S 865-C11
(9)
Move the captain's stabilizer-trim control-wheel-switches down (airplane nose up).
(a)
Make sure that the stabilizer moves.
S 865-C12
(10)
Let the stabilizer move until it stops.
S 865-C13
(11)
Release the stabilizer-trim control-wheel-switches.
S 865-C14
(12)
Put the CENTER STAB TRIM SHUTOFF switch on the P10 panel to CUTOUT.
S 215-C15
(13)
Make sure that dimension B on the stabilizer jackscrew is 0.80 to 1.40 inches (20-35 mm).
S 215-C16
(14)
Extend the trailing edge flaps to the 15 unit position (Ref 27-51-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-00
ALL ú ú 02 Page 529 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
S 865-C17
(15)
Do the deactivation procedure for the trailing edge flap system (Ref 27-51-00/201).
S 865-C18
(16)
Put the CENTER STAB TRIM SHUTOFF switch on the P10 panel to NORM.
S 865-C19
(17)
Move the captain's stabilizer-trim control-wheel-switches up (airplane nose down).
(a)
Make sure that the stabilizer moves.
S 865-C20
(18)
Let the stabilizer move until it stops then release the stabilizer-trim control-wheel-switches.
S 865-C21
(19)
Put the CENTER STAB TRIM SHUTOFF switch on the P10 panel to CUTOUT.
S 215-C22
(20)
Make sure that dimension B on the stabilizer jackscrew is 24.86 to 25.46 inches (631.4-646.6 mm) (Fig. 502).
S 865-C23
(21)
Put the RIGHT STAB TRIM SHUTOFF switch on P10 to NORM.
S 865-C24
(22)
Move the captain's stabilizer-trim control-wheel-switches down (airplane nose up).
(a)
Make sure the stabilizer moves.
S 865-C25
(23)
Let the stabilizer move until it stops.
S 865-C26
(24)
Release the stabilizer-trim control-wheel-switches.
S 865-C27
(25)
Put the RIGHT STAB TRIM SHUTOFF switch on the P10 panel to CUTOUT.
S 215-C28
(26)
Make sure that dimension B on the stabilizer jackscrew is 0.80 to 1.40 inches.
(27)
Put the RIGHT STAB TRIM SHUTOFF switch on the P10 panel to NORM.
S 865-C29
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-00
ALL ú ú 02 Page 530 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
S 865-C30
(28)
Move the captain's stabilizer-trim control-wheel-switches up (airplane nose down).
(a)
Make sure that the stabilizer moves.
S 865-C31
(29)
Let the stabilizer move until it stops.
S 865-C32
(30)
Release the stabilizer-trim control-wheel-switches.
S 865-C33
(31)
Put the RIGHT STAB TRIM SHUTOFF switch on the P10 panel to CUTOUT.
S 215-C34
(32)
Make sure that dimension B on the stabilizer jackscrew is 24.86 to 25.46 inches (631.4-646.6 mm).
S 865-C35
(33)
Move the flaps to the fully retracted position (Ref 27-51-00/201).
S 865-C36
(34)
Put the RIGHT STAB TRIM SHUTOFF switch on the P10 panel to NORM.
S 865-C37
(35)
Move the captain's stabilizer-trim control-wheel-switches down (airplane nose up).
(a)
Make sure the stabilizer moves.
S 865-C38
(36)
Let the stabilizer move until it reaches 6.0 units of trim, as shown on the control stand stabilizer-position-indicators.
S 865-C39 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 4(16)
