AD 83-24-07
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
Possible loss of roll control due to aileron stub fairing installation issues at rib 15 on left and right wings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the aileron stub fairing installation on the outboard side of the fixed flap track center fairing at rib 15, left and right wing, per British Aerospace Service Bulletin 57-PM5856, Revision 1. Alternate means of compliance may be approved by the FAA Manager, Seattle Aircraft Certification Office.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 30 days after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
British Aerospace Model BAC 1-11 200 and 400 Series airplanes, all serial numbers
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Aileron Stub Fairing
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_83-24-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-24-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes Subject: Aileron Stub Fairing Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/20/1983 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Model: BAC 1-11 200 Series | BAC 1-11 400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 83-24-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4778 AD NUMBER: 83-24-07 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective December 20, 1983. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-24-07 BRITISH AEROSPACE: Amendment 39-4778. Applies to Model BAC 1-11 200 and 400 series airplanes, certificated in all categories. Compliance is required as indicated. To prevent possible loss of roll control, accomplish the following within the next 30 days after the effective date of this AD, unless previously accomplished: A. Modify the aileron stub fairing installation attached to the outboard side of the fixed flap track center fairing at rib 15, left and right wing, in accordance with the Accomplishment Instructions of British Aerospace BAC 1-11 Service Bulletin 57-PM5856, Revision 1, dated March 30, 1983. B. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. This amendment becomes effective December 20, 1983. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_83-24-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-24-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes Subject: Aileron Stub Fairing Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/20/1983 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: 83-24-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4778 AD NUMBER: 83-24-07 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective December 20, 1983. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-24-07 BRITISH AEROSPACE: Amendment 39-4778. Applies to Model BAC 1-11 200 and 400 series airplanes, certificated in all categories. Compliance is required as indicated. To prevent possible loss of roll control, accomplish the following within the next 30 days after the effective date of this AD, unless previously accomplished: A. Modify the aileron stub fairing installation attached to the outboard side of the fixed flap track center fairing at rib 15, left and right wing, in accordance with the Accomplishment Instructions of British Aerospace BAC 1-11 Service Bulletin 57-PM5856, Revision 1, dated March 30, 1983. B. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. This amendment becomes effective December 20, 1983. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.