- Effective
- July 9, 1974
- Models
- IVO-540-A1A, TIVO-540-A2A, TVO-540-A1A, VO-540-A1A, VO-540-A2A, VO-540-B1A and 18 more
- Registered aircraft
- 119 matched by model
- Product
- Engine
- Amendment
- 39-1889
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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On this page
The airworthiness directive
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.
Affected TCDS · 3
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 119
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1954 | 1 |
|---|---|
| 1958 | 1 |
| 1959 | 5 |
| 1960 | 6 |
| 1961 | 9 |
| 1962 | 4 |
| 1963 | 4 |
| 1964 | 11 |
| 1965 | 11 |
| 1966 | 4 |
| 1967 | 3 |
| 1968 | 1 |
| 1969 | 2 |
| 1970 | 3 |
| 1971 | 3 |
| 1975 | 1 |
| 1976 | 4 |
| 1977 | 4 |
| 1978 | 1 |
| 1979 | 2 |
| 1980 | 4 |
| 1981 | 1 |
| 1982 | 2 |
| 1984 | 1 |
| 1988 | 1 |
| 1993 | 2 |
| 1996 | 1 |
| 2000 | 2 |
25 with no year recorded