AD Amdt-39-10051

final rule
Data completeness: 70%

Airworthiness Directives; Fokker Model F28 Mark 0100 Series Airplanes

AD Number
Amdt-39-10051
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 96-NM-154-AD
FR Citation
62 FR 34617

Applicability

TypeManufacturerModelDetails
aircraft Fokker F28 Mark 0100 Airworthiness Directives; Fokker Model F28 Mark 0100 Series Airplanes

Unsafe Condition

Stress corrosion resulting from overtightening of nuts on bolts in the horizontal stabilizer control unit (HSCU) has caused bolts to crack and fail.

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

Required Actions

Loosen certain nuts on the HSCU to reduce stress on bolts; perform a one-time inspection of bolts for cracking and replace if necessary; apply corrosion protection to bolts; reassemble and reidentify the modified HSCU.

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 F28 Mark 0100 series airplanes subject to the AD

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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