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2006-06-16: Crankshaft

FAA order 2006-06-16 is an airworthiness directive in force since April 27, 2006. The FAA's subject line: Crankshaft. It names the Lycoming AEIO-360-A1B6, Lycoming AEIO-360-A1E6, Lycoming IO-360-A1B6, Lycoming IO-360-A1B6D, Lycoming IO-360-A3B6, Lycoming IO-360-A3B6D, Lycoming IO-360-B1G6, Lycoming IO-360-C1C6, Lycoming IO-360-C1D6, Lycoming IO-360-C1E6, Lycoming IO-360-C1G6, Lycoming LIO-360-C1E6, Lycoming LO-360-A1G6D, Lycoming LO-360-A1H6, Lycoming O-360-A1F6, Lycoming O-360-A1F6D, Lycoming O-360-A1G6D, Lycoming O-360-A1H6, Lycoming O-360-E1A6D, Lycoming O-360-F1A6 engines: about 1,570 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Engine
Makes
Lycoming Engines
Models
AEIO-360-A1B6, AEIO-360-A1E6, IO-360-A1B6, IO-360-A1B6D, IO-360-A3B6, IO-360-A3B6D, IO-360-B1G6, IO-360-C1C6, IO-360-C1D6, IO-360-C1E6, IO-360-C1G6, LIO-360-C1E6, LO-360-A1G6D, LO-360-A1H6, LO-360-E1A6D, O-360-A1F6, O-360-A1F6D, O-360-A1G6D, O-360-A1H6, O-360-E1A6D, O-360-F1A6
Engine series
Lycoming AEIO-360-A1B6 11 aircraft
Lycoming AEIO-360-A1E6 2 aircraft
Lycoming IO-360-A1B6 141 aircraft
Lycoming IO-360-A1B6D 844 aircraft
Lycoming IO-360-A3B6 5 aircraft
Lycoming IO-360-A3B6D 74 aircraft
Lycoming IO-360-B1G6 173 aircraft
Lycoming IO-360-C1C6 64 aircraft
Lycoming IO-360-C1D6 14 aircraft
Lycoming IO-360-C1E6 43 aircraft
Lycoming IO-360-C1G6 3 aircraft
Lycoming LIO-360-C1E6 6 aircraft
Lycoming LO-360-A1G6D 3 aircraft
Lycoming LO-360-A1H6 9 aircraft
Lycoming O-360-A1F6 13 aircraft
Lycoming O-360-A1F6D 18 aircraft
Lycoming O-360-A1G6D 11 aircraft
Lycoming O-360-A1H6 106 aircraft
Lycoming O-360-E1A6D 7 aircraft
Lycoming O-360-F1A6 23 aircraft

Dates and paperwork

In force since
April 27, 2006
Published
March 23, 2006 (signed March 15, 2006)
Docket
FAA-2005-23269
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain Lycoming Engines (formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and LO-360 series reciprocating engines. This AD requires replacing certain crankshafts. This AD results from a crankshaft failure in a Lycoming LO-360-A1H6 reciprocating engine. We are issuing this AD to prevent failure of the crankshaft, which could result in total engine power loss, in-flight engine failure, and possible loss of the aircraft.

