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时间:2011-04-10 09:48来源:蓝天飞行翻译 作者:航空
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 (a)  Make sure the lights go off.
 S 864-297
 (5) Push and hold the TEST 2 switch on the SQUIB TEST panel, M7327.
 (a)  Make sure the cargo A, B, C and D lights come on.
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 26-21-01
 ALL  ú ú 04 Page 430 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-298
 (6) Release the switch.
 (a) Make sure the lights go off.
 P. Return to Normal
 S 864-320
 (1) Remove the DO-NOT-CLOSE tags and close these circuit breakers:
 (a) 6C1, ALTN PWR ENG FIRE/OVHT DET LOOP A ENG 1
 (b) 6C2, ALTN PWR ENG FIRE/OVHT DET LOOP A ENG 2
 (c) 6C3, ALTN PWR ENG FIRE/OVHT DET LOOP A ENG 3
 (d) 6C4, ALTN PWR ENG FIRE/OVHT DET LOOP A ENG 4
 (e) 6C5, ALTN PWR LOOP A APU FIRE/BLD DUCT OVHT
 (f) 6F1 IGN 1 ENG 1
 (g) 6F2 IGN 1 ENG 2
 (h) 6F3 IGN 1 ENG 3
 (i) 6F4 IGN 1 ENG 4
 (j) 6G10, ENG FIRE/OVHT DET ENG 2 LOOP A
 (k) 6G11, ENG FIRE/OVHT DET ENG 2 LOOP B
 (l) 6G12, ENG FIRE/OVHT DET ENG 4 LOOP A
 (m) 6G13, ENG FIRE/OVHT DET ENG 4 LOOP B
 (n) 6G19 STBY IGN ENG 1
 (o) 6G20 STBY IGN ENG 2
 (p) 6G21 STBY IGN ENG 3
 (q) 6G22 STBY IGN ENG 4
 (r) 6H10, ENG FIRE/OVHT DET ENG 1 LOOP A
 (s) 6H11, ENG FIRE/OVHT DET ENG 1 LOOP B
 (t) 6H12, ENG FIRE/OVHT DET ENG 3 LOOP A
 (u) 6H13, ENG FIRE/OVHT DET ENG 3 LOOP B
 (v) 6H14, APU FIRE/BLD DUCT OVHT LOOP A
 (w) 6H15, APU FIRE/BLD DUCT OVHT LOOP B
 (x) 6K19 IGN 2 ENG 1
 (y) 6K20 IGN 2 ENG 2
 (z) 6K21 IGN 2 ENG 3 (aa) 6K22 IGN 2 ENG 4 (ab) 6L11 FUEL CONT VALVE ENG 2 (ac) 6L12 FUEL CONT VALVE ENG 3 (ad) 6L13 FUEL CONT VALVE ENG 4 1) 180H4 FUEL BOOST PMP CONT AFT 2 & FWD 3 2) 414M18 FUEL BOOST PUMP MAIN 2 AFT
 S 844-303
 (2) Remove electrical power if it is not necessary (AMM 24-22-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 26-21-01
 ALL  ú ú 03 Page 431 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 FIRE CONTROL MODULE - ADJUSTMENT/TEST
_____________________________________
 1.  General_______
 A.  This procedure has one task. The task is a system test of the fire control module. These are the components tested in the system test:
 (1)  
Power source for the Fire Extinguishing Systems

 (2)  
Solenoids that release the fire handles.

 (3)  
Functions of the Engine fire handle

 (4)  
Functions of the APU fire handle (AMM 26-15-00/501)

 (5)  
APU Fire Extinguishing Squib Discharge Circuit Test (AMM 26-22-00/501)

 (6)  
APU Fire Extinguishing Bottle Pressure Switch Test
 (AMM 26-22-00/501)


 (7)  
Engine Fire Extinguishing Squib Discharge Circuit Test (AMM 26-21-00/501)

 (8)  
Engine Fire Extinguishing Pressure Switch Test (AMM 26-21-00/501)

 (9)  
Cargo Fire Extinguishing System Test - Squib Discharge Circuit (AMM 26-23-00/501)

 (10)
 Cargo Fire Extinguishing System Test - Bottle Pressure Switch (AMM 26-23-00/501)


 TASK 26-21-01-735-006
 2.  System Test - Fire Control Module_________________________________
 A.  References
 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
AMM 26-15-00/501, APU Fire Detection System

 (3)  
AMM 26-21-00/501, Engine Fire Extinguishing System

 (4)  
AMM 26-22-00/501, APU Fire Exinguishing System

 (5)  
AMM 26-23-00/501, Lower Cargo Compartment Fire Extinguishing System

 (6)  
AMM 29-11-00/201, Main Hydraulic Supply System

 (7)  
AMM 36-00-00/201, Pneumatic System

 (8)  
AMM 54-62-00/201, Nacelle Strut Access Panels

 (9)  
AMM 78-31-00/201, Thrust Reverser Systems
 
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本文链接地址:747-400 AMM 飞机维护手册 防火 FIRE PROTECTION 2(73)