問題一覧
1
Records of maintenance, alterations, preventive maintenance, 100-hour, annual, and progressive inspections
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1,3
3
Approval for return to service only for the performed
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Eight 1/4 — 20-inch standard heli-coils were replaced. The damaged inserts were extracted, the tapped holes gauged, then new inserts installed, and tangs removed
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Airworthiness Directives
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Dented section removed and replaced with identical new tubing flared to 37
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Overhaul of a hydraulic pressure pump
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A description (or reference to acceptable data) of work performed, date of completion, the name of the person performing the work ( if someone else), signature, certificate number, and king of certificate held
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The aircraft owner
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Any format that provides record continuity and includes the required information may be used
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FAA Form 337
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In each record
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The person who performs or supervises the work
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Certifying that the work was done in accordance with the requirements of 14 CFR Part 43
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Aircraft total time is required to be included only in the inspection entry
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Data must be FAA-approved prior to its use for that purpose
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Aircraft maintenance records
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Aircraft nationality and registration mark, and the date work was accomplished
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Two; one copy for the aircraft owner and one copy for the FAA
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2
21
Welded a reinforcing plate over the dented area
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Provide a written notice of the defect to the owner
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Except for these discrepancies, the item inspected is airworthy
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After satisfactorily completing inspections
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Records of the current status of applicable AD’s, and date and time when recurring AD’s are next due
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FAA Form 337 is not authorized for use with other than U.S. registered aircraft
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Major repairs and major alterations
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2
29
The product, part, or materials meets FAA airworthiness standards
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Make the proper entries in the aircraft’s maintenance record
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The repair of portions of skin sheets by making additional seems
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Wear within acceptable limits, repair not necessary
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The person approving or disapproving of return to service
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The owner must obtain a special flight permit
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Total time-in-service of the airframe
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14 CFR Part 43
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Standardized electronic documentation for aircraft modules