Commonwealth legislation

AD/BEECH 65/45 Amdt 2 - Fuselage Rear Bulkhead

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Commonwealth

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legislative instrument

Plain English Summary

4/10 complexity

This directive mandates owners/operators of specified Beechcraft Queen Air 65 and 70 aircraft to perform the actions in Beechcraft Service Instruction No. 0755‑103, Revision II, on a schedule starting within 100 flight hours after reaching 500 hours TIS and repeating at intervals not exceeding 600 hours until the SI-required modification is done. Affected operators and their maintenance organisations bear the costs and must obtain and follow the external SI for the technical work.

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AD/BEECH 65/45 Amdt 2 - Fuselage Rear Bulkhead

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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Beechcraft 65 and 70 (Queen Air) Series Aeroplanes

AD/BEECH 65/45

Amdt 2

Fuselage Rear Bulkhead 3/89

Applicability: All models Queen Air 65, A65 & A65-8200 with S/Nos. L-1, L-2, L-6, LF-7, LF-8 & LC-1 to LC-335;

All models 65- 80, 65-A80, 65-A80-8800 & 65-B80 with S/Nos. LD-1 to LD- 512.

All models 65-A88 with S/Nos. LP-1 to LP-26, LP-28 & LP-30 to LP-47. Models 70 with S/Nos LB-1 through LB-35.

Requirement: Action in accordance with Beechcraft SI No. 0755-103, Rev. II.

Compliance: Within 100 hours’ time in service after achieving 500 hours’ time in service and thereafter at intervals not exceeding 600 hours’ time in service until modified in accordance with SI No. 0755-103, Rev. II.

Background: Amendment 2 references Rev II of the SI and consolidates Queen Air series 65 and 70 aircraft.

Source text

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

1 AD/BEECH 65/45 Amdt 2 - Fuselage Rear Bulkhead