AD 63-06-03
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Kelowna Flightcraft R & D Ltd. | 340 | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 340 and 440 Series Aircraft |
| aircraft | Kelowna Flightcraft R & D Ltd. | 440 | Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 340 and 440 Series Aircraft |
Unsafe Condition
Failure of the Bendix Redbank Type 35E05 fault detection panel could result in loss of electrical power.
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Required Actions
Install a blocking rectifier (G.E. IN-93 or FAA approved equivalent) by soldering the negative lead to lug No. 3 of the locating relay and the positive lead to terminal No. P on the terminal board.
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Compliance Time
within the next 300 hours' time in service following the effective date of this AD
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Affected Aircraft
All Models 340 and 440 Series Aircraft Equipped With a Bendix Redbank Type 35E05 Fault Detection Panel
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Federal Register Abstract
Electrical Fault Detection Panel
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_63-06-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 63-06-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 340 and 440 Series Aircraft Subject: Electrical Fault Detection Panel Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/20/1963 Make: Kelowna Flightcraft R & D Ltd. Model: 340 | 440 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 63-06-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 63-06-03 SUBJECT HEADING: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 340 and 440 Series Aircraft ACTION: SUMMARY: DATES: Effective March 20, 1963. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 63-06-03 GENERAL DYNAMICS/CONVAIR: Amdt. 545 Part 507 Federal Register March 20, 1963. Applies to All Models 340 and 440 Series Aircraft Equipped With a Bendix Redbank Type 35E05 Fault Detection Panel. Compliance required within the next 300 hours' time in service following the effective date of this AD, unless already accomplished. To prevent the loss of electrical power, modify the type 35E05 fault detection panel by installing a blocking rectifier (G.E. IN-93 or FAA approved equivalent). Solder the negative lead to lug No. 3 of the locating relay and the positive lead to terminal No. P on the terminal board. (Convair Airgram No. 200 dated September 24, 1956, and Bendix Redbank Service Bulletin No. R-47 pertains to this same modification.) This directive effective March 20, 1963. FOOTER:
Document Text
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AD Final Rules - DRS_63-06-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 63-06-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 340 and 440 Series Aircraft Subject: Electrical Fault Detection Panel Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/20/1963 Make: Kelowna Flightcraft R & D Ltd. Model: 340 | 440 Product Type: Aircraft Product Subtype: Large 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: 63-06-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 63-06-03 SUBJECT HEADING: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 340 and 440 Series Aircraft ACTION: SUMMARY: DATES: Effective March 20, 1963. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 63-06-03 GENERAL DYNAMICS/CONVAIR: Amdt. 545 Part 507 Federal Register March 20, 1963. Applies to All Models 340 and 440 Series Aircraft Equipped With a Bendix Redbank Type 35E05 Fault Detection Panel. Compliance required within the next 300 hours' time in service following the effective date of this AD, unless already accomplished. To prevent the loss of electrical power, modify the type 35E05 fault detection panel by installing a blocking rectifier (G.E. IN-93 or FAA approved equivalent). Solder the negative lead to lug No. 3 of the locating relay and the positive lead to terminal No. P on the terminal board. (Convair Airgram No. 200 dated September 24, 1956, and Bendix Redbank Service Bulletin No. R-47 pertains to this same modification.) This directive effective March 20, 1963. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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