Headsets and hats must be removed before donning oxygen mask.
Page 81: High Pressure Air Overheat
Hawker 850XP Pro Line 21 Airplane Flight Manual HIGH PRESSURE AIR OVERHEAT HP AIR 1 HP AIR 2 OVHT OVHT MAIN AIR VLV (affected engine) ....... CLOSE F/DK VLV ............. CLOSE When Warning Extinguishes MAIN AIR VLV (affected engine)........LP ON F/DK VLV ...............As required...
Page 82: Electrical
Hawker 850XP Pro Line 21 Airplane Flight Manual ELECTRICAL DOUBLE GENERATOR FAILURE BATT 1 CNTCTR ELECT BATT 2 CNTCTR BUS TIE GEN 1 GEN 2 FAIL OPEN FAIL XS 1 XS 2 FAIL FAIL INV 1 INV 2 FAIL FAIL NOTES: 1.
Page 83 Hawker 850XP Pro Line 21 Airplane Flight Manual DOUBLE GENERATOR FAILURE (continued) If Generator Reset Unsuccessful ENG CMPTERs 1 & 2 ............OFF ENG ANTICE 1 & 2............ON Electrical loads...............Reduce to minimum, at pilot’s discretion. NOTES: 1. It is essential that electrical loads are kept to a minimum for flight. If this procedure is followed, there is sufficient battery power to maintain emergency loads for approximately 30 minutes.
Page 84 Hawker 850XP Pro Line 21 Airplane Flight Manual DOUBLE GENERATOR FAILURE (continued) If Generator Reset Unsuccessful (continued) 3. The emergency flight time quoted is based upon the assumption that at the time double generator failure occurs, the airplane batteries are at a minimum °...
Page 85 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Page 18 Section - 3 FAA Approved EMERGENCY PROCEDURES Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 86: Fire Or Smoke
Hawker 850XP Pro Line 21 Airplane Flight Manual FIRE OR SMOKE ELECTRICAL FIRE OR SMOKE NOTE: Headsets and hats must be removed before donning oxygen mask. Crew oxygen............Don masks - 100% EMERG Mic selector ............OXY- MIC Cabin notices ............ON DUMP VALVE..............
Page 87: Fuselage Fire Or Smoke
Hawker 850XP Pro Line 21 Airplane Flight Manual ELECTRICAL FIRE OR SMOKE (continued) SMOKE CEASES Services may be re-instated individually as required. Identify defective service and leave off. Visually verify that any fire has been extinguished and land at the nearest suitable airport.
Page 88: Smoke From Air Conditioning Ducts
Hawker 850XP Pro Line 21 Airplane Flight Manual SMOKE FROM AIR CONDITIONING DUCTS NOTE: Headsets and hats must be removed before donning oxygen mask. Crew oxygen............Don masks - 100% EMERG Mic selector ............OXY- MIC Cabin notices ............ ON DUMP VALVE ..............
Page 89 Hawker 850XP Pro Line 21 Airplane Flight Manual SMOKE FROM AIR CONDITIONING DUCTS (continued) WARNING: THE HIGHEST RECOMMENDED CABIN ALTITUDE FOR SUSTAINED FLIGHT IS 25,000 FT. Visually verify that any fire has been extinguished. If verification is not established, land at the nearest suitable airport.
Page 90: Landing Gear
P/N 140-590035-0005TC13 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE EFFECTIVITY: All Hawker 850XP airplanes. DESCRIPTION OF CHANGE: Additional procedures for THREE GREENS NOT INDICATED. FILING INSTRUCTIONS: Insert Temporary Change 13, Page 1 of 2, into Section 3, EMERGENCY PROCEDURES, to face Page 22.
Page 91 Read the following in place of the existing procedures that precede the CAUTION on Page 23. The CAUTION and remaining procedures are unchanged. THREE GREENS NOT INDICATED Annunciators.............. Test Are all gear locked down as shown by standby indicators? Make a normal landing HYD SUPPLY pressure ..........
Page 92 Hawker 850XP Pro Line 21 Airplane Flight Manual LANDING GEAR THREE GREENS NOT INDICATED Annunciators ............. Test HORN................ Pull circuit breaker (DA-D, K1) EGPWS..............Pull circuit breaker (DA-A, F8) Are all gear locked down as shown by standby indicators? Make a normal landing AUX HYD SYSTEM...........
Page 93 Hawker 850XP Pro Line 21 Airplane Flight Manual THREE GREENS NOT INDICATED (continued) Prepare For Landing Passengers..............Brief for emergency landing Loose equipment ............Secure Emergency exit............Confirm clear MAIN AIR VLVs 1 & 2 ..........CLOSE DUMP VALVE ............OPEN Landing • Land at as low a weight as possible.
Page 94: Nosewheel Not Centered With Landing Gear Locked Down
Hawker 850XP Pro Line 21 Airplane Flight Manual NOSEWHEEL NOT CENTERED WITH LANDING GEAR LOCKED DOWN If steering handwheel is offset to such a position that the nose gear is likely to steer the airplane off the runway: Turn the handwheel to the center position...
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Page 96: Wheel Brakes
Hawker 850XP Pro Line 21 Airplane Flight Manual WHEEL BRAKES BRAKE FAILURE Total or partial (asymmetric) failure of normal braking. Brake pedals.............Release WHEEL BRAKE lever ........EMERGY Brake pedals.............Apply gently - Use one continuous application if possible. NOTES: 1. Anti-skid will be inoperative.
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Page 98: Avionics
Hawker 850XP Pro Line 21 Airplane Flight Manual AVIONICS EGPWS WARNING (PULL UP MESSAGE ON PFD and/or PULL UP, or TERRAIN, TERRAIN PULL UP or OBSTACLE, OBSTACLE, PULL UP AURAL ALERT) NOTES: Only vertical maneuvers are recommended, unless operating in visual...
Page 99: Autopilot Malfunctions
Hawker 850XP Pro Line 21 Airplane Flight Manual AUTOPILOT MALFUNCTIONS ALTITUDE LOSSES The maximum altitude losses observed during autopilot malfunction tests were: Climb .................450 ft Cruise ................300 ft Descent ..............550 ft Maneuvering..............170 ft Non-Precision Approach (one or two engine)....75 ft Precision Approach (one or two engine) ....
Page 100: Autopilot Trim Fail Annunciation
Hawker 850XP Pro Line 21 Airplane Flight Manual AUTOPILOT MALFUNCTIONS (continued) AUTOPILOT TRIM FAIL ANNUNCIATION Illumination of a red TRIM annunciation on the PFDs indicates that the autopilot pitch trim system has failed. The autopilot will not automatically disengage, but it may not function properly.
Page 101: Flight Display Failure Flags
Hawker 850XP Pro Line 21 Airplane Flight Manual FLIGHT DISPLAY FAILURE FLAGS The following failure flags are available for display on the PFD. The flags will appear flashing red for 5 seconds and then remain illuminated. In the following steps, # is 1 when referencing the pilot’s side and 2 when referencing the copilot’s side.
Page 102: Fms
Hawker 850XP Pro Line 21 Airplane Flight Manual FLIGHT DISPLAY FAILURE FLAGS (continued) FMS # This annunciation indicates that the selected FMS navigation data is invalid. The course pointer, lateral deviation bar and to/from pointer are removed. Nav source..............Select another source This annunciation indicates that glideslope data is invalid and the glideslope pointer is removed.
Page 103: Ditching
Hawker 850XP Pro Line 21 Airplane Flight Manual DITCHING DITCHING PROCEDURES NOTE: Ditching has not been demonstrated; however, the following procedures are recommended: Preparation Cabin Notices ............ON Passengers..............Advise Life Jackets..............Don Pressurization............Set cabin altitude of 1500 ft DUMP VALVE ............Check SHUT External Lights............All On, unless reflections become...
Page 104: Emergency Evacuation
Hawker 850XP Pro Line 21 Airplane Flight Manual EMERGENCY EVACUATION In order to evacuate the airplane quickly, where possible the following procedures may be conducted concurrently. The pilot should brief actions to the copilot as appropriate. Airplane ............Stop WHEEL BRAKE lever........PARK HP COCKS............
Page 105 Hawker 850XP Pro Line 21 Airplane Flight Manual SECTION 4 - ABNORMAL / NORMAL PROCEDURES This section is divided into the following Sub-sections: Sub-section 4.05 ...........ABNORMAL PROCEDURES Sub-section 4.10 ...........NORMAL PROCEDURES FAA Approved Page 1 Original Issue: Feb 28, 2006...
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Page 107 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 4.05 ABNORMAL PROCEDURES Table of Contents Page ENGINES ENGINE RELIGHT..................5 IMMEDIATE RELIGHT ................5 WINDMILL RELIGHT .................6 STARTER ASSISTED (NORMAL) RELIGHT ..........7 Figure 4.05.1 - ENGINE RELIGHT ENVELOPE........8 ENGINE COMPUTER FAILURE ..............9 ABNORMAL INDICATIONS OR BEHAVIOR..........10...
Page 108 Hawker 850XP Pro Line 21 Airplane Flight Manual Page BATTERY CONTACTOR................24 XS 1 OR XS 2 FAIL.................. 25 SINGLE INVERTER FAILURE..............26 DOUBLE INVERTER FAILURE ............... 26 MWS DIMMER FAIL ................26 FLIGHT CONTROLS OUT OF TRIM INDICATION ..............27 MACH TRIM FAIL ..................
Page 109 Hawker 850XP Pro Line 21 Airplane Flight Manual Page Dual CDU Failure ................44 CVR Fault (CVR Fault Annunciator Illuminated) ........ 44 Single Audio System Failure .............. 45 Dual Audio System Failure ..............45 CAT II Malfunctions................45 Autopilot Mistrim Annunciation ............45 Radio Equipment Failure ..............
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Page 111: Engine Relight
Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINES ENGINE RELIGHT CAUTION: RELIGHTS SHOULD NOT BE ATTEMPTED IF ENGINE FAILURE IS ACCOMPANIED BY SYMPTOMS OF INTERNAL ENGINE DAMAGE OR THERE IS NO INDICATION OF N IMMEDIATE RELIGHT This procedure may be used if flame-out is detected quickly.
Page 112: Windmill Relight
Hawker 850XP Pro Line 21 Airplane Flight Manual WINDMILL RELIGHT Airspeed and altitude ..........Within envelope shown in Figure 4.05.1. RPM..............Indicating RPM..............10% or more HP COCK (affected engine) ........Close LP COCK (affected engine) ........OPEN ENG ANTICE (affected engine) ......... OFF Fuel pump (affected engine) ........
Page 113 Hawker 850XP Pro Line 21 Airplane Flight Manual STARTER ASSISTED (NORMAL) RELIGHT Airspeed and altitude..........Within envelope shown in Figure 4.05.1. & N RPM............. Both indicating HP COCK (affected engine) ........Close LP COCK (affected engine)........OPEN ENG ANTICE (affected engine)......... OFF Fuel pump (affected engine)........
Page 114 Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINE RELIGHT ENVELOPE STARTER ASSISTED RELIGHT ENGINE COMPUTER WINDMILLING OPERATIVE ENGINE STARTER COMPUTER ASSISTED INOPERATIVE RELIGHT INDICATED AIRSPEED - KIAS Engine Relight Data STARTER ASSISTED RELIGHT WINDMILL RELIGHT ENGINE Complete envelope available...
Page 115: Engine Computer Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual ENGINE COMPUTER FAILURE ENG 1 ENG 2 CMPTER CMPTER NOTE: The engine synchronizer disengages with an engine computer failure. If Malfunction Occurs During Takeoff Below 80 KIAS............Abort Above 80 KIAS ............Continue takeoff - Keep engine within N 1 REF.
Page 116: Abnormal Indications Or Behavior
