AD 46-41-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bellanca Aircraft Corporation | 14-13 | Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes |
| aircraft | Bellanca Aircraft Corporation | 14-13-2 | Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes |
Unsafe Condition
The control wheel universal joints may fail due to excessive wear or fatigue, leading to loss of control system connectivity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace universal joints connecting the control wheel axle with the control system yoke with the 'Apex UJ-402' universal joints furnished by the airplane manufacturer.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
prior to November 15, 1946
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bellanca Model 14-13, 14-13-2, serial numbers 1060 to 1065, inclusive.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Control Wheel Universal Joints
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_46-41-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 46-41-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes Subject: Control Wheel Universal Joints 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Aircraft Corporation Model: 14-13 | 14-13-2 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 46-41-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 46-41-03 SUBJECT HEADING: Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 46-41-03 BELLANCA: (Was Mandatory Note 3 of AD-773-5.) Applies to Models 14-13, 14-13-2 Serial Numbers 1060 to 1065, Inclusive. Compliance required prior to November 15, 1946. Replace universal joints connecting the control wheel axle with the control system yoke with the "Apex UJ-402" universal joints furnished by the airplane manufacturer. (Bellanca Service Bulletin No. 3 covers this same subject.) FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_46-41-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 46-41-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes Subject: Control Wheel Universal Joints 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: 46-41-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 46-41-03 SUBJECT HEADING: Airworthiness Directives; Bellanca Model 14-13, 14-13-2 Airplanes ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 46-41-03 BELLANCA: (Was Mandatory Note 3 of AD-773-5.) Applies to Models 14-13, 14-13-2 Serial Numbers 1060 to 1065, Inclusive. Compliance required prior to November 15, 1946. Replace universal joints connecting the control wheel axle with the control system yoke with the "Apex UJ-402" universal joints furnished by the airplane manufacturer. (Bellanca Service Bulletin No. 3 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.
Related Airworthiness Directives
2022-03-15
final ruleAirworthiness Directives; Various Airplanes
Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...
2005-01-19
final ruleAirworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders
Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...
79-19-05
final ruleAirworthiness Directives; Bellanca Model 14-13 Aircraft
Unsafe Condition: Reversal of aileron control system leading to incorrect operation
79-07-02
final ruleAirworthiness Directives; ESB WISCO, INCORPORATED: Applies To Those Batteries Manufactured During December 1978, January and February 1979
Unsafe Condition: The Exide AC 78M and Willard W 78M batteries manufactured between December 1978 and February 1979, identified by N-8, A-9, or B-9 stamped on terminal posts, may fail due to internal short circuits ...