AD Amdt-39-10266

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Fokker F28 Mark 1000, 2000, 3000, and 4000 Series Airplanes

AD Number
Amdt-39-10266
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 96-NM-174-AD
FR Citation
62 FR 68154

Applicability

TypeManufacturerModelDetails
aircraft Fokker F28 Mark 1000 Airworthiness Directives; Fokker F28 Mark 1000, 2000, 3000, and 4000 Series Airplanes

Unsafe Condition

Corrosion in the rear cargo door and luggage auxiliary structure could result in structural failure of the cargo door and loss of the door during flight, and consequent rapid decompression, aerodynamic instability, and/or damage to other fuselage structures.

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

Required Actions

Perform a one-time visual inspection of the rear cargo door and luggage auxiliary structure for corrosion, followed by removal and repair of any corrosion found before further flight. Drill drain holes and apply corrosion preventive and sealing compound inside the door. Modify the door to provide inspection holes for borescope inspections. Conduct repetitive borescope inspections every 6,000 hours or 3 years for corrosion, repairing any findings before further flight.

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Compliance Time

Within 2 years after the effective date (February 4, 1998) for initial actions. Repetitive borescope inspections due within 6,000 hours time-in-service or 3 years after the initial inspection, whichever comes first.

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Affected Aircraft

All Fokker Model F28 Mark 1000, 2000, 3000, and 4000 series airplanes, regardless of modifications.

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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