| AD Number | 2012-03-07 | Status | Active |
| Effective Date | March 27, 2012 | Issue Date | February 01, 2012 |
| Docket Number | FAA-2011-0533 | Amendment | 39-16948 |
| Product Type | ["Engine"] | Product Subtype | Not specified |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | Federal Register Volume 77, Number 34 (Tuesday, February 21, 2012) | ||
| Manufacturer(s) | Lycoming Engines Textron Lycoming, AVCO Corporation |
| Model(s) | GO-435 GO-435-C2 (O-435-17) GO-435-C2A GO-435-C2A2 GO-435-C2B GO-435-C2B1 GO-435-C2B2 GO-435-C2C GO-435-C2D GO-435-C2E GO-435-D1 GO-480 GO-480-A1A GO-480-B GO-480-B1 GO-480-B1A6 GO-480-B1B GO-480-B1C GO-480-B1D GO-480-C1B6 GO-480-C1D6 GO-480-C2C6 GO-480-C2D6 GO-480-C2E6 GO-480-C3A6 GO-480-D1A GO-480-E1A6 GO-480-F1A6 GO-480-F2A6 GO-480-F2D6 GO-480-F3A6 GO-480-F3B6 GO-480-F4A6 GO-480-F4B6 GO-480-F6 GO-480-G1A6 GO-480-G1B6 GO-480-G1D6 GO-480-G1H6 GO-480-G1J6 GO-480-G2D6 GO-480-G2F6 GSO-435-B GSO-435-B2 GSO-480-A1A6 GSO-480-A1C6 GSO-480-A2A6 GSO-480-B1A6 GSO-480-B1B3 GSO-480-B1B6 (O-480-1) GSO-480-B1C6 GSO-480-B1E6 GSO-480-B1F6 GSO-480-B1G6 GSO-480-B1J6 GSO-480-B2C6 GSO-480-B2D6 GSO-480-B2G6 GSO-480-B2H6 HO-360-A1A HO-360-B1A HO-360-B1B HO-360-C1A LO-360-A1G6D LO-360-A1H6 LO-360-E1A6D LO-360-E1AD LO-360-E1BD LO-360-E2AD LO-360-E2BD LTO-360-A1A6D LTO-360-E1A6D O-233-A1 O-235 O-235-A O-235-AP O-235-B O-235-BP O-235-C O-235-C1 O-235-C1A O-235-C1B O-235-C1C O-235-C2A O-235-C2B O-235-C2C O-235-E1 O-235-E1B O-235-E2A O-235-E2B O-235-F1 O-235-F1B O-235-F2A O-235-F2B O-235-G1 O-235-G1B O-235-G2A O-235-G2B O-235-H2C O-235-J2A O-235-J2B O-235-K2A O-235-K2B O-235-K2C O-235-L2A O-235-L2C O-235-M1 O-235-M2C O-235-M3C O-235-N2A O-235-N2C O-235-P1 O-235-P2A O-235-P2C O-235-P3C O-320-A1A O-320-A1B O-320-A2A O-320-A2B O-320-A2C O-320-A2D O-320-A3A O-320-A3B O-320-A3C O-320-B1A O-320-B1B O-320-B2A O-320-B2B O-320-B2C O-320-B2D O-320-B2E O-320-B3A O-320-B3B O-320-B3C O-320-C1A O-320-C1B O-320-C2A O-320-C2B O-320-C2C O-320-C3A O-320-C3B O-320-C3C O-320-D1A O-320-D1B O-320-D1C O-320-D1D O-320-D1F O-320-D2A O-320-D2B O-320-D2C O-320-D2F O-320-D2G O-320-D2H O-320-D2J O-320-D3G O-320-E1A O-320-E1B O-320-E1C O-320-E1F O-320-E1J O-320-E2A O-320-E2B O-320-E2C O-320-E2D O-320-E2F O-320-E2G O-320-E2H O-320-E3D O-320-E3H O-320-H1AD O-320-H1BD O-320-H2AD O-320-H2BD O-320-H3AD O-320-H3BD O-340-A1A O-340-A2A O-340-B1A O-360-A1A O-360-A1AD O-360-A1C O-360-A1D O-360-A1F O-360-A1F6 O-360-A1F6D O-360-A1G O-360-A1G6 O-360-A1G6D O-360-A1H O-360-A1H6 O-360-A1LD O-360-A1P O-360-A2A O-360-A2D O-360-A2E O-360-A2F O-360-A2G O-360-A2H O-360-A3A O-360-A3AD O-360-A3D O-360-A4A O-360-A4AD O-360-A4D O-360-A4G O-360-A4J O-360-A4K O-360-A4M O-360-A4N O-360-A4P O-360-A5AD O-360-B1A O-360-B1B O-360-B2A O-360-B2B O-360-B2C