AD 2008-13-01

final rule
Data completeness: 70%

Airworthiness Directives; Fokker Model F27 Mark 050 Airplanes

AD Number
2008-13-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2008-0639
FR Citation
73 FR 40948

Applicability

TypeManufacturerModelDetails
aircraft Fokker F27 Mark 050 Airworthiness Directives; Fokker Model F27 Mark 050 Airplanes
aircraft Aviat Various Airworthiness Directives; Fokker Model F27 Mark 050 Airplanes

Unsafe Condition

Welding defects in Fokker 50 (F27 Mark 050) engine mounting frames, where unintentional sideways movement of the electric arc resulted in welds running beside the borderline for a part of the tube circumference, directly affecting the structural integrity of the engine mounting frame connections. This could lead to failure of the engine mounting frame in cases where multiple welds are severely affected, potentially resulting in in-flight loss of an engine.

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

Required Actions

Inspect engine mounting frames using non-destructive test (NDT) methods to identify welding defects. Repair or replace affected engine mounting frames as necessary, following Fokker's repair instructions.

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

Fokker Model F27 Mark 050 airplanes

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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