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Start Preamble
AGENCY:
Federal Aviation Administration (FAA), Department of Transportation (DOT).
ACTION:
Final Rule.
SUMMARY:
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 aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
To prevent cracks developing in the aileron spar adjacent to the inboard hinge attachment * * *
We are issuing this AD to require actions to correct the unsafe condition on these products.
DATES:
This AD becomes effective October 2, 2007.
On October 2, 2007, the Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD.
ADDRESSES:
You may examine the AD docket on the Internet at http://dms.dot.gov or in person at Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590.
Start Further InfoFOR FURTHER INFORMATION CONTACT:
Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090.
End Further Info End Preamble Start Supplemental InformationSUPPLEMENTARY INFORMATION:
Discussion
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 July 6, 2007 (72 FR 36905). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states:
To prevent cracks developing in the aileron spar adjacent to the inboard hinge attachment accomplish the following:
Remove both ailerons, inspect and modify the aileron spar at the inboard hinge attachment point in accordance with Pacific Aerospace Ltd Service Bulletin PACSB/XL/027.
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.
Conclusion
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 FAA policies. Any such differences are highlighted in a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect 7 products of U.S. registry. We also estimate that it will take about 6 work-hours per product to comply with basic requirements of this AD. The average labor rate is $80 per work-hour. Required parts will cost about $864 per product.
Based on these figures, we estimate the cost of this AD to the U.S. operators to be $9,408 or $1,344 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.
Regulatory Findings
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 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 Start Printed Page 49173List of Subjects in 14 CFR Part 39
- Air transportation
- Aircraft
- Aviation safety
- Incorporation by reference
- Safety
Adoption of the Amendment
Start Amendment PartAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
End Amendment Part Start PartPART 39—AIRWORTHINESS DIRECTIVES
End Part Start Amendment Part1. The authority citation for part 39 continues to read as follows:
End Amendment Part[Amended]2. The FAA amends § 39.13 by adding the following new AD:
End Amendment Part2007-17-20 Pacific Aerospace Limited: Amendment 39-15178; Docket No. FAA-2007-28436; Directorate Identifier 2007-CE-055-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective October 2, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to 750XL airplanes, serial numbers 101, 102, 104 through 120, and 122 through 129, certificated in any category.
Subject
(d) Air Transport Association of America (ATA) Code 27: Flight Controls.
Reason
(e) The mandatory continuing airworthiness information (MCAI) states:
To prevent cracks developing in the aileron spar adjacent to the inboard hinge attachment accomplish the following:
Remove both ailerons, inspect and modify the aileron spar at the inboard hinge attachment point in accordance with Pacific Aerospace Ltd Service Bulletin PACSB/XL/027.
Actions and Compliance
(f) Unless already done, within the next 6 months after October 2, 2007 (the effective date of this AD) or within the next 150 hours time-in-service after October 2, 2007 (the effective date of this AD), whichever occurs first, rework the left and right ailerons in accordance with Pacific Aerospace Ltd drawing number 11-03141/42, drawn March 26, 2007, as specified in Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/027, dated March 27, 2007.
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, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090. 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 Civil Aviation Authority of New Zealand AD DCA/750XL/13, effective date April 26, 2007; Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/027, dated March 27, 2007; and Pacific Aerospace Ltd drawing number 11-03141/42, drawn March 26, 2007, for related information.
Material Incorporated by Reference
(i) You must use Pacific Aerospace Limited Mandatory Service Bulletin PACSB/XL/027, dated March 27, 2007; and Pacific Aerospace Ltd drawing number 11-03141/42, drawn March 26, 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 Pacific Aerospace Limited, Private Bag HN3027, Hamilton, New Zealand, telephone: +(64) 7-843-6144, fax: +(64) 7-843-6134, e-mail: pacific@aerospace.co.nz.
(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.
Start SignatureIssued in Kansas City, Missouri, on August 16, 2007.
Terry L. Chasteen,
Acting Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-16652 Filed 8-27-07; 8:45 am]
BILLING CODE 4910-13-P
Document Information
- Effective Date:
- 10/2/2007
- Published:
- 08/28/2007
- Department:
- Federal Aviation Administration
- Entry Type:
- Rule
- Action:
- Final Rule.
- Document Number:
- E7-16652
- Dates:
- This AD becomes effective October 2, 2007.
- Pages:
- 49172-49173 (2 pages)
- Docket Numbers:
- Docket No. FAA-2007-28436 Directorate Identifier 2007-CE-055-AD, Amendment 39-15178, AD 2007-17-20
- RINs:
- 2120-AA64: Airworthiness Directives
- RIN Links:
- https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
- Topics:
- Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety
- PDF File:
- e7-16652.pdf
- CFR: (1)
- 14 CFR 39.13