Hawker Checklist Thru Rev02 & TR03

BAe 125-800A

AVN FLIGHT CREW PROCEDURES CHECKLIST

NORMAL

EMERGENCY/ABNORMAL PERFORMANCE

APPLICABLE TO: N96-----------------------------------258134 N97-----------------------------------258154 N98-----------------------------------258156

AVN CFM through Change 02 MARCH, 1999 AVN CHECKLIST CHANGE 02 JULY, 2003 AVN CHECKLIST TEMP REV 01 JUNE, 2005 AVN CHECKLIST TEMP REV 02 OCTOBER, 2005 AVN CHECKLIST TEMP REV 03 JULY 2006

TI 4040.25 BAe 125-800A CHG 02, 07/03 AVN CHECKLIST

The AVN Flight Crew Procedures (abbreviated) checklist for FAA aircraft is condensed from the description Checklist contained in the Company Flight Manual (CFM). These procedures must be thoroughly understood to safely and effectively operate the aircraft.

Upon receipt of an Operations Alert Directive (OAD) affecting this Checklist, write the information in the appropriate section. Changes to the checklist will be distributed after each approved checklist change.

Checklist procedures may be accomplished by the “Do-Verify” method. The DV method consists of the checklist being accomplished in a variable sequence without a preliminary challenge. After all the action items on the checklist have been completed, the checklist is then read again while each item is verified. The Pilot-Not-Flying (PNF) shall read the checklist, or verify the checklist completion and will announce "________ Checklist Complete." Checklist complete must always be announced.

When the Before Landing Checklist Complete is not announced prior to crossing the runway threshold, a go around is mandatory.

If an item of the checklist is interrupted, that item of the checklist shall be verified or repeated.

In an emergency, FLY THE AIRCRAFT. The pilot flying (PF) does not perform tasks, which detract from, or compromise, the duty to maintain control of the aircraft. The PF will ensure that the emergency checklist immediate items are completed and the emergency checklist be called for and accomplished.

CHECKLIST SYMBOLS + Plus items are for through flight items.

* Asterisk items are for Battery start items.

Immediate Action items in bold print and bold boxed. list text represents pause point for radio communications and crew coordination.

DEFINITIONS These definitions of flight crew positions are used throughout the FAA Flight Inspection.

P-Pilot, PIC-Pilot-in-Command, SIC-Second-in-Command, LP-Left Pilot, RP-Right Pilot, PF-Pilot Flying, PNF-Pilot Not Flying ET-Electronic Technician Airborne.

Request for changes, corrections or recommendations for this procedures checklist should be submitted to the Director of Operations, AVN-200.

BAe 125-800A TI 4040.25 AVN CHECKLIST CHG 02, 07/2003

CONTROL PAGE Description Change No Date Cover 02 07/2003 Description 01 06/1999 Control Page 02 07/2003 List of Effective Pages 02 07/2003

NORMAL Description Change No Date All pages in this Section 01 06/1999 N –21 and Administrative 02 07/2003

EMERGENCY/ABNORMAL Description Change No Date E-i Thru E-iii, E-1 Thru E-13, E-15, E-17 Thru h E-19, E-21 Thru E-22, and E-24 Thru E-32

Original 03/97

E-iv, E-14, E-16, E-20, and E-23 01 06/99

PERFORMANCE Description Change No Date P-ii Thru P-iii, and P-1 Thru P-22 Original 03/97

P-i, P-iv, and P-23 Thru P-30 01 06/99

A

BAe 125-800A TI 4040.25.2 AVN CHECKLIST Temp Rev 03, July 2006

A

CONTROL PAGE Description Change No Date Cover TR 03 07/2006Description 01 06/1999Control Page TR 03 07/2006List of Effective Pages TR 03 07/2006

NORMAL Page No Change No Date All pages in this Section 01 06/1999N –21 and Administrative 02 07/2003N-16 TR 03 07/2006

EMERGENCY/ABNORMAL Page No Change No Date E-i Thru E-iii, E-1 Thru E-13, E-15, E-17 Thru h E-19, E-21 Thru E-22, and E-24 Thru E-32

Original 03/97

E-iv, E-14, E-16, E-20, and E-23 01 06/99

E-iii, E-8, E-10, and E-11 TR 01 06/2005E-iv, E-27 TR 02 10/2005

PERFORMANCE Page No Change No Date P-ii Thru P-iii, and P-1 Thru P-22 Original 03/97

P-i, P-iv, and P-23 Thru P-30 01 06/99


LIST OF EFFECTIVE PAGES Section Page

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Cover ........... 02 N-25............. 01 E-1 .......OriginalDescription... 01 N-26............. 01 E-2 .......OriginalControl Page 02 N-27............. 01 E-3 .......OriginalLOEP ........... 02 N-28............. 01 E-4 .......Original N-29............. 01 E-5 .......Original

NORMAL N-30............. 01 E-6 .......OriginalTable of Contents N-31............. 01 E-7 .......Original N-i .............. 02 N-32............. 01 E-8 .......Original N-ii ........... 02 N-33............. 01 E-9 .......OriginalN-1.............. 01 N-34............. 01 E-10 .....OriginalN-2.............. 01 N-35............. 01 E-11 .....OriginalN-3.............. 01 N-36............. 01 E-12 .....OriginalN-4.............. 01 N-37............. 01 E-13 .....OriginalN-5.............. 01 N-38............. 01 E-14 .....OriginalN-6.............. 01 N-39............. 01 E-15 .....OriginalN-7.............. 01 N-40............. 01 E-16 .............01N-8.............. 01 N-41............. 01 E-17 .....OriginalN-9.............. 01 N-42............. 01 E-18 .....OriginalN-10............ 01 N-43............. 01 E-19 .....OriginalN-11............ 01 N-44............. 01 E-20 .............01N-12............ 01 N-45............. 01 E-21 .....OriginalN-13............ 01 N-46............. 01 E-22 .....OriginalN-14............ 01 E-23 .............01N-15............ 01 E-24 .....OriginalN-16............ 01 Emergency/ E-25 ...Original N-17............ 01 Abnormal E-26 ...Original N-18............ 01 E-i ................ 01 E-27 ...Original N-19............ 01 E-ii ............... 01 E-28 ...Original N-20............ 01 E-29 ...Original N-21............ 02 Table of Contents E-30 ...Original N-22............ 01 E-iii............... 01 E-31 ...Original N-23............ 01 E-iv .............. 01 E-32 ...Original N-24............ 01

B

TI 4040.25.2 BAe 125-800A Temp Rev 03, July 2006 AVN CHECKLIST

B

LIST OF EFFECTIVE PAGES Section Page

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Cover.......... TR 03 N-25............. 01 E-1 .......OriginalDescription ....... 01 N-26............. 01 E-2 .......OriginalControl PageTR 03 N-27............. 01 E-3 .......OriginalLOEP.......... TR 03 N-28............. 01 E-4 .......Original N-29............. 01 E-5 .......Original

NORMAL N-30............. 01 E-6 .......OriginalTable of Contents N-31............. 01 E-7 .......Original N-i............ 02 N-32............. 01 E-8 ......... TR 01 N-ii ........... 02 N-33............. 01 E-9 .......OriginalN-1.............. 01 N-34............. 01 E-10 ....... TR 01N-2.............. 01 N-35............. 01 E-11 ....... TR 01N-3.............. 01 N-36............. 01 E-12 .....OriginalN-4.............. 01 N-37............. 01 E-13 .....OriginalN-5.............. 01 N-38............. 01 E-14 .....OriginalN-6.............. 01 N-39............. 01 E-15 .....OriginalN-7.............. 01 N-40............. 01 E-16 .............01N-8.............. 01 N-41............. 01 E-17 .....OriginalN-9.............. 01 N-42............. 01 E-18 .....OriginalN-10............ 01 N-43............. 01 E-19 .....OriginalN-11............ 01 N-44............. 01 E-20 .............01N-12............ 01 N-45............. 01 E-21 .....OriginalN-13............ 01 N-46............. 01 E-22 .....OriginalN-14............ 01 E-23 .............01N-15............ 01 E-24 .....OriginalN-16.......TR 03 Emergency/ E-25 ...Original N-17............ 01 Abnormal E-26 ...Original N-18............ 01 E-i ................ 01 E-27 ..... TR 02 N-19............ 01 E-ii ............... 01 E-28 ...Original N-20............ 01 E-29 ...Original N-21............ 02 Table of Contents E-30 ...Original N-22............ 01 E-iii......... TR 02 E-31 ...Original N-23............ 01 E-iv .............. 01 E-32 ...Original N-24............ 01


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Performance Table of Contents

P-i ...... Original P-iii..... Original P-iv .... Original

P-1......... Original P-2......... Original P-3......... Original P-4......... Original P-5......... Original P-6......... Original P-7......... Original P-8......... Original P-9......... Original P-10....... Original P-10....... Original P-11....... Original P-12....... Original P-13....... Original P-14....... Original P-15....... Original P-16....... Original P-17....... Original P-18....... Original P-19....... Original P-20....... Original P-21....... Original P-22....... Original P-23....... Original P-24....... Original P-25....... Original P-26....... Original P-27....... Original P-28....... Original P-29....... Original P-30....... Original


D

This Page Intentionally Left Blank

BAe 125-800A TI 4040.25 AVN CHECKLIST CHG 02, 07/2003 TABLE OF CONTENTS Page 6

NORMAL PROCEDURES Before Exterior Inspection .............................................N-1 Exterior Inspection.........................................................N-1 Cabin Inspection............................................................N-5 Before Starting Engines ................................................N-5 Starting Engines..........................................................N-10 Before Taxi..................................................................N-11 Taxi .............................................................................N-12 Before Takeoff.............................................................N-12 Lineup .........................................................................N-13 After Takeoff/Climb......................................................N-13 Cruise..........................................................................N-14 In Range/Descent........................................................N-15 Before Landing............................................................N-16 Traffic Pattern/Before Landing ....................................N-17 After Landing...............................................................N-19 Taxi Back ....................................................................N-20 Stopping Engines ........................................................N-20

EXPANDED NORMAL Weather Radar Check.................................................N-22 Nav and Radio Check .................................................N-23 EFD Check..................................................................N-28 Autopilot Check ...........................................................N-29 Overhead Test Panel Check .......................................N-31 Engine Starting Malfunctions.......................................N-33 APS-85 Autopilot Diagnostics .....................................N-35 Passenger Briefing ......................................................N-36 Takeoff Crew Briefing/Considerations .........................N-37 Instrument Approach Review ......................................N-38

N-i

TI 4040.25 BAe 125-800A CHG 02, 07/2003 AVN CHECKLIST TABLE OF CONTENTS Page 6

SCHEMATICS DC Power System - De-Energized Schematic ............N-39

AC Power System - Schematic ...................................N-40

DC Power Distribution - PE Bus Bar ...........................N-41

DC Power Distribution - PS1 Bus Bar .........................N-42

DC Power Distribution - PS2 Bus Bar .........................N-43

AC Power Distribution .................................................N-44

Refuel/De-fuel System Schematic...............................N-45

Hydraulic System Schematic.......................................N-46

N-ii


NORMAL PROCEDURES PREFLIGHT CHECKLIST Before Exterior Inspection

+ 1. Chocks ..............................................IN PLACE + 2. Rampguard (If Applicable)...............Check OFF + 3. Manuals & Documents ..........................CHECK 4. Fire Extinguisher Indicators and Switches (2) .............................Check OFF 5. Landing Gear Handle .............................DOWN 6. Override Gear Selector ..........................DOWN 7. Nose Gear Downlock Indicator.............VISIBLE 8. Aux Hyd System Selector...................... CYCLE Reset Fully IN + 9. Wheelbrake ............................................. PARK

Exterior Inspection Thru flight Inspection: complete all items. Fuselage Nose - Left Side 1. Airflow Angle Sensor Vane..........CHECK Movement 2. Pitot Probe ...................................REMOVE COVER Check 3. Static Vents (Upper/Lower) .......... REMOVE PLUGS Check 4. Air Temp Probe .............................................CHECK 5. Rotary Ice Detector ................................Rotor FREE 6. Nose Wheel Well..................... AUX HYD RES FULL No Leaks 7. Nose Gear Lock Pin ...................................REMOVE Stow 8. Nose Wheel Doors ..................................... SECURE

NORMAL N-1


9. Nose Steering Pin .........................................CHECK Vertical 10. Nose Strut .....................................................CHECK 11. Nose Tires & Wheels ....................................CHECK 12. Radome/Taxi Lights ................................... SECURE Check Fuselage Nose - Right Side 13. Static Vents(Upper/Lower) ............REMOVE PLUGS Check 14. Pitot Probe ................................... REMOVE COVER Check 15. Airflow Angle Sensor Vane ...........................CHECK Movement 16. Venturi Outlet ................................................CHECK 17. SAT/TAS Probe.............................................CHECK 18. Emergency Exit .............................................CHECK 19. Dorsal Air Intake..............................REMOVE PLUG Check Right Engine - Front of Wing 20. Intake ............................................................CHECK 21. P2T2 Sensor ..................................................CHECK 22. Fan Blades....................................................CHECK 23. Starter Generator Air Intake ..........................CHECK Right Wing 24. Wing Ice Inspection Light ..............................CHECK 25. Top Surface ..................................................CHECK 26. TKS Panels ...................................................CHECK 27. Landing & Taxi Lights....................................CHECK 28. Stall Vent.........................................REMOVE PLUG Check 29. Fuel Cap .................................................... SECURE 30. Vortex Generators.........................................CHECK 31. NAV & Strobe Lights .....................................CHECK

N-2 NORMAL


32. Undersurface.................................................CHECK 33. Vent Tank Intake ...........................................CHECK 34. Static Wicks...................................................CHECK 35. Aileron & Tab ................................................CHECK 36. Flaps .............................................................CHECK 37. Airbrakes .......................................................CHECK Right Main Gear 38. Fairing & Inboard Door ..................................CHECK 39. Wheel Well ....................................................CHECK 40. Main Gear Lock Pin....................................REMOVE Stow 41. Strut...............................................................CHECK 42. Tires & Wheels..............................................CHECK 43. Brake Lines ...................................................CHECK Fuel Tanks & Keel 44. Water Drain Valves .......................................CHECK 45. Anti-Collision Light ........................................CHECK 46. Antennas .......................................................CHECK Right Engine 47. Oil Level & Filter............................................CHECK 48. Drain Mast.....................................................CHECK 49. Cowling & Latches ..................................... SECURE 50. Rear Turbine Blades & Exhaust Section ............................................CHECK Rear Fuselage 51. Pressure Refuel Cap & Door...................... SECURE 52. Aux Cooling Pack Inlet & Exhaust .................CHECK 53. Ground Power Receptacle Door ................ SECURE 54. Oxygen Charging Panel Cover................... SECURE 55. Tail Cone.......................................................CHECK Latches Secure 56. Laser Alt Inlet, Exhaust & Optics...................CHECK 57. Anti-Collision Light ........................................CHECK 58. Vertical Stabilizer & Rudder ..........................CHECK

NORMAL N-3


59. Horizontal Stabilizer & Elevators ...................CHECK 60. Equipment Bay Door .................................. SECURE 61. Fire Extinguisher Indicators (3) .....................CHECK 62. Toilet Tank Drain Door ............................... SECURE Left Engine 63. Oil Level & Filter............................................CHECK 64. Drain Mast.....................................................CHECK 65. Rear Turbine Blades & Exhaust Section ............................................CHECK 66. Cowling & Latches ..................................... SECURE Left Main Gear 67. Fairing & Inboard Door..................................CHECK 68. Wheel Well ....................................................CHECK 69. Main Gear Lock Pin....................................REMOVE Stow 70. Strut ..............................................................CHECK 71. Tires & Wheels..............................................CHECK 72. Brake Lines ...................................................CHECK Left Wing 73. Airbrakes.......................................................CHECK 74. Flaps .............................................................CHECK 75. Aileron & Tab ................................................CHECK 76. Vent Tank Intake...........................................CHECK 77. Undersurface ................................................CHECK 78. NAV & Strobe Lights .....................................CHECK 79. Vortex Generators.........................................CHECK 80. Fuel Cap .................................................... SECURE 81. Stall Vent.........................................REMOVE PLUG Check 82. Landing & Taxi Lights....................................CHECK 83. TKS Panels ...................................................CHECK 84. Top Surface ..................................................CHECK 85. Wing Ice Inspection Light ..............................CHECK

N-4 NORMAL


Left Engine/Left Fuselage - Front of Wing 86. Intake ............................................................CHECK 87. P2T2 Sensor...................................................CHECK 88. Fan Blades ....................................................CHECK 89. Starter Generator Air Intake ..........................CHECK 90. Entrance Door ...............................................CHECK

Cabin Inspection Thruflight Inspection: complete (+) items only. 1. Aft Baggage Compartment and Door ....CHECK Secure 2. Lavatory ................................................CHECK 3. Cabin Windows .....................................CHECK for Cracks/Damage 4. Crew Seats & Tables ............................CHECK + 5. Emergency Exit ............CLOSED Pin Removed 6. Emergency & Survival Equipment.........CHECK 7. Cabin Fire Extinguisher .........................CHECK 8. First Aid Kit............................................CHECK 9. Galley....................................................CHECK + 10. Baggage & Cargo Areas .................... SECURE + 11. Refuel Panel Switches OFF Door Closed + 12. Circuit Breakers.....................................CHECK

BEFORE STARTING ENGINES + Thruflight Inspection: complete plus (+) items only. * Battery Start: complete asterisk (*) items following

the Starting Engines checklist and prior to the Taxi checklist.

