AD 80-13-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Nomad TC Pty Ltd | N22B | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes |
| aircraft | Nomad TC Pty Ltd | N24A | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes |
Unsafe Condition
Possible control obstruction when aileron is applied at the extreme aft stick position due to insufficient clearance between the end of the control wheel attachment bolt and the attachment plates.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Before the first flight of each day, check longitudinal and lateral controls for freedom of movement in the aft stick position with full left and right aileron. Within 25 hours time in service after the AD's effective date, inspect the gimbal support structure tie rod attachment plates and ensure a minimum 0.125 inches clearance between the control wheel attachment bolt end and plates per GAF Alert Service Bulletin ANMD-27-14 or FAA-approved equivalent.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 25 hours time in service after the effective date of this AD
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Affected Aircraft
GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B (Serial Nos. N22B-5 and up) and N24A (Serial Nos. N24A-42 and up)
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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