Commonwealth legislation

AD/PA-24/35 - Beryl Aviation Filtrator Assembly - Replacement

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legislative instrument

Plain English Summary

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This AD requires owners/operators of Piper PA-24, PA24-250 and PA24-260 aeroplanes modified under FAA STC SA2653WE to remove Beryl Aviation filtrator P/N B-1113-1 and install P/N B-1113-M or B-1113-RM (or comply with FAA AD 75-05-02) within 100 hours TIS after 30 April 1975. Owners/operators pay for and arrange the parts and licensed maintenance; it creates short-term aircraft downtime and procurement/qualification considerations.

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AD/PA-24/35 - Beryl Aviation Filtrator Assembly - Replacement

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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 Piper PA-24 (Comanche) Series Aeroplanes

AD/PA-24/35 Beryl Aviation Filtrator Assembly - Replacement 4/75

Applicability: Models PA24, PA24-250, PA24-260 series 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-1113-1 and install either P/N B-1113-M or P/N B-1113-RM; or

FAA AD No. 75-05-02.

Compliance: Within 100 hours time in service after 30 April 1975.

Source text

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