(ii) systems and components - for improper installation, apparent defects, and
unsatisfactory operation;
(iii) the cabin and cockpit group; (iv) generally - for uncleanness and loose equipment that might foul the
Controls;
(v) seats and safety belts - for poor condition and apparent defects;
(vi) windows and windshields - for deterioration and breakage;
(vii) instruments - for poor condition, mounting, marking, and (where practicable)
for improper operation;
(viii) flight and engine controls - for improper installation and improper operation;
(ix) batteries - for improper installation and improper charge;
(x) all systems - for improper installation, poor general condition, apparent and
(xi) obvious defects, and insecurity of attachment.
(2) Engine and nacelle group —
(i) engine section - for visual evidence of excessive oil, fuel, or hydraulic leaks,
and sources of such leaks;
(ii) studs and nuts - for improper torquing and obvious defects;
(iii) internal engine - for cylinder compression and for metal particles or foreign matter on screens and sump drain plugs. If there is weak cylinder
compression, for improper internal condition and improper internal tolerances;
(iv) engine mount - for cracks, looseness of mounting, and looseness of engine
to mount;
(v) flexible vibration dampeners - for poor condition and deterioration;
(vi) engine controls - for defects, improper travel, and improper safety;
(vii) lines, hoses, and clamps - for leaks, improper condition, and looseness;
(viii) exhaust stacks - for cracks, defects, and improper attachment.
(ix) accessories - for apparent defects in security of mounting;
(x) all systems - for improper installation, poor general condition, defects, and
insecure attachment;
(xi) cowling - for cracks and defects.
(3) Landing gear group —
(i) all units - for poor condition and insecurity of attachment;
(ii) shock absorbing devices - for improper oleo fluid level;
(iii) linkage, trusses, and members - for undue or excessive wear, fatigue, distortion;
(iv) retracting and locking mechanism - for improper operation;
(v) hydraulic lines - for leakage;
(vi) electrical system - for chafing and improper operation of switches;
(vii) wheels - for cracks, defects, and condition of bearings;
(viii) tires - for wear and cuts;
(ix) brakes - for improper adjustment;
(x) floats and skis - for insecure attachment and obvious or apparent defects.
(4) Wing and centre section assembly for —
(i) poor general condition;
(ii) fabric or skin deterioration;
(iii) distortion;
(iv) evidence of failure; and
(v) insecurity of attachment.
(5) Complete empennage assembly for —
(i) poor general condition,;
(ii) fabric or skin deterioration,
(iii) distortion, 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：飞机持续适航 CONTINUING AIRWORTHINESS OF AIRCRAFT(24)
