S 864-028
(2)
Close these circuit breakers and remove the DO-NOT-CLOSE tags:
(a)
P6 Circuit Breaker Panel
1) AUTO FLT CONT SYS B MACH TRIM AC
2) AUTO FLT CONT SYS B MACH TRIM DC
3) AFDS MCP CRS-2
4) AUTO FLT CONT SYS B SNSR EXC AC
5) AUTO FLT CONT SYS B FCC DC
6) AUTO FLT CONT SYS B ENGAGE INTLK B
7) AUTO FLT CONT SYS B WARN LIGHT BAT
(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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-11-25
ALL ú ú 01 Page 407 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
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 864-029
(3)
Remove the hydraulic power if it is not necessary (Ref 29-15-00/201).
S 864-030
(4)
Remove the electrical power if it is not necessary (Ref 24-22-00/201).
TASK 22-11-25-214-039
4. Shear Rivet Inpection
_____________________
NOTE: This is a scheduled maintenance task.
____
A. Procedure
S 214-037
(1)
Try to turn the shear rivets by hand to see if they are loose.
S 214-045
(2)
Quickly move the fitting and the arm of the lever assembly in opposite directions.
S 214-051
(3)
If there is movement between the parts, one or both of the rivets are loose.
S 214-052
(4)
Put a 0.0375 to 0.0395inch (0.9525 to 1.0033 millimeter) diameter pin into the rivet inspection hole.
(a)
Make sure that the pin moves freely.
(b)
Repeat this step for the other rivet inspection hole.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-11-25
ALL ú ú 02 Page 408 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 214-050
(5) If rivets are loose or if pins will not fit, then replace the lever assembly.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-11-25
ALL ú ú 01 Page 409 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
AUTOPILOT AILERON ACTUATOR - ADJUSTMENT/TEST
____________________________________________
1. General_______
A. This procedure contains three tasks. The first task and second task are the adjustment of the autopilot aileron actuator. The first task uses the F80217-125 test set for the adjustment of the actuator. The second task uses the DFCS BITE test for the adjustment of the actuator (airplanes with -912 and on FCC). You can use one of these tests to adjust the actuator. The third task is the autopilot aileron actuator test.
TASK 22-11-25-825-043
2. Autopilot Aileron Actuator Adjustment (F80217-125 test set)_____________________________________
A. References
(1)
AMM 22-11-00/501 or AMM 22-11-01/501, Digital Flight Control System
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 27-11-00/501, Aileron and Aileron Trim System
(4)
AMM 29-15-00/201, Hydraulic A, B, and Standby System
(5)
AMM 32-00-01/201, Ground Lock Assemblies
(6)
OHM 27-09-05, Lever Assembly, Aileron/Elevator Autopilot Actuator Shear
B. Access
(1) Location Zone
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(172)
