AD 84-09-02
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
Breakage of the fuel and hydraulic line attaching clamps in the engine pylons could result in line breakage and a consequent fire hazard.
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Required Actions
Remove existing fuel and hydraulic line attaching clamps and brackets, install new reinforced teflon-lined clamps and redesigned brackets per Airbus Industrie Service Bulletin A300-54-007, Revision 5. Alternate means of compliance may be used if approved by the FAA.
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Compliance Time
within the next 750 hours time in service after the effective date of this AD
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Affected Aircraft
AIRBUS INDUSTRIE Model A300 B2 and B4 series airplanes, including specific models: A300 B2-1A, A300 B2-1C, A300 B2-203, A300 B2K-3C, A300 B4-103, A300 B4-203, A300 B4-2C.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Clamps and Brackets
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_84-09-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-09-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes Subject: Clamps and Brackets Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/01/1984 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: 84-09-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4853 AD NUMBER: 84-09-02 SUBJECT HEADING: Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes ACTION: SUMMARY: DATES: Effective June 1, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-09-02 AIRBUS INDUSTRIE: Amendment 39-4853. Applies to Model A300 B2 and B4 series airplanes, certificated in all categories. Compliance is required within the next 750 hours time in service after the effective date of this AD, unless already accomplished. To prevent breakage of the fuel and hydraulic line attaching clamps in the engine pylons, which could result in line breakage and a consequent fire hazard, accomplish the following: A. Remove the existing fuel and hydraulic line attaching clamps and brackets, and install new reinforced teflon-lined clamps and redesigned brackets in accordance with paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Airbus Industrie Service Bulletin A300-54-007, Revision 5, dated December 22, 1978. 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 June 1, 1984. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_84-09-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-09-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes Subject: Clamps and Brackets Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/01/1984 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: 84-09-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4853 AD NUMBER: 84-09-02 SUBJECT HEADING: Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2 and B4 Series Airplanes ACTION: SUMMARY: DATES: Effective June 1, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-09-02 AIRBUS INDUSTRIE: Amendment 39-4853. Applies to Model A300 B2 and B4 series airplanes, certificated in all categories. Compliance is required within the next 750 hours time in service after the effective date of this AD, unless already accomplished. To prevent breakage of the fuel and hydraulic line attaching clamps in the engine pylons, which could result in line breakage and a consequent fire hazard, accomplish the following: A. Remove the existing fuel and hydraulic line attaching clamps and brackets, and install new reinforced teflon-lined clamps and redesigned brackets in accordance with paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Airbus Industrie Service Bulletin A300-54-007, Revision 5, dated December 22, 1978. 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 June 1, 1984. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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