AD 2009-18-09 Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes

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

This AD applies to airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Fokker Model F.28 Mark 0100 airplanes, all serial numbers. (2) Fokker Model F.28 Mark 0070 airplanes, serial numbers 11521, 11528 through 11537 inclusive, 11545, 11547, 11553, 11557, 11561, 11562, 11566, 11567, 11571, 11572, 11576 through 11579 inclusive, and 11581 through 11583 inclusive. All airplanes with these serial numbers are fitted with center wing fuel tanks.

Unless already done, do the following actions. (1) Within 36 months after the effective date of this AD, replace FWC units having part number (P/N) 80-0610-3-45 and P/N 80-0610-3-50 with modified units having P/N 80-0610-3-55, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-31-067, Revision 1, dated April 24, 2008. (2) Within 36 months after the effective date of this AD and concurrently with the accomplishment of paragraph (h)(1) of this AD, revise the Emergency and Abnormal Procedures sections of the airplane flight manual (AFM), as specified in Fokker Manual Change Notification-Operational Documentation MCNO-F100-050, dated January 31, 2008, which is included in Fokker Service Bulletin SBF100-31-067, Revision 1, dated April 24, 2008. These AFM sections provide alterations, which are introduced in Fokker Service Bulletin SBF100-31-067, Revision 1, dated April 24, 2008. Note 4: Revisions to the Emergency Procedures and Abnormal Procedures sections of the AFM, as specified in Fokker MCNO-F100-050, dated January 31, 2008, may be done by inserting copies of Fokker MCNO-F100-050, dated January 31, 2008, into the AFM. When the information in Fokker MCNO-F100-050, dated January 31, 2008, has been included in general revisions of the AFM, the general revisions may be inserted in the AFM, provided the relevant information in the general revisions are identical to that in Fokker MCNO-F100-050, dated January 31, 2008. (3) After accomplishing paragraph (h)(1) of this AD, no person may install an FWC having P/N 80-0610-3-45 or P/N 80-0610-3-50, unless it has been modified to P/N 80-0610-3-55 standard in accordance with Honeywell Service Bulletin 80-0610-31-0003, dated February 13, 2008. (4) Within 36 months after the effective date of this AD, install software version V12 for the MFDU in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-31-060, dated June 1, 2002. (5) Within 36 months after the effective date of this AD, modify the thrust reverser indication and control system in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-78-016, dated October 1, 1999; or modify the thrust reverser unlock indication relay in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-78-017, dated December 1, 1999. FAA AD Differences Note 5: This AD differs from the MCAI and/or service information as follows: (1) Replacing the MFDU in accordance with Fokker Service Bulletin SBF100-31-060, dated June 1, 2002, is not included in the MCAI; however, this AD includes that action. It is necessary to install a new version of the MFDU software before installing the new version of the FWC software. (2) Modifying the thrust reverser indication and control system in accordance with Fokker Service Bulletin SBF100-78-016, dated October 1, 1999; or modifying the thrust reverser unlock indication relay in accordance with Fokker Service Bulletin SBF100-78-017, dated December 1, 1999, is not included in the MCAI; however, this AD includes those actions. It is necessary to do one of those actions before installing the MFDU software. Other FAA AD Provisions (i) 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, Transport Airplane Directorate, FAA, 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 principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. (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 (j) Refer to MCAI European Aviation Safety Agency Airworthiness Directive 2008-0090, dated May 13, 2008, and the service information identified in Table 1 of this AD, for related information. Table 1—Related Information Service information— Revision level— Dated— Fokker Service Bulletin SBF100-31-047 1 March 21, 1997. Fokker Service Bulletin SBF100-31-051 Original August 15, 1998. Fokker Service Bulletin SBF100-31-060 Original June 1, 2002. Fokker Service Bulletin SBF100-31-067, including Fokker Manual Change Notification-Operational Documentation MCNO-F100-50, dated January 31, 2008 1 April 24, 2008. Fokker Service Bulletin SBF100-78-016 Original October 1, 1999. Fokker Service Bulletin SBF100-78-017 Original December 1, 1999. Material