AD 93-07-12

final rule
Data completeness: 70%

FAIRCHILD AIRCRAFT (formerly Swearingen Aircraft Corporation) SA226-T, A226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AC and SA227-AT Airplanes

AD Number
93-07-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-CE-36-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft M7 Aerospace LLC SA226-AT FAIRCHILD AIRCRAFT (formerly Swearingen Aircraft Corporation) SA226-T, A226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AC and SA227-AT Airplanes
aircraft M7 Aerospace LLC SA226-T FAIRCHILD AIRCRAFT (formerly Swearingen Aircraft Corporation) SA226-T, A226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AC and SA227-AT Airplanes
aircraft M7 Aerospace LLC SA226-TC FAIRCHILD AIRCRAFT (formerly Swearingen Aircraft Corporation) SA226-T, A226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AC and SA227-AT Airplanes
aircraft M7 Aerospace LLC SA226-T(B) FAIRCHILD AIRCRAFT (formerly Swearingen Aircraft Corporation) SA226-T, A226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AC and SA227-AT Airplanes
aircraft M7 Aerospace LLC SA227-AC (C-26A) FAIRCHILD AIRCRAFT (formerly Swearingen Aircraft Corporation) SA226-T, A226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AC and SA227-AT Airplanes
aircraft M7 Aerospace LLC SA227-AT FAIRCHILD AIRCRAFT (formerly Swearingen Aircraft Corporation) SA226-T, A226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AC and SA227-AT Airplanes
aircraft M7 Aerospace LLC SA227-TT FAIRCHILD AIRCRAFT (formerly Swearingen Aircraft Corporation) SA226-T, A226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AC and SA227-AT Airplanes

Unsafe Condition

Failure of the horizontal stabilizer rear spar, which could result in loss of control of the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Within the next 50 hours time-in-service (TIS), inspect the horizontal stabilizer rear spar for cracks using dye penetrant per specified service bulletins. Repair any cracks prior to further flight. Modify the outboard hinge within 2,200 hours TIS per applicable service bulletins.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Required as indicated after the effective date of this AD, unless already accomplished within the last 450 hours TIS.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Fairchild Aircraft (formerly Swearingen Aircraft Corporation) SA226-T, SA226-T(B), SA226-AT, SA226-TC (all serial numbers); SA227-TT (TT421 through TT527); SA227-AC (AC406, AC415, AC416, AC420 through AC509, AC511 through AC530); SA227-AT (AT423 through AT524).

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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