27-48-00
ALL ú ú 02 Page 6 ú Sep 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
ELECT SYS CARD FILE, P50
MAIN EQUIPMENT CTR
RIGHT STABILIZER
POSITION MODULE SEE
B
LEFT STABILIZER
POSITION MODULE
SEE
B
CENTER STABILIZER POSITION MODULE SEE
P50
BIT/VERIFY
TEST GOOD
STAB RVDT
A
Stabilizer Position Module
Figure 3
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-48-00
ALL ú
ú 01 Page 7
ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-48-00
ALL ú ú 01 Page 8 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
FAULT ISOLATION/MAINT MANUAL
STABILIZER TRIM POSITION INDICATING SYSTEM
COMPONENT SHT 102 FIG. QTY ACCESS/AREA REFERENCE AMM
CIRCUIT BREAKER - 2 FLT COMPT, P11
STAB POS MOD C, C1525 1 11F19 *
STAB POS MOD L, C1523 1 11G15 *
STAB POS MOD R, C1526 1 11G24 *
STAB TRIM POS IND L, C1002 1 11H10 *
STAB TRIM POS IND R, C1009 1 11H19 *
INDICATOR - STAB TRIM POS L, N69 2 1 FLT COMPT, CONT STAND, P10 27-48-06
INDICATOR - STAB TRIM POS R, N68 2 1 FLT COMPT, CONT STAND, P10 27-48-06
MODULE - STAB TRIM LIMIT SW & POS XMTR C, M521 ; M108951 2 3 1 311AL, AFT FUSELAGE 27-48-01
MODULE - STAB TRIM LIMIT SW & POS XMTR L, M519 ; M108991 2 3 1 311AL, AFT FUSELAGE 27-48-01
MODULE - STAB TRIM LIMIT SW & POS XMTR R, M520 ; M108961 2 3 1 311AL, AFT FUSELAGE 27-48-01
MODULE STABILIZER POSITION C, M10409 4 1 119BL, MAIN EQUIP CTR, P50 27-48-03
MODULE STABILIZER POSITION L, M10408 4 1 119BL, MAIN EQUIP CTR, P50 27-48-03
TRANSFORMER - (FIM 31-01-36-1/101) CTR STAB POS PWR, T10031 MODULE STABILIZER POSITION R, M10410 4 1 119BL, MAIN EQUIP CTR, P50 27-48-03
* SEE THE WDM EQUIPMENT LIST
AIRPLANES WITH STAB TRIM LEVERS ON THE CONTROL STAND AIRPLANES WITH ALTERNATE STAB TRIM SWITCHES ON THE CONTROL STAND
Stabilizer Trim Position Indicating System - Component Index
Figure 101
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-48-00
ALL ú
ú 02 Page 101
ú Jan 20/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 FAULT ISOLATION/MAINT MANUAL
OVERHEAD PANEL, P11
CONTROL STAND PANEL, P10
SEE A
FLIGHT COMPARTMENT
STAB TRIM
LEVERS
(REF) S T
T R
A I
BM
NORM
CUT
OUT
STABILIZER TRIMSTABILIZER TRIM
CR
POSITIONPOSITION
STAB TRIM
INDICATOR, N68INDICATOR, N69
CONTROL STAND PANEL, P10
A1
1 AIRPLANES WITH STAB TRIM LEVERS ON THE CONTROL STAND
Horizontal Stabilizer Trim Control System - Component Location
Figure 102 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-48-00
ALL ú ú 02 Page 102 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
中國航空網(wǎng) www.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(88)
