AD 2004-13-17

final rule
Data completeness: 80%

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

AD Number
2004-13-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-223-AD
FR Citation
69 FR 39833

Applicability

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

Unsafe Condition

Restricted elevator movement and consequent reduced controllability of the airplane due to the existing elevator tension control mechanism.

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

Required Actions

Modify the elevator tension control mechanism within 18 months after the effective date, in accordance with Fokker Service Bulletin SBF100-27-081 or Fokker Component Service Bulletin D78179-27-017. No person may install an unmodified elevator tension control assembly after the effective date.

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

Compliance Time

Within 18 months after the effective date of August 5, 2004.

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 series airplanes, certificated in any category, equipped with elevator tension control assemblies having part numbers D78179-405, -407, -409, -411, or -413.

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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