AD 79-09-02

final rule

Airworthiness Directives; CESSNA Model 441 Airplanes

AD Number
79-09-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 441 Airworthiness Directives; CESSNA Model 441 Airplanes

Unsafe Condition

Improper drainage of the aileron control surfaces could lead to moisture accumulation, potentially causing control surface malfunction.

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

Required Actions

Drill new drain holes in the ailerons per Cessna Propjet Service Information Letter PJ 79-3, or an equivalent method approved by the FAA. Compliance must be completed within 100 hours time-in-service after the effective date.

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 after the effective date of this AD

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

Affected Aircraft

Cessna Model 441 airplanes with serial numbers 441-0001 through 441-0090

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

Federal Register Abstract

Aileron Control Surfaces Drainage

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_79-09-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
79-09-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CESSNA Model 441 Airplanes
Subject:
Aileron Control Surfaces Drainage
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/07/1979
Make:
Cessna Aircraft Company
Model:
441
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Superseded AD: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Superseded By: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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 79-09-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3453

AD NUMBER:   79-09-02

SUBJECT HEADING:   Airworthiness Directives; CESSNA Model 441 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 7, 1979.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
79-09-02 CESSNA: Amendment 39-3453. Applies to Model 441 (Serial Numbers 441-0001 through 441-0090) airplanes.

COMPLIANCE: Required as indicated, unless already accomplished.

To assure proper drainage of the aileron control surfaces, within the next 100 hours time-in-service after the effective date of this AD, accomplish the following:

A) Incorporate additional drainage of the ailerons by drilling new drain holes in accordance with the instructions provided in Cessna Propjet Service Information Letter PJ 79-3, dated March 5, 1979.

B) Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

NOTE: The FAA has determined that there is insufficient justification to require mandatory compliance with the elevator portion of Cessna Service Information Letter PJ 79-3. Therefore, this AD is not applicable to elevator drainage improvements provided by that letter.

This Amendment becomes effective May 7, 1979.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_79-09-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
79-09-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; CESSNA Model 441 Airplanes
Subject:
Aileron Control Surfaces Drainage
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/07/1979
Make:
Cessna Aircraft Company
Model:
441
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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 79-09-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3453

AD NUMBER:   79-09-02

SUBJECT HEADING:   Airworthiness Directives; CESSNA Model 441 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 7, 1979.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
79-09-02 CESSNA: Amendment 39-3453. Applies to Model 441 (Serial Numbers 441-0001 through 441-0090) airplanes.

COMPLIANCE: Required as indicated, unless already accomplished.

To assure proper drainage of the aileron control surfaces, within the next 100 hours time-in-service after the effective date of this AD, accomplish the following:

A) Incorporate additional drainage of the ailerons by drilling new drain holes in accordance with the instructions provided in Cessna Propjet Service Information Letter PJ 79-3, dated March 5, 1979.

B) Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

NOTE: The FAA has determined that there is insufficient justification to require mandatory compliance with the elevator portion of Cessna Service Information Letter PJ 79-3. Therefore, this AD is not applicable to elevator drainage improvements provided by that letter.

This Amendment becomes effective May 7, 1979.

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.