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Docket ID: [Docket No. FAA-2008-0296; Directorate Identifier 2007-NM-307-AD; Amendment 39-15567; AD 2008-13-04]
RIN ID: RIN 2120-AA64
SUBJECT CATEGORY: Airworthiness Directives; Dassault Model Mystere-Falcon 20-C5, 20-D5, and 20-E5 Airplanes
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 24, 2008.
DOCUMENT SUMMARY: We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
This Airworthiness Directive (AD) is prompted by the discovery on an inservice MystereFalcon 20C5 of a collapsed wing antiice flexible hose due to internal ply separation.
Consequences on the aircraft can be insufficient antiicing not
detected by the monitoring system. Ice accretion on the wing might
then occur and might jeopardize the aircraft flight performance and safety.
* * * * *
The unsafe condition is undetected excessive ice buildup on the wings,
which could interfere with controllability of the airplane. We are
issuing this AD to require actions to correct the unsafe condition on
these products.
SUMMARY: Dassault Model Mystere-Falcon 20-C5, 20-D5, and 20-E5 Airplanes,
DOCUMENT BODY: [[Page 34850]]
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 March 13, 2008 (73 FR 13509). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states:
This Airworthiness Directive (AD) is prompted by the discovery on an inservice MystereFalcon 20C5 of a collapsed wing antiice flexible hose due to internal ply separation.
Consequences on the aircraft can be insufficient antiicing not detected by the monitoring system. Ice accretion on the wing might then occur and might jeopardize the aircraft flight performance and safety.
The present AD mandates replacement of the wing antiice flexible hoses by new ones of an improved design.
The unsafe condition is undetected excessive ice buildup on the wings,
which could interfere with controllability of the airplane. You may
obtain further information by examining the MCAI in the AD docket. Comments
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 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 highlighted in a NOTE within the AD.
We estimate that this AD will affect about 214 products of U.S. registry. We also estimate that it will take about 5 workhours per product to comply with the basic requirements of this AD. The average labor rate is $80 per workhour. Required parts will cost about $887 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 $275,418, or $1,287 per product.
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 this AD:
1. Is not a ``significant regulatory action'' under Executive Order 12866;
2. Is not a ``significant rule'' under the 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.
You may examine the AD docket on the Internet at http:// www.regulations.gov; or in person at the Docket Operations office 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 Operations office (telephone (800) 6475527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
[[Page 34851]]
Adoption of the Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
2. The FAA amends Sec. 39.13 by adding the following new AD:
20081304 Dassault Aviation (Formerly Avions Marcel Dassault
Breguet Aviation (AMD/BA)): Amendment 3915567. Docket No. FAA2008 0296; Directorate Identifier 2007NM307AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective July 24, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Dassault Model MystereFalcon 20C5, 20
D5, and 20E5 airplanes, certificated in any category, all serial numbers.
Subject
(d) Air Transport Association (ATA) of America Code 30: Ice and Rain Protection.
Reason
(e) The mandatory continuing airworthiness information (MCAI) states:
This Airworthiness Directive (AD) is prompted by the discovery on an inservice MystereFalcon 20C5 of a collapsed wing antiice flexible hose due to internal ply separation.
Consequences on the aircraft can be insufficient antiicing not detected by the monitoring system. Ice accretion on the wing might then occur and might jeopardize the aircraft flight performance and safety.
The present AD mandates replacement of the wing antiice flexible hoses by new ones of an improved design.
The unsafe condition is undetected excessive ice buildup on the
wings, which could interfere with controllability of the airplane. Actions and Compliance
(f) Within 7 months after the effective date of this AD, unless already done, do the following actions.
(1) Inspect to determine whether any wing antiice flexible hose
having part number (P/N) FAL1006 or P/N ARM224A is installed. A
review of airplane maintenance records is acceptable in lieu of this
inspection if the part number of the wing antiice flexible hose can
be conclusively determined from that review. If any wing antiice
flexible hose does not have P/N FAL1006 or P/N ARM224A, no further
action is required by this AD for that hose, except as required by paragraph (f)(3) of this AD.
(2) Remove any wing antiice flexible hose having P/N FAL1006 or
P/N ARM224A, and install a new hose having ESPA (brand) P/N
60503104509; in accordance with the Accomplishment Instructions of Dassault Service Bulletin F20775, dated July 9, 2007.
(3) As of the effective date of this AD, no person shall install
any flexible hose having P/N FAL1006 or P/N ARM224A on any Model
MystereFalcon 20C5, 20D5, or 20E5 airplane specified in the applicability of this AD.
Note 1: This AD differs from the MCAI and/or service information
as follows: The MCAI does not require inspecting to determine the
part numbers of the wing antiice flexible hoses. This AD requires such an inspection.
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM116, 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, ANM116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton,
Washington 980573356; telephone (425) 2271137; fax (425) 2271149.
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 FAAapproved. Corrective actions are considered
FAAapproved 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 European Aviation Safety Agency Airworthiness
Directive 20070227, dated September 17, 2007; and Dassault Service
Bulletin F20775, dated July 9, 2007; for related information. Material Incorporated by Reference
(i) You must use Dassault Service Bulletin F20775, dated July
9, 2007, 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
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) 7416030,
or go to: http://www.archives.gov/federalregister/cfr/ibr locations.html.
Issued in Renton, Washington, on June 9, 2008.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. E813576 Filed 61808; 8:45 am]
BILLING CODE 491013P
FOR FURTHER INFORMATION CONTACT Tom Rodriguez, Aerospace Engineer, International Branch, ANM116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 980573356; telephone (425) 2271137; fax (425) 2271149.
14 CFR Part 39 40 CFR Part 52 14 CFR Part 71 33 CFR Part 165 47 CFR Part 73 26 CFR Part 1 50 CFR Part 679 40 CFR Part 180 50 CFR Part 17 33 CFR Part 117 44 CFR Part 67 50 CFR Part 648 14 CFR Part 97 40 CFR Part 63 6 CFR Part 5 33 CFR Part 100 50 CFR Part 622 50 CFR Part 660 26 CFR Part 301 44 CFR Part 65 39 CFR Part 111 40 CFR Part 271 40 CFR Part 300 47 CFR Part 64 40 CFR Parts 52 and 81 50 CFR Part 665 39 CFR Part 3020 50 CFR Part 229 44 CFR Part 64 49 CFR Part 571