AD 84-02-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes |
| aircraft | The Boeing Company | DC-10-15 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes |
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes |
| aircraft | The Boeing Company | DC-10-40 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes |
| aircraft | The Boeing Company | DC-10-40F | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes |
Unsafe Condition
Chafing and electrical arcing in fuel tank pump electrical conduits.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install teflon tubing in all aft fuel tank pump harness conduits (main tank aft pumps and center wing tank pumps) in accordance with Service Bulletin 24-123. Install teflon tubing in all remaining fuel tank pump harness conduits following the same service bulletin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 20,000 hours time in service, or within the next 4000 hours time in service, or one year after the effective date of this AD, whichever occurs later for part A. For part B, prior to 30,000 hours time in service, or within the next 4000 hours time in service, or one year after the effective date of this AD, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas Model DC-10 and KC-10A (Military) series airplanes, certificated in all categories.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fuel Tank Pump Conduits
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_84-02-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-02-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes Subject: Fuel Tank Pump Conduits Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/02/1984 Make: The Boeing Company Model: DC-10-10 | DC-10-10F | DC-10-15 | DC-10-30 | DC-10-30F (KC-10A, KDC-10) | DC-10-40 | DC-10-40F 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: 84-02-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4799 AD NUMBER: 84-02-06 SUBJECT HEADING: Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes ACTION: SUMMARY: DATES: Effective March 2, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-02-06 McDONNELL DOUGLAS: Amendment 39-4799. Applies to McDonnell Douglas Model DC-10 and KC-10A (Military) series airplanes, certificated in all categories. Compliance required as indicated, unless previously accomplished. To prevent chafing and electrical arcing in fuel tank pump electrical conduits, accomplish the following: A. Prior to the accumulation of 20,000 hours time in service, or within the next 4000 hours time in service, or one year after the effective date of this AD, whichever occurs later, install teflon tubing in all aft fuel tank pump harness conduits (main tank aft pumps and center wing tank pumps) in accordance with the Accomplishment Instructions in McDonnell Douglas DC-10 Service Bulletin 24-123, Revision 1, dated November 22, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. B. Prior to the accumulation of 30,000 hours time in service, or within the next 4000 hours time in service, or one year after the effective date of this AD, whichever occurs later, install teflon tubing in all remaining fuel tank pump harness conduits in accordance with the Accomplishment Instructions in McDonnell Douglas DC-10 Service Bulletin 24-123, Revision 1, dated November 22, 1983, or later revisions approved by the Manager, Los Angeles 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 in order to comply with the requirements of this AD. D. Alternate means of compliance providing an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. All persons affected by this amendment who have not already received these documents from the manufacturer may obtain copies upon request to the McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington or at 4344 Donald Douglas Drive, Long Beach, California. This amendment becomes effective March 2, 1984. FOOTER:
Document Text
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AD Final Rules - DRS_84-02-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-02-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes Subject: Fuel Tank Pump Conduits Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/02/1984 Make: The Boeing Company Model: DC-10-10 | DC-10-10F | DC-10-15 | DC-10-30 | DC-10-30F (KC-10A, KDC-10) | DC-10-40 | DC-10-40F 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: 84-02-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4799 AD NUMBER: 84-02-06 SUBJECT HEADING: Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes ACTION: SUMMARY: DATES: Effective March 2, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-02-06 McDONNELL DOUGLAS: Amendment 39-4799. Applies to McDonnell Douglas Model DC-10 and KC-10A (Military) series airplanes, certificated in all categories. Compliance required as indicated, unless previously accomplished. To prevent chafing and electrical arcing in fuel tank pump electrical conduits, accomplish the following: A. Prior to the accumulation of 20,000 hours time in service, or within the next 4000 hours time in service, or one year after the effective date of this AD, whichever occurs later, install teflon tubing in all aft fuel tank pump harness conduits (main tank aft pumps and center wing tank pumps) in accordance with the Accomplishment Instructions in McDonnell Douglas DC-10 Service Bulletin 24-123, Revision 1, dated November 22, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. B. Prior to the accumulation of 30,000 hours time in service, or within the next 4000 hours time in service, or one year after the effective date of this AD, whichever occurs later, install teflon tubing in all remaining fuel tank pump harness conduits in accordance with the Accomplishment Instructions in McDonnell Douglas DC-10 Service Bulletin 24-123, Revision 1, dated November 22, 1983, or later revisions approved by the Manager, Los Angeles 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 in order to comply with the requirements of this AD. D. Alternate means of compliance providing an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. All persons affected by this amendment who have not already received these documents from the manufacturer may obtain copies upon request to the McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington or at 4344 Donald Douglas Drive, Long Beach, California. This amendment becomes effective March 2, 1984. FOOTER:
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