Airworthiness Directives; Dassault Aviation Airplanes
Federal Register, Volume 81 Issue 245 (Wednesday, December 21, 2016)
Federal Register Volume 81, Number 245 (Wednesday, December 21, 2016)
Proposed Rules
Pages 93645-93647
From the Federal Register Online via the Government Publishing Office www.gpo.gov
FR Doc No: 2016-30029
Page 93645
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Docket No. FAA-2016-9504; Directorate Identifier 2016-NM-107-AD
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 7X airplanes. This proposed AD was prompted by reports that during the assembly of structural elements on some airplanes, lack of established procedures and tools caused boring and torqueing defects to be present at some locations. This proposed AD would require a detailed visual inspection of bore holes for defects, replacement of bolts, and repair if necessary. We are proposing this AD to address the unsafe condition on these products.
DATES: We must receive comments on this proposed AD by February 6, 2017.
ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this NPRM, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com. You may view this referenced service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9504; 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 this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2016-9504; Directorate Identifier 2016-NM-107-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD based on those comments.
We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD.
Discussion
The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2016-0116, dated June 16, 2016 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Dassault Aviation Model FALCON 7X airplanes. The MCAI states:
During the assembly of structural elements on some aeroplanes, lack of established procedures and tools caused boring and torqueing defects to be present at some locations on the foot of frame (FR) 36 and FR39. Dassault Aviation (DA) identified the individual aeroplanes that are potentially affected by this production deficiency. Quality control actions have been implemented to ensure that new aeroplanes, from s/n 183, cannot be affected by this defect.
This condition, if not detected and corrected, would adversely affect the structural integrity of the aeroplane.
For the reasons described above, this EASA AD requires a detailed visual inspection of bore holes for defects and replacement of bolts at FR36 and FR39 and, depending on findings, accomplishment of a repair.
To address this potential unsafe condition, DA published Service Bulletin (SB) F7X-379 to provide corrective action instructions.
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
9504.
Related Service Information Under 1 CFR Part 51
We reviewed Dassault Service Bulletin 7X-379, dated February 29, 2016. The service information describes procedures for a detailed visual inspection of bore holes at FR36 and FR39 for defects, replacement of bolts at FR36 and FR39, and repair. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section.
FAA's Determination and Requirements of This Proposed AD
This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of the same type design.
Costs of Compliance
We estimate that this proposed AD affects 41 airplanes of U.S. registry.
We estimate the following costs to comply with this proposed AD:
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Estimated Costs
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Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Inspection and Replacement.......... 6 work-hours x $85 per $26 $536 $21,976
hour = $510.
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We have received no definitive data that would enable us to provide cost estimates for the on-condition repair specified in this proposed AD.
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.
Regulatory Findings
We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 proposed regulation:
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);
3. Will not affect intrastate aviation in Alaska; and
4. 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.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
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
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD):
Dassault Aviation: Docket No. FAA-2016-9504; Directorate Identifier 2016-NM-107-AD.
(a) Comments Due Date
We must receive comments by February 6, 2017.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Dassault Aviation Model FALCON 7X airplanes, certificated in any category, serial numbers (S/Ns) 2, 5, and 8 through 182 inclusive; except S/Ns 141, 148, 149, 157, 159, 166, 170, 171, 174, 175, and 177 through 180 inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Reason
This AD was prompted by reports that during the assembly of structural elements on some airplanes, lack of established procedures and tools caused boring and torqueing defects to be present at some locations on the foot of frame (FR) 36 and FR39. We are issuing this AD to detect and correct defects in the bore holes at FR36 and FR39 that could adversely affect the structural integrity of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified, unless already done.
(g) Inspection of Bore Holes
At the applicable time identified in paragraphs (g)(1) or (g)(2) of this AD, remove the sheer bolts at FR36 and FR39, left hand and right hand, as identified in Dassault Service Bulletin 7X-379, dated February 29, 2016, and do a detailed visual inspection of the bore holes for defects, in accordance with Dassault Service Bulletin 7X-
379, dated February 29, 2016.
(1) For airplanes with S/N 2 and 5: Before exceeding 4,100 flight cycles after the date of release to service after the first C-Check or within 3 months from the effective date of this AD, whichever occurs later.
(2) For airplanes other than those identified in paragraph (g)(1) of this AD: Before exceeding 4,100 flight cycles since the date of issuance of the original certificate of airworthiness or the original export certificate of airworthiness or within 3 months from the effective date of this AD, whichever occurs later.
(h) Repair of Bore Holes and Bolt Replacement
(1) If, during any inspection required by paragraph (g) of this AD, any defect is found, before further flight, repair the affected areas, and replace the sheer bolts at FR36 and FR39, in accordance with Dassault Service Bulletin 7X-379, dated February 29, 2016; except where Dassault Service Bulletin 7X-379, dated February 29, 2016, specifies to contact Dassault Aviation for instructions, before further flight, repair using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Dassault Aviation's EASA Design Organization Approval (DOA).
(2) If, during any inspection required by paragraph (g) of this AD, no defect is found, before further flight, replace the sheer bolts at FR36 and FR39, in accordance with Dassault Service Bulletin 7X-379, dated February 29, 2016.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to ATTN: Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/
certificate holding district office.
(2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the EASA; or Dassault Aviation's EASA
Page 93647
DOA. If approved by the DOA, the approval must include the DOA-
authorized signature.
(j) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2016-0116, dated June 16, 2016, for related information. This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-9504.
(2) For service information identified in this AD, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com. You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221.
Issued in Renton, Washington, on December 6, 2016.
Dionne Palermo,
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
FR Doc. 2016-30029 Filed 12-20-16; 8:45 am
BILLING CODE 4910-13-P