Hawker 850XP Pro Line 21 Airplane Flight Manual ABNORMAL INDICATIONS OR BEHAVIOR If ITT or RPM Above Limits Thrust lever (affected engine)........Close If Indications Not Controlled Within Limits: HP COCK (affected engine) ........Close Complete ENGINE SHUTDOWN or FAILURE IN FLIGHT procedure - EMERGENCY PROCEDURES - Section 3.
Page 117: High Engine Vibration
Hawker 850XP Pro Line 21 Airplane Flight Manual HIGH ENGINE VIBRATION If engine malfunction is confirmed or general vibration is present, complete ENGINE SHUTDOWN or FAILURE IN FLIGHT procedure - EMERGENCY PROCEDURES - Section 3. If high engine vibration is suspected, complete the following procedure on each engine, one at a time: •...
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Page 119: One Engine Inoperative Approach And Landing
Hawker 850XP Pro Line 21 Airplane Flight Manual OPERATIONS ONE ENGINE INOPERATIVE APPROACH and LANDING Altimeters ..............Set and checked Fuel ................Check quantity and balance F/DK VLV ..............CLOSE EXTERIOR LIGHTS............As required Cabin notices ..............On Seats and harnesses ............ Secure Nosewheel steering ............
Page 120: Overweight Landing
Hawker 850XP Pro Line 21 Airplane Flight Manual OVERWEIGHT LANDING Perform normal APPROACH and LANDING CHECKS - NORMAL PROCEDURES - Sub-section 4.10. NOTES: 1. Touch down as smoothly as possible. 2. For the purpose of brake cooling, an overweight landing should be considered as a rejected takeoff.
Page 121: Flaps 25° Approach And Landing
Hawker 850XP Pro Line 21 Airplane Flight Manual FLAPS 25° APPROACH and LANDING Perform normal APPROACH and LANDING CHECKS - NORMAL PROCEDURES - Sub-section 4.10. FLAP OVRD...............Select Airspeed..............V +20 KIAS When Landing Is Assured Airspeed..............V +5 KIAS After Touchdown Lower Nosewheel to the Runway AIR BRAKE..............OPEN...
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Page 123: Thrust Reversers
Hawker 850XP Pro Line 21 Airplane Flight Manual THRUST REVERSERS RUDDER BIAS NOT INHIBITED REVERSER On the Ground With Thrust Reverse Selected Both Thrust Reverse Levers ........Reverse Idle UNLOCK AND/OR ARM INDICATIONS IN FLIGHT UNLCK and/or Associated THRUST REVERSER POWER switch ............OFF...
Page 124: Landing With One Thrust Reverser Deployed
Hawker 850XP Pro Line 21 Airplane Flight Manual LANDING WITH ONE THRUST REVERSER DEPLOYED Final Approach Airspeed..............150 KIAS maximum Landing Gear .............Down FLAP OVRD ............... Select FLAPS................Up Rudder Trim ...............Neutral position prior to touchdown At Landing Threshold Airspeed..............V +15 KIAS After Touchdown Airbrakes ..............OPEN - Lift Dump not available...
Page 125: Fuel
Hawker 850XP Pro Line 21 Airplane Flight Manual FUEL FUEL LOW LEVEL When the fuel contents of either wing tank are reduced to less than 320 lb (150 kg), set the WING FUEL/X-FEED/TRANSFER lever to X-FEED. A fuel quantity of at least 400 lb (180 kg) is required to complete a go-around and subsequent traffic pattern and landing.
Page 126: Auxiliary Fuel Transfer Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual AUXILIARY FUEL TRANSFER FAILURE AUX FUEL FUEL VENTRAL TANK indicator does not change from FULL within two minutes of selecting the AUX FUEL TRANSFER lever to the down position. Wing FUEL contents ..........Check...
Page 127: Air Conditioning & Pressurization
Hawker 850XP Pro Line 21 Airplane Flight Manual AIR CONDITIONING & PRESSURIZATION DUCT OVERHEAT DUCT OVHT CABIN TEMP (if installed)..........CPIT CABIN TEMP selector ..........Manual - Hold full COOL NOTE: Temperature changes in MANUAL mode should be made by short applications of the control.
Page 128: Flight Deck Heat Valve Stuck Open
Hawker 850XP Pro Line 21 Airplane Flight Manual FLIGHT DECK HEAT VALVE STUCK OPEN Air Conditioning Noise and Warm Incoming Air with F/DK VLV Selected CLOSE F/DECK AIR VLV circuit breaker........ Check (DA-D, E2) F/DK VLV ..............OPEN then CLOSE If Flight Deck Valve Remains Open MAIN AIR VLV 2............LP ON...
Page 129: Electrical
Hawker 850XP Pro Line 21 Airplane Flight Manual ELECTRICAL SINGLE GENERATOR FAILURE GEN 1 GEN 2 ELECT FAIL FAIL Failed GEN..............TRIP BUS TIE (if open) ............CLOSE GEN AMPS (operative unit) ........Check - If above limit (300 AMPS), reduce non-essential loads.
Page 130: Generators Out Of Balance
Hawker 850XP Pro Line 21 Airplane Flight Manual GENERATORS OUT OF BALANCE IF GENERATORS DIFFER BY MORE THAN 40 AMPS BUS TIE ......OPEN GEN 1 and GEN 2 AMPS ....Check each less than limit (300 AMPS). PS 1 and PS 2 volts ..Check each within 24.5 to 29.5 volts.
Page 131: Xs 1 Or Xs 2 Fail
Hawker 850XP Pro Line 21 Airplane Flight Manual XS 1 or XS 2 FAIL XS 2 XS 1 ELECT FAIL FAIL By use of the AC voltmeter, establish whether supplies are available on the affected busbar. Proceed as appropriate: If Supplies Not Available...
Page 132: Single Inverter Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual SINGLE INVERTER FAILURE INV 1 INV 2 ELECT FAIL FAIL All AC systems are available Do Not Attempt To Reset If INV 1 FAIL or INV 2 FAIL Annunciators Illuminate. DOUBLE INVERTER FAILURE...
Page 133: Out Of Trim Indication
Hawker 850XP Pro Line 21 Airplane Flight Manual FLIGHT CONTROLS OUT OF TRIM INDICATION ELEV/AIL TRIM If On Takeoff and Below 80 KIAS Thrust levers .............. Close Brakes ............... Apply AIR BRAKES ............. As required Thrust reversers ............As required...
Page 134: Landing By Use Of Trim System
Hawker 850XP Pro Line 21 Airplane Flight Manual LANDING BY USE OF TRIM SYSTEM Perform Normal APPROACH and LANDING CHECKS - NORMAL PROCEDURES - Sub-section 4.10. NOTES: 1. Steep turns should be avoided. 2. Attempt to utilize a runway that will result in as small a crosswind component as possible.
Page 135 Hawker 850XP Pro Line 21 Airplane Flight Manual LANDING BY USE OF TRIM SYSTEM (continued) Rudder and Elevator Unusable in Conjunction with an Engine Failure FLAP OVRD ...............Select FLAPS................25° Airspeed ..............V +20 KIAS Maintain this configuration and speed until touchdown.
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Page 137: Stall Warning & Identification
Hawker 850XP Pro Line 21 Airplane Flight Manual STALL WARNING & IDENTIFICATION STALL IDENTIFICATION Operation of the STALL WARNING (stick shake) or STALL IDENTIFICATION (stick push) must be accepted as indicative of a stall. Proceed with normal stall recovery actions.
Page 138: Stall Identification Component Malfunctions
Hawker 850XP Pro Line 21 Airplane Flight Manual STALL IDENTIFICATION COMPONENT MALFUNCTIONS Pilot Panel Copilot Panel STALL SQUAT IDENT FLAP SSU - Indicates a failure of one or both of the Signal Summing Units. Stall warning and identification may not operate. Continue flight with caution.
Page 139: Main Hydraulic Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual HYDRAULICS MAIN HYDRAULIC FAILURE HYD 1 HYD 2 LO PRESS LO PRESS If Hydraulic Supply Pressure Reduces to Approximately 2300 PSI or Below Refer to the Lowering of LANDING GEAR and FLAPS procedure below:...
Page 140: Emergency Brake Low Pressure
Hawker 850XP Pro Line 21 Airplane Flight Manual MAIN HYDRAULIC FAILURE (continued) Wheelbrake Operation Before Landing WHEEL BRAKE lever ..........If SUPPLY pressure is approximately 2300 PSI, leave in NORMAL (forward) position. If SUPPLY pressure is zero, select EMERGY. Brake pedals .............. Avoid use before landing Actions On Landing Brake pedals ..............
Page 141: Hydraulic System Overheat
Hawker 850XP Pro Line 21 Airplane Flight Manual HYDRAULIC SYSTEM OVERHEAT OVHT During Taxi (High Ambient Temperatures) Cycle the flaps twice over the operating range. If warning extinguishes, continue taxi. If warning remains illuminated, have fault corrected before flight. During Flight No in-flight action.
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Page 143: Landing Gear
Hawker 850XP Pro Line 21 Airplane Flight Manual LANDING GEAR LANDING GEAR DOES NOT RETRACT NOTE: Observe the V of 220 KIAS and the altitude limit of 20,000 ft. AUX HYD SYSTEM hand pump ....... Check socket fully down AUX HYD SYSTEM PULL handle......Set in If Gear Fails To Retract LANDING GEAR lever ..........
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Page 145: Ice Protection
Revised text with additional information and procedures for AIRFRAME ICE PROTECTION SYSTEM MALFUNCTIONS. FILING INSTRUCTIONS: Insert this Temporary Change Page 2 of 2 into the Hawker 850XP FAA Approved Airplane Flight Manual to face Page 39 in Section 4, Sub-section 4.05 - ABNORMAL PROCEDURES.
Page 146 TEMPORARY CHANGE P/N 140-590035-0005TC12 ICE PROTECTION AIRFRAME ICE PROTECTION SYSTEM MALFUNCTIONS The following information is directed toward TKS protected surfaces Indications of malfunction may include: • No pump running noise • No fluid remaining • Ice evident on wing TKS panel If a malfunction is apparent or suspected during flight, proceed as follows: •...
Page 147: Engine Antice
Hawker 850XP Pro Line 21 Airplane Flight Manual ICE PROTECTION ENGINE ANTICE ENG 2 ENG 1 and/or A/ICE A/ICE Thrust lever (affected engine) ........Gradually increase in small increments. If annunciator remains illuminated Avoid icing conditions if possible. ANTICE LOW QUANTITY...
Page 148: Pitot Heater Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual PITOT HEATER FAILURE L PITOT R PITOT HTR FAIL HTR FAIL PROT PITOT HEAT circuit breaker (affected side)....Check (DA-D, E4 & E5) PITOT/VANE HEAT (affected side)......Check - ON PITOT AMPS..............Check left and right AMPS to identify and verify failed heater (current below 6 AMPs).
Page 149: Windscreen Overheat
Hawker 850XP Pro Line 21 Airplane Flight Manual WINDSCREEN OVERHEAT L SCREEN R SCREEN and/or OVHT OVHT PROT SCREEN HEAT switch (affected side)....... OFF then ON The warning will extinguish when the switch is turned OFF, but may recur either immediately or subsequently when the switch is turned ON.
Page 150: Alternator Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual ALTERNATOR FAILURE ALTR 2 ALTR 1 FAIL FAIL PROT ALTERNATOR (affected side) ........OFF then ON Warning Persists: ALTERNATOR (affected side).........OFF NOTE: Both windscreens (A panels) will remain heated but both sidescreens (B panels) will be unheated.
Page 151: Afd Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual AVIONICS AFD FAILURE In the event of any failures, the airplane should be flown by the pilot who has the fully operational system, or the better system in the case of multiple failures.
Page 152: Single Ahrs Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual AVIONICS SYSTEMS (continued) Single AHRS Failure AHRS circuit breakers ..........Check (DA-A - E18, E19, F18 or F19) AHS reversion switch ..........Select operative AHRS • The autopilot and yaw damper will disconnect and will no longer function.