** Double asterisk (**) items indicate an expanded description is found at the end of the checklist section.

NORMAL N-5


1. Battery Isolate ........................................ NORM + 2. External Power Switch ............................... OFF + 3. Battery (B1 & B2 23V min ; B3 23.5V; PS1 & PS2 0V)............................ON + 4. Bus Tie Open Annunciator ...........................ON + 5. Navigational Lights.......................................ON + 6. Landing Gear Indicators.................... 3 GREEN 7. Fuel Pumps (2) ...........................EMERG, OFF (23V MIN on PE) + 8. Fuel Quantity.........................................CHECK + 9. Oxygen............................... ON Quantity Check + 10. TKS Contents........................................CHECK For APU Power + 11. Engine No. 1 LP fuel cock............................ON + 12. Aux Cooling Pack....................................... OFF + 13. APU Bleed Air ............................................ OFF + 14. APU Master..................................................ON + 15. APU Fire Warning and Annunciators ....... TEST

and Check + 16. Fire Extinguisher Switch OFF

and Guard Secured + 17. APU....................................................... START + 18. Bus Tie.................................................. CLOSE Skip to Item 22 for APU Starts For EXT Ground Power or Battery Only Start + 19. EXT PWR.......................................... AS REQD + 20. External Battery Charge.................... AS REQD + 21. BATT CNTCTR Annunciators (2) ................ON + * 22. Inverters (3)..............................Check ARM/ON + * 23. APU Bleed Air & Aux Cooling Pack..................................... AS REQD

N-6 NORMAL


Left Side + * 24. Emergency Exit Lights ............................Check AUTO + 25. Oxygen Cabin Isolation Valve ...........AS REQD 26. Fire Extinguisher, Axe, Flashlight and Smoke Goggles..............................CHECK Stow + * 27. IRS .............................................................NAV 28. Oxygen Mask ............................. 100% CHECK 29. UHF Radio ...................................................ON 30. Audio Control Panel ................................... SET 31. HF Radio #1 ...............................................SBY + 32. Gust Lock & Aux Hyd Pump Handle ..REMOVE STOW Front Panels + 33. No.1 Clock.................................................. SET + 34. Flight Annunciators ..................................TEST + 35. Standby Instrument Emerg Power ...........TEST + 36. Standby Attitude Indicator .....................ERECT 37. ELT ......................................................... AUTO + * 38. ADS(2), EFD(2), MFD, AHRS(2) MSTRS .........................................ON + 39. Transfer Switches .................................CHECK + 40. Fuel Contents and Flowmeters................................. Check RESET + 41. MWS and DIM OVRD ..............................TEST + 42. GPWS Flap Warn OVRD Annunciator ............................................... OUT + * 43. Weather Radar ** ............................. STANDBY 44. Marker .......................................................... LO + * 45. FMS ................................................PROGRAM + * 46. Nav Radios **............................................. SET * 47. EFD (2) **.............................................CHECK

NORMAL N-7


48. XPNDR and ATNR Switches/Lights ...........OUT * 49. Avionics Lighting ............................... AS REQD + * 50. Autopilot & Yaw Damper ** ...................CHECK Disengage + * 51. IRS Heading...................................... AS REQD + * 52. Transponder Antenna ................................ ATC + * 53. FIS Power ........................................ AS REQD + * 54. 115VAC 60HZ................................... AS REQD 55. Lazer Altimeter........................................... OFF 56. Dump Valve ............................................ SHUT 57. Manual Trim ..........................................CHECK Movement 58. Electric Trim ..........................................CHECK Movement + 59. HP COCKs............................................ CLOSE + 60. LP COCKs .............................................. OPEN + 61. WG Fuel/X Feed/Transfer ......CLOSE Light Out + 62. AUX Fuel Transfer .................CLOSE Light Out + * 63. No. 2 Clock ................................................ SET + 64. Cabin Controller .............. ALTITUDE RATE Set + * 65. AHRS DG Annunciators (2) .......................OUT

Right Side + * 66. VHF #2....................................................... SET 67. Audio Control Panel ................................... SET + * 68. IFF (If Applicable)..................................CHECK Standby + * 69. Standby Gear Indicators (2) ................. GREEN 70. Pitot Isolation .....................................NORMAL 71. Pressurization ....................................NORMAL 72. Manual Control........................Full DECREASE

N-8 NORMAL


73. Oxygen Mask ............................. 100% CHECK + 74. HF Radio #2 ...............................................SBY 75. Goggles, Smoke Set

O2, Flashlight............................... Check STOW Glareshield * 76. Emergency & Storm Lights (L) .................TEST * 77. Lighting Controls (L)..........................AS REQD * 78. FD BARS, DEV & F/S Switches (L)...AS REQD * 79. GPWS ......................................................TEST + * 80. Display Select Panel (L) ....................AS REQD + * 81. Radar Altimeters (2) .......................TEST (100’) Set (1’) + * 82. Altitude Alerter..........................................TEST Set + * 83. Display Select Panel (R) ...................AS REQD * 84. F/S, DEV & FD BARS Switches (R) ..AS REQD * 85. Lighting Controls (R) .........................AS REQD * 86. Emergency & Storm Lights (R).................TEST Roof Panel + * 87. TEST Panel (**)........................................TEST Thruflight: only ENG FIRE tests required. 88. Alternators (2) ............................................OFF + 89. External Battery Charge.............................OFF + 90. External Power..................................AS REQD * 91. Cabin & Lav Lights Switch.................AS REQD * 92. TKS .................................... PRIME Check Flow 93. Ice Detector............................................. AUTO 94. Fuel Pumps (2)...........................................OFF Fuel LO Press Lights....................................ON 95. GEN Fail Annunciators (2) ...........................ON 96. No Smoking..................................................ON 97. Screen Heat (2) & Pitot Vane Heat (2) .......OFF

NORMAL N-9


98. Engine Anti-Ice (2) & Ignitions (2) .............. OFF 99. Engine Computers (2) ................................ OFF CMPTR Lights..............................................ON 100. ENG SYNC ...............................................OFF 101. Pack Valve .............................................. AUTO 102. Flood Valve ...................................... AS REQ’D 103. Pressn Valve........................................... AUTO 104. Cabin Temperature Control................Auto SET 105. Flt Deck & Main Air Valves................. CLOSED Main Air Valve Lights .................................OUT 106. Takeoff Data .................................COMPUTED Posted

STARTING ENGINES 1. Fasten Seat Belts Sign.........................ON RP 2. Seat Belts & Shoulder Harness............ON LP/RP 3. Wheelbrake................PARK HYDRAULIC LP Check 4. Aux Cooling Pack...............................OFF LP Recirc 5. NAV & Beacon Lights...........................ON LP 6. Engine Computers (2) ..................... AUTO LP Lights Out 7. Fuel Pumps (2) ....................................ON LP Lights Out 8. Start Power ..........................................ON LP 9. Engines 2 & 1................................ START LP 10. External Power (If Applicable) ............OFF RP Disconnect 11. Start Power ........................................OFF LP 12. APU Generator .................................TRIP RP 13. DC Power......................................CHECK RP 14. Alternators (2) ......................................ON LP Lights Out

N-10 NORMAL


15. Screen Heat (2)....................................ON LP 16. Pitot/Vane Heat (2)...............................ON LP Check 17. Eng Ignitions (2) & Anti-Ice (2) ..AS REQD LP

Set ICE DET to OVRD before taxiing in icing 18. FIS Power .................................AS REQD RP 19. TACAN 2 Tuning .......................AS REQD RP 20. Windows..................................... CLOSED LP/RP 21. Starting Engines Checklist .... COMPLETE RP

BEFORE TAXI 1. IRS .....................................................NAV LP 2. Altimeters ...........................................SET LP/RP Check 3. Chocks ....................................REMOVED LP 4. Entrance Door ............................ LOCKED RP Lights Out

Check CVR, FLT RCDR and ENT Door Unlocked Annunciators Out.

5. Exterior Lights ...........................AS REQD RP Do not use landing lights for taxi.

6. Taxi Area....................................... CLEAR LP/RP Do not move the aircraft until attitude and heading warnings have cleared.

7. Before Taxi Checklist ............ COMPLETE RP

NORMAL N-11


TAXI 1. Brakes...........................................CHECK LP/RP 2. Steering.........................................CHECK LP 3. Flaps .................................................. SET RP 4. Trims (3)............................................. SET RP 5. Flight Controls ...............................CHECK PF 6. Flight Instruments..........................CHECK LP/RP 7. Taxi Checklist........................ COMPLETE RP

Before Takeoff 1. Rudder Bias and Engine Computers ....................Check ON LP 2. Airbrakes......................................... SHUT LP 3. APR...............................................CHECK LP 4. Crew Brief ............................. COMPLETE PF 5. Nav/Radio/Flight Sys/FMS Equipment.......................................... SET LP/RP 6. Battery Charge.................. 20 AMPS MAX RP 7. Cockpit & Cabin ......................... SECURE RP/ET 8. Flight Deck & Main Air Valves (2) ................................CLOSE RP 9. APU Bleed Air ....................................OFF RP 10. APU Overspeed .................................OFF RP 11. Before Takeoff Checklist ....... COMPLETE RP

N-12 NORMAL


LINEUP 1. Weather Radar..........................AS REQD RP 2. Transponder/ IFF ...............................SET RP 3. Engine Ignitions (2) ...................AS REQD RP 4. Engine Anti-Ice (2) & TKS .........AS REQD RP 5. Exterior Lights ....................................SET RP 6. MWS ............................................ CHECK LP/RP 7. APR.............................................. ARMED RP 8. Lineup Checklist .................... COMPLETE RP

AFTER TAKEOFF/CLIMB If approaches are conducted within 15 minutes of takeoff, use Traffic Pattern/Before Landing checklist in lieu of After Takeoff/Climb, Cruise, and In Range/Descent checklists. 1. Gear .....................................................UP PM 2. Main Air Valves (2) ..........................OPEN PM 3. Yaw Damper ..............................ENGAGE PM 4. Flaps ....................................................UP PM 5. APR............................................. DISARM PM 6. Engine Ignitions (2) ...................AS REQD PM 7. Engine Anti-Ice (2) & TKS .........AS REQD PM 8. ENG SYNC ........................................SET PM 9. Landing Lights....................................OFF PM 10. Aux Cooling Pack......................AS REQD PM OFF/RECIRC above 9000 ft. 11. Fasten Seat Belts Sign..............AS REQD PM 12. Engine Instruments ...................... CHECK PM 13. Cabin Pressure ............................ CHECK RP 14. Altimeters (2)......................................SET PF/PM 15. Taxi Lights.......................... OFF at 18000' PM 16. Fuel Balance & Aux Transfer ....... CHECK PM 17. After Takeoff/Climb Checklist COMPLETE PM

NORMAL N-13


N-14 NORMAL

CRUISE 1. Altimeters ......................................CHECK PF/PNF 2. Cabin Pressure & Temp................CHECK RP 3. Engine Instruments .......................CHECK PNF 4. Exterior Lights .................................... SET PNF 5. Electrical Systems.........................CHECK PNF 6. Fuel Balance & Aux Transfer ........CHECK PNF 7. Cruise Checklist .................... COMPLETE PNF

NOTE Before entering and every hour thereafter.

MAXIMUM CRUISE N1(N1 - %; Indicated OAT - °C)

ENG ANTI-ICE OFF

Applicable at all flight speeds ENG Anti-ice ON:deduct 1% from values given

Monitor: N2 not more than 100% ITT not more than 908°C

FL

-40

-35

-30

-25

-20

-15

-10

-5

0

+5

+10

410 98.5 98.5 98.2 98.0 97.7 97.2 390 97.7 98.1 97.9 98.0 97.7 97.0 96.4 370 97.5 97.8 97.7 97.6 97.5 96.9 96.3 350 97.0 97.5 97.5 97.4 97.4 97.0 96.5 96.0 330 96.6 96.9 97.4 97.3 97.2 97.2 96.7 96.2 310 96.4 96.6 96.9 97.3 97.3 97.0 96.9 96.4 95.8 290 97.0 96.5 96.7 97.0 97.2 97.0 96.8 96.5 96.1 95.4 270 96.9 96.6 96.7 96.9 96.7 96.8 96.7 96.3 95.6 250 97.1 96.8 96.7 96.7 96.7 96.7 96.6 96.4 96.0 95.3230 97.1 96.9 96.7 96.7 96.8 96.6 96.4 96.0 95.3

Refer to the Performance Section for the above chart in its entirety.


IN RANGE - DESCENT 1. Main Air Valves (2)..................OPEN PM 2. Flight Deck Valve ..................CLOSE PM 3. Fasten Seat Belts Sign.................ON PM 4. Seat Belts & Shoulder Harness....ON PF/PM 5. ATIS/Landing Data...............OBTAIN PM Computed 6. Arrival Briefing............... COMPLETE PF 7. Nav, Radios, Display Select Panel ..........................................SET PF/PM 8. Ice Protection ....................AS REQD PF/PM 9. Cabin Altitude & Rate.................SET RP 10. WG Fuel/Xfeed/Transfer .......CLOSE PM 11. Altimeters ...................................SET PF/PM 12. Taxi Lights....................................ON PM at 18000ft 13. In Range/Descent Checklist .............. ...................................... COMPLETE PM

NORMAL N-15

TI 4040.25.2 BAe 125-800A Temp Rev 03, 07/13/06 AVN Checklist

BEFORE LANDING 1. Engine Ignitions (2) ................... AS REQD PF/PM 2. Engine Anti-Ice (2) & TKS ......... AS REQD PF/PM

...... COMPLETE PF 3. Approach Briefing & VREF Set 4. Nav, Radios, Display Select Panel.................................................. SET PF/PM 5. ILS Offset .................................. AS REQD PF/PM ILS Offset must be OFF for landing. 6. Altimeters ........................................... SET PF/PM 7. Airbrakes......................................... SHUT PF/PM 8. Flaps ....................................................15° PF/PM 9. ENG SYNC ........................................OFF PM 10. Cockpit & Cabin ......................... SECURE PM/ET 11. Nosewheel Steering ...................... CLEAR PF 12. Gear ............................ DOWN / 3 GREEN PM 13. Nosewheel Steering .............. CENTERED PF 14. Flaps ......................................... AS REQD PM 15. Landing Lights........................... AS REQD PM 16. Main Air Valves (2)..................... CLOSED PM 17. Autopilot & Yaw Damper ......DISENGAGE PF 18. Before Landing Checklist ...... COMPLETE PM

N-16 NORMAL


NORMAL N-17

TRAFFIC PATTERN - BEFORE LANDING If approaches/landings are conducted within 15 minutes of takeoff, use the Traffic Pattern-Before Landing checklist in lieu of After Takeoff/Climb, Cruise, and In Range/Descent checklists. 1. Gear .....................................................UP PNF 2. Main Air Valves (2) ....................AS REQD PNF 3. Yaw Damper ..............................ENGAGE PNF 4. Flaps .........................................AS REQD PNF 5. APR (If Applicable) ...................... DISARM PNF 6. Approach Briefing & VREF ...Complete SET PF 7. Flaps .................................................. 15� PNF 8. Nosewheel Steering ...................... CLEAR LP 9. Gear .............................DOWN, 3 GREEN PNF 10. Brakes .......................................... CHECK PF 11. Flaps .........................................AS REQD PNF 12. Landing Lights...........................AS REQD PNF 13. Main Air Valves (2) ........................CLOSE PNF 14. Autopilot & Yaw Damper ......DISENGAGE PF 15. TFS Pattern/Before Landing Cklist ..................................... COMPLETE PNF

PATTERN SPEEDS Flap Setting 0° 15° 25° 45° Min Maneuver Speed (kts) V+30 V+25 V+20 V+10THR Speed (still air) V+15 V+10 V+5 V

REFERENCE SPEED (VREF) Weight (lb x 1000) 17 18 19 20 21 22 23

VREF (Knots) 112 115 119 122 125 128 130


ABOVE MAXIMUM LANDING WEIGHTS REFERENCE SPEED (VREF)

Weight (lb x 1000) 24 25 26 27 28 VREF (Knots) 133 136 138 140 142

LANDING DISTANCE REQUIRED (Factored) ZERO WIND, ISA, DRY RUNWAY

Wt x 1000lbs

23.35

23.0

22.0

21.0

20.0

19.0

18.0

17.0

VREF IAS

131

130

128

125

122

119

115

112

AFLD Elev

C�/Feet

C�/Feet

C�/Feet

C�/Feet

Feet

Feet

Feet

Feet

6000 20/5300 27/5230 31/5070 35/4900 4740 4580 4400 4230

5000 30/5180 31/5120 35/4950 39/4790 4630 4470 4300 4130

4000 33/5060 34/5000 38/4840 41/4680 4520 4360 4200 4040

3000 37/4930 38/4880 41/4720 45/4570 4410 4260 4110 3950

2000 39/4810 41/4760 44/4610 4460 4310 4160 4010 3860

1000 42/4700 44/4650 47/4500 4350 4200 4060 3910 3770

SL 45/4600 46/4540 49/4400 4250 4100 3960 3820 3680

NOTES:

• The temperature shown in the above columns for the higher weights are the landing WAT limited temperatures for that weight and altitude. (Single engine, flap 15°.)

• Chart based on ISA. Add 3% for each 10°C above ISA.

• Flaps 25° -- Add 10%. • Flaps 0° -- Reduce landing distance available by

30% and compare to landing distance required above.

• Unfactored = dist x 0.6. (i.e., landing distance factored by 1.67)

• No lift dump--Recommend adding at least 250 feet. • No lift dump or airbrakes--Recommend increasing

distance by 35%.

N-18 NORMAL


NORMAL N-19

WIND CORRECTION Tailwind ZeroWind Headwind

10 Kt Distance 10 Kt 20 Kt 30 Kt 40 KtAdd ft Ft Subtract Ft 1000 5500 300 550 850 1100 950 5000 250 550 800 1050 900 4500 250 500 750 1000 800 4000 250 500 750 950 750 3500 250 450 700 900

AFTER LANDING

If both engines are to be shut down, accomplish the After Landing checklist. Otherwise, proceed to the Taxi Back checklist. 1. Exterior Lights ....................................SET RP

Landing lights, if used, should be turned off as soon as practical after landing.

2. Airbrakes ......................................... SHUT LP/RP Flaps ....................................................UP 3. Pitot/Vane Heat (2).............................OFF RP 4. Engine Anti-Ice (2) & TKS ..................OFF RP 5. Engine Ignitions (2) ............................OFF RP 6. Weather Radar...................................OFF RP 7. Transponder............................. STANDBY RP IFF......................................................OFF 8. Laser Altimeter ...................................OFF RP 9. APU...........................................AS REQD RP 10. After Landing Checklist ......... COMPLETE RP Proceed to Stopping Engines checklist.


TAXI BACK 1. Exterior Lights .................................... SET RP

Landing lights, if used, should be turned off as soon as practical after landing.

2. Engine Ignitions (2) ................... AS REQD RP 3. Engine Anti-Ice (2) & TKS ......... AS REQD RP 4. Weather Radar.......................... AS REQD RP 5. Transponder/ IFF ...................... AS REQD RP 6. Airbrakes......................................... SHUT LP 7. Flaps .................................................. SET RP 8. Trim.................................................... SET RP If one engine is shut down, proceed with Starting Engines checklist, then continue with this checklist. 9. Takeoff Data & Crew Briefing.................................. COMPLETE PF 10. Nav/Radio/Flight Sys/FMS Equipment.......................................... SET LP/RP 11. Flt Deck Valve & Main Air Valves (2)......................................CLOSE RP 12. Cockpit & Cabin ......................... SECURE RP/ET 13. Taxi Back Checklist............... COMPLETE RP Proceed to Lineup Checklist.

STOPPING ENGINES 1. Taxi Lights..........................................OFF RP 2. Parking Brake .................................... SET LP 3. IRS.....................................................OFF LP

CAUTION IRS Mode Select switch must be OFF for at least 10 seconds prior to turning off acft power or the IRU Backup Battery will discharge completely.

N-20 NORMAL


4. Screen Heat (2).................................... OFF RP 5. Alternators (2) ...................................... OFF RP 6. EFD(2), MFD, ADS(2), AHRS(2) MSTRS ................................. OFF RP 7. Nav/FMS Equipment ............................ OFF RP 8. FIS Power ....................................AS REQD RP/ET 9. HP COCKs (2)..................................CLOSE LP 10. Engine Computers (2) .......................... OFF RP 11. Fuel Pumps (2)..................................... OFF RP 12. GEN FAIL Annunciators (2).................... ON RP 13. No Smoking and Fasten Seat Belts Signs....................... OFF RP 14. Oxygen and Cabin Isolation Valves (2) .................... OFF LP 15. Flight Control Locks .....................AS REQD LP 16. Aux Cooling Pack................................. OFF RP 17. APU Bleed Air ...................................... OFF RP 18. APU Generator.................................... TRIP RP 19. APU.................................... Overspeed OFF RP 20. Inverters ............................................... OFF RP 21. Cabin Emergency Lights ...................... OFF RP 22. Radios .................................................. OFF LP/RP 23. Exterior Lights ...................................... OFF RP 24. Battery.................................................. OFF RP 25. Chocks ........................................ IN PLACE RP 26. Parking Brake....................................... OFF RP 27. CVR Circuit Breaker (B17 &18) ....................................AS REQ’D LP/RP

Pull the CVR Circuit Breaker when a reportable in-flight incident ensuring data is preserved for investigation. Make a logbook entry and verbally notify maintenance.

28. Stopping Engines Checklist ...COMPLETE RP

NORMAL N-21


EXPANDED NORMAL WEATHER RADAR CHECK

WARNING Do not turn the WXP-85 Weather Radar panel mode switch to any position except OFF, STBY, or TEST when the antenna will be directed toward ground personnel, nearby hangars or other large metal buildings, or other aircraft. Never operate the weather radar during fueling or de-fueling operations. If either MFD PWR or RDR buttons are OFF, the radar transmitter may still be transmitting. This can occur if the mode switch on the WXP control unit is in the WX, NORM or MAP position, and could possibly result in injury to ground personnel.

