AD 73-05-01

Active

Connecting Rod Bearing Assemblies

Key Information
73-05-01
Active
July 09, 1974
Not specified
Unknown
39-1889
Applicability
["Engine"]
Not specified
Lycoming Engines
IVO-540-A1A TIVO-540-A2A TVO-540-A1A 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 VO-540-C2B VO-540-C2C
Regulatory Text

73-05-01 AVCO LYCOMING: Amendment 39-1595 as amended by Amendment 39-1843 is further amended by Amendment 39-1889. Applies to VO-540 Series engines beginning with S/N 101-43 thru 2299-43, IVO-540 series engines beginning with S/N 101-60 thru 150-60, TVO-540 Series engines beginning with S/N 101-53 thru 103-53 and TIVO-540 Series engines beginning with S/N 101-57 thru 163-57 and all similar series engines overhauled (also known as remanufactured) by Lycoming before January 2, 1974 except the following Serial Numbers: RL-376-43, RL-483-43, RL-693-43, RL-695-43, RL-1091-43, RL-1205-43, RL-1429-43, RL- 1753-43, RL-1960-43, RL-2017-43, RL-2032-43, RL-2125-43, RL-2139-43, RL-2244-43, RL-2245-43 and RL-2275-43.

Compliance required as indicated after the effective date of this AD, unless already accomplished or unless higher crush bearing P/N LW13212 has been installed in accordance with Lycoming Service Bulletins No. 303E or 303F.

To prevent failures of P/N 71947, P/N 73174, P/N75548 and P/N LW10776 connecting rod assemblies and P/N 77450 connecting rod assembly with P/N 75547 connecting rod bearing installed in accordance with Lycoming Service Bulletins No. 303B, 303C or 303D, accomplish the following:

a. Engines with connecting rod assemblies that have accumulated 400 hours or more in service since new or overhaul must have the connecting rod assemblies replaced with new connecting rod assembly, P/N LW13422 and new connecting rod bearing P/N LW13212, within the next 50 hours in service.

b. Engines that have connecting rod assemblies with less than 400 hours in service must have the connecting rod assemblies replaced with new connecting rod assembly, P/N LW13422 and new connecting rod bearing, P/N LW13212 prior to 450 hours in service.

c. Engines that have been modified in accordance with Lycoming Service Bulletins No. 303B, 303C or 303D must comply with items (a) or (b) above, except that the P/N 77450 connecting rod, free of any galling maybe reused with P/N LW12596 connecting rod bolts and identified as assembly number LW13422.

NOTE: Lycoming Service Bulletin No. 371A applies to this subject.

Amendment 39-1595 superseded AD 65-13-07 and became effective February 28, 1973.

Amendment 39-1843 was effective May 17, 1974.

This Amendment 39-1889 is effective July 9, 1974.

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References
This information is not available.
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FAA Documents