Page 153: Single Audio System Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual AVIONICS SYSTEMS (continued) Single Audio System Failure Audio switch (affected side) ........EMERG Audio volume control is provided through the other crewmember’s audio panel. Dual Audio System Failure No in flight action. Only Comm 1 audio is available through the headset. The boom microphone must be used as the hand microphone will be inoperative.
Page 154: Radio Equipment Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual AVIONICS SYSTEMS (continued) Radio Equipment Failure If power failure to individual radio system components is observed or suspected, power may be regained by operation of the PE, PS 1 and/or PS 2 Avionics Master Bypass switches, located on the DA-A circuit breaker panel, behind the copilot.
Page 155: Comparators
Hawker 850XP Pro Line 21 Airplane Flight Manual COMPARATORS Miscompare Annunciators Miscompare annunciators are displayed on the PFD to alert the pilots that redundant data from dual systems is not agreeing within limits. Attitude, heading, altitude and airspeed data are monitored full time.
Page 156: Loc
Hawker 850XP Pro Line 21 Airplane Flight Manual COMPARATORS (continued) This annunciation indicates a mismatch between the pilot’s and copilot’s displayed localizer data. Determine correct NAV source and select as necessary. If unable to determine the correct source, proceed visually if able or execute a missed approach.
Page 157: No Compare Annunciators
Hawker 850XP Pro Line 21 Airplane Flight Manual COMPARATORS (continued) No Compare Annunciators No Compare annunciators are displayed on the PFD when compared parameters are valid, but no valid data is being received from a second source allowing the comparators to function.
Page 158: Egpws Caution
Hawker 850XP Pro Line 21 Airplane Flight Manual EGPWS CAUTION (GND PROX CAUTION ANNUNCIATION and/or ACTIVATION OF SINK RATE, or DON’T SINK, or TOO LOW FLAPS, or TOO LOW GEAR, or TOO LOW TERRAIN, or GLIDESLOPE, or CAUTION, TERRAIN or CAUTION, OBSTACLE AURAL ALERT) SINK RATE..............
Page 159: Egpws Mode Failure
Hawker 850XP Pro Line 21 Airplane Flight Manual EGPWS MODE FAILURE (GPWS, WS or TERR) OR TERRAIN FAIL MESSAGE GPWS................ One or more of the basic GPWS modes (1-6) are inoperative and some or all of the aural alerts and visual warnings and cautions may not be provided.
Page 160: Entry Door Unlocked
Hawker 850XP Pro Line 21 Airplane Flight Manual MISCELLANEOUS ENTRY DOOR UNLOCKED ENT DOOR UNLOCKED WARNING: DO NOT ATTEMPT TO CHECK THE SECURITY OF THE CABIN ENTRY DOOR DURING FLIGHT. REMAIN AS FAR FROM THE DOOR AS POSSIBLE WITH SEAT BELTS SECURELY FASTENED.
Page 161 Airplane Flight Manual SUB-SECTION 4.10 NORMAL PROCEDURES Table of Contents Page Figure 4.10.1 - RECOMMENDED WALK-AROUND PATTERN ....2 GROUND HANDLING CHECKLIST..............3 EXTERNAL CHECKS ..................3 BEFORE START CHECKS................4 START CHECKS....................7 AFTER START CHECKS..................8 BEFORE TAKE-OFF CHECKS.................8 LINE UP CHECKS ....................9 AFTER TAKE-OFF CHECKS................9 CLIMB CHECKS ....................9 CRUISE CHECKS.....................9...
Page 162 Airplane Flight Manual RECOMMENDED WALK-AROUND PATTERN START VIEW VIEW M9410_0.A NOTE: Dashed lines indicate check areas underneath the airplane. Figure 4.10.1 Page 2 Sub-section - 4.10 FAA Approved NORMAL PROCEDURES Revision A3: Apr 26, 2007 For Training Purposes Only...
Page 163: Ground Handling Checklist
Airplane Flight Manual GROUND HANDLING CHECKLIST A stand-alone Ground Handling Checklist, containing the Pre-Flight and Post Flight Checks and Procedures, is issued to each airplane replacing the Pre-Flight and Post Flight Inspections in the Airplane Flexible Maintenance Schedule (AFMS). The Pre-Flight Check must be accomplished prior to or concurrent with the External Checks.
Page 164: Before Start Checks
Airplane Flight Manual BEFORE START CHECKS NOTE: Throughout these Normal Procedures where an APU operation is required, refer to the APU Supplement located in Section 7 - SUPPLEMENTS. Cabin................Check Cabin overwing emergency exit locking pin ....Check removed and stowed REFUEL switches ............
Page 165 Airplane Flight Manual BEFORE START CHECKS (continued) Abort Conditions • NO LIGHT-OFF WITHIN 10 SECONDS OF OPENING THE HP COCK. • ITT RAPIDLY APPROACHES 978° C. • IDLE RPM (APPROXIMATELY 27% N WITH 48-67% N ) NOT REACHED BY 50 SECONDS AFTER LIGHT-OFF. •...
Page 166 Airplane Flight Manual BEFORE START CHECKS (continued) CABIN HIGH DATUM ..........As required EGPWS switches............Deselected MWS ................TEST - DIM OVRD to NORM AHRS Mode (L & R) ............ NORM Transfer switches (L & R)..........Extinguished AUX HYD SYSTEM handle ......... Fully in DUMP VALVE ..............
Page 167: Start Checks
Airplane Flight Manual START CHECKS Brakes................PARK BEACON..............On ENG CMPTRs..............AUTO Fuel pumps ..............ON START PWR ..............Push PWR ON - light illuminates NOTE: During start, there may be a slow or erratic indication of fuel flow. CAUTION: VERIFY N ROTOR ROTATION PRIOR TO PLACING THE HP COCK TO ON. CHECK THE OPERATING ANNUNCIATOR EXTINGUISHES AT APPROXIMATELY 45% N RPM.
Page 168: After Start Checks
Airplane Flight Manual AFTER START CHECKS START PWR ..............Off EXT PWR (if used) ............Disconnect and OFF Generators 1 & 2 ............Check on line APU GEN (if APU installed)......... TRIP Volts and Amps............Check NOTE: If APU is installed and air is being used for air conditioning, the MAIN AIR VLVs 1 &...
Page 169: Line Up Checks
Airplane Flight Manual LINE UP CHECKS EXTERIOR LIGHTS ........... As required Transponders ............... Check TCAS ................TA/RA Flight controls .............. Full and free movement ANTICE and ENG IGNITION........As required MWS ................Check FATS ................Check - FLAPS, Airbrakes, Trims and V SPEEDS.
Page 170: Cabin Altitude Setting For Landing
Airplane Flight Manual CABIN ALTITUDE SETTING FOR LANDING (Apply setting correction to field pressure altitude) 1000 QNH - mb or HPa 28.64 28.79 28.94 29.09 29.23 29.38 29.53 in Hg +1500 +1350 +1250 +1100 +950 +800 +650 Correction - ft 1005 1010 1015...
Page 171 Instructions regarding erroneous EGPWS announcements during approach or landing. FILING INSTRUCTIONS: Insert this Temporary Change into the Hawker 850XP FAA Approved Airplane Flight Manual to face page 11 in Sub-Section 4.10 (Normal Procedures Section). Discard and rescind this Temporary Change upon implementation of the appropriate corrective software for the EGPWS system.
Page 172: Approach Checks
Airplane Flight Manual APPROACH CHECKS Altimeters..............Set and checked F/DK VLV ..............CLOSE EXTERIOR LIGHTS ............ As required Cabin notices ............... On Seats and harnesses........... Secure Nosewheel steering ............. Handwheel clear Fuel................Check quantity and balance NOTE: When set through the FMS, V is automatically set at V +10.
Page 173: After Landing Checks
Airplane Flight Manual AFTER LANDING CHECKS AIR BRAKES ...............SHUT FLAPS................Up Exterior lights ...............As required PITOT/VANE HEAT L & R ..........OFF ANTICE................As required APR................Disarm Transponder ..............STANDBY WARNING: DO NOT USE RADAR IN THE VICINITY OF GROUND PERSONNEL. A HAZARDOUS AREA EXTENDS UP TO 2 FEET IN FRONT OF THE RADAR DISH.
Page 174 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE EFFECTIVITY: All Hawker 850XP serial numbers DESCRIPTION OF CHANGE: Changed "EMERG LIGHTS" to read "EMERG lights". Revised the ENG CMPTR steps in the SHUT DOWN CHECKS and LEAVING AIRPLANE (TERMINATING FLIGHT) CHECKS in Sub-section 4.10 - NORMAL PROCEDURES.
Page 175: Leaving Airplane (Terminating Flight) Checks
TEMPORARY CHANGE P/N 140-590035-0005TC8 SECTION 4 - ABNORMAL/NORMAL PROCEDURES Sub-section 4.10 - NORMAL PROCEDURES LEAVING AIRPLANE (TERMINATING FLIGHT) CHECKS If the LEAVING AIRPLANE (TERMINATING FLIGHT) CHECKS are completed, the EXTERNAL CHECKS should be completed before the next flight. With APU (if installed) Only Running With No.
Page 176 Airplane Flight Manual LEAVING AIRPLANE (TERMINATING FLIGHT) CHECKS If the LEAVING AIRPLANE (TERMINATING FLIGHT) CHECKS are completed, the EXTERNAL CHECKS should be completed before the next flight. With APU (if installed) Only Running With No. 2 Engine Only Running RADIO 1 & 2 Masters ....OFF RADIO 1 &...
Page 177: Egpws Pre-Flight Checks
Airplane Flight Manual EGPWS PRE-FLIGHT CHECKS Pilot’s & Copilot’s PFDs and MFDs ......Terrain enabled NOTES: 1. Prior to initiating the self test, make sure PS1, PS2, PE, XS 1, XS 2 and XE busses are powered. 2. Aural volume during the test is approximately 6dB lower than the actual volume during a warning.
Page 178: Tcas Checks
Airplane Flight Manual EGPWS PRE-FLIGHT CHECKS (continued) (p) The aural "TERRAIN TERRAIN PULL UP" message is announced. (q) The red PULL UP message is removed from the PFDs. (r) The GND PROX message is displayed momentarily on the PFDs. (s) The Terrain Display Self Test Pattern turns off after several sweeps of the terrain display. (t) The TERR TEST message is removed from the MFDs and PFDs.
Page 179 Airplane Flight Manual TCAS CHECKS (continued) 5. Resolution Advisories (RA) are inhibited below 1100 ft AGL in a climb and 900 ft AGL in a descent, (a TA ONLY message will be presented under these conditions). Increased climb RAs are inhibited with FLAPS DN. 6.
Page 180 Airplane Flight Manual TCAS CHECKS (continued) 9. A Go-Around procedure should be executed if a CLIMB RA is issued with the airplane in a landing configuration. Certain climb RAs are inhibited with the FLAPS fully extended. By reconfiguring the airplane, the TCAS will have greater flexibility in resolving any conflict. Care has been taken to make sure of airplane capability to comply with issued RAs under most normal circumstances.
Page 181: Cat Ii Checks
Airplane Flight Manual CAT II CHECKS Approach Checks (Before Localizer Capture) Reversion/sensor switches...........Normal/Green Active NAV Source ............LOC 1 (pilot) - LOC 2 (copilot) Localizer Frequency (both) ..........Select and identify Localizer course (both) ..........Set DH (both) ..............Set to Radio Altitude When Ready To Capture Localizer Flight Guidance............Arm APP Autopilot ...............Engaged When Ready To Capture Glideslope...
Page 182: Takeoff And Landing At Airfields Above 9000 Ft Field Pressure Altitude
Airplane Flight Manual TAKEOFF and LANDING at AIRFIELDS ABOVE 9000 ft FIELD PRESSURE ALTITUDE BEFORE START CHECKS CABIN HI DATUM ..........Select DUMP VALVE ...........Check - SHUT GROUND PRESS TEST VALVE ......Check - NORMAL FLIGHT position MANUAL CABIN ALTITUDE CONTROL ..Check - Full DECREASE position F/DK VLV ............CLOSE FLOOD .............CLOSE FAN ..............As required...
