AD 63-20-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bellanca Aircraft Corporation | 14-13 | Airworthiness Directives; Bellanca Model 14-13 Series Aircraft |
| aircraft | Bellanca Aircraft Corporation | 14-13-2 | Airworthiness Directives; Bellanca Model 14-13 Series Aircraft |
| aircraft | Bellanca Aircraft Corporation | 14-13-3 | Airworthiness Directives; Bellanca Model 14-13 Series Aircraft |
| aircraft | Bellanca Aircraft Corporation | 14-13-3W | Airworthiness Directives; Bellanca Model 14-13 Series Aircraft |
Unsafe Condition
Cracks in the welds and adjacent structure where the brake-cylinder support brackets (P/N 9811-17 and -21) are attached to fuselage cross tube P/N 9802-47.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect welds and adjacent structure for cracks using dye penetrant and 10-power glass or FAA approved equivalent. Remove grease/dirt prior to inspection. Repair or replace cracked parts with FAA approved methods or equivalent part before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 hours' time in service after October 21, 1963, and every 50 hours' time in service thereafter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bellanca Model 14-13, 14-13-2, 14-13-3, 14-13-3W aircraft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Brake Cylinder Support Bracket
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_63-20-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 63-20-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14-13 Series Aircraft Subject: Brake Cylinder Support Bracket Status: Current Citation: Federal Register: September 19, 1963 Citation Publish Date: 09/19/1963 Effective Date: 10/21/1963 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Model: 14-13 | 14-13-2 | 14-13-3 | 14-13-3W Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 63-20-01 CITATION: [Federal Register: September 19, 1963] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 63-20-01 SUBJECT HEADING: Airworthiness Directives; Bellanca Model 14-13 Series Aircraft ACTION: SUMMARY: DATES: Effective October 21, 1963. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 63-20-01 BELLANCA: Amdt. 620 Part 507 Federal Register September 19, 1963. Applies to All Model 14-13 Series Aircraft. Compliance required as indicated. Within 50 hours' time in service after the effective date of this AD, and at intervals thereafter not to exceed 50 hours' time in service from the last inspection, accomplish the following: (a) Inspect for cracks in the welds and the structure immediately adjacent to the area where the left and right brake-cylinder support brackets, P/N's 9811-17 and -21, are attached to the fuselage cross tube P/N 9802-47 (located directly aft of the firewall, below the cabin floor), using a dye penetrant and a 10-power glass or an FAA approved equivalent. Prior to inspection, all grease and dirt shall be removed from the surfaces involved. (b) If cracks are found, that part must be repaired in accordance with an FAA approved repair, or replaced by a part of the same part number, or an FAA approved equivalent part before further flight. This directive effective October 21, 1963. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_63-20-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 63-20-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Bellanca Model 14-13 Series Aircraft Subject: Brake Cylinder Support Bracket Status: Current Citation: Federal Register: September 19, 1963 Citation Publish Date: 09/19/1963 Effective Date: 10/21/1963 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: 63-20-01 CITATION: [Federal Register: September 19, 1963] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 63-20-01 SUBJECT HEADING: Airworthiness Directives; Bellanca Model 14-13 Series Aircraft ACTION: SUMMARY: DATES: Effective October 21, 1963. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 63-20-01 BELLANCA: Amdt. 620 Part 507 Federal Register September 19, 1963. Applies to All Model 14-13 Series Aircraft. Compliance required as indicated. Within 50 hours' time in service after the effective date of this AD, and at intervals thereafter not to exceed 50 hours' time in service from the last inspection, accomplish the following: (a) Inspect for cracks in the welds and the structure immediately adjacent to the area where the left and right brake-cylinder support brackets, P/N's 9811-17 and -21, are attached to the fuselage cross tube P/N 9802-47 (located directly aft of the firewall, below the cabin floor), using a dye penetrant and a 10-power glass or an FAA approved equivalent. Prior to inspection, all grease and dirt shall be removed from the surfaces involved. (b) If cracks are found, that part must be repaired in accordance with an FAA approved repair, or replaced by a part of the same part number, or an FAA approved equivalent part before further flight. This directive effective October 21, 1963. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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