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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | slats | | | | | | | | | (Ref. TASK 27-84-00-710-001). | | | | | | | | | | | | | | | | C.| | If you find damage on the flap track | | | | | | | | | fairings: | | | | | | | | | (1) Refer to allowable damage and | |  X  | | | | | | | repair (Ref. SRM) | | | | | | | | | | | | | | | | D.| | If you find damage on the flaps: | | | | | | | | | (1) Refer to allowable damage and | |  X  | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine the bonding leads (on the | |  X  | | | | | | | hinges) of the related damaged | | | | | | | | | flap for breakage and defective | | | | | | | | | attachment. | | | | | | | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | |  X  | | | | | | the defective attachment | | | | | | | | | (3) Do the operational test of the | |  X  | | | | | | | flaps | | | | | | | | | (Ref. TASK 27-54-00-710-001). | | | | | | | | | | | | | | | | E.| | If you find damage on the spoilers: | | | | | | | | | (1) Refer to allowable damage and | |  X  | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine the bonding leads (on the | |  X  | | | | | | | hinges) of the related damaged | | | | | | | | | spoiler for breakage and | | | | | | | | | defective attachment. | | | | | | | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | |  X  | | | | | | the defective attachment | | | | | | | | | (3) Do the operational test of the | |  X  | | | | | | | spoilers | | | | | | | | | (Ref. TASK 27-64-00-710-001). | | | | | | | | | | | | | | | | F.| | If you find damage on the ailerons: | | | | | | | | | (1) Refer to allowable damage and | |  X  | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) Examine all the bonding leads of  | |  X  | | | | | | | the aileron hinges and | | | | | | | | | servocontrols of the related | | | | | | | | | damaged aileron for breakage and | | | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | defective attachment. | | | If you find damage: | | | | | | | | | - replace the bonding lead and/or | | |  X  | | | | | | the defective attachment | | | | | | | | | (3) Examine the piston rod of each | |  X  | | | | | | | servocontrol (it must be fully | | | | | | | | | extended) of the related damaged | | | | | | | | | aileron for burn marks, damage and| | | | | | | | | leaks. | | | | | | | | | If you find a leak or damage: | | | | | | | | | (a) replace the related aileron | | |  X  | | | | | | servocontrol | | | | | | | | | (Ref. TASK 27-14-51-000-001) | | | | | | | | | (Ref. TASK 27-14-51-400-001) | | | | | | | | |NOTE: If you are at a line station and | | | | | | | | | you cannot do the inspection of | | | | | | | | | the piston rod, do this check: | | | | | | | | | - operate the ailerons 10 times | | | | | | | | | fully in each direction then | | | | | | | | | make sure from the ground that | | | | | | | | | there are no leaks below the | | | | | | | | | aileron servocontrols. | | | | | | | | | You must do this check before | | | | | | | | | each flight until the return to| | | | | | | | | the main base. you can do the | | | | | | | | | check before each flight for a | | | | | | | | | maximum of 3 days or 10 flights| | | | | | | | | - at the first return to the main| | | | | | | | | base, you must do the | | | | | | | | | inspection of the piston rods. | | | | | | | | | (4) Do the operational test of the | |  X  | | | | | | | ailerons | | | | | | | | | (Ref. TASK 27-14-00-710-001). | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-18-210-056
 T. Check after Damage on the Engine Nacelles and Pylons
 NOTE : If there is damage to the aircraft structure, refer to the
____ Structural Repair Manual (SRM). The SRM has the approved damage limits and repair procedures.
 1EFF : ALL 1 05-51-18Page 641 1 1 Aug 01/05R 1 1 1CES 1

 (Ref. TASK 78-31-00-710-042) (Ref. TASK 73-29-00-710-040) (Ref. TASK 73-21-60-720-040) (Ref. TASK 24-22-51-200-001)
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the air intake, | | | | | | | | | inlet cowl, fan cowl, thrust reverser,| | | | | | | | | exhaust nozzle or the pylon: | | | | | | | | | (1) Refer to the allowable damage and | |  X  | | | | | | | repair (Ref. SRM) | | | | | | | | | (2) At the first return to the main | |  X  | | | | | | | base, do the inspection of the | | | | | | | | | lightning protection module | | | | | | | | | (Ref. TASK 24-22-51-200-001) | | | | | | | | | (3) If you find damage on the thrust | | | | | | | | | reverser: | | | | | | | | | (a) Do an operational test of the | |  X  | | | | | | | thrust reverser system | | | | | | | | | (Ref. TASK 78-31-00-710-042). | | | | | | | | | (4) If you find a through hole | | | | | | | | | on the fan cowl: | | | | | | | | | (a) Do a ground test of the FADEC | |  X  | | | | | | | (Ref. TASK 73-29-00-710-040) | | | | | | | | | (b) Do a ground test of the ECU | |  X  | | | | | | | (Ref.TASK 73-21-60-720-040). | | | | | | -------------------------------------------------------------------------------
　
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