Commonwealth legislation

AD/BEECH 36/18 Amdt 1 - Landing Gear Shock Strut Position

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Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

Owners/operators of Beechcraft A36 aeroplanes with serial numbers E-425 to E-475 (except E-431) are required by this Airworthiness Directive to perform the landing gear shock strut position action specified in Beechcraft Service Instruction No. 612-200.

The work must be done within 100 hours TIS after 31 January 1974 (unless already completed); operators bear the cost and rely on the SI for technical details.

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AD/BEECH 36/18 Amdt 1 - Landing Gear Shock Strut Position

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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 36 (Bonanza) Series Aeroplanes

AD/BEECH 36/18

Amdt 1

Landing Gear Shock Strut Position 1/74

Applicability: All model A36 with S/Nos. E-425 to E-475 except E-431. Requirement: Action in accordance with Beechcraft SI No. 612-200.

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.