AD 67-19-02
final rule
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
Honeycomb delamination on moveable control surfaces and tabs, leading to skin separation from honeycomb structure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Tap test all control surfaces and tabs for delamination per BAC Alert Service Bulletin No. 55/57-A-PM 2597. Inspect at intervals not exceeding 300 hours' time in service if delamination is within limits. Repair or replace surfaces with delamination exceeding limits before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 600 hours' time in service after the effective date for airplanes with 1000+ hours, or before 1500 hours' time in service for those with less than 1000 hours as of the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
British Aircraft Corporation Model BAC 1-11, 200 and 400 Series Airplanes.
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Federal Register Abstract
Honeycomb Delamination
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-19-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-19-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11, 200 and 400 Series Airplanes Subject: Honeycomb Delamination Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/10/1967 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Model: BAC 1-11 200 Series | BAC 1-11 400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 67-19-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-434 AD NUMBER: 67-19-02 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11, 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective July 10, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-19-02 BRITISH AIRCRAFT: Amdt. 39-434, Part 39, Federal Register June 10, 1967. Applies to British Aircraft Corporation Model BAC 1-11, 200 and 400 Series Airplanes. Compliance required as indicated, unless already accomplished. To detect honeycomb delamination on all moveable control surfaces and tabs, accomplish the following: (a) Within the next 600 hours' time in service after the effective date of this AD for airplanes with 1000 or more hours' time in service, or for airplanes with less than 1000 hours' time in service as of the effective date of this AD before the accumulation of 1500 hours' time in service, tap test all control surfaces and tabs for evidence of delamination of the skin from the honeycomb structure in accordance with British Aircraft Corporation Alert Service Bulletin No. 55/57-A-PM 2597, dated September 19, 1966, or later ARB-approved issue. (b) If the control surfaces with delamination are within the permissible limits specified in BAC Structural Repair Manual, they may remain in service, but must be inspected in accordance with paragraph (a) at intervals not to exceed 300 hours' time in service from the date of the last inspection. (c) Control surfaces with delaminations exceeding the permissible limits as specified in BAC Structural Repair Manual, must be repaired or replaced, before further flight, in accordance with this Structural Repair Manual, or later ARB-approved issue, or FAA-approved equivalent. This amendment effective July 10, 1967. FOOTER:
Document Text
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AD Final Rules - DRS_67-19-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-19-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11, 200 and 400 Series Airplanes Subject: Honeycomb Delamination Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/10/1967 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: 67-19-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-434 AD NUMBER: 67-19-02 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11, 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective July 10, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-19-02 BRITISH AIRCRAFT: Amdt. 39-434, Part 39, Federal Register June 10, 1967. Applies to British Aircraft Corporation Model BAC 1-11, 200 and 400 Series Airplanes. Compliance required as indicated, unless already accomplished. To detect honeycomb delamination on all moveable control surfaces and tabs, accomplish the following: (a) Within the next 600 hours' time in service after the effective date of this AD for airplanes with 1000 or more hours' time in service, or for airplanes with less than 1000 hours' time in service as of the effective date of this AD before the accumulation of 1500 hours' time in service, tap test all control surfaces and tabs for evidence of delamination of the skin from the honeycomb structure in accordance with British Aircraft Corporation Alert Service Bulletin No. 55/57-A-PM 2597, dated September 19, 1966, or later ARB-approved issue. (b) If the control surfaces with delamination are within the permissible limits specified in BAC Structural Repair Manual, they may remain in service, but must be inspected in accordance with paragraph (a) at intervals not to exceed 300 hours' time in service from the date of the last inspection. (c) Control surfaces with delaminations exceeding the permissible limits as specified in BAC Structural Repair Manual, must be repaired or replaced, before further flight, in accordance with this Structural Repair Manual, or later ARB-approved issue, or FAA-approved equivalent. This amendment effective July 10, 1967. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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