AD 2020-21-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron | Aviation Inc | Airworthiness Directives; Textron Aviation Inc. Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Textron Aviation Inc. Airplanes |
Unsafe Condition
The combination of the attachment structure design and high loads during landing contribute to the development of cracks in the tailcone and horizontal stabilizer attachment structure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the tailcone and horizontal stabilizer for corrosion, cracks, and loose or sheared rivets and repairing or replacing damaged parts as necessary.
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Compliance Time
Within 50 flight hours
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Affected Aircraft
Textron Aviation Inc. Models 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 182, 182A, 182B, 182C, 182D, 185, 185A, 185B, 185C, 185D, 185E, A185E, and A185F airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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