EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-00
ALL ú ú 01 Page 582A ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
S 865-A32
(65)
Release the stabilizer-trim control-wheel-switches.
S 865-A33
(66)
Let the control columns go to the neutral position.
S 865-A34
(67)
Push the first officer's control column 3 to 4 inches (76-101 mm) forward and hold in position.
S 865-A35
(68)
At the same time, pull the captain's control column 3 to 4 inches (76-101 mm) aft and hold in position.
S 865-A36
(69)
Move the captain's stabilizer-trim control-wheel-switches down (airplane nose up).
(a)
Make sure the stabilizer moves.
S 865-A37
(70)
Move the captain's stabilizer-trim control-wheel-switches up (airplane nose down).
(a)
Make sure the stabilizer moves.
S 865-A38
(71)
Release the stabilizer-trim control-wheel-switches.
S 865-A39
(72)
Let the control columns go to the neutral position.
S 865-A40
(73)
Put the CENTER STAB TRIM SHUTOFF switch on the P10 panel to CUTOUT.
S 865-A41
(74)
Put the RIGHT STAB TRIM SHUTOFF switch on the P10 panel to NORM.
S 865-A42
(75)
Pull the first officer's control column 3 to 4 inches (76-101 mm) aft and hold in position.
S 865-A43
(76)
At the same time, push the captain's control column 3 to 4 inches (76-101 mm) forward and hold in position.
S 865-A44
(77)
Move the captain's stabilizer-trim control-wheel-switches down (airplane nose up).
(a)
Make sure the stabilizer moves.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-41-00
ALL ú ú 01 Page 582B ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
S 865-A45
(78)
Move the captain's stabilizer-trim control-wheel-switches up (airplane nose down).
(a)
Make sure the stabilizer moves.
S 865-A46
(79)
Release the stabilizer-trim control-wheel-switches.
S 865-A47
(80)
Let the control columns go to the neutral position.
S 865-A48
(81)
Push the first officer's control column 3 to 4 inches forward and hold in position (67-101 mm).
S 865-A49
(82)
At the same time, pull the captain's control column 3 to 4 inches (76-101 mm) aft and hold in position.
S 865-A50
(83)
Move the captain's stabilizer-trim control-wheel-switches down (airplane nose up).
(a)
Make sure the stabilizer moves.
S 865-A51
(84)
Move the captain's stabilizer-trim control-wheel-switches up (airplane nose down).
(a)
Make sure the stabilizer moves.
S 865-A52
(85)
Release the stabilizer-trim control-wheel-switches.
S 865-A53
(86)
Let the control columns go to the neutral position.
F.
Put the Airplane Back to Its Usual Condition
S 865-965
(1)
Remove the power from the right and center hydraulic systems (Ref 29-11-00/201).
S 865-966
(2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P11 panel:
(a)
11C6, CSEU 1L AC
or FLT CONT ELEC 1L AC
(b)
11C8, CSEU 2L AC
or FLT CONT ELEC 2L AC
(c)
11G17, CSEU 1R AC
or FLT CONT ELEC 1R AC
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 中國(guó)航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 飛行操縱 FLIGHT CONTROLS 4(51)