Page 183 Airplane Flight Manual TAKEOFF and LANDING at AIRFIELDS ABOVE 9000 ft FIELD PRESSURE ALTITUDE (continued) When Established In The Climb CABIN CONTROLLER ........Set the ACFT ALT to cruise altitude + 2000 ft. RATE knob............Set desired rate of descent not to exceed 300 ft/minute.
Page 184 Airplane Flight Manual TAKEOFF and LANDING at AIRFIELDS ABOVE 9000 ft FIELD PRESSURE ALTITUDE (continued) Prior to 250 ft AGL: MAIN AIR VLVs 1 & 2 ..........CLOSE F/DK VLV ..............CLOSE NOTE: If necessary, open the Dump Valve slowly, so as to make sure zero differential pressure prior to touchdown.
Page 185 Hawker 850XP Pro Line 21 Airplane Flight Manual SECTION 5 PERFORMANCE PERFORMANCE IS PRESENTED IN THIS SECTION FOR CONDITIONS WHICH MAY EXCEED APPROVED LIMITATIONS. ALWAYS CONSULT SECTION - 2 FOR AIRPLANE LIMITATIONS. This Section is divided into the following Sub-sections: 5.05 ..........General...
Page 186 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Section - 5 FAA Approved Page 2 Original Issue: Feb 28, 2006 PERFORMANCE For Training Purposes Only...
Page 187 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.05 GENERAL Table of Contents Page INTRODUCTION....................5 Standard Condition of Airplane ..............5 Procedures and Information ................ 5 Performance....................5 CONFIGURATION ..................... 6 Normal Take-off Thrust ................6 Maximum (APR) Thrust................6 Figure 5.05.1 - TAKE- OFF REFERENCE N...
Page 188 Hawker 850XP Pro Line 21 Airplane Flight Manual Page Paved Runway/Hard Runway ..............14 Wet Runway ....................15 Climb Gradient ..................15 FLIGHT IN ICING CONDITIONS ..............15 WIND COMPONENT/CROSSWIND ..............15 Operation In High Surface Winds.............. 15 Maximum Demonstrated Crosswind ............15 Critical Engine ...................
Page 189 Hawker 850XP Pro Line 21 Airplane Flight Manual Page Figure 5.05.11A - STATIC POSITION ERROR CORRECTION TO ALTIMETER 29000 FEET AND ABOVE ......27 Figure 5.05.12 - STATIC POSITION ERROR CORRECTION TO ESIS ALTITUDE............28 Figure 5.05.13 - CORRECTION TO INDICATED MACH NUMBER ........29 Figure 5.05.14 - CORRECTION TO...
Page 190 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Sub-section - 5.05 Page 4 FAA Approved Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 191: Introduction
Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION This Sub-section contains performance information necessary for operation in compliance with applicable performance requirements, data required by applicable noise regulations and other information essential for implementing special operational requirements. Standard Condition of Airplane...
Page 192: Configuration
Hawker 850XP Pro Line 21 Airplane Flight Manual CONFIGURATION Normal Take-off Thrust Normal take-off thrust is verified by the fan RPM (N ) and is set with thrust levers fully 1 REF forward. Refer to Figures 5.05.1 and 5.05.2. The target value of N...
Page 193 Hawker 850XP Pro Line 21 Airplane Flight Manual TAKE-OFF REFERENCE N APR ARMED CABIN AIR OFF (Part 1 of 2: -50° C to 0° C) ENG ANTICE OFF (NOT OPERATING) Outside Air Temperature° C ALTITUDE ALTITUDE 15,000 98.7 99.8 100.0 100.0...
Page 194 Hawker 850XP Pro Line 21 Airplane Flight Manual TAKE-OFF REFERENCE N TAKE-OFF REFERENCE N APR ARMED CABIN AIR OFF (NOT OPERATING) ENG ANTICE OFF (Part 2 of 2: 0° C to 50° C) (Part 2 of 2: 0 C to 50 Outside Air Temperature°...
Page 195: Cabin Air Off - Engine Antice On
Hawker 850XP Pro Line 21 Airplane Flight Manual APR ARMED TAKE-OFF REFERENCE N CABIN AIR OFF ENG ANTICE ON (NOT OPERATING) Outside Air Temperature° C ALTITUDE ALTITUDE 15,000 15,000 98.7 99.8 100.0 100.0 100.0 100.0 100.0 100.0 99.7 99.0 98.3 97.6...
Page 196: Maximum Continuous Thrust
Hawker 850XP Pro Line 21 Airplane Flight Manual Maximum Continuous Thrust Maximum continuous thrust is defined by fan RPM (compensated N ), and is scheduled by altitude and air temperature. APR must be disarmed. Refer to Figures 5.05.3 and 5.05.4.
Page 197: En-Route Reference N
SYNCH ~ AS REQUIRED MAXIMUM CONTINUOUS CABIN AIR ~ ON THRUST RATING Hawker 850XP Pro Line 21 Airplane Flight Manual ENG ANTICE ~ OFF EN-ROUTE REFERENCE N TEMPERATURE (T )° C ALTITUDE ALTITUDE 41,000 98.25 99.45 100.0 100.0 99.4 98.15 97.25 96.4...
Page 198: En-Route Reference N
SYNCH ~ AS REQUIRED MAXIMUM CONTINUOUS CABIN AIR ~ ON Hawker 850XP Pro Line 21 Airplane Flight Manual THRUST RATING ENG ANTICE ~ ON EN-ROUTE REFERENCE N ° ALTITUDE TEMPERATURE (T ALTITUDE 41,000 98.25 97.1 96.15 96.82 97.5 96.65 95.7 94.9...
Page 199: Air Conditioning
Hawker 850XP Pro Line 21 Airplane Flight Manual Air Conditioning Engine bleed air for air conditioning is not to be used during takeoff at maximum or normal take- off thrust. Engine Intake Ice Protection Engine intake ice protection bleeds are to be selected OFF unless accounting for performance loss in accordance with the information in this Sub-section.
Page 200: Definitions
Hawker 850XP Pro Line 21 Airplane Flight Manual DEFINITIONS Some of the terms which are used in several sections of this manual are defined in Section 1. Those terms which are used mainly in the Performance Section are defined as follows.
Page 201: Wet Runway
Hawker 850XP Pro Line 21 Airplane Flight Manual Wet Runway A runway is considered as wet when it is well soaked but without significant areas of standing water. A runway is considered well soaked when there is sufficient moisture on the runway surface to cause it to appear reflective.
Page 202 Hawker 850XP Pro Line 21 Airplane Flight Manual WIND COMPONENT Figure 5.05.5 Sub-section - 5.05 Page 16 FAA Approved Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 203: Stalls
Hawker 850XP Pro Line 21 Airplane Flight Manual STALLS Power-off stall speeds, in terms of Indicated Air Speed (IAS), are given for various configurations in Figure 5.05.6. These airspeeds apply to an altitude of 15,000 feet and are the stall identification speeds at forward CG and therefore differ from the values shown in Sub-section 5.10 Figure 5.10.4 which are based on the minimum airspeed obtained during the stall.
Page 204: Maneuvering At High Altitudes
Hawker 850XP Pro Line 21 Airplane Flight Manual MANEUVERING AT HIGH ALTITUDES Figure 5.05.7 defines for a given Mach number and Altitude the cruising weight at which the maximum demonstrated buffet level will be reached in a 1.5g maneuver or at which buffet onset will be reached in a 1.3g maneuver, whichever occurs first.
Page 205: Noise Certification
Hawker 850XP Pro Line 21 Airplane Flight Manual NOISE CERTIFICATION General The Hawker 800XP, powered by TFE731-5BR-1H engines, has demonstrated compliance with the Appendix C noise certification requirements of CFR Part 36 (Amendment 36-20) which are equivalent to those of ICAO, Annex 16, Volume 1, Chapter 3. The certificated noise levels at the maximum certificated take-off and landing weights of 28,000 lb (12,701 kg) and 23,350 lb (10,591 kg) respectively are below the Stage 3 limits of CFR 36 as shown below.
Page 206 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.05.8 Sub-section - 5.05 Page 20 FAA Approved Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 207: Associated Conditions
Hawker 850XP Pro Line 21 Airplane Flight Manual Associated Conditions Engines Both engines operating Air conditioning bleed on; see NOTE 1 for the effect of engine Engine Bleed Air antice bleed. Flaps 0° or 15° (See NOTE 2) Landing Gear...
Page 208: Position And Compressibility Error Correction To Airspeed Indicator
Hawker 850XP Pro Line 21 Airplane Flight Manual Position and Compressibility Error Correction to Airspeed Indicator The position and compressibility error correction to be made to IAS to obtain EAS is shown in Figure 5.05.9 for varying flap settings. Position and Compressibility Error Correction to ESIS Airspeed The residual position error correction to the IAS shown on the ESIS is given in Figure 5.05.10 for...
Page 209 Hawker 850XP Pro Line 21 Airplane Flight Manual AIRSPEED CORRECTION TAKE-OFF GROUND ROLL ° FLAPS UP AND 15 4000 8000 12000 INDICATED AIRSPEED FIELD PRESSURE ALTITUDE AIR TEMPERATURE ~ KNOTS IAS ~ FEET ~ ° C M7525_0 Figure 5.05.8A FAA Approved Sub-section - 5.05...
Page 210 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.05.9 Sub-section - 5.05 Page 24 FAA Approved Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 211 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.05.10 FAA Approved Sub-section - 5.05 Page 25 Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 212 Hawker 850XP Pro Line 21 Airplane Flight Manual STATIC POSITION ERROR CORRECTION TO ALTIMETER BELOW 29000 FEET NOTE: This chart not applicable at FLAPS UP NOTE: This chart not applicable at 29,000 ft 29000 feet and above. and above. For altitudes of 29,000 ft BELOW 29000 FEET and above, see Figure 5.05.11A.
Page 213 Hawker 850XP Pro Line 21 Airplane Flight Manual STATIC POSITION ERROR CORRECTION TO ALTIMETER 29000 FEET AND ABOVE STATIC POSITION ERROR CORRECTION TO ALTIMETER FLAPS UP 29000 FEET AND ABOVE -100 SPEED ~ KNOTS IAS Figure 5.05.11A FAA Approved Sub-section - 5.05...
Page 214 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.05.12 Sub-section - 5.05 Page 28 FAA Approved Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 215 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.05.13 FAA Approved Sub-section - 5.05 Page 29 Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 216 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.05.14 Sub-section - 5.05 Page 30 FAA Approved Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 217 Hawker 850XP Pro Line 21 Airplane Flight Manual CONVERSION FACTORS Parameter To Convert Factor Multiply by 9, divide by 5, °C to °F add 32 Temperature Subtract 32, multiply by 5, °F to °C divide by 9 Kilograms (kg) to Pounds (lb) Divide by 0.45359...
Page 218 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.05.15 Sub-section - 5.05 Page 32 FAA Approved Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 219 Hawker 850XP Pro Line 21 Airplane Flight Manual ISA TEMPERATURES Figure 5.05.16 FAA Approved Sub-section - 5.05 Page 33 Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 220 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.05.17 Sub-section - 5.05 Page 34 FAA Approved Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 221 Hawker 850XP Pro Line 21 Airplane Flight Manual METERS - FEET CONVERSION 1 Foot = 0.3048 Meters 1 Meter = 3.2808 Feet FEET METERS Figure 5.05.18 FAA Approved Sub-section - 5.05 Page 35 Original Issue: Feb 28, 2006 GENERAL For Training Purposes Only...
Page 222 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.10 OPERATING SPEEDS Table of Contents Page INTRODUCTION....................3 DEFINITIONS ....................3 INSTRUCTIONS FOR USE OF CHARTS ............4 To Determine V and V ..............4 To Determine Final Take-Off Climb Speed (V )........4 To Determine En-Route Climb Speed (V ) ..........4...
