Commonwealth legislation

AD/CESSNA 210/28 - Gear Warning and Fuel Pump Switches Operating Cable - Inspection and Replacement

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD applies to Cessna 210/T210 aircraft (S/N 21061020 and up) and requires inspection of the control cable assembly (P/N 9860057-1) that operates the landing-gear warning and fuel-pump switches. If the cable has a plastic-coated flexible inner cable (identified by swaged end fittings), it must be replaced with the stronger piano‑wire inner cable or the entire assembly. It prevents unreliable warnings or fuel‑pump operation that could compromise safety.

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AD/CESSNA 210/28 - Gear Warning and Fuel Pump Switches Operating Cable - Inspection and 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 Cessna 210 Series Aeroplanes

AD/CESSNA 210/28 Gear Warning and Fuel Pump Switches

Operating Cable - Inspection and Replacement

Applicability: All models 210 and T210 with S/Nos. 21061020 and on.

3/77

Requirement: 1. Inspect control cable assembly P/N 9860057-1 to determine if a plastic coated flexible inner cable is fitted.

Note: This can be identified by the presence of swaged end fittings.

If a plastic coated flexible inner cable is fitted replace with a piano wire type inner cable as per earlier Model Cessna 210 installations, or replace with a complete inner and outer piano wire type cable assembly.

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

Source text

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