AD 73-15-04

final rule

AVCO LYCOMING Model HIO-360-D1A Engines

AD Number
73-15-04
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Lycoming Engines HIO-360-D1A AVCO LYCOMING Model HIO-360-D1A Engines

Unsafe Condition

Failure of Bendix part numbers 10-349235-3 and 10-349235-4 magnetos due to degraded rubber drive plate grommet (part number 10-391315).

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace the part number 10-391315 rubber drive plate grommet in accordance with Lycoming Service Bulletin No. 364 or equivalent procedure approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within 300 hours time in service after the effective date of this AD and every 300 hours in service thereafter

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

AVCO Lycoming Model HIO-360-D1A engines installed on Hughes Models 269C and 300C helicopters.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Rubber Drive Plate Grommet

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_73-15-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
73-15-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVCO LYCOMING Model HIO-360-D1A Engines
Subject:
Rubber Drive Plate Grommet
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/23/1973
Make:
Lycoming Engines
Model:
HIO-360-D1A
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 73-15-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1689

AD NUMBER:   73-15-04

SUBJECT HEADING:   AVCO LYCOMING Model HIO-360-D1A Engines

ACTION:  

SUMMARY:  

DATES:   Effective July 23, 1973.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

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.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_73-15-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
73-15-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVCO LYCOMING Model HIO-360-D1A Engines
Subject:
Rubber Drive Plate Grommet
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/23/1973
Make:
Lycoming Engines
Model:
HIO-360-D1A
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 73-15-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1689

AD NUMBER:   73-15-04

SUBJECT HEADING:   AVCO LYCOMING Model HIO-360-D1A Engines

ACTION:  

SUMMARY:  

DATES:   Effective July 23, 1973.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

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.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.