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Page 1: XM655 Flight Reference Cards AL5

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COPY – Uncontrolled copy

XM655 Flight Reference Cards

AL5

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XM655 AL5

Amendment list AL No Amended by Date

Initial issue XM655 MaPS 13/04/2017AL1 XM655 MaPS 14/05/2017AL2 XM655 MaPS 25/01/2018AL3 XM655 MaPS 13/05/2018AL4 XM655 MaPS 07/10/2018AL5 XM655 MaPS 25/07/2021

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Contents Section 1 – External – Internal ............................................................................................................. 2-1

Section 2 – Engine Starting .................................................................................................................. 2-1

Section 3 – After Start checks .............................................................................................................. 3-1

Section 4 – Governor Check ................................................................................................................. 4-1

Section 5 – Taxy ................................................................................................................................... 5-1

Section 6 – Pre-Take off ....................................................................................................................... 6-1

Section 7 – After landing ...................................................................................................................... 7-1

Section 8 – Shutdown checks when after landing checks have NOT been used ................................. 8-1

Section 9 – Shutdown checks when after landing checks HAVE been used ........................................ 9-1

Section 10 – Emergency procedures .................................................................................................. 10-1

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Section 1 – External – Internal EXTERNAL

Pilots1. Aircraft locks, jury struts, blanks and chocks. a) Undercarriage locks in place

b) Main undercarriage bay jury struts in placec) Crew door lock support frame removed.d) Main undercarriage pigeon netting removede) Air intake and jet pipe blanks removedf) Cooling duct “bird” blanks removedg) Pressure head, probe, ADD covers and static vent plugs removed.h) Main chocks in place

2. Hydraulic accumulator gauges 2550~2600 PSI (pressure exhausted)3. Pneumatic normal pressure. Minimum 1000 PSI

AEO1. AAPP scoop. OPEN – Bird blanks removed2. 200V AC, 28V DC OFF. Cables connected. Houchin running3. Portable fire extinguishers available a) Foam and powder at Houchin

b) Powder and CO2 at Palouste/VWc) CO2 with lance at Port main bogie

4. Air start (Palouste/VW) a) Hose connectedb) Control cable connected (for Palouste only)

5. Aircraft Battery Connected

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INTERNAL

AEO1. Rear seat movement Full and free2. Aircraft Battery ON3. Intercoms a) Normal ON

b) Conference ONc) External ONd) Station box one) Normal I/C selected, volume up

4. Aircraft Battery Check 22V minimum for 30 seconds on standing load before 28V external requested5. Circuit breakers on 3P Check all made AL26. Circuit breakers on 4P Check all made AL27. Nosewheel steering override switch Normal/Wire Locked AL28. External 28V ON, voltmeter rise (On Houchin only)9. Airbrake emergency isolation Normal10. Alternators Four OFF, four ambers11. Non-Essential Supplies a) Trip, check indicators (2)

b) Reset, check indicators (2)c) Normal, guarded

12. Frequency changers No.1 and 2 Stop switches pressed – FAIL switch central13. RAT field switch. Normal, guarded14. AAPP. a) LP cock OPEN

b) Fire warning testc) Oxygen switch OFFd) Fuel MI indicates ‘HIGH’e) Master switch OFF

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Pilots1. Intercom (P1 and P2) a) Station box ON

b) Normal I/C selected, volume up2. PFCs, autostabs and feel a) Yaw dampers OFF (3 way switch central)

b) Pitch dampers OFF (pressed), four amber lightsc) Mach trimmers OFF – amber button pushed (light on), blue lights outd) Artificial feel, three pulled up, three amber lightse) PFC buttons, ten pressed, ten amber lights

3. Main warning lights Both ON4. Reminder MIs Three white5. Fuel pumps All OFF6. Bomb doors emergency switch Normal, guarded7. Emergency hydraulic power pack Press OFF8. Airbrake switch Corresponds