To test WXP-85 for operational considerations set control unit switches as follows: MODE selector to TEST. RANGE to 25 miles. GAIN

to MAX. TILT to +5°. STB button in (ON). Ensure MFD PWR is on and RDR mode selected.

Confirm correct test pattern (allow 60 seconds for this to appear):

1. Four distinct colors from apex to center of screen.

2. From lower center of display, nine distinct color bands extend outwards in the following order: Green, Yellow, Red (contour band cycling to black in a one to one ratio), Magenta, Red (contour band cycling to black in a one to one ratio), Yellow, Green, Black, Yellow (alert band located at outer perimeter of the display).

N-22 NORMAL


3. No noise present on the display (no more than six random dots).

4. Momentarily set mode selector to WX, then back to TEST.

Press and release HLD button before completion of test pattern. Confirm that test pattern freezes on display. Confirm HOLD and TEST display alternately in upper left of MFD display. Press and release HLD button. Confirm that test pattern returns to normal updating. Set MODE selector to WX. Confirm "WX" is annunciated in upper left of MFD display. Set RANGE to 10 mi. Confirm range mark annunciation is "5". Adjust TILT between +15° and -15°. Observe that close in ground clutter appears at lower settings and any local detectable weather appears at higher settings. Set MODE selector to STBY.NAV and RADIOS CHECK Tune and identify the desired NAVAIDs. If a more detailed check is required, complete the following tests.

NAV and RADIO CHECK Tune and identify the desired NAVAIDs. If a more detailed check is required, complete the following tests. General 1. TACAN (2)...................... Set ON/OFF Switch To ON TEST/ON/SBY Switch To SBY 2. V/UHF NAV (3).................... Set Mode Switch To TR 3 ATC Xpndr ......................Set Mode Switch To STBY 4 ADF...................................Set Mode Switch To ADF 5 VHF 1 Radio................Set OFF/TR/DF Switch to TR 6. UHF Radios (2) ...........Set Function Switch to BOTH

NORMAL N-23


TACAN Equipment (2) 1. Set both NAV 1 SELECT and NAV 2 SELECT to

TACAN. 2. Set DSP (2) switches as follows: BRG to VOR 1, VOR 2 FORMAT to ROSE CRS to VOR/LOC Course arrow to 000° 3. Set BDI Switches (4) to TACAN 1 & TACAN 2. 4 Set TEST/ON/SBY switch to TEST. 5. Check distance warning flags on BDI show for 3

seconds and are then replaced by 00.0, accompanied by identification tone in headset.

6. Both BDI pointers indicate 180° 7. With DSP CRS set to north, ND gives zero bearing

and deviation, and FROM indication. 8. Set TEST/ON/SBY switch to ON or SBY as required. VHF NAV Equipment (2) 1. Set both NAV 1 SELECT and NAV 2 SELECT to

VOR/LOC. 2. Set DSP (2) switches as follows: BRG to VOR 1, VOR 2 FORMAT to ROSE CRS to VOR/LOC Course arrow to 000° 3. Select BDI switches (4) to VOR 1 and VOR 2. 4. Select usable VOR/VOT frequency. 5. Depress and hold TEST button on VHF NAV

control unit and confirm the following: (a) Active and preset display brightness varies from

minimum to maximum. The preset frequency display shows 00, and active frequency display shows "----"

N-24 NORMAL


(b) Lateral deviation warning legends appear on PFD and ND. After approximately 3 seconds, the warning legends are removed, the lateral deviation bar centers and a TO indication appears. The BDI pointers indicate approximately 000° magnetic bearing.

(c) NAV 1 test only: marker annunciator symbols flash on left PFD. Airways marker annunciator symbol flashes on right PFD. MKR annunciators light on left and right instrument panels.

(d) Diagnostic legends appear in the control unit displays. After approximately 15 seconds, the lateral deviation warning legends appear. After approximately another 3 seconds, the system reverts to normal operation.

(e) Release TEST button. BDI DME’s briefly show all 8's.

6. Set each VHF NAV control unit mode switch to HLD and check appropriate HOLD annunciator lights on BDI's, and HLD annunciator lights on control unit.

7. The letter "H", in yellow, appears to the right of the DIST digits on the ND.

8. The freq digits of "held" station appear on preset display.

9. Select local localizer frequency. 10. Select course pointer under lubber line. 11. Depress and hold TEST button on the VHF NAV

control unit and confirm the following: (a) The LOC and GS warning legends are

displayed. (b) After approximately 3 seconds, the LOC and

GS warning legends are removed, the lateral deviation bar deflects right approximately 1/2 full scale, and the GS pointer deflects down approximately 1/2 full scale.

NORMAL N-25


(c) (NAV 1 test only): marker annunciator symbols appear in sequence, flashing, on left PFD. Airways marker annunciator symbol appears, flashing, on right PFD. MKR annunciators light on left and right instrument panels.

(d) After approximately 15 seconds, the LOC and GS warning legends reappear. After approximately another 3 seconds, the system reverts to normal operation.

(e) Release TEST button. BDI DME displays briefly, showing all 8’s.

FAR 91.171 VOR Equipment Check 1. Perform VHF NAV Equipment steps (a) through (d)

above. 2. If using one NAV system against the other: Center

each course arrow on the received radial (FROM bearing).

3. If using a VOT signal: Center each course arrow. This should occur at or

near 000°. 4. If using a Ground Receiver Checkpoint: Align the aircraft on the checkpoint and center each

course arrow. 5. Note the bearings received in (b), (c), or (d) above.

The difference must be within 4°. Enter the required data on the VOR Equipment Check form in the Aircraft Logbook.

ATC Transponder The TEST position of the selector knob is for ground use only. ADF Equipment 1. Set DSP switches (2) as follows: BRG to ADF FORMAT to ROSE 2. Select BDI switches (2) to ADF.

N-26 NORMAL


3. Select usable local frequency and set mode switch to TONE and check the following:

(a) 1 kHz tone is audible in headset. (b) Magenta cross ended bearing pointers on ND’s

and BDI single pointers indicate relative bearing of transmitting station.

NOTE If no ADF signal is received, the bearing pointers will park at 90°.

4. Set mode switch to ADF. Check ND and BDI pointers maintain relative bearing.

5. Press and hold ADF TEST button. Check the following:

(a) Active and preset brightness varies from minimum to maximum.

(b) ND bearing pointers and BDI pointers rotate 90� clockwise from previously valid positions.

(c) Diagnostic legends appear in the control unit displays.

6. Release TEST button. Check that pointers return to their previously valid positions.

7. Set ADF mode switch to ANT. Check that ND and BDI pointers park at 90° and a 1 kHz tone is audible in the headset.

8. Set ADF mode switch to ADF.

NORMAL N-27


EFD - CHECK 1. Right DPU switch ........................................... PRESS

White ALTN legend lights 2. Left EFIS GRND TEST .................................. PRESS

and HOLD

NOTE Note that 10° is added to current values of pitch and roll and 20° is added to heading, with a positive increment added to the pilot’s side.

3. Left and right PFD........................................... Check Yellow PIT and ROL comparator warnings flash. 4. Left and right ND............................................. Check Yellow HDG comparator warning flashes.

NOTE Note that after four seconds the attitude displays on the PFD and the MFD are removed from view and that all flags associated with the PFD and ND are in view.

5. Left EFIS GRND TEST .............................RELEASE Check altitude display normal, all comparator

warnings on. 6. CMPTR PTR (2)............................................ PRESS Check comparator warnings out. 7. Right DPU ALTN Switch ............................... PRESS White ALTN legend out. 8. Left DPU ALTN switch .................................. PRESS White ALTN legend lights. 9. Right EFIS GRND TEST ............................... PRESS and Hold Repeat test for copilot's EFIS ground test. Release.

Check altitude display normal, all comparator warnings on.

N-28 NORMAL


10. Both CMPTR PTR.........................................PRESS Check comparator warnings out. 11 Left DPU ALTN .............................................PRESS White ALTN legend out.

AUTOPILOT CHECK CAUTION

Autopilot shall not be used in flight if auto-trim is unserviceable. Do not permit autopilot to drive primary controls or elevator trim onto stops. The yaw damper must not be engaged for takeoff or landing. Yaw damper may be engaged after takeoff but must be disengaged before touchdown.

NOTE When power is applied to the autopilot system, an internal self-test cycle ensures proper operation of command limiters. Autopilot and yaw damper engagement is inhibited during this 30 second cycle.

1. Check full free movement of flight controls. 2. Centralize and hold flying controls. 3. Engage autopilot AP and YD levers. 4. Push control column forward and check nose up trim

wheel movement occurs in pulses and trim indicator moves to rear. Check AP TRIM EL indicator reading moves aft.

5. After a delay, check AP TRIM annunciators lit on both pilots’ panels and E legend displayed on PFD’s.

6. Pull control column back and check nose down trim wheel movement occurs in pulses and trim indicator moves forward. Check AP TRIM EL indicator moves forward.

7. Check AP TRIM annunciator and PFD E legends go out, then reappear after a short delay.

8. Center the control column.

NORMAL N-29


9. Rotate control column wheel slightly clockwise. Check AP TRIM AIL indicator reading moves counterclockwise.

10. After a short delay, check AP TRIM annunciator lit and A legend displayed on PFD’s.

11. Rotate control column wheel slightly counterclockwise. Check AP TRIM AIL indicator reading moves clockwise.

12. Check AP TRIM annunciator and PFD A legends go out and then reappear after a short delay

13. Center the control column. 14. With autopilot engaged. Check AP DISC buttons (2),

autopilot panel AP lever, and either No. 1 or No. 2 Stall Test button disengage the autopilot. Check AP annunciators flash and audio warning operates.

15. With only yaw damper engaged, check AP DISC button disengages yaw damper.

16. With autopilot engaged, press both GA buttons in turn, and check autopilot disengages, annunciators flash, audio warning operates, PFD FD bars command 12° nose up and wings level, and GA legend is displayed on PFD’s.

17. Confirm turn knob is centered.

N-30 NORMAL


OVERHEAD TEST PANEL CHECK NOTE

When preparing for a Battery Only Engine Start, not all tests can be completed on battery power. Ensure Engine Fire tests are accomplished, and perform remainder of the tests after engine start.

NOTE On Thruflight, only the ENG FIRE tests are required.

1. Press No 1 Stall Test button. Check stick shaker motors operate and IDNT 1 and MWS Stall IDENT annunciators light after a 4 to 5 second delay. Release No 1 Stall Test button. Reset MWS. Repeat for No 2 Stall Test button (IDNT 2 lights) Press No 3 Stall Test button. Stick shaker should not operate. Check IDNT 3 and MWS Stall IDENT annunciators light after 4 to 5 second delay. Release No 3 Stall Test button. Reset MWS. Press any two Stall Test buttons at the same time. Check stick shaker operates and pusher operates after a slight delay. Pilot's and copilot's Stall VLV A OPEN and Stall VLV B OPEN annunciators light. Pusher will not operate unless the yoke is held slightly back from neutral and the main hydraulic system is charged.

2. Press and hold ENG Fire 1 Test button. ENG 1 Fire annunciator, MWS red flashers, MWS ENG 1 Fire repeater, and No 1 HP COCK warning light all illuminate. engine fire warning bell rings. Press Bell Cancel 1. Fire warning bell stops. Bell CNCLD 1 annunciator lights.

NORMAL N-31


Press Bell Cancel 1 a second time. Fire warning bell rings. Bell CNCLD 1 annunciator goes out. Release ENG Fire 1 Test button. Engine fire warning bell stops. ENG 1 Fire annunciator, MWS ENG 1 Fire repeater, and No. 1 HP Cock warning light all extinguish. Repeat test for No. 2 engine using ENG Fire 2 Test button and corresponding No. 2 engine warning indicators.

3. Press HP Air OVHT Test button. Check MWS HP Air 1 OVHT and HP Air 2 OVHT annunciators and MWS flashers illuminate. Release HP Air OVHT Test button. MWS HP AIR 1 OVHT and HP AIR 2 OVHT annunciators extinguish.

4. Press ICE DET Test button. ICE DETECTD annunciator lights. MWS ICE PROT repeater annunciator flashes. Release ICE DET Test button. ICE DETECTD annunciator goes out after approx 20 seconds.

5. With flaps up, press Cabin Alt Test button. MWS Cabin Alt annunciator lights. Steady warning horn sounds. Silence horn using Horn Isolate button on No 1 throttle. Release Cabin Alt Test button. Warnings cease.

6. Press and hold ADS AHRS 1 TEST button. Pilot's Air Data Fail annunciator lights momentarily. MSI flag on, IAS and VMO pointer at zero, Mach blank. Altimeter flag on, pointer at 250 feet. VSI flag on, pointer at 6,000 ft/min down. SAT/TAS indicator blank. Confirm ATT and HDG warnings do not appear. Press Air Data Transfer switch in order to test the transfer function, then release after confirming operation.

Release ADS AHRS 1 Test button. Check flags off. Repeat for copilot's instruments using ADS AHRS 2 test.

N-32 NORMAL


NOTE If ATT and HDG warnings appear during the ADS AHRS 1 Test procedure, the AHRS backup power is not available. This defect must be rectified before flight. If Air Data Fail annunciators remain lit for approximately 45 seconds after release of test button, ADS backup power is not available. This defect must be rectified before flight.

7. Press VMO/MMO Test button 1 and 2 in turn and check intermittent operation of warning horn. With fuel in ventral tank, press LO VMO Test buttons 1 and 2 in turn and check intermittent operation of warning horn. Pressing and holding the LO VMO Test buttons also checks the related air data system.

ENGINE STARTING MALFUNCTIONS

Abort Start Procedures Abort start by closing HP Cock immediately, then operating Press For Abort switch if any of the following conditions occur: - No light-up within 10 secs of opening HP Cock. - ITT rapidly approaches 952°C. - Idle rpm (27% N1; 48-67% N2) not reached by 50

secs after light up. - Oil 2 LO Press annunciator not out before idle rpm. - N1 or N2 stops increasing before idle rpm.

NORMAL N-33


After Aborting Engine Start If an engine fails to start and is shut down by closing the HP COCK and operating the PRESS FOR ABORT switch, proceed as follows: - Wait 3 minutes to allow fuel to drain, or motor engine

for 15 seconds (do not exceed 2 minutes of motoring).

- Check the ignitor plugs are functioning correctly by operating the appropriate ENG IGNITION switch. The sparking of the ignitor plugs can be checked aurally by the ground crew.

Reset ENG Ignition switch to OFF. If satisfactory, resume normal starting procedure. - If two unsuccessful attempts to start are made, the

cause must be investigated and any fault rectified before making further attempts.

CAUTION Do not attempt a restart until indicated ITT is less than 200°C.

WARNING Electrical discharge from high energy units is potentially lethal. If for any reason ignitor leads are disconnected, do not handle LT leads or ignitor plugs for at least one minute after disconnecting the LT input.

N-34 NORMAL


APS-85 AUTOPILOT DIAGNOSTICS Pilot Instructions 1. If autopilot disengages during flight it is important to

record the AP DIS CODE and the YD DIS CODE prior to power shutdown.

2. If the autopilot cannot be engaged it is important to record the AP ENG CODE and the YD ENG CODE prior to power shutdown.

3. If the EFIS "FD" flag is in view it is important to record the STEER CODE while the FD flag is displayed.

4. If possible, allow maintenance personnel to view diagnostic data prior to power shutdown.

To Enter Diagnostics 1. Press and hold the EFIS GROUND TEST button.

Then press and release the RA TEST button on the DCP (display control panel) or the TST button on the DSP (display select panel). The DCP or DSP are part of the EFIS system.

2. Release the EFIS GROUND TEST button. 3. Press and release the RA TEST (or TST) button 3

times, or until FCS DIAGNOSTICS appears at top of the EFIS display.

4. Press and hold any 3 active MSP buttons for 2 seconds. The EFIS should now display REPORT MODE.

5. Record the appropriate AP and YD DIS CODES, AP and YD ENG CODES, or the STEER CODE. If the two YD CODES or the STEER CODE are not on the screen, use the APP pitch wheel to select the codes (as described below). The codes are selectable in alphabetical order. To change codes, increment the APP pitch wheel in either direction. Hold pitch wheel out-of-detent to continuously cycle through the parameter codes.

6. Each parameter code consists of 6 digits for both left and right side data. Record all 6 digits (in proper sequence) of both left and right columns of pertinent parameters. Include all zeros.

NORMAL N-35


To Exit Diagnostics Press the AP DISC switch, or press any 3 active MSP buttons.

PASSENGER BRIEFING (Pic or Crewmember) 1. Smoking: Prohibited in FAA aircraft.

Tampering, disabling, or destroying any smoke detector is prohibited. The NO SMOKING sign will be on at all times.

2. Safety belts: This is to include specific instructions on the fastening and release of seatbelts, directions to keep the seatbelts fastened during all surface movement, takeoffs, landings, and a recommendation that seatbelts be kept fastened en route to avoid injury resulting from unexpected turbulence.

3. Seat backs: If applicable, the placement of seat backs in the upright position while the aircraft is taxiing and during takeoff and landing operations.

4. Passenger entry door and emergency exits: Location and means of opening the cabin door and emergency exits.

NOTE Persons who need assistance to exit the aircraft will not be carried aboard flight inspection airplanes.

5. Fire extinguisher: Location and operation of fire extinguisher(s).

6. Survival equipment: Location and use of survival equipment.

7. Ditching procedures: If the flight includes extended overwater operation, ditching procedures, and the use of required flotation equipment.

8. Oxygen: If the flight involves operations above 12,000 feet mean sea level (MSL), the normal and emergency use of oxygen.

9. Headsets: The location of the additional headset.

N-36 NORMAL


TAKEOFF CREW BRIEFING/CONSIDERATIONS

Takeoff Briefing Crewmembers shall adhere to the following procedures. After the first flight, the term "standard briefing" may be used provided the crew positions and duties are not changed. Before taking the active runway for departure, a takeoff briefing will be accomplished by the Pilot Flying (PF). Prior to takeoff, the PF will cover the following items. (1) Aircraft Configuration, (2) Power Limitations, (3) Engine instruments, monitor during takeoff, (4) V Speeds, (5) Emergency Procedures, (6) Emergency Return, (7) Initial altitude and heading for departure, and (8) Answer any questions from other

crewmembers.

NORMAL N-37


INSTRUMENT APPROACH REVIEW When executing any instrument approach for the purpose of landing, including a visual approach for the intention of landing, an oral briefing will be accomplished by the PF and will cover the following items, as applicable. 1. Review the name of the Approach--i.e., ILS RWY

17R, Will Rogers Airport. 2. Field Elevation -- _____________ MSL. 3. Approach Altitudes - __________________ MSL (as

applicable) 4. Minimum Altitude on Approach -- DH/MDA of

__________ MSL. 5. How procedure will be flown; i.e., time, rate of

descent, etc. 6. Missed approach point and procedure. 7. Other instructions by the PF such as: (a) Tuning and setting of navigation radios. (b) Heading changes required on approach. (c) Other call-out procedures as requested. (d) Verify systems not working applicable to the

approach in use. (e) Verify runway conditions.

