AD 61-07-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | D & R Nevada LLC | 22 | CONVAIR Model 22 (880) Aircraft |
| aircraft | D & R Nevada LLC | 22M | CONVAIR Model 22 (880) Aircraft |
Unsafe Condition
Cracks in the upper surface skin of foreflaps, P/N 22-18600-5 or -807, particularly in the mid-span area, could propagate and lead to structural failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct daily inspections of all foreflaps for cracks. Stop-drill cracks with 1/4-inch diameter holes, visually inspect after each flight. Modify per Service Bulletin 27-22, repair per Alert SB A-27-22, or replace based on crack limits and time-in-service thresholds.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Compliance required as indicated.
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Affected Aircraft
All Model 22 (880) Aircraft with foreflaps P/N 22-18600-5 or -807.
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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