AD 96-26-05

final rule
Data completeness: 70%

Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes

AD Number
96-26-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
96-NM-88-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Fokker Services F27 Mark 100 Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes
aircraft Fokker Services F27 Mark 200 Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes
aircraft Fokker Services F27 Mark 300 Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes
aircraft Fokker Services F27 Mark 400 Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes
aircraft Fokker Services F27 Mark 500 Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes
aircraft Fokker Services F27 Mark 600 Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes
aircraft Fokker Services F27 Mark 700 Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes

Unsafe Condition

Fatigue cracking of the torque tube support of the left-hand (LH) elevator could result in failure of the torque tube or its support structure, leading to reduced controllability of the airplane.

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

Required Actions

Inspect the torque tube assembly and surrounding structure of the LH elevator for cracking and loose or sheared rivets using Fokker Service Bulletin F27/55-66. Replace discrepant parts, repair cracks in the rib at station 300, or stop drill and repeat inspections for cracks not exceeding 30 mm, all as specified in the service bulletin.

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

Compliance Time

Prior to the accumulation of 45,000 total flight cycles, or within 4 months after the effective date of this AD, whichever occurs later.

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

Affected Aircraft

Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 series 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 8, 2026

Rights: U.S. Government Public Domain

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