PULLEY
E
Manual Extension Control Mechanism Installation
Figure 401 (Sheet 2)
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32-34-11
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 024-009
(8) Remove the control mechanism with the control drums (10) from the airplane structure and move the outboard end of mechanism forward.
TASK 32-34-11-404-010
3. Manual Extension Control Mechanism Installation (Fig. 401)_______________________________________________
A. References
(1)
32-34-00/501, Manual Extension System - Main Landing Gear
(2)
32-35-00/501, Manual Extension System - Nose Landing Gear
B.
Procedure to Install the Control Mechanism of the Manual Extension
S 424-011
(1)
Put the control drums (10) and the spacer (7) in the cable guard assembly (8).
S 024-012
(2)
Put the control mechanism in its position on the airplane structure.
S 424-013
(3)
Put the shaft (4) in through the support (3), the cable guard assembly (8), the spacer (7), the control drums (10), and the structure.
S 434-014
(4)
Install the bolt (5) which attach the inboard cable guard (6) to the support (3).
S 434-015
(5)
Install the washer (12) and the nut (13) on the shaft (4).
(a)
Tighten the nut to 50 - 350 pound-inch and install the cotter pin.
S 434-016
(6)
Put the elevator cable EAR (9) in through the slot in the clip on the outboard cable guard.
(a)
Install the grommet on the clip.
S 434-017
(7)
Install the control cables (14) on the control drums (10) with the cable retainers (1).
S 434-018
(8)
Install the cables (2) of the manual extension handle on the control drums (10) with the cotter pins.
(a)
Bend the end of the cotter pin into the drum.
S 434-019
(9)
Connect the cables MLGEA-L and MLGEA-R at approximately body station
420.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 434-020
(10)
Connect the cable MNGEA.
S 824-021
(11)
Adjust the manual extension system of the main landing gear (Ref 32-34-00/501).
S 714-022
(12)
Do a test on the operation of the manual extension system of the main landing gear (Ref 32-34-00/501).
S 824-023
(13)
Adjust the manual extension system of the nose landing gear (Ref 32-35-00/501).
S 714-024
(14)
Do a test on the operation of the manual extension system of the nose landing gear (Ref 32-35-00/501).
S 414-025
(15)
Install the ceiling panels of the cargo compartment at approximately body station 420.
(16)
Install the cabin floor panel (15).
S 414-026
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