Aviation Insurance, 78958 [E8-30838]

Download as PDF 78958 Federal Register / Vol. 73, No. 248 / Wednesday, December 24, 2008 / Rules and Regulations the FAA amends 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new AD: ■ 2008–26–08 Saab AB, Saab Aerosystems: Amendment 39–15774. Docket No. FAA–2008–1044; Directorate Identifier 2008–NM–095–AD. Effective Date (a) This airworthiness directive (AD) becomes effective January 28, 2009. Affected ADs (b) None. Applicability (c) This AD applies to Saab AB, Saab Aerosystems Model 340A (SAAB/SF340A) and SAAB 340B airplanes, all serial numbers, certificated in any category. pwalker on PROD1PC71 with RULES Subject (d) Air Transport Association (ATA) of America Code 32: Landing Gear. Reason (e) The mandatory continuing airworthiness information (MCAI) states: Several landing gear emergency extension valves have been found seized when performing checks according to the SAAB 340 Maintenance Review Board (MRB) Report, Section F (Airworthiness Limitation Section) task number 323106. The valves have seized due to lack of internal lubrication. This condition, if not corrected, could result in malfunctioning of the landing gear release during an operational emergency. Because the valve lubrication performance is dependant on calendar time since last valve operation, SAAB has revised the check to cycle the emergency release handle 5 times and amended the interval in MRB section F from 5,000 FH [flight hours] to every 2 years. For the reasons described above, this Airworthiness Directive (AD) requires a functional check [for discrepancies, (e.g., landing gear does not extend, does not lock in down position)] of the landing gear emergency extension valve at the newly established intervals. Malfunction of the landing gear release could cause failure of the landing gear to extend and lock in the extended position, which could result in a gear up landing and reduced controllability of the airplane on the ground. The corrective action for any discrepancy that is found is repair using a method approved by either the FAA or the European Aviation Safety Agency (EASA) (or its delegated agent). Actions and Compliance (f) Unless already done, do the following actions. VerDate Aug<31>2005 19:33 Dec 23, 2008 Jkt 217001 (1) Within 6 months after the effective date of this AD, do a functional check of the landing gear emergency extension valve in accordance with the Accomplishment Instructions of SAAB Service Bulletin 340– 32–136, dated January 9, 2008. Repeat the functional check thereafter at intervals not to exceed 24 months. (2) If any discrepancy is found during any functional check required by paragraph (f)(1) of this AD, before further flight, repair using a method approved by either the Manager, International Branch, ANM–116, Transport Airplane Directorate, FAA; or the EASA (or its delegated agent). FAA AD Differences Note 1: This AD differs from the MCAI and/or service information as follows: Although the MCAI includes a note that allows the option of the repetitive inspections (functional checks) to be accomplished in accordance with SAAB 340 Maintenance Review Board Report, Section F, Revision 6, Task Number 323106, this AD does not include that option. That document is not yet available. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM–116, 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: Shahram Daneshmandi, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057– 3356; telephone (425) 227–1112; 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 (h) Refer to MCAI EASA Airworthiness Directive 2008–0054, dated March 5, 2008; and SAAB Service Bulletin 340–32–136, dated January 9, 2008; for related information. Material Incorporated by Reference (i) You must use SAAB Service Bulletin 340–32–136, dated January 9, 2008, to do the PO 00000 Frm 00042 Fmt 4700 Sfmt 4700 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 Saab Aircraft AB, SAAB Aerosystems, SE–581 88, Linkping, Sweden; telephone +46 13 18 5591; fax +46 13 18 4874; e-mail saab2000.techsupport@saabgroup.com; Internet http://www.saabgroup.com. (3) You may review copies of the service information that is incorporated by reference at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425–227–1221 or 425–227–1152. (4) You may also review copies of the service information 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/ code_of_federal_regulations/ ibr_locations.html. Issued in Renton, Washington, on December 12, 2008. Michael J. Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8–30262 Filed 12–23–08; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 198 Aviation Insurance CFR Correction In title 14 of the Code of Federal Regulations, parts 140 to 199, revised as of January 1, 2008, on page 316, in § 198.3, in paragraph (a), revise the reference ‘‘§ 198.19’’ to read ‘‘§ 198.1’’. [FR Doc. E8–30838 Filed 12–23–08; 8:45 am] BILLING CODE 1505–01–D DEPARTMENT OF HEALTH AND HUMAN SERVICES Food and Drug Administration 21 CFR Part 573 Food Additives Permitted in Feed and Drinking Water of Animals CFR Correction In title 21 of the Code of Federal Regulations, parts 500 to 599, revised as of April 1, 2008, on pages 551 and 552, in § 573.640, in paragraphs (b)(4)(i) and (b)(4)(ii), before the words ‘‘at the National Archives and Records E:\FR\FM\24DER1.SGM 24DER1

Agencies

[Federal Register Volume 73, Number 248 (Wednesday, December 24, 2008)]
[Rules and Regulations]
[Page 78958]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-30838]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 198


Aviation Insurance

CFR Correction

    In title 14 of the Code of Federal Regulations, parts 140 to 199, 
revised as of January 1, 2008, on page 316, in Sec.  198.3, in 
paragraph (a), revise the reference ``Sec.  198.19'' to read ``Sec.  
198.1''.

[FR Doc. E8-30838 Filed 12-23-08; 8:45 am]
BILLING CODE 1505-01-D