(2)
The installation of the RVDT transmitter at the flap transmission
(3)
The removal of the RVDT transmitter at the flap power package
(4)
The installation of the RVDT transmitter at the flap power package
B.
The removal and installation procedure for the RVDT transmitter at the flap transmission is the same for all four transmitters.
C.
The removal and installation procedure for the RVDT transmitter at the flap power package is the same for the inboard and the outboard power package transmitters.
TASK 27-58-01-004-001
2. Removal of the RVDT Transmitter at the Flap Transmission (Fig. 401)________________________________________________________
A. References
(1)
AMM 27-51-00/201, Trailing Edge Flap System
(2)
AIPC 27-58-01, Fig. 1
(3)
SSM 27-58-01
(4)
WDM 27-58-11
B.
Access
(1)
Location Zone 581 Rear Spar to Trailing Edge, LH (LO Transmitter) 572 Rear Spar to Trailing Edge, LH (LI Transmitter) 672 Rear Spar to Trailing Edge, RH (RI Transmitter) 681 Rear Spar to Trailing Edge, RH (RO Transmitter)
(2)
Access Panels 581MB Flap Drive Access Panel (LO Transmitter) 572FB Trailing Edge Lowerng Edge (LI Transmitter) 672FB Trailing Edge Access Panel (RI Transmitter) 681MB Flap Drive Access Panel (RO Transmitter)
C.
Procedure
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-58-01
ALL ú ú 01 Page 401 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
SEE A
SEE B
MANUAL OVERRIDE LEVER
TORQUE TUBE
ALTERNATE LIMIT SWITCH PACK
INBOARD POWER
PACKAGE
INBOARD POWER PACK RVDT TRANSMITTER
SEE D 1
A H
OR 2 ____INBOARD POWER PACKAGE AND LEFT WING RVDT
NOTE: TRANSMITTERS SHOWN. OUTBOARD POWER PACKAGE AND RIGHT WING RVDT TRANSMITTERS SIMILAR.
Trailing Edge Flap Position Transmitter Installation
Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-58-01
ALL ú ú 01 Page 402 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
RVDT TRANSMITTER
SEEF 1
OR
J2
TORQUE TUBE
SEE C
OUTBOARD FLAP
TRANSMISSION
B
FWD FWD FWD FWD
LEFT OUTBOARD LEFT INBOARD RIGHT INBOARD RIGHT OUTBOARD
RVDT INSTALLATION RVDT INSTALLATION RVDT INSTALLATION RVDT INSTALLATION
C
MPC TRANSMITTERS
1
ALLIED SIGNAL
TRANSMITTERS
2
Trailing Edge Flap Position Transmitter Installation
Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-58-01
ALL ú ú 01 Page 403 ú Feb 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
FINE ADJUSTMENT INDICATOR WINDOW
A-A
Trailing Edge Flap Position Transmitter Installation Figure 401 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. MPC TRANSMITTERS ú
27-58-01
ú ú 01 Page 404 ú Feb 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
C
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ALLIED SIGNAL TRANSMITTERS ú 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 6(17)
