AD 96-13-06

final rule
Data completeness: 70%

Airworthiness Directives; Fokker Model F28 Series Airplanes (Excluding Fokker Model F28 Mark 0100 Series Airplanes)

AD Number
96-13-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-NM-151-AD
FR Citation
This information is not available.

Unsafe Condition

Stress corrosion cracking of the junction fitting lug of the horizontal stabilizer could result in failure of the lug and uncommanded movement of the horizontal stabilizer.

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

Required Actions

Replace aluminum 7079 junction fittings with improved aluminum 7075 fittings within 18 months after the effective date. For airplanes not previously modified per F28/55-24, replace drive-fitting bushings and bolts within 18 months 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 this AD

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Affected Aircraft

Fokker Model F28 series airplanes; serial numbers 11003 through 11151 inclusive, 11991, and 11992; 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 8, 2026

Rights: U.S. Government Public Domain

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View Official Source ↗