(a)
Make sure the white fuel jettison schematic shows.
(b)
Make sure the pump box symbols for the override/jettison pumps for the No. 2 and No. 3 main tanks change color in this sequence: 1) Green (pump on - pressure) 2) Amber (pump on - low pressure)
S 715-116
(15)
Put the FUEL JETTISON control selector switch to OFF position.
S 715-118
(16)
Monitor the fuel synoptic.
(a)
Make sure the pump box symbols for the override/jettison pumps for the No. 2 and No. 3 main tanks change color in this sequence: 1) Amber (pump on - low pressure) 2) Green (pump on - pressure)
S 715-119
(17)
Put these override/jettison pump switches to the off position (white ON indication symbol in the switch does not show):
(a)
OVRD 2 FWD
(b)
OVRD 2 AFT
(c)
3 OVRD FWD
(d)
3 OVRD AFT
S 715-157
(18)
Monitor the fuel synoptic.
(a)
Make sure the pump box symbols for the override/jettison pumps for the No. 2 and No. 3 main tanks change color in this sequence: 1) Green (pump on - pressure)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-31-00
ALL ú ú 15 Page 527 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
2) Amber (pump on - low pressure) (does not always show) 3) White (pump off)
G. Put the Airplane Back to Its Usual Condition
S 865-154
(1) Remove electrical power if it is not necessary (AMM 24-22-00/201).
TASK 28-31-00-705-177
7. Fuel Jettison Transfer Valves - Fuel Transfer Operational Test (Fig. 502)______________________________________________________________
A. General
(1)
This task transfers fuel from one tank to another tank through the jettison transfer valves to make sure the valves are in the commanded position. This task also makes sure that the jettison transfer valve bodies and valve adapter shafts are installed correctly.
(2)
You can test one or all four of the jettison transfer valves in this procedure.
(3)
This procedure operates the fuel boost pumps in the inboard and outboard main tanks. Make sure the minimum and maximum fuel quantities called out in the prepare for the test procedure are available.
(4)
You must manually open the jettison transfer valves in this procedure. The transfer valves are located in the wheel wells for the main landing gear. Make sure to install the door locks on the landing gear doors.
B.
References
(1)
AMM 12-11-01/301, Fuel Servicing
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 28-22-16/401, Fuel System Card File
(4)
AMM 28-26-00/201, Defueling
(5)
AMM 31-61-00/501, Integrated Display System (IDS)
(6)
AMM 32-09-02/201, Air/Ground Relays
(7)
AMM 34-61-02/401, Control display Unit
(8)
AMM 45-10-00/501, Central Maintenance Computer (CMC)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-31-00
ALL ú ú 13 Page 528 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
CROSSFEED MANIFOLD LEFT JETTISON (REF)
Jettison Transfer Valve Fuel Flow Diagram
Figure 502
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
28-31-00
ALL ú ú 13 Page 529 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
F51614
A
747-400
MAINTENANCE MANUAL
(9)
AMM 27-81-00/201, Leading Edge Flap System
(10)
AMM 28-26-00/201, Defueling
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 燃油 FUEL 4(12)
