AD 63-23-02

final rule

LYCOMING Model O-320 Engines

AD Number
63-23-02
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
engine Lycoming Engines O-320-A1A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-A1B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-A2A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-A2B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-A2C LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-A3A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-A3B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-A3C LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-B1A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-B1B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-B2A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-B2B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-B2C LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-B3A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-B3B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-B3C LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-C2A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-C2B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-C3A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-C3B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-D1A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-D1B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-D2A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-D2B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-E1A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-E1B LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-E2A LYCOMING Model O-320 Engines
engine Lycoming Engines O-320-E2B LYCOMING Model O-320 Engines

Unsafe Condition

Exhaust valve stem and camshaft assembly (P/N 68769) may fail due to excessive wear, leading to engine failure.

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

Required Actions

Inspect and replace exhaust valves and guides as necessary per Lycoming Service Bulletin No. 293B or an approved alternative method.

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

Compliance Time

Within the next 100 hours' time in service and every 300 or 500 hours' time in service thereafter, depending on engine usage and time since last inspection.

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

Affected Aircraft

Lycoming Engines Model O-320 with exhaust valve stem diameter 7/16" and camshaft assembly P/N 68769, including specific models: O-320-A1A, O-320-A1B, O-320-A2A, O-320-A2B, O-320-A2C, O-320-A3A, O-320-A3B, O-320-A3C, and others as listed.

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

Federal Register Abstract

Exhaust Valves

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_63-23-02.html
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AD Number:
63-23-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LYCOMING Model O-320 Engines
Subject:
Exhaust Valves
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/06/1968
Make:
Lycoming Engines
Model:
O-320-A1A | O-320-A1B | O-320-A2A | O-320-A2B | O-320-A2C | O-320-A3A | O-320-A3B | O-320-A3C | O-32...Show more
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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 63-23-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-627

AD NUMBER:   63-23-02

SUBJECT HEADING:   LYCOMING Model O-320 Engines

ACTION:  

SUMMARY:  

DATES:   Effective August 6, 1968.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   63-23-02 LYCOMING: As amended by Amendment 39-627 - is corrected as follows: Applies to all O-320 type engines which incorporate the 7/16" diameter exhaust valve stem with camshaft assembly P/N 68769.

Compliance with (d) required at the times indicated in (a), (b), or (c) as applicable.

(a) Engines used for aerial dusting or chemical application service since new or since replacement of all exhaust valves and valve guides.

(1) As of the effective date of this AD, engines with more than 200 hours' time in service since new or since replacement of all exhaust valves and valve guides, shall comply within the next 100 hours' time in service and every 300 hours' time in service thereafter.

(2) As of the effective date of this AD, engines with 200 hours' or less time in service since new or since replacement of all exhaust valves and valve guides, shall comply prior to the accumulation of 300 hours' time in service since new or since exhaust valve and valve guide replacement and every 300 hours' time in service thereafter.

(b) Engines used in all operations other than those covered in paragraph (a).

(1) New engines and engines which have a record of at least No. 3 and No. 4 exhaust valve and valve guide replacement.

(i) As of the effective date of this AD, engines with more than 400 hours' time in service since new or since the replacement of No. 3 and No. 4 exhaust valves and valve guides, shall comply within the next 100 hours' time in service and every 500 hours' time in service thereafter.

(ii) As of the effective date of this AD, engines with 400 hours' or less time in service since new or since replacement of No. 3 and No. 4 exhaust valves and valve guides shall comply prior to the accumulation of 500 hours' time in service since new or since No. 3 and No. 4 exhaust valve and valve guide replacement and every 500 hours' time in service thereafter.

(2) Engines which have a record of exhaust valve replacement of at least No. 3 and No. 4 valves but no record of valve guide replacement.

(i) As of the effective date of this AD, engines with more than 200 hours' time in service since replacement of No. 3 and No. 4 exhaust valves shall comply within the next 100 hours' time in service and every 500 hours' time in service thereafter.

(ii) As of the effective date of this AD, engines with 200 hours' or less time in service since replacement of No. 3 and No. 4 exhaust valves shall comply prior to the accumulation of 300 hours' time in service since exhaust valve replacement and every 500 hours' time in service thereafter.

