FWD
C-C
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-00
ALL ú ú 02 Page 513 ú Mar 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
FIRST OFFICER'S AFT QUADRANT
CONTROL ROD FOR THE FIRST OFFICER'S FEEL AND CENTERING UNIT
CONTROL ROD FOR THE CAPTAIN'S FEEL AND CENTERING UNIT
A
INPUT ARM FOR THE FIRST OFFICER'S FEEL UNIT
757
MAINTENANCE MANUAL
CAPTAIN'S AFT
QUADRANT
NEUTRAL SHIFT AND OVERRIDE MECHANISM
A
NEUTRAL SHIFT OVERRIDE SPRINGS
NEUTRAL SHIFT GROUNDING
INPUT SPRINGS
CRANK
ELEVATOR FEEL AND CENTERING UNIT
FWD DECENTERING SPRINGS (4 LOCATIONS)
ELEVATOR CONTROL AFT MECHANISM
CONTROL RODS FOR FIRST OFFICER'S THE FEEL AND
AFT QUADRANT CENTERING UNIT
INPUT ARM FOR THE(2 LOCATIONS) CAPTAIN'S FEEL UNIT
CAPTAIN'S AFT QUADRANT
NEUTRAL SHIFT NEUTRAL SHIFT
TRANSDUCER
CONTROL RODS SEE A (2 LOCATIONS)
AFT
MECHANISM
TORQUE
BOX
FEEL
ACTUATOR
NEUTRAL SHIFT POGO ROD (TO STABILIZER)
B
FWD
B
DECENTERING E/ST10
SPRINGS RIG PIN NEUTRAL SHIFT
FEEL AND (4 LOCATIONS) HOLE AND OVERRIDE
CENTERING UNIT MECHANISM
A-A
Feel, Centering, and Neutral Shift Adjustments
Figure 507 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-00
ALL ú ú 02 Page 514 ú May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
STRUCTURE
B-B
Feel, Centering, and Neutral Shift Adjustment
Figure 507 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-00
ALL ú ú 02 Page 515 ú Mar 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
ELEVATOR
FEEL
COMPUTER
SEE A
FRONT END OF
THE STABILIZER
E/ST11
HOLE RIG PIN COMPUTER FEEL
ARM
OF AIRPLANE RIGHT SIDE FEEL COMPUTER
CONTROL ROD FOR THE FEEL COMPUTER
FWD INBD STABILIZER COMPARTMENT BULKHEAD OF THE FORWARD
ELEVATOR FEEL COMPUTER
A
Elevator Feel Computer Adjustment
Figure 508
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-00
ALL ú ú 02 Page 516 ú Mar 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
(BOTTOM VIEW)
Elevator PCA Adjustment
Figure 509 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-00
ALL ú ú 02 Page 517 ú Jan 20/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
H98797
A
757
MAINTENANCE MANUAL
AFT QUADRANTS AND ELEVATOR PCA'S
SEE C
INPUT CONTROL ROD
RIGHT ELEVATOR FOR THE RIGHT PCA
POSITION INDICATOR ELEVATOR PCA'S
OUTPUT CONTROL ROD FOR THE RIGHT AFT QUADRANT SEE D
中國航空網(wǎng) 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(8)