Any Additional Crew1. Intercom a) Station boxes ON

b) Normal I/C selected, volume up, microphones OFF

AEO1. Extra Supplies Trip button. Pressed2. 200V supply. External ON and checked (65V on Incoming Alternator gauge)3. External 28 Volts Off. Check battery volts 22 volts min AL44. 28V TRU’s a) No.1 On – Check TRU busbar indicator AL4

b) No.2 On – Check TRU busbar indicator AL45. 115V transformers. a) ON, check both MI AL4

b) Check auto-coupling by isolating No 1 & 4 synch bus bars in turn – check MI AL4 c) Check manual coupling by selecting control switch through OFF to COUPLE and

back to ON in turn – check MI indication AL4

6. RT1 a) Set frequency 124.025 for Wellesbourne Informationb) Set TR on rotary dial

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c) Check volume with pilots7. Compass switches (2) ON – check de-synched with pilots8. Navigator's bomb door switches a) Nav. Radar switch CLOSED

b) Nav. Plotter switch CLOSED9. Emergency door opening switches a) Nav. Radar switch CLOSED and guarded

b) Nav. Plotter switch CLOSED and guarded AL1c) AEO switch cover wire locked AL1

10. Engine fire warning Press Test switch, check 4 red lights with Pilot, release switch, check 4 lights off

Pilots1. PFCs, autostabs and artificial feel a) Check with ASC – Clear to start PFCs AL1

b) PFC’s ON – Order A,E,R – Check each group with ASC AL1c) Autostabs: AL1i) Yaw dampers – set to 1 (aft)ii) Pitch dampers (4) – pull up – if lights not out, press comparator reset buttoniii) Mach trimmers – pull amber button up, confirm 2 blue and 1 amber light outd) Artificial feel – confirm 3 amber lights out AL1

2. Feel lock a) Set switch to aft (locked) – amber light onb) Set switch forward (normal) – amber light out

3. Reminder MI Three black4. Main warning lights OUT5. Frequency changers a) No.1 – START – Black MI AL1

b) No.2 – START – Black MI AL1c) FAIL switch – No.1 AL1d) No.1 – STOP – White MI AL1

6. Abandon aircraft switches a) Ensure cabin light OFF (switches at AEO position and crew entrance [starboard])b) Operate P1 switch, check Abandon sign and cabin light ONc) P1 switch normal (forward and latched), check sign and cabin light OFFd) Operate P2 switch, check Abandon sign and cabin light ONe) P2 switch normal (forward and latched), check sign and cabin light OFFf) Cabin light as required (switches at AEO position and crew entrance [starboard])

7. Bomb door normal control Corresponds

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8. Tail skid lights Check, ask ASC to operate9. LP fuel cocks All open and guarded10. Alternator failure warning Flashing11. Canopy jettison levers Pip-pins removed and stowed. AL512. Canopy lift struts Pip-pins removed and stowed AL313. Canopy unlocked MI Black14. Entrance door MI White15. Pitot Heater MI White16. Accelerometer Reset17. Undercarriage a) Emergency override horizontal

b) Down button INc) Six green lightsd) Day/night screens checked

18. Brakes/accumulator pressure a) Parking brake SETb) Check both pressure indicators in green sectorc) Start EHPPd) Check both pressure indicators in green sectore) Stop EHPP, centre switch

19. Anti-dazzle lighting Checked20. Take-off/cruise selector Cruise selected, guarded & Wire locked AL121. JPT limiters ON selected and guarded & Wire locked AL122. HP cocks SHUT23. Under carriage emergency selector Fully in and wire-locked AL124. Fuel contents/CG Checked, switch normal25. Fuel console Set as required AL126. Bomb bay & wing/fuselage fire warning light Press, check warning light27. Windscreen demister a) Check operation

b) Set as required28. Throttle detent isolation switch IN29. Pressure selector CRUISE30. Cabin air switches SHUT (2)31. Air Ventilated Suit Master switch CLOSED AL4