Incorporated by Reference (k) You must use the service information contained in Table 2 of this AD to do the actions required by this AD, unless the AD specifies otherwise. Table 2—All Material Incorporated by Reference Document Revision Date Fokker Service Bulletin SBF100-31-047 1 March 21, 1997. Fokker Service Bulletin SBF100-31-051 Original August 15, 1998. Fokker Service Bulletin SBF100-31-060 Original June 1, 2002. Fokker Service Bulletin SBF100-31-067, including Fokker Manual Change Notification-Operational Documentation MCNO-F100-50, dated January 31, 2008 1 April 24, 2008. Fokker Service Bulletin SBF100-78-016 Original October 1, 1999. Fokker Service Bulletin SBF100-78-017 Original December 1, 1999. (1) The Director of the Federal Register approved the incorporation by reference of the service information contained in Table 3 of this AD under 5 U.S.C. 552(a) and 1 CFR part 51. Table 3—New Material Incorporated by Reference Document Revision Date Fokker Service Bulletin SBF100-31-060 Original June 1, 2002. Fokker Service Bulletin SBF100-31-067, including Fokker Manual Change Notification-Operational Documentation MCNO-F100-50, dated January 31, 2008 1 April 24, 2008. Fokker Service Bulletin SBF100-78-016 Original October 1, 1999. Fokker Service Bulletin SBF100-78-017 Original December 1, 1999. (2) The Director of the Federal Register previously approved the incorporation by reference of Fokker Service Bulletin SBF100-31-047, Revision 1, dated March 21, 1997; and Fokker Service Bulletin SBF100-31-051, dated August 15, 1998; on October 27, 1999 (64 FR 51202, September 22, 1999). (3) For Fokker service information identified in this AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands; telephone +31 (0)252-627-350; fax +31 (0)252-627-211; e-mail technicalservices.fokkerservices@stork.com ; Internet http://www.myfokkerfleet.com . (4) For AlliedSignal Grimes Aerospace and Honeywell service information identified in this AD, contact Honeywell Aerospace, Technical Publications and Distribution, M/S 2101-201, P.O. Box 52170, Phoenix, Arizona 85072-2170; telephone 602-365-5535; fax 602-365-5577; Internet http://www.honeywell.com . (5) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152. (6) You may also review copies of the service information that is incorporated by reference 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/code_of_federal_regulations/ibr_locations.html. Issued in Renton, Washington, on August 18, 2009. Stephen P. Boyd, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E9-20840 Filed 9-8-09; 8:45 am] BILLING CODE 4910-13-P

Unless already done, do the following actions. (1) Within 36 months after the effective date of this AD, replace FWC units having part number (P/N) 80-0610-3-45 and P/N 80-0610-3-50 with modified units having P/N 80-0610-3-55, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-31-067, Revision 1, dated April 24, 2008. (2) Within 36 months after the effective date of this AD and concurrently with the accomplishment of paragraph (h)(1) of this AD, revise the Emergency and Abnormal Procedures sections of the airplane flight manual (AFM), as specified in Fokker Manual Change Notification-Operational Documentation MCNO-F100-050, dated January 31, 2008, which is included in Fokker Service Bulletin SBF100-31-067, Revision 1, dated April 24, 2008. These AFM sections provide alterations, which are introduced in Fokker Service Bulletin SBF100-31-067, Revision 1, dated April 24, 2008. Note 4: Revisions to the Emergency Procedures and Abnormal Procedures sections of the AFM, as specified in Fokker MCNO-F100-050, dated January 31, 2008, may be done by inserting copies of Fokker MCNO-F100-050, dated January 31, 2008, into the AFM. When the information in Fokker MCNO-F100-050, dated January 31, 2008, has been included in general revisions of the AFM, the general revisions may be inserted in the AFM, provided the relevant information in the general revisions are identical to that in Fokker MCNO-F100-050, dated January 31, 2008. (3) After accomplishing paragraph (h)(1) of this AD, no person may install an FWC having P/N 80-0610-3-45 or P/N 80-0610-3-50, unless it has been modified to P/N 80-0610-3-55 standard in accordance with Honeywell Service Bulletin 80-0610-31-0003, dated February 13, 2008. (4) Within 36 months after the effective date of this AD, install software version V12 for the MFDU in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-31-060, dated June 1, 2002. (5) Within 36 months after the effective date of this AD, modify the thrust reverser indication and control system in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-78-016, dated