N-38 NORMAL


DC Power System – De-Energized Schematic

NORMAL N-39


AC Power System - Schematic

N-40 NORMAL


DC Power Distribution - PE Bus Bar

NORMAL N-41


DC Power Distribution - PS1 Bus Bar

N-42 NORMAL


DC Power Distribution - PS2 Bus Bar

NORMAL N-43


AC Power Distribution

N-44 NORMAL


Refuel/De-fuel System Schematic

NORMAL N-45


Hydraulic System Schematic

N-46 NORMAL

BAe 125-800A TI 4040.25 AVN CHECKLIST Original, 03/1997

EMERGENCY/ABNORMAL PROCEDURES

IMMEDIATE ACTION Memory items (“phase one” or “boldface”) are in bold text, and are boxed and shaded. These items should be completed in as timely matter as possible consistent with controlling the aircraft on the desired flight path. Hurried action can result in a more serious situation than the emergency itself. Therefore, memory items must be accomplished with care and coordination between all crewmembers. In addition to the outlined items in the checklist procedure, the following steps are considered part of all emergency or abnormal situations: 1. Fly the aircraft. 2. Silence any aural warning. 3. Identify the emergency or abnormality. 4. Perform memory items at a safe altitude (400 ft

AGL minimum). 5. Use the appropriate checklist(s) to confirm

accomplishment of memory items. Complete the checklist observing any NOTE, CAUTION , or WARNING , as applicable.

SPECIFIC PROCEDURES It is not possible to develop specific procedures to cover all possible combinations of emergency/abnormal situations. Therefore, if a situation exists for which these procedures are not adequate or applicable, the pilot’s best judgment must prevail.

A

TI 4040.25 BAe 125-800A Original, 03/1997 AVN CHECKLIST

MASTER WARNING ANNUNCIATION TAB# TAB# TAB#

SMOKE 4 ________ AUX PACK

HP AIR 1 OVHT 6 REAR BAY

OVHT 6 HP AIR 2 OVHT 6

ENG 1 FIRE 1/2 CABIN

ALTITUDE 5/10 ENG 2 FIRE 1/2

OIL 1 LO PRESS 14 ELEV/AIL

TRIM 9 OIL 2 LO PRESS 14

HYD 1 LO PRESS 16 HYD OVHT 16 HYD 2

LO PRESS 16

MAIN AIR VALVE 1 AUX HYD

LO LEVEL MAIN AIR VALVE 2

ENG 1 CMPTER 4 EMER BRK

LO PRESS 8 ENG 2 CMPTER 4

ENG 1 A-ICE ICE

PROT ENG 2 A-ICE

ELECT 11 FUEL 15 DUCT OVHT 10

ENT DOOR UNLOCKED APU MSTR

SW ON RUDDER BIAS

ICE PROT SELECTED FUEL

XFD TFR STALL IDENT

B

BAe 125-800A TI 4040.25.2 AVN Checklist Temp Rev 01, June 2005

Table of Contents TAB

E-iii

Ground Emergencies APU Fire ...................................................................... 1 APU Failure.................................................................. 1 APU Generator Overheat............................................. 1 Engine Fire................................................................... 1 Takeoff Emergencies Rejected Takeoff.......................................................... 2 Landing Gear Retraction Fail ....................................... 2 Gear Handle Can’t Be Moved ...................................... 2 In Flight Emergencies Engine/Fire/Failure/Shutdown...................................... 2 Two Engine Failure ...................................................... 3 Starter Assisted Air Start.............................................. 3 Windmill Air Start ......................................................... 4 Compressor Stall ......................................................... 4 Engine Computer Malfunction...................................... 4 Smoke and Fumes ..................................................... 5 Smoke/Fire In Aft Baggage.......................................... 5 Smoke/Fire In Vestibule, Cabin or Cockpit..................................................................... 5 Smoke and Fume Elimination ...................................... 5 Electrical Fire ............................................................... 5 Air Conditioning Smoke/Fumes ................................... 6 Depressurization/EMERG Descent........................... 6 Rear Equipment Bay Overheat ................................. 6 High Pressure Air Overheat ......................................... 7 Landing Emergencies Landing Gear Extension Failure .................................. 7 Hydraulic system failures ............................................. 8 Main System Brake Failure.......................................... 8 Emergency brake low pressure ................................... 8 No Flap Landing........................................................... 9 Landing Emergencies Cont’d Asymmetric Airbrakes .................................................. 9 Single Engine Landing................................................. 9 Single Engine Go Around ............................................ 9 Trim Only Landing........................................................ 9 Ditching...................................................................... 10 Forced Landing.......................................................... 10 Air Conditioning/ Pressurization Duct Overheat............................................................ 10 Automatic Temp Control Failure ................................ 10 Failure To Pressurize................................................. 10 Automatic Pressure Control Fail ................................ 10 Auxiliary Cooling Pack Failure ................................... 10 Pressurization Regulation Failure .............................. 10

Continued Next Page

TI 4040.25.2 BAe 125-800A Temp Rev 02, October 2005 AVN Checklist

Table of Contents TAB

E-iv

Avionics/Pitot Static Air Data Computer Failure..........................................11 AP/AHRS Fan Fail PTR .............................................11 EFIS Fan Failure ........................................................11 EFIS Overheat............................................................11 DPU Failure................................................................11 PFD Failure ................................................................11 ND Failure ..................................................................11 Unreliable Airspeed....................................................11 Pitot Heat Failure .......................................................11 Electrical Double Generator Failure...........................................12 Single Generator Failure ............................................12 Fluctuating/Abnormal Voltage ....................................12 PS2 Powered Circuits ................................................12 Generators Out of Balance.........................................13 Battery Hot .................................................................13 Battery Overheat ........................................................13 XE Failure...................................................................13 XS1 and XE Failure....................................................14 XS1 or XS2 Failure.....................................................14 Double Inverter Failure ............................................14 Single Inverter Failure..............................................14 Alternator Failure........................................................14 Double Alternator Failure ...........................................14 Engines High RPM or High ITT................................................15 Fluctuating RPM.........................................................15 High Oil Temperature .................................................15 Oil Low Pressure........................................................15 Flight Controls/Autopilot False Stick Shaker/Pusher.........................................15 Electric Pitch Trim Runway ........................................15 Autopilot Trim Warnings.............................................15 Fuel Auxiliary Fuel Transfer Failure ...................................16 Fuel Low Pressure .....................................................16 Engine Fuel Malfunction.............................................16 Hydraulics Hydraulic Low Pressure .............................................16 Main Hydraulic Failure................................................16 Hydraulic System Overheat............................................ Windscreen Windscreen Overheat.................................................16 Side Screen Overheat ................................................16 Windscreen Failure ....................................................16

BAe 125-800A TI 4040.25C Original, March 1997

EMERGENCY/ABNORMAL GROUND EMERGENCIES

APU Fire

1. APU MASTER.....................OFF (Wait 10 Seconds) RP 2. APU EXTINGUISHER...........................DISCHARGE (If Required) RP

CAUTION If APU is not running when fire bell and annunciator are activated, discharge APU extinguisher immediately.

3. No. 1 LP Cock ................................................CLOSE RP

APU Failure

1. APU Master .........................................................OFF RP

APU Generator Overheat

1. APU Master .........................................................OFF RP Do not attempt to restart APU until the problem is rectified.

E-1

Engine Fire ENG FIRE

1. HP COCK.......................................................CLOSE LP

2. LP COCK .......................................................CLOSE LP

3. START PWR....... PUSH FOR ABORT (If Required) LP

4. EXTINGUISHER .....................SHOT 1 (If Required) LP

5. Extinguisher.............................. SHOT 2 (If Required) LP

6. Battery Power......................................................OFF LP

7. Evacuate Aircraft ..................................................ALL

NOTE

1. Make no attempt to restart the engine after a fire warning.

2. Closure of No. 1 LP cock will automatically shut down the APU if it is running.

TI 4040.25C BAe 125-800A Original, March 1997

E-2

TAKEOFF EMERGENCIES Rejected Takeoff

1. Throttles ....................................................... IDLE PF 2. Airbrakes....................................................OPEN PF 3. Brakes......................................... AS REQUIRED PF On Slippery Runways: 4. Flaps ...............................................................45° PNF 5. Lift Dump..............................OPEN AT 45° FLAP PF 6. Downwind Engine HP Cock.....................CLOSE (As Required) PF

Landing Gear Retraction Failure 1. Aux Hyd Hand Pump ....SOCKET FULLY DOWN PNF

2. Aux Hyd Pull Selector ...............................SET IN PNF If Gear Still Fails to Retract: 3. Ground Locks .........................CHECK STOWED PNF

4. Landing Gear Lever ..................................DOWN PNF

LAND AS SOON AS PRACTICAL after reducing aircraft weight to below normal landing limit of 23,350 lb.

Landing Gear Handle Cannot Be Moved If Retraction is Essential: 1. O/Ride and Landing Gear Levers ................SELECT UP TOGETHER PNF


IN FLIGHT EMERGENCIES

E-3

Engine Fire / Failure / Shutdown ENG FIRE

1. HP COCK.......................................................CLOSE PF

2. LP COCK .......................................................CLOSE PF

3. EXTINGUISHER ...................... SHOT 1 (If required) PF

4. Generator ...........................................................TRIP PNF

5. Bustie .............................................................CLOSE PNF

6. Main Air Valve ................................................CLOSE PNF

7. Flight Deck Valve (No. 2 Engine Only)...........CLOSE PNF

CAUTION If shutdown occurs during climb, close both main air valves to ensure maximum thrust from the operating engine. If shutdown is during descent, set main air valve on remaining engine to LP ON. Do not attempt to restart engine if there are any reasons to suspect mechanical malfunction or failure.

8. Engine Ignition ............................................ OFF PNF 9. Extinguisher .......................SHOT 2 (If required) PNF

If warning goes out, release canceled fire bell and test fire detection system. If system does not function, confirm engine status visually.

10. Engine Sync................................................ OFF PNF 11. Alternator .................................................... OFF PNF 12. Generator Amps ....................................CHECK PNF BELOW 400 UP TO 10,000 FT OR 330 ABOVE 10,000 FT 13. Wing Fuel/X Feed/Transfer ................... X FEED PNF 14. Fuel L and R Pump Switches.. BALANCE FUEL PNF

NOTE If engine failure occurs during normal climb, and if cruise flight is to be continued, increase power on the operating engine to maximum continuous (100% or 924°C, whichever is lower) and climb at enroute climb speed to the required cruise altitude.


Two Engine Failure 1. THROTTLES ......................................................IDLE PF

2. ENGINE IGNITIONS............................................. ON PF

3. Engine Indications .....................................MONITOR PNF If N1 and N2 RPM do not increase within 10 seconds:

or if ITT rapidly approaches 952°C: 4. HP Cock (Affected Engine)............................ CLOSE PNF 5. Engine Ignition (Affected Engine) ........................OFF PNF When engine(s) has successfully started: 6. Throttles .....................................SET AS REQUIRED PF

Wait until engines have stabilized before selecting ignition(s) off, then confirm IGN ON annunciator out. If only one engine starts, leave the running engine ignition on.

7. Engine Ignitions ...................................................OFF PNF 8. Engine Indications ...................................... NORMAL PNF 9. Generators..................................................... CLOSE PNF 10. Bustie ............................................................. CLOSE PNF

Check generators balanced and below 400 amps up to 10,000 ft or 330 amps above 10,000 ft.

If engine does not airstart: accomplish ENGINE FIRE/FAILURE/SHUTDOWN Checklist

Airstart Envelope

30

20

10 0

0 100 200 300 ALTITUDE INDICATED AIRSPEED (knots) (1000s of ft)

WINDMILL

COMPUTER INOPERATIVE

E-4


Starter Assisted Airstart 1. Speed and Altitude....................WITHIN ENVELOPE PF 2. N1 and N2.................................... BOTH INDICATING PNF

CAUTION Do not attempt airstart if there is no indication of N1 rotation.

3. HP Cock .........................................................CLOSE PNF 4. LP Cock............................................................OPEN PNF 5. Engine Anti-Ice ....................................................OFF PNF 6. Fuel Pump .............................................................ON PNF 7. Engine Sync ........................................................OFF PNF 8. Main Air Valve ................................................CLOSE PNF 9. Start Power............................................................ON PNF 10. Engine Starter Switch............................................ON PNF 11. HP Cock ...........................OPEN AT/ABOVE 10% N2 PNF 12. Fuel Enrichment ............... PRESS UP TO 400°C ITT PNF 13. Fuel Flow..................................CHECK INDICATION PNF 14. ITT ............................................................. MONITOR PNF

If light up does not occur within 10 secs, or: If ITT rapidly approaches 952°C, or: If no oil pressure is indicated within 10 sec of light up:

15. HP Cock .........................................................CLOSE PNF 16. Start Power................................. PUSH FOR ABORT PNF

CAUTION Wait 10 seconds between airstart attempts (for fuel drainage).

After Start: 17. Engine Start Switch...... LIGHT OUT ABOVE 45% N2 PNF 18. Start Power..................................PUSH, LIGHT OUT PNF 19. Generator .....................................................ON LINE PNF 20. Bustie .............................................................CLOSE PNF 21. Engine Indications .......................................NORMAL PNF 22. Main Air Valve ...............OPEN/LP ON (As Required) PNF 23. Throttles .................................... SET AS REQUIRED PF 24. Wing Fuel/X Feed/Transfer ............... AS REQUIRED PNF 25. Inverter ..................................................................ON PNF 26. Alternator...............................................................ON PNF

E-5


E-6

Windmill Airstart

1. Speed and Altitude ................... WITHIN ENVELOPE PF 2. N1 ........................................................... INDICATING PNF

CAUTION Do not attempt airstart if there is no indication of N1 rotation.

3. N2 ...................................................... 10% OR MORE PNF 4. HP Cock......................................................... CLOSE PNF 5. LP Cock ............................................................OPEN PNF 6. Engine Anti-Ice ....................................................OFF PNF 7. Fuel Pump............................................................. ON PNF 8. Engine Sync.........................................................OFF PNF 9. Main Air Valve................................................ CLOSE PNF 10. Engine Ignition ...................................................... ON PNF 11. HP Cock (when N2 at or above 10%) ...............OPEN PNF 12. Fuel Enrichment (If Required) ..........................................PRESS UP TO 400°C ITT PNF (Not available with engine computer inoperative) 13. Fuel Flow ................................. CHECK INDICATION PNF 14. ITT..............................................................MONITOR PNF

If light up does not occur within 10 secs, or: If ITT rapidly approaches 952°C, or: No oil pressure indicated within 10 secs of light up:

15. HP Cock......................................................... CLOSE PNF

CAUTION Wait 10 seconds between airstart attempts (for fuel drainage).

After Start: Check engine at self-sustaining speed above 45% N2 and stabilized. 16. Engine Ignition .....................................................OFF PNF 17. Generator..................................................... ON LINE PNF 18. Bustie ............................................................. CLOSE PNF 19. Engine Indications ...................................... NORMAL PNF 20. Main Air Valve............... OPEN/LP ON (As Required) PNF 21. Throttles .....................................SET AS REQUIRED PF 22. Wing Fuel/X Feed/Transfer................AS REQUIRED PNF 23. Inverter.................................................................. ON PNF 24. Alternator .............................................................. ON PNF


Compressor Stall 1. Throttle ................. RETARD UNTIL STALL CEASES THEN SLOWLY ACCELERATE TO REQUIRED POWER PF

If compressor stall cannot be eliminated, accomplish Engine Fire/Failure/Shutdown procedure. Airstart is not recommended but may be attempted if circumstances dictate.

2. Main Air Valve ................................................. LP ON PNF

If compressor stall is due to bleed air system check valve failure, there is a risk of engine surge at high altitude cruise or at descent power.

3. ITT ............................................................. MONITOR PNF

If compressor instability does not clear at low rpm and ITT is well within limits: 4. Engine Computer .............CYCLE AUTO/OFF/AUTO PNF

Engine Computer Malfunction Engine synchronizer will disengage and ENG CMPTR annunciator lights. 1. Engine Computer Switch.................... OVSPD PROT PNF 2. Throttle .............ADJUST FOR REQUIRED RPM/ITT PF 3. Engine Indications ..................................... MONITOR PNF Accomplish the following procedure relevant to the flight condition: TAKEOFF At Maximum Power: Below 80 KIAS, reject the takeoff. Above 80 KIAS, continue. If N1 rises, throttle back to N1RFF. At Maximum Continuous Power: Adjust throttle to achieve maximum continuous ITT, 924°C. CRUISE Set ITT of 908°C LANDING

Select Engine Anti-ice OFF and Main Air Valves to CLOSE whenever possible. N1 on engine with inoperative computer should not be reduced below 60% during the approach. Delay bringing throttle to idle until after touchdown.

The other engine should be operated normally.

ENG CMPTER

E-7

TI 4040.25.2 BAe 125-800A Temp Rev 01, June 2005 AVN Checklist

SMOKE and FUMES SMOKE

1. Oxygen Masks........................................ON/100% ALL 2. Passenger Oxygen.......................................PULL LP

2a. Communications................................... Establish ALL

NOTE Aircraft incorporating Engineering Order 05-25-07 (Rev 1) are modified with a MASK MIC ON/OFF toggle switch on the pilot and copilot headset jack panels. To enable the oxygen mask microphone, the audio panel toggle BOOM/MASK switch must be set to MASK and, additionally, the MASK MIC switch must be set to ON.

3. Smoke Goggles.............................. AS REQUIRED ALL 4. Seat Belts Sign...................................................ON PNF

Smoke/Fire In Aft Baggage Compartment

1. Auxiliary Cooling Pack ..................................OFF PNF 2. Portable Oxygen, Goggles, Fire Extinguisher...... .............................................. DON EQUIPMENT PNF

WARNING Insure contact is maintained with at least one other crew member in case fire fighter is overcome by fumes.

3. Enter Toilet and Close Door................................. PNF 4. Aft Baggage Compartment ........................OPEN PNF ............................... and Take Appropriate Action Accomplish Smoke and Fume Elimination checklist.

Smoke/Fire In Vestibule, Cabin or Cockpit

1. Auxiliary Cooling Pack ..................................OFF PNF 2. Portable Oxygen, Goggles, Fire Extinguisher...... .............................................. DON EQUIPMENT PNF 3. Fire Extinguisher ..............................FIGHT FIRE PNF Accomplish Smoke and Fume Elimination checklist.

Smoke and Fume Elimination

1. Descend ............................................................... PF 2. Dump Valve................................................OPEN PNF SLOWLY To Maintain Pressurization 3. Below 15,000 ft ........................DEPRESSURIZE PNF

Set PRESS CONTROL to GROUND TEST and MANUAL CABIN ALT CONTROL to full INCREASE.

Continued Next Page

E-8


NOTE With MAIN AIR VLV switches OPEN, selecting FLOOD may help disperse cabin smoke.

4. Dump Valve....................................... AS REQUIRED PNF

Electrical Fire 1. Autopilot and Yaw Damper ...................DISENGAGE PF 2. Panel Lights....................EMERGENCY (If Required) PNF 3. Cabin & Lav Lights ............................................STBY PNF 4. Battery .................................................EMERGENCY PNF 5. Standby Inverter ................................................. ARM PNF 6. FIS Power............................................................OFF PNF 7. Auxiliary Cooling Pack.........................................OFF PNF 8. Generators 1 and 2 ............................................TRIP PNF 9. Engine Computers 1 and 2 .................................OFF PNF If smoke decreases, proceed with A: If smoke persists proceed with B: A. Fault on PS1 or PS2 Busbar: 10. Battery ...................................................................ON PNF 11. PS1b/2b Circuit Breaker (M10, Panel D) .........OPEN PNF 12. Generator 2 ....................................................CLOSE PNF If smoke recurs, fault is on PS2. 13. Generator 2 ........................................................TRIP PNF 14. Generator 1 ....................................................CLOSE PNF If smoke persists, fault is also on PS1. 15. Generator 1 ........................................................TRIP PNF 16. Accomplish Double Generator Failure Checklist.PNF

NOTE If fault is isolated to PS1 or PS2, energize good busbar and reinstate systems powered from that source. When smoke ceases it may be possible to link busbars with the bustie, and identify smoke source to particular equipment. Disconnect suspect equipment and reinstate all other equipment. Close circuit breaker M10 as required.

