Identification and treatment of corrosive attack on aircraft structure and engine materials is presented. Corrosion inspection frequency, corrosion identification, and corrosion treatment continues to be the responsibility of the operator and should be accomplished per this Advisory Circular (AC), the manufacturer's recommendations, or the operator's own maintenance program. The procedures presented in this AC are an acceptable means, but not the only acceptable means, of corrosion treatment. The information contained in this AC is applicable to aircraft for which the manufacturer has not published corrosion control information. Where the aircraft manufacturer has published a recommended corrosion inspection schedule and treatment program for a particular aircraft, that program should take precedence over the recommendations of this AC.
Advisory Circular: Corrosion Control for Aircraft
1991
136 pages
Report
Keine Angabe
Englisch
Aircraft , Corrosion & Corrosion Inhibition , Aircraft maintenance , Aircraft structures , Corrosion prevention , Corrosion , Damage assessment , Inspection , Oxidation , Aircraft engines , Aluminum alloys , Corrosion resistance , Electrolytes , Ferrous metals , Magnesium alloys , Rusting , Schedules , Stress corrosion
SLUB | 1981
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