AD 83-09-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Nomad TC Pty Ltd | N24A | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Model N24A Nomad Airplanes |
Unsafe Condition
Failure to reduce weight as specified may result in not achieving one engine inoperative climb performance as required by the Aircraft Flight Manual.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Fabricate and install a placard on the instrument panel stating 'REDUCE WEIGHT OBTAINED FROM WEIGHT/ALTITUDE/TEMPERATURE CHARTS BY 200 LBS' and operate accordingly. The placard may be installed by the pilot but requires a maintenance record entry under FAR 91.173. It can be removed once DOA AFM General Amendment G8 is incorporated.
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Compliance Time
within the next 50-hours time-in-service
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Affected Aircraft
GOVERNMENT AIRCRAFT FACTORIES (GAF) Model N24A Nomad airplanes (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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