(5) replacing defective safety wiring or cotter keys; (6) lubrication not requiring disassembly other than removal of non-structural items
such as cover plates, cowlings, and fairings; (7) making simple fabric patches not requiring rib stitching or the removal of structural
parts or control surfaces;
(8) replenishing hydraulic fluid in the hydraulic reservoir; (9) refinishing decorative coating of fuselage, wings, tail group surfaces (excluding
balanced control surfaces), fairings, cowling, landing gear, cabin, or cockpit interior
when removal or disassembly of any primary structure or operating system is not
required; (10) applying preservative or protective material to components where no disassembly
of any primary structure or operating system is involved and where such coating is
not prohibited or is not contrary to good practices; (11) repairing upholstery and decorative furnishings of the cabin or cockpit when the
repairing does not require disassembly of any primary structure or operating system
or interfere with an operating system or affect primary structure of the aircraft. (12) making small simple repairs to fairings, non-structural cover plates, cowlings, and
small patches and reinforcements not changing the contour so as to interfere with
proper airflow; (13) replacing side windows where that work does not interfere with the structure of any
operating system such as controls, electrical equipment, etc.;
(14) replacing safety belts; (15) replacing seats or seat parts with replacement parts approved for the aircraft, not
involving disassembly of any primary structure or operating system;
(16) troubleshooting and repairing broken circuits in landing light wiring circuits;
(17) replacing bulbs, reflectors, and lenses of position and landing lights;
(18) replacing wheels and skis where no weight and balance computation is involved; (19) replacing any cowling not requiring removal of the propeller or disconnection of
flight controls;
(20) replacing or cleaning spark plugs and setting of spark plug gap clearance;
(21) replacing any hose connection except hydraulic connections;
(22) replacing prefabricated fuel lines;
(23) cleaning fuel and oil strainers;
(24) replacing and servicing batteries
(25) replacement or adjustment of non-structural fasteners incidental to operations. (26) the installation of anti-misfueling devices to reduce the diameter of fuel tank filler
openings provided the specific device has been made a part of the aircraft type
certificate data by the aircraft manufacturer, the manufacturer has provided
appropriately approved instructions acceptable to the Authority for the installation of
the specific device, and installation does not involve the disassembly of the existing
filler opening.
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本文链接地址：飞机持续适航 CONTINUING AIRWORTHINESS OF AIRCRAFT(18)
