AD 95-12-23
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Twin Commander Aircraft LLC | 690C | Airworthiness Directives; Twin Commander Aircraft Corporation Models 690C and 695 Airplanes |
| aircraft | Twin Commander Aircraft LLC | 695 | Airworthiness Directives; Twin Commander Aircraft Corporation Models 690C and 695 Airplanes |
Unsafe Condition
Wing damage caused by fatigue cracking, which could progress to structural failure if not detected and corrected.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the wing structure for cracks in accordance with Twin Commander SB No. 213. If cracks are found, replace damaged structure and modify the wing structure as specified. If no cracks, reinspect at intervals not exceeding 1,000 hours TIS or modify the wing structure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Required upon the accumulation of 6,000 hours time-in-service (TIS) or within the next 50 hours TIS after the effective date of this AD, whichever occurs later, and thereafter as indicated.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Twin Commander Aircraft LLC Models 690C (serial numbers 11600 through 11735) and 695 (serial numbers 95000 through 95084).
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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