AD 2006-06-07

final rule
Data completeness: 70%

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

AD Number
2006-06-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-23476
FR Citation
71 FR 14363

Applicability

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

Unsafe Condition

An MLG main fitting failed on an airplane that was braking while moving backward, leading to a report of cracks in the MLG main fitting which could result in reduced structural integrity.

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

Required Actions

Inspect the main landing gear (MLG) main fitting for cracks using eddy current inspection and repair as necessary. Amend the AFM to prohibit application of brakes during backward movement. Affix a placard next to the parking brake handle to prohibit brake application during backward movement.

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

Compliance Time

Within 14 days for AFM revision and placard installation; within 3 months or 2,000 flight cycles for MLG main fitting inspection, depending on prior inspections.

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 equipped with Messier-Dowty main landing gears (MLGs).

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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