AD 67-27-03
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
Fatigue failures of the flap carriage links P/N AB09 A943 and post modification PM 2245 flap carriage links P/N AB09 A3657.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace carriage links P/N AB09 A943 with new links of the same part number or with P/N AB09 A3657 within specified landing intervals. For P/N AB09 A3657 links, replace with same part number or P/N AB09 A943 within specified landing intervals.
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Compliance Time
Within the next 500 landings after January 15, 1967, or before the accumulation of the number of landings specified in Column 2 or 3 for respective flap numbers and series, whichever occurs later, and thereafter at intervals not exceeding specified landings.
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Affected Aircraft
BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series airplanes equipped with flap carriage links P/N AB09 A943 or AB09 A3657.
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Federal Register Abstract
Flap Carriage Links
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-27-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-27-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes Subject: Flap Carriage Links Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 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Model: BAC 1-11 200 Series | BAC 1-11 400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 67-27-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-762 AD NUMBER: 67-27-03 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-27-03 BRITISH AIRCRAFT: Amendment 39-762. Applies to Model BAC 1-11 200 and 400 Series airplanes. Compliance required as indicated. To prevent fatigue failures of the flap carriage links P/N AB09 A943 and post modification PM 2245 flap carriage links P/N AB09 A3657, accomplish the following: (a) For airplanes equipped with carriage links P/N AB09 A943, within the next 500 landings after January 15, 1967, or before the accumulation of the number of landings specified in Column 2 or Column 3, as applicable, for the respective flap numbers specified in Column 1, whichever occurs later, and thereafter at intervals not to exceed the number of landings specified for that flap number and series of airplane, replace carriage links P/N AB09 A943 with new links of the same part number; or replace with carriage links P/N AB09 A3657. If carriage links P/N AB09 A3657 are used as replacements, they must be replaced in accordance with the requirements of paragraph (b). (Column 1) (Column 2) (Column 3) Flap No. Number of Landings Number of Landings (link location) 200 Series Airplanes 400 Series Airplanes 1 3,000 2,000 2 10,000 8,000 3 24,000 16,000 (b) For airplanes equipped with carriage links P/N AB09 A3657, within the next 300 landings after the effective date of this AD or before the accumulation of the number of landings specified in Column 2 or Column 3, as applicable, for the respective flap number specified in Column 1, whichever occurs later, and thereafter at intervals not to exceed the number of landings specified for that flap number and series of airplane, replace carriage links P/N AB09 A3657 with new links of the same part number, or replace with carriage links P/N AB09 A943. If carriage links P/N AB09 A943 are used as replacements, they must be replaced in accordance with the requirements of paragraph (a). (Column 1) (Column 2) (Column 3) Flap No. Number of Landings Number of Landings (link location) 200 Series Airplanes 400 Series Airplanes 1 4,000 3,000 2 12,000 10,000 3 32,000 24,000 FOOTER:
Document Text
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AD Final Rules - DRS_67-27-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-27-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes Subject: Flap Carriage Links Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 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: 67-27-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-762 AD NUMBER: 67-27-03 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-27-03 BRITISH AIRCRAFT: Amendment 39-762. Applies to Model BAC 1-11 200 and 400 Series airplanes. Compliance required as indicated. To prevent fatigue failures of the flap carriage links P/N AB09 A943 and post modification PM 2245 flap carriage links P/N AB09 A3657, accomplish the following: (a) For airplanes equipped with carriage links P/N AB09 A943, within the next 500 landings after January 15, 1967, or before the accumulation of the number of landings specified in Column 2 or Column 3, as applicable, for the respective flap numbers specified in Column 1, whichever occurs later, and thereafter at intervals not to exceed the number of landings specified for that flap number and series of airplane, replace carriage links P/N AB09 A943 with new links of the same part number; or replace with carriage links P/N AB09 A3657. If carriage links P/N AB09 A3657 are used as replacements, they must be replaced in accordance with the requirements of paragraph (b). (Column 1) (Column 2) (Column 3) Flap No. Number of Landings Number of Landings (link location) 200 Series Airplanes 400 Series Airplanes 1 3,000 2,000 2 10,000 8,000 3 24,000 16,000 (b) For airplanes equipped with carriage links P/N AB09 A3657, within the next 300 landings after the effective date of this AD or before the accumulation of the number of landings specified in Column 2 or Column 3, as applicable, for the respective flap number specified in Column 1, whichever occurs later, and thereafter at intervals not to exceed the number of landings specified for that flap number and series of airplane, replace carriage links P/N AB09 A3657 with new links of the same part number, or replace with carriage links P/N AB09 A943. If carriage links P/N AB09 A943 are used as replacements, they must be replaced in accordance with the requirements of paragraph (a). (Column 1) (Column 2) (Column 3) Flap No. Number of Landings Number of Landings (link location) 200 Series Airplanes 400 Series Airplanes 1 4,000 3,000 2 12,000 10,000 3 32,000 24,000 FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
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