AD 84-06-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2-1A | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B2-1C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B2-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B2K-3C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B4-103 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B4-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
| aircraft | Airbus | A300 B4-2C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes |
Unsafe Condition
Failure of the flap and slat control linkages
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect, repair, and modify the slat and flap linkages in accordance with specified service bulletins. Alternate means of compliance may be used if approved. Special flight permits may be issued under FAR 21.197 and 21.199.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 120 days after the effective date of this AD or upon reaching the landing thresholds specified in the service bulletins, whichever occurs later
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Affected Aircraft
AIRBUS INDUSTRIE Model A300 B2 and B4 series airplanes, including A300 B2-1A, B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C, certificated in all categories
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Slat and Flap Linkages
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_84-06-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-06-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes Subject: Slat and Flap Linkages Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/14/1984 Make: Airbus Model: A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C | A300 B4-103 | A300 B4-203 | A300 B4-2C 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: 84-06-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4832 AD NUMBER: 84-06-01 SUBJECT HEADING: Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes ACTION: SUMMARY: DATES: Effective May 14, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-06-01 AIRBUS INDUSTRIE: Amendment 39-4832. Applies to Model A300 B2 and B4 series airplanes, certificated in all categories. To prevent failure of the flap and slat control linkages, within 120 days after the effective date of this AD or upon reaching the landing thresholds specified in the service bulletins, whichever occurs later, accomplish the following, unless previously accomplished: A. Inspect, repair, and modify, as necessary, the slat and flap linkages in accordance with the service bulletins listed below: Airbus Industrie A300-27-151, Revision 4, dated December 20, 1982; Airbus Industrie A300-27-159, Revision 2, dated December 20, 1982; Airbus Industrie A300-27-158, Revision 1, dated March 9, 1982; Airbus Industrie A300-27-101, Revision 2, dated March 2, 1982; Lucas Aerospace 704-27-599, Revision 1, dated September 25, 1981; Lucas Aerospace 704-27-1053, Revision 1, dated October 11, 1982; and Lucas Aerospace 704-27-602, Revision 1, dated November 27, 1981. 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 May 14, 1984. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_84-06-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-06-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes Subject: Slat and Flap Linkages Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/14/1984 Make: Airbus Model: A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C | A300 B4-103 | A300 B4-203 | A300 B4-2C 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: 84-06-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4832 AD NUMBER: 84-06-01 SUBJECT HEADING: Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes ACTION: SUMMARY: DATES: Effective May 14, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-06-01 AIRBUS INDUSTRIE: Amendment 39-4832. Applies to Model A300 B2 and B4 series airplanes, certificated in all categories. To prevent failure of the flap and slat control linkages, within 120 days after the effective date of this AD or upon reaching the landing thresholds specified in the service bulletins, whichever occurs later, accomplish the following, unless previously accomplished: A. Inspect, repair, and modify, as necessary, the slat and flap linkages in accordance with the service bulletins listed below: Airbus Industrie A300-27-151, Revision 4, dated December 20, 1982; Airbus Industrie A300-27-159, Revision 2, dated December 20, 1982; Airbus Industrie A300-27-158, Revision 1, dated March 9, 1982; Airbus Industrie A300-27-101, Revision 2, dated March 2, 1982; Lucas Aerospace 704-27-599, Revision 1, dated September 25, 1981; Lucas Aerospace 704-27-1053, Revision 1, dated October 11, 1982; and Lucas Aerospace 704-27-602, Revision 1, dated November 27, 1981. 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 May 14, 1984. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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