AD 2007-12-16 Airworthiness Directives; Dassault Model Falcon 2000EX and Falcon 900EX Airplanes

Models named: Falcon 2000EX. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to Dassault Model Falcon 2000EX airplanes, S/N (serial number) 82; and Model Falcon 900EX (version F900DX) airplanes, S/Ns 601 through 605; certificated in any category. Reason (d) The mandatory continuing airworthiness information (MCAI) states that following the incorporation of a design change to the Karman fairing, it has been determined that some stringer reinforcements (F900DX) and some rivets (F900DX/F2000EX) are missing from the skin panels on each side of the fuselage between frames 9 and 10 on certain Falcon 900DX and Falcon 2000EX EASy aircraft. This situation affects the structural integrity of the fuselage and may lead to an unsafe condition if left uncorrected. The MCAI was issued to recover the certificated structural strength by adding the missing rivets and checking the condition of the adjacent structure, and to add the missing stringer caps on F900DX (as appropriate). These actions include inspecting the area, including holes and structure, where missing rivets are found, and contacting the manufacturer if the holes are out-of-round beyond tolerance, or if cracks are found, as applicable.

Within 3 months after the effective date of this AD, unless already done, do the following actions: Inspect and repair the aircraft in accordance with the instructions of Dassault Service Bulletin F900EX-308, dated October 18, 2006, for version F900DX, S/N 601 through 605; and Dassault Service Bulletin F2000EX-133, dated September 28, 2006, for Model F2000EX S/N 82. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, 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, 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 (g) Refer to MCAI European Aviation Safety Agency (EASA) Emergency Airworthiness Directive 2006-0320-E, dated October 18, 2006; Dassault Service Bulletin F900EX-308, dated October 18, 2006; and Dassault Service Bulletin F2000EX-133, dated September 28, 2006; for related information. Material Incorporated by Reference (h) You must use Dassault Service Bulletin F900EX-308, dated October 18, 2006; or Dassault Service Bulletin F2000EX-133, dated September 28, 2006; as applicable, 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 Dassault Falcon Jet, P.O. Box 2000, South Hackensack, New Jersey 07606. (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 June 1, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-11203 Filed 6-13-07; 8:45 am] BILLING CODE 4910-13-P

Within 3 months after the effective date of this AD, unless already done, do the following actions: Inspect and repair the aircraft in accordance with the instructions of Dassault Service Bulletin F900EX-308, dated October 18, 2006, for version F900DX, S/N 601 through 605; and Dassault Service Bulletin F2000EX-133, dated September 28, 2006, for Model F2000EX S/N 82. FAA AD Differences Note: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (f) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate, 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, 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 (g) Refer to MCAI European Aviation Safety Agency (EASA) Emergency Airworthiness Directive 2006-0320-E, dated October 18, 2006; Dassault Service Bulletin F900EX-308, dated October 18, 2006; and Dassault Service Bulletin F2000EX-133, dated September 28, 2006; for related information. Material Incorporated by Reference (h) You must use Dassault Service Bulletin F900EX-308, dated October 18, 2006; or Dassault Service Bulletin F2000EX-133, dated September 28, 2006; as applicable, 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 Dassault Falcon Jet, P.O. Box 2000, South Hackensack, New Jersey 07606. (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 June 1, 2007. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E7-11203 Filed 6-13-07; 8:45 am] BILLING CODE 4910-13-P