(c) Engines whose usage is changed between inspections.

(1) Engines whose usage is changed from that specified in (a) to that specified in (b) will comply as originally required in (a) for the first inspection after usage change. Subsequent inspections will be as required in (b).

(2) Engines whose usage is changed from that specified in (b) to that specified in (a) will comply with the requirements of (a) for the first inspection after usage change and for subsequent inspections.

(d) Inspect and, where necessary, replace exhaust valves and guides in accordance with Lycoming Service Bulletin No. 293B or other alternative method approved by the Chief, Engineering and Manufacturing Branch of the Eastern Region.

This amendment is effective Dec. 9, 1963.

Revised August 6, 1968.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_63-23-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
63-23-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LYCOMING Model O-320 Engines
Subject:
Exhaust Valves
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/06/1968
Make:
Lycoming Engines
Model:
O-320-A1A | O-320-A1B | O-320-A2A | O-320-A2B | O-320-A2C | O-320-A3A | O-320-A3B | O-320-A3C | O-32...Show more
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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 63-23-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-627

AD NUMBER:   63-23-02

SUBJECT HEADING:   LYCOMING Model O-320 Engines

ACTION:  

SUMMARY:  

DATES:   Effective August 6, 1968.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   63-23-02 LYCOMING: As amended by Amendment 39-627 - is corrected as follows: Applies to all O-320 type engines which incorporate the 7/16" diameter exhaust valve stem with camshaft assembly P/N 68769.

Compliance with (d) required at the times indicated in (a), (b), or (c) as applicable.

(a) Engines used for aerial dusting or chemical application service since new or since replacement of all exhaust valves and valve guides.

(1) As of the effective date of this AD, engines with more than 200 hours' time in service since new or since replacement of all exhaust valves and valve guides, shall comply within the next 100 hours' time in service and every 300 hours' time in service thereafter.

(2) As of the effective date of this AD, engines with 200 hours' or less time in service since new or since replacement of all exhaust valves and valve guides, shall comply prior to the accumulation of 300 hours' time in service since new or since exhaust valve and valve guide replacement and every 300 hours' time in service thereafter.

(b) Engines used in all operations other than those covered in paragraph (a).

(1) New engines and engines which have a record of at least No. 3 and No. 4 exhaust valve and valve guide replacement.

(i) As of the effective date of this AD, engines with more than 400 hours' time in service since new or since the replacement of No. 3 and No. 4 exhaust valves and valve guides, shall comply within the next 100 hours' time in service and every 500 hours' time in service thereafter.

(ii) As of the effective date of this AD, engines with 400 hours' or less time in service since new or since replacement of No. 3 and No. 4 exhaust valves and valve guides shall comply prior to the accumulation of 500 hours' time in service since new or since No. 3 and No. 4 exhaust valve and valve guide replacement and every 500 hours' time in service thereafter.

(2) Engines which have a record of exhaust valve replacement of at least No. 3 and No. 4 valves but no record of valve guide replacement.

(i) As of the effective date of this AD, engines with more than 200 hours' time in service since replacement of No. 3 and No. 4 exhaust valves shall comply within the next 100 hours' time in service and every 500 hours' time in service thereafter.

(ii) As of the effective date of this AD, engines with 200 hours' or less time in service since replacement of No. 3 and No. 4 exhaust valves shall comply prior to the accumulation of 300 hours' time in service since exhaust valve replacement and every 500 hours' time in service thereafter.

(c) Engines whose usage is changed between inspections.

(1) Engines whose usage is changed from that specified in (a) to that specified in (b) will comply as originally required in (a) for the first inspection after usage change. Subsequent inspections will be as required in (b).

(2) Engines whose usage is changed from that specified in (b) to that specified in (a) will comply with the requirements of (a) for the first inspection after usage change and for subsequent inspections.

(d) Inspect and, where necessary, replace exhaust valves and guides in accordance with Lycoming Service Bulletin No. 293B or other alternative method approved by the Chief, Engineering and Manufacturing Branch of the Eastern Region.

This amendment is effective Dec. 9, 1963.

Revised August 6, 1968.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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