AD 47-25-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bellanca Aircraft Corporation | 14-13 | Airworthiness Directives; Bellanca Model 14- 13, 14-13-2 |
| aircraft | Bellanca Aircraft Corporation | 14-13-2 | Airworthiness Directives; Bellanca Model 14- 13, 14-13-2 |
Unsafe Condition
Cracks in the fin and stabilizer fittings to which the tail bracing tie rods attach could lead to structural failure of the tail assembly.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the fin and stabilizer fittings for cracks at each 25-hour inspection up to the next 100-hour check. Replace cracked fittings by the next 100-hour check or September 1, 1947, whichever comes first, and install reinforcing gussets.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
prior to August 1, 1947
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 through 1560 inclusive
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fin and Stabilizer Fittings
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_47-25-09.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 47-25-09 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14- 13, 14-13-2 Subject: Fin and Stabilizer Fittings 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Bellanca Aircraft Corporation Model: 14-13 | 14-13-2 Product Type: Aircraft Product Subtype: Rotorcraft Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 47-25-09 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 47-25-09 SUBJECT HEADING: Airworthiness Directives; Bellanca Model 14- 13, 14-13-2 ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 47-25-09 BELLANCA: (Was Mandatory Note 6 of AD-773-05.) Applies to Models 14- 13, 14-13-2 Serial Numbers 1060 through 1560, Inclusive. Compliance required prior to August 1, 1947. Inspect the fin and stabilizer fittings to which the tail bracing tie rods attach for cracks and at each 25-hour inspection thereafter up to the next 100-hour check. Replace fitting if cracks are found not later than the next 100 hour check or September 1, 1947, whichever comes first and add reinforcing gussets. (Bellanca Service Bulletin No. 6 covers this same subject.) FOOTER:
Document Text
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AD Final Rules - DRS_47-25-09.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 47-25-09 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14- 13, 14-13-2 Subject: Fin and Stabilizer Fittings 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: Rotorcraft Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 47-25-09 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 47-25-09 SUBJECT HEADING: Airworthiness Directives; Bellanca Model 14- 13, 14-13-2 ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 47-25-09 BELLANCA: (Was Mandatory Note 6 of AD-773-05.) Applies to Models 14- 13, 14-13-2 Serial Numbers 1060 through 1560, Inclusive. Compliance required prior to August 1, 1947. Inspect the fin and stabilizer fittings to which the tail bracing tie rods attach for cracks and at each 25-hour inspection thereafter up to the next 100-hour check. Replace fitting if cracks are found not later than the next 100 hour check or September 1, 1947, whichever comes first and add reinforcing gussets. (Bellanca Service Bulletin No. 6 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.
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