AD 63-06-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 340 | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 340 and 440 Series Aircraft |
| aircraft | Kelowna Flightcraft R & D Ltd. | 440 | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 340 and 440 Series Aircraft |
Unsafe Condition
Failure of the Bendix Redbank Type 35E05 fault detection panel could result in loss of electrical power.
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Required Actions
Install a blocking rectifier (G.E. IN-93 or FAA approved equivalent) by soldering the negative lead to lug No. 3 of the locating relay and the positive lead to terminal No. P on the terminal board.
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Compliance Time
within the next 300 hours' time in service following the effective date of this AD
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Affected Aircraft
All Models 340 and 440 Series Aircraft Equipped With a Bendix Redbank Type 35E05 Fault Detection Panel
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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