AD 79-19-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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
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Affected Aircraft
Bellanca Aircraft Corporation Model 14-13, 14-13-2, 14-13-3, 14-13-3W aircraft certificated in all categories
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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Model: 14-13 | 14-13-2 | 14-13-3 | 14-13-3W Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 79-19-05 CITATION: This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
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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
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