AD 2007-11-10

final rule
Data completeness: 80%

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

AD Number
2007-11-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-27509
FR Citation
72 FR 29245

Applicability

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

Unsafe Condition

Failure of one or more brake control levers, which could result in uncommanded braking and loss of control of the airplane during takeoff, landing, or taxiing.

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

Required Actions

Perform a detailed inspection for excessive wear of the brake control levers and take applicable corrective actions as specified in Fokker Service Bulletin SBF100-32-142. Replace the control lever if dimension X2 is less than or equal to 2.0 millimeters.

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

Compliance Time

Within 1,500 flight cycles or 12 months after the effective date, whichever occurs first.

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

Affected Aircraft

All Fokker Model F.28 Mark 0070 and 0100 airplanes, certificated in any category.

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

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