(b) Put a warning notice to tell persons not to energize the FADEC 1(2).
Subtask 78-36-41-010-058
B. Open the fan cowl doors (Ref. TASK 71-13-00-010-040)
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR
F 『 EEFF : ALL E Page 60278-36-41
E E Feb 01/98 E E ECES E Subtask 78-36-41-040-055
F 『
E C F M E
E E
E 56-5B E
E E
C. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041)
Subtask 78-36-41-010-059
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 78-36-41-991-305, 602/TASK 78-36-41-991-306, 603/TASK
78-36-41-991-307, 604/TASK 78-36-41-991-308)
Subtask 78-36-41-210-050
A. Do a visual inspection of the thrust reverser half door latches,
bushings, stirrups and centering pin as follows:
-------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
1. Inspect the half door latches for :
A. Damage No damage permitted If you find some damage, (Ref. Fig. 601/TASK 78-36-41-991-305)
replace the door latch (Ref. TASK 78-36-41-000-043) and (Ref. TASK 78-36-41-400-043).
2. Inspect the related hardware of the door latches for:
A. Damage No damage permitted If you find some damage, replace the damaged part (Ref. TASK 78-36-41-000-043) and (Ref. TASK 78-36-41-400-043).
F 『 EEFF : ALL E Page 60378-36-41
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
Thrust Reverser Half Door Latches
Figure 601/TASK 78-36-41-991-305
F 『 EEFF : ALL E Page 60478-36-41
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
Thrust Reverser Half Centering Pins
Figure 602/TASK 78-36-41-991-306
F 『 EEFF : ALL E Page 60578-36-41
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
Permissible Wear - Centering Pin
Figure 603/TASK 78-36-41-991-307
F 『 EEFF : ALL E Page 60678-36-41
E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E
Permissible Damage - Bushing
Figure 604/TASK 78-36-41-991-308
F 『 EEFF : ALL E Page 60778-36-41
E E Feb 01/98 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
-------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
3. Inspect the bushing
for:
A. Wear Wear serviceable limits If two bushings, on each (Ref. Fig. 604/TASK 78-36-41-991-308)
side of the latch are less than satisfactory limits, replace the half door. If three bushings on one half door are less than permitted limits, replace the half door. (Ref. TASK 78-32-11-000-002) and (Ref. TASK 78-32-11-400-002)
4. Inspect the stirrups
for:
A. Damage No damage permitted If you find some damage, (Ref. Fig. 602/TASK 78-36-41-991-306)
replace the damaged part. (Ref. TASK 78-36-41-000-044) and (Ref. TASK 78-36-41-400-044)
B. Wear No wear permitted If there is wear, replace the stirrups. (Ref. TASK 78-36-41-000-044) and (Ref. TASK 78-36-41-400-044)
C. Crack No crack permitted If there is a crack, replace the stirrup . (Ref. TASK 78-36-41-000-044) and (Ref. TASK 78-36-41-400-044)
5. Inspect the related
stirrups hardware
for:
F 『 EEFF : ALL E Page 60878-36-41
E E Feb 01/98 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
-------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
A. Damage
6. Inspect the centering pins for:
A. Damage
B. Crack
C. Wear
7. Inspect the related centering pin hardware for:
A. Damage
No damage permitted
No damage permitted
No crack permitted
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 EXHAUST 2(108)
