AD 69-08-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes |
Unsafe Condition
Failure of the shear pin installed within the Elevator Centralizing Spring Pots (Part Numbers AB34-A881, A3003, A3017, A3019, and A3021) could result in loss of elevator control.
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Required Actions
Remove and disassemble the spring pots from the right and left elevators, and modify in accordance with BAC 1-11 Service Bulletin No. 27-A-PM 3536 or later ARB-approved issue, or FAA-approved equivalent.
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Compliance Time
within the next 1500 hours' time in service after the effective date of this AD
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Affected Aircraft
BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series airplanes
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Federal Register Abstract
Elevator Spring Pot
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_69-08-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-08-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes Subject: Elevator Spring Pot Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/11/1969 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Model: BAC 1-11 200 Series | BAC 1-11 400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 69-08-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-749 AD NUMBER: 69-08-05 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective May 11, 1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-08-05 BRITISH AIRCRAFT CORPORATION: Amdt. 39-749. Applies to Model BAC 1-11, 200 and 400 Series airplanes. Compliance required within the next 1500 hours' time in service after the effective date of this AD, unless already accomplished. To ensure that the shear pin which is installed within the Elevator Centralizing Spring Pots, Part Numbers AB34-A881, A3003, A3017, A3019, and A3021 remains effective, remove and disassemble the spring pots from the right and left elevators and modify in Accordance with BAC 1-11 Service Bulletin No. 27-A-PM 3536 or later ARB-approved issue, or FAA-approved equivalent. This amendment becomes effective May 11, 1969. FOOTER:
Document Text
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AD Final Rules - DRS_69-08-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-08-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes Subject: Elevator Spring Pot Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/11/1969 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: 69-08-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-749 AD NUMBER: 69-08-05 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective May 11, 1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-08-05 BRITISH AIRCRAFT CORPORATION: Amdt. 39-749. Applies to Model BAC 1-11, 200 and 400 Series airplanes. Compliance required within the next 1500 hours' time in service after the effective date of this AD, unless already accomplished. To ensure that the shear pin which is installed within the Elevator Centralizing Spring Pots, Part Numbers AB34-A881, A3003, A3017, A3019, and A3021 remains effective, remove and disassemble the spring pots from the right and left elevators and modify in Accordance with BAC 1-11 Service Bulletin No. 27-A-PM 3536 or later ARB-approved issue, or FAA-approved equivalent. This amendment becomes effective May 11, 1969. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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