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32. Ram air valve SHUT33. Temperature selector COLD34. Cold air turbine MI Black35. External lights master switch ON36. Navigation lights FLASH, check with ASC37. Tank pressurisation OFF, four MI white38. Air-to-air refuelling panel. OFF39. Engine anti-icing OFF (2)40. Airframe anti-icing OFF (3)41. Systems check – Flight controls Check for full and free movement and correct surface operation with ASC AL1

End of External & Internal checklist

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Section 2 – Engine Starting PilotsAdvise ASC to start Palouste/VW

1. Parking Brake SET2. Clearance to start RT - Request clearance to start engines from tower AL13. Normal/Rapid Air selector switch NORMAL4. Ignition switch ON5. Engine master switch ON6. Air cross feed MI OPEN7. Palouste Request ASC to make available, and confirm when ready for automatic AL18. Start procedure/checks8.1. Appropriate engine air switch OPEN, remainder shut8.1a. AEO – Rotary bus selector Select alternator AL18.2. Appropriate fuel flow indication button Pressed8.3. Individual engine start button Pressed8.4. Oil pressure Rising8.5. RPM indication 4%8.6. Throttle lever/HP Cock Open to 8~10 lbs fuel flow8.7. JPT Peaks at less than 700°C and falling8.8. Throttle lever Open slowly to idle detent8.9. Fire warning OUT8.10. Engine start light OUT by 16% RPM indication If Not8.10a. Engine master switch OFF, check Engine start light goes off8.10b. Engine master switch ON, check Engine start light remains off8.11. RPM indication Advise AEO at 22%8.12 Idling RPM 24.5% minimum

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AEO8.13. Alternator a) Within limits at 22% engine RPM

b) Close A breakerc) Amber light out, S breaker MI horizontal, kW/kVAR meters reading

d) Alternator failure warning light as appropriate 3 of 4 – Alternator fail light – Steady red 4 of 4 – Alternator fail light - Out

AL1

8.14. Palouste ASC - After all engines start – Shut down AL1End of Engine Starting checklist

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Section 3 – After Start checks Pilots1. Alternator failure warning light OUT at pilots panel and AEO2. Engine master switch OFF3. Ignition switch OFF4. Air crossfeed MI SHUT5. Fuel console As required6. Hot air ducting leak check a) OPEN all (4) engine air switches

b) Confirm no ducting leaks with ASCc) OPEN both cabin air switchesd) Confirm no ducting leaks with ASCe) CLOSE both cabin air switchesf) CLOSE all (4) engine air switches

7. Engine anti-icing Check operation of port/starboard with ASC, set as required8. Airbrakes Pilots – Check with ASC – Clear to operate Airbrakes AL1

a) Select emergency motor AL1b) Select mid position, check with ASCc) Select in position, check with ASCd) Select normal motore) Select mid position, check with ASCf) Select high drag position, check with ASCg) Select mid position, check with ASCh) Select in position, check with ASCi) Select normal motor, switch guarded

9. Hydraulic pressure Checked, normal10. Bomb door normal operation. a) Clear with ASC – (MI cross hatched while traveling) AL1

b) Select OPEN, MI white, 8 seconds maximumc) Select CLOSE, MI black, pressure normal

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AEO11. Extra supplies trip Press, check that No 2 alternator synchs on busbar. Check 200V indication

OFF with ASC

Line deleted AL512. 28V TRU s a) Check each TRU On DC volt meter by isolating each TRU in turn (27 V

min) b) Both ON, indications checked on TRU ammeters

13. Check external equipment removed a) Air start hoseb) Air start control cable (if using Palouste)c) External 200Vd) External 28V

14. AAPP a) Clear with ASCb) Master switch ON (left side first) – check scoop OPEN with ASCc) Press start button (springs out within 3 seconds)d) JPT / oil pressure within limitse) Fire warning light OUT

15. AAPP a) Within limits – press AAPP Test Button to check outputb) AAPP ON button pressed (1 second max)c) Check indicationsd) Press Extra Supplies Trip, check No 2 alternator synchs on busbar

16. Alternators a) Synchronise all alternators onto busbarb) Check load sharing, kW /kVARc) Isolate No 1, 3 and 4 from busbard) Check No 2 alternator remains synched on busbar

