22-32-00
ALL ú ú 10 Page 39 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
(e) Initial Target for EPR (or THR) Mode
1) When the A/T is in the EPR (or THR) mode and T/O is disengaged, the thrust levers track the new reference EPR. Flap placard and maximum airspeed and Mach protection is provided.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-32-00
ALL ú ú 09 Page 40 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
FAULT ISOLATION/MAINT MANUAL
THRUST MANAGEMENT SYSTEM
* SEE THE WDM EQUIPMENT LIST
Thrust Management System - Component Index
Figure 101
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-32-00
ALL ú ú 14 Page 101 ú Sep 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 FAULT ISOLATION/MAINT MANUAL
AUTOTHROTTLE DRIVE ASSEMBLY AUTOTHROTTLE
(REF)
CLUTCH PACK SEE A
FORWARD EQUIPMENT BAY ACCESS DOOR, 113AL
P11 PANEL
CONTROL STAND
SEE C
AUTOTHROTTLE
SERVOMOTOR
GENERATOR,
AUTOTHROTTLE M229
MICROSWITCH
PACK, M966
FLIGHT COMPARTMENT SEE B
2
AUTOTHROTTLE DRIVE ASSEMBLY (REF)
A AUTOTHROTTLE DISENGAGE SWITCHES, S3 AND S4
1 2
AUTOTHROTTLE MICROSWITCH PACK, M966 P10
PANEL B
CONTROL STAND
1
GUN 001-050,101-104 C2 GUN 051-099,105-999
Thrust Management System - Component Location
Figure 102
C98991
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
22-32-00
ALL ú ú 23 Page 102 ú Dec 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
THRUST MANAGEMENT SYSTEM - ADJUSTMENT/TEST
__________________________________________
1. General_______
A. This part of the Maintenance Manual contains a system test of the Thrust Management System (TMS). The test uses the Maintenance Control Display Panel (MCDP). Each test part may be completed independently if all the conditions in the "prepare for test" step have been completed.
B. The test examines the Thrust Management System (TMS) to make sure of the best system performance. This test uses the not fully automatic maintenance functions in the TMS. These functions are controlled by the Maintenance Control and Display Panel (MCDP).
C. The MCDP is on shelf E3-2 of the main equipment center. It supplies switches for test control, test direction and it shows any failure. The MCDP front panel shows general operation instructions. A connection, from the MCDP, is in the control cabin for a hand-held MCDP remote control unit. The connector for the remote unit is on the forward side of the P61 panel. Use of the remote unit decreases test time. The remote unit lets messages displayed on the MCDP in the main equipment center to be shown on the bottom EICAS display unit.
TASK 22-32-00-735-002
2. System Test - Thrust Management System______________________________________
A. Equipment
(1) Remote Control Unit, Maintenance Control Display Panel -A22001-22 (preferred), A22001-15 (optional).
B. References
(1)
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 自動(dòng)飛行 AUTOFLIGHT 2(127)