Page 223 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Sub-section - 5.10 FAA Approved Page 2 OPERATING SPEEDS Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 224: Introduction
Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION This Sub-section provides the operating speeds relevant to the certified performance of the airplane. DEFINITIONS The minimum control speed after an engine failure on the ground during a continued takeoff with flaps 15° or 0° ranges from 87.5 KIAS to 113 KIAS, depending on temperature, altitude and weight conditions.
Page 225: To Determine Landing Reference Speed
Hawker 850XP Pro Line 21 Airplane Flight Manual INSTRUCTIONS FOR USE OF CHARTS To Determine V and V Speeds • Refer to TABULATED TAKEOFF DATA Sub-section 5.20. To Determine Final Take-Off Climb Speed (V • Enter Figure 5.10.1 with the airplane weight.
Page 226 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.10.1 FAA Approved Sub-section - 5.10 Page 5 Original Issue: Feb 28, 2006 OPERATING SPEEDS For Training Purposes Only...
Page 227 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.10.2 Sub-section - 5.10 FAA Approved Page 6 OPERATING SPEEDS Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 228 Hawker 850XP Pro Line 21 Airplane Flight Manual Sub-section - 5.10 FAA Approved Page 7 Figure 5.10.3 Original Issue: Feb 28, 2006 OPERATING SPEEDS For Training Purposes Only...
Page 229 Hawker 850XP Pro Line 21 Airplane Flight Manual POWER OFF STALLING SPEEDS M6293_0 HA00D 012836AA.AI Figure 5.10.4 Page 8 Sub-section - 5.10 FAA Approved OPERATING SPEEDS Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 230 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.15 TAKE-OFF WAT DATA Table of Contents Page INTRODUCTION....................2 INSTRUCTIONS FOR USE OF CHARTS............2 To Determine the WAT Limit Required ............2 Figure 5.15.1 - MAXIMUM TAKE-OFF WEIGHT FOR ALTITUDE AND TEMPERATURE, FLAPS 15°......
Page 231 Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION This Sub-section contains weight, altitude and temperature (WAT) data which limit the take-off weight of the airplane from a consideration of airworthiness climb requirements and tire speed limitations. The climb performance upon which the curves are based is given in Sub-section 5.55.
Page 232 Hawker 850XP Pro Line 21 Airplane Flight Manual MAXIMUM TAKE-OFF WEIGHT FOR ALTITUDE AND TEMPERATURE MAXIMUM CERTIFICATED TAKE-OFF WEIGHT is stated in Section 2. With engine antice in use, add 10 C to the actual air temperature before entering the graph.
Page 233 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Sub-section - 5.15 FAA Approved Page 4 Original Issue: Feb 28, 2006 TAKE-OFF WAT DATA For Training Purposes Only...
Page 234 Hawker 850XP Pro Line 21 Airplane Flight Manual MAXIMUM TAKE-OFF WEIGHT FOR ALTITUDE AND TEMPERATURE M6296_0 HA00D 012839AA.AI Figure 5.15.2 FAA Approved Sub-section - 5.15 Page 5 Original Issue: Feb 28, 2006 TAKE-OFF WAT DATA For Training Purposes Only...
Page 235 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Sub-section - 5.15 FAA Approved Page 6 Original Issue: Feb 28, 2006 TAKE-OFF WAT DATA For Training Purposes Only...
Page 236 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.20 TAKE-OFF FIELD LENGTH - APR ON Table of Contents Page INTRODUCTION ....................3 INSTRUCTIONS FOR USE OF TABLES AND CHARTS ........3 Associated Conditions..................4 Rolling Start Takeoffs ..................4 FLAPS 15°...
Page 237 Hawker 850XP Pro Line 21 Airplane Flight Manual Page FLAPS 0° Figure 5.20.18 Flaps 0° Maximum Take-Off Weight Limited by Maximum Brake Energy - Flaps 0° ........23 Figure 5.20.19 Flaps 0° - Field Pressure Altitude - Sea Level ....25 Figure 5.20.20 Flaps 0°...
Page 238 Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION This Sub-section provides tabulated take-off data along with graphs to correct for the effects of runway gradient and wind. The maximum take-off weight at a particular airfield may be restricted by some other performance criteria, such as the WAT limit, the net take-off flight path or en-route terrain clearance requirements.
Page 239 Hawker 850XP Pro Line 21 Airplane Flight Manual Associated Conditions The performance is based on the following assumptions: Both engines are at take-off thrust with APR armed. Engines Failure of the critical engine occurs at V Air conditioning bleed off; see NOTE 1 for the effect of Engine Bleed Air engine antice bleed.
Page 240 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (Sea Level) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS 28,000 lb VR ~ KIAS 12,701 kg V2 ~ KIAS TOFL ~ FT 4365 4426 4488...
Page 241 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (1000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS 28,000 lb VR ~ KIAS V2 ~ KIAS 12,701 kg TOFL ~ FT 4520 4585 4648...
Page 242 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (2000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS 28,000 lb VR ~ KIAS 12,701 kg V2 ~ KIAS TOFL ~ FT 4683 4742 4811...
Page 243 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (3000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS VR ~ KIAS 28,000 lb V2 ~ KIAS 12,701 kg TOFL ~ FT 4833 4907 4985...
Page 244 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (4000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS VR ~ KIAS 28,000 lb V2 ~ KIAS 12,701 kg TOFL ~ FT 4999 5089 5173...
Page 245 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (5000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS VR ~ KIAS 28,000 lb V2 ~ KIAS 12,701 kg TOFL ~ FT 5176 5284 5370...
Page 246 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (6000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS 28,000 lb VR ~ KIAS V2 ~ KIAS 12,701 kg TOFL ~ FT 5280 5407 5530...
Page 247 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (7000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS VR ~ KIAS 28,000 lb V2 ~ KIAS 12,701 kg TOFL ~ FT 5291 5488 5700...
Page 248 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (8000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS VR ~ KIAS 28,000 lb V2 ~ KIAS 12,701 kg TOFL ~ FT 5568 5808 6051...
Page 249 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (9000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS VR ~ KIAS 28,000 lb V2 ~ KIAS 12,701 kg TOFL ~ FT 6008 6239 6502...
Page 250 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (10,000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS 28,000 lb VR ~ KIAS V2 ~ KIAS 12,701 kg TOFL ~ FT 6470 6729 7031...
Page 251 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (11,000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS VR ~ KIAS 28,000 lb V2 ~ KIAS 12,701 kg TOFL ~ FT 6999 7286 7601...
Page 252 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (12,000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS 28,000 lb VR ~ KIAS V2 ~ KIAS 12,701 kg TOFL ~ FT 7656 7965 V1 ~ KIAS...
Page 253 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (13,000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS VR ~ KIAS 28,000 lb V2 ~ KIAS 12,701 kg TOFL ~ FT V1 ~ KIAS...
Page 254 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 15 Field Pressure Altitude (14,000 feet) OUTSIDE AIR TEMPERATURE ~ T.O. WEIGHT V1 ~ KIAS 28,000 lb VR ~ KIAS V2 ~ KIAS 12,701 kg TOFL ~ FT V1 ~ KIAS...
Page 255 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Page 20 Sub-section - 5.20 FAA Approved TAKE OFF FIELD LENGTH - APR ON Original Issue: , 2006 Feb 28 For Training Purposes Only...
Page 256 Hawker 850XP Pro Line 21 Airplane Flight Manual TAKE-OFF FIELD LENGTH CORRECTION FLAPS 15º 4000 13000 13000 12000 12000 3500 11000 11000 10000 10000 3000 9000 9000 2500 8000 8000 7000 7000 2000 6000 6000 5000 5000 1500 4000 4000...
Page 257 Hawker 850XP Pro Line 21 Airplane Flight Manual TAKE-OFF DECISION SPEED ( V ) CORRECTION FLAPS 15º DOWNHILL UPHILL REPORTED WIND COMPONENT RUNWAY SLOPE ~ % ~ knots M7530_0 Figure 5.20.17 Page 22 Sub-section - 5.20 FAA Approved TAKE OFF FIELD LENGTH - APR ON...
Page 258 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.20.18 FAA Approved Sub-section - 5.20 Page 23 Original Issue: Feb 28 , 2006 TAKE-OFF FIELD LENGTH - APR ON For Training Purposes Only...
Page 259 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Page 24 Sub-section - 5.20 FAA approved TAKE-OFF FIELD LENGTH - APR ON Original: Feb 28 , 2006 For Training Purposes Only...
Page 260 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (Sea Level) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 4656 4720 4789 4864 4942 5022 5104 5188 5281 5377 5457 5647 6095...
Page 261 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (1000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 4835 4901 4975 5051 5133 5218 5304 5390 5487 5580 5722 6097 6624...
Page 262 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (2000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 5022 5086 5163 5246 5332 5420 5511 5603 5705 5821 6152 6631 7207...
Page 263 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (3000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 5199 5278 5362 5450 5541 5636 5731 5833 5947 6251 6705 7214 7834...
Page 264 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (4000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 5391 5490 5581 5677 5777 5868 5963 6085 6377 6811 7302 7850 9328...
Page 265 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (5000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 5599 5714 5809 5926 6010 6097 6233 6536 6955 7434 7955 8926 11923...
Page 266 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (6000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 5732 5872 6004 6140 6252 6434 6748 7144 7595 8111 8814 11208 16270...
Page 267 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (7000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 5756 5975 6206 6449 6695 7015 7368 7800 8288 8971 11142 15367 V1 ~ KIAS...
Page 268 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (8000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 6067 6332 6637 6969 7303 7665 8048 8518 9165 11187 14763 V1 ~ KIAS...
Page 269 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (9000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 6584 6898 7248 7614 7987 8380 8792 9876 11887 14988 V1 ~ KIAS...
Page 270 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (10,000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 7216 7556 7937 8332 8737 9285 10716 12526 15422 V1 ~ KIAS VR ~ KIAS...
Page 271 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (11,000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 7916 8286 8694 9126 10176 11800 13911 V1 ~ KIAS VR ~ KIAS...
Page 272 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (12,000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 8771 9177 9871 11451 13267 16132 V1 ~ KIAS VR ~ KIAS V2 ~ KIAS...
Page 273 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (13,000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 9801 11246 12989 15531 V1 ~ KIAS VR ~ KIAS V2 ~ KIAS...
