AD 48-05-03
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 trim tab bracket bolts could result in spreading of the brackets and loss of trim tab retention.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install a 3/16-inch bolt with self-locking nut and three washers through each bracket retaining the trim tab brass trunnions. Position the bolt 7/16 of an inch above the trunnion centerline.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
March 15, 1948
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, serial numbers 1060 through 1576.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Trim Tab Bracket Bolts
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_48-05-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 48-05-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes Subject: Trim Tab Bracket Bolts 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Aircraft Corporation Model: 14-13 | 14-13-2 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 48-05-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 48-05-03 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: 48-05-03 BELLANCA: Applies to 14-13 and 14-13-2 Serial Numbers 1060 Through 1576. Compliance required by March 15, 1948. Install a 3/16-inch bolt with self-locking nut and three washers (installed as spacers) through each of the brackets which retain the trim tab brass trunnions at the tab and elevator. Install the bolt 7/16 of an inch above the trunnion centerline to prevent spreading of the brackets. (Bellanca Service Bulletin No. 14 covers this same subject.) FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_48-05-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 48-05-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14-13 and 14-13-2 Airplanes Subject: Trim Tab Bracket Bolts 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: 48-05-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 48-05-03 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: 48-05-03 BELLANCA: Applies to 14-13 and 14-13-2 Serial Numbers 1060 Through 1576. Compliance required by March 15, 1948. Install a 3/16-inch bolt with self-locking nut and three washers (installed as spacers) through each of the brackets which retain the trim tab brass trunnions at the tab and elevator. Install the bolt 7/16 of an inch above the trunnion centerline to prevent spreading of the brackets. (Bellanca Service Bulletin No. 14 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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