AD 2007-04-23

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes

AD Number
2007-04-23
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25391
FR Citation
72 FR 8615

Applicability

TypeManufacturerModelDetails
aircraft Fokker F Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes

Unsafe Condition

Fatigue cracking of the sliding member in the main landing gear (MLG) could result in possible separation of the MLG from the airplane, leading to reduced controllability upon landing and potential injury to passengers.

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

Required Actions

Inspect the sliding members of the main landing gear (MLG) for cracking. Replace the sliding members with serviceable parts if necessary. Perform repetitive magnetic particle inspections of the sliding members for cracking and take corrective actions as needed.

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 F.28 Mark 0070 and 0100 airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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