AD 99-21-05

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Aircraft, Inc. Models SA226-T, SA226-T(B), SA226-AT, and SA226-TC Airplanes

AD Number
99-21-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
99-CE-15-AD
FR Citation
Federal Register: October 7, 1999 (Volume 64, Number 194)

Applicability

TypeManufacturerModelDetails
aircraft M7 Aerospace LLC SA226-AT Airworthiness Directives; Fairchild Aircraft, Inc. Models SA226-T, SA226-T(B), SA226-AT, and SA226-TC Airplanes
aircraft M7 Aerospace LLC SA226-T Airworthiness Directives; Fairchild Aircraft, Inc. Models SA226-T, SA226-T(B), SA226-AT, and SA226-TC Airplanes
aircraft M7 Aerospace LLC SA226-TC Airworthiness Directives; Fairchild Aircraft, Inc. Models SA226-T, SA226-T(B), SA226-AT, and SA226-TC Airplanes
aircraft M7 Aerospace LLC SA226-T(B) Airworthiness Directives; Fairchild Aircraft, Inc. Models SA226-T, SA226-T(B), SA226-AT, and SA226-TC Airplanes

Unsafe Condition

Failure of the landing gear actuator caused by cracks in the rod ends, which could result in the inability to lower the landing gear during a landing with consequent possible loss of control of the airplane.

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

Required Actions

Replace any landing gear actuator rod end not part number VTA00350 (or FAA-approved equivalent) within 500 hours time-in-service after the effective date. Accomplish replacement per Fairchild Aircraft Alert Service Bulletin SB A32-014. No installation of non-compliant rod ends permitted after effective date.

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

Compliance Time

Within 500 hours time-in-service after the effective date

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

Affected Aircraft

Fairchild Aircraft Models 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-TC396, TC398-TC413, TC418-TC419) equipped with landing gear actuator rod ends other than P/N VTA00350.

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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