End of After Start checklist

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Section 4 – Governor Check Must be carried out 24hrs BEFORE public displays

SAFE AIRCRAFT POSITIONING MUST BE AGREED BEFORE START OF CHECK

Pilots1.Clearance to start a) Check with ASC

b) RT clearance for high power to Control Tower2. Parking brake SET3. Chocks Forward chocks REMOVED – confirm with ASC4. Take-off/cruise selector CRUISE selected and guarded5. JPT limiters ON selected and guarded6. Engine fire warning Press Test switch, check 4 red lights with Pilot, release switch, check 4 lights 7. Hydraulic pressure Checked, normalAEO monitors CSDU temps during checks Within limitsASC monitors for brake slip during checks Confirm with ASC to warn immediately if aircraft moves.8. Engine Cruise Governor Procedure All engines stable at idle

Engines 1 and 4 to 40%Engines stabilisedEngines 1 and 4 to 75%Engines stabilisedNo 1 to maximum throttleConfirm RPM, oil pressure and JPT stable, AEO to logConfirm visually ok with ASCReduce to 75%Engines stabilisedNo 4 to maximum throttleConfirm RPM, oil pressure and JPT stable, AEO to log

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Confirm visually ok with ASCReduce to 75%Engines stabilisedReduce Nos 1 and 4 to idleEngines 2 and 3 to 40%Engines stabilisedEngines 2 and 3 to 75%Engines stabilisedNo 2 to maximum throttleConfirm RPM, oil pressure and JPT stable, AEO to logConfirm visually ok with ASCReduce to 75%Engines stabilisedNo 3 to maximum throttleConfirm RPM, oil pressure and JPT stable, AEO to logConfirm visually ok with ASCReduce to 75%Engines stabilisedReduce Nos 2 and 3 to idle

9. Chocks SET – confirm with ASCEnd of Governor Check checklist

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Section 5 – Taxy Pilots1.Clearance to start a) Check with ASC

b) RT to Control Tower2. Pitot heaters ON – confirm with ASC3. Entrance Door Closed, MI black, green light, handle aligned4. Landing lights ON at Taxy setting5. Parking brake SET6. Hydraulic pressures Checked, two in the green7. Chocks REMOVE - confirm with ASC8. Engine throttles 2 and 3 Increase to 40%8. Aircraft not moving forward Confirm with ASC9. Parking brake RELEASE10. Aircraft moving Confirm with ASC – increase throttles if necessary11. Main brakes Apply at P2 position and hold12. Aircraft not moving forward Confirm with ASC13. Main brakes Apply at P1 position and hold, release at P2 position14. Aircraft not moving forward Confirm with ASC15. Short straight taxi a) Confirm clear to taxi with ASC

b) Release brakesc) Allow short roll forwardd) Stop aircraft with main brakes at P1 position and holde) Confirm stationary with ASC

16. Nosewheel steering check a) Confirm clear to taxi with ASCb) Release P1 brakes

c) As aircraft rolls forward, P1 steers fully left, then through to fully right, then back to straight ahead. d) Stop aircraft with main brakes at P1 position and holde) Confirm stationary with ASC

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f) Release P1 brakes g) As aircraft rolls forward, P2 steers fully left, then through to fully right, then

back to straight ahead.

h) Stop aircraft with main brakes at P2 position and holdj) Throttles to idle

k) Confirm aircraft stationary, steering satisfactory and no hydraulic leaks with ASC

17. Parking brake SETIf intending to carry out other operations/Fast taxi RT to inform Tower of intended activity AL3

Go to Pre-Take off (Section 6) AL3

If intending to Shutdown Go to Shut down checks when after Landing checks have NOT been used (Section 8)

AL3

End of Taxy checklist

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Section 6 – Pre-Take off 1. Electrics All checked

a) Alternators all ONb) No.2 on Synch barc) AAPP runningd) 115V transformers ONe) 28V TRU’s both ONf) All indications normalg) Frequency changers – No.2 ON – No.1 OFF – FAIL switch to No.1

