AD 65-14-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 35-33 | Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft |
| aircraft | Textron Aviation Inc. | H35 | Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft |
| aircraft | Textron Aviation Inc. | J35 | Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft |
| aircraft | Textron Aviation Inc. | K35 | Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft |
Unsafe Condition
Failure of the alternator support bracket due to elongated bolt holes or cracks.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect alternator supporting brackets (P/N's 195814, 195820, 195836, 195838, 195840, 626131) for elongated bolt holes. Inspect for cracks using dye penetrant or magnetic particle method. Replace brackets with elongated holes or cracks before further flight.
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Compliance Time
within the next 25 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 50 hours' time in service from the last inspection
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Affected Aircraft
BEECH Models H35, J35, K35, and 35-33 Series Aircraft equipped with Ellingsworth Products Co., Inc. Alternator Kit Number 195860 installed under STC SA1-377
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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