AD 2018-01-05

final rule
Data completeness: 80%

Airworthiness Directives; Fokker Services B.V.

AD Number
2018-01-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2017-1182
FR Citation
83 FR 596

Applicability

TypeManufacturerModelDetails
aircraft Fokker Services B Airworthiness Directives; Fokker Services B.V.

Unsafe Condition

The fuselage frames are subject to widespread fatigue damage (WFD) due to fatigue cracking, which can compromise the structural integrity of the center fuselage.

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

Required Actions

Modification of the affected fuselage frames, and post-modification inspections will be included in a revision to the Airworthiness Limitations Section (ALS).

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

Affected Aircraft

Fokker Services B.V. Model F28 Mark 0070 and 0100 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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