AD Amdt-39-10100

final rule
Data completeness: 70%

Airworthiness Directives; Fokker Model F28 Mark 0100 Series Airplanes

AD Number
Amdt-39-10100
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-NM-149-AD
FR Citation
62 FR 41839

Applicability

TypeManufacturerModelDetails
aircraft Fokker F28 Mark 0100 Airworthiness Directives; Fokker Model F28 Mark 0100 Series Airplanes

Unsafe Condition

Fatigue cracking of the hinges of the cargo doors could result in structural failure of the cargo doors, consequent rapid decompression of the airplane, and possible separation of the cargo doors from the airplane during flight.

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

Required Actions

Perform a one-time inspection to detect fatigue cracking of the cargo door hinges and repair 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 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.