AD 95-17-09 R1

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Aircraft SA226 and SA227 Series Airplanes

AD Number
95-17-09 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-CE-13-AD
FR Citation
Federal Register: March 25, 1996 (Volume 61, Number 58)

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

Failure of the left hand (LH) and right hand (RH) essential bus when engine failure results in a blown generator current limiter, which could result in loss of airplane electrical power.

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

Required Actions

Relocate the LH and RH essential bus current limiters (225 amp) to the battery bus (main bus tie) in accordance with Fairchild Aircraft Engineering Kit Drawing 27K82376 and referenced service bulletins. Special flight permits may be issued under 14 CFR 21.197 and 21.199 to operate the airplane to a location where the requirements can be accomplished.

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

Compliance Time

within the next 2,000 hours time-in-service after the effective date of this AD, unless already accomplished

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

Affected Aircraft

Fairchild Aircraft SA226-T, SA226-AT, SA226-TC, SA226-T(B), SA227-AC, SA227-AT, SA227-BC, SA227-TT (serial numbers 420 through 783, 785 through 789), SA227-CC, and SA227-DC (serial numbers 784, 790 through 883) airplanes that utilize a direct current (DC) generator.

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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