SERVICE BULLETIN MANDATORY
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1 652 Oliver Street Williamsport, PA U.S.A. Tel Fax MANDATORY SERVICE BULLETIN DATE: July 20, 2007 Service Bulletin No. 574A (Supersedes Service Bulletin No. 574) Engineering Aspects are FAA Approved SUBJECT: MODELS AFFECTED: Cylinder Stud Hole Cross-Threaded Any Lycoming engine model listed in Table 1 that was manufactured, rebuilt, or overhauled between September 7, 2006 and October 18, Any cylinder kit listed in Table 2 that was received between September 7, 2006 and October 18, TIME OF COMPLIANCE: At the next maintenance event or within 50 hours of engine operation, whichever occurs first. Certain cylinders either installed in an engine or received in a cylinder kit listed in Tables 1 and 2 between September 7, 2006 and October 18, 2006 may have a cross-threaded cylinder stud hole. This stud holds the shroud tube retaining components. If the stud is loose due to the cross-threading, the shroud tubes will also become loose and subsequent damage to the engine may occur due to the loss of engine oil. INSTRUCTIONS FOR COMPLIANCE: 1. Review Tables 1 and 2 for applicability. If the engine model and serial number, or cylinder kit number, is not shown in either Table 1 or Table 2, then no additional action is required. 2. If either the engine model and serial number or cylinder kit number is listed in Table 1 or 2 then each individual cylinder must be inspected for visible damage, the manufacturing lot code and the Lycoming part number. 3. The manufacturing lot code and Lycoming part number can be found on the bottom of the cylinder near the cylinder valve cover, as viewed mounted on the engine. See Figures 1 and 3. If the engine is mounted in an aircraft, depending on the model, removal of the baffling and other associated parts may be necessary. a. Note: The cylinders shown in Figures 1, 2, and 3 are from different cylinders and are for illustrative purposes only. 4. The format of the manufacturing lot code is six digits, starting with the number zero (ex ). The format of the Lycoming part number may be either a. The letters LW followed by a dash, then by five digits. b. The digits 16 followed by the letter A, then by five digits. 5. If the manufacturing lot code and Lycoming part number is not listed in Table 3 then proceed with Step by Lycoming All Rights Reserved Page 1 of 6
2 6. If the manufacturing lot code and Lycoming part number is listed in Table 3 then proceed with Step Figure 1 illustrates the rocker flange area of the cylinder. Where the cylinder stud hole is located, inspect the cylinder exterior surface and threaded stud hole area. A flashlight and a small mirror may be needed to conduct the inspection. Also, depending on the aircraft model, removal of the valve covers should not be necessary but removal of the baffling and other associated parts may be necessary. a. If there is visible damage such as shown in Figure 2, contact Lycoming Customer Service at for further instructions regarding warranty replacement. Visible damage is defined as a cross-thread, stripped thread, cracked boss, or other similar damage that would not allow the cylinder stud to seat squarely and securely in the hole. b. If there is no visible damage then proceed with Step Either stamp, or use an electric vibrator to permanently etch the letter T on the exterior surface of the cylinder stud boss to indicate compliance with this Service Bulletin. Locate the letter T in the cross-hatched area as shown in Figure 2 so that it is both near the stud hole and is easily accessible. Make an appropriate logbook entry of compliance. Page 2 of 6 Figure 1. Interior View of the Cylinder. Inspect the exterior surface and threaded hole area.
