AD 63-15-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 340 | Airworthiness Directives; GENERAL DYNAMICS Models 340 and 440 Aircraft |
| aircraft | Kelowna Flightcraft R & D Ltd. | 440 | Airworthiness Directives; GENERAL DYNAMICS Models 340 and 440 Aircraft |
Unsafe Condition
Cracks have been found in the nose landing gear actuating cylinder rod end eyebolt, Peacock P/N C50137-2.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the eyebolt using dye penetrant or FAA-approved equivalent method. Replace cracked eyebolts with uncracked Peacock P/N C50137-2 before further flight. Continue repetitive inspections based on modification status.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 225 hours' time in service after the effective date of this AD, unless already accomplished within the last 775 hours' time in service, and thereafter at periods not to exceed 1,000 hours' time in service from the last inspection
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
GENERAL DYNAMICS Models 340 and 440 Aircraft with nose landing gear actuating cylinder rod end eyebolt Peacock P/N C50137-2
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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