AD 49-30-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 240 Series | Airworthiness Directives; Convair Model 240 Aircraft |
Unsafe Condition
Augmenter vanes showed a tendency to bind under high temperature.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Increase the I.D. of the augmenter vane shaft bushing to 0.509 +0.003/-0.0000 inch. Reduce the O.D. of the augmenter vane shaft to 0.499 +0.000/-0.003 inch. Alternatively, secure specified clearance by increasing bushing I.D. without exceeding 0.514 inch upper limit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
at next scheduled engine change
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Affected Aircraft
Convair Model 240 Aircraft
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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