(2)
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
C. Access
(1) Location Zone
113 Area forward of NLG wheel well (left)
D. Prepare for Removal
S 864-002
(1) Open these circuit breakers on the overhead circuit breaker panel, P11, and attach DO-NOT-CLOSE tags:
(a)
11C11, STICK SHAKER LEFT
(b)
11E17, FLT CONT COMPUTER POWER LEFT
(c)
11E20, FLT CONT COMPUTER PWR CENTER
(d)
11E35, FLT CONT COMPUTER PWR RIGHT
(e)
11H11, STAB TRIM CONT L
(f)
11H17, FLT CONT SHUTOFF TAIL LEFT
(g)
11H18, FLT CONT SHUTOFF TAIL CENTER
(h)
11H20, STAB TRIM CONT RIGHT
(i)
11H28, FLT CONT SHUTOFF TAIL RIGHT
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A
757
MAINTENANCE MANUAL
SEE A
113AL FORWARD ACCESS DOOR CAPTAIN'S CONTROL COLUMN
A SEE B
CONTROL COLUMN
A CONTROL COLUMNS CONTROL COLUMN BASE CRANK AND SHAFT ASSEMBLY
A
STOP CRANK AND SHAFT ASSEMBLY TRANSDUCER MICRO-ADJUSTABLE THUMB NUT ROD ASSEMBLY CRANK ARM
RIG PIN E/ST6 HOLE A-A FWD LOCKWIRE COLLAR BRACKET
TRANSDUCER INSTALLATION
B
Control Column Position Transducer Installation Figure 401
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A
757 MAINTENANCE MANUAL
(j)
11J7, FLIGHT RECORDER AC
(k)
11J8, FLIGHT RECORDER DC
(l)
11J21, STICK SHAKER RIGHT
(m)
11S1, AIDS SENSOR
S 864-003
(2)
Remove the power from the left, right, and center hydraulic systems (AMM 29-11-00/201).
S 864-004
(3)
Set the control column in the neutral position and attach DO-NOT-OPERATE tags to the two control wheels.
S 434-005
(4) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 AMM 飞机维护手册 仪表 CHAPTER 31 - INSTRUMENTS 1(140)
