AD 89-25-06

final rule
Data completeness: 70%

Airworthiness Directives; FOKKER Model F-28 Series Airplanes

AD Number
89-25-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-140-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Fokker Services F.28 Mark 0070 Airworthiness Directives; FOKKER Model F-28 Series Airplanes
aircraft Fokker Services F.28 Mark 0100 Airworthiness Directives; FOKKER Model F-28 Series Airplanes
aircraft Fokker Services F.28 Mark 1000 Airworthiness Directives; FOKKER Model F-28 Series Airplanes
aircraft Fokker Services F.28 Mark 2000 Airworthiness Directives; FOKKER Model F-28 Series Airplanes
aircraft Fokker Services F.28 Mark 3000 Airworthiness Directives; FOKKER Model F-28 Series Airplanes
aircraft Fokker Services F.28 Mark 4000 Airworthiness Directives; FOKKER Model F-28 Series Airplanes

Unsafe Condition

Fatigue cracks in the rear spar web plate between Wing Stations 4790 and 5280 could reduce structural capability of the wing.

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

Required Actions

Perform external high-frequency eddy current inspection of the rear spar web plate per Fokker Service Bulletin F28/57-84. If cracks are found, repair prior to further flight. Alternate compliance may be approved by the FAA.

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

Compliance Time

Inspect within specified landing intervals based on accumulated landings: 2,000 landings after AD effective date or prior to 35,000 landings (for <45,000 landings); 1,000 landings after AD effective date (for 45,000-55,000 landings); 500 landings after AD effective date (for ≥55,000 landings).

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

Affected Aircraft

Fokker Services Model F-28 series airplanes, Serial Numbers 11003 through 11241, 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

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