曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
EFFECTIVITY 24-21-00 Page 2
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 120
ALL
AC GENERATION - IDG COMPONENTS - INTEGRATED DRIVE GENERATOR / FILTER CLOGGING INDICATOR
TMUELAH04-P01 LEVEL 2
EFFECTIVITY 24-21-00 Page 3
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 121
ALL
AC GENERATION - IDG COMPONENTS
INTEGRATED DRIVE GENERATOR
QUICK ATTACH DETACH
The IDG is attached to the engine gearbox by a Quick
Attach Detach device.
OIL LEVEL INDICATOR
1 - If the oil level is above the line between the
green and the yellow band (IDG cold) or above the
yellow band (IDG hot), oil servicing is required.
2 - If the oil level is within the green band (IDG
cold) or within green or yellow bands (IDG hot), oil
servicing is not required.
3 - If the oil level is below the green band, oil
servicing is required.
Note : The yellow band corresponds to the oil thermal
expansion margin.
TMUELAH04-T02 LEVEL 2
EFFECTIVITY 24-21-00 Page 4
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 122
ALL
TMUELAH04-P02 LEVEL 2
AC GENERATION - IDG COMPONENTS - INTEGRATED DRIVE GENERATOR - QUICK ATTACH DETACH / OIL
LEVEL INDICATOR
EFFECTIVITY 24-21-00 Page 5
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 123
ALL
AC GENERATION - IDG COMPONENTS
INTEGRATED DRIVE GENERATOR
OIL FILTER
DISCONNECT MECHANISM
The disconnect mechanism consists of a solenoid, a
spring-loaded disconnect plunger with threaded pawl,
a worm shaft, and a reset handle.
The purpose of the disconnect mechanism is to decouple
the power supply of the gearbox from the IDG in the
event of an IDG failure.
Once uncoupled, the disconnect mechanism cannot be
reset in flight.
TMUELAH04-T03 LEVEL 2
EFFECTIVITY 24-21-00 Page 6
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 124
ALL
AC GENERATION - IDG COMPONENTS - INTEGRATED DRIVE GENERATOR - OIL FILTER / DISCONNECT
MECHANISM
TMUELAH04-P03 LEVEL 2
EFFECTIVITY 24-21-00 Page 7
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 125
ALL
AC GENERATION - IDG COMPONENTS
OIL COOLER
IDENTIFICATION
FIN:
LOCATION
ZONE: 400
TMUELAH04-T04 LEVEL 2
EFFECTIVITY 24-21-00 Page 8
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 126
ALL
AC GENERATION - IDG COMPONENTS - OIL COOLER
TMUELAH04-P04 LEVEL 2
EFFECTIVITY 24-21-00 Page 9
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 127
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUELAH04 LEVEL 2
EFFECTIVITY 24-21-00 Page 10
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 128
ALL
24 - ELECTRICAL POWER
24-21-00 AC GENERATION - IDG OIL SERVICING
CONTENTS:
Oil Replenishing of the IDG after Replacement of the
IDG or a Cooling Circuit Component
TMUELAI03 LEVEL 2
EFFECTIVITY 24-21-00 Page 1
May 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 24 ELECTRICAL POWER
UF94200
EFFECTIVITY Page 129
ALL
AC GENERATION - IDG OIL SERVICING
OIL REPLENISHING OF THE IDG AFTER REPLACEMENT OF THE
IDG OR A COOLING CIRCUIT COMPONENT
Refer to your Aircraft Maintenance Manual when
performing this procedure by yourself.
VIDEO SEQUENCE
Do not touch the IDG system components for a short
time after the engine is shutdown. The engine
components stay hot for sometime and can cause injury.
If the oil is below the minimum level (the green band),
add oil to the IDG.
Now prepare the IDG for servicing.
Remove the caps from the overflow drain and pressure
fill valves.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:
ATA 24 ELECTRICAL POWER(14)