AD 2016-24-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker | Services B | Airworthiness Directives; Fokker Services B.V. Airplanes |
Unsafe Condition
Heavy corrosion found on the wing rear spar lower girder, potentially reducing the load carrying capability of the wing and possibly resulting in structural failure and loss of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the affected areas of the wing rear spar lower girder. Modify the wing trailing edge lower skin panels into access panels. Accomplish applicable corrective actions if corrosion is found, including removing corrosion, repairing, and restoring protective finish. Report inspection results to Fokker Services.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date (January 9, 2017).
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Affected Aircraft
All 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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