Page 274 Hawker 850XP Pro Line 21 Airplane Flight Manual Flaps 0° Field Pressure Altitude (14,000 feet) V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT 12782 14942 V1 ~ KIAS VR ~ KIAS V2 ~ KIAS TOFL ~ FT...
Page 275 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Page 40 Sub-section - 5.20 FAA approved TAKE-OFF FIELD LENGTH - APR ON Original Issue: Feb 28 , 2006 For Training Purposes Only...
Page 276 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.20.34 Sub-section - 5.20 FAA Approved Page 41 Original Issue: , 2006 Feb 28 TAKE-OFF FIELD LENGTH - APR ON For Training Purposes Only...
Page 277 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.20.35 Sub-section - 5.20 FAA Approved Page 42 TAKE-OFF FIELD LENGTH - APR ON Original Issue: , 2006 Feb 28 For Training Purposes Only...
Page 278 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.25 NET TAKE-OFF FLIGHT PATH - APR ON Table of Contents Page INTRODUCTION ....................3 DEFINITIONS.....................3 Reference Zero....................3 Minute Point..................3 Five Minute Point ..................3 First Segment ....................3 Second Segment ..................3 Third Segment .....................4 Fourth Segment ...................4...
Page 279 Hawker 800XP Pro Line 21 Airplane Flight Manual Page NET TAKE-OFF FLIGHT PATH SECOND, THIRD AND FOURTH SEGMENTS - FLAPS 0° ..................15 Associated Conditions................. 15 Instructions for Use of Chart ............... 15 NET TAKE-OFF FLIGHT PATH FIFTH SEGMENT NET ACCELERATION DISTANCE........16 Associated Conditions.................16 Instructions for Use of Chart ...............16 Figure 5.25.6 - FIFTH SEGMENT NET...
Page 280 Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION The charts in this Sub-section are provided to enable a complete net take-off flight path to be constructed, should it be necessary to establish that any obstacles along the intended line of flight will be cleared by the safety margin required by the relevant operating regulations.
Page 281 Hawker 850XP Pro Line 21 Airplane Flight Manual Third Segment During this segment the airplane accelerates in level flight from V to final take-off climb speed on maximum thrust. The height may be 1500 feet or some lower height. If take-off was with flaps 15°, flaps are selected up at V...
Page 282 Hawker 850XP Pro Line 21 Airplane Flight Manual ILLUSTRATED EXAMPLES Figure 5.25.1 shows two examples of the use of the flight path charts. A further example where only the second segment needs to be considered is also provided. Example 1 Flaps 0°...
Page 283 Hawker 850XP Pro Line 21 Airplane Flight Manual Using Figure 5.25.5, this example comes in the area where acceleration takes place at 1500 feet and the Horizontal Distance from Reference Zero: • To 1500 feet is 36,500 feet. • To achieve final take-off climb speed is 46,000 feet.
Page 284 Hawker 850XP Pro Line 21 Airplane Flight Manual NET FLIGHT PATH - EXAMPLES APR ON POINT WHERE FINAL TAKE-OFF 1500 feet 1500 feet CLIMB SPEED IS ACHIEVED 1600 1400 MINUTE POINT 1200 1000 POINT WHERE FINAL TAKE-OFF CLIMB SPEED IS ACHIEVED...
Page 285 Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH SECOND SEGMENT NET GRADIENT - FLAPS 15° Figure 5.25.2 shows the second segment net gradient of climb. Associated Conditions Engines One engine operating at maximum thrust with APR ON.
Page 286 TEMPORARY CHANGE P/N 140-590035-0005TC2 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE EFFECTIVITY: All Hawker 850XP airplanes. DESCRIPTION OF CHANGE: To provide a correction factor for turning climbs. Insert Temporary Change 2 into the Airplane Flight Manual FILING INSTRUCTIONS: Section 5 - PERFORMANCE as follows: Sub-section 5.25: NET TAKE-OFF FLIGHT PATH - APR ON...
Page 287 TEMPORARY CHANGE P/N 140-590035-0005TC2 P/N 140-590035-0005TC2 Page 2 of 12 Jun 2, 2009 For Training Purposes Only...
Page 288 Print on GREEN Paper Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH SECOND SEGMENT NET GRADIENT 8X041A APR-ON FLAPS 15 With engine antice in use, add 10 C to actual air temperature before entering the graph.
Page 289 Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH - SECOND, THIRD AND FOURTH SEGMENTS 8X042 DISTANCE FROM REFERENCE ZERO APR-ON FLAPS 15 (x1000) REF.LINE With engine antice in use, add 10 C to actual air temperature before entering the graph.
Page 290: Net Take-Off Flight Path Second, Third And Fourth
Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH SECOND, THIRD AND FOURTH SEGMENTS - FLAPS 15° Figure 5.25.3 shows the distance from reference zero to the end of the second, third, and where appropriate fourth, segments of the flight path.
Page 291 Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH SECOND SEGMENT NET GRADIENT - FLAPS 0° Figure 5.25.4 shows the second segment net gradient of climb at the mean height of this segment. Associated Conditions Engines One engine operating at maximum thrust with APR ON.
Page 292 TEMPORARY CHANGE P/N 140-590035-0005TC2 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE EFFECTIVITY: All Hawker 850XP airplanes. DESCRIPTION OF CHANGE: To provide a correction factor for turning climbs. FILING INSTRUCTIONS: Insert Temporary Change 2 into the Airplane Flight Manual Section 5 - PERFORMANCE as follows: Sub-section 5.25: NET TAKE-OFF FLIGHT PATH - APR ON...
Page 293 TEMPORARY CHANGE P/N 140-590035-0005TC2 Intentionally left blank P/N 140-590035-0005TC2 Page 4 of 12 Jun 2, 2009 For Training Purposes Only...
Page 294 Hawker 850XP Pro Line 21 Airplane Flight Manual FAA Approved Sub-section - 5.25 Page 13 Original Issue: Feb 28, 2006 NET TAKE-OFF FLIGHT PATH Figure 5.25.4 For Training Purposes Only...
Page 295 Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH - SECOND, THIRD AND FOURTH SEGMENTS DISTANCE FROM REFERENCE ZERO APR-ON FLAPS 0 80 m (x 1000) With engine antice in use add 10 C REF. LINE to the actual air temperature before entering the graph.
Page 296 Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH SECOND, THIRD AND FOURTH SEGMENTS - FLAPS 0° Figure 5.25.5 shows the distance from reference zero to the end of the second, third, and where appropriate fourth, segments of the flight path.
Page 297: Net Take-Off Flight Path Fifth Segment Net Acceleration Distance
Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH FIFTH SEGMENT NET ACCELERATION DISTANCE Figure 5.25.6 shows the fifth segment net acceleration distance. Associated Conditions Engines One engine operating at maximum continuous thrust. Engine Bleed Air Air conditioning bleed off ; Antice off or on.
Page 298 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.25.6 FAA Approved Page 17 Sub-section - 5.25 Original Issue: Feb 28, 2006 NET TAKE-OFF FLIGHT PATH For Training Purposes Only...
Page 299: Net Take-Off Flight Path Radius Of Steady Turn
Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH RADIUS OF STEADY TURN The minimum radius which may be assumed for a steady turn made during the flight path is shown in Figure 5.25.7 for flaps 15° and 0°, for varying climb speed, air temperature and mean altitude.
Page 300 Hawker 850XP Pro Line 21 Airplane Flight Manual FAA Approved Sub-section - 5.25 Page 19 Original Issue: Feb 28, 2006 Figure 5.25.7 NET TAKE-OFF FLIGHT PATH For Training Purposes Only...
Page 301: Net Take-Off Flight Path Horizontal Distance Covered In A Steady Turn
Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH HORIZONTAL DISTANCE COVERED IN A STEADY TURN Figure 5.25.8 shows the horizontal distance travelled for a given radius of steady turn. Instructions for Use of Chart • Enter Figure 5.25.8 with the radius of steady turn. Proceed vertically to the appropriate change in heading.
Page 302 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.25.8 FAA Approved Page 21 Sub-section - 5.25 Original Issue: Feb 28, 2006 NET TAKE-OFF FLIGHT PATH For Training Purposes Only...
Page 303: Net Take-Off Flight Path Effect Of Wind During Steady Turn
Hawker 850XP Pro Line 21 Airplane Flight Manual NET TAKE-OFF FLIGHT PATH EFFECT OF WIND DURING STEADY TURN When a turn is included in the flight path there will be, in general a change in wind component. This may be accounted for by the method shown in Figure 5.25.9.
Page 304 Hawker 850XP Pro Line 21 Airplane Flight Manual Figure 5.25.9 FAA Approved Page 23 Sub-section - 5.25 Original Issue: Feb 28, 2006 NET TAKE-OFF FLIGHT PATH For Training Purposes Only...
Page 305 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.30 TAKE-OFF FIELD LENGTH DE-RATE This information is to be supplied at a later date. FAA Approved Page 1 Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 306 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.35 TAKE-OFF FLIGHT PATH DE-RATE This information is to be supplied at a later date. FAA Approved Page 1 Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 307 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.40 EN-ROUTE DATA Table of Contents Page INTRODUCTION....................2 EN-ROUTE NET GRADIENT OF CLIMB (ONE ENGINE INOPERATIVE) ..2 Associated Conditions ................2 Instructions for Use of Chart ............... 2 Figure 5.40.1 - EN-ROUTE NET GRADIENT OF CLIMB (ONE ENGINE INOPERATIVE) .........
Page 308 Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION This Sub-section contains data for use in ensuring compliance with the operating regulations relating to en-route flight. EN-ROUTE NET GRADIENT OF CLIMB (ONE ENGINE INOPERATIVE) The en-route net climb gradient with one engine inoperative is shown on Figure 5.40.1 for varying weight, altitude and air temperature.
Page 309 TEMPORARY CHANGE P/N 140-590035-0005TC2 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE EFFECTIVITY: All Hawker 850XP airplanes. DESCRIPTION OF CHANGE: To provide a correction factor for turning climbs. FILING INSTRUCTIONS: Insert Temporary Change 2 into the Airplane Flight Manual Section 5 - PERFORMANCE as follows: Sub-section 5.25: NET TAKE-OFF FLIGHT PATH - APR ON...
Page 310 TEMPORARY CHANGE P/N 140-590035-0005TC2 Intentionally left blank P/N 140-590035-0005TC2 Page 6 of 12 Jun 2, 2009 For Training Purposes Only...
Page 311 Hawker 850XP Pro Line 21 Airplane Flight Manual FAA Approved Sub-section - 5.40 Page 3 Figure 5.40.1 Original Issue:Feb 28, 2006 EN-ROUTE DATA For Training Purposes Only...
Page 312 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.45 LANDING WAT DATA Table of Contents Page INTRODUCTION....................2 MAXIMUM LANDING WEIGHT FOR ALTITUDE AND TEMPERATURE..2 Instructions For Use Of Chart............2 Figure 5.45.1 - MAXIMUM LANDING WEIGHT FOR ALTITUDE AND TEMPERATURE ......
Page 313 Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION This Sub-section contains curves of weights at which for varying altitude and temperature the Go-around and Approach Climb requirements of 14 CFR PART 25.119 and 25.121(d) respectively are complied with and at which the energy input to the wheel brakes during a normal landing is within the wheel brake normal capacity.
