S 434-028-N00
(22)
Install the protection covers on the 2.9 bleed valves to prevent unwanted objects during the power plant removal.
S 864-058-N00
WARNING: YOU MUST KEEP THE ELECTRICAL POWER OFF WHEN YOU DISCONNECT OR
_______ CONNECT THE FUEL, HYDRAULIC, AND ELECTRICAL LINES. IF THE ELECTRICAL POWER IS OFF, IT WILL PREVENT THE ACCIDENTAL OPERATION OF THE FLUIDS WITH PRESSURE, ELECTRICAL CIRCUITS WHICH ARE ENERGIZED, OR FIRE. IF THE ELECTRICAL POWER IS NOT OFF, INJURY TO PERSONS CAN OCCUR.
(23)
If supplied, remove electrical power (AMM 24-22-00/201).
S 034-025-N00
(24)
Disconnect the power feeder cable (2) for the IDG with the steps that follow (Fig. 405):
(a)
Disconnect the hinged clamps at the 11 locations along the
power feeder cable (2).
(b)
Remove the screws (6) and washers (7) which attach the terminal block cover (5) to the IDG.
(c)
Remove the terminal block cover (5).
(d)
Remove the nuts (4) and washers (3) which attach the phase
leads of the power feeder cable (2) to the terminal studs on
the IDG.
(e)
Remove the phase leads from the terminal studs.
1) Make a mark on each phase lead for the correct
installation.
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////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
2. IDG POWER
FEEDER CABLE
ELECTRICAL
RACEWAY
SEE A
CLAMP
(5 LOCATIONS)
FWD
SEE B
A
IDG Power Feeder Cable Installation
Figure 405 (Sheet 1)
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SEE A
IDG
FWD SEE C
(6 LOCATIONS) CLAMP
FEEDER CABLE 2. IDG POWER B IDG
(4 LOCATIONS) PHASE LEAD
(2 LOCATIONS) 7. WASHER (2 LOCATIONS) BLOCK SCREW 6. TERMINAL
C (4 LOCATIONS) (4 LOCATIONS) BLOCK COVER 5. TERMINAL 4. TERMINAL NUT 3. WASHER
Figure 405 (Sheet 2) IDG Power Feeder Cable Installation
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////////////////////////A / PW4000 SERIES /747-400 / ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE D
THRUST REVERSER
HYDRAULIC TUBE SUPPORT BRACKET
SUPPORT HOOK
IDG POWER FEEDER CABLE
D
IDG Power Feeder Cable Installation Figure 405 (Sheet 3)
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71-00-02 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:747-400 AMM 飞机维护手册 动力装置 POWER PLANT 1(118)