AD 90-24-08

final rule
Data completeness: 70%

Airworthiness Directives; FOKKER Model F-28 Series Airplanes

AD Number
90-24-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-140-AD
FR Citation
This information is not available.

Unsafe Condition

Reduced structural integrity of the fuselage due to potential cracks in the fuselage lap joint at stringer 73 between frames 5305 and 9305.

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

Required Actions

Inspect the fuselage lap joint per Fokker Service Bulletin F-28/53-A94, Rev 1. Repeat inspections at intervals not exceeding 1,000 landings. Replace the lap joint per Fokker Service Bulletin F28/53-95, Rev 1 according to specified schedules.

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

Compliance Time

Required as indicated, unless previously accomplished.

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Affected Aircraft

Fokker Model F-28 series airplanes, Serial Numbers 11003 to 11241, inclusive, and 11991 and 11992.

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

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View Official Source ↗