AD 97-01-08

final rule
Data completeness: 70%

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

AD Number
97-01-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
96-NM-28-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

Loose or missing rivets at the rib-to-stringer connections of the upper and lower wing skin at stringers 5 and 6 could result in reduced structural integrity of the wings.

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

Required Actions

Perform a one-time visual inspection to detect missing rivet heads or loose rivets in accordance with Fokker Service Bulletin F27/57-74. Repair any detected issues before further flight. Replace rivets with part number MS20600AD4W2 using new rivets CR3553P4 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 10,000 total flight cycles, or within 2 months after the effective date of this AD, whichever occurs later for the inspection; and within 1 year after the effective date of this AD, or prior to 10,000 flight cycles, whichever is later for the rivet replacement.

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, serial numbers 10653 through 10692 inclusive, where Part 1 of Fokker Service Bulletins F27/57-68 and F27/57-70 has not been accomplished.

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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