Commonwealth legislation

AD/BEECH 65/42 - Elevator Stop Bolts - Modification

In ForceCTH

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Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

The directive mandates a specific modification to the elevator stop bolts on Beechcraft Model 65‑B80 aircraft S/N LD‑452 to LD‑468, to be carried out per Beechcraft Service Instruction No. 0618‑152. Owners/operators must complete the work within 100 hours’ time‑in‑service after 30 September 1974; they bear costs and must arrange qualified maintenance and any downtime.

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AD/BEECH 65/42 - Elevator Stop Bolts - Modification

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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 65 and 70 (Queen Air) Series Aeroplanes

AD/BEECH 65/42 Elevator Stop Bolts - Modification 9/74

Applicability: All model 65-B80 with S/Nos. LD-452 to LD-468. Document: Beechcraft SI No. 0618-152.

Compliance: Within 100 hours’ time in service after 30 September 1974.

Source text

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