AD 2012-18-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | M7 | Aerospace LLC | Airworthiness Directives; M7 Aerospace LLC Airplanes |
Unsafe Condition
Fatigue cracking in the left and right forward (main) spar wing-to-fuselage attach fittings, which could lead to failure of the wing-to-fuselage attach fitting and wing separation from the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect the left and right forward (main) and aft spar wing-to-fuselage attach fittings for cracks. Replace any cracked fitting. Report certain inspection results to the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
M7 Aerospace LLC Models SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), SA227-AT, and SA227-TT airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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