4. Procedure
_________
 (Ref. Fig. 601/TASK 05-51-21-991-001, 602/TASK 05-51-21-991-002)

R **ON A/C 001-049, 101-105, 151-199, 201-210,
 Subtask 05-51-21-210-050-A
 A. Inspection of the Tail Area (Ref. TASK 49-16-00-200-002)
 NOTE : You must do this inspection if:
____
 -
the tail hits the runway during the take-off,

 -
the tail hits the runway during the landing.

 NOTE : All inspections are visual unless the text gives other
____
 instructions.

 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Fuselage | | | | | | | | | | | | | | | |  A.| | Examine the skin panels, the splices  |  X  | | | | | | | | and the rivets for distortion, cracks,| | | | | | | | | pulled or torn fasteners and damaged | | | | | | | | | paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the frames, the| |  X  | | | | | | | cleats and the stringers for | | | | | | | | | distortion, cracks, pulled and | | | | | | | | | torn fasteners. | | | | | | | | | (2) Internally examine the lower part | |  X  | | | | | | | of the pressure bulkhead FR70, on | | | | | | | | | the forward and the aft face, in | | | | | | | | | the area below the | | | | | | | | | passenger-compartment floor level,| | | | | | | | | between the L STGR28 and R STGR28,| | | | | | | | | the pressure dome, the frame | | | | | | | | | segment and the vertical cross | | | | | | | | | beam at the aircraft center line | | | | | | | | | for: | | | | | | | | | - distorsion, cracks and dents. | | | | | | | | | | | | | | | |2. | | APU Air Intake and Tail Cone | | | | | | | | | Attachment Fittings | | | | | |

 Tailcone Equipment (L Side)
 Figure 601/TASK 05-51-21-991-001
 1EFF :  ALL  1  05-51-21 Page 603 
1  1  Feb 01/98
 1  1
 1CES  1

 APU Installation (R side)
 Figure 602/TASK 05-51-21-991-002
 1EFF :  ALL  1  05-51-21 Page 604 
1  1  Feb 01/98
 1  1
 1CES  1

 -------------------------------------------------------------------------------
|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | |  A.| | Examine the APU diverter, intake flap,|  X  | | | | | | | | intake nose and drain mast for | | | | | | | | | distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork | | | | | | | | | (Ref. TASK 49-16-00-200-002). | | | | | | | | | If you find damage: | | | | | | | | | (1) Internally examine the diverter | |  X  | | | | | | | system, the ball bearing control | | | | | | | | | and the flap actuator for | | | | | | | | | distortion. | | | | | | | | | Make sure that they are correctly | | | | | | | | | attached. | | | | | | -------------------------------------------------------------------------------

R **ON A/C 051-099,
R Subtask 05-51-21-210-050
R A. inspection of the Tail Area (Ref. TASK 49-16-00-210-001).
R NOTE : You must do this inspection if:
____ R - the tail hits the runway during the take-off, R - the tail hits the runway during the landing.
R NOTE : All inspections are visual unless the text gives other
____ R instructions.
R -------------------------------------------------------------------------------R |ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| R  | |CODE| |  1  |  2  |  3  |SIGN|FIG.| R |----|----|---------------------------------------|-----|-----|-----|----|----| R |1. | | Fuselage | | | | | | R | | | | | | | | | R  |  A.| | Examine the skin panels, the splices  |  X  | | | | | R | | | and the rivets for distortion, cracks,| | | | | | R | | | pulled or torn fasteners and damaged | | | | | | R | | | paintwork. | | | | | | R | | | If you find damage: | | | | | | R  | | | (1) Internally examine the frames, the| |  X  | | | | R | | | cleats and the stringers for | | | | | | R | | | distortion, cracks, pulled and | | | | | |
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 05-51-21Page 605 1201-210, 1May 01/05 1 1 1CES 1
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 2(73)