O-360-C1A O-360-C1C O-360-C1E O-360-C1F O-360-C1G O-360-C2A O-360-C2B O-360-C2C O-360-C2D O-360-C2E O-360-C4F O-360-C4P O-360-D1A O-360-D2A O-360-D2B O-360-E1A6D O-360-E1AD O-360-E1BD O-360-E2AD O-360-E2BD O-360-F1A6 O-360-G1A6 O-360-J2A O-435 O-435-25 O-435-A O-435-A2 O-435-B (O-435-5) O-435-C (O-435-1) O-435-C1 (O-435-11) O-435-C2 (O-435-13) O-435-K O-435-K1 (O-435-4) O-540-A1A O-540-A1A5 O-540-A1B5 O-540-A1C5 O-540-A1D O-540-A1D5 O-540-A2B O-540-A3D5 O-540-A4A5 O-540-A4B5 O-540-A4C5 O-540-A4D5 O-540-B1A5 O-540-B1B5 O-540-B1D5 O-540-B2A5 O-540-B2B5 O-540-B2C5 O-540-B4A5 O-540-B4B5 O-540-D1A5 O-540-E4A5 O-540-E4B5 O-540-E4C5 O-540-F1A5 O-540-F1B5 O-540-G1A5 O-540-G2A5 O-540-H1A5 O-540-H1A5D O-540-H1B5D O-540-H2A5 O-540-H2A5D O-540-H2B5D O-540-J1A5D O-540-J1B5D O-540-J1C5D O-540-J1D5D O-540-J2A5D O-540-J2B5D O-540-J2C5D O-540-J2D5D O-540-J3A5 O-540-J3A5D O-540-J3C5D O-540-L3C5D SO-580-A1A SO-580-A1B TO-360-A1A6D TO-360-C1A6D TO-360-E1A6D TO-360-F1A6D TVO-435-A1A TVO-435-B1A (O-435-25A) TVO-435-B1B TVO-435-C1A TVO-435-D1A TVO-435-D1B TVO-435-E1A TVO-435-F1A TVO-435-G1A TVO-435-G1B TVO-540-A1A VO-360-A1A VO-360-A1B VO-360-B1A VO-435-A1A (O-435-21) VO-435-A1B (O-435-6) VO-435-A1C (O-435-23, -23A, -23B, -23C) VO-435-A1D (O-435-6A) VO-435-A1E VO-435-A1F VO-435-B1A VO-540-A1A VO-540-A2A VO-540-B1A VO-540-B1B VO-540-B1B3 VO-540-B1C VO-540-B1D VO-540-B1E VO-540-B1F VO-540-B1H3 VO-540-B2A VO-540-B2C VO-540-B2D VO-540-B2E VO-540-B2G VO-540-C1A VO-540-C1B VO-540-C1C3 VO-540-C2A (O-540-9) VO-540-C2B VO-540-C2C VSO-580-A1A GO-145-C1 GO-145-C2 GO-145-C3 GSO-580 GSO-580-B GSO-580-C GSO-580-D Military O-435-2-M1 O-145-A1 O-145-A2 O-145-B1 O-145-B2 O-145-B3 O-145-C1 O-145-C2 O-290 O-290-A O-290-AP O-290-B O-290-C O-290-CP O-290-D O-290-D2 O-290-D2A O-290-D2B O-290-D2C O-350 O-350-A P220 R-530-D1 R-530-D2 R-680 R-680-2 R-680-4 R-680-5 R-680-6 R-680-B2 R-680-B4 Series R-680-B5 R-680-B6 R-680-BA R-680-D5 R-680-D6 R-680-E1 R-680-E2 R-680-E3 R-680-E3A R-680-E3B |
We are adopting a new airworthiness directive (AD) for certain Lycoming Engines reciprocating engines. This AD was prompted by a report of a "machined-from-billet'' HA-6 carburetor having a loose mixture control sleeve that rotated in the carburetor body causing restriction of fuel and power loss. This AD requires removing certain "machined-from-billet'' Volare LLC (formerly Precision Airmotive Corporation, formerly Facet Aerospace Products Company, formerly Marvel-Schebler (BorgWarner)) HA-6 carburetors, inspecting for a loose mixture control sleeve or for a sleeve that may become loose, repairing the carburetor, or replacing the carburetor with one eligible for installation. We are issuing this AD to prevent engine in-flight shutdown, power loss, and reduced control of the airplane.
