AD Amdt-39-10623
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker | F | Airworthiness Directives; Fokker Model F.28 Mark 0100 Series Airplanes |
Unsafe Condition
Cracking of the main fitting subassembly of the main landing gear, which could result in collapse of the main landing gear.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct interim inspections to detect discrepancies of the main fitting subassembly, perform follow-on corrective actions if necessary, complete a one-time inspection, repair the fitting if necessary, and apply new surface protection to terminate interim inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fokker Model F.28 Mark 0100 series airplanes affected by mandatory continuing airworthiness information from a foreign civil airworthiness authority.
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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