B. Fault on PE Busbar: 10. Battery ...................................................................ON PNF 11. Generators 1 and 2 ........................................CLOSE PNF 12. Bustie .............................................................CLOSE PNF 13. Inverters 1 and 2 ............................................ START PNF 14. Screen Heat L .....................................................OFF PNF

Continued Next Page

E-9

TI 4040.25.2 BAe 125-800A Temp Rev 01, June 2005 AVN Checklist

If Smoke Persists: 15. White Circuit Breakers (Panels A & D) ......OPEN PNF Once smoke ceases, reinstate equipment one at a time.

Identify and disconnect equipment causing smoke.

Air Conditioning Smoke/Fumes Accomplish Smoke and Fumes and Smoke and Fume Elimination checklists if conditions warrant. 1. Main Air Valve 2.......................................CLOSE PNF 2. Flight Deck Valve .....................................CLOSE PNF If contaminated air still persists: 3. Main Air Valve 2.........................................OPEN PNF 4. Main Air Valve 1.......................................CLOSE PNF If contaminated air still persists: 5. Descend below 15,000 ft ............................... PF 6. Main Air Valve 2 ................................CLOSE PNF

DEPRESSURIZATION/EMERGENCY DESCENT

CABIN ALTITUDE

1. OXYGEN MASKS................................ ON/100% ALL 2. PASSENGER OXYGEN .............................PULL LP

2a. Communications................................... Establish ALL

E-10


3. Main Air Valves .............................BOTH CLOSE PNF 4. Flight Deck Valve ...............OPEN (hold 10 secs) PNF 5. Seat Belts Sign................................................ON PNF 6. Cabin Altitude.......................................... CHECK RP If Above 15,000 ft Cabin Altitude: 7. Throttles ....................................................... IDLE PF 8. Speed.........................................MMO/VMO Unless PF Structural Damage Suspected 9. Airbrakes ....................................................OPEN PF 10. Dump Valve................................................ SHUT PNF 11. Manual Altitude Control........FULLY DECREASE RP

BAe 125-800A TI 4040.25.2 AVN Checklist Temp Rev 01, June 2005

When Below 10,000 ft Cabin Altitude: 12. Cabin Altitude ....................CHECK STABILIZED RP 13. Flight Deck Valve.....................................CLOSE PNF 14. Dump Valve ................................ AS REQUIRED PNF

It should now be possible for crew/passengers to remove masks.

REAR EQUIPMENT BAY OVERHEAT REAR BAY

OVHT 1. Main Air Valves ...........................BOTH CLOSE PF 2. Flight Deck Valve ..................................... OPEN PF

If warning persists (after 10 seconds): 3. Flight Deck Valve.....................................CLOSE PNF 4. Oxygen Masks ................................................ON ALL 4a. Communications................................... Establish ALL


5. Passenger Oxygen ..................................... PULL LP 6. Descend................. 15,000 Ft Cabin Alt or Lower PF 7. Throttles....................................................... IDLE PF 8. Speed..................................................... MMO/VMO PF Unless Structural Damage Suspected 9. Airbrakes.................................................... OPEN PF 10. Dump Valve ................................ AS REQUIRED PNF 11. LAND AS SOON AS POSSIBLE If warning ceases: 12. DESCEND .....................................As Necessary PF To Maintain Comfortable Cabin Conditions If closing hot engine bleed air resolves emergency indication, flight may be continued at a lower altitude in an unpressurized condition.

E-11


E-12

High Pressure Air Overheat HP AIROVHT

1. Main Air Valve...............................................CLOSE PNF

2. Flight Deck Valve (If HP AIR 2 OVHT) .........CLOSE PNF When warning ceases: 3. Main Air Valve................................................ LP ON PNF

4. Flight Deck Valve............................. AS REQUIRED PNF


LANDING EMERGENCIES Landing Gear Extension Failure

Switch off all electrical loads just prior to landing. 1. Horn ...............................PULL CIRCUIT BREAKER RP 2. GPWS (if fitted) ..............PULL CIRCUIT BREAKER RP All gear locked down shown by standby indicators? Yes Make a normal landing

E-13

No AUX HYD SYSTEM........................................... Pull Handle HAND PUMP...................... Operate, (see NOTES a and b) Proceed according to how many gear legs are locked down (see NOTE c).

All gear legs locked down

Landing Gear Handle.........................CONFIRM DOWN Make a normal landing

Only two gear legsLocked down OR (see NOTE d)

Landing Gear Handle.........................CONFIRM DOWN Go to Prepare for Landing procedure

Only one gear leg locked down No gear legs locked down

Ensure all landing gear are fully retracted by: Hand Pump ...................... FULLY DOWN AUX HYD System ..... PUSH HANDLE IN Landing Gear Handle ...........SELECT UP All Gear Locked Up .................CONFIRM Go To Prepare For Landing Procedure

NOTE

a. Vigorous pumping mist be needed if gear is stuck in partially lowered position.

b. After three greens are seen, continue pumping until significant resistance is felt.

c. The position of the landing gear shall be established by checking the normal (green) and standby indicators.

d. The flight crew has the choice to land with the gear down OR to retract the gear and perform an all gear up landing. Although an all gear up landing should result in less damage to the aircraft than landing with two gears locked down, passengers will experience an unpleasant landing impact and a longer period of time may be required to clear the aircraft from the runway.

Continued Next Page

TI 4040.25C BAe 125-800A CHG 01, June 1999

Preparing for Landing 3. Passengers....BRIEF FOR EMERGENCY LANDING RP 4. Loose equipment .........................................SECURE ALL 5. Emergency exit .............................CONFIRM CLEAR TECH 6. MAIN AIR VLVs .................................. CLOSE BOTH RP 7. DUMP VALVE...................................................OPEN RP Landing 8. Flaps ..................................................................45O RP

NOTE a. Land at as low a weight as possible.

b. Touchdown at as low a speed as practicable.

c. Do not use lift dump. After Touchdown With Two Gear Legs Locked Down

NOTE a. Keep the unsupported wing or nose off the ground until

at a low speed, but lower wing or nose before control is lost.

b. After lowering the unsupported wing or nose, use wheel brakes and nosewheel steering, if appropriate, to keep in a straight line.

If the Nose Gear is Not Locked Down 9. HP COCKS at touchdown............................CLOSED RP With All Gear Up 10. HP COCKS at touchdown............................CLOSED RP

E-14


Hydraulic System Failures Landing Gear Lowering Using the Auxiliary Hydraulic System 1. Operate AUX HYD SYSTEM ...........................PULL LP 2. HAND PUMP....................OPERATE (see NOTE a) RP 3. LANDING GEAR Lever ................................. DOWN RP

NOTE a. After three greens are seen, continue pumping until

significant resistance is felt.

b. Lowering of the landing gear (or flaps) by means of the auxiliary hydraulic hand pump system will not be possible until item 1 has been completed.

c. The hand pump cannot be used to raise the landing gear.

d. Following a main hydraulic system failure, the AUX HYD SYSTEM PULL handle must not be reset in flight.

Main System Brake Failure

If main braking system failure is suspected but not confirmed before landing, the emergency system should only be selected if complete failure of the normal system is confirmed after touchdown. 1. Brake Pedals ..............................................RELEASE PF 2. Brake Lever ...................................................EMERG PF

WARNING Do not set wheel brake to PARK position when setting lever to EMER as this will cause the brakes to lock with possibile tire failure

3. Brake Pedals ................................APPLY GENTLY PF

Shut down one engine, where possible, to reduce required braking. The aircraft should not be taxied as differential braking is now the only means of aircraft steering.

E-15

Emergency Brake Low Pressure EMER BRKLO PRESS

1. Brake Pedals ..................................... Apply Sparingly PF

CAUTION Apply brakes gently and use as few applications as possible. Aircraft should not be taxied as only differential braking will be available for aircraft steering.

TI 4040.25C BAe 125-800A CHG 01, June 1999

No Flap Landing 1. GPWS FLAP WARN OVRD ..................... OPERATE PNF 2. Gear ................................................................ DOWN PF/PNF 3. Approach KIAS ..............................VREF + 30 KNOTS PF 4. Threshold KIAS..............................VREF + 15 KNOTS PF 5. Nosewheel .................................................................. ............. LOWER IMMEDIATELY ON TOUCHDOWN PF 6. Airbrakes...........................................................OPEN PF

CAUTION With hydraulic failure, airbrakes may not open.

Asymmetric Airbrakes 1. Airbrakes...........................................................SHUT PF 2. If Airbrakes Asymmetric or Out................................... .......................... ACCOMPLISH NO FLAP LANDING PF

Single Engine Landing 1. APR....................................................AS REQUIRED PNF

2. Ignition .................................................................. ON PNF

3. Approach Flaps .......................................................... .......................... 25° (Precision), 15° (Non-Precision) PF/PNF

4. Landing Flaps ................. 45° (LANDING ASSURED) PF/PNF

Single Engine Go Around 1. Throttle................................................................MAX PF

2. Airspeed...................... VREF + 5 KIAS OR GREATER PF

3. Flaps ..................................................................... 15° PF/PNF

4. Gear .......................................................................UP PF/PNF

5. APR....................................................AS REQUIRED PNF

6. FLAPS................................................AS REQUIRED PF/PNF

WARNING Airworthiness requirements do not ensure positive climb performance in the final landing configuration with one engine inoperative. The decision to discontinue the approach should be made before the flaps are extended to 45°.

E-16


Trim Only Landing A. Elevator Failure: 1. Trim Indicator .................................................CHECK PF 2. Autopilot ................................................DISENGAGE PF 3. Airspeed ......................................................160 KIAS PF 4. Flaps......................................................................15° PF/PNF 5. Gear ................................................................DOWN PF/PNF Final Approach: 6. Flaps......................................................................45° PF/PNF 7. Airspeed .............................................VREF + 10 KIAS PF 8. Airspeed Control............................ ELEVATOR TRIM PF 9. Rate of Descent Control .......................... THROTTLE PF B. Rudder, Elevator and Single Engine Failure: 1. Airspeed ......................................................160 KIAS PF 2. Flaps......................................................................15° PF/PNF 3. Gear ................................................................DOWN PF/PNF Final Approach: 4. Flaps......................................................................25° PF/PNF 5. Airspeed .............................................VREF + 20 KIAS PF

Maintain VREF + 20 KIAS to threshold and land with flaps 25°. C. Aileron Failure: 1. Trim Indicator .................................................CHECK PF 2. Autopilot ................................................DISENGAGE PF 3. Airspeed ......................................................160 KIAS PF 4. Flaps........................................................................0° PF/PNF 5. GPWS FLAP WARN OVRD......................OPERATE PNF 6. Gear ................................................................DOWN PF/PNF

Final Approach: 7. Lateral Control..............RUDDER or AILERON TRIM PF 8. Flaps.................................................. AS REQUIRED PF/PNF

Should lateral control be seriously impaired, it is recommended the landing be made with flaps 0°.

9. Airspeed .......................... VREF + 25 KIAS MINIMUM PF

Greater airspeed may be necessary to retain lateral control.

ELEV/AILTRIM

E-17


E-18

Ditching

1. Crewmembers .............................................. ADVISE PF 2. Surface Stations & Ships .............................. NOTIFY PNF 3. Loose Equipment.........................................SECURE ALL 4. Life Vests ............................................................DON ALL 5. Aircraft Weight ............................................ REDUCE PF 6. Cabin...............DEPRESSURIZE BELOW 10,000 FT PNF 7. Main Air Valves (2) ........................................ CLOSE PNF 8. Flight Deck Valve........................................... CLOSE PNF 9. Overwing Escape Hatch ................STOW IN TOILET PNF/ET 10. Dump Valve ................................................... CLOSE PNF

If required, open dump valve to confirm depressurized, then close.

11. Exterior Lights....................................................... ON PNF 12. Cockpit & Cabin Interior Lights ..................... EMERG PNF 13. Circuit Breakers: Gear Horn (K1 on Panel D), and GPWS (H19 on Panel A) ...........................OPEN PNF 14. Determine Direction of Ditching.................................. PF Ditching Imminent: 15. Autopilot ................................................ DISENGAGE PF 16. Gear .......................................................................UP PF/PNF 17. Flaps ..................................................................... 45° PF/PNF 18. Give Final Warning .................BRACE FOR IMPACT PF After Ditching: 19. Life Raft.........................................LAUNCH, BOARD ALL

Forced Landing

1. Advise Crewmembers................................................. PF 2. Ground Emergency Facilities........................ NOTIFY PNF 3. Loose Equipment.........................................SECURE ALL 4. Aircraft Weight ............................................ REDUCE PF 5. Cabin...............DEPRESSURIZE BELOW 10,000 FT PNF 6. Main Air Valves (2) ........................................ CLOSE PNF 7. Flight Deck Valve........................................... CLOSE PNF 8. Overwing Escape Hatch ................STOW IN TOILET PNF/ET 9. Dump Valve ......................................................OPEN PNF

If Gear Up: 10. Circuit Breakers: Gear Horn (K1 on Panel D), and GPWS (H19 on Panel A) ...........................OPEN PNF

Crash Landing Imminent: 11. Autopilot ...................... DISENGAGE ABOVE 150 FT PF 12. Gear ...................................................AS REQUIRED PF/PNF 13. Flaps ..................................................................... 45° PF/PNF 14. Give Final Warning .................BRACE FOR IMPACT PF 15. Generators 1 & 2 ................................................TRIP PNF 16. Battery..................................................................OFF PNF 17. Throttles ..............................................................IDLE PF 18. HP Cocks (2) ................................................. CLOSE PNF 19. LP Cocks (2) .................................................. CLOSE PNF

After Landing: 20. Evacuate Aircraft ..................................................... ALL


AIR CONDITIONING / PRESSURIZATION

Duct Overheat

1. Cabin Temp Selector.................................................. ..................................MANUAL, HOLD FULLY COOL PNF

If Warning Ceases: 2. Cabin Temp Selector...............USE MANUAL MODE PNF

If Warning Persists: 2. Cabin Temp Selector................AUTO, FULLY COOL PNF

Automatic Temperature Control Failure

1. Cabin Temp Selector.................................................. ........................ MANUAL, COOL OR HOT AS REQD PNF

Failure To Pressurize

1. Main Air Valves .................................. CHECK/OPEN PNF 2. Dump Valve...................................................... SHUT PNF 3. Pressurization Switch.......................................OVRD PNF

Automatic Pressure Control Failure

1. Manual Alt Control.................TURN SLOWLY UNTIL CABIN ALT INCREASES SLIGHTLY PNF 2. Pressurization Valve.........................GROUND TEST PNF 3. Manual Alt Control....... CONTROL AS NECESSARY PNF If this is ineffective, use dump valve to control pressurization.

Auxiliary Cooling Pack Failure

1. Aux Cooling Pack Switch ....................................OFF PNF CONTINUE FLIGHT.

Pressurization Regulation Failure

1. Main Air Valve 2 .............................................CLOSE PNF 2. No. 2 Throttle............................REDUCE TO 85% N1 PF 3. Main Air Valve 2 ...............................................OPEN PNF A. If Main Air Valve 2 Annunciator NOT Lit: CONTINUE FLIGHT B. If Main Air Valve 2 Annunciator Lit: 4. Main Air Valve 2 .............................................CLOSE PNF LAND AS SOON AS PRACTICAL

AUX PACK

DUCT OVHT

CABIN ALTITUDE

E-19

TI 4040.25C BAe 125-800A CHG 01, June 1999

AVIONICS / PITOT STATIC

Air Data Computer Failure 1. Relevant Flight Instruments.................. CHECK FOR FAILURE FLAGS PF/PNF

2. Failed Instruments .............................................TEST PF/PNF (to determine whether air data computer or instrument failed) If MSI And Altimeter Are Both Inoperative: 3. Relevant Air Data Transfer Switch ........... OPERATE PF/PNF

AP/AHRS Fan Fail PTR 1. AP/AHRS FAN FAIL PTR Switch PRESS TO RESET PNF

CONTINUE FLIGHT

EFIS Fan Failure 1. No pilot action ............................CONTINUE FLIGHT PF

This may lead to subsequent EFIS OVHT warning.

EFIS Overheat Warning On Left Hand Panel Only: 1. EFIS OVHT indicators below ND1............. EXAMINE PF If EFD Overheat Annunciator Lit: 2. Left EFD Master Switch .......................................OFF PF If MFD Overheat Annunciator Lit: 2. MFD Master Switch .............................................OFF PF If MPU Overheat Annunciator Lit: 2. MFD Master Switch .............................................OFF PF 3. Circuit Breaker H4 (MPU 2 on Panel A) ...........OPEN PNF Warning On Right Hand Panel Only:

1. Right EFD Master Switch ....................................OFF PNF Warning On Both Panels: 1. Both EFD Master & MFD Master Switches .........OFF PF/PNF

E-20


DPU Failure 1. DPU Transfer Switch...................................PRESS PF/PNF (White "ALTN" legend lit)

PFD Failure

1. Relevant PFD to ND Switch ......................... PRESS PF/PNF (White "TO ND" legend lit) If PFD Displayed On ND: CONTINUE IN THIS CONDITION If PFD Not Displayed On ND: 2. Relevant PFD to ND Switch ......................... PRESS PF/PNF (White "TO ND" legend not lit)

3. DPU ALTN Switch........................................ PRESS PF/PNF (White "ALTN" legend lit)

ND Failure 1. ND to MFD Switch..........................................PRESS PF (White "TO MFD" legend lit) If ND Displayed On MFD: CONTINUE IN THIS CONDITION If ND Not Displayed On MFD: 2. ND to MFD Switch..........................................PRESS PF (White "TO MFD" legend out)

3. DPU ALTN Switch..........................................PRESS PF (White "ALTN" legend lit)

Unreliable Airspeed 1. Pitot Isolation Control ................................ ISOLATE RP

Pitot Heat Failure 1. Pitot/Vane Heat Switches (2) .................. CHECK ON PNF

2. Pitot Amps ........................CHECK L & R READINGS PNF

3. Associated Instruments............................. MONITOR PNF

E-21


ELECT ELECTRICAL

Double Generator Failure

1. Panel Lights ...................... EMERGENCY (IF REQD) PNF 2. Battery................................................. EMERGENCY PNF 3. Standby Inverter ..........................ARM/XE FAIL OUT PNF 4. Engine Computers (2)..........................................OFF PNF 5. Engine Anti-Ice (2) ................................................ ON PNF 6. DC Volts.................................................................PE PNF 7. Electrical Loads ......................................... MINIMIZE PNF 8. Emergency Lighting .............................................OFF PNF 9. Circuit Breakers A13, A17, B11, B13, B14 and H19 on Panel A..........................................OPEN PNF 10. Emerg Lighting......... MANUAL, ONLY WHEN REQD PNF

After completing checklist, the following major systems ARE AVAILABLE: (if PE & XE buses are powered):

- STBY ADI with ILS capability (Batt 3 backup) - Pilot's BDI (NO DME) with ADF & VOR capability (from AHRS 2) - #1 NAV Radio (NO DME); Localizer, VOR, MKR BCNS - Pilot's VSI, CSI, ALTIMETER - VHF 1 & UHF 1 - STBY ALTM (Batt 3 backup) - ATC Transponder and IFF - Fuel Qty (L & R) - Altitude Alerter - Lights: Nav, Left Landing Light, Left Wing Taxi Light

IMPACT ON NORMAL PROCEDURES: - No TACAN or DME required approaches - Fly instruments from left seat - Radar ALT is inop - GPWS is unreliable and disabled by pulling H-19, Panel A - FLAP and AIRBRAKE position indicators are inop - Brake supply/pressure gage is inop, but HYD 1/2 LO PRESS,

EMERG BRK LO PRESS and AUX HYD LO LVL lights work - TKS and ICE DETECT are inop - Shot 2 of Fire Ext system is inop

Single Generator Failure 1. Failed Generator.................................................TRIP PNF 2. Bustie ............................................................. CLOSE PNF 3. Generator Amps .......................CHECK BELOW 400 UP TO 10,000 FT OR 330 ABOVE 10,000 FT PNF 4. Volts ...................................... CHECK PSI, PS2 & PE PNF

E-22

BAe 125-800A TI 4040.25C CHG 01, June 1999

Fluctuating / Abnormal Voltage If Fluctuating: 1. Bustie ...............................................................OPEN PNF Continue with Steps 2 thru 5 If Abnormal (Above 29.5 / Below 24.5): 2. DC volts.........................................CHECK PS1, PS2 PNF 3. Affected Generator .............................................TRIP PNF 4. Bustie .............................................................CLOSE PNF 5. Generator Amps....................... CHECK BELOW 400 UP TO 10,000 FT OR 330 ABOVE 10,000 FT PNF

PS2 POWERED CIRCUITS FLIGHT INSTRUMENTS NAV EQUIPMENTRight VSI + Right CSI FMS #2 + DME #2 Right Altimeter Right BDI AP/FD Computer Fan NAV #2 (ILS/VOR/MKR) ANTI-ICE SYSTEMSTKS Pump ICE Detection circuit R Pitot Heat+ Fwd Static Plate Heat Half of Rudder Bias Heat Drain Heater

EFIS As long as PSB1-PSB2 Tie CB (white outline M-10) doesn't trip, Right side EFIS will be powered via the PS1 bus thru PSB1. The #2 ADS will also get power this way.

