AD Amdt-39-10709
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker | F28 Mark 0070 and Mark 0100 | Airworthiness Directives; Fokker Model F28 Mark 0070 and Mark 0100 Series Airplanes |
Unsafe Condition
Malfunction of the wing leading edge thermal anti-ice system due to incorrect amount of bleed air exhaust holes, which could result in reduced controllability and/or reduced structural integrity of the wing due to overheating.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the wing leading edge sections for the correct amount of bleed air exhaust holes and perform corrective actions if necessary.
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 F28 Mark 0070 and Mark 0100 series airplanes.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.