2011-15-10: Fuel servos

Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 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): 2011-15-10 Superior Air Parts and Lycoming Engines (formerly Textron Lycoming): Amendment 39-16757; Docket No. FAA-2011-0547; Directorate Identifier 2011-NE-13-AD. (a) Effective Date This AD is effective August 16, 2011. (b) Affected ADs None. (c) Applicability This AD applies to the Superior Air Parts engine models and Lycoming engine models listed in Table 1 of this AD with an AVStar Fuel Systems (AFS) fuel servo diaphragm, part numbers (P/Ns) AV2541801 and AV2541803, installed. Table 1--Affected Lycoming and Superior Air Parts Engines ------------------------------------------------------------------------ Engine manufacturer Engine model ------------------------------------------------------------------------ Lycoming Engines..................... AEIO-320-D1B, -D2B, -E1A, -E1B, - E2A, -E2B. AIO-320-A1A, -A1B, -A2A, -A2B, - B1B, -C1B. IO-320-A1A, -A2A, -B1A, -B1B, - B1C, -B1E, -B1D, -B2A, -C1A, - C1B, -D1A, -D1C, -D1B, -E1A, - E1B, -E2A, -E2B, -F1A. LIO-320-B1A, -C1A. AEIO-360-A1A, -A1B, -A1B6, -A1E6, -A1C, -A1D, -A1E, -A2A, -A2B, - A2C, -B1B, -B1D, -B1F, -B1F6, - B1G6, -B2F, -B2F6, -B1H, -B4A, - H1A, -H1B. AIO-360-A1A, -A1B, -A2A, -A2B, - B1B. HIO-360-A1A, -A1B, -B1A, -B1B, - C1A, -C1B, -E1AD, -E1BD, -F1AD, G1A. IO-360-A1A, -A1B, -A1B6, -A1B6D, A1C, -A1D, -A1D6, -A1D6D, -A2A, A2B, -A2C, -A3B6, -A3B6D, - A3D6D, -B1A, -B1B, -B1C, -B1D, - B1E, -B1F, -B1F6, -B1G6, -B2E, - B2F, -B2F6, -B4A, -C1A, -C1B, -C1C, -C1C6, -C1D6, -C1E6, - C1E6D, -C1F,-C1G6, -D1A, -E1A, - F1A, -J1AD, -J1A6D, -K2A, -L2A, M1A, -M1B. LIO-360-C1E6, -M1A. TIO-360-A1A, -A1B, -A3B6, -C1A6D. [[Page 45657]] IO-540-A1A5, -B1A5, -B1B5, -B1C5, -C1B5, -C1C5, -C2C, -C4B5, - C4B5D, -C4D5, -C4C5, -C4D5D, - D4A5, -D4B5, -D4C5, -E1A5, - E1B5, -E1C5, -G1A5, -G1B5, - G1C5, -G1D5, -G1E5, -G1F5, - J4A5, -K1A5, -K1A5D, -K1B5, - K1B5D, -K1C5, -K1D5, -K1E5, - K1E5D, -K1F5, -K1F5D, -K1G5, - K1G5D, -K1H5, -K1J5, -K1J5D, - K1K5, -K2A5, -L1A5, -L1A5D, - L1B5D, -L1C5, -M1A5, -M1A5D, - M1B5D, -M1C5, -M2A5D, -N1A5, - P1A5, -R1A5, -S1A5, -T4A5D, - T4B5, -T4B5D, -T4C5D, -U1A5D, - U1B5D, -V4A5D, -V4A5, -W1A5, - W1A5D, -W3A5D, -AA1A5, -AA1B5, - AB1A5, -AC1A5, -AE1A5, -AF1A5. IGO-480-A1A6, -A1B6. AEIO-540-D4A5, -D4B5, -D4C5, - D4D5, -L1B5D, -L1B5, -L1D5. IVO-540-A1A. TIO-540-A1A, -A1B, -A2A, -A2B, - A1C, -A2C, -C1A, -E1A, -F2BD, - G1A, -H1A,-J2B, -J2BD, -K1AD, - N2BD, -R2AD, -S1AD, -T2AD, -U2A, -V2AD, -W2A, -AA1AD, -AB1AD, - AB1BD, -AE2A, -AF1A, -AF1B, - AG1A, -AH1A, -AJ1A, -AK1A. LTIO-540-F2BD, -J2B, -J2BD, - K1AD, -N2BD, -R2AD, -U2A, -V2AD, -W2A. IO-720-A1A, -A1B, -A1BD, -B1A, - B1B, -B1BD, -C1B, -C1BD, -D1B, - D1BD, -D1C, -D1CD. TIGO-541-B1A, -C1A, -D1A, -D1B, - E1A, -G1AD. Superior Air Parts................... IO-360-A1A1, A1A2, A2A1, A2A2, A3A1, A3A2, B1A1, B1A2, B2A1, B2A2, B3A1, B3A2, B4A1, B4A2, B5A1, B5A2, B6A1, B6A2, C1A1, C1A2, C2A1, C2A2, C2A1, C3A2, D1A1, D1A2, D2A1, D2A2, D3A1, D3A2, D4A1, D4A2, D5A1, D5A2, D6A1, D6A2, E1A1, E1A2, E2A1, E2A2, E3A1, E3A2. ------------------------------------------------------------------------ (d) Unsafe Condition This AD was prompted by an accident involving a Piper PA32R-301. We are issuing this AD to correct the unsafe condition on these products. (e) Compliance Comply with this AD within the compliance times specified, unless already done. (f) Remove Fuel Servo If an AFS fuel servo diaphragm P/N AV2541801 or AV2541803 was installed in your fuel servo at any time after May 20, 2010, do the following as specified AVStar Fuel Systems (AFS) Mandatory Service Bulletin (MSB) AFS-SB6, Revision 2, dated April 6, 2011: (1) Before further flight remove the fuel servo. (2) After the effective date of this AD, don't install any affected fuel servo containing a discrepant AVStar fuel servo diaphragm, P/N AV2541801 or AV2541803, as listed in AFS MSB AFS-SB6, Revision 2, dated April 6, 2011. (g) Special Flight Permit We will not issue a special flight permit. (h) Alternative Methods of Compliance (AMOCs) The Manager, Atlanta Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. (i) Related Information For more information about this AD, contact Neil Duggan, Aerospace Engineer, Atlanta Certification Office, FAA, 1701 Columbia Avenue, College Park, GA 30337; phone: (404) 474-5576; fax: (404) 474-5606; e-mail: neil.duggan@faa.gov. (j) Material Incorporated by Reference (1) You must use AVStar Fuel Systems Mandatory Service Bulletin AFS-SB6, Revision 2, dated April 6, 2011, to do the actions required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference (IBR) under 5 U.S.C. 552(a) and 1 CFR part 51 of the following service information on the date specified: (2) The Director of the Federal Register approved the incorporation by reference of AVStar Fuel Systems Mandatory Service Bulletin AFS-SB6, Revision 2, dated April 6, 2011, on September 6, 2011 under 5 U.S.C. 552(a) and 1 CFR part 51. (3) For service information identified in this AD, contact AVStar Fuel Systems, Inc., 1365 Park Lane South, Jupiter, FL 33458; 561-575-1560; Web site: http://www.avstardirect.com. (4) You may review copies of the service information at the FAA, 12 New England Executive Park, Burlington, MA 01803. For information on the availability of this material at the FAA, call 781-238-7125. (5) You may also review copies of the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at an NARA facility, call 202-741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.