AD 96-03-03

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes

AD Number
96-03-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-CE-17-AD
FR Citation
Federal Register: February 12, 1996 (Volume 61, Number 29)

Applicability

TypeManufacturerModelDetails
aircraft M7 Aerospace LLC SA226-AT Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA226-T Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA226-TC Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA226-T(B) Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA227-AC (C-26A) Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA227-AT Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA227-BC (C-26A) Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA227-CC Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA227-DC (C-26B) Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes
aircraft M7 Aerospace LLC SA227-TT Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes

Unsafe Condition

Power control cable disconnecting from the lever attach point clevis due to failure of attaching hardware, which could result in engine shutdown and subsequent loss of control of the airplane.

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

Required Actions

Replace the nuts attaching the power control cable to the lever attach point clevis with nuts having safety wire holes, safety-wire the power control cable to the lever attach clevis, inspect to ensure secure attachment to the power control cable bracket, and correct any attachment issues following specified service bulletins.

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

Compliance Time

within the next 100 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 models SA226-T, SA226-T(B), SA226-AT, SA226-TC, SA227-TT, SA227-AT, SA227-AC, SA227-BC, SA227-CC, and SA227-DC airplanes (all serial numbers)

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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