Federal Aviation Administration (FAA), Department of Transportation (DOT).
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an airworthiness authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as some stringer reinforcements (F900DX) and some rivets (F900DX/F2000EX) 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. We are issuing this AD to require actions to correct the unsafe condition on these products.
This AD becomes effective July 19, 2007.
The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of July 19, 2007.
You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC.Start Further Info
FOR FURTHER INFORMATION CONTACT:
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.End Further Info End Preamble Start Supplemental Information
The FAA is implementing a new process for streamlining the issuance of ADs related to MCAI. This streamlined process will allow us to adopt MCAI safety requirements in a more efficient manner and will reduce safety risks to the public. This process continues to allow all FAA AD issuance processes to meet legal, economic, Administrative Procedure Act, and Federal Register requirements. We also continue to meet our technical decision-making responsibilities to identify and correct unsafe conditions on U.S.-certificated products.
This AD references the MCAI and related service information that we considered in forming the engineering basis to correct the unsafe condition. The AD contains text copied from the MCAI and for this reason might not follow our plain language principles.
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to the specified products. That NPRM was published in the Federal Register on April 12, 2007 (72 FR 18415). That NPRM proposed to require inspecting skin panels on each side of the fuselage between frames 9 and 10, including holes and structure, where missing rivets are found, adding missing rivets and stringer caps, as applicable, and contacting the manufacturer if the holes are out-of-round beyond tolerance, or if cracks are found, as applicable. The MCAI states that following the incorporation of a design change to the Karman fairing, it has been determined that some stringer reinforcements Start Printed Page 32777(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. 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). This situation affects the structural integrity of the fuselage and may lead to an unsafe condition if left uncorrected.
We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM or on the determination of the cost to the public.
We reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed.
Differences Between This AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the AD is clear for U.S. operators and is enforceable in a U.S. court of law. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information.
We might also have required different actions in this AD from those in the MCAI in order to follow our FAA policies. Any such differences are described in a separate paragraph of the AD. These requirements, if any, take precedence over the actions copied from the MCAI.
Costs of Compliance
We estimate that this AD will affect about 2 products of U.S. registry. We also estimate that it will take about 170 work-hours per product to comply with this AD. The average labor rate is $80 per work-hour. Required parts will cost $0 per product. Where the service information lists required parts costs that are covered under warranty, we have assumed that there will be no charge for these parts. As we do not control warranty coverage for affected parties, some parties may incur costs higher than estimated here. Based on these figures, we estimate the cost of this AD to the U.S. operators to be $27,200, or $13,600 per product.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. “Subtitle VII: Aviation Programs,” describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in “Subtitle VII, Part A, Subpart III, Section 44701: General requirements.” Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action.
We determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a “significant regulatory action” under Executive Order 12866;
(2) Is not a “significant rule” under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and
(3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to comply with this AD and placed it in the AD Docket.
Examining the AD Docket
You may examine the AD docket on the Internet at http://dms.dot.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains the NPRM, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone (800) 647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.Start List of Subjects
List of Subjects in 14 CFR Part 39End List of Subjects
Adoption of the AmendmentStart Amendment Part
Accordingly, under the authority delegated to me by the Administrator, the FAA amendsEnd Amendment Part Start Part
PART 39—AIRWORTHINESS DIRECTIVESEnd Part Start Amendment Part
1. The authority citation for part 39 continues to read as follows:End Amendment Part
2. The FAA amends § 39.13 by adding the following new AD:End Amendment Part
2007-12-16 Dassault Aviation: Amendment 39-15094. Docket No. FAA-2007-27849; Directorate Identifier 2006-NM-249-AD.
(a) This airworthiness directive (AD) becomes effective July 19, 2007.
(c) 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.
(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.
Actions and Compliance
(e) 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 Start Printed Page 32778Bulletin F2000EX-133, dated September 28, 2006, for Model F2000EX S/N 82.
FAA AD Differences
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.
(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.
(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.Start Signature
Issued in Renton, Washington, on June 1, 2007.
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-11203 Filed 6-13-07; 8:45 am]
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