AD 81-15-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | M7 Aerospace LLC | SA226-AT | Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes |
| aircraft | M7 Aerospace LLC | SA226-T | Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes |
| aircraft | M7 Aerospace LLC | SA226-TC | Airworthiness Directives; Swearingen Models SA226-T, SA226-AT, and SA226-TC Airplanes |
Unsafe Condition
Structural wear or damage to the lower wing-to-fuselage aerodynamic fairing stiffeners, attached grommets, and lower fuselage pressure vessel skin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the lower wing-to-fuselage aerodynamic fairing stiffers, attached grommets, and lower fuselage pressure vessel skin for deterioration, wear, or damage. Repair damaged areas and modify the structure in accordance with Swearingen Service Bulletin SB53-006 or equivalent means approved by the FAA.
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Compliance Time
within the next 200 hours' time in service after the effective date of this AD
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Affected Aircraft
Swearingen Models SA226-T (S/N T201 through T275 and T277 through T291), SA226-AT (S/N AT001 through AT074), and SA226-TC (S/N TC201 through TC407) airplanes certificated in all categories.
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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