AD 96-12-03 R2
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aviat Aircraft Inc | S-1S | Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes |
| aircraft | Aviat Aircraft Inc | S-1T | Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes |
| aircraft | Aviat Aircraft Inc | S-2 | Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes |
| aircraft | Aviat Aircraft Inc | S-2A | Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes |
| aircraft | Aviat Aircraft Inc | S-2B | Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes |
| aircraft | Aviat Aircraft Inc | S-2S | Airworthiness Directives; Aviat Aircraft, Inc. Models S-1S, S-1T, S-2, S-2A, S-2S, and S-2B Airplanes |
Unsafe Condition
Possible in-flight separation of the wing from the airplane caused by a cracked aft lower fuselage wing attach fitting.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the aft lower fuselage wing attach fitting on both wings for cracks within 50 hours time-in-service after October 3, 1997, and thereafter every 50 hours TIS. Modify any cracked fitting prior to further flight as per Aviat SB No. 25 revisions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours time-in-service after October 3, 1997, and thereafter at intervals not to exceed 50 hours TIS.
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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