AD 96-04-09

final rule
Data completeness: 70%

Airworthiness Directives; Fokker Model F28 Mark 0100 Series Airplanes

AD Number
96-04-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
94-NM-215-AD
FR Citation
This information is not available.

Unsafe Condition

Corrosion of the auxiliary power unit (APU) mounting frames due to moisture accumulation through drain holes could lead to frame failure, resulting in APU displacement and potential fuel leakage posing a fire hazard or rendering the APU inoperative.

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

Required Actions

Inspect mounting frames for drain holes. If present, inspect for corrosion; replace frames if corrosion is found. Compliance times are 3 months if corrosion exists, 9 months if no corrosion.

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

Compliance Time

Replacement must be accomplished within 3 months if corrosion is found, or within 9 months if no corrosion is found.

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

Affected Aircraft

Fokker Model F28 Mark 0100 series airplanes, all serial numbers.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

View Official Source ↗