2. PFC/auto stab ids panel All lights out3. Compasses Synchronised, set for take-off4. All red and amber lights Out5. Magnetic indicators All black6. Hydraulic pressures Checked, two in the green7. Fuel console Checked, as required8. Transfer switches Centre and guarded, lights out9. DV windows (port/stbd) Locked10. Tank pressurisation switch OFF11. External intercom OFF12. Crew brief Completed13. Flying controls Checked, full and free movement, set for take-off14. Cabin air switches Port or Stbd open15. Engine air switches 1 and 2 or 3 and 4 OPEN (all OPEN if anti-icing required)

End of Pre Take-off checklist

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Section 7 – After landing 1. Airframe anti-icing OFF2. Engine anti-icing As required3. Engine air switches All SHUT4. External intercom ON5. Brake check If required6. Parking brake As required7. Tank pressurisation switch OFF8. No 3 alternator ON synch busbar9. No 2 alternator Isolate from synch busbar10. AAPP Checked, OFF11. PFCs and autostabs All PFCs Off except auxiliary rudder (9 amber lights)

a) Yaw dampers off (3 way switch central)b) Pitch dampers off (pressed), four amber lightsc) Mach trimmers off – amber button pressed (light on), blue lights outd) Artificial feel, three pressed, three amber lights

12. Airbrakes IN13. Auto/manual switches Four to MANUAL14. Alternators No 1 and 4 OFF - Check flashing light15. HP cocks No 1 and 4 SHUT16. Fuel pumps Groups 1 and 4 Off17. Hydraulic and brake pressure Checked, two in the green

End of After Landing checklist

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Section 8 – Shutdown checks when after landing checks have NOT been used

1. Parking brake SET2. External intercom ON – Confirm ASC connected3. Chocks Request placed with ASC AL54. Airframe anti-icing OFF AL55. Engine anti-icing OFF AL56. Engine air switches All SHUT AL57. Tank pressurisation switch OFF AL58. No.3 alternator On sync bus bar9. No.2 alternator Isolate from sync bus bar10. AAPP Checked, OFF AL511. PFC and Autostabs All PFC’s OFF (10 amber lights)

a) Yaw dampers off (3 way switch central)b) Pitch dampers off (pressed), 4 amber lightsc) Mach trimmers off – amber button pressed (light on), blue lights outd) Artificial feel, three pressed, 3 amber lights

12. Airbrakes IN AL513. Auto/manual switches Four to MANUAL AL514. Alternators No.1 and 4 OFF – Check flashing light15. HP cocks No.1 and 4 SHUT16. Fuel pumps Groups 1 and 4 OFF17. Hydraulic and brake pressure Checked, two in the green18. Bomb doors As required19. Pitot heaters OFF AL520. Engine master switch OFF21. Air to Air refuelling panel OFF AL122. Landing lamps Retracted

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23. Windscreen demister OFF24. Entrance door Open – Confirm with ASC25. Compasses Both OFF26. Frequency changers OFF – FAIL switch central27. 115V transformers Both OFF28. 28V TRU Both OFF29. Alternators No.2 and No.3 – Off – All amber alternator lamps on, Red Alt Fail flashing AL130. HP cocks No.2 and No.3 - SHUT AL131. Fuel pumps All OFF32. External lighting All OFF, Master OFF33. Cabin air switches Both SHUT34. Parking brake Release35. Completion notification RT to Tower – Inform activity complete AL136. RT1 OFF AL537. Station boxes All OFF38. Intercom and RT1 OFF39. Battery Volts normal, OFF

Ground crew AL540. Canopy jettison levers Replace Pip-pins AL542. Canopy lift struts Replace Pip-pins AL543. PEC covers Replace AL5

End of Shutdown checklist

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Section 9 – Shutdown checks when after landing checks HAVE been used

