A320飞机维护手册 AMM EXHAUST 2(56)

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1. Examine the upper/lower cut corners, the 3/9 o'clock beams and aft ring for:
 A. Delamination
B. Abrasion
C. Crack 1.5 in. (38.1 mm) maximum length 7.4 in. (188 mm) minimum separation, between other delaminations, holes or cracks. Five delaminations maximum per half door.
No carbon fiber damage permitted.
1 in. (25.4 mm) maximum length in any direction.
7.4 in. (188 mm) minimum separation, between other cracks, holes or delaminations.
Monitor at "A" check.It is recommended that alldelaminations be repairedno later than airplane "C"check.If the delamination is notpermitted, replace thehalf door (Ref. TASK 78-32-11-000-002) and (Ref. TASK 78-32-11-400-002) .
Seal surface damage (paintand surface resin only) with aerodynamic tape (Material No. CP2517). Replace tape if peeled. Monitor at "A" check.
Seal damaged area fromentrance of moisture with aerodynamic tape (Material No. CP2517).
Monitor at "A" check.
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D. Gouge
E. Hole
F. Nick, scratch
F EEFF : ALL E E ECES Five cracks maximum per half door.
0.008 in. (0.20 mm) maximum depth over a 8 in. (203.2 mm) length.
1 in. (25.4 mm) maximum diameter
7.4 in. (188 mm) minimum separation, between other holes, cracks or delaminations.
 Five holes maximum per half door.
0.008 in. (0.20 mm) maximum depth over a 8 in. (203.2 mm) length.
『E EEEIf more than five cracks,replace the half door (Ref. TASK 78-32-11-000-002) and (Ref. TASK 78-32-11-400-002).
Seal damaged aera fromentrance of moisture withaerodynamic tape (Material No. CP2517). Replace tape if peeled or damaged. Monitor at "A" check. If the gouges are not in the serviceable limits, replace the half door (Ref. TASK 78-32-11-000-002) and (Ref. TASK 78-32-11-400-002) .
Seal damaged area fromentrance of moisture with aerodynamic tape (Material No. CP2517).
Moisture at "A" check.
If more than five holes,replace the half door (Ref. TASK 78-32-11-000-002) and (Ref. TASK 78-32-11-400-002).
Seal damaged aera fromentrance of moisture withaerodynamic tape (Material No. CP2517). Replace tape if peeled or damaged. Monitor at "A" check.

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 -------------------------------------------------------------------------------If the nick or scratch is not permitted, replace the half door (Ref. TASK 78-32-11-000-002) and (Ref. TASK 78-32-11-400-002).
 2. Examine the internal area of the strut for:
 A. Crack  None permitted. If there is crack, replace the half door (Ref. TASK 78-32-11-000-002) and (Ref. TASK 78-32-11-400-002) .
 Subtask 78-32-11-010-052
 B. Open the thrust reverser doors to the 45 degrees position (Ref. TASK 78-36-00-010-040): FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
 Subtask 78-32-11-210-051
 C. Do a visual inspection of the one and eleven o'clock struts as follows:
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1. Examine the strut for:
 A. Crack or buckle on  No damage is permitted If there are cracks or the part near the buckles on the part near inner barrel the inner barrel, replace
 the strut, (Ref. SRM 54-30-00).
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B. Movement: try to  No movement is permitted If there is movement of move the strut by the strut, replace the hand bushing (Ref. TASK 78-32-
11-000-001) and (Ref. TASK 78-32-11-400-001).
 Subtask 78-32-11-980-050
 D. Open the blocker door manually (Ref. TASK 78-32-41-860-001).
　
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