AD 73-15-04

Airworthiness directive · Rubber Drive Plate Grommet · Lycoming Engines HIO-360-D1A

Effective
July 23, 1973
Model
HIO-360-D1A
Data sheet
TCDS1E10
Registered aircraft
431 matched by model
Product
Engine
Amendment
39-1689

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

73-15-04 AVCO LYCOMING: Amdt. 39-1689. Applies to HIO-360-D1A model engines installed on Hughes Models 269C and 300C helicopters. Compliance required within 300 hours time in service after the effective date of this AD and every 300 hours in service thereafter. To prevent possible failures of the Bendix part numbers 10-349235-3 and 10-349235-4 magnetos, replace the part number 10-391315 rubber drive plate grommet in accordance with Lycoming Service Bulletin No. 364 or equivalent procedure approved by Chief, Engineering and Manufacturing Branch, FAA, Eastern Region. This amendment is effective July 23, 1973.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 431

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
  • Schweizer127 aircraft
  • Enstrom115 aircraft
  • Hughes111 aircraft
  • Enstrom Helicopter31 aircraft
  • Cessna3 aircraft
  • Other makers4044 aircraft
By year built
19462025
Registered aircraft by year built: 337 aircraft
19462
19591
19632
19643
19657
19669
19677
196812
19695
19701
19714
19723
19733
19744
19751
19769
197723
197818
197910
198011
198115
19829
19833
19842
19857
19865
19878
19889
19897
19906
19918
19929
19934
19947
19954
19967
19978
19986
19996
20002
20017
20029
20035
20045
200518
20065
20073
20087
20094
20103
20161
20231
20241
20251

94 with no year recorded

By model

Aircraft

See all 431 aircraft