AD 62-23-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | D & R Nevada LLC | 30 | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Model 30 Aircraft |
| aircraft | D & R Nevada LLC | 30A | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Model 30 Aircraft |
Unsafe Condition
Cracking of the main landing gear door upper forward attachment fitting, P/N 30-55153, in the vicinity of the attachment of the door actuator, particularly at the radii between the leg and base of these tee-shaped fittings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct a close visual and dye penetrant inspection of P/N 30-55153 within 100 hours' time in service after the effective date, unless done within the preceding 250 hours. Inspections must recur at intervals not exceeding 350 hours' time in service. Replace or repair cracked fittings (≤4 inches) per approved methods; replace fittings with cracks >4 inches immediately. Discontinue inspections if reworked per Service Bulletin 32-38 or equivalent.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 100 hours' time in service after the effective date of this AD, unless already accomplished within the preceding 250 hours' time in service
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
GENERAL DYNAMICS/CONVAIR Model 30 Aircraft (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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.