27-00-01
ALL ú ú 01 Page 222 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
FLIGHT CONTROL SHEAR RIVETS - MAINTENANCE PRACTICES
___________________________________________________
TASK 27-00-02-302-003
1. Flight Control Shear Rivets References______________________________________
A. General
_______
(1)
Shear rivets provide a means by which normal operation of essential flight systems can be maintained in the event of failure or jamming of related or interconnected secondary systems. Each shear rivet location is marked by a SHEAROUT placard that includes the quantity and part number of the shear rivet. The chart below contains a list of all the shear rivets that are used in the flight control system along with the references to the related maintenance manual sections.
(2)
GUN 001-015, 051, 206;
Refer to the table that follows:
~................................................................. |MAINTENANCE MANUAL | | PART THAT CONTAINS THE | | SECTION | RIVET TYPE | SHEAR RIVET | ................................................................... |27-11-14/201 |BACR15BB5AD |Arm Assembly - Lateral Feel, | | | |Centering, and Trim Mechanism| ................................................................... |27-21-12/201 | |Output Crank - Rudder Ratio | | | |Changer | ................................................................... |27-21-17/401 |BACR15BB4B1 |Output Link - Yaw Damper | | | |Summing Lever | ................................................................... |27-21-20/201 |BABC30MB6A1 |Lever Assembly - PCA Input, | | | |Rudder Control | ................................................................... |27-31-06/401 |NAS1398CWS |Crank Assembly - PCU Input, | | | |Elevator Control | ................................................................... |27-48-00/501 | |LSTM Cables - Stabilizer | ................................................................... |27-51-26/401 |BACR15BA4D |Output Drum - Trailing Edge | | | |Flap Power Drive Unit | 2...................…...............….............................1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-02
ALL ú ú 13 Page 201 ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
(3) GUN 016-050, 052-205, 207-295, 297-999; Refer to the table that follows:
~................................................................. |MAINTENANCE MANUAL | | PART THAT CONTAINS THE | | SECTION | RIVET TYPE | SHEAR RIVET | ................................................................... |27-11-14/201 |BACR15BB5AD |Arm Assembly - Lateral Feel, | | | |Centering, and Trim Mechanism| ................................................................... |27-21-12/201 | |Output Crank - Rudder Ratio | | | |Changer | ................................................................... |27-21-20/201 |BABC30MB6A1 |Lever Assembly - PCA Input, | | | |Rudder Control | ................................................................... |27-31-06/401 |NAS1398CWS |Crank Assembly - PCU Input, | | | |Elevator Control | ................................................................... |27-48-00/501 | |LSTM Cables - Stabilizer | ................................................................... |27-51-26/401 |BACR15BA4D |Output Drum - Trailing Edge | | | |Flap Power Drive Unit | 2...................…...............….............................1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-02
ALL ú ú 12 Page 202 ú May 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
1.
ú ú ú
2.
757 MAINTENANCE MANUAL
FLIGHT CONTROL LATERAL TRIM CORRECTION - ADJUSTMENT TEST
________________________________________________________
General
_______
A. This procedure supplies the data that is necessary to adjust the trailing edge flaps for straight and level flight. The procedure will decrease the quantity of rudder and aileron trim that is needed during flight at a constant speed.
B. This adjustment installs and/or removes shims from each outboard-flap-track location for each of the two outboard flaps. The installation of more shims will move the flap trailing edge up. The removal of shims will make the flap trailing edge move down.
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 1(20)
