AD 65-14-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 35-33 | Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft |
| aircraft | Textron Aviation Inc. | H35 | Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft |
| aircraft | Textron Aviation Inc. | J35 | Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft |
| aircraft | Textron Aviation Inc. | K35 | Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft |
Unsafe Condition
Failure of the alternator support bracket due to elongated bolt holes or cracks.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect alternator supporting brackets (P/N's 195814, 195820, 195836, 195838, 195840, 626131) for elongated bolt holes. Inspect for cracks using dye penetrant or magnetic particle method. Replace brackets with elongated holes or cracks before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 25 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 50 hours' time in service from the last inspection
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Affected Aircraft
BEECH Models H35, J35, K35, and 35-33 Series Aircraft equipped with Ellingsworth Products Co., Inc. Alternator Kit Number 195860 installed under STC SA1-377
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Alternator Support Bracket
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_65-14-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 65-14-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft Subject: Alternator Support Bracket Status: Current Citation: Federal Register: June 26, 1965 Citation Publish Date: 06/26/1965 Effective Date: 06/26/1965 Make: Textron Aviation Inc. Model: 35-33 | H35 | J35 | K35 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 65-14-01 CITATION: [Federal Register: June 26, 1965] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-96 AD NUMBER: 65-14-01 SUBJECT HEADING: Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft ACTION: SUMMARY: DATES: Effective June 26, 1965. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 65-14-01 BEECH: Amdt. 39-96 Part 39 Federal Register June 26, 1965. Applies to Models H35, J35, K35, and 35-33 Series Aircraft Equipped with Ellingsworth Products Co., Inc. Alternator Kit Number 195860 Installed Under STC SA1-377. Compliance required within the next 25 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 50 hours' time in service from the last inspection. To prevent further failures of the alternator support bracket, accomplish the following: (a) Remove alternator supporting brackets, P/N's 195814, 195820, 195836, 195838, 195840 and 626131, thoroughly clean and inspect for elongated bolt holes. (b) Inspect brackets not having elongated bolt holes, for cracks using dye penetrant or magnetic particle method or FAA-approved equivalent. (c) Replace brackets having elongated bolt holes or cracks with unused parts of the same part number or FAA-approved equivalent before further flight. (d) Upon request of the operator, and FAA maintenance inspector, subject to prior approval of the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, may adjust the repetitive inspection intervals specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the increase for such operator. This directive effective June 26, 1965. FOOTER:
Document Text
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AD Final Rules - DRS_65-14-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 65-14-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft Subject: Alternator Support Bracket Status: Current Citation: Federal Register: June 26, 1965 Citation Publish Date: 06/26/1965 Effective Date: 06/26/1965 Make: Textron Aviation Inc. Model: 35-33 | H35 | J35 | K35 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: 65-14-01 CITATION: [Federal Register: June 26, 1965] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-96 AD NUMBER: 65-14-01 SUBJECT HEADING: Airworthiness Directives; BEECH Models H35, J35, K35, and 35-33 Series Aircraft ACTION: SUMMARY: DATES: Effective June 26, 1965. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 65-14-01 BEECH: Amdt. 39-96 Part 39 Federal Register June 26, 1965. Applies to Models H35, J35, K35, and 35-33 Series Aircraft Equipped with Ellingsworth Products Co., Inc. Alternator Kit Number 195860 Installed Under STC SA1-377. Compliance required within the next 25 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 50 hours' time in service from the last inspection. To prevent further failures of the alternator support bracket, accomplish the following: (a) Remove alternator supporting brackets, P/N's 195814, 195820, 195836, 195838, 195840 and 626131, thoroughly clean and inspect for elongated bolt holes. (b) Inspect brackets not having elongated bolt holes, for cracks using dye penetrant or magnetic particle method or FAA-approved equivalent. (c) Replace brackets having elongated bolt holes or cracks with unused parts of the same part number or FAA-approved equivalent before further flight. (d) Upon request of the operator, and FAA maintenance inspector, subject to prior approval of the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, may adjust the repetitive inspection intervals specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the increase for such operator. This directive effective June 26, 1965. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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