1. Parking brake SET2. External Intercom On – Check ASC On AL13. Chocks In position – Confirm with ASC4. Pitot heaters OFF AL15. Auxiliary rudder STOP – All 10 PFC amber lights ON6. Bomb doors As required7. Engine master switch OFF8. Air to Air Refuelling panel OFF AL49. Landing lamps Retracted10. Windscreen demister OFF11. Entrance door Open – Confirm with ASC12. Frequency changers OFF – FAIL switch central13. Compasses Both OFF14. 115V transformers Both OFF15. 28V TRU Both OFF16. Alternators No.2 and No.3 – OFF – Alternator Amber lamps – ON – Red Alt fail flashing AL117. HP cocks No.2 and No.3 - Shut AL118. Fuel pumps All OFF19. External lighting All OFF, Master OFF20. Alternators All OFF21. Engine air switches All SHUT22. Cabin air switches Both OFF23. Engine anti-icing OFF24. Completion notification RT to Tower – Inform activity complete AL125. Parking brake Release26. Station boxes All OFF

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27. Intercom and RT 1 OFF28. Battery Volts normal, OFF

Ground Crew AL529. Canopy jettison levers Replace Pip-pins AL530. Canopy lift struts Replace Pip-pins AL531. PEC covers Replaced AL5

End of Shutdown checklist

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Section 10 – Emergency procedures FIRE AL5

Engine Fire AL5

Indication: Fire warning light on

Pilot’s action

1. Warn crew 2. Close HP cock 3. Close LP cock 4. Press fire extinguisher button 5. Shut engine air switch 6. Switch off booster pumps of appropriate engine 7. Order AEO to switch OFF appropriate alternator 8. Order AEO to inspect engine through periscope

AL5

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Engine Fire - Continued AL5

AEO’s actions

1. Switch OFF appropriate alternator. Carry out alternator failure drill2. Inspect engine through periscope

NOTE 1: Should any other indications of fire be observed apart from the fire-warning light, e.g. excessive JPT smoke, flames, etc., the captain may also close down the adjacent engine on the same side, using drills laid down above, except for operating the fire extinguisher button and switching OFF the alternator.

NOTE 2: (a) If the fire warning light goes out and there are no other indications of fire, it can be assumed that the fire has been extinguished. No attempt should be made to relight the engine.

NOTE 2: (b) If the adjacent engine has been closed down, the captain may at his discretion, when the fire has been extinguished, relight the engine, or use its fuel to feed the other engines.

AL5

End of Emergency procedure – Fire – Engine Fire

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AAPP Fire AL5

Indication: Fire warning light on in head of extinguisher button

AEO’s actions

1. Warn crew 2. Press extinguisher button 3. Master switch OFF

The warning light should go out when the fire is extinguished

NOTE: The LP cock is closed automatically when the fire extinguisher button is pressed and consequently, on run-down of the engine, the AAPP supply will come off the bus-bar. The AAPP starting circuit is electrically locked out and can only be broken by removing fuse No. 961 in 62P (vital bus-bar).

AL5

End of Emergency procedure – Fire – AAPP Fire

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Brake Fires AL5

Captain’s actions

After clearing the runway, stop the aircraft and have the brakes inspected by a rear crew member.

AL5

Brakes smoking AL5

1. Warn the control and request that a fire tender be dispatched to the aircraft.2. Do not apply the parking brake; hold the aircraft with minimum amount of foot brake 3. Order the crew to take fire extinguishers and powder (if carried) to the brakes to assist the fire

tender party. 4. Carry out the after-landing checks; do not close down Nos.1 and 4 engines if still running. 5. When the brakes are cool, recall the crew and order the fire tender to follow the aircraft. 6. Start taxying. Close down Nos.1 and 4 engines when the aircraft is moving. 7. Use the minimum amount of breaking. 8. On reaching dispersal, do not apply the parking brake; hold the aircraft with the minimum amount

of foot brake until the chocks are in position. 9. Warn the crew chief to keep the fire tender in the vicinity of the aircraft until the brakes are cold. 10. Order the brakes to be checked in the F.700

AL5

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Brake fires – Continued AL5

Brakes on fire AL5

Captain’s actions

1. Warn the control tower and request that the fire tender be dispatched to the aircraft. 2. Stop the aircraft. Do not apply the parking brake. Hold the aircraft with the minimum of foot

brake. 3. Order the crew members to take the fire extinguishers and powder to the brakes. 4. Do not close the HP cocks on Nos.1 and 4 engines, if still running in case of fuel dump into the

brakes. 5. When the file is under control, carry out the closing down checks and leave the aircraft to be

towed to dispersal.

