Supersedes Service Instruction No. 1489B March 9, 2011 MODELS AFFECTED IO-360-L2A model engines installed in Cessna 172R and 172S aircraft; IO- 540-AB1A5 model engines installed in Cessna 182 aircraft; IO-540-AC1A5 model engines installed in Cessna 206 aircraft; TIO-540-AJ1A model engines installed in Cessna T206 aircraft with a 2 psi fuel flow divider spring (with detail P/N 2576532-1 or 2576556...

Supersedes Service Instruction No. 1420 February 25, 2011 MODELS AFFECTED All Lycoming reciprocating aircraft engines with AN type gear driven fuel pump TIME OF COMPLIANCE Any time the pump is installed. To decrease wear on the fuel pump drive spline, it is recommended that Castrol Contractor Special NLGI #1 or greases shown in the latest revision of Service Instruction No. 1059 be applied to the...

Supersedes Service Instruction No. 1508B February 10, 2011 MODELS AFFECTED All Lycoming engines with dual magnetos TIME OF COMPLIANCE At the next oil change, not to exceed 50 hours of engine operation or at each magneto timing check or service This Service Instruction identifies the necessary steps to install new clamps on dual magnetos to securely attach a Teledyne/Bendix or other dual magneto to...

DATE: February 4, 2011 MODELS AFFECTED All Lycoming aircraft engines. TIME OF COMPLIANCE Immediately after flight or ground operation in particulate-laden atmospheres. This service instruction gives guidelines for operation, inspection, and service of Lycoming engines which have been operated in atmospheres that have particulate matter such as dust, sand, debris, and volcanic ash.

DATE: February 4, 2011 MODELS AFFECTED AEIO-540-D4B5 Model Engine Installed in H.A.L. HPT-32 Aircraft. TIME OF COMPLIANCE At owner’s discretion. This Service Instruction identifies a new 4 psi flow divider spring Precision P/N 2577011 that is available as a replacement for the 2 psi flow divider spring for improved idle characteristics, especially in hot weather, for Lycoming engine model AEIO-540...

DATE: January 27, 2011 MODELS AFFECTED All Lycoming aircraft engines using automotive fuel. TIME OF COMPLIANCE Before engine storage for a duration of 6-months or longer. The Service Instruction only applies to Lycoming engines that have been operated on automotive fuel (as specified in the latest revision of Service Instruction No. 1070) and are to be stored for 6 or more consecutive months.

Supersedes Service Instruction No. 1427B December 29, 2010 MODELS AFFECTED All fixed wing and rotary wing aircraft (horizontal installations only) with Lycoming reciprocating aircraft engines installed TIME OF COMPLIANCE After field overhaul This Service Instruction identifies the necessary steps for engine break­in, including engine preparation for ground operational tests, flight tests, after...

Supersedes Service Instruction No. 1483 December 21, 2010 MODELS AFFECTED All Lycoming reciprocating aircraft engines TIME OF COMPLIANCE In the field, anytime the intake or exhaust valves are removed from a cylinder that has been removed from the engine, the following valve leak check procedure must be done after the valves (new, repaired, or re-used) are assembled with the valve springs and the...

Supersedes Service Instruction No. 1436 September 29, 2010 MODELS AFFECTED O­360­A3A Engine TIME OF COMPLIANCE At Owner’s discretion In some instances it has been found that operators of the O­360­A3A engine, with certain propellers, have experienced vibration in the right magneto. As a product improvement, a modification kit, P/N LW­15436, is available to the field. Installation of this kit...