S 865-206
(2)
Remove the electrical power if it is not necessary
(AMM 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-00
ALL ú ú 02 Page 557 ú Sep 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
INBOARD TRAILING EDGE FLAP DRIVE SYSTEM - INSPECTION/CHECK
__________________________________________________________
1. General
_______
A. There are four tasks in this procedure:
(1)
A check of the axial shaft movement in the angle tee gearbox for the inboard trailing edge (TE) flap.
(2)
A check of the axial shaft movement in the outboard tee gearbox for the inboard trailing edge (TE) flap.
(3)
A check of the axial shaft movement in the outboard angle gearbox for the inboard trailing edge (TE) flap.
(4)
A check of the wear in the U-joints of the driveshafts for the inboard trailing edge (TE) flap drive system.
TASK 27-51-00-026-001
2. Inboard TE Flap Angle Tee Gearbox Inspection (Fig. 601)
_______________________________________________________
A. Equipment
(1)
Dial Indicator - (clamp type with adjustable stem adaptor)
B.
References
(1)
AMM 24-22-00/201, Electrical Power - Control
(2)
AMM 27-51-07/401, Inboard TE Flap Drive Inboard Tee Gearbox
(3)
AMM 32-00-15/201, Landing Gear Door Locks
(4)
AMM 32-00-20/201, Landing Gear Down Locks
C.
Access
(1)
Location Zones
143/144 MLG Wheel Well
211/212 Control Cabin
710 Nose Landing Gear and Doors
730/740 Main Landing Gear and Doors
D.
Procedure
S 216-002
(1)
Make sure the downlocks are installed on the nose and main landing gear (AMM 32-00-20/201).
(2)
Supply electrical power (AMM 24-22-00/201).
S 866-066
S 016-003
WARNING: USE THE PROCEDURE IN AMM 32-00-15 TO INSTALL THE DOOR LOCKS.
_______ THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(3) Open the doors for the landing gear and install the door locks (AMM 32-00-15/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-00
ALL ú ú 01 Page 601 ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
ANGLE TEE GEARBOX
SEE A (EXAMPLE) ASSEMBLY ANGLE TEE GEARBOX
SEE B
ASSEMBLY TORQUE TUBE
INBD
ANGLE TEE GEARBOX
A
Angle Tee Gearbox Inspection Figure 601 (Sheet 1)
H98201
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-00
ALL ú ú 01 Page 602 ú Jan 20/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
DIAL INDICATOR
TORQUE TUBE
SETUP (EXAMPLE)
ASSEMBLY
COUPLING SLEEVE
ANGLE TEE GEARBOX ASSEMBLY
INBDOUTPUT SEE C
SHAFT
ANGLE TEE GEARBOX ASSEMBLY NO. 4
(ANGLE TEE GEARBOX ASSEMBLY NO. 5 IS OPPOSITE)
B
ANGLE TEE GEARBOX COUPLING ASSEMBLY
PUSH
SHAFT
PULL
OUTPUT SHAFT AXIAL MOVEMENT
0.015
0.000
ANGLE TEE GEARBOX ASSEMBLY
C
Angle Tee Gearbox Inspection
Figure 601 (Sheet 2)
H98203
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國航空網 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(153)
