Service Instruction No. 1299 B
Supersedes Service Instruction No. 1299A
September 24, 2010
Supersedes Service Instruction No. 1299A
September 24, 2010
September 2010
TIO-LTIO-540 Parts Catalog
PC-315-5
LTIO-540-F2BD, LTIO-540-J2B, LTIO-540-J2BD, LTIO-540-N2BD, LTIO-540-R2AD
Supersedes Service Instruction No. 1065A and No. 1204C
August 26, 2010
All Lycoming Engines using either V-Shaped Spiral Wound or Beaded Exhaust Flange Gaskets.
At overhaul or whenever exhaust flange gaskets are replaced.
July 6, 2015
Lycoming Engine Models: IO-540-AC1A5, (L)TIO-540-V2AD, TIO-540- AJ1A, TIO-540-W2A, TO-360-C1A6D, TIO-360-C1A6D, TIO-541-E Series, TIGO-541-E1A, and IO-580-A1A Applies to:
August 2010
IVO-360-A1A Parts Catalog
PC-306-17
IVO-360-A1A
July 9, 2010
All Lycoming series engines.
Prior to flight and/or during engine operation.
Supersedes Service Instruction No. 1132A
June 18, 2010
All Lycoming Opposed Series Aircraft Engines with Magnetos.
During Pre-Flight Inspection
A basic magneto drop-off check based on engine speed is typically done during the pre-flight inspection to determine the loss of engine speed that occurs when magnetos are switched from BOTH magnetos to one (LEFT or RIGHT) magneto. The maximum drop-off limit is specified in most Lycoming publications as Revolutions Per Minute (RPM) from a stated engine speed.
DATE: June 11, 2010
All Lycoming new, overhauled, rebuilt, or repaired TIO-540-AE2A, IO-540- V4A5.
When upgrading to a Kelly Aerospace E-drive Starter.
June 2010
O, LO & TO-360 Parts Catalog
PC-306-2
O-360-B2A, O-360-C1A, O-360-C1C, O-360-C1E, O-360-C1F, O-360-C2A, O-360-C2C, O-360-C2E, O-360-D2A, O-360-F1A6
Supersedes Service Bulletin No. 591
May 10, 2010
All Lycoming engines equipped with a rebuilt Kelly Aerospace Energy Systems turbocharger manufactured between January 2007 and June 2009 as per the part effectivity in Table I and per the serial number effectivity in Table III found in the attached reprint.
Within 10 hours of engine operation or at the next maintenance event, whichever occurs first.