Crew members

1. When the aircraft has stopped, collect fire extinguishers and powder (if carried) and go to the fire. 2. Approach the wheels from the fore-and-aft direction, i.e. in line with the tyres and not, repeat

not, in line with the axle. 3. Apply powder to the brakes and endeavour to bring the fire under control.

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Brake fires – Continued AL5

Brakes on fire - Continued AL5

4. Keep the captain informed of the state of the fire5. Do not use water/glycol extinguishers on the burning brakes, unless in emergency and if no other

method of fighting the fire is available. 6. When the fire is out, return to the cabin and carry out the closing-down checks

NOTE 1: After brakes smoking or on fire the aircraft should not be flown until the brakes have been inspected.

NOTE 2: Aircraft are not, repeat not, to be taxied with a crew member on the door to watch the brakes.

AL5

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Electrical Failures AL5

Alternator Failures - General AL5

(a) Indications. A protective systems malfunction or light failure may result in one or more indications not being immediately apparent.

(b) Bus-bar failures. If it is not possible to restore power to the failed bus-bar(s) before loads begin to run down (3-4 secs.) the loads must be switched OFF before attempting to restore the electrical supply.

NOTE 1: If an alternator has failed but not tripped off line, switch OFF all loads connected to its bus-bar before switching off the alternator.

NOTE 2: If the RAT has taken over the sync. Bar and failed do not press the extra supplies trip unless all four bus-bars are feeding their loads satisfactorily.

(c) Paralleling. Do not parallel alternators subsequent to unexplained failures. (d) AAPP starting. Post-Mod 1271, a cartridge start will be available only whilst the non-essential bus-

bar are tripped.

AL5

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Electrical Failures - Continued AL5

Single Alternator Failure AL5

Indications

1. Pilot’s and AEO’s alternator failure light Steady Red 2. “A” breaker light One amber 3. Failed alternator volts/frequency Abnormal 4. Failed alternator loading KW/KVAR Zero

Actions

AEO

1. Switches OFF failed alternator 2. Checks failed alternator volts and frequency 3. Presses RESET button, observing volts/frequency meters 4. If volts and frequency are normal, switches ON alternator. If they remain outside limits leaves

alternator switched OFF and monitors periodically.

AL5

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Electrical Failures – Continued AL5

Two Alternator Failure AL5

Indications

1. Pilot’s and AEO’s alternator failure light Flashing Red 2. “A” breaker light Two amber 3. Failed alternator volts/frequency Abnormal 4. Failed alternator loading KW/KVAR Zero

Actions Captain Pulls RAT and maintains speed above 0.85M/250 kts AEO 1. Warns captain, checks RAT released, trips non-essential supplies. 2. Switches OFF failed alternators 3. For each failed alternator in turn

(a) Selects volts/frequency (b) Presses RESET button (c) If volts/frequency within limits, switch ON; if not, leaves OFF

AL5

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Electrical Failures AL5

Two Alternator Failure – Continued AL5

4. If RAT is on sync. Bar and serviceable replace by main alternator5. At low level (or when below 30,000 feet): Cartridge starts AAPP, checks volts/frequency within limits.

