Commonwealth legislation

AD/P68/16 Amdt 1 - Engine and Engine Mount Attach Bolts

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Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

Mechanically, this airworthiness directive requires operators of specified Partenavia P68 series aeroplanes (P68, P68B, P68R, P68C, P68 Obs, P68‑TC, P68‑TC Obs) to inspect the MS bolts that attach the engine to the mount and the mount to the airframe and to check the associated nuts for correct torque, using Partenavia Service Bulletin 76 Rev 1. Inspections are required at each engine installation and thereafter at intervals not exceeding 100 hours time in service. Owners/operators must carry out and fund the checks.

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AD/P68/16 Amdt 1 - Engine and Engine Mount Attach Bolts

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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 Partenavia P68 Series Aeroplanes

AD/P68/16

Amdt 1

Engine and Engine Mount Attach Bolts 4/89

Applicability: P68, P68B, P68R, P68C, P68 Obs, P68-TC, and P68-TC Obs.

Requirement: 1. Inspect the MS bolts attaching the engine to the engine mount and the MS bolts attaching the engine mount to the aircraft structure in accordance with Partenavia

S.B. 76 Rev 1.

Check the nuts associated with the bolts in para 1 for correct torque loading. Compliance: 1. At each engine installation.
At intervals not exceeding 100 hours time in service.

Background: This Amendment revises the original Australian Requirement to include recently published manufacturer’s inspection criteria, and to expand the Applicability.

Source text

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