AD 86-16-01
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
Jamming of the rudder pedals due to inadequate sidewall structure and rudder pedal design.
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Required Actions
Modify the airplane sidewall structure and rudder pedals in accordance with GAF Service Bulletin No. NMD-27-34, Paragraph 2. Special flight permits may be obtained for ferrying to a maintenance base. Equivalent compliance methods require approval from the FAA Manager, Western Aircraft Certification Office.
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Compliance Time
within 100 hours time-in-service after the effective date of this AD or one calendar year after the effective date of this AD, whichever occurs first
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Affected Aircraft
GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A (all serial numbers) airplanes certificated in any category, unless Service Bulletin No. NMD-27-34 has been accomplished.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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