27-31-41
ALL ú ú 01 Page 407 ú Mar 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
ELEVATOR BALANCE PANELS - ADJUSTMENT/TEST
_________________________________________
1. General_______
A. This procedure has one task. The task is a test of the elevator balance panel.
B. The test is the same for the left or the right elevator.
TASK 27-31-41-705-008
2. Elevator Balance Panels Test____________________________
A. Special Tools and Equipment
(1)
F80055-1 - Trammel Bar
B.
Standard Tools and Equipment
(1)
Spring scale (compression type) - 0-15 pound capacity, in 1 pound increments
(2)
Loading block - 17 inches long, 2 inch x 4 inch wood block
(3)
Scale - 0-2 feet, in inches and tenths of an inch increments
(4)
Scale - 0-6 inches, in tenths and hundredths of an inch increments
C.
References
(1)
AMM 27-31-00/201, Elevator and Tab Control System
D.
Access
(1)
Location Zone
101 Control Cabin, LH
102 Control Cabin, RH
704 Tail Cone
711 Elevator and Tab, LH
712 Elevator and Tab, RH
(2)
Access Panels
3801 Tail Cone Access Door, LH
3802 Tail Cone Access Door, RH
9107 Access Panel Trailing Edge, LH
9207 Access Panel Trailing Edge, RH
9108 Access Panel Trailing Edge, LH
9208 Access Panel Trailing Edge, RH
9109 Access Panel Trailing Edge, LH
9209 Access Panel Trailing Edge, RH
E.
Procedure
(1)
Remove the elevator hydraulic systems A and B (AMM 27-31-00/201).
S 865-002
(2)
Use the trammel bar to set the B dimension at 41.57 |0.05 inches (Fig. 501).
S 865-003
(3)
Move the control columns fully forward and attach DO-NOT-MOVE tags.
(a)
Make sure the control columns are held in this position.
S 865-001
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27-31-41
ALL ú ú 02 Page 501 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 035-004
CAUTION:_______ DO NOT PERMIT THE INNER RACE OF THE CRANK BEARING TO TURN TO A
POSITION WHERE THE ROLLERS CAN FALL THROUGH THE HOLE IN THE
INNER RACE. THIS CAN CAUSE DAMAGE TO EQUIPMENT.
(4)
Remove the bolts that attach the aft end of each elevator control pushrod to its elevator (Fig. 502).
S 865-005
(5)
Remove the DO-NOT MOVE tags and move the control columns fully aft to the stops:
(a)
Remove the clevis of the elevator control pushrod from the elevator.
(b)
Make sure the control columns are held in this position and attach the DO-NOT-MOVE tags.
S 225-010
(6)
Measure the breakaway forces:
(a)
Hold a loading block against the elevator rear spar adjacent to the elevator inboard rib.
(b)
Push the loading block by hand until the trailing edge of each elevator aligns with the index mark, then release (Fig. 502).
____ 1 "B" DIMENSION IS MEASURED BETWEEN CENTER OF UPPER AND LOWER GIMBAL PINS NOTE: STABILIZER TRIM JACKSCREW SHOWN WITH STABILIZER LEADING EDGE AT ZERO DEGREES "B" DIM 1 TRAMMEL BAR
FWD
Stabilizer Trim Jackscrew Setting
Figure 501
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 中國航空網 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 2(169)
