Commonwealth legislation

AD/CESSNA 210/39 - Pre-Certification Requirements - Modifications

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This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

This directive requires owners, operators or importers of Cessna P210 (pressurized) aeroplanes to fit two safety modifications before an Australian Certificate of Airworthiness will be issued: protective inner transparencies for passenger windows and visible inspection ports on cabin door latch pins. It affects newly imported or re‑registered P210s and aims to prevent cabin decompression and ensure door latches remain sealed during pressurized flight.

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AD/CESSNA 210/39 - Pre-Certification Requirements - Modifications

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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 Cessna 210 Series Aeroplanes

AD/CESSNA 210/39 Pre-Certification Requirements - Modifications

9/79

Applicability: All models P210.

Requirement: Modify the aircraft in accordance with requirements of ANO 101.22 to schemes approved by the Secretary in respect of the following:

Install protective inner transparencies to passenger cabin windows.

2. Provide witness windows to a least three (3) cabin door lock pins to enable the correct engagement of latches to be ascertained by direct visual inspection.

Compliance: Before issue of Australian Certificate of Airworthiness.

Background: Refer W.A. Region first of type report on VH-SWM and equivalent safety determination ES AWB 6/79.

Source text

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