AD 51-16-01

final rule

Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes

AD Number
51-16-01
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 and 14-13-2 Airplanes
aircraft Bellanca Aircraft Corporation 14-13-2 Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes

Unsafe Condition

Failure of the elevator trim tab in flight.

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

Required Actions

Modify the trim tab attachment to the elevator as shown in Figure 1. The modification is covered by Bellanca Service Bulletin No. 14.

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

Compliance Time

within the next 25 hours of operation, but not later than August 1, 1951

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

Affected Aircraft

Bellanca Model 14-13 and 14-13-2 airplanes, all serial numbers.

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

Federal Register Abstract

Trim Tab Modification

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
51-16-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes
Subject:
Trim Tab Modification
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Bellanca Aircraft Corporation
Model:
14-13 | 14-13-2
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Superseded AD: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Superseded By: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: 51-16-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   51-16-01

SUBJECT HEADING:   Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
51-16-01 BELLANCA: Applies to All Models 14-13 and 14-13-2 Airplanes.

Compliance required within the next 25 hours of operation, but not later than August 1, 1951.

As a result of a recent failure of the elevator trim tab in flight, the modification of the trim tab attachment to the elevator as shown in Figure 1 should be made.



FIGURE 1


(Bellanca Service Bulletin No. 14, Models 14-13 and 14-13-2, covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_51-16-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
51-16-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes
Subject:
Trim Tab Modification
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Bellanca Aircraft Corporation
Model:
14-13 | 14-13-2
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: 51-16-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   51-16-01

SUBJECT HEADING:   Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
51-16-01 BELLANCA: Applies to All Models 14-13 and 14-13-2 Airplanes.

Compliance required within the next 25 hours of operation, but not later than August 1, 1951.

As a result of a recent failure of the elevator trim tab in flight, the modification of the trim tab attachment to the elevator as shown in Figure 1 should be made.



FIGURE 1


(Bellanca Service Bulletin No. 14, Models 14-13 and 14-13-2, covers 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.