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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Do the inspection of the related | | X | | | | | | | component: | | | | | | | | | (a) for the windshield | | | | | | | | | (Ref. TASK 56-11-11-200-001) | | | | | | | | | (b) for the fixed windows | | | | | | | | | (Ref. TASK 56-11-12-200-001) | | | | | | | | | (c) for the sliding windows | | | | | | | | | (Ref. TASK 56-12-11-200-001) | | | | | | | | | (d) for the attaching fasteners: | | | | | | | | | - if you find damage, remove | | | | | | | | | the windshield, the fixed | | | | | | | | | windows or the sliding | | | | | | | | | windows | | | | | | | | | (Ref. TASK 56-11-11-000-001)| | | | | | | | | (Ref. TASK 56-11-12-000-001)| | | | | | | | | (Ref. TASK 56-12-11-000-001)| | | | | | | | | - do the inspection of the | | | | | | | | | window bearing surface | | | | | | | | | (fuselage side) for damage. | | | | | | | | | (2) Do the operational test of the | | X | | | | | | | windshield anti-icing and | | | | | | | | | defogging | | | | | | | | | (Ref. TASK 30-42-00-710-001). | | | | | | | | | (3) Do the operational test of the | | X | | | | | | | standby compass | | | | | | | | | (Ref. TASK 34-22-00-710-001). | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-18-210-055
R E. Check after Damage on the Nose and/or the Main Landing Gear Doors
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.
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage during the | | | | | | | | | inspection: | | | | | | | | | (1) Refer to allowable damage and | | X | | | | | | | repair (Ref. SRM). | | | | | | | | | (2) If you find a through hole: | | X | | | | | | | - examine internally the adjacent | | | | | | | | | and underneath area including | | | | | | | | | all the components (pipes, items| | | | | | | | | of equipment, electrical | | | | | | | | | harnesses...) for damage. | | | | | | | | | if you find damage: | | | | | | | | | - replace or repair the | | | X | | | | | | the related component | | | | | | | | | | | | | | | | B.| | If you find damage on the electrical | | | | | | | | | bonding leads during the inspection: | | | | | | | | | (1) Replace the electrical bonding | | X | | | | | | | lead and/or the defective | | | | | | | | | attachment. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-18-210-053
R F. Check after Damage on the Nose and/or the Main Landing Gear (Ref. TASK 32-21-00-200-002) (Ref. TASK 32-11-00-200-001) (Ref. TASK 32-69-00-740-001) (Ref. TASK 32-46-00-740-001)
-------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | A.| | If you find damage on the nose and/or | | | | | | | | | the main landing gear during the | | | | | | | | | inspection: | | | | | | | | | (1) do the inspection of the LG: | | | | | | | | | (a) For the NLG: | | X | | | | | | | - (Ref. TASK 32-21-00-200-002)| | | | | | | | | (b) For the MLG: | | X | | | | | | | - (Ref. TASK 32-11-00-200-001)| | | | | | | | | (2) Do a BITE test of the landing gear| | X | | | | | | | (Ref. TASK 32-69-00-740-001) | | | | | | | | | (3) Do a BITE test of the BSCU | | X | | | | | | | (Ref. TASK 32-46-00-740-001) | | | | | |
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|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| | 1 | 2 | 3 |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| | | | | | | | | | | B.| | If you find damage on the components | | | | | | | | | attached to the landing gear: | | | | | | | | | (1) Examine the electrical components | | X | | | | | | | internally. | | | | | | -------------------------------------------------------------------------------
Subtask 05-51-18-210-054
R G. Check after Damage on the Belly Fairing
NOTE : If there is damage to the aircraft structure, refer to the
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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