AD 48-43-02

final rule

Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes

AD Number
48-43-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company | Rogers, Burl A. 170 Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes
aircraft Cessna Aircraft Company | Rogers, Burl A. 170A Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes
aircraft Cessna Aircraft Company | Rogers, Burl A. 15AC Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes
aircraft Cessna Aircraft Company | Rogers, Burl A. S15AC Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes

Unsafe Condition

Piston pin plugs of the loose fit type (P/N 25262-A1) are subject to rapid and excessive wear, leading to disintegration of the piston pin plugs, piston failure, and complete engine failure due to oil stoppage from metal particles on the screen and in the system.

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

Required Actions

Replace piston pin and plug assemblies P/N 25262-A1 with P/N 530830 (press fit plugs) as soon as possible, and inspect oil screens prior to each flight until the replacement is completed.

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

Compliance Time

not later than December 31, 1948

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

Affected Aircraft

Cessna Models 170 and Aeronca Models 15AC equipped with Continental C-145-2 engines, serial numbers 3001-8-2 to 3775-8-2 inclusive.

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

Federal Register Abstract

Continental C-145-2 Engines

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_48-43-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
48-43-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes
Subject:
Continental C-145-2 Engines
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Cessna Aircraft Company | Rogers, Burl A.
Model:
170 | 170A | 15AC | S15AC
Product Type:
Aircraft
Product Subtype:
Small Airplane
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: 48-43-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-43-02

SUBJECT HEADING:   Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-43-02 CESSNA and AERONCA: Applies to All Cessna Model 170 and Aeronca Model 15AC Airplanes Equipped With Continental C-145-2 Engines Serial Numbers 3001-8-2 to 3775- 8-2, Inclusive.

Compliance required not later than December 31, 1948.

Some piston pin plugs of the loose fit type with which the engines as noted were originally equipped, are subject to rapid and excessive wear which may eventually cause disintegration of the piston pin plugs, failure of pistons, and complete engine failure due to oil stoppage caused by metal particles on the screen and in the system.

To preclude the possibility of such failures, piston pin and plug assemblies, P/N 25262-A1 (with loose fit plugs), should be removed and replaced with piston pin and plug assemblies, P/N 530830 (with press fit plugs) as soon as possible, and in no case later than the compliance date shown.

Pending installation of the new assemblies, oil screens should be inspected prior to each flight. If aluminum particles are evident on the screen the airplane should be removed from service until the change is accomplished.

(Continental Service Bulletins Nos. M48-20 and M48-25 cover this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_48-43-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
48-43-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes
Subject:
Continental C-145-2 Engines
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Cessna Aircraft Company | Rogers, Burl A.
Model:
170 | 170A | 15AC | S15AC
Product Type:
Aircraft
Product Subtype:
Small Airplane
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: 48-43-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   48-43-02

SUBJECT HEADING:   Airworthiness Directives; Cessna All Models 170 and Aeronca Models 15AC Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
48-43-02 CESSNA and AERONCA: Applies to All Cessna Model 170 and Aeronca Model 15AC Airplanes Equipped With Continental C-145-2 Engines Serial Numbers 3001-8-2 to 3775- 8-2, Inclusive.

Compliance required not later than December 31, 1948.

Some piston pin plugs of the loose fit type with which the engines as noted were originally equipped, are subject to rapid and excessive wear which may eventually cause disintegration of the piston pin plugs, failure of pistons, and complete engine failure due to oil stoppage caused by metal particles on the screen and in the system.

To preclude the possibility of such failures, piston pin and plug assemblies, P/N 25262-A1 (with loose fit plugs), should be removed and replaced with piston pin and plug assemblies, P/N 530830 (with press fit plugs) as soon as possible, and in no case later than the compliance date shown.

Pending installation of the new assemblies, oil screens should be inspected prior to each flight. If aluminum particles are evident on the screen the airplane should be removed from service until the change is accomplished.

(Continental Service Bulletins Nos. M48-20 and M48-25 cover this same subject.)

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.

View Official Source ↗