AD 78-25-01

final rule

AVCO LYCOMING Model O-235-L2C Engines

AD Number
78-25-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Lycoming Engines O-235-L2C AVCO LYCOMING Model O-235-L2C Engines

Unsafe Condition

Failure of condensers installed in the Slick 40xx series magnetos can cause engine stoppage.

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

Required Actions

Replace Slick Models 4050, 4051, 4052, or 4081 magnetos with Models 4150, 4151, 4152, or 4181 (serial numbers 8100001 and up) or approved equivalents. Compliance must be done prior to further flight for engines with less than 75 hours, or within 50 hours in service after the AD's effective date for those with 75+ hours.

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

Compliance Time

Prior to further flight for engines with less than 75 hours of operation; within 50 hours in service after December 8, 1978 for engines with 75 hours or more.

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

Affected Aircraft

AVCO Lycoming Model O-235-L2C engines installed in Piper Model PA-38-112 aircraft.

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

Federal Register Abstract

Condensers

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
78-25-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVCO LYCOMING Model O-235-L2C Engines
Subject:
Condensers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/08/1978
Make:
Lycoming Engines
Model:
O-235-L2C
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Superseded AD: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Superseded By: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: 78-25-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3360

AD NUMBER:   78-25-01

SUBJECT HEADING:   AVCO LYCOMING Model O-235-L2C Engines

ACTION:  

SUMMARY:  

DATES:   Effective December 8, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   78-25-01 AVCO LYCOMING: Amendment 39-3360. Applies to all AVCO Lycoming Model O-235-L2C engines installed in Piper Model PA-38-112 aircraft.
Compliance required as indicated, unless already accomplished.
To prevent engine stoppage caused by failure of condensers installed in the Slick 40xx series magnetos, comply with the following:
a. Prior to further flight, engines whose Slick 40xx series magnetos have not accumulated 75 hours of operation in a Piper Model PA-38-112 aircraft must have their Slick Models 4050, 4051, 4052, or 4081 magnetos replaced with Slick Models 4150, 4151, 4152, or 4181 magnetos respectively having serial numbers 8100001 and up, or an approved equivalent part.
b. Engines whose Slick 40xx series magnetos have accumulated 75 hours or more of operation in a Piper Model PA-38-112 aircraft must have their Slick Models 4050, 4051, 4052, or 4081 magnetos replaced with Slick Models 4150, 4151, 4152, or 4181 magnetos respectively having serial numbers 8100001 and up or an approved equivalent part within 50 hours in service after the effective date of this AD.
c. Equivalent methods of compliance may be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
d. Upon submission of substantiating data by an owner or operator through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region, may adjust the compliance time specified in paragraph (b) in this AD.
AVCO Lycoming Service Bulletin No. 432 is the subject of the AD.
This amendment is effective December 8, 1978.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_78-25-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
78-25-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVCO LYCOMING Model O-235-L2C Engines
Subject:
Condensers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/08/1978
Make:
Lycoming Engines
Model:
O-235-L2C
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: 78-25-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3360

AD NUMBER:   78-25-01

SUBJECT HEADING:   AVCO LYCOMING Model O-235-L2C Engines

ACTION:  

SUMMARY:  

DATES:   Effective December 8, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   78-25-01 AVCO LYCOMING: Amendment 39-3360. Applies to all AVCO Lycoming Model O-235-L2C engines installed in Piper Model PA-38-112 aircraft.
Compliance required as indicated, unless already accomplished.
To prevent engine stoppage caused by failure of condensers installed in the Slick 40xx series magnetos, comply with the following:
a. Prior to further flight, engines whose Slick 40xx series magnetos have not accumulated 75 hours of operation in a Piper Model PA-38-112 aircraft must have their Slick Models 4050, 4051, 4052, or 4081 magnetos replaced with Slick Models 4150, 4151, 4152, or 4181 magnetos respectively having serial numbers 8100001 and up, or an approved equivalent part.
b. Engines whose Slick 40xx series magnetos have accumulated 75 hours or more of operation in a Piper Model PA-38-112 aircraft must have their Slick Models 4050, 4051, 4052, or 4081 magnetos replaced with Slick Models 4150, 4151, 4152, or 4181 magnetos respectively having serial numbers 8100001 and up or an approved equivalent part within 50 hours in service after the effective date of this AD.
c. Equivalent methods of compliance may be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
d. Upon submission of substantiating data by an owner or operator through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region, may adjust the compliance time specified in paragraph (b) in this AD.
AVCO Lycoming Service Bulletin No. 432 is the subject of the AD.
This amendment is effective December 8, 1978.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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