COMM EQUIPMENT LIGHTSNONE Beacon Right Landing + Taxi Lights STALL WARNING Right Panel Light Right Stall Warning Motor Storm Lights Right MSP Mode Lights INDICATORS Right Reading Light Stby gear indicators Chime SWITCHING CNTRL FOR...Air brake indicator Right Screen Heat Hydr Supply Press gage (bottom)

Aux Cool Pack Auto Cabin Temp Control

Cabin Temperature gauge Flood Flow Valve MISC. AC & PRESSURIZATIONStby Inst Emerg Power Chrg Aux Cool Pack Valve Right Fuel Pump (PE backup) Aux Cool Pack Evaporators Right Rud Bias on/off Valve Aux Cool Pack Annunciator Galley Power Auto Cabin Temp Control 115 V 60 Hz Power Press Reg Control Valve Toilet Flush (airborne) Recirc Fan Wash Basin pump/heater FIRE SYSTEMS FIRE EXT SHOT 2

E-23


E-24

Generators Out Of Balance Generator Amps Differ By More Than 40 Amps: 1. Bustie ................................................................OPEN PNF

2. Gen Amps...........CHECK, PROCEED WITH A OR B PNF A. Higher Load Above 400 Amps Up To 10,000 ft, or 330 Amps Above 10,000 ft: 3. Associated Generator .........................................TRIP PNF

4. Bustie ............................................................. CLOSE PNF

5. Generator Amps .................CHECK BELOW 400 UP TO 10,000 FT OR 330 ABOVE 10,000 FT PNF

6. Electrical Loads ......................SHED AS REQUIRED PNF If Excessive Load Persists: 7. Bustie ................................................................OPEN PNF

CONTINUE FLIGHT with one busbar failed B. Higher Load Below 400 Amps Up To 10,000 ft, or 330 Amps Above 10,000 ft: 3. DC volts ........................................ CHECK PS1, PS2 PNF Proceed with C or D: C. Voltages Normal (24.5 to 29.5): 4. Bustie ............................................................. CLOSE PNF

CONTINUE FLIGHT with out of balance condition

5. DC Volts & Amps ........... MONITOR PERIODICALLY PNF D. One Voltage Abnormal (Outside 24.5 to 29.5): 4. Associated Generator .........................................TRIP PNF

5. Bustie ............................................................. CLOSE PNF

6. Generator Amps .......................CHECK BELOW 400 UP TO 10,000 FT OR 330 ABOVE 10,000 FT PNF 7. Electrical Loads .............................. SHED AS REQD PNF CONTINUE FLIGHT with one busbar failed


Battery Hot If Battery Hot Annunciator Lit: 1. Affected Battery Amps....................................CHECK PNF Proceed with A or B: A. Battery Amps Decreasing: 2. Battery Amps, Temperature .........MONITOR EVERY 5 MINUTES UNTIL WARNING CEASES PNF B. Battery Amps Steady or Increasing: 2. Battery Amps, Temperature .........MONITOR EVERY 5 MINUTES PNF If Amps or emperature Increase: 3. Affected Battery........................................... ISOLATE PNF 4. BATT CNTCTR Annunciators (2).......................... LIT PNF

Battery Overheat If Battery Overheat Annunciator Lit In The Air: 1. Battery .................................................EMERGENCY PNF LAND AS SOON AS PRACTICAL If Battery Overheat Annunciator Lit On The Ground: 1. Battery .................................................................OFF PNF 2. Engines & APU......................................SHUTDOWN PNF 3. External Power (If Connected) ........... DISCONNECT PNF

XE Failure

1. AC Voltmeter ..............................XE, CHECK VOLTS PNF Proceed with A or B: A. XE Supplies Available: NO FURTHER ACTION B. XE Supplies Not Available: 2. Each White, Panel D AC (XE Supplied) Circuit Breakers....................................TRIP, RESET PNF 3. If Tripping Any Circuit Breaker Causes XE FAIL Annunciator To Extinguish .............. DO NOT RESET PNF CONTINUE FLIGHT If XE FAIL persists: 5. Standby Inverter ..................................................OFF PNF CONTINUE FLIGHT

XE FAIL

BATT OVHT

BATT HOT

E-25


XS1 and XE Failure

1. XE BUS PROT Circuit Breaker (A1 on Panel D) ................................................OPEN PNF

2. STBY INV Circuit Breaker (B9 on Panel D) ............................................. CLOSE PNF

3. Standby Inverter .................................................ARM PNF

4. XE FAIL Annunciator ..................................... CHECK PNF Proceed With A or B: A. XE FAIL Annunciator Still Lit: 5. Accomplish XE FAILURE Checklist............................ PNF B. XE FAIL Annunciator Out: 5. XE FAIL BUS PROT Circuit Breaker (A1 on Panel D) ..............................................RESET PNF

6. XS1 FAIL Annunciator ................................... CHECK PNF If XS1 Still Lit: 7. Accomplish XS1 FAILURE Checklist.......................... PNF

XS1 or XS2 Failure

1. AC Voltmeter .................. SET TO FAILED BUSBAR, CHECK VOLTS PNF

XS2 FAIL

XS1 FAIL

XE FAIL

XS1 FAIL

E-26


Double Inverter Failure

1. Inverter 1 ................... SELECT START FOR 30 SEC PNF

2. AC Supply Annunciators ................................CHECK PNF

If XS1 FAIL and INV FAIL Annunciators Still Lit: 3. Inverter 2 ................... SELECT START FOR 30 SEC PNF

CONTINUE FLIGHT

Single Inverter Failure

1. Failed Inverter ................................................ START PNF

Alternator Failure

1. Failed Alternator ................................OFF, THEN ON PNF

If Warning Persists: 2. Alternator.............................................................OFF PNF

CONTINUE FLIGHT

Double Alternator Failure

If both alternators fail, causing total loss of windscreen heating:

1. SCREEN HEAT Switches ........................BOTH OFF PNF

2. Alternators ........ BOTH OFF THEN ON(wait 10 secs) PNF

Proceed with A or B:

A. If either ALTR FAIL light is on: 3. Wait another 20 seconds; SCREEN HEAT........................................ BOTH ON PNF

B. If an ALTR FAIL light is not on: 3. L SCREEN HEAT switch............... ON (wait 10 secs) PNF

4. If ALTR FAIL comes on:

L SCREEN HEAT................................................OFF

ALTERNATOR Switches........BOTH OFF, THEN ON

R SCREEN HEAT .................................................ON PNF

Do not reselect L SCREEN HEAT.

With these switch selections, available power is fed to right ‘A’ screen and left ‘B’ screen.

Continued Next Page

E-27


5. If the L ALTR FAIL light is not on, do not reselect R SCREEN HEAT.

With these switch selections, available power is fed to left ‘A’

screen and right ‘B’ screen.

NOTE

In the case of repeated tripping, repeat resets only if windscreen heat is operationally essential.

ENGINES

High RPM or High ITT 1. Throttle................................................................IDLE PF If Indications Not Controlled Within Limits: 2. Accomplish Engine Fire/Failure/Shutdown ChecklistPNF

Fluctuating RPM 1. Engine Computer................................OVSPD PROT PNF

2. Throttle............ADJUST TO KEEP REQUIRED RPM PF

3. ITT..............................................................MONITOR PNF

High Oil Temperature 1. Accomplish Engine Fire/Failure/.Shutdown Checklist PNF

2. Note Maximum Temperature & Duration.................... PNF

Oil Low Pressure 1. Oil Pressure ...................... CHECK GAGE READING PNF If Below 25 psi: 2. Accomplish Engine Fire/Failure/Shutdown Checklist PNF

OIL LO PRESS

E-28


FLIGHT CONTROLS

E-29

False Stick Shaker / Pusher STALL IDENT

1. STALL IDENT 1 & 2 .........PUSH BOTH TOGETHER PNF If Stick Shake Persists: 2. STALL WARN MOTOR L and R Circuit Breakers (B6/B7 on Panel D)................OPEN PNF

CONTINUE FLIGHT WITH CAUTION

Electric Pitch Trim Runaway 1. Control Column ........................................RESTRAIN PF

2. Trim Wheel ...............................................RESTRAIN PF

3. Autopilot ................................................DISENGAGE PF

4. Trim Switch................................................OPERATE PF

5. ELECT PITCH TRIM Circuit Breaker (B10 on Panel D)..............................................OPEN PNF

Autopilot Trim Warnings 1. PFD Mistrim Warning .........CK A OR E INDICATION PF

2. Appropriate Trim Wheel ..............ZERO AUTOPILOT OUT OF TRIM INDICATION PF If Mistrim Indication Still Present: 3. Autopilot ................................................DISENGAGE PF

Anticipate heavy out-of-trim loads


FUEL

Auxiliary Fuel Transfer Failure 1. Wing Fuel Contents ....................................... CHECK PNF Wing Fuel Contents Decreasing: LAND AS SOON AS POSSIBLE Wing Contents Increasing: CONTINUE FLIGHT

Fuel Low Pressure 1. Wing Fuel/X Feed/Transfer Valve .................X FEED PNF

2. FUEL LO PRESS Annunciator ............. CHECK OUT PNF

3. Failed Fuel Pump.................................................OFF PNF Ventral Tank Not Empty: 4. Aux Fuel Transfer Valve ...... SELECT OPEN/CLOSE TO MAINTAIN WING FUEL BALANCE WITHIN 500 LBS PNF Ventral Tank Empty: 4. Wing Fuel/X Feed/Transfer Valve ......... TRANSFER, THEN X FEED ALTERNATELY PNF

Engine Fuel Malfunction 1. Throttle................................. REDUCE TO MINIMUM POWER TO COMPLETE FLIGHT PF If Warning Persists, Accompanied By Engine Malfunction: 2. Accomplish Engine Fire/Failure/Shutdown Checklist PNF

FUEL

E-30


HYDRAULICS

Hydraulic Low Pressure CONTINUE FLIGHT

Main Hydraulic Failure CONTINUE FLIGHT Landing Gear and Flaps Lowering: 1. Aux Hyd System Handle .....PULL (DO NOT RESET) PNF 2. Aux Hyd Pump Handle.................. OPERATE UNTIL GEAR DOWN/LIGHTS ON PNF 3. Gear ................................................................DOWN PF/PNF 4. Flaps.................................................................... SET PF/PNF 5. Aux Hyd Pump Handle.................. OPERATE UNTIL DESIRED FLAP POSITION ACHIEVED PNF Before Landing: 6. Brake Lever ............................... LEAVE IN NORMAL (FORWARD) POSITION PNF Actions On Landing: 7. Wheelbrakes ................................... APPLY GENTLY PF

WARNING Do not dissipate brake pressure needlessly by applying brakes with pumping action. Apply slow steady pressure.

If Normal Braking Fails: 8. Brake Pedals ..............................................RELEASE PF 9. Brake Lever ...................................................EMERG PF

WARNING Do not set wheel brake to PARK position when setting lever to EMER as this will cause the brakes to lock and possible tire failure

10. Brake Pedals ................................... APPLY GENTLY PF 11. Steering ........... USE FLIGHT CONTROLS, BRAKES PF

HYD LO PRESS

E-31

TI 4040.25C BAe 125-800A CHG 01, June 1999

E-32

Hydraulic System Overheat HYD OVHT

CONTINUE FLIGHT

WINDSCREEN

Windscreen Overheat 1. Screen Heat Switch.............OFF, THEN ON PNF CONTINUE FLIGHT

Sidescreen Overheat 1. L or R Screen Heat Switch .............. OFF, THEN ON TO IDENTIFY AFFECTED SCREEN PNF CONTINUE FLIGHT

Windscreen Failure Outer Acrylic Single Crack: 1. Screen Heat .......................................... OFF PN

BAe 125-800A TI 4040.25C CHG 01, June 1999

PERFORMANCE

TEMPERATURE CONVERSION TABLE P-iii

TABULATED TAKEOFF DATA P-1

SINGLE ENGINE NET GRADIENT REQUIRED P-1

FLAPS 15° - APR P-2

FLAPS 0° - APR P-5

TAKEOFF REFERENCE N1% - ENG ANTICE OFF P-8

TAKEOFF REFERENCE N1% - ENG ANTICE ON P-9

TAKEOFF REFERENCE N1% - LOW PRESS ALTITUDES P-10

MAXIMUM CRUISE N1% P-11

MAX TAKEOFF WEIGHT FOR CRUISING ALTITUDE P-12

MIN CRUISING SPEED AND MAX CRUISING ALTITUDE P-13

MAXIMUM CRUISING WEIGHT P-14

MAX ALTITUDE FOR MAX LIFT COEFFICIENT P-15

INTERMEDIATE SPEED CRUISE P-16

LONG RANGE CRUISE SPEED P-23

SHORT RANGE AND DIVERSION FUEL AND TIME P-26

HOLDING ON TWO ENGINES (ANTI-ICING OFF) P-27

HOLDING IN ICING CONDITIONS P-28

WIND COMPONENT P-29

SUMMARY OF SINGLE-ENGINE CEILINGS DRIFT DOWN P-30

P-i


This Page Intentionally Left Blank

P-ii


TEMPERATURE CONVERSION TABLE °F - °C °F - °C °F - °C

-148.0 -146.2 -144.4 -142.6 -140.8

-100 -99 -98 -97 -96

-73.3 -72.8 -72.2 -71.7 -71.1

5.0 6.8 8.6

10.4 12.2

-15 -14 -13 -12 -11

-26.1 -25.6 -25.0 -24.4 -23.9

158.0 159.8 161.6 163.4 165.2

70 71 72 73 74

21.1 21.7 22.2 22.8 23.3

-139.0 -137.2 -135.4 -133.6 -131.8

-95 -94 -93 -92 -91

-70.6 -70.0 -69.4 -68.9 -68.3

14.0 15.8 17.6 19.4 21.2

-10 -9 -8 -7 -6

-23.3 -22.8 -22.2 -21.7 -21.1

167.0 168.8 170.6 172.4 174.2

75 76 77 78 79

23.9 24.4 25.0 25.6 26.1

-130.0 -128.2 -126.4 -124.6 -122.8

-90 -89 -88 -87 -86

-67.8 -67.2 -66.7 -66.1 -65.6

23.0 24.8 26.6 28.4 30.2

-5 -4 -3 -2 -1

-20.6 -20.0 -19.4 -18.9 -18.3

176.0 177.8 179.6 181.4 183.2

80 81 82 83 84

26.7 27.2 27.8 28.3 28.9

-121.0 -119.2 -117.4 -115.6 -113.8

-85 -84 -83 -82 -81

-65.0 -64.4 -63.9 -63.3 -62.8

32.0 33.8 35.6 37.4 39.2

0 1 2 3 4

-17.8 -17.2 -16.7 -16.1 -15.6

185.0 186.8 188.6 190.4 192.2

85 86 87 88 89

29.4 30.0 30.6 31.1 31.7

-112.0 -110.2 -108.4 -106.6 -104.8

-80 -79 -78 -77 -76

-62.2 -61.7 -61.1 -60.6 -60.0

41.0 42.8 44.6 46.4 48.2

5 6 7 8 9

-15.0 -14.4 -13.9 -13.3 -12.8

194.0 195.8 197.6 199.4 201.2

90 91 92 93 94

32.2 32.8 33.3 33.9 34.4

-103.0 -101.2 -99.4 -97.6 -95.8

-75 -74 -73 -72 -71

-59.4 -58.9 -58.3 -57.8 -57.2

50.0 51.8 53.6 55.4 57.2

10 11 12 13 14

-12.2 -11.7 -11.1 -10.6 -10.0

203.0 204.8 206.6 208.4 210.2

95 96 97 98 99

35.0 35.6 36.1 36.7 37.2

-94.0 -92.2 -90.4 -88.6 -86.8

-70 -69 -68 -67 -66

-56.7 -56.1 -55.6 -55.0 -54.4

59.0 60.8 62.6 64.4 66.2

15 16 17 18 19

-9.4 -8.9 -8.3 -7.8 -7.2

212.0 213.8 215.6 217.4 219.2

100 101 102 103 104

37.8 38.3 38.9 39.4 40.0

-85.0 -83.2 -81.4 -79.6 -77.8

-65 -64 -63 -62 -61

-53.9 -53.3 -52.8 -52.2 -51.7

68.0 69.8 71.6 73.4 75.2

20 21 22 23 24

-6.7 -6.1 -5.6 -5.0 -4.4

221.0 222.8 224.6 226.4 228.2

105 106 107 108 109

40.6 41.1 41.7 42.2 42.8

-76.0 -74.2 -72.4 -70.6 -68.8

-60 -59 -58 -57 -56

-51.1 -50.6 -50.0 -49.4 -48.9

77.0 78.8 80.6 82.4 74.2

25 26 27 28 29

-3.9 -3.3 -2.8 -2.2 -1.7

230.0 231.8 233.6 235.4 237.2

110 111 112 113 114

43.3 43.9 44.4 45.0 45.6

-67.0 -65.2 -63.4 -61.6 -59.8

-55 -54 -53 -52 -51

-48.3 -47.8 -47.2 -46.7 -46.1

86.0 87.8 89.6 91.4 93.2

30 31 32 33 34

-1.1 -0.6 0.0 0.6 1.1

239.0 240.8 242.6 244.4 246.2

115 116 117 118 119

46.1 46.7 47.2 47.8 48.3

-58.0 -56.2 -54.4 -52.6 -50.8

-50 -49 -48 -47 -46

-45.6 -45.0 -44.4 -43.9 -43.3

95.0 96.8 98.6

100.4 102.2

35 36 37 38 39

1.7 2.2 2.8 3.3 3.9

248.0 249.8 251.6 253.4 255.2

120 121 122 123 124

48.9 49.4 50.0 50.6 51.1

-49.0 -47.2 -45.4 -43.6 -41.8

-45 -44 -43 -42 -41

-42.8 -42.2 -41.7 -41.1 -40.6

104.0 105.4 107.6 109.4 111.2

40 41 42 43 44

4.4 5.0 5.6 6.1 6.7

257.0 258.8 260.6 262.4 264.2

125 126 127 128 129

51.7 52.2 52.8 53.3 53.9

-40.0 -38.2 -36.4 -34.6 -32.8

-40 -39 -38 -37 -36

-40.0 -39.4 -38.9 -38.3 -37.8

113.0 114.8 116.6 118.4 120.2

45 46 47 48 49

7.2 7.8 8.3 8.9 9.4

266.0 267.8 269.6 271.4 273.2

130 131 132 133 134

54.4 55.0 55.8 56.1 57.7

-31.0 -29.2 -27.4 -25.6 -23.8

-35 -34 -33 -32 -31

-37.2 -36.7 -36.1 -35.6 -35.0

122.0 123.8 125.6 127.4 129.2

50 51 52 53 54

10.0 10.6 11.1 11.7 12.2

275.0 276.8 278.6 280.4 282.2

135 136 137 138 139

57.2 57.3 58.3 58.9 59.4

-22.0 -20.2 -18.4 -16.6 -14.8

-30 -29 -28 -27 -26

-34.4 -33.9 -33.3 -32.8 -32.2

131.0 132.8 134.6 136.4 138.2

55 56 57 58 59

12.8 13.3 13.9 14.4 15.0

284.0 285.8 287.6 289.4 291.2

140 141 142 143 144

60.0 60.6 61.1 61.7 62.2

-13.0 -11.2 -9.4 -7.6 -5.8

-25 -24 -23 -22 -21

-31.7 -31.1 -30.6 -30.0 -29.4

140.0 141.8 143.6 145.4 147.2

60 61 62 63 64

15.6 16.1 16.7 17.2 17.8

293.0 294.8 296.6 298.4 300.2

145 146 147 148 149

62.8 63.3 63.9 64.4 65.0

-4.0 -2.2 -0.4 1.4 3.2

-20 -19 -18 -17 -16

-28.9 -28.3 -27.8 -27.2 -26.7

149.0 150.8 152.6 154.4 156.2

65 6

67 68 69

18.3 18.9 19.4 20.0 20.6

P-iii

TI 4040.25C BAe 125-800A CHG 01, June 1999

EFFECT OF RUNWAY CONDITION READING ON

ACCELERATE - STOP DISTANCE

P-iv


TABULATED TAKEOFF DATA

1. Enter with pressure altitude (round up to next higher). 2. Do not use with tailwind or up slope. 3. Do not interpolate horizontally or vertically between boxes

or between numbers within shaded areas. 4. "Distance" is paved runway length only. 5. The lowest temperature for each altitude is ISA. 6. The highest temperature shown in the shaded area in

each block is either the WAT limit or the temperature determined by a distance of 8,400 feet, below which brake energy limitations will not apply. For distances exceeding 8,400 feet, brake energy may be limiting, and V1 may be lower than VR; for these cases the Flight Manual graphs must be used.

