A320飞机维护手册 AMM 时间限制/维护检查 2(140)

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 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
R |1. | | Inspection of the Flight Control | | | | | | | | | Surfaces | | | | | | | | | | | | | | | | A.| | Rudder | | | | | | | | | | | | | | | | | | (1) Examine the rudder external |  X  | | | | | | | | surface for distortion and damage | | | | | | | | | | | | | | | | | | (2) Do a detailed visual inspection |  X  | | | | | | | | (Ref. TASK 55-30-00-210-001) | | | | | | | | | of the actuator fittings 1, 2 and | | | | | | | | | 3 at: | | | | | | | | | - the vertical stabilizer | | | | | | | | | center-box, | | | | | | | | | - the rudder front spar. | | | | | | | | | NOTE: Carefully examine the | | | | | | | | | actuator fitting lugs and | | | | | | | | | the areas of the fitting | | | | | | | | | around the fasteners. | | | | | | | | | | | | | | | | B.| | Elevators | | | | | | | | | | | | | | | | | | (1) Examine the elevator external |  X  | | | | | | | | surface for distortion and damage | | | | | | | | | | | | | | | | | | (2) Do a detailed visual inspection |  X  | | | | | | | | (Ref. TASK 55-16-00-200-004) | | | | | | | | | (Ref. TASK 55-20-00-200-003) of | | | | | | | | | these parts in the actuator areas:| | | | | | | | | - the actuator fittings 1 and 2 | | | | | | | | | and their attachments, | | | | | | | | | - the hinge fittings 2, 3 and 4 | | | | | | | | | and their attachments, | | | | | | | | | - the hinge arms 2, 3 and 4 and | | | | | |

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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.|
 | |CODE| |  1  |  2  |  3  |SIGN|FIG.|
 |----|----|---------------------------------------|-----|-----|-----|----|----|

 |  |  | their attachments | |  |  |  |  |
 |  |  | at the horizontal stabilizer | |  |  |  |  |
 |  |  | rear-spar and at the elevator | |  |  |  |  |
 |  |  | front spar. | |  |  |  |  |
 |  |  | | |  |  |  |  |
 | C.|  | Flaps | |  |  |  |  |
 |  |  | | |  |  |  |  |
 |  |  | (1) Do a general visual inspection of |  X  |  |  |  |  |
 |  |  | each control surface and its | |  |  |  |  |
 |  |  | attachments for distortion and | |  |  |  |  |
 |  |  | damage. | |  |  |  |  |
 |  |  | | |  |  |  |  |
 |  |  | (2) Do a visual inspection of: |  X  |  |  |  |  |
 |  |  | - the flap track fairings, | |  |  |  |  |
 |  |  | - the pylon aft movable-fairings | |  |  |  |  |
 |  |  | and their attachments | |  |  |  |  |
 |  |  | for distortion and damage. | |  |  |  |  |
 |  |  | | |  |  |  |  |
 |  |  | (1) Examine the external surface and  |  X  |  |  |  |  |
 |  |  | the attachments of each control | |  |  |  |  |
 |  |  | surface for distortion and damage.| |  |  |  |  |
 |  |  | | |  |  |  |  |
 |2.  |  | Operational Test of the Flight Control| |  |  |  |  |
 |  |  | Surfaces | |  |  |  |  |
 |  |  | | |  |  |  |  |
 |  A.|  | Make sure that the work area is clean |  X  |  |  |  |  |
 |  |  | and clear of tool(s) and other items. | |  |  |  |  |
 |  |  | | |  |  |  |  |
 |  B.|  | Do an operational test of each control|  X  |  |  |  |  |
 |  |  | surface and make sure that the related| |  |  |  |  |
 |  |  | surface(s) move(s) smoothly and freely| |  |  |  |  |
 |  |  | | |  |  |  |  |
 |  |  | (1) For the rudder: | |  |  |  |  |
 |  |  | (Ref. TASK 27-24-00-710-001) | |  |  |  |  |
　
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