AD 2008-11-12 Airworthiness Directives; Fokker Model F.28 Mark 0070 and Mark 0100 Airplanes

Models named: F.28 Mark 0070, 0100. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to Fokker Model F.28 Mark 0070 and 0100 airplanes, all serial numbers; certificated in any category.

Within 36 months after the effective date of this AD, unless already done, install autopilot disconnect units and do associated wiring changes in accordance with Section 3, “Accomplishment Instructions,” of Fokker Service Bulletin SBF100-22-050, dated April 25, 2006, including the drawings listed in Table 1 of this AD. Table 1.—Drawings Included in Fokker Service Bulletin SBF100-22-050 Fokker drawing Sheet Issue Date W41501 057 CQ April 25, 2006. W41501 058 CQ April 25, 2006. W41501 059 CQ April 25, 2006. W41501 060 CQ April 25, 2006. W41501 061 CR April 25, 2006. W41501 062 CR April 25, 2006. W41504 009 K April 25, 2006. W41504 010 K April 25, 2006. W41504 011 J April 25, 2006. W41504 012 L April 25, 2006. W41504 013 L April 25, 2006. W46140 27 AR March 5, 2002. W46140 28 AR March 8, 2002. W46143 02 K February 26, 2002. W46143 03 K March 7, 2002. W46144 06 R March 4, 2002. W46144 07 S March 7, 2002. W46912 01 D March 12, 2002. W46930 01 Original March 14, 2002. W46930 02 E March 14, 2002. W46932 01 D March 13, 2002. W59140 177 GC February 8, 2006. W59140 178 GB February 6, 2006. W59140 221 GB February 6, 2006. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1137; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI Dutch Airworthiness Directive NL-2006-010, dated July 14, 2006; and Fokker Service Bulletin SBF100-22-050, dated April 25, 2006, including the drawings listed in Table 1 of this AD, for related information. Material Incorporated by Reference (i) You must use Fokker Service Bulletin SBF100-22-050, dated April 25, 2006, including the drawings specified in Table 2 of this AD, to do the actions required by this AD, unless the AD specifies otherwise. Table 2.—Drawings Included in Fokker Service Bulletin SBF100-22-050 Fokker drawing Sheet Issue Date W41501 057 CQ April 25, 2006. W41501 058 CQ April 25, 2006. W41501 059 CQ April 25, 2006. W41501 060 CQ April 25, 2006. W41501 061 CR April 25, 2006. W41501 062 CR April 25, 2006. W41504 009 K April 25, 2006. W41504 010 K April 25, 2006. W41504 011 J April 25, 2006. W41504 012 L April 25, 2006. W41504 013 L April 25, 2006. W46140 27 AR March 5, 2002. W46140 28 AR March 8, 2002. W46143 02 K February 26, 2002. W46143 03 K March 7, 2002. W46144 06 R March 4, 2002. W46144 07 S March 7, 2002. W46912 01 D March 12, 2002. W46930 01 Original March 14, 2002. W46930 02 E March 14, 2002. W46932 01 D March 13, 2002. W59140 177 GC February 8, 2006. W59140 178 GB February 6, 2006. W59140 221 GB February 6, 2006. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands. (3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html . Issued in Renton, Washington, on May 14, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-11501 Filed 5-28-08; 8:45 am] BILLING CODE 4910-13-P

Within 36 months after the effective date of this AD, unless already done, install autopilot disconnect units and do associated wiring changes in accordance with Section 3, “Accomplishment Instructions,” of Fokker Service Bulletin SBF100-22-050, dated April 25, 2006, including the drawings listed in Table 1 of this AD. Table 1.—Drawings Included in Fokker Service Bulletin SBF100-22-050 Fokker drawing Sheet Issue Date W41501 057 CQ April 25, 2006. W41501 058 CQ April 25, 2006. W41501 059 CQ April 25, 2006. W41501 060 CQ April 25, 2006. W41501 061 CR April 25, 2006. W41501 062 CR April 25, 2006. W41504 009 K April 25, 2006. W41504 010 K April 25, 2006. W41504 011 J April 25, 2006. W41504 012 L April 25, 2006. W41504 013 L April 25, 2006. W46140 27 AR March 5, 2002. W46140 28 AR March 8, 2002. W46143 02 K February 26, 2002. W46143 03 K March 7, 2002. W46144 06 R March 4, 2002. W46144 07 S March 7, 2002. W46912 01 D March 12, 2002. W46930 01 Original March 14, 2002. W46930 02 E March 14, 2002. W46932 01 D March 13, 2002. W59140 177 GC February 8, 2006. W59140 178 GB February 6, 2006. W59140 221 GB February 6, 2006. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1137; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI Dutch Airworthiness Directive NL-2006-010, dated July 14, 2006; and Fokker Service Bulletin SBF100-22-050, dated April 25, 2006, including the drawings listed in Table 1 of this AD, for related information. Material Incorporated by Reference (i) You must use Fokker Service Bulletin SBF100-22-050, dated April 25, 2006, including the drawings specified in Table 2 of this AD, to do the actions required by this AD, unless the AD specifies otherwise. Table 2.—Drawings Included in Fokker Service Bulletin SBF100-22-050 Fokker drawing Sheet Issue Date W41501 057 CQ April 25, 2006. W41501 058 CQ April 25, 2006. W41501 059 CQ April 25, 2006. W41501 060 CQ April 25, 2006. W41501 061 CR April 25, 2006. W41501 062 CR April 25, 2006. W41504 009 K April 25, 2006. W41504 010 K April 25, 2006. W41504 011 J April 25, 2006. W41504 012 L April 25, 2006. W41504 013 L April 25, 2006. W46140 27 AR March 5, 2002. W46140 28 AR March 8, 2002. W46143 02 K February 26, 2002. W46143 03 K March 7, 2002. W46144 06 R March 4, 2002. W46144 07 S March 7, 2002. W46912 01 D March 12, 2002. W46930 01 Original March 14, 2002. W46930 02 E March 14, 2002. W46932 01 D March 13, 2002. W59140 177 GC February 8, 2006. W59140 178 GB February 6, 2006. W59140 221 GB February 6, 2006. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands. (3) You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html . Issued in Renton, Washington, on May 14, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-11501 Filed 5-28-08; 8:45 am] BILLING CODE 4910-13-P