AD 66-16-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 Series Airplanes |
Unsafe Condition
Chafing of the fuselage frame forward flange by the aft end of the headliner P/N AB77 A1605.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Rework the headliner P/N AB77 A1605, inspect the flange of fuselage frame P/N AB29 A501, and rework as necessary in accordance with BAC One-Eleven Alert Service Bulletin 53-A-PM 2107 or later ARB-approved issue.
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Compliance Time
Before the accumulation of 3,000 hours' time in service for airplanes with less than 2,900 hours' time in service on the effective date of this AD and within the next 100 hours' time in service after the effective date of this AD for airplanes with 2,900 or more hours' time in service on the effective date of this AD unless already accomplished.
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Affected Aircraft
BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 Series Airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Engine Mounting Fuselage Frame
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_66-16-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 66-16-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 Series Airplanes Subject: Engine Mounting Fuselage Frame Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/31/1966 Make: Airbus SAS Model: BAC 1-11 200 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 66-16-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-254 AD NUMBER: 66-16-02 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 Series Airplanes ACTION: SUMMARY: DATES: Effective July 31, 1966. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 66-16-02 BRITISH AIRCRAFT CORPORATION: Amdt. 39-254 Federal Register July 1, 1966. Applies to Model BAC 1-11 200 Series Airplanes. Compliance required before the accumulation of 3,000 hours' time in service for airplanes with less than 2,900 hours' time in service on the effective date of this AD and within the next 100 hours' time in service after the effective date of this AD for airplanes with 2,900 or more hours' time in service on the effective date of this AD unless already accomplished. To prevent chafing of the fuselage frame forward flange by the aft end of the headliner, rework the headliner, P/N AB77 A1605, and inspect the flange of fuselage frame, P/N AB29 A501, and rework as necessary in accordance with British Aircraft Corporation (BAC) One- Eleven Alert Service Bulletin 53-A-PM 2107, dated February 1, 1966, or later ARB-approved issue. This directive effective July 31, 1966. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_66-16-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 66-16-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 Series Airplanes Subject: Engine Mounting Fuselage Frame Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/31/1966 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: 66-16-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-254 AD NUMBER: 66-16-02 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 Series Airplanes ACTION: SUMMARY: DATES: Effective July 31, 1966. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 66-16-02 BRITISH AIRCRAFT CORPORATION: Amdt. 39-254 Federal Register July 1, 1966. Applies to Model BAC 1-11 200 Series Airplanes. Compliance required before the accumulation of 3,000 hours' time in service for airplanes with less than 2,900 hours' time in service on the effective date of this AD and within the next 100 hours' time in service after the effective date of this AD for airplanes with 2,900 or more hours' time in service on the effective date of this AD unless already accomplished. To prevent chafing of the fuselage frame forward flange by the aft end of the headliner, rework the headliner, P/N AB77 A1605, and inspect the flange of fuselage frame, P/N AB29 A501, and rework as necessary in accordance with British Aircraft Corporation (BAC) One- Eleven Alert Service Bulletin 53-A-PM 2107, dated February 1, 1966, or later ARB-approved issue. This directive effective July 31, 1966. FOOTER:
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