October 1, 1999; or modify the thrust reverser unlock indication relay in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-78-017, dated December 1, 1999. FAA AD Differences Note 5: This AD differs from the MCAI and/or service information as follows: (1) Replacing the MFDU in accordance with Fokker Service Bulletin SBF100-31-060, dated June 1, 2002, is not included in the MCAI; however, this AD includes that action. It is necessary to install a new version of the MFDU software before installing the new version of the FWC software. (2) Modifying the thrust reverser indication and control system in accordance with Fokker Service Bulletin SBF100-78-016, dated October 1, 1999; or modifying the thrust reverser unlock indication relay in accordance with Fokker Service Bulletin SBF100-78-017, dated December 1, 1999, is not included in the MCAI; however, this AD includes those actions. It is necessary to do one of those actions before installing the MFDU software. Other FAA AD Provisions (i) 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, Transport Airplane Directorate, FAA, 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 principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. (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 (j) Refer to MCAI European Aviation Safety Agency Airworthiness Directive 2008-0090, dated May 13, 2008, and the service information identified in Table 1 of this AD, for related information. Table 1—Related Information Service information— Revision level— Dated— Fokker Service Bulletin SBF100-31-047 1 March 21, 1997. Fokker Service Bulletin SBF100-31-051 Original August 15, 1998. Fokker Service Bulletin SBF100-31-060 Original June 1, 2002. Fokker Service Bulletin SBF100-31-067, including Fokker Manual Change Notification-Operational Documentation MCNO-F100-50, dated January 31, 2008 1 April 24, 2008. Fokker Service Bulletin SBF100-78-016 Original October 1, 1999. Fokker Service Bulletin SBF100-78-017 Original December 1, 1999. Material Incorporated by Reference (k) You must use the service information contained in Table 2 of this AD to do the actions required by this AD, unless the AD specifies otherwise. Table 2—All Material Incorporated by Reference Document Revision Date Fokker Service Bulletin SBF100-31-047 1 March 21, 1997. Fokker Service Bulletin SBF100-31-051 Original August 15, 1998. Fokker Service Bulletin SBF100-31-060 Original June 1, 2002. Fokker Service Bulletin SBF100-31-067, including Fokker Manual Change Notification-Operational Documentation MCNO-F100-50, dated January 31, 2008 1 April 24, 2008. Fokker Service Bulletin SBF100-78-016 Original October 1, 1999. Fokker Service Bulletin SBF100-78-017 Original December 1, 1999. (1) The Director of the Federal Register approved the incorporation by reference of the service information contained in Table 3 of this AD under 5 U.S.C. 552(a) and 1 CFR part 51. Table 3—New Material Incorporated by Reference Document Revision Date Fokker Service Bulletin SBF100-31-060 Original June 1, 2002. Fokker Service Bulletin SBF100-31-067, including Fokker Manual Change Notification-Operational Documentation MCNO-F100-50, dated January 31, 2008 1 April 24, 2008. Fokker Service Bulletin SBF100-78-016 Original October 1, 1999. Fokker Service Bulletin SBF100-78-017 Original December 1, 1999. (2) The Director of the Federal Register previously approved the incorporation by reference of Fokker Service Bulletin SBF100-31-047, Revision 1, dated March 21, 1997; and Fokker Service Bulletin SBF100-31-051, dated August 15, 1998; on October 27, 1999 (64 FR 51202, September 22, 1999). (3) For Fokker service information identified in this AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE Nieuw-Vennep, the Netherlands; telephone +31 (0)252-627-350; fax +31 (0)252-627-211; e-mail technicalservices.fokkerservices@stork.com ; Internet http://www.myfokkerfleet.com . (4) For AlliedSignal Grimes Aerospace and Honeywell service information identified in this AD, contact Honeywell Aerospace, Technical Publications and Distribution, M/S 2101-201, P.O. Box 52170, Phoenix, Arizona 85072-2170; telephone 602-365-5535; fax 602-365-5577; Internet http://www.honeywell.com . (5) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152. (6) You may also review copies of the service information that is incorporated by reference 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/code_of_federal_regulations/ibr_locations.html. Issued in Renton, Washington, on August 18, 2009. Stephen P. Boyd, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E9-20840 Filed 9-8-09; 8:45 am] BILLING CODE 4910-13-P