Base
Rule01-300812001-12-05

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

Transportation Department, Federal Aviation Administration

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Fokker Model F.28 Mark 0100 series airplanes. This action requires repetitive inspections of certain main landing gear (MLG) main fittings to detect forging defects, and rework of the main fittings if necessary. This action is necessary to detect forging defects of the MLG main fittings, which could lead to cracking and result in significant structural damage to the airplane and possible injury to the occupants.

Action & Dates

Action
Final rule; request for comments.
Dates
Effective December 20, 2001.
Effective Date
2001-12-20

CFR References

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Document Excerpt

Document Headings Document headings vary by document type but may contain the following: the agency or agencies that issued and signed a document the number of the CFR title and the number of each part the document amends, proposes to amend, or is directly related to the agency docket number / agency internal file number the RIN which identifies each regulatory action listed in the Unified Agenda of Federal Regulatory and Deregulatory Actions See the Document Drafting Handbook for more details. Department of Transportation Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-327-AD; Amendment 39-12527; AD 2001-24-10] RIN 2120-AA64 AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule; request for comments. SUMMARY: This amendment adopts a new airworthiness directive (AD) that is applicable to certain Fokker Model F.28 Mark 0100 series airplanes. This action requires repetitive inspections of certain main landing gear (MLG) main fittings to detect forging defects, and rework of the main fittings if necessary. This action is necessary to detect forging defects of the MLG main fittings, which could lead to cracking and result in significant structural damage to the airplane and possible injury to the occupants. DATES: Effective December 20, 2001. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of December 20, 2001. Comments for inclusion in the Rules Docket must be received on or before January 4, 2002. ADDRESSES: Submit comments in triplicate to the Federal Aviation Administration (FAA), Transport Airplane Directorate, ANM-114, Attention: Rules Docket No. 2001-NM-327-AD, 1601 Lind Avenue, SW., Renton, Washington 98055-4056. Comments may be inspected at this location between 9 a.m. and 3 p.m., Monday through Friday, except Federal holidays. Comments may be submitted via fax to (425) 227-1232. Comments may also be sent via the Internet using the following add…

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Full Document

Citation: 66 FR 63159