AD 69-08-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 203/AE and 204/AF Airplanes |
Unsafe Condition
Fuel leakage into the wing center section torque box area
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Required Actions
Replace the aluminum alloy refuel/defuel valve housing P/N AB 45A101 with modified stainless steel valve housing P/N AB 45A1239 in accordance with BAC 1-11 Service Bulletin No. 28-PM 924 or later ARB-approved issue or FAA-approved equivalent.
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Compliance Time
within the next 2500 hours' time in service after the effective date of this AD
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Affected Aircraft
BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 203/AE and 204/AF airplanes
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Federal Register Abstract
Fuel Leakage Into Wing
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_69-08-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-08-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 203/AE and 204/AF Airplanes Subject: Fuel Leakage Into Wing 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Make: Airbus SAS Model: BAC 1-11 200 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 69-08-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-748 AD NUMBER: 69-08-04 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 203/AE and 204/AF Airplanes ACTION: SUMMARY: DATES: Effective May 11,1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-08-04 BRITISH AIRCRAFT CORPORATION: Amdt. 39-748. Applies to Model BAC 1-11, 203/AE and 204/AF airplanes. Compliance required within the next 2500 hours' time in service after the effective date of this AD, unless already accomplished. To prevent fuel leakage into the wing center section torque box area, replace the aluminum alloy refuel/defuel valve housing P/N AB 45A101 with modified stainless steel valve housing P/N AB 45A1239 in accordance with BAC 1-11 Service Bulletin No. 28-PM 924 or later ARB-approved issue or FAA-approved equivalent. This amendment becomes effective May 11,1969. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_69-08-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-08-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 203/AE and 204/AF Airplanes Subject: Fuel Leakage Into Wing 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 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: 69-08-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-748 AD NUMBER: 69-08-04 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 203/AE and 204/AF Airplanes ACTION: SUMMARY: DATES: Effective May 11,1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-08-04 BRITISH AIRCRAFT CORPORATION: Amdt. 39-748. Applies to Model BAC 1-11, 203/AE and 204/AF airplanes. Compliance required within the next 2500 hours' time in service after the effective date of this AD, unless already accomplished. To prevent fuel leakage into the wing center section torque box area, replace the aluminum alloy refuel/defuel valve housing P/N AB 45A101 with modified stainless steel valve housing P/N AB 45A1239 in accordance with BAC 1-11 Service Bulletin No. 28-PM 924 or later ARB-approved issue or FAA-approved equivalent. This amendment becomes effective May 11,1969. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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