Subsequent actions

AEO

1. Non-essential supplies (Card 22) (a) All OFF (b) Switches to RESET (c) Restores loads as required within the limitations of the electrical supplies

AL5

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10-11

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Electrical Failure – Continued AL5

Three Alternator Failure AL5

Indications

1. Pilot’s and AEO’s alternator failure light Flashing Red 2. “A” breaker light Three amber 3. Failed alternator volts/frequency Abnormal 4. Failed alternator loading KW/KVAR Zero

Actions Captain Pulls RAT and initiates descent to below 30,000 feet, maintaining speed above 0.85M/250 kts, as required by RAT AEO 1. Trips non-essential supplies, checks RAT released. 2. For each failed alternator in turn

(a) Selects volts/frequency (b) Presses RESET button (c) Switches ON

AL5

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10-12

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Electrical Failure – Continued AL5

Three Alternator Failure - Continued AL5

(d) High altitude. If RAT on sync. Bar, monitors and maintains within limits.(e) Below 30,000 feet (or at low level). Cartridge AAPP and brings onto sync. Bar.

AL5

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10-13

XM655 AL5

Electrical Failure – Continued AL5

Three Alternator Failure - Continued AL5

Subsequent actions All crew Carry out initial actions of abandon aircraft of abandon aircraft drill (Cards xx, xx) but, if necessary, maintaining speed above 0.85M/250 kts. as required by RAT. AEO1. Replaces RAT by serviceable alternator 2. Below 30,000 feet brings AAPP onto sync. Busbar. 3. Continues to attempt to reset alternators. If partially successful, then continues checks under two/single

alternators failure (Card 10-8, 10-9). 4. Non-essential supplies

(a) All off (b) Switch to RESET (c) Below 10,000 feet. Restore loads as required with limits of remaining electrical supply, do not operate

airbrakes.

AL5

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10-14

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Electrical Failure – Continued AL5

Three Alternator Failure - Continued AL5

Pre-landing 1. If AAPP is on load, do not lower the undercarriage until the aircraft is 3 mins/5 miles from finals. 2. Monitor AAPP volts/frequency/JPT/oil pressure. 3. Select serviceable alternator on sync. Switch. 4. If AAPP volts/frequency or JPT fluctuates hold sync. Selector switch in and press extra supplies trip to allow

serviceable alternator to take over sync. Bar.

AL5

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10-15

XM655 AL5

Electrical Failure – Continued AL5

Four Alternator Failure AL5

Indications

1. Pilot’s and AEO’s alternator failure light Flashing Red 2. “A” breaker light Four amber 3. Failed alternator volts/frequency Abnormal 4. Failed alternator loading KW/KVAR Zero

Initial Actions Captain Pulls RAT and initiates descent to below 30,000 feet, maintaining speed above 0.85M/250 kts, as required by RAT AEO 1. Trips non-essential supplies, checks RAT released. 2. Alternator (in order 4, 3, 2, 1)

(a) Switches OFF (b) Presses RESET button (c) Switches ON

AL5

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10-16

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Electrical Failure – Continued AL5

Four Alternator Failure - Continued AL5

3. High level. If RAT on sync. Bar, maintains within limitsLow level (or below 30,000 feet.) Cartridge starts AAPP, checks volts/frequency within limits. Presses AAPP ON button.

AL5

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10-17

XM655 AL5

Electrical Failure – Continued AL5

Four Alternator Failure - Continued AL5

Subsequent actions All crew Carry out initial actions of abandon aircraft of abandon aircraft drill (Cards xx, xx) but, if necessary, maintaining speed above 0.85M/250 kts. as required by RAT. AEO1. Continues to attempt to reset alternators and, if partially successful, replaces RAT on sync. Bar by one of the

restored alternators or AAPP, continues checks under 3, 2 or single alternator failure (Card xxx, xxx). 2. Non-essential supplies (Card xxx)

(a) All off (b) Only if absolutely necessary is switch to be placed to RESET (c) Restore minimum number of loads. Airbrakes must not be used.

AL5

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10-18

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Electrical Failure – Continued AL5

Four Alternator Failure - Continued AL5

Pre-landing 1. Do not lower the undercarriage until the aircraft is 3 mins/5 miles from finals.

AL5

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10-19

XM655 AL5

AVRO

VULCAN

B Mk.2

COPY

Un-controlled

copy

FRC’s For use on

XM655 AL5