AD 2007-13-12 Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 Airplanes

Models named: P-180. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to Model P-180 airplanes, serial numbers 1002, 1004 through 1107, 1109, and 1110, certificated in any category.

Unless already done, do the following actions: (1) Within the next 200 hours time-in-service (TIS) after August 3, 2007 (the effective date of this AD) or within 60 days after August 3, 2007 (the effective date of this AD), whichever occurs first, replace the outboard flap track forward bushing and the outboard flap track forward support. Do the replacements using the Accomplishment Instructions detailed in Part A of Piaggio Aero Industries S.p.A. Mandatory Service Bulletin (SB) No. 80-0210, Rev 4, dated July 19, 2006. (2) At intervals not to exceed 1,500 hours TIS after doing the replacements required in paragraph (f)(1) of this AD, visually inspect the outboard flap track forward support for traces of any kind of corrosion and/or protective coat/finishing wear damage. Do the inspections using the Accomplishment Instructions detailed in Part B of Piaggio Aero Industries S.p.A. Mandatory SB No. 80-0210, Rev 4, dated July 19, 2006. (3) Before further flight after each inspection required in paragraph (f)(2) of this AD in which any kind of corrosion or wear damage is found, contact the manufacturer for a repair scheme and incorporate the repair. 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, Standards Staff, FAA, Small Airplane Directorate, ATTN: Sarjapur Nagarajan, Aerospace Engineer, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4145; fax: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. 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 (44 U.S.C. 3501 et seq. ), 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 European Aviation Safety Agency (EASA) AD No. 2006-0305, dated October 9, 2006; and Piaggio Aero Industries S.p.A. Mandatory Service Bulletin No. 80-0210, Rev 4, dated July 19, 2006, for related information. Material Incorporated by Reference (i) You must use Piaggio Aero Industries S.p.A. Mandatory Service Bulletin No. 80-0210, Rev 4, dated July 19, 2006, to do the actions required by this AD, unless the AD specifies otherwise. (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 PIAGGIO AERO INDUSTRIES S.p.A, Via Cibrario 4, 16154 Genoa, Italy; telephone: +39 010 6481 856; facsimile: +39 010 6481 374. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; 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 Kansas City, Missouri, on June 15, 2007. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-12008 Filed 6-28-07; 8:45 am] BILLING CODE 4910-13-P

Unless already done, do the following actions: (1) Within the next 200 hours time-in-service (TIS) after August 3, 2007 (the effective date of this AD) or within 60 days after August 3, 2007 (the effective date of this AD), whichever occurs first, replace the outboard flap track forward bushing and the outboard flap track forward support. Do the replacements using the Accomplishment Instructions detailed in Part A of Piaggio Aero Industries S.p.A. Mandatory Service Bulletin (SB) No. 80-0210, Rev 4, dated July 19, 2006. (2) At intervals not to exceed 1,500 hours TIS after doing the replacements required in paragraph (f)(1) of this AD, visually inspect the outboard flap track forward support for traces of any kind of corrosion and/or protective coat/finishing wear damage. Do the inspections using the Accomplishment Instructions detailed in Part B of Piaggio Aero Industries S.p.A. Mandatory SB No. 80-0210, Rev 4, dated July 19, 2006. (3) Before further flight after each inspection required in paragraph (f)(2) of this AD in which any kind of corrosion or wear damage is found, contact the manufacturer for a repair scheme and incorporate the repair. 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, Standards Staff, FAA, Small Airplane Directorate, ATTN: Sarjapur Nagarajan, Aerospace Engineer, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4145; fax: (816) 329-4090, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. 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 (44 U.S.C. 3501 et seq. ), 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 European Aviation Safety Agency (EASA) AD No. 2006-0305, dated October 9, 2006; and Piaggio Aero Industries S.p.A. Mandatory Service Bulletin No. 80-0210, Rev 4, dated July 19, 2006, for related information. Material Incorporated by Reference (i) You must use Piaggio Aero Industries S.p.A. Mandatory Service Bulletin No. 80-0210, Rev 4, dated July 19, 2006, to do the actions required by this AD, unless the AD specifies otherwise. (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 PIAGGIO AERO INDUSTRIES S.p.A, Via Cibrario 4, 16154 Genoa, Italy; telephone: +39 010 6481 856; facsimile: +39 010 6481 374. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; 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 Kansas City, Missouri, on June 15, 2007. Kim Smith, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-12008 Filed 6-28-07; 8:45 am] BILLING CODE 4910-13-P