27-51-82
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
ELECTRICAL CONNECTOR
SEE B
SEE A
VALVE MOTOR CONNECTOR ELECTRICAL HOUSING A FWD
SCREWS
BOLTS
VALVE
VALVE CAM (5 LOCATIONS) 0-RINGS
Figure 401 Trailing Edge Flap Bypass Valve Installation B
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-82
ALL ú ú 01 Page 402 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
S 024-010
(3)
Remove the bypass valve assembly:
(a)
Remove the fasteners that attach the bypass valve assembly to the structure.
(b)
Remove the bypass valve assembly from the airplane.
TASK 27-51-82-404-011
3. Trailing Edge Flap Bypass Valve Assembly Installation
_____________________________________________________
A. Consumable Materials
(1)
D00288 Lubricant, Skydrol Assembly - MCS 352
(2)
D00148 Hydraulic Fluid, BMS 3-11, Type IV, Class 1
B.
References
(1)
12-12-00/301, Hydraulic Reservoir
(2)
27-51-82/501, Trailing Edge Flap Bypass Valve
(3)
AMM 29-09-00/201, Hydraulic Reservoir Pressurization System
C.
Access
(1)
Location Zones
101, 102 Control Cabin
217 Right Main Wheel Well
D.
Procedure
S 424-059
(1)
Install the bypass valve assembly (Fig. 401):
(a)
Attach the bypass valve assembly to the structure with the fasteners.
S 434-012
(2)
Connect the hydraulic lines to the bypass valve assembly:
(a)
Remove the caps from the hydraulic lines and ports.
(b)
If it is necessary, install the O-rings and unions in the bypass valve: 1) Apply the hydraulic fluid or the assembly lube to the
O-rings. 2) Install an O-ring and a union in each port of the housing.
(c)
Connect the hydraulic lines to the bypass valve assembly.
S 434-018
(3)
Connect the electrical connector to the valve motor.
E.
Put the Airplane Back to Its Usual Condition
S 864-019
(1)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P6-2 Panel
1) ALT TE FLAP DRIVE
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-82
ALL ú ú 01 Page 403 ú Nov 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
2) FLAP (SHUTOFF VALVES)
S 864-020
(2)
Do this task: "Restore Airplane To Normal" (AMM 29-09-00/201).
S 724-022
(3)
Do this task: "Trailing Edge Flap Bypass Valve Functional Test" (Ref 27-51-82/501).
S 614-023
(4)
Do this task: "Service Hydraulic Reservoir" (Ref 12-12-00/301).
TASK 27-51-82-004-024
4. Trailing Edge Flap Bypass Valve and Valve Motor Removal_______________________________________________________
A. References
(1)
AMM 29-09-00/201, Hydraulic Reservoir Pressurization System
(2)
29-15-00/201, Hydraulic Systems A, B and Standby
B.
Access
(1)
Location Zones
101, 102 Control Cabin
217 Right Main Wheel Well
C.
Prepare for the Removal
S 864-025
(1)
Do this task to depressurize hydraulic system B: "Depressurize Hydraulic System A, B, or Standby (Ref 29-15-00/201).
S 864-026
(2)
Do this task to depressurize the hydraulic system B reservoir: "Depressurize Hydraulic Reservoir" (AMM 29-09-00/201).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 4(145)