AD 68-06-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
Failure of the static inverter panel could result in loss of electrical power to essential systems.
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Required Actions
Install 'P' clips, part number VGS 6750-2, to the static inverter panel following British Aircraft Corporation Service Bulletin No. 34-PM 2709, Revision 1, or later ARB-approved issue, or an FAA-approved equivalent.
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Compliance Time
Within the next 300 hours' time in service after the effective date of this AD
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Affected Aircraft
BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series airplanes
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Federal Register Abstract
Static Inverter Panel
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_68-06-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 68-06-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes Subject: Static Inverter Panel Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/26/1968 Make: Airbus SAS Model: BAC 1-11 200 Series | BAC 1-11 400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 68-06-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-567 AD NUMBER: 68-06-04 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective March 26, 1968. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 68-06-04 BRITISH AIRCRAFT: Amendment 39-567. Applies to Model BAC 1-11 200 and 400 Series airplanes. Within the next 300 hours' time in service after the effective date of this AD, unless already accomplished, install "P" clips, P/N VGS 6750-2, to the static inverter panel, in accordance with British Aircraft Corporation BAC 1-11 Service Bulletin No. 34-PM 2709, Revision 1, or later ARB-approved issue, or an FAA-approved equivalent. This amendment becomes effective March 26, 1968. FOOTER:
Document Text
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AD Final Rules - DRS_68-06-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 68-06-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes Subject: Static Inverter Panel Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/26/1968 Make: Airbus SAS Model: BAC 1-11 200 Series | BAC 1-11 400 Series 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: 68-06-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-567 AD NUMBER: 68-06-04 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective March 26, 1968. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 68-06-04 BRITISH AIRCRAFT: Amendment 39-567. Applies to Model BAC 1-11 200 and 400 Series airplanes. Within the next 300 hours' time in service after the effective date of this AD, unless already accomplished, install "P" clips, P/N VGS 6750-2, to the static inverter panel, in accordance with British Aircraft Corporation BAC 1-11 Service Bulletin No. 34-PM 2709, Revision 1, or later ARB-approved issue, or an FAA-approved equivalent. This amendment becomes effective March 26, 1968. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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