AD 81-11-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Nomad TC Pty Ltd | N22B | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22 and N24 Series Airplanes |
| aircraft | Nomad TC Pty Ltd | N22S | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22 and N24 Series Airplanes |
| aircraft | Nomad TC Pty Ltd | N24A | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22 and N24 Series Airplanes |
Unsafe Condition
Improper operation of the emergency exit door handle and door locking mechanism could prevent the emergency exit door from opening, leading to door trim panel fracture or door inoperability during an emergency.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 10 hours time-in-service after the effective date, visually inspect the emergency exit door operation by rotating the handle and pushing outward 0.5 inches. If door does not open properly, remove trim panel, inspect door locking mechanism and linkage, correct assembly if needed, free and lubricate corroded or seized pins, reassemble, and reinspect. Record compliance in maintenance records.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 10 hours time-in-service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Nomad TC Pty Ltd Models N22B, N22S, N24A, all serial numbers
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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