FWD 6. SCREW 2. BOLT 8. POCKET (4 LOCATIONS)ASSEMBLY
2
LOWER SIDE COVER
2. NUT
CONTROL STAND (RIGHT SIDE IS SHOWN, LEFT SIDE IS OPPOSITE) 1
A
1 AIRPLANES WITH A TIE ROD THROUGH THE SPLINE SHAFT.
2 AIRPLANES WITHOUT A TIE ROD THROUGH THE SPLINE SHAFT
Stabilizer Trim Control Wheel Installation
Figure 401
L85886
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-64
ALL ú ú 01 Page 402 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 414-007
(2)
Install the stabilizer trim control wheel on the control stand:
(a)
Install the stabilizer trim control wheel on the shaft with the handle 90 +/- 15 degrees apart from the handle on the other stabilizer trim control wheel.
(b)
Install (finger tight) the fastener that attaches the
stabilizer trim wheel to the splined shaft.
NOTE: If you are installing a nut, discard the old
____ nut and use a new nut when you install the trim wheel. The old bolt can be used again.
1) AIRPLANES WITH THE STABILIZER TRIM WHEEL TIE ROD NUT; Torque the nut to 60 - 70 lb-in (6.8 - 7.9 N-m).
NOTE: Two tie rod threads need to show after torquing
____ the nut. 2) AIRPLANES WITH THE STABILIZER TRIM WHEEL BOLT; Torque the bolt to 150 - 170 lb-in (17.0 - 19.2 N-m).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-64
ALL ú ú 01 Page 403 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
PRIMARY STABILIZER TRIM ACTUATOR - REMOVAL/INSTALLATION
_______________________________________________________
1. General_______
A. This procedure has two tasks, one for the removal and one for the installation of the stabilizer trim electric actuator or primary stabilizer trim actuator (which is referred to as the actuator). The procedure has these parts:
(1)
The removal of the actuator
(2)
The installation of the actuator
(3)
An operational test of the actuator.
TASK 27-41-71-004-014
2. Primary Stabilizer Trim Actuator Removal (Fig. 401)________________________________________
A. Access
(1)
Location Zones
101 Control Cabin, LH
102 Control Cabin, RH
702 Tail Compartment Access Door
(2)
Access Panels
3701 Stabilizer Trim Access Door
B.
Procedure
S 014-002
(1)
Open the access door 3701.
S 864-003
(2)
Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
AIRPLANES WITH PRIMARY STABILIZER TRIM ACTUATOR; P18-0 Circuit Breaker Panel 1) AUTOPILOT STABILIZER TRIM SERVO
S 024-004
(3)
Remove the actuator:
(a)
Remove electrical connector(s) from the actuator.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-71
ALL ú ú 03 Page 401 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
Primary Stabilizer Trim Actuator Installation
Figure 401
L86879
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-71
ALL ú ú 03 Page 402 ú Mar 12/01
中國航空網(wǎng) www.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 飛行操縱 FLIGHT CONTROLS 3(107)
