(2)
29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
B.
Access
(1)
Location Zones
211/212 Control Cabin
C.
Prepare for the Removal
S 864-002
(1)
Supply electrical power (Ref 24-22-00).
S 864-003
(2)
Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to the CUTOUT position.
S 864-004
(3)
Open these circuit breakers on the overhead panel, P11, and attach DO-NOT-CLOSE tags:
(a)
11B19, STAB TRIM ALT (IF INSTALLED)
(b)
11C12, STAB TRIM SHUTOFF LEFT
(c)
11C13, STAB TRIM SHUTOFF RIGHT
(d)
11H10, STAB TRIM LEFT POS IND
or STAB TRIM POS IND L
(e)
11H11 or 11C05, STAB TRIM CONT L
(f)
11H19, STAB TRIM POS IND RIGHT
(g)
11H20, STAB TRIM CONT R
D.
Remove the Position Indicator (Fig. 401)
(1)
Remove the access panel from the side of the control stand.
S 014-005
NOTE: To remove the captain's position indicator, remove the left
____ side panel. To remove the first officer's position indicator, remove the right side panel.
S 034-006
(2) Disconnect the electrical connector from the position indicator.
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27-48-06
ALL ú ú 01 Page 401 ú Jan 20/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
STAB TRIM LEVERS
SCREW (4 LOCATIONS)
CAPTAIN'S STABILIZER POSITION INDICATOR CONTROL STAND PANEL, P10
SEE A
FLIGHT COMPARTMENT
ST
TR
AI
BM
NORM
CUT
OUT
CR
STAB TRIM
STABILIZER TRIM
SHUTOFF SWITCHES
CONTROL STAND PANEL, P10
A
Stabilizer Position Indicator Installation Figure 401 (Sheet 1)
FIRST OFFICER'S STABILIZER POSITION INDICATOR
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STAB TRIM LEVERS ON THE ú
27-48-06
CONTROL STAND ú ú 02 Page 402 ú Dec 20/90
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A
757
MAINTENANCE MANUAL
CONTROL STAND PANEL, P10
SEE B
ALTERNATE
STAB TRIM
FLIGHT COMPARTMENT
SWITCHES
APL NOSE DN
APL NOSE UP
ALTN STAB TRIM
NORM
CUT OUT
CR
STAB TRIM
SCREW
(4 LOCATIONS) FIRST STABILIZER TRIM
CAPTAIN'S STABILIZER
OFFICER'S POSITION SHUTOFF
CONTROL STAND PANEL, P10 STABILIZER INDICATOR SWITCHES
POSITION B INDICATOR
Stabilizer Position Indicator Installation Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH ALTERNATE STAB TRIM ú
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SWITCHES ON THE CONTROL STAND ú ú 02 Page 403 ú Dec 20/90
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A
757
MAINTENANCE MANUAL
S 034-007
(3)
Remove the screws that hold the position indicator to the control stand.
S 024-008
(4)
Remove the position indicator from the control stand.
TASK 27-48-06-424-009
3. Install the Position Indicator
______________________________
A. References
(1)
24-22-00/201, Electrical Power - Control
(2)
29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems
B. 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 飞行操纵 FLIGHT CONTROLS 4(106)