Page 314 Hawker 850XP Pro Line 21 Airplane Flight Manual MAXIMUM LANDING WEIGHT FOR ALTITUDE AND TEMPERATURE M6323_0 HA00D 012866AA.AI Figure 5.45.1 Sub-section - 5.45 FAA Approved Page 3 Original Issue: Feb 28, 2006 LANDING WAT DATA For Training Purposes Only...
Page 315 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.50 LANDING FIELD LENGTHS Table of Contents Page INTRODUCTION....................3 MAXIMUM LANDING WEIGHT FOR LANDING DISTANCE AVAILABLE ..3 Associated Conditions................3 Instructions for Use of Chart............... 4 Figure 5.50.1 - MAXIMUM LANDING WEIGHT FOR LANDING DISTANCE AVAILABLE, FLAPS 45 °...
Page 316 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Sub-section - 5.50 Page 2 FAA Approved LANDING FIELD LENGTHS Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 317: Introduction
Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION The maximum weight for landing distance available (dry runway factored landing distance) is given on Figure 5.50.1. The gross landing distance measured in performance tests is equal to 60% of that scheduled in Figure 5.50.1.
Page 318: Instructions For Use Of Chart
Hawker 850XP Pro Line 21 Airplane Flight Manual MAXIMUM LANDING WEIGHT FOR LANDING DISTANCE AVAILABLE (continued) Figure 5.50.3 gives the effect on landing distance of a very slippery surface having a braking coefficient of friction of 0.05, and is intended to cover the effect of icy surfaces and aquaplaning.
Page 319 Hawker 850XP Pro Line 21 Airplane Flight Manual Instructions for Use of Charts (continued) • Reduce the landing distance available to obtain an unfactored landing distance. (For a dry runway, 14 CFR PARTs require unfactored landing distance to be 60% of landing distance available, but there may be occasions when a lower standard of safety is acceptable to the operator and to the Airworthiness Authority).
Page 320 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Sub-section - 5.50 Page 6 FAA Approved LANDING FIELD LENGTHS Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 321 Hawker 850XP Pro Line 21 Airplane Flight Manual MAXIMUM LANDING WEIGHT FOR LANDING DISTANCE AVAILABLE FAA Approved Sub-section - 5.50 Page 7 Figure 5.50.1 Original Issue: Feb 28, 2006 LANDING FIELD LENGTHS For Training Purposes Only...
Page 322: Landing Distance
Hawker 850XP Pro Line 21 Airplane Flight Manual OPERATIONAL FACTOR ADJUSTMENTS LANDING DISTANCE Figure 5.50.2 Sub-section - 5.50 Page 8 FAA Approved Original Issue: Feb 28, 2006 LANDING FIELD LENGTHS For Training Purposes Only...
Page 323: Distance Available
Hawker 850XP Pro Line 21 Airplane Flight Manual EFFECT OF A SLIPPERY RUNWAY ON LANDING DISTANCE AVAILABLE M6336_0 HA00D Figure 5.50.3 014086AA Page 9 FAA Approved Sub-section - 5.50 Original Issue: Feb 28, 2006 LANDING FIELD LENGTHS For Training Purposes Only...
Page 324: Landing On Slippery Runway
Hawker 850XP Pro Line 21 Airplane Flight Manual WIND AND GRADIENT RESTRICTIONS LANDING ON SLIPPERY RUNWAY Figure 5.50.4 Sub-section - 5.50 Page 10 FAA Approved LANDING FIELD LENGTHS Original Issue: Feb 28, 2006 For Training Purposes Only...
Page 325 Hawker 850XP Pro Line 21 Airplane Flight Manual SUB-SECTION 5.55 GROSS PERFORMANCE Table of Contents Page INTRODUCTION....................3 FIRST AND SECOND SEGMENT CLIMB GRADIENT - FLAPS 15° ....4 Associated Conditions................. 4 Instructions for Use of Chart................ 4 Figure 5.55.1 - FIRST AND SECOND SEGMENT CLIMB GRADIENT (APR ON) FLAPS 15°......
Page 326 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank Page 2 Sub-section - 5.55 FAA Approved Original Issue: Feb 28, 2006 GROSS PERFORMANCE For Training Purposes Only...
Page 327 Hawker 850XP Pro Line 21 Airplane Flight Manual INTRODUCTION This Sub-section gives gross gradients of climb. Gross gradients for first and second segment and final take-off climb are the basis of the take- off WAT curves in Sub-section 5.15. Gross gradients for approach and go-around climbs in accordance with 14 CFR PART 25.121 (d) and 14 CFR PART 25.119 are the basis of the landing WAT curves in Sub-section 5.45.
Page 328 Hawker 850XP Pro Line 21 Airplane Flight Manual FIRST AND SECOND SEGMENT CLIMB GRADIENT - FLAPS 15° The gross gradient of climb for the first and second segments with flaps extended to 15° is shown on Figure 5.55.1 for varying weight, altitude and air temperature.
Page 329 TEMPORARY CHANGE P/N 140-590035-0005TC2 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE EFFECTIVITY: All Hawker 850XP airplanes. DESCRIPTION OF CHANGE: To provide a correction factor for turning climbs. Insert Temporary Change 2 into the Airplane Flight Manual FILING INSTRUCTIONS: Section 5 - PERFORMANCE as follows: Sub-section 5.25: NET TAKE-OFF FLIGHT PATH - APR ON...
Page 330 TEMPORARY CHANGE P/N 140-590035-0005TC2 Intentionally left blank P/N 140-590035-0005TC2 Page 8 of 12 Jun 2, 2009 For Training Purposes Only...
Page 331 Hawker 850XP Pro Line 21 Airplane Flight Manual FIRST AND SECOND SEGMENT CLIMB GRADIENT APR-ON FLAPS 15 M6326_0 HA00D 012869AA.AI FAA Approved Sub-section - 5.55 Original Issue: Feb 28 , 2006 GROSS PERFORMANCE Page 5 Figure 5.55.1 For Training Purposes Only...
Page 332 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank FAA Approved Page 6 Sub-section - 5.55 Original Issue: , 2006 Feb 28 GROSS PERFORMANCE For Training Purposes Only...
Page 333 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank FAA Approved Page 7 Sub-section - 5.55 Original Issue: Feb 28, 2006 GROSS PERFORMANCE For Training Purposes Only...
Page 334: Associated Conditions
Hawker 850XP Pro Line 21 Airplane Flight Manual FIRST AND SECOND SEGMENT CLIMB GRADIENT - FLAPS 0° The gross gradient of climb for the first and second segments with flaps retracted is shown on Figure 5.55.2 for varying weight, altitude and air temperature.
Page 335: Instructions For Use Of Chart
TEMPORARY CHANGE P/N 140-590035-0005TC2 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE EFFECTIVITY: All Hawker 850XP airplanes. DESCRIPTION OF CHANGE: To provide a correction factor for turning climbs. FILING INSTRUCTIONS: Insert Temporary Change 2 into the Airplane Flight Manual Section 5 - PERFORMANCE as follows: Sub-section 5.25: NET TAKE-OFF FLIGHT PATH - APR ON...
Page 336 TEMPORARY CHANGE P/N 140-590035-0005TC2 Intentionally left blank P/N 140-590035-0005TC2 Page 10 of 12 Jun 2, 2009 For Training Purposes Only...
Page 337 Hawker 850XP Pro Line 21 Airplane Flight Manual FAA Approved Sub-section - 5.55 Original Issue: Feb 28 , 2006 GROSS PERFORMANCE Page 9 Figure 5.55.2 For Training Purposes Only...
Page 338 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank FAA Approved Page 10 Sub-section - 5.55 Original Issue: , 2006 Feb 28 GROSS PERFORMANCE For Training Purposes Only...
Page 339 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank FAA Approved Page 11 Sub-section - 5.55 Original Issue: Feb 28, 2006 GROSS PERFORMANCE For Training Purposes Only...
Page 340: Associated Conditions
Hawker 850XP Pro Line 21 Airplane Flight Manual FINAL TAKE-OFF CLIMB GRADIENT The gross and net gradients of climb for the final take-off configuration are shown on Figure 5.55.3 for varying weight, altitude and air temperature. Associated Conditions One engine operating at maximum continuous thrust, the other engine Engines stopped.
Page 341: Instructions For Use Of Chart
TEMPORARY CHANGE P/N 140-590035-0005TC2 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005. AIRPLANE EFFECTIVITY: All Hawker 850XP airplanes. DESCRIPTION OF CHANGE: To provide a correction factor for turning climbs. FILING INSTRUCTIONS: Insert Temporary Change 2 into the Airplane Flight Manual Section 5 - PERFORMANCE as follows: Sub-section 5.25: NET TAKE-OFF FLIGHT PATH - APR ON...
Page 342 TEMPORARY CHANGE P/N 140-590035-0005TC2 Intentionally left blank P/N 140-590035-0005TC2 Page 12 of 12 Jun 2, 2009 For Training Purposes Only...
Page 343 Hawker 850XP Pro Line 21 Airplane Flight Manual FAA Approved Sub-section - 5.55 Original Issue: Feb 28 , 2006 GROSS PERFORMANCE Page 13 Figure 5.55.3 For Training Purposes Only...
Page 344 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank FAA Approved Page 14 Sub-section - 5.55 Original Issue: , 2006 Feb 28 GROSS PERFORMANCE For Training Purposes Only...
Page 345 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank FAA Approved Page 15 Sub-section - 5.55 Original Issue: Feb 28, 2006 GROSS PERFORMANCE For Training Purposes Only...
Page 346: Associated Conditions
Hawker 850XP Pro Line 21 Airplane Flight Manual APPROACH CLIMB GRADIENT The gross gradient of climb in the go-around configuration is shown on Figure 5.55.4 for varying weight, airfield altitude and air temperature. Associated Conditions One engine operating at maximum take-off thrust with APR OFF; the Engines other engine stopped.
Page 347 Hawker 850XP Pro Line 21 Airplane Flight Manual APPROACH CLIMB GRADIENT M6324_0 HA00D 012867AA.AI FAA Approved Sub-section - 5.55 Original Issue: Feb 28 , 2006 GROSS PERFORMANCE Page 17 Figure 5.55.4 For Training Purposes Only...
Page 348: Go-Around Climb Gradient
Hawker 850XP Pro Line 21 Airplane Flight Manual GO-AROUND CLIMB GRADIENT The gross gradient of climb for the go-around configuration is shown on Figure 5.55.5 for varying weight, field pressure altitude and air temperature. Associated Conditions Engines Both engines operating at maximum take-off thrust with APR OFF.
Page 349 Hawker 850XP Pro Line 21 Airplane Flight Manual GO-AROUND CLIMB GRADIENT GO AROUND CLIMB GRADIENT M6325_0 HA00D 012868AA.AI FAA Approved Sub-section - 5.55 Original Issue: Feb 28 , 2006 GROSS PERFORMANCE Page 19 Figure 5.55.5 For Training Purposes Only...
Page 350 Airplane Flight Manual SECTION - 6 WEIGHT & BALANCE Table of Contents Page PART 1 - AS CERTIFICATED................3 BASIC EMPTY WEIGHT and BALANCE - As Certificated ........ 3 WEIGHT and BALANCE TERMINOLOGY ............4 CONVERSION FACTORS................. 5 WEIGHT and CENTER of GRAVITY (CG) LIMITATIONS/DATA ...... 6 Center of Gravity (CG) Data ................
Page 351 Airplane Flight Manual NOTE: The "BASIC EMPTY WEIGHT and BALANCE - As Certificated", inserted Page 3, and the "EQUIPMENT LIST", at the end of PART 1 - AS CERTIFICATED, are not FAA Approved. These pages will be inserted into each Airplane Flight Manual Section 6 at the time of certification.
Page 352: Part 1 - As Certificated
Airplane Flight Manual PART 1 - AS CERTIFICATED BASIC EMPTY WEIGHT and BALANCE - As Certificated (Page 3 will be added with the airplane actual weight data) Page 3 FAA Approved Section - 6 Revision A3: Apr 26, 2007 WEIGHT & BALANCE For Training Purposes Only...
Page 353: Weight And Balance Terminology
