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MAINTENANCE MANUAL
SPREADER BAR
JACK ASSEMBLY (2 LOCATIONS)
BALL NUT LOCK
HORIZONTAL STABILIZER JACKSCREW ACCESS DOOR, 312A FWD
HANDLING TOOL USAGE
Stabilizer Trim Drive Mechanism Wear Limits
Figure 601 (Sheet 5)
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MAINTENANCE MANUAL
A A SEE A NOTE:____ STA 2436 BAR SPREADER PITOT AND STATIC POINTS FOR DISCONNECTION SEE B PITOT AND STATIC LINES MAY NEED TO BE REMOVED TO INSTALL SPREADER BAR.
(2 LOCATIONS) JACK ASSEMBLY
SEE C
BULKHEAD (STA 2460)
FWD JACKSCREW ACCESS DOOR, 312A HORIZONTAL STABILIZER
A
Stabilizer Trim Drive Mechanism Wear Limits
(Jack Assembly Installation)
Figure 602 (Sheet 1)
M04343
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MAINTENANCE MANUAL
Stabilizer Trim Drive Mechanism Wear Limits
(Jack Assembly Installation)
Figure 602 (Sheet 2)
M04348
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MAINTENANCE MANUAL
HORIZONTAL STABILIZER
CENTER SECTION
BULKHEAD
TRUSS
JACK
ASSEMBLY
SEE D
INDICATOR
ASSEMBLY
FWD
HYDRAULIC
PUMP ASSEMBLY
SEE D
A-A
JACK ASSEMBLY
HYDRAULIC PUMP ASSEMBLY
D
Stabilizer Trim Drive Mechanism Wear Limits
(Jack Assembly Installation)
Figure 602 (Sheet 3)
M04353
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TASK 27-41-06-206-015
4. Stabilizer Trim Drive Mechanism Visual Inspection_________________________________________________
A. Standard Tools and Equipment
(1)
A Flash Light
B.
References
(1)
AMM 06-09-05/201, Body Section 48 Access Doors and Panels
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 27-41-06/401, Stabilizer Trim Drive Mechanism
(4)
AMM 29-11-00/201, Main Hydraulic Supply System
C.
Access
(1)
Location Zone
311 Area Aft of Pressure Bulkhead, LH
312 Area Aft of Pressure Bulkhead, RH
(2)
Access Panel 312A Horizontal Stabilizer Jackscrew Access Door
D.
Procedure
S 866-016
(1)
Remove the hydraulic power for hydraulic systems No. 2 and No. 3 (AMM 29-11-00/201).
S 866-017
(2) 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 3(182)
