Airworthiness directives › 2006-03-07
AD 2006-03-07 Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes
Models named: F.28 Mark 0070, 0100. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Fokker Model F.28 Mark 0070 and 0100 airplanes, certificated in any category, as identified in Fokker Service Bulletin SBF100-52-069, Revision 3, dated December 18, 2002.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Installation (f) Within 30 months after the effective date of this AD, modify the passenger door and install new placards, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-52-069, Revision 3, dated December 18, 2002; including Fokker Manual Change Notification—Operational Documentation MCNO-F100-031, dated December 3, 2001; and Fokker Manual Change Notification—Maintenance Documentation MCNM-F100-064, Revision 2, dated December 18, 2002; and including the drawings listed in Table 1 of this AD. (To conform to certain Office of the Federal Register requirements for incorporating these materials by reference, the table identifies the date of the service bulletin for undated drawings.) Table 1.—Drawings Included in Service Bulletin SBF100-52-069 Fokker drawing Sheet Issue Date W41074 065 DB December 18, 2002. W41418 003 L December 18, 2002. W41418 005 E December 18, 2002. W41418 006 E December 18, 2002. W41418 007 E December 18, 2002. W41418 008 M December 18, 2002. W42310 001 D August 14, 2000. W42310 002 B August 14, 2000. W42310 003 F June 11, 2001. W59243 024 AU June 12, 2001. W59261 017 W August 9, 2002. W59261 025 S July 3, 2001. Alternative Methods of Compliance (AMOCs) (g)(1) The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with 14 CFR 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Related Information (h) Dutch airworthiness directive 2002-057, dated April 29, 2002, also addresses the subject of this AD. Material Incorporated by Reference (i) You must use Fokker Service Bulletin SBF100-52-069, Revision 3, dated December 18, 2002; including Fokker Manual Change Notification—Operational Documentation MCNO-F100-031, dated December 3, 2001; and including Fokker Manual Change Notification—Maintenance Documentation MCNM-F100-064, Revision 2, dated December 18, 2002; and including the drawings listed in Table 2 of this AD, to do the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Fokker Services B.V., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands, for a copy of this service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov ; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html . Table 2.—Drawings Included in Service Bulletin SBF100-52-069 Fokker drawing Sheet Issue Date W41074 065 DB December 18, 2002. W41418 003 L December 18, 2002. W41418 005 E December 18, 2002. W41418 006 E December 18, 2002. W41418 007 E December 18, 2002. W41418 008 M December 18, 2002. W42310 001 D August 14, 2000. W42310 002 B August 14, 2000. W42310 003 F June 11, 2001. W59243 024 AU June 12, 2001. W59261 017 W August 9, 2002. W59261 025 S July 3, 2001. Issued in Renton, Washington, on January 26, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 06-988 Filed 2-7-06; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD results from reports of the airstairs-type passenger door opening during flight. We are issuing this AD to prevent rapid decompression of the airplane, or ejection of a passenger or crew member out the door during flight.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1