Commonwealth legislation

AD/BEECH 36/24 - Beryl Aviation Filtrator Assembly

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

The directive mandates removal of filtrator P/N B-1116-1 and installation of P/N B-1116-M or B-1116-RM on Beechcraft 36/A36 aeroplanes modified under STC No. SA2653WE, to be completed within 100 hours TIS after 28 November 1975.

Owners/operators bear parts, labour and downtime costs; the entry cites FAA AD 75-05-02 as related authority but does not reproduce its safety rationale.

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Current sections

Direct links to the current provisions in AD/BEECH 36/24 - Beryl Aviation Filtrator Assembly.

AD/BEECH 36/24 - Beryl Aviation Filtrator Assembly

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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 36/24 Beryl Aviation Filtrator Assembly 11/75

Applicability: All models 36 and A36 which have been modified in accordance with FAA Supplemental Type Certificate No. SA2653WE (Installation of engine crankcase breather and vacuum pump air-oil separator).

Requirement: 1. Remove the Beryl Aviation filtrator assembly P/N B-1116-1 and install either P/N B-1116-M or P/N B-1116-RM.

Note: FAA AD 75-05-02 refers.

Compliance: Within 100 hours time in service after 28 November 1975.

Source text

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