AD 73-05-01

Airworthiness directive · Connecting Rod Bearing Assemblies · Lycoming Engines IVO-540-A1A, TIVO-540-A2A, TVO-540-A1A and 21 more

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.

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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.

By aircraft maker
  • Hiller62 aircraft
  • Bell44 aircraft
  • Piper6 aircraft
  • Brantly2 aircraft
  • Texas Helicopter2 aircraft
  • Other makers33 aircraft
By year built
19542000
Registered aircraft by year built: 94 aircraft
19541
19581
19595
19606
19619
19624
19634
196411
196511
19664
19673
19681
19692
19703
19713
19751
19764
19774
19781
19792
19804
19811
19822
19841
19881
19932
19961
20002

25 with no year recorded

By model

Aircraft

See all 119 aircraft