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时间:2011-04-01 08:47来源:蓝天飞行翻译 作者:航空
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 22-11-33
 ALL  ú ú 01 Page 401 ú Mar 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (b)  P18 Circuit Breaker panel 1) AUTO FLT CONT SYS A MACH TRIM AC 2) AUTO FLT CONT SYS A MACH TRIM DC 3) AFDS MCP DC 4) Airplanes with mechanical aileron force limiter:
 AFDS AIL FORCE LIM 5) AUTO FLT CONT SYS A SNSR EXC AC 6) AUTO FLT CONT SYS A FCC DC 7) AUTO FLT CONT SYS A ENGAGE INTLK A 8) AUTO FLT CONT SYS A WARN LIGHT BAT
 S 914-014
 CAUTION: DO NOT TOUCH THE FCC BEFORE YOU DO THE PROCEDURE FOR DEVICES
___________ THAT ARE SENSITIVE TO ELECTROSTATIC DISCHARGE. ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE FCC.
 (3)  
Do the procedure for devices that are sensitive to electrostatic discharge (AMM 20-40-12/201).

 S 024-015

 (4)  
Remove the FCC (AMM 20-10-07/201).


 TASK 22-11-33-424-008
 3. Flight Control Computer Installation
____________________________________
 A. References
 (1)  
AMM 12-31-11/201, Access Doors and Panels

 (2)  
AMM 20-10-07/201, Electrical/Electronic Black Boxes

 (3)  
AMM 20-40-12/201, Electrostatic Discharge Sensitive Devices


 B. Access
 (1)  
Location Zone
 205 Electronic Compartment


 (2)  
Access Panel
 1201L Electronic Equipment Access Doorss

 

 C. Computer Installation
 S 914-009
 CAUTION: DO NOT TOUCH THE FCC BEFORE YOU DO THE PROCEDURE FOR DEVICES
_______ THAT ARE SENSITIVE TO ELECTROSTATIC DISCHARGE. ELECTROSTATIC DISCHARGE CAN CAUSE DAMAGE TO THE FCC.
 (1)  
Do the procedure for devices that are sensitive to electrostatic discharge (AMM 20-40-12/201).

 (2)  
Install the FCC (AMM 20-10-07/201).


 S 424-010
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 22-11-33
 ALL  ú ú 01 Page 402 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (3)  S 864-004Close all of the autopilot and mach trim circuit breakers.
 NOTE:____ Make sure that you close the AFCS A FCC DC and AFCS B FCC DC circuit breakers last.
 (4)  S 744-005Do the Flight Control Computer Adjustment/Test procedure (AMM 22-11-33/501).

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 22-11-33
 ALL  ú ú 01 Page 403 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 FLIGHT CONTROL COMPUTER - ADJUSTMENT/TEST
_________________________________________
 1.  General
_______
 A.  This procedure contains one task. The task does a DFCS BITE test of the Flight Control Computer (FCC).
 TASK 22-11-33-745-007
 2.  Flight Control Computer Test
____________________________
 A.  References
 (1)  24-22-00/201, Electrical Power Control
 B.  Access
 (1)  Location Zone
 102 Control Cabin

 C.  Prepare for DFCS BITE test
 S 865-001
 (1)  
Supply electrical power (Ref 24-22-00/201).

 S 865-008

 (2)  
Make sure that the circuit breakers (on the P6 and P18 circuit breaker panels) for the systems shown below are closed and that the systems will operate:

 (a)  
FMCS

 (b)  
DADC (No. 1 and 2)

 (c)  
LANDING GEAR AIR/GND RELAY & LIGHTS

 (d)  
AFCS (A and B)

 


 NOTE: Make sure that you close the AFCS A FCC DC and AFCS B
____ FCC DC circuit breakers last.
 (e)  
Mach Trim
 
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