The order itself the regulatory text, as published

Show the full text (5,037 characters)
2006-06-16 Lycoming Engines (Formerly Textron Lycoming): Amendment 39-14525. Docket No. FAA-2005-23269; Directorate Identifier 2005-NE- 50-AD. Effective Date (a) This airworthiness directive (AD) becomes effective April 27, 2006. Affected ADs (b) None. Applicability (c) This AD applies to Lycoming Engines AEIO-360, IO-360, O-360, LIO-360, and LO-360 series reciprocating engines, manufactured new or rebuilt, overhauled, or that had a crankshaft installed after March 1, 1999. These engines are installed on, but not limited to, the following aircraft: Engine model Manufacturer Aircraft model AEIO 360 A1B6 Moravan Scottish Avia Valmet Z242L Zlin Bulldog L 70 Vinka AEIO 360 A1E6 Integrated Systems Omega IO 360 A1B6 Aircraft Manufacturing Factory Beech Cessna Korean Air Lake Mooney Partenavia Saab Scottish Avia Socata Mushshak C 24R Sierra or 200 Sierra R G Cardinal Chang Gong 91 LA 4 200 Buccaneer M 20 J P 68 Series Observer MFI 15 Safari or MFI 17 Supporter Bulldog TB 200 IO 360 A1B6D Cessna Mooney Siai Marchetti R G Cardinal M 201 S 205 IO 360 A3B6 Mooney Mod Works M 201 Trophy 212 Conversion IO 360 A3B6D Mooney M20J 201 IO 360 C1C6 Piper Ruschmeyer PA 28R 201 Arrow MF 85 IO 360 B1G6 American Blimp IO 360 C1G6 Zeppelin Blimp IO 360 C1E6 Piper PA 34 200 Seneca I LO 360 A1G6D Beech 76 Duchess LO 360 A1H6 Piper PA 44 180 Seminole O 360 A1F6 Cessna 177 Cardinal O 360 A1F6D Cessna 177 Cardinal O 360 A1G6D Beech 76 Duchess O 360 A1H6 Piper PA 44 180 O 360 E1A6D Piper PA 44 180 O 360 F1A6 Cessna C 172RG Cutlass RG IO 360 C1D6 Sold as a spare engine. LIO 360 C1E6 Sold as a spare engine. LO 360 E1A6d Sold as a spare engine. LIO 360 C1D6 Sold as a spare engine. Unsafe Condition (d) This AD results from a crankshaft failure in a Lycoming LO- 360-A1H6 reciprocating engine. We are issuing this AD to prevent failure of the crankshaft, which could result in total engine power loss, in-flight engine failure, and possible loss of the aircraft. Compliance (e) You are responsible for having the actions required by this AD performed within 50 hours time-in-service or 6 months after the effective date of this AD, whichever is earlier, unless the actions have already been done. (f) If Lycoming Engines manufactured new, rebuilt, overhauled, or replaced the crankshaft in your engine before March 1, 1999, and you haven't had the crankshaft replaced, no further action is required. (g) If Table 1 of Supplement No. 1 to Lycoming Mandatory Service Bulletin (MSB) No. 566, dated November 30, 2005, lists your engine serial number (SN), use Table 2 of Supplement No. 1 to verify if your crankshaft SN is listed. (h) If Table 1 of Supplement No. 1 to Lycoming MSB No. 566, dated November 30, 2005, does not list your engine SN, use Table 2 of Supplement No. 1 to verify if your crankshaft SN is listed, if an affected crankshaft was installed as a replacement. (i) If Table 2 of Supplement No. 1 to Lycoming Engines MSB No. 566, dated November 30, 2005, lists your crankshaft SN, replace the crankshaft with a crankshaft that is not listed in Table 2 of Supplement No. 1 to Lycoming MSB No. 566, dated July 11, 2005. (j) The engine and crankshaft SNs listed in Table 1 and Table 2 of Supplement No.1 to Lycoming Engines MSB No. 566 are different from the engine and crankshaft SNs affected by Lycoming MSBs No. 552, No. 553 and No. 566; and ADs 2002-19-03 and 2005-19-11. Prohibition Against Installing Certain Crankshafts (k) After the effective date of this AD, do not install any crankshaft that has a SN listed in Table 2 of Supplement No. 1 to Lycoming MSB No. 566, dated November 30, 2005, into any engine. Alternative Methods of Compliance (l) The Manager, New York Aircraft Certification Office, has the authority to approve alternative methods of compliance for this AD if requested using the procedures found in 14 CFR 39.19. Related Information (m) None. Material Incorporated by Reference (n) You must use Lycoming Engines Supplement No. 1 to Mandatory Service Bulletin No. 566, dated November 30, 2005, to perform the crankshaft replacements required by this AD. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Lycoming, 652 Oliver Street, Williamsport, PA 17701; telephone (570) 323-6181; fax (570) 327-7101, or go on the Internet at http://www.Lycoming.Textron.com for a copy of this service information. You may review copies at the Docket Management Facility; U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC 20590-0001, on the Internet at http://dms.dot.gov, or at the National Archives andRecords 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 .

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2006-06-16.json · aircraft systems.