Final rule.
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):
2012-03-07 Lycoming Engines (formerly Textron Lycoming Division, AVCO Corporation): Amendment 39-16948; Docket No. FAA-2011-0533; Directorate Identifier 2011-NE-16-AD.
(a) Effective Date
This AD is effective March 27, 2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Lycoming Engines reciprocating engines with carburetor part numbers listed in Table 1 of this AD.
Table 1--Part Numbers (Including All Dash Numbers) of Known Affected HA-
6 Model Carburetors ------------------------------------------------------------------------
------------------------------------------------------------------------
10-5219-XX 10-5224-XX 10-5230-XX 10-5235-XX 10-5253-XX
10-5255-XX 10-5283-XX 10-6001-XX 10-6019-XX 10-6030-XX ------------------------------------------------------------------------
(d) Unsafe Condition
This AD was prompted by a report of a "machined-from-billet'' HA-6 carburetor having a loose mixture control sleeve that rotated in the carburetor body causing restriction of fuel and power loss. We are issuing this AD to prevent engine in-flight shutdown, power loss, and reduced control of the airplane.
(e) Compliance
Comply with this AD within 50 flight hours after the effective date of this AD, unless already done.
(f) Inspection
Inspect the carburetor to determine the type of body the carburetor has. Use Marvel-Schebler Emergency Service Bulletin (SB) No. SB-18, dated October 14, 2010, or Revision A, dated March 15, 2011, Figure (3) to determine which type of body is used.
(g) If the carburetor has a die-cast body, no further action is required.
(h) If the carburetor has an affected "machined-from-billet'' body, remove the carburetor; and replace the carburetor with:
(1) An HA-6 carburetor not listed in Table 1 of this AD; or
(2) An HA-6 carburetor that is listed in Table 1 but is exempted as described in paragraphs 1.A. and 1.B of Marvel-Schebler Emergency SB No. SB-18, dated October 14, 2010 or Revision A, dated March 15, 2011; or that has already been repaired using that Emergency SB.
(i) Alternative Methods of Compliance (AMOCs)
The Manager, Atlanta Aircraft Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request.
(j) Related Information
For more information about this AD, contact Kevin Brane, Aerospace Engineer, Propulsion, Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate; 1701 Columbia Avenue, College Park, Georgia 30337; phone: (404) 474-5582; fax: (404) 474- 5606; email: kevin.brane@faa.gov.
(k) Material Incorporated by Reference
(1) You must use the following service information 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:
(i) Marvel-Schebler Emergency Service Bulletin No. SB-18, dated October 14, 2010.
