Subtask 72-31-00-010-055
R B. Open the fan cowl doors: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR.
Subtask 72-31-00-040-052
C. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041).
Subtask 72-31-00-010-056
D. Open the thrust reverser doors (Ref. TASK 78-36-00-010-040):
FOR 1000EM1
451AL, 452AR
FOR 1000EM2
461AL, 462AR.
4. Procedure
_________
(Ref. Fig. 601/TASK 72-31-00-991-300, 602/TASK 72-31-00-991-301, 603/TASK 72-31-00-991-302, 604/TASK 72-31-00-991-309, 605/TASK 72-31-00-991-306, 606/TASK 72-31-00-991-307, 607/TASK 72-31-00-991-308, 608/TASK 72-31-00-991-310)
F 『 EEFF : ALL E Page 60372-31-00
E E May 01/04 E E ECES E F 『 E C F M E E E E 56-5B E
Core Rotation Drive Motor Installation
Figure 601/TASK 72-31-00-991-300
F 『 EEFF : ALL E Page 60472-31-00
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
VSV System Connections at the HMU
Figure 602/TASK 72-31-00-991-301
F 『 EEFF : ALL E Page 60572-31-00
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E
R Borescope Ports of the High-Pressure Compressor Figure 603/TASK 72-31-00-991-302
F EEFF : E E ECES ALL 『E 72-31-00EEE Page 606 Aug 01/98
R Removal of IGV Borescope Plug (S1) Figure 604/TASK 72-31-00-991-309
F EEFF : E E ECES ALL 『E 72-31-00EEE Page 607 Aug 01/98
R HPC Rotor Indexing to Zero Figure 605/TASK 72-31-00-991-306
F EEFF : E E ECES ALL 『E 72-31-00EEE Page 608 Aug 01/98
Locally Manufactured Alignment Rod
Figure 606/TASK 72-31-00-991-307
F 『 EEFF : ALL E Page 60972-31-00
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
Locally Manufactured Deep Socket Wrench
Figure 607/TASK 72-31-00-991-308
F EEFF : ALL 『E 72-31-00 Page 610
E E Feb 01/98
E E
ECES E
F 『
E C F M E
E E
E 56-5B E
E E
INTENTIONALLY BLANK
F 『 E E Page 61172-31-00
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E Subtask 72-31-00-410-055
R Compressor Blades Inspection Figure 608/TASK 72-31-00-991-310- 13 (SHEET 1)
F EEFF : E E ECES ALL 『E 72-31-00EEE Page 612 May 01/05
R Compressor Blades Inspection Figure 608/TASK 72-31-00-991-310- 23 (SHEET 2)
F EEFF : E E ECES ALL 『E 72-31-00EEE Page 613 May 01/05
R Compressor Blades Inspection Figure 608/TASK 72-31-00-991-310- 33 (SHEET 3)
F EEFF : E E ECES ALL 『E 72-31-00EEE Page 614 May 01/05
F 『
E C F M E
E E
E 56-5B E
E E
A. Do a borescope installation:
(1) Use the MONITOR, RESOLUTION BORESCOPE (856A1323G01) to make sure that the borescope or fiberscope and light source are serviceable. See the Non-Destructive Test Manual for this procedure (Ref. NTM 720000).
(2) Install the tools to turn the core engine. NOTE : The core engine may be turned using a breaker bar (see step
____ (a)) or with a drive motor (see step (b)).
(a) To turn the core manually with a breaker bar, do the steps that follow:
(b) To turn the core with a drive motor, do the steps that follow: 1 Remove the starter (Ref. TASK 80-11-10-000-002).
1_ Remove the handcranking drive cover from the core rotation pad
on the left side of the accessory gearbox (AGB), opposite the
starter. (Ref. TASK 72-63-00-000-002)
2_ Install a 0.75 in. square drive socket with a 2ft. long
breaker bar into the handcranking drive pad. When you do the
borescope inspection, turn the core engine clockwise (CW, aft
looking forward).
NOTE : To turn the core engine CW, the handcranking drive must____
be turned counterclockwise (CCW).
_ 2 Install the MOTOR, DRIVE - CORE ENGINE ROTATION
_ (856A1488P0/P02) into the accessory gearbox (AGB) starter drive pad. Align the drive shaft of the drive motor with the starter drive pad drive shaft and engage the splines.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM ENGINE 发动机 2(18)