AD Amdt-39-9353

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Aircraft Models SA226-AT and SA226-TC Airplanes

AD Number
Amdt-39-9353
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 95-CE-52-AD
FR Citation
60 FR 47862

Applicability

TypeManufacturerModelDetails
aircraft Fairchild Various Airworthiness Directives; Fairchild Aircraft Models SA226-AT and SA226-TC Airplanes

Unsafe Condition

Fatigue of the two bottom cargo door receptacles caused the bottom third of the cargo door to bend outward and upward, causing damage to the fuselage door frame.

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

Required Actions

Replace the two lower aluminum cargo door receptacles with steel receptacles.

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

Compliance Time

Before further flight

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

Affected Aircraft

Fairchild Aircraft Models SA226-AT and SA226-TC airplanes with the affected cargo door receptacles.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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