Commonwealth legislation

AD/BEECH 33/18 Amdt 1 - Landing Gear Shock Strut Piston

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Commonwealth

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legislative instrument

Plain English Summary

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This AD requires owners/operators of Beechcraft F33A aeroplanes S/N CE-436 to CE-463 (except CE-439 and CE-462) to carry out the work specified in Beechcraft Service Instruction No. 0612-200 on the landing gear shock strut piston.

The work must be done within 100 hours time in service after 31 January 1974 unless already completed; owners/operators pay, arrange qualified maintenance and obtain any required parts.

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AD/BEECH 33/18 Amdt 1 - Landing Gear Shock Strut Piston

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes

AD/BEECH 33/18

Amdt 1

Landing Gear Shock Strut Piston 1/74

Applicability: All model F33A with S/Nos. CE-436 to CE-463 except CE-439 and CE-462. Requirement: Action in accordance with Beechcraft SI No. 0612-200.

Compliance: Within 100 hours time in service after 31 January 1974 unless already accomplished.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.