AD 62-12-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | D & R Nevada LLC | 22 | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 Aircraft |
| aircraft | D & R Nevada LLC | 22M | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 Aircraft |
Unsafe Condition
Cracked inboard wing flap carriage support fittings P/N's 22-18703-11, -12 and 22-18702-11, -12 attributed to fatigue.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct close visual inspection of fittings P/N's 22-18703-11, -12 and 22-18702-11, -12 on the inboard flaps. Replace any cracked fitting prior to further flight. If modified per General Dynamics Service Bulletin No. 27-63 or FAA Western Region Engineering approved equivalent, discontinue 150-hour inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 25 hours' time in service unless already accomplished within the last 125 hours' time in service and thereafter within each 150 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/CONVAIR Models 22 Aircraft with 3,000 hours or more time in service.
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.