AD 48-13-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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 four engine-cowl-support brackets, Bellanca P/N 9892-13, mounted on the firewall and possible cowl loss in flight.
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Required Actions
Inspect the four engine-cowl-support brackets for cracks. If cracks are found, install heavier brackets available from the factory, which eliminates the need for further inspection.
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Compliance Time
after each 25 hours of operation
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Affected Aircraft
Bellanca Model 14-13 and 14-13-2, serial numbers 1060 through 1310.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Engine Cowl Brackets
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_48-13-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 48-13-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes Subject: Engine Cowl Brackets 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Aircraft Corporation Model: 14-13 | 14-13-2 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 48-13-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 48-13-06 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: 48-13-06 BELLANCA: Applies to Models 14-13, 14-13-2 Serial Numbers 1060 Through 1310. Compliance required after each 25 hours of operation. To prevent failure of the four engine-cowl-support brackets, Bellanca P/N 9892-13, mounted on the firewall and possible cowl loss in flight, the brackets should be closely examined for cracks. If cracks are noted, heavier brackets available from the factory should be installed, in which case inspection is no longer required. (Bellanca Service Bulletin No. 16 dated December 8, 1947, covers this same subject.) FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_48-13-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 48-13-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes Subject: Engine Cowl Brackets 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: 48-13-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 48-13-06 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: 48-13-06 BELLANCA: Applies to Models 14-13, 14-13-2 Serial Numbers 1060 Through 1310. Compliance required after each 25 hours of operation. To prevent failure of the four engine-cowl-support brackets, Bellanca P/N 9892-13, mounted on the firewall and possible cowl loss in flight, the brackets should be closely examined for cracks. If cracks are noted, heavier brackets available from the factory should be installed, in which case inspection is no longer required. (Bellanca Service Bulletin No. 16 dated December 8, 1947, covers this same subject.) FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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