AD 95-25-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | M7 Aerospace LLC | SA226-AT | Airworthiness Directives; Fairchild Aircraft SA226 Series Airplanes |
| aircraft | M7 Aerospace LLC | SA226-T | Airworthiness Directives; Fairchild Aircraft SA226 Series Airplanes |
| aircraft | M7 Aerospace LLC | SA226-TC | Airworthiness Directives; Fairchild Aircraft SA226 Series Airplanes |
| aircraft | M7 Aerospace LLC | SA226-T(B) | Airworthiness Directives; Fairchild Aircraft SA226 Series Airplanes |
Unsafe Condition
The main landing gear door actuation roller contacting the lower edge of the tang and causing the linkage to lock over-center, which could result in inability to extend the main landing gear.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the main landing gear door actuator tangs and associated hardware with improved design parts (P/N 27-55001-299 and 27-55001-301) following Fairchild Aircraft Service Bulletin 226-32-059. Special flight permits may be issued under 14 CFR 21.197/21.199 to operate to a location where the AD can be accomplished.
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Compliance Time
within the next 1,000 hours time-in-service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fairchild Aircraft SA226-T (T201-T275, T277-T291), SA226-T(B) (T(B) 276, T(B) 292-T(B) 417), SA226-AT (AT001-AT074), SA226-TC (TC201-TC419) equipped with part number 27-55001-229 actuator assembly.
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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