1AD/CESSNA 550/2 - Landing Gear - Structural Life Limitation

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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Cessna 550 (Citation II) Series Aeroplanes

AD/CESSNA 550/2 Landing Gear - Structural Life Limitation 2/82

Applicability: All models 550 series aeroplanes.

Requirement: All landing gear components listed in the Component Time Limits Schedule, Chapter 5 of the Cessna Citation II Maintenance Manual dated January 1978, Revision 6 dated 15 December 1980, shall be retired from service at or before the times shown therein.

Note: Where reference is made in the Schedule to FAA and CAA certified aeroplanes, for the purposes of this Directive the component lives may be taken as the lives applicable to FAA certified aeroplanes.

Effective: Forthwith.

Background: This Directive formally promulgates the landing gear component lives determined by the manufacturer.

Note: ANOs Part 105 “NOT GREATER THAN 5700 KG” refer to CESSNA 551 (CITATION II) SERIES AEROPLANES.