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时间:2011-04-11 09:15来源:蓝天飞行翻译 作者:航空
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 S 815-275

 (15)
 Compare the measured capacitance and resistance values with the values shown in Figure 504.

 (a)  
If the capacitance value for a tank unit is out of tolerance, remove and replace the tank unit or the wire bundle (AMM 28-41-01/401).

 (b)  
If the capacitance value for the compensator is out of tolerance, remove and replace the compensator or the FQIS wire bundle (AMM 28-41-02/401).

 (c)  
If the insulation resistance value for the wire bundle is out of tolerance, remove or repair the in-tank FQIS wire bundle (AMM 28-41-09/401).


 S 085-167
 (16) Remove the test equipment.
PSD747-22 PSD60
INTERCONNECT CABLES


In-Tank Component Test Set-Up (at Tank Wall)
Figure 503

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 28-41-00
 ALL  ú ú 07 Page 521 ú Feb 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E53750
A
747-400 MAINTENANCE MANUAL
 S 425-168
 (17)
 Connect the FQIS wire bundle connector that was disconnected (AMM 28-41-09/401).

 S 415-266

 (18)
 Go out of and close the applicable access door, 511FB or 611FB.


 S 095-251
 WARNING:_______DO THE PROCEDURE IN AMM 27-81-00/201 TO REMOVE THE LOCKS. THE FLAPS MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (19) Remove the leading edge flap safety locks, if installed (AMM 27-81-00/201).
 S 865-252
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LEADING
_______ EDGE AND TRAILING EDGE FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER.
 (20) Retract the leading edge flaps, if extended (AMM 27-81-00/201).
 S 095-253
 WARNING:_______DO THE PROCEDURE IN AMM 32-00-30/201 TO REMOVE THE LOCKS. THE DOORS MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (21)
 Remove the wing and body gear door locks (AMM 32-00-30/201).

 S 865-169

 (22)
 Close these circuit breakers and remove the DO-NOT-CLOSE tags:

 (a)  
On the main power distribution panel, P6:
 1) 6D5, FUEL QTY 1
 2) 6D6, FUEL QTY 2


 (b)  
On the DC power distribution panel, P180:
 1) 180M9, FUELING PWR - HOT BAT
 2) 180C25, FUELING LTS PANEL
 3) 180C26, FUELING LTS RECP


 (c)  
On the left power distribution center, P414:
 1) 414F22, FUELING PWR

 

 S 745-170
 (23) Do this CMCS ground test:  <FUEL QUANTITY IND (Reference the Fuel Quantity Indicating System Operational Test).
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 28-41-00
 ALL  ú ú 06 Page 522 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 815-277
 (24) If the problem continues, do a check at the FQPU, M7860.
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 28-41-00
 ALL  ú ú 15 Page 523 ú Feb 10/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

NO. 2 AND 3 RESERVE TANK
(AT THE TANK WALL - FRONT SPAR)
TABLE A

PSD 747-2 TANK UNIT
NO. 2
NO. 3
DRY CAPACITANCE
INSULATION
PROBE (PROBE) OR
RESERVE
RESERVE
(PICOFARADS)
RESISTANCE
COMPENSATORSELECT
TANK EQUIP
TANK EQUIP
(MEGOHMS)
MINIMUM MAXIMUM
CMCS NUMBERSWITCH
NUMBER
NUMBER
A
COMP
F181
F180
50.4
51.8
10
B
1
F187
F186
31.1
32.5
 
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