Commonwealth legislation

AD/GAF-N22/41 - Emergency Exit Door Lock Mechanism - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

The directive mandates a time-critical inspection of the emergency-exit door lock spindle on all GAF Nomad N22 and N24 aircraft, to detect and correct reported incorrect spindle positioning. Operators/owners must complete the inspection within 10 hours time-in-service after 16 April 1981 and follow the procedure in GAF Telex Nomad Alert SB ANMD 52-2.

It imposes immediate maintenance costs and potential downtime on operators, relying on the referenced telex for detailed steps and corrective actions.

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AD/GAF-N22/41 - Emergency Exit Door Lock Mechanism - Inspection

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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 GAF N22 and N24 Series Aeroplanes

AD/GAF-N22/41 Emergency Exit Door Lock Mechanism - Inspection

Applicability: All models N22 and N24.

Document: GAF Telex Nomad Alert SB ANMD 52-2.

5/81

Compliance: Unless already accomplished, within 10 hours time in service after 16 April 1981.

Background: Instances have occurred in which the lock mechanism spindle on the emergency exit door has been incorrectly positioned before fitting the handle.

Source text

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