AD 81-08-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Nomad TC Pty Ltd | N22B | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Model N22B and N24A Airplanes |
| aircraft | Nomad TC Pty Ltd | N24A | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Model N22B and N24A Airplanes |
Unsafe Condition
Wear in the horizontal stabilizer trim tab control linkages and excessive free play causing instability.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the horizontal stabilizer structure to accept balanced trim tabs per GAF Service Bulletin NMD-55-12, Part A within 50 hours time in service. Install balanced trim tabs per Part B of the same Service Bulletin within 100 hours time in service. Equivalent FAA-approved methods are acceptable.
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Compliance Time
Within the next 50 hours time in service after the effective date of this AD for paragraph (a), and within the next 100 hours time in service after the effective date for paragraph (b).
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Affected Aircraft
Nomad TC Pty Ltd Model N22B (Serial Nos. N22B-5 and up) and Model N24A (Serial Nos. N24A-42 and up)
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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