27-31-00

 CONTROL STAND  ú
 ú  02  Page 505
 ú  Sep 20/96 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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

STEPS THAT FOLLOW:
1.  
PUT THE GAGE ASSEMBLY AGAINST THE BALLSCREW SUCH THAT THE BOLT HEADS ARE ON THE SHOULDERS OF THE UPPER AND LOWER STOPS

2.  
MAKE SURE THAT THE FEELER BLADE CAN BE PUT BETWEEN THE BOLT HEAD OF THE GAGE ASSEMBLY AND ON THE SHOULDER OF THE UPPER STOP (THIS WILL PREVENT PRELOADING)

Measurement of Stabilizer Dimension B
Figure 502

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-00
 ALL  ú ú 02 Page 506 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

Not Used
Figure 503

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-00
 ALL  ú ú 02 Page 507 ú Mar 20/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

E1A
E1B  TURNBUCKLE 
(EXAMPLE) 
CONTROL ROD 
FIRST OFFICER'S 
FORWARD QUADRANT 
E2B 
A  E2A 
E1B 
E1A 
ROD CONTROL  A  E1A  E2A  E2B  E1B  E2B 
CAPTAIN'S 
FORWARD QUADRANT/ TENSION REGULATOR  E1B  E1A E2A 

AFTCONTROL COLUMN QUADRANTS
CONTROL ROD FORWARD QUADRANT/E/ST6 TENSION REGULATOR
RIG PIN HOLE SEE A
FWD
A-A
TENSION REGULATOR HOLDING TOOL
CONTROL ROD
TENSION 
INBD  BSEE SCALE REGULATOR  CRANK  TENSION REGULATOR  FWD
FORWARD QUADRANT/TENSION REGULATOR  TENSION REGULATOR SCALE 
(CAPTAIN'S QUADRANT ONLY) A  B 

Elevator Control Cable Adjustment
Figure 504 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-00
 ALL  ú ú 05 Page 508 ú Mar 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
AMBIENT TEMPERATURE (`C) -62 -40 -29-18-7 4 16 27 38 49 60 71
H
9
8

AMBIENT TEMPERATURE (`C) -62 -40-18 4 27 49
7
260
6 220

SCALE POSITION ON THE TENSION REGULATOR
5
CABLE RIG LOAD (LBS)
180
4
140
3
100
2
60
1
C
20
-65 -40 -20 0 20 40 60 80 100 120 140 160

-80-40 0 40 80 120
70 AMBIENT TEMPERATURE (`F) AMBIENT TEMPERATURE (`F)
TENSION REGULATOR CABLE TENSION vs TEMPERATURE SCALE SETTING vs TEMPERATURE (FIRST OFFICER'S FORWARD QUADRANT) (CAPTAIN'S FORWARD QUADRANT)

THE PRESSURIZED AREA IS AT 70`F (21`C). THE AREA THAT IS NOT PRESSURIZED IS AT AMBIENT TEMPERATURE

BOTH THE PRESSURIZED AND NOT PRESSURIZED AREA ARE AT AMBIENT TEMPERATURE

NOTE:THE TEMPERATURE OF THE AREA THAT IS NOT PRESSURIZED MUST BE LESS THAT |10`F (|5.5`C) OF THE AMBIENT TEMPERATURE AND MUST BE STABLE FOR ONE HOUR IMMEDIATELY BEFORE ADJUSTMENT.
Elevator Control Cable Adjustment
Figure 504 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-00
 ALL  ú ú 05 Page 509 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

ELEVATORELEVATOR AFT
CONTROL COLUMN
SEE
COLUMN TOUCHES
INDEX PLATE

CONTROL COLUMN

B
A

3 ELEVATOR OVERTRAVEL IS THE DISTANCE TRAVELLED

1  ELEVATOR UP TRAVEL IS THE STRAIGHT LINE WITH POWER SUPPLIED AND THE PCA LINKAGES DISTANCE FROM THE BOTTOM EDGE OF THE INDEX DISCONNECTED AND THE PCAS ARE MANUALLY MOVED PLATE TO THE INBOARD CORNER OF THE UPPER TO BOTTOM. OVERTRAVEL MUST BE A LEAST SURFACE OF THE ELEVATOR TRAILING EDGE 0.50 INCH (12.7 mm) LARGER THAN THE MEASURED
　
中國航空網 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 3(6)