7. The second temperature in the shaded area (15° takeoff) is that at which VR and V2 start to rise sharply, or ISA if higher. Within the shaded area tabulation is not sufficiently accurate for interpolation; refer to the Flight Manual.

8. When engine anti-ice is used, add 10° to the actual temperature before entering the table.

SINGLE ENGINE NET GRADIENT REQUIRED

OBSTACLE HEIGHT. X 100 = % GRADIENT DIST TO OBSTACLE

97 ft = 1.6% 6076 ft = 1 NM

ft/nm 146 150 200 250 300 350 375 400 425 450 500 %Grad 2.4 2.5 3.3 4.1 4.9 5.8 6.2 6.6 7.1 7.4 8.3

TEMPERATURE CONVERSION TABLE °C -40 -35 -30 -25 -20 -15 -10 -5 0 5 °F -40 -31 -22 -13 -4 5 14 23 32 41

°C 10 15 20 25 30 35 40 45 50 55 °F 50 59 68 77 86 95 104 113 122 131

P-1


FLAPS 15° - APR

ZERO WIND AND GRADIENT V1 = VR

A/C Wt lb 28,000 27,000 26,000 PRESS ALT - ft

OAT °C

Dist ft

VR kt

V2 kt

OAT °C

Dist ft

VR kt

V2 kt

OAT°C

Distft

VR kt

V2 kt

15 8400 135 136

6000 7 8400 138 140 11 8400 137 138 14 7960 133 134 6 8100 136 138 10 8050 134 136 10 7260 132 134 3 7600 136 138 3 7020 134 136 3 6540 132 134 15 8400 137 138 19 8400 135 137

5000 12 8400 139 141 14 7770 134 136 18 7800 133 134 10 7900 136 138 10 7160 134 136 10 6620 132 134 5 7150 136 138 5 6630 134 136 5 6210 132 134 24 8400 137 138 17 8400 141 143 20 8400 139 140 22 7610 133 134

4000 15 7850 136 138 18 7610 134 136 20 7240 133 134 10 7050 136 138 10 6520 135 136 10 6110 132 134 7 6800 136 138 7 6300 133 136 7 5930 132 134 22 8400 143 145 24 8400 139 141 28 8400 139 140

3000 19 7700 136 138 22 7560 135 136 26 7550 133 134 15 7000 136 138 20 7140 134 136 20 6550 132 134 9 6400 135 138 9 6010 133 136 9 5650 131 134 26 8400 146 148 28 8400 140 141 32 8400 140 142

2000 23 7600 136 138 26 7450 134 136 29 7270 133 134 20 7050 136 138 20 6460 134 136 20 6040 132 134 11 6200 135 138 11 5830 133 136 11 5500 131 134 35 8400 139 141 30 8400 148 150 32 8400 143 144 32 7000 133 134

1000 26 7350 136 138 29 7200 134 136 30 6660 133 134 20 6450 136 138 20 5990 134 136 20 5640 132 134 13 6100 135 138 13 5730 133 136 13 5400 131 134 33 8400 148 151 35 8400 142 144 39 8300 143 145 30 7350 136 138 33 7180 134 136 36 7030 133 134

S-L 25 6550 136 138 30 6600 134 136 30 6120 132 134 20 6050 136 138 20 5750 133 136 20 5400 131 134 15 5950 135 138 15 5690 133 136 15 5340 131 134

VFTO kt

170

169

166

VERC

kt

187

183

180

VREF

kt

142

140

138

1. When data is in shaded area refer to Flight Manual performance graphs;

either WAT limited, brake energy limited, or tabulation not sufficiently accurate.

2. When ice prevention bleeds are in use add 10 deg C to the actual air temperature before entering the table.

3. Distances are balanced field length or greater.

P-2


FLAPS 15° - APR



OAT°C

Distft

VR kt

V2 kt

OAT°C

Dist ft

VR kt

V2 kt

OAT°C

Distft

VR kt

V2 kt

23 8400 131 132 28 8400 130 132 19 8400 133 135 22 7660 128 130 26 7430 126 127

6000 18 7800 131 132 20 7280 128 130 20 6550 125 127 10 6630 130 132 10 6130 127 130 10 5640 124 127 3 6100 129 132 33 5650 127 130 3 5260 124 127 23 8400 134 135 27 8400 131 132 32 8400 132 134 22 7600 131 132 26 7550 128 130 30 7310 126 127

5000 20 7270 131 132 20 6590 128 130 20 6000 125 127 10 6130 130 132 10 5690 127 130 10 5270 124 127 5 5790 129 132 5 5400 127 130 5 5030 124 127 36 8400 133 135 27 8400 133 135 31 8400 131 133 33 7020 126 127

4000 26 7480 131 132 29 7260 128 130 30 6600 125 127 20 6580 130 132 20 6040 128 130 20 5560 125 127 10 5700 129 132 10 5330 127 130 10 4970 124 127 7 5530 129 132 7 5200 126 130 7 4820 123 127 35 8400 134 135 39 8400 133 135 31 8400 135 137 33 7240 128 130 37 7000 126 127

3000 29 7210 131 132 30 6650 128 130 30 6050 125 127 20 6040 130 132 20 5620 127 130 20 5200 124 127 9 5330 129 132 9 5000 126 130 9 4660 123 127 35 8400 137 139 39 8350 137 139 43 8400 136 139 33 7170 131 132 36 7000 128 130 40 6900 126 127

2000 30 6650 130 132 30 6070 128 130 30 5600 125 127 20 5620 129 132 20 5260 127 130 20 4940 124 127 11 5150 129 132 11 4830 126 130 11 4510 123 127 45 7480 132 134 38 8400 136 138 42 8130 137 139 43 6730 126 127

1000 36 7000 131 132 39 6810 128 130 40 6240 125 127 30 6110 130 132 30 5660 127 130 30 5230 124 127 20 5310 129 132 20 4960 126 130 20 4660 123 127 13 5100 129 132 13 4790 126 130 13 4500 123 127 45 7950 138 140 48 7500 132 134 42 8250 140 143 43 6830 130 131 46 6570 126 127

S-L 39 6810 131 132 40 6320 128 130 40 5760 125 127 30 5700 130 132 30 5320 127 130 30 4950 124 127 20 5100 129 132 20 4790 126 130 20 4500 123 127 15 5000 129 132 15 4700 126 130 15 4410 123 127

VFTO kt

164

160

157

VERC

kt

176

172

168

VREF

kt

136

133

130





P-3


FLAPS 15° - APR



OAT °C

Dist ft

VR kt

V2 kt

OAT°C

Dist ft

VR kt

V2 kt

OAT°C

Distft

VR kt

V2 kt

36 7650 124 125 32 8400 127 129 34 6970 120 121 38 6520 117 118

6000 30 7230 123 124 30 6400 120 121 30 5760 116 118 20 5870 122 124 20 5460 119 121 20 5200 115 118 10 5200 121 124 10 4950 118 121 10 4800 114 118 3 4850 121 124 3 4700 117 121 3 4560 117 121 36 8120 129 130 39 7320 123 124 34 7140 123 124 38 6940 120 121 40 6250 117 118

5000 30 6510 123 124 30 5830 119 121 30 5440 116 118 20 5530 122 124 20 5140 118 121 20 4970 115 118 10 4900 121 124 10 4700 117 121 10 4560 117 121 5 4700 120 124 5 4540 119 123 5 4400 119 123 40 8300 131 133 42 7080 122 124 42 6040 117 118 37 6860 123 124 41 6730 120 121 40 5810 117 118

4000 30 5960 122 124 30 5440 119 121 30 5150 116 118 20 5150 121 125 20 4860 118 121 20 4700 115 118 10 4630 120 124 10 4500 119 123 10 4360 119 123 7 4550 121 125 7 4400 121 125 7 4270 121 125 43 8100 132 134 44 6550 120 121 44 5730 117 118 40 6730 123 124 40 5970 120 121 40 5470 116 118

3000 30 5540 122 124 30 5110 119 121 30 4910 115 118 20 4860 121 124 20 4630 118 121 20 4500 116 119 9 4400 122 126 9 4220 122 126 9 4140 122 126 46 7900 130 132 43 6510 123 124 46 6250 123 121 46 5600 117 118

2000 40 6130 123 124 40 5550 119 121 40 5190 116 118 30 5170 122 124 30 4890 118 121 30 4700 115 118 20 4600 121 124 20 4460 118 122 20 4310 122 126 11 4260 122 126 11 4150 122 126 11 4030 121 126 48 7180 127 128 46 6460 123 124 48 5960 120 121 48 5400 116 118

1000 40 5660 122 124 40 5200 119 121 40 4940 116 118 30 4860 121 124 30 4630 118 121 30 4500 114 118 20 4400 120 124 20 4300 120 124 20 4160 120 124 13 4300 122 126 13 4150 122 126 13 4020 122 126 50 6700 124 126 49 6370 123 124 50 5850 120 121 50 5290 116 118

S-L 40 5300 122 124 40 4910 119 121 40 4720 115 118 30 4600 121 124 30 4450 117 121 30 4340 116 120 20 4260 122 126 20 4110 122 126 20 4030 122 126 15 4210 122 126 15 4090 122 126 15 3970 122 126

VFTO kt

154

150

146

VERC

kt

164

159

155

VREF

kt

128

125

122

1. When data is in shaded area refer to Flight Manual performance graphs; either WAT limited, brake energy limited, or tabulation not sufficiently accurate.



P-4


FLAPS 0° - APR



OAT°C

Distft

VRkt

V2 kt

OAT°C

Dist ft

VR kt

V2 kt

OAT°C

Distft

VR kt

V2kt

13 8400 142 144

6000 4 8400 145 148 8 8400 144 146 10 7970 142 144 3 8350 145 148 3 7830 144 146 3 7340 141 144 14 8400 144 146 19 8400 142 144

5000 10 8400 145 148 10 7930 144 146 10 7420 142 144 5 7950 145 148 5 7460 143 146 5 7010 141 144 24 8400 143 144

4000 16 8400 146 148 19 8400 144 146 20 7860 142 144 10 7900 145 148 10 7390 143 146 10 6920 141 144 7 7650 145 148 7 7140 143 146 7 6650 141 144 20 8400 146 148 24 8400 144 146 29 8400 143 144

3000 15 7850 145 148 20 7770 144 146 20 7290 142 144 9 7250 144 148 9 6770 142 146 9 6380 140 144 33 8400 144 144

2000 25 8400 146 148 29 8400 144 146 30 7860 142 144 20 7850 145 148 20 7240 143 146 20 6800 141 144 11 7000 144 148 11 6510 142 146 11 6100 140 144 30 8400 146 148 33 8400 144 146 37 8400 143 144

1000 25 7800 145 148 30 7760 144 146 30 7230 142 144 20 7250 145 148 20 6740 143 146 20 6330 141 144 13 6800 144 148 13 6450 142 146 13 6070 140 144 41 8400 143 144 34 8400 146 148 37 8400 144 146 40 8100 143 144

S-L 30 7900 146 148 30 7230 144 146 30 6770 142 144 20 6800 144 148 20 6400 142 146 20 6000 140 144 15 6700 144 148 15 6300 142 146 15 5930 140 144

VFTO kt

170

169

166

VERC

kt

187

183

180

VREF

kt

142

140

138





P-5


FLAPS 0° - APR


A/C Wt lb

25,000 24,000 23,000 PRESS ALT - ft

OAT °C

Dist ft

VR kt

V2 kt

OAT °C

Dist ft

VR kt

V2kt

OAT°C

Dist ft

VRkt

V2kt

23 8400 138 139 28 8400 135 136

6000 18 8400 140 142 20 7880 137 139 20 7250 134 136 10 7400 139 142 10 6850 139 139 10 6370 133 136 3 6830 139 142 3 6370 139 139 3 5890 132 136 33 8350 135 136 24 8400 140 142 28 8400 138 139 30 7860 135 136

5000 20 7860 140 142 20 7250 137 139 20 6720 133 136 10 6910 139 142 10 6440 136 139 10 5970 132 136 5 6540 138 142 5 6110 135 139 5 5660 131 136 33 8400 138 139 37 8259 135 136 28 8400 140 142 30 7860 138 139 30 7200 134 136

4000 20 7300 139 142 20 6750 136 139 20 6270 133 136 10 6470 138 142 10 6000 135 139 10 5580 132 136 7 6280 138 142 7 5810 135 139 7 5400 131 136 33 8400 140 142 37 8270 138 139 40 7970 135 136

3000 30 7840 140 142 30 7210 137 139 30 6690 134 136 20 6800 139 142 20 6300 136 139 20 5850 132 136 9 5970 138 142 9 5550 134 139 9 5160 131 136 41 8270 138 139 43 7760 135 136 37 8400 140 142 40 8060 138 139 40 7310 135 136

2000 30 7260 140 142 30 6750 137 139 30 6270 133 136 20 6340 139 142 20 5910 135 139 20 5480 132 136 11 5700 138 142 11 5300 134 139 11 4900 131 136 41 8250 141 142 44 8030 138 139 46 7550 135 136 40 8080 141 142 40 7350 138 139 40 6750 134 136

1000 30 6750 139 142 30 6300 136 139 30 5840 133 136 20 5930 138 142 20 5500 135 139 20 5110 131 136 13 5670 138 142 13 5260 134 139 13 4900 131 136 44 8160 141 142 47 7930 138 139 49 7470 135 136 40 7400 140 142 40 6850 137 139 40 6320 134 136

S-L 30 6320 139 142 30 5880 136 139 30 5450 132 136 20 5610 138 142 20 5200 134 139 20 4870 131 136 15 5540 138 142 15 5140 134 139 15 4800 131 136

VFTO kt

164

160

157

VERC

kt

176

172

168

VREF

kt

136

133

130





P-6


FLAPS 0° - APR



OAT°C

Distft

VRkt

V2 kt

OAT°C

Dist ft

VR kt

V2 kt

OAT°C

Distft

VRkt

V2kt

33 8210 132 133 36 7710 128 130 38 7160 125 126 30 7730 131 133 30 7000 128 130 30 6400 124 126

6000 20 6670 130 133 20 6090 127 130 20 5580 123 126 10 5880 129 133 10 5390 125 130 10 4900 121 126 3 5400 128 133 3 4970 125 130 3 4800 120 126 36 7930 132 133 39 7460 128 130 40 6840 125 126 30 7120 131 133 30 6490 128 130 30 5950 124 126

5000 20 6200 130 133 20 5700 126 130 20 5200 122 126 10 5500 129 133 10 5020 125 130 10 4730 121 126 5 5200 128 133 5 4800 124 130 5 4560 121 127 42 7270 128 130 42 6600 125 126 40 7820 132 133 40 7020 128 130 40 6400 124 126

4000 30 6600 131 133 30 6060 127 130 30 5540 123 126 20 5800 129 133 20 5320 126 130 20 4860 122 126 10 5120 128 133 10 4750 124 130 10 4560 120 127 7 4950 128 133 7 4600 124 130 7 4450 122 128 43 7590 132 133 44 6960 128 130 44 6340 124 126 40 7180 131 133 40 6530 128 130 40 5950 124 126

3000 30 6160 130 133 30 5660 127 130 30 5170 123 126 20 5400 129 133 20 4960 125 130 20 4600 121 126 9 4750 127 133 9 4410 124 130 9 4300 124 130 46 7390 132 133 46 6610 128 130 46 6100 124 126 40 6660 131 133 40 6090 127 130 40 5570 124 126

2000 30 5760 130 133 30 5310 126 130 30 4850 122 126 20 5050 128 133 20 4660 124 130 20 4450 120 126 11 4540 127 133 11 4220 124 130 11 4110 124 130 48 7110 132 133 48 6440 128 130 48 5900 124 126 40 6210 131 133 40 5700 127 130 40 5210 123 126

1000 30 5380 129 133 30 4960 125 130 30 4520 121 126 20 4730 128 133 20 4350 124 130 20 4240 122 128 13 4540 127 133 13 4200 124 130 13 4090 124 130 50 6830 132 133 50 6230 128 130 50 5700 124 126 40 5830 130 133 40 5350 127 130 40 4900 123 126

S-L 30 5020 129 133 30 4650 125 130 30 4370 121 126 20 4500 127 133 20 4180 124 130 20 4060 124 130 15 4450 127 133 15 4130 124 130 15 4020 124 130

VFTO kt

154

150

146

VERC

kt

164

159

155

VREF

kt

128

125

122





P-7


P-8


P-9


P-10


P-11


P-12


P-13


P-14


MAXIMUM ALTITUDE FOR MAXIMUM DEMONSTRATED

LIFT COEFFICIENT

P-15


INTERMEDIATE SPEED CRUISE

5000 FT

CRUISING WEIGHT

(LB)

TEMP. REL. TO ISA (DEG C) AMBIENT TEMP. (DEG C) O.A.T GAUGE (DEG C)

-20 -15 -7

-15 -10 -2

-10 -5 3

-5 0 8

0 5

13

5 10 18

10 15 23

15 20 29

20 25 34

26000 T.A.S. (KT) TOTAL FUEL FLOW (LB/HR) I.A.S. (KT)

283 1850 280

286 1900 280

289 1900 280

291 1900 280

294 1950280

297 1950280

299 2000280

302 2000280

304 2050280


283 1850 280

286 1850 280

289 1850 280

291 1900 280

294 1900280

297 1950280

299 1950280

302 2000280

304 2000280


283 1800 280

286 1800 280

289 1850 280

291 1850 280

294 1900280

297 1900280

299 1950280

302 1950280

304 2000280


283 1750 280

286 1800 280

289 1800 280

291 1850 280

294 1850280

297 1850280

299 1900280

302 1900280

304 1950280


283 1750 280

286 1750 280

289 1800 280

291 1800 280

294 1850280

297 1850280

299 1850280

302 1900280

304 1900280

9C411

7000 FTCRUISING WEIGHT

(LB)


