• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-21 08:08来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

STABILIZER 
TRIM SWITCHES 

APL 
NOSE DN
APL 
NOSE UP 
STAB TRIM  STAB TRIM 
ALTN 
STAB TRIM 
NOSE APL  0  NOSE APL  0 
DOWN  DOWN 
2  2 
S  S 
A T  4  A T  4 
B  6  B  6 
T  T 
R  8  R  8 
I  I 
M  10  M  10 
12  12 
UP NOSE APL F F O 16 14  NORM  UP NOSE APL F F O 16 14 
CUT 
OUT 
C  R 
STAB TRIM 
POSITION  STABILIZER 
INDICATOR  TRIM SHUTOFF  CONTROL STAND PANEL, P10 
(2 LOCATIONS)  SWITCHES 

Horizontal Stabilizer Trim Control System 
Figure 501 (Sheet 2) 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH ALTERNATE STAB TRIM ú

 27-48-00
 SWITCHES ON THE CONTROL STAND  ú ú 02 Page 504 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
MASTER CAUTION AND WARNING LIGHTS (2 LOCATIONS)

PILOT'S CENTER INSTRUMENT PANEL


Horizontal Stabilizer Trim Control System
Figure 501 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-48-00
 ALL  ú
 ú  02  Page 505
 ú  Mar 20/91 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

STABILIZER COMPARTMENT COMPONENTS SEE A 
SP2B  SLA  SLB 
SLA  SP1B SLB  SP1A  SP2A  STABILIZER 

RIG PIN 
E/ST-5 
HOLE 
STABILIZER TRIM  RIG PIN 
AFT QUADRANT  E/ST-4 HOLE 
SEE  B  FWD 
STABILIZER TRIM LIMIT 
SWITCH AND POSITION  STABILIZER TRIM 
TRANSMITTER MODULE  BALLSCREW 
(3 LOCATIONS)  RIG PIN  ACTUATOR 
CONNECTOR ELECTRICAL  E/ST-3 HOLE  SEE  C 
(EXAMPLE)  A 

Stabilizer Compartment Components
Figure 502 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH STAB TRIM LEVERS ON THE ú

 27-48-00
 CONTROL STAND  ú
 ú  02  Page 506
 ú  May 28/00 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

SEE A STABILIZER COMPARTMENT COMPONENTS 
SP2B  SP2A  SP3B  SP3A STABILIZER 
SP1B  SP1A 

STABILIZER TRIM LIMIT 
SWITCH AND POSITION 
TRANSMITTER MODULE  RIG PIN 
(3 LOCATIONS)  HOLE E/ST5 

RIG PIN HOLE E/ST4 
FWD (EXAMPLE) ELECTRICAL CONNECTOR  RIG PIN HOLE E/ST3  CSEE ACTUATOR BALLSCREW STABILIZER TRIM 

Stabilizer Compartment Components Figure 502 (Sheet 2) 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH ALTERNATE STAB TRIM ú

 27-48-00
 SWITCHES ON THE CONTROL STAND  ú ú 02 Page 507 ú May 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL 
ST1A  SLA ST2B  ST2A  SLB 
ST1B 

STABILIZER TRIM CONTROL MODULE (2 LOCATIONS) RIG PIN
RIG PIN
HOLE E/ST2
HOLE E/ST1
STABILIZER TRIM AFT QUADRANT
1  THE GAGE ASSEMBLY CAN BE USED TO ACCURATELY SET THE STABILIZER DIMENSION B TO 19.07 |0.01 INCHES.
TO USE, PUT THE GAGE ASSEMBLY AGAINST THE BALLSCREW SUCH THAT THE LOWER BOLTHEAD IS ON THE SHOULDER OF THE LOWER STOP. MAKE SURE THAT THE FEELER BLADE CANNOT BE PUT BETWEEN THE GAGE ASSEMBLY UPPER BOLTHEAD AND THE SHOULDER OF THE UPPER STOP. MAKE SURE THE SHOULDER OF THE UPPER STOP DOES NOT TOUCH THE UPPER BOLTHEAD.
 
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(91)