(2)
The FLAPS display appears on the main EICAS whenever flaps are not fully retracted. The normal FLAPS display appears for normal flap configurations and disappears 10 seconds after flaps are retracted. One of two multiple FLAPS displays appear for non-normal flap configurations.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-58-00
ALL ú ú 01 Page 1 ú Feb 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
TRAILING EDGE FLAP POSITION INDICATION ON MAIN AND AUXILIARY EICAS DISPLAYS
FLAP CONTROL UNITS
SEE A
SEE C
SEE B
Trailing Edge Flap Position Indicating System Component Location
Figure 1 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-58-00
ALL ú ú 01 Page 2 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
INBOARD POWER PACK
INBOARD POWER PACK RVDT TRANSMITTER
A
LEFT INBOARD RVDT TRANSMITTER
LEFT OUTBOARD RVDT TRANSMITTER
INBOARD FLAP TRANSMISSION
B
OUTBOARD FLAP TRANSMISSION
NOTE:INBOARD POWER PACK AND LEFT WING RVDT TRANSMITTERS SHOWN. OUTBOARD POWER PACK AND RIGHT WING RVDT
C TRANSMITTERS SIMILAR.
Trailing Edge Flap Position Indicating System Component Location
Figure 1 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-58-00
ALL ú ú 01 Page 3 ú Feb 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
F
5
L
A
P
S
NORMAL FLAPS
F L
5
A
LEADING EDGE FLAPS UP, DOWN, OR
P IN-TRANSIT/FAILURE
S
EXPANDED FLAPS DISPLAY
F
L
5
5
A P S
25 25
ALTERNATE FLAPS DISPLAY
10.00 10.00 TE FLAPS 10.00 10.00
ACT. 10.00
INBD DRIVE 8.75 OUTBD DRIVE 8.75
Trailing Edge Flap Position Indicating System EICAS Displays
Figure 2
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-58-00
ALL ú ú 01 Page 4 ú Feb 10/92
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(13)