-20 -19 -11

-15 -14 -6

-10 -9 -1

-5 -4 5

0 1

10

5 6

15

10 11 20

15 16 25

20 21 30


291 1850 280

294 1850 280

297 1900 280

300 1900 280

303 1900280

305 1950280

308 1950280

311 2000280

314 2050280


291 1850 280

294 1800 280

297 1850 280

300 1850 280

303 1900280

305 1900280

308 1950280

311 1950280

314 2000280


291 1750 280

294 1800 280

297 1800 280

300 1850 280

303 1850280

305 1900280

308 1900280

311 1950280

314 1950280


291 1750 280

294 1750 280

297 1800 280

300 1800 280

303 1850280

305 1850280

308 1850280

311 1900280

314 1900280


283 1700 280

294 1750 280

297 1750 280

300 1800 280

303 1800280

305 1850280

308 1850280

311 1900280

314 1900280

9C412


(LB)


-20 -23 -14

-15 -18 -9

-10 -13 4

-5 -8 1

0 -3 6

5 2

11

10 7

17

15 12 22

20 17 27


300 1800 280

303 1800 280

306 1850 280

309 1850 280

312 1900280

315 1900280

318 1950280

320 1950280

323 2000280


300 1750 280

303 1800 280

306 1800 280

309 1850 280

312 1850280

315 1900280

318 1900280

320 1950280

323 1950280


300 1750 280

303 1750 280

306 1800 280

309 1800 280

309 1850280

315 1850280

318 1900280

320 1900280

323 1950280


300 1700 280

303 1750 280

306 1750 280

309 1800 280

309 1800280

315 1850280

318 1850280

320 1850280

323 1900280


300 1700 280

303 1700 280

306 1750 280

309 1750 280

309 1800280

315 1800280

318 1850280

320 1850280

323 1900280

9C413

P-16



11000 FT

CRUISING WEIGHT

LB)

TEMP. REL. TO ISA (DEG C)AMBIENT TEMP. (DEG C)O.A.T GAUGE (DEG C)

-20 -27 -18

-15 -22 -13

-10 -17 -8

-5 -12 -2

0 -7 3

5 -2 8

10 3

13

15 8

18

20 13 24

26000 T.A.S. (KT)TOTAL FUEL FLOW (LB/HR)I.A.S. (KT)

309 1800280

312 1800 280

315 1850 280

318 1850 280

321 1850280

324 1900280

327 1900280

330 1950280

333 2000 280


309 1750280

312 1750 280

315 1800 280

318 1800 280

321 1850280

324 1850280

327 1900280

330 1900280

333 1950 280


309 1700280

312 1750 280

315 1750 280

318 1800 280

321 1800280

324 1850280

327 1850280

330 1900280

333 1900 280


309 1700280

312 1700 280

315 1750 280

318 1750 280

321 1800280

324 1800280

327 1850280

330 1850280

333 1900 280


309 1650280

312 1700 280

315 1700 280

318 1750 280

321 1750280

324 1800280

327 1800280

330 1850280

333 1850 280

9C414


(LB)


-20 -31 -21

-15 -26 -16

-10 -21 -11

-5 -16 -6

0 -11 -1

5 -6 5

10 -1 10

15 4

15

20 9

20 26000 T.A.S. (KT)

TOTAL FUEL FLOW (LB/HR)I.A.S. (KT)

318 1750280

321 1800 280

324 1800 280

327 1850 280

330 1850280

334 1900280

337 1900280

340 1900280

343 1950280


318 1700280

321 1750 280

324 1750 280

327 1800 280

330 1800280

334 1850280

337 1850280

340 1900280

343 1900280


318 1700280

321 1700 280

324 1750 280

327 1750 280

330 1800280

334 1800280

337 1850280

340 1850280

343 1900280


318 1650280

321 1700 280

324 1700 280

327 1750 280

330 1750280

334 1800280

337 1800280

340 1850280

343 1850280


318 1650280

321 1650 280

324 1700 280

327 1700 280

330 1750280

334 1750280

337 1800280

340 1800280

343 1850280

9C415


(LB)


-20 -35 -25

-15 -30 -20

-10 -2

-14

-5 -20 -8

0 -15 -4

5 -10 1

10 -5 6

15 0

12

20 5

17 26000 T.A.S. (KT)


327 1750280

330 1750 280

334 1800 280

337 1800 280

340 1850280

344 1850280

347 1900280

350 1900280

353 1900280


327 1700280

330 1700 280

334 1750 280

337 1750 280

340 1800280

344 1800280

347 1850280

350 1850280

353 1900280


327 1650280

330 1700 280

334 1700 280

337 1750 280

340 1750280

344 1800280

347 1800280

350 1850280

353 1850280


327 1650280

330 1650 280

334 1700 280

337 1700 280

340 1750280

344 1750280

347 1800280

350 1800280

353 1800280


327 1600280

330 1650 280

334 1650 280

337 1700 280

340 1700280

344 1750280

347 1750280

350 1800280

353 1800280

9C416

P-17




(LB)


-20 -39 -28

-34 -23

-10 -29 -18

-5 -24 -12

0 -19 -7

5 -14 -2

10 -9 3

15 -4 8

20 5

14 26000 T.A.S. (KT)

TOTAL FUEL FLOW (LB/HR) I.A.S. (KT)

337 1700 280

1750

-15

341 344 348 351 354 358 361 365 1750 1800 1800 1850 1850 1900 1900

280 280 280 280 280 280 280 280 24000 T.A.S. (KT)

TOTAL FUEL FLOW (LB/HR) I.A.S. (KT)

337 1650 280

341 1700 280

344 1700 280

348 1750 280

351 1750280

354 1800280

358 1800280

361 1850280

1850280


337

280

365

1650 341 1650 280

344 1700 280

348 1700 280

351 1750280

354 1750280

358 1800280

361 1800280

365 1850280


337 1600 280

341 1650 280

344 1650 280

348 1700 280

351 1700280

354 1750280

358 1750280

361 1750280

365 1800280


337 1600 280

341 1600 280

344 1650 280

348 1650 280

351 1700280

354 1700280

358 1750280

361 1750280

365 1750280

9C417


(LB)


-20 -43 -31

-15 -38 -26

-10 -33 -21

-5 -28 -16

0 -23 -10

5 -18 -5

10 -13 0

15 -8 5

20 -3 11


348 1700 280

351 1700 280

355 1750 280

359 1750 280

362 1800280

366 1800280

369 1850280

373 1850280

377 1900280


348 1650 280

351 1700 280

355 1700 280

359 1750 280

362 1750280

366 1750280

369 1800280

373 1800280

377 1850280


348 1600 280

351 1650 280

355 1650 280

359 1700 280

362 1700280

366 1750280

369 1750280

373 1800280

377 1800280


348 1600 280

351 1600 280

355 1650 280

359 1650 280

362 1700280

366 1700280

369 1750280

373 1750280

377 1800280


348 1550 280

351 1600 280

355 1600 280

359 1650 280

362 1650280

366 1700280

369 1700280

373 1750280

377 1750280

9C418


(LB)


-20 -47 -35

-15 -42 -29

-10 -37 -24

-5 -32 -19

0 -27 -14

5 -22 -8

10 -17 -3

15 -12 2

20 -7 7


358 1650 280

362 1700 280

366 1750 280

370 1750 280

374 1750280

377 1800280

381 1800280

385 1850280

388 1900280


358 1650 280

362 1650 280

366 1700 280

370 1700 280

374 1750280

377 1750280

381 1800280

385 1800280

388 1850280


358 1600 280

362 1650 280

366 1650 280

370 1700 280

374 1700280

377 1700280

381 1750280

385 1750280

388 1800280


358 1550 280

362 1600 280

366 1650 280

370 1650 280

374 1650280

377 1700280

381 1700280

385 1750280

388 1750280


358 1550 280

362 1600 280

366 1600 280

370 1650 280

374 1650280

377 1650280

381 1700280

385 1700280

388 1750280

9C419

P-18



23000 FT

CRUISING WEIGHT

(LB)


-20 -50 -38

-15 -45 -33

-10 -40 -27

-5 -35 -22

0 -30 -17

5 -25 -12

10 -20 -6

15 -15 -1

20 -10 4


369 1650280

373 1700 280

377 1700 280

381 1750 280

385 1750280

389 1800280

393 1800280

397 1850280

401 1900280


369 1650280

373 1650 280

377 1700 280

381 1700 280

385 1750280

389 1750280

393 1800280

397 1800280

401 1850280


369 1600280

373 1600 280

377 1650 280

381 1650 280

385 1700280

389 1700280

393 1750280

397 1750280

401 1800280


369 1550280

373 1600 280

377 1600 280

381 1650 280

385 1650280

389 1700280

393 1700280

397 1750280

401 1750280


369 1550280

373 1550 280

377 1600 280

381 1600 280

385 1650280

389 1650280

393 1700280

397 1700280

401 1750280

9C420


(LB)


-20 -54 -41

-15 -49 -36

-10 -44 -30

-5 -39 -25

0 -34 -20

5 -29 -15

10 -24 -9

15 -19 -4

20 -14 1


380 1650280

385 1700 280

389 1700 280

393 1750 280

397 1750280

401 1800280

405 1800280

410 1850280

414 1850280


380 1650280

385 1650 280

389 1650 280

393 1700 280

397 1750280

401 1750280

405 1800280

410 1800280

414 1850280


380 1600280

385 1600 280

389 1650 280

393 1650 280

1800397 1700280

401 1700280

405 1750280

410 1750280

414

280 20000 T.A.S. (KT)


380 1550280

385 1600 280

389 1600

410

280

393 1650 280

397 1650280

401 1700280

405 1700280

1750280

414 1750280


380 1550280

385 1550 280

389 1600 280

393 1600 280

397 1650280

401 1650280

405 1700280

410 1700280

414 1750280

9C421

27000 FT-48 -34

15 CRUISING WEIGHT

(LB)


-20 -58 -44

-15 -53 -39

-10 -5 -43 -28

0 -38 -23

5 -33 -18

10 -28 -12

-23 -7

20 -18 -2


393 1700280

397 1700 280

402 1750 280

406 1800 280

410 1800280

415 1850280

419 1850280

423 1850280

428 1900280


1750393 1650280

397 1700 280

402 1700 280

406 1750 280

410

280

415 1800280

419 1800280

423 1800280

428 1850280

T.A.S. (KT)TOTAL FUEL FLOW (LB/HR)I.A.S. (KT)

393 1600280

397 1650 280

402 1650 280

1700 280

410 1700280

415 1750280

419 1750280

423 1750280

428 1800280

20000 T.A.S. (KT)TOTAL FUEL FLOW (LB/HR)I.A.S. (KT) 280

393 1600280

397 1600

402 1650 280

406 1650 280

410 1700280

415 1700280

419 1700280

423 1750280

428 1750280


393 1550

415

280

397 1600 280

402 1600 280

406 1600 280

410 1650280

1700280

419 1700280

423 1700280

428 1750280

9C422

22000 406

P-19



29000 FT

CRUISING WEIGHT

(LB)


-20 -62 -47

-37 -15 -57 -42

-10 -52 -36

-5 -47 -31

0 -42 -26

5

-20

10 -32 -15

15 -27 -10

20 -22 -4


425 406 1750 280

411 1750 280

415 1800 280

420 1800 280

1850280

429 1850280

434 1900280

438 1950280

431 1850280


406 1700 280

411 1700 280

415 1750

438

280

420 1800 280

425 1800280

429 1850280

434 1850280

1900280

437 1850280


406 1650 280

411 1700 280

415 1700 280

420 1750 280

425 1750280

429 1800280

434 1800280

438 1850280

443 1850280


406 1600 280

411 1650 280

415 1650 280

420 1700 280

425 1750280

429 1750280

434 1750280

438 1800280

443 1850280


406 1600 280

411 1600 280

415 1650 280

420 1650 280

425 1700280

429 1700280

434 1750280

438 1750280

443 1800280

9C423


(LB)


-20 -66 -50

-15 -61 -45

-10 -56 -39

-5 -51 -34

0 -46 -29

5 -41 -23

10 -36 -18

15 -31 -13

20 -26 -8

26000 T.A.S. (KT) TOTAL FUEL FLOW (LB/HR) I.A.S. (KT) 278

416 1750 278

421 1800

426 1850 278

431 1850 278

436 1850278

441 1900278

441 1900275

435 1800268

428 1750261


416 1700 278

421 1750 278

426 1800 278

431 1800 278

436 1850278

441 1850278

446 1900278

441 1800272

435 1750265

22000 T.A.S. (KT) TOTAL FUEL FLOW (LB/HR) I.A.S. (KT) 278

416 1700 278

421 1700

426 1750 278

431 1750 278

436 1800278

441 1800278

446 1850278

447 1850276

441 1750269


416 1650 278

421 1650 278

426 1700 278

431 1750 278

436 1750278

441 1800278

446 1800278

450 1850278

446 1750273


416 1600 278

421 1650 278

426 1650 278

431 1700 278

436 1750278

441 1750278

446 1750278

450 1800278

450 1750275

9C424


(LB)


-20 -70 -54

-15 -65 -49

-10 -60 -44

-5 -55 -38

0 -50 -33

5 -45 -28

10 -40 -22

15 -35 -17

20 -30 -12


413 1650 267

418 1700 267

423 1700 267

428 1750 267

433 1750267

437 1800267

438 1750264

432 1700257

424 1650249


413 1600 267

418 1650 267

423 1650 267

428 1700 267

433 1700267

437 1750267

442 1750267

439 1700262

431 1650254


413 1550 267

418 1600 267

423 1650 267

428 1650 267

433 1650267

437 1700267

442 1700267

445 1750265

438 1650258


413 1550 267

418 1550 267

423 1600 267

428 1600 267

433 1650267

437 1650267

442 1650267

447 1700267

444 1650262


413 1500 267

418 1500 267

423 1550 267

428 1550 267

433 1600267

437 1600267

442 1650267

447 1650267

449 1650265

9C425

P-20



35000 FT

CRUISING WEIGHT

(LB)


-20 -74 -59

-15 -69 -53

-10 -64 -48

-5 -59 -43

0 -54 -37

5 -49 -32

10 -44 -26

15 -39 -21

20 -34 -16


409 1550255

414 1600 255

419 1600 255

424 1650 255

429 1650255

434 1700255

433 1650252

426 1600244

414 1500235


409 1500

414 1550 255

419 1550 255

424 1600 255

429 1600255

434 1650255

439 1650255

435 1600250

426 1550242


409 1450255

414 1500

419 1500

424

255 255 1550

429 1550255

434 1600255

439 1600255

441 1600254

434 1550247


409 1450255

414 1450 255

419 1450 255

424 1500 255

429 1500255

434 1550255

439 1550255

443 1600255

441 1550251


409 1400255

414 1400 255

419 1450 255

424 1450 255

429 1500255

434 1500255

439 1500255

443 1550255

447 1550255

9C426


(LB)


-20 -77 -61

-15 -72 -56

-10 -67 -50

-5 -62 -45

0 -57 -40

5 -52 -34

10 -47 -29

15 -42 -24

20 -37 -18


407 1500244

412 1500 244

417 1550 244

422 1550 244

427 1600244

428 1600241

420 1500234

407 1450223


407 1400244

412 1450 244

417 1500 244

422 1500 244

427 1500244

432 1550244

433 1550242

426 1500235

414 1400225


407 1350244

412 1400 244

417 1450 244 244

1450422 1450

427

244

432 1500244

437 1500244

435 1500240

427 1400232


407 1350244

412 1350 244

417 1400 244

422 1400 244

427 1450244

432 1450244

437 1450244

441 1500244

436 1450238


407 1300244

412 1300 244

417 1350 244

422 1350 244

427 1400244

432 1400244

437 1400244

441 1450244

443 1450242

9C427


(LB)


-20 -77 -61

-15 -72 -56

-10 -67 -50

-5 -62 -45

0 -57 -40

5 -52 -34

10 -47 -29

15 -42 -24

20 -37 -19


407 1450232

412 1500 232

417 1550 232

416 1500 228

408 1450221

394 1400210


407 1400232

412 1400 232

417 1450 232

422 1450 232

427 1500232

423 1450227

412 1400218

396 1300206


407 1300232

412 1350 232

417 1350 232

422 1400 232

427 1400232

432 1450232

429 1400228

421 1350221

410 1300212


407 1250232

412 1300 232

417 1300 232

422 1350 232

427 1350232

432 1400232

437 1400232

433 1350227

426 1300220


407 1200232

412 1250 232

417 1250 232

422 1300 232

427 1300232

432 1350232

437 1350232

441 1350232

435 1300226

9C428

P-21



41000 FT

CRUISING WEIGHT

(LB)


-20 -77 -61

-15 -72 -56

-10 -67 -50

-5 -62 -45

0 -57 -40

5 -52 -34

10 -47 -29

15 -42 -24

20 -37 420



399 1400 214

404 1400 214

409 1400 214

408 1350 213

398 1300205


407 1300 221

412 1300 221

417 1350 221

422 1350 221

424 1350220

416 1300213

404 1250203


407 1200 221

412 1250 221

417 1250 221

422 1300 221

427 1300221

432 1350221

427 1300216

419 1250209

408 1200201


407 1150 221

412 1200 221

417 1200 221

422 1250 221

427 1250221

432 1300221

436 1300221

431 1250216

425 1200210

9C429

P-22

BAe 125-800A TI 4040.25C CHG 01, June 1999

LONG RANGE CRUISE SPEED UP TO 31,000 FT

P-23

TI 4040.25C BAe 125-800A CHG 01, June 1999

LONG RANGE CRUISE SPEED 33,000 FT, 35,000 FT

P-24

BAe 125-800A TI 4040.25C CHG 01, June 1999

LONG RANGE CRUISE SPEED 37,000 FT, 39,000 FT

LONG RANGE CRUISE SPEED 41,000 FT

P-25

TI 4040.25C BAe 125-800A CHG 01, June 1999

P-26

BAe 125-800A TI 4040.25C CHG 01, June 1999

P-27

TI 4040.25C BAe 125-800A CHG 01, June 1999 TI 4040.25C BAe 125-800A CHG 01, June 1999

P-28

P-28

BAe 125-800A TI 4040.25C CHG 01, June 1999

WIND COMPONENT

P-29

TI 4040.25C BAe 125-800A CHG 01, June 1999

SUMMARY OF SINGLE-ENGINE

CEILINGS DRIFT DOWN

WEIGHT

(LB)

SPEED

IAS KTS

ENG ANTI- ICING

SINGLE-ENGINE CEILING AT

ISA-15 ISA ISA+10 ISA+20

26,000 E.R.CLIMB 180 OFF 23000 21000 18000 13000 MIN CRUISE 210 OFF 23000 19000 16000 9000 L.R.CRUISE 240 OFF 19000 15000 10000 L.R.CRUISE 240 ON 17000 11000 7000 2000

25,000 E.R.CLIMB 176 OFF 24000 22000 19000 15000 MIN CRUISE 206 OFF 24000 21000 18000 12000 L.R.CRUISE 235 OFF 21000 17000 12000 5000 L.R.CRUISE 235 ON 18000 12000 8000 3000








3000

NOTE: The ceilings in this table are based on average performance

on maximum continuous power. To check obstacle clearance, use the enroute net gradient in the performance manual. Enroute net ceiling is 5000 to 8000 feet below the average ceiling given above at enroute climb speed.

P-30