Airplane Flight Manual WEIGHT and BALANCE TERMINOLOGY Approved Loading Envelope - Those combinations of airplane weight and center of gravity which define the limits beyond which loading is not approved. Arm - The distance from the center of gravity of an object to a line about which moments are to be computed.
Page 354: Conversion Factors
Airplane Flight Manual Standard Mean Chord (SMC) - The average distance from the wing leading edge to the trailing edge. Station - The longitudinal distance from some point to the zero datum or zero fuselage station. Take-off Weight - The weight of the airplane at lift-off from the runway. Tare - The apparent weight which may be indicated by scales before any load is applied.
Page 355 Airplane Flight Manual WEIGHT and CENTER of GRAVITY (CG) LIMITATIONS/DATA See Figures 6.1 and 6.2 for the Loading and Flight Envelope Weight Limitations lb (kg) Unless otherwise noted Maximum Ramp Weight........28,120 (12,755) Maximum Take-Off Weight........28,000 (12,701) Maximum Landing Weight (except in an emergency) ........
Page 356 Airplane Flight Manual Intentionally left blank Page 7 FAA Approved Section - 6 Revision A3: Apr 26, 2007 WEIGHT & BALANCE For Training Purposes Only...
Page 357 Airplane Flight Manual Center of Gravity (CG) Data NOTE: All CG values and calculations in this section are expressed in feet or meters from the CG datum. The CG Datum (0.000) is at fuselage station 353.04 inches or 8.967 meters, which is 11 feet or 3.353 meters forward of the Reference Point located on the aft fuselage, below the right engine pylon.
Page 358 Airplane Flight Manual LOADING and FLIGHT ENVELOPE - POUNDS/FEET PERCENT STANDARD MEAN CHORD (SMC) 29,000 MAXIMUM RAMP WEIGHT 28,120 lb MAXIMUM TAKE-OFF WEIGHT 28,000 lb 28,000 27,000 ZONE A 26,000 USABLE ONLY WITH VENTRAL TANK FUEL 25,000 24,000 MAXIMUM LANDING WEIGHT 23,350 lb 23,000 22,000 21,000...
Page 359 Airplane Flight Manual LOADING and FLIGHT ENVELOPE - KILOGRAMS/METERS PERCENT STANDARD MEAN CHORD (SMC) 12,900 MAXIMUM RAMP WEIGHT 12,755 kg MAXIMUM TAKE-OFF WEIGHT 12,701 kg 12,400 11,900 ZONE A USABLE ONLY WITH VENTRAL TANK FUEL 11,400 10,900 MAXIMUM LANDING WEIGHT 10,591 kg 10,400 9,900 9,400...
Page 360 Airplane Flight Manual FUSELAGE STATION LOCATING DIAGRAM Percent Standard Mean Chord FRAME SPACING IN INCHES REFERENCE POINT (RIGHT SIDE) 485.04 C. G. DATUM 353.04 FEET FROM C. G. DATUM NOTE: REFER TO CONVERSION FACTORS FOR METRIC EQUIVALENT. M9411_0.AI Figure 6.3 Page 11 FAA Approved Section - 6...
Page 361: Useful Load Data
Airplane Flight Manual USEFUL LOAD DATA Occupants Arm - ft (m ) Crew............... -17.05 (-5.197) Jump Seat Observer ..........-14.00 (-4.267) NOTE: See Part 2 for airplane serial number specific payload data. DENSITY VARIATION of AVIATION FUEL - POUNDS/U.S. GALLONS Figure 6.4 Section - 6 Page 12...
Page 362 Airplane Flight Manual DENSITY VARIATION of AVIATION FUEL - KILOGRAMS/LITERS Figure 6.5 Page 13 FAA Approved Section - 6 Revision A3: Apr 26, 2007 WEIGHT & BALANCE For Training Purposes Only...
Page 363: Usable Fuel - Pounds/U.s. Gallons
Airplane Flight Manual USABLE FUEL - POUNDS/U.S. GALLONS USEFUL LOAD DATA USABLE FUEL WING TANKS Table 1 - Pounds/US Gallons 6.40 lb/gal 6.66 lb/gal 6.90 lb/gal Note Gal. Weight Moment Weight Moment Weight Moment lb-ft lb-ft lb-ft -188 -196 -203 1024 -460 1066...
Page 364 Airplane Flight Manual 6.40 lb/gal 6.66 lb/gal 6.90 lb/gal Note Gal. Weight Moment Weight Moment Weight Moment lb-ft lb-ft lb-ft 1120 7168 2315 7459 2409 7728 2496 1160 7424 2957 7726 3077 8004 3188 1200 7680 3732 7992 3883 8280 4023 1240 7936...
Page 365: Usable Fuel - Kilograms/Liters
Airplane Flight Manual USABLE FUEL - KILOGRAMS/LITERS USEFUL LOAD DATA USABLE FUEL WING TANKS Table 2 - Kilograms/Liters 0.77 kg/L 0.80 kg/L 0.83 kg/L Note Liter Weight Moment Weight Moment Weight Moment kg-m kg-m kg-m -40.9 -42.5 -44.1 -71.3 -74.0 -76.8 -98.6 -102.5...
Page 366 Airplane Flight Manual 0.77 kg/L 0.80 kg/L 0.83 kg/L Note Liter Weight Moment Weight Moment Weight Moment kg-m kg-m kg-m 4100 3157 241.9 3280 251.4 3403 260.8 4250 3273 327.8 3400 340.5 3528 353.3 4400 3388 416.2 3520 432.4 3652 448.7 4550 3504...
Page 367: Unusable Fuel
Airplane Flight Manual UNUSABLE FUEL Weight Moment lb (kg) ft (m) lb-ft (kg-m) Drainable (See NOTE: below) With ventral tank installed 59 (26.76) -32 (-4.4) Without ventral tank installed 54 (24.49) -63 (-8.7) Trapped With or without 22 (9.98) -1.30 (-0.396) -29 (-4.0) ventral tank installed Total...
Page 368: General Weighing Instructions
Airplane Flight Manual GENERAL WEIGHING INSTRUCTIONS Periodic weighing of the airplane may be required to keep the Basic Empty Weight current, with the frequency of weighing determined by the operator. All changes to the airplane affecting weight and/or balance are the responsibility of the operator. Airplane weighing should be done in an enclosed, draft free hangar.
Page 369 Airplane Flight Manual Wheel Change Jack Weighing Place the airplane on the scales and place the jacks under the jacking points. Operate the jack(s) to level the airplane and record the scale readings. Be sure to subtract the weight of the jacks from the scale readings.
Page 370: Jack Point Weighing
Airplane Flight Manual AIRPLANE WEIGHING and REACTION POINTS C. G. DATUM REFERENCE POINT (RIGHT SIDE) 4.12 FT (1.256 M) 11.00 FT (3.353 M) 15.65 FT (4.770 M) MAIN JACK TAIL JACK POINT POINT Figure 6.6 JACK POINT WEIGHING M9465_0. C. G. DATUM REFERENCE POINT...
Page 371: Basic Empty Weight & Balance Form (Blank)
Airplane Flight Manual Model 850XP Basic Empty Weight & Balance Form Facility : Airplane Serial No: Scales : Date : Wheel Reaction Measurements (as applicable) Wheels C/L Actual Correction Corrected ft (m) ft (m) ft (m) Inboard Main Wheel C/L to Fuselage Reference 0.058 (0.018) Point Left Nose Wheel C/L to Inboard Main Wheel C/L...
Page 372 Airplane Flight Manual Equipment List - As Certificated Airplane Serial No.: Date: (same as inserted page 3 date) Total Weight Moment Item Qty. lb (kg) ft (m) lb-ft (kg-m) Engines - Allied Signal TFE 731-5BR 1,832.0 ( 830.99) 9.30 ( 2.83) 17,038 (2,355.6) Thrust Reversers 220.0 ( 99.79) 11.86 ( 3.61)
Page 373 Airplane Flight Manual Equipment List - As Certificated Airplane Serial No.: Date: (same as inserted page 3 date) Total Weight Moment Item Qty. lb (kg) ft (m) lb-ft (kg-m) Collins IFIS-5000 Proline 21 Avionics Air Data System ADC-3000 Air Data Computer 4.2 ( 1.91) -15.79 (-4.81) -66 (-9.2)
Page 374 Airplane Flight Manual Equipment List - As Certificated Airplane Serial No.: Date: (same as inserted page 3 date) Total Weight Moment Item Qty. lb (kg) ft (m) lb-ft (kg-m) EGPWS 965-0976 Computer 7.0 ( 3.18) -16.10 (-4.91) -113 (-15.6) Weather Radar RTA-858 Receiver/Transmitter/Antenna 21.5 ( 9.75) -22.92 (-6.99)
Page 375: Part 2 - Post Certificated
Airplane Flight Manual PART 2 - POST CERTIFICATED Page 1 FAA Approved Section - 6 Revision A3: Apr 26, 2007 WEIGHT & BALANCE For Training Purposes Only...
Page 376 Airplane Flight Manual PART 2 - POST CERTIFICATED (continued) Section - 6 Page 2 FAA Approved WEIGHT & BALANCE Revision A3: Apr 26, 2007 For Training Purposes Only...
Page 377 Hawker 850XP Pro Line 21 Airplane Flight Manual Weight and Balance Report This page will be replaced by the multi-page Weight and Balance Report, which is prepared on an individual airplane basis. Section - 6 Page 30 FAA Approved WEIGHT & BALANCE...
Page 378 Hawker 800XP configuration prior to the installation of Raytheon Aircraft Company Kit 140-1702 (modification to the 850XP configuration). Raytheon Aircraft Company has evaluated the Hawker 850XP configuration (including Airplane Flight Manual P/N 140-590035-0005) and found it to be compatible with the Hawker 800XP Airplane Flight Manual Supplements listed below.
Page 379 TEMPORARY CHANGE P/N 140-590035-0005TC3 PUBLICATION AFFECTED: FAA Approved Airplane Flight Manual, P/N 140-590035-0005, Dated February 28, 2006 or latest revision. AIRPLANE SERIAL NUMBERS AFFECTED: Only serial numbers with Raytheon Aircraft Company Kit 140- 1702 installed. DESCRIPTION OF CHANGE: Information for transferring 800XP STC supplements into the 850XP Airplane Flight Manual.
Page 380 Hawker 850XP Pro Line 21 Airplane Flight Manual SECTION - 7 SUPPLEMENTS When a new airplane is delivered from the factory, the Airplane Flight Manual delivered with it contains either a Supplemental Type Certificate (STC) supplement or a Raytheon Aircraft Company Type Certificate (TC) supplement for every installed item not covered by sections 1 through 6 of this Airplane Flight Manual.
Page 381 Hawker 850XP Pro Line 21 Airplane Flight Manual Intentionally left blank FAA Approved Section - 7 Page 2 Original Issue: Feb 28, 2006 SUPPLEMENTS For Training Purposes Only...
Page 382 FAA Approved Airplane Flight Manual LOG OF SUPPLEMENTS FAA Approved Airplane Flight Manual P/N 140-590035-0005 Serials 258750 thru 258788, 258795 and 258802 When Kit 140-1702 is Installed Serials 258789 thru 258794, 258796 thru 258801, 258803 and After December 23, 2010 All applicable FAA approved supplements for your airplane must be in the Airplane Flight Manual on board the airplane for all flights.
Page 383 FAA Approved Airplane Flight Manual Part Number Subject Date 140-590035-0053 Collins FMS-6000 FLIGHT MANAGEMENT SYSTEM Version 3.0.3 Nov 20, Only applicable to 850XP airplanes with winglets 2007 equipped with Collins FMS-6000 software version 3.0.3. 140-590035-0055 AIRPLANES EQUIPPED WITH A STANDBY Feb 28, INVERTER 2006...
Page 384 FAA Approved Airplane Flight Manual Part Number Subject Date 140-590035-0115 ROCKWELL COLLINS FMS-6000 FLIGHT MANAGEMENT SYSTEM Version 4.0 WAAS/ Nov 3, 2009 Only applicable to 850XP Airplane Serials 258789 thru 258794, 258796 thru 258801, 258803 and After with Kit 149-3432 installed. 43-8027-003 HONEYWELL DIGITAL ELECTRONIC ENGINE May 11,...
Page 385 FAA Approved Airplane Flight Manual Intentionally left blank Page 4 of 4 P/N 140-590035-0005LOS Dec 23, 2010 For Training Purposes Only...
Page 386 Pro Line 21 LOG OF APPENDIX TOPICS APPENDIX OF NON-FAA APPROVED DATA APPLICABLE TO FAA APPROVED AIPLANE FLIGHT MANUAL P/N 140-590035-0005 Serials 258750 thru 258788, 258795 and 258802 When Kit No. 140-1702 is Installed Serials 258789 thru 258794, 258796 thru 258801, 258803 and After February 28, 2006 All topics of information contained in this Appendix are not FAA approved and do not replace or supersede data found in the FAA approved sections of this manual.
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Hawker Beechcraft Hawker 850XP Flight Manual

Section 1 General

Section 2 Limitations

Section 3 Emergency Procedures

Engines

Air Conditioning & Pressurization

Electrical

Fire or Smoke

Landing Gear

Wheel Brakes

Avionics

Ditching

Emergency Evacuation

Sub-Section 4.05 Abnormal Procedures

Sub-Section 4.10 Normal Procedures

Quick Links

Chapters

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Questions and answers

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Summary of Contents for Hawker Beechcraft Hawker 850XP