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(e)
(f)
(g)
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737-300/400/500MAINTENANCE MANUAL
2) Adjust the bulb seal to have an clearance of
0.03 +0.03/-0.03 inch between the seal and the aft side of
the rib. 3) Tighten the seal mounting bolts. 4) Make sure the tolerance between the bulb seal and the rib
is 0.03 +0.03/-0.03 inch.At the balance bays No. 1, 2, 3, or 4 (Fig. 502, View D): Adjust the bulb seals between the balance panel and the rib of the stabilizer trailing edge: 1) Loosen the seal mounting bolts. 2) Adjust the bulb seal to have a clearance of 0.02 +/- 0.01
inch between the seal and the rib. 3) Tighten the seal mounting bolts. 4) Make sure the clearance between the bulb seal and the rib
is 0.02 +/- 0.01 inch.At the balance bays No. 1, 2, 3, or 4 (Fig. 502, View D): Adjust the flat seals between the idler hinge of the balance panel and the rib of the stabilizer trailing edge: 1) Loosen the seal mounting bolts. 2) Adjust the flat seal to have a clearance of 0.01
+0.06/-0.00 inch between the seal and the rib. 3) Make sure there is a clearance of 0.20 inch between the
flat seal and the bulb seal of the balance panel. 4) Tighten the seal mounting bolts. 5) Make sure the clearance between the flat seal and the rib
is 0.01 +0.06/-0.00 inch.At the elevator inboard rib (Fig. 502, View E): Adjust the elevator-to-body seals between the elevator and the tail cone: 1) Loosen the seal mounting bolts. 2) Adjust the elevator-to-body seal to have a clearance of
0.02 +/- 0.01 inch between the seal and the tail cone. 3) Tighten the seal mounting bolts. 4) Make sure the clearance between the elevator-to-body seal
and the tail cone is 0.02 +/- 0.01 inch.
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A 737-300/400/500MAINTENANCE MANUAL
(h) At the elevator inboard rib No. 1: Adjust the gap between the bulb seal on the stabilizer and the elevator (Fig. 502): 1) Loosen the adjustment screw. 2) Adjust the screw to have a clearance of 0.03 +/- 0.03 inch gap between the bulb seal on the stabilizer and the elevator.
3) 4) Tighten the screw.Make sure the clearance between the bulb seal on the stabilizer and the elevator is 0.03 +/- 0.03 inch.
S 865-006
(5) Do this task: "Put the Elevator Hydraulic Systems A and B Back to the Condition Before the Pressure Removal" (Ref 27-31-00/201).
S 715-007
(6) Do this task: "System Test - Elevator Surface Friction and Balance" (Ref 27-31-00/501).
S 415-008
(7) Install the access panels 9107, 9108, 9109, 9149, and 9150, or 9207, 9208, 9209, 9249, and 9250.
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737-300/400/500MAINTENANCE MANUAL
CONTROL COLUMN - REMOVAL/INSTALLATION
_____________________________________
1. General_______
A. This procedure has two tasks, one for the removal and one for the installation of the control column. The procedure has these parts:
(1)
The removal of the control column
(2)
The installation of the control column
(3)
A test of the control column.
TASK 27-31-51-004-001
2. Control Column Removal______________________
A. Special Tools and Equipment
(1)
F52485-500, or 4MIT65B80207-1 - Bubble Protractor
(2)
Rig Pin (E-1) - 0.309/0.311 inch diameter, 6.7 |0.25 inches long
NOTE: The rig pin is a part of the kit F70207-69, -78 or -83.
____
B. References
(1)
27-31-00/201, Elevator and Tab Control System
C.
Access
(1)
Location Zone
101 Control Cabin, LH
102 Control Cabin, RH
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本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 2(173)
