AD 79-19-05

final rule

Airworthiness Directives; Bellanca Model 14-13 Aircraft

AD Number
79-19-05
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 Bellanca Aircraft Corporation 14-13 Airworthiness Directives; Bellanca Model 14-13 Aircraft
aircraft Bellanca Aircraft Corporation 14-13-2 Airworthiness Directives; Bellanca Model 14-13 Aircraft
aircraft Bellanca Aircraft Corporation 14-13-3 Airworthiness Directives; Bellanca Model 14-13 Aircraft
aircraft Bellanca Aircraft Corporation 14-13-3W Airworthiness Directives; Bellanca Model 14-13 Aircraft

Unsafe Condition

Reversal of aileron control system leading to incorrect operation

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

Required Actions

Inspect the aileron control system for correct rigging and proper operation. If reversal is detected, rerig the system correctly.

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

Compliance Time

within the next 10 hours 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

Bellanca Aircraft Corporation Model 14-13, 14-13-2, 14-13-3, 14-13-3W aircraft certificated in all categories

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

Federal Register Abstract

Aileron Control System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_79-19-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
79-19-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Model 14-13 Aircraft
Subject:
Aileron Control System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/10/1979
Make:
Bellanca Aircraft Corporation
Model:
14-13 | 14-13-2 | 14-13-3 | 14-13-3W
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Superseded AD: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Superseded By: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: 79-19-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3551

AD NUMBER:   79-19-05

SUBJECT HEADING:   Airworthiness Directives; Bellanca Model 14-13 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective September 10, 1979.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
79-19-05 BELLANCA: Amendment 39-3551. Applies to all Bellanca Model 14-13 aircraft, certificated in all categories.

Compliance required within the next 10 hours in service after the effective date of this AD, unless already accomplished.

Inspect the aileron control system for correct rigging and proper operation. If reversal of control system is detected, rerig the system correctly.

NOTE: Do not use the Bellanca 14-13 Handbook for guidance in rigging procedure as the aileron system depicted on page 14, Figure 11, is shown in reverse.

This amendment is effective September 10, 1979.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_79-19-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
79-19-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Model 14-13 Aircraft
Subject:
Aileron Control System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/10/1979
Make:
Bellanca Aircraft Corporation
Model:
14-13 | 14-13-2 | 14-13-3 | 14-13-3W
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: 79-19-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3551

AD NUMBER:   79-19-05

SUBJECT HEADING:   Airworthiness Directives; Bellanca Model 14-13 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective September 10, 1979.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
79-19-05 BELLANCA: Amendment 39-3551. Applies to all Bellanca Model 14-13 aircraft, certificated in all categories.

Compliance required within the next 10 hours in service after the effective date of this AD, unless already accomplished.

Inspect the aileron control system for correct rigging and proper operation. If reversal of control system is detected, rerig the system correctly.

NOTE: Do not use the Bellanca 14-13 Handbook for guidance in rigging procedure as the aileron system depicted on page 14, Figure 11, is shown in reverse.

This amendment is effective September 10, 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.