(ii) Marvel-Schebler Emergency Service Bulletin No. SB-18, Revision A, dated March 15, 2011.
(2) For service information identified in this AD, contact Marvel-Schebler Aircraft Carburetors LLC, 125 Piedmont Avenue, Gibsonville, NC 27249; phone: 336-446-0002; fax: 336-446-0007; email: customerservice@msacarbs.com; Web site: www.msacarbs.com.
(3) You may review copies of the service information at the FAA, Engine & Propeller Directorate,12 New England Executive Park, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125.
(4) 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.
[[Page 9839]]
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 published in the Federal Register on September 1, 2011 (76 FR 54397). That NPRM proposed to require removing certain "machined-from- billet'' Volare LLC (formerly Precision Airmotive Corporation, formerly Facet Aerospace Products Company, formerly Marvel-Schebler (BorgWarner)) HA-6 carburetors, inspecting for a loose mixture control sleeve or for a sleeve that may become loose, repairing the carburetor, or replacing the carburetor with one eligible for installation.
Comments
We gave the public the opportunity to participate in developing this AD. The following presents the comment received on the proposal and the FAA's response.
Request To Incorporate All Affected Engine Models
One commenter, a private citizen, requested that we incorporate all affected engine models with HA-6model carburetors installed in the AD. The commenter provided a list, which he compiled from reviewing all applicable published Type Certificate Data Sheets (TCDS).
We partially agree. We agree that some additional models are affected because the list provided by the commenter is mostly consistent with the applicable TCDS. We do not agree with the commenter on some of the models he thinks are affected, because we could not confirm they are affected, based on the TCDS. However, we determined that we need to change the applicability from a table of specific engine models, to all Lycoming Engines reciprocating engines with carburetor part numbers listed in Table 1 of the AD. We changed the AD applicability to all Lycoming Engines reciprocating engines with carburetor part numbers listed in Table 1 of the AD.
Change to the Alternative Methods of Compliance (AMOC) Paragraph
Since we issued the proposed AD, we found that we referenced the wrong office in the AMOC paragraph. Wechanged that sentence to state that the Manager, Atlanta Aircraft Certification Office, FAA, may approve AMOCs for this AD.
Change to Service Information
Marvel-Schebler Aircraft Carburetors LLC has revised their Marvel- Schebler Emergency Service Bulletin (SB) No. SB-18, dated October 14, 2010, to Revision A, dated March 15, 2011. We reviewed Revision A, and determined that it also is acceptable. We changed the incorporated by reference paragraph k of the AD to include the original issue and Revision A.
Conclusion
We reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting the AD with the changes described previously. We also determined that these changes will not increase the economic burden on any operator or increase the scope of the AD.
[[Page 9838]]
Costs of Compliance
We estimate that this AD affects 10,700 engines installed on aircraft of U.S. registry. We also estimate that it will take about 0.5 work-hours per aircraft to perform the inspection, and that about 409 carburetors will need repair. Approximately 2 work-hours per carburetor are required to repair the carburetor. The average labor rate is $85 per work-hour. Required parts will cost about $600 per carburetor. Based on these figures, we estimate the cost of the AD on U.S. operators to be $769,680. Our estimate is exclusive of possible warranty coverage.
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 aircraftin 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
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 that 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),
(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.
For service information identified in this AD, contact Marvel-Schebler Aircraft Carburetors LLC, 125 Piedmont Avenue, Gibsonville NC 27249; phone: 336-446-0002; fax: 336-446-0007; email: customerservice@msacarbs.com; Web site: www.msacarbs.com. You may review copies of the referenced service information at the FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.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 this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 800-647-5527) is 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.
Kevin Brane, Aerospace Engineer, Propulsion, Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate; 1701 Columbia Avenue, College Park, Georgia 30337; phone: 404-474-5582; fax: 404-474-5606; email: kevin.brane@faa.gov.