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AD 73-15-04 ACTIVE

Rubber Drive Plate Grommet
Key Information
AD Number 73-15-04 Status Active
Effective Date July 23, 1973 Issue Date Not specified
Docket Number Unknown Amendment 39-1689
Product Type ["Engine"] Product Subtype Not specified
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Lycoming Engines
Model(s) HIO-360-D1A
Regulatory Text

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.