3 Figure 2. Cross-Threaded Stud Hole as Viewed on the Side Opposite of the Cylinder Stud Called Out in Figure 1. Figure 3 Page 3 of 6
4 TABLE 1 Engine Model Engine S/N Engine Model Engine S/N Engine Model Engine S/N O-320-H2AD L T IO-360-L2A L E IO-360-L2A L E O-320-H2AD L T IO-360-L2A L E IO-360-L2A L E O-320-H2AD L T IO-360-L2A L E IO-360-L2A L E O-320-H2AD L T IO-360-L2A L E IO-360-L2A L E O-320-H2AD L T IO-360-L2A L E IO-360-L2A L E O-320-H2AD RL T IO-360-L2A L E IO-360-L2A L E AEIO-360-B2F RL A IO-360-L2A L E IO-360-L2A L E AEIO-360-B2F RL A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A L A IO-360-L2A L E IO-360-L2A L E HIO-360-G1A RL A IO-360-L2A L E IO-360-L2A L E HO-360-C1A L A IO-360-L2A L E IO-360-L2A L E HO-360-C1A L A IO-360-L2A L E IO-360-L2A L E IO-360-L2A L A IO-360-L2A L E IO-360-L2A L E IO-360-L2A L E IO-360-L2A L E IO-360-L2A L E IO-360-L2A L E IO-360-L2A L E IO-360-L2A L E IO-360-L2A L E IO-360-L2A L E IO-360-L2A RL E IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-L2A L E IO-360-M1A L A IO-360-L2A L E IO-360-M1A L A Page 4 of 6
5 TABLE 1 (CONT.) Engine Model Engine S/N Engine Model Engine S/N Engine Model Engine S/N IO-360-M1A L A O-360-A3A L A O-540-E4C5 L E IO-360-M1A L A O-360-A4A RL E O-540-E4C5 RL E IO-360-M1A L A O-360-A4M L E TIO-540-AK1A L A IO-360-M1A L A O-360-A4M L E TIO-540-AK1A L A IO-360-M1A L A O-360-A4M L E TIO-540-AK1A L A IO-360-M1A L A O-360-A4M L E TIO-540-AK1A L A IO-360-M1A L A O-360-A4M L E TIO-540-AK1A L A IO-360-M1A L A O-360-A4M L E TIO-540-AK1A L A IO-360-M1A L A O-360-A4M L E TIO-540-AK1A L A IO-360-M1B L E O-360-A4M L E TIO-540-AK1A L A IO-360-M1B L E O-360-A4M L E TIO-540-AK1A L A LO-360-A1G6D L E O-360-A4M L E TIO-540-AK1A L A LO-360-A1H6 L E O-360-A4M L E TIO-540-AK1A L A LO-360-A1H6 L E O-360-A4M L E TIO-540-AK1A L A LO-360-A1H6 L E O-360-A4M L E TIO-540-AK1A L A LO-360-A1H6 L E O-360-A4M L E TIO-540-AK1A L A LO-360-A1H6 L E O-360-A4M L E TIO-540-AK1A L A LO-360-A1H6 L E O-360-A4M L E TIO-540-AK1A L A LO-360-A1H6 L E O-360-C1F L A TIO-540-AK1A L A LO-360-A1H6 L E O-360-C1F L E TIO-540-AK1A L A LO-360-A1H6 RL E O-360-C1F L E TIO-540-AK1A L A O-360-A1A L E O-360-C1F L E TIO-540-AK1A L A O-360-A1A L A O-360-C1F L E TIO-540-AK1A L A O-360-A1D RL A O-360-C1F L E TIO-540-AK1A L A O-360-A1G6D L E O-360-C1F RL A TIO-540-AK1A L A O-360-A1G6D L E O-360-C1G L E TIO-540-AK1A L A O-360-A1G6D L E O-360-C4F L A TIO-540-AK1A L A O-360-A1H6 L E O-360-C4P RL A TIO-540-AK1A L A O-360-A1H6 L E O-360-F1A6 RL A TIO-540-AK1A L A O-360-A1H6 L E AEIO-540-D4A5 L A TIO-540-AK1A L A O-360-A1H6 L E AEIO-540-D4A5 RL E TIO-540-AK1A L A O-360-A1H6 L E AEIO-540-D4A5 RL A TIO-540-AK1A L A O-360-A1H6 L E IO-540-V4A5 L A TIO-540-AK1A L A O-360-A1H6 L E O-540-A1D5 RL A TIO-540-AK1A L A O-360-A1H6 L E O-540-E4A5 RL TIO-540-AK1A L A O-360-A1H6 RL A O-540-E4A5 RL A TIO-540-AK1A L A O-360-A1H6 RL A O-540-E4A5 RL A TIO-540-AK1A L A O-360-A1P L A O-540-E4B5 L A TIO-540-AK1A L A O-360-A1P L A O-540-E4B5 RL E TIO-540-AK1A L A O-360-A1P L A O-540-E4C5 L E TIO-540-AK1A L A O-540-E4C5 L A Page 5 of 6
6 TABLE 2 Kit No. 05K K K K21119 TABLE 3 Lycoming P/N Mfg. Lot Code LW LW LW LW LW A Page 6 of 6
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652 Oliver Street Williamsport, PA 17701 U.S.A. Tel. 570-323-6181 Fax. 570-327-7101 www.lycoming.textron.com MANDATORY SERVICE BULLETIN November 30, 2005 Supplement No. 1 To Service Bulletin No. 566 SUBJECT:
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