Commonwealth legislation

AD/BEECH 90/40 Amdt 1 - Propeller Secondary Low Pitch Stop System - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This directive requires owners/operators of the listed Beechcraft C‑90 and E‑90 serial numbers to modify the propeller secondary low‑pitch‑stop system, using Beechcraft Service Instruction No. 0808‑247 Rev.1 or FAA AD 77‑02‑07, within 100 hours' time‑in‑service after 31 May 1977. It makes the modification mandatory for those airframes, imposing scheduling, compliance recordkeeping and the direct cost of parts, labour and downtime on operators.

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AD/BEECH 90/40 Amdt 1 - Propeller Secondary Low Pitch Stop System - 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 90 and 65-90 (King Air) Series Aeroplanes

AD/BEECH 90/40

Amdt 1

Propeller Secondary Low Pitch Stop System - Modification

5/77

Applicability: Models C-90, S/Nos. LJ-584, LJ-586 to LJ-589, LJ-591, LJ-594 to LJ-600, LJ-602, LJ-603, LJ-605 to LJ-611, LJ-613 to LJ-618, LJ-621, LJ-623 to LJ-651, LJ-653 to LJ- 691. Models E-90, S/Nos. LW-1 to LW-190.

Document: Beechcraft SI No. 0808-247, Rev. 1. or FAA AD 77-02-07.

Compliance: Within 100 hours’ time in service after 31 May 1977.

Source text

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