AD/GAF-N22/41 - Emergency Exit Door Lock Mechanism - Inspection
1AD/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
Image unavailable in extracted text 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.