AD 84-15-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes |
| aircraft | The Boeing Company | DC-10-15 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes |
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes |
| aircraft | The Boeing Company | DC-10-40 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes |
| aircraft | The Boeing Company | DC-10-40F | Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes |
Unsafe Condition
Chafing and improper routing of left-hand and right-hand wiring bundles beneath the cockpit glareshield could lead to electrical system failure.
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Required Actions
Inspect both left and right wiring bundles beneath the cockpit glareshield for chafing and proper routing per Douglas All Operators Letter 10-1759 and Service Sketch 3597. Repair chafed wires by replacement or methods in the DC-10 Maintenance Manual. Verify proper routing over the fluorescent light shroud as specified.
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Compliance Time
within 30 days after the effective date of this AD unless previously accomplished
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Affected Aircraft
McDonnell Douglas DC-10 and KC-10A (military) airplanes, certificated in all categories
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Federal Register Abstract
Wiring
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_84-15-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-15-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes Subject: Wiring Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/20/1984 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: 84-15-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4896 AD NUMBER: 84-15-06 SUBJECT HEADING: Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes ACTION: SUMMARY: DATES: Effective August 20, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-15-06 McDONNELL DOUGLAS: Amendment 39-4896. Applies to McDonnell Douglas DC-10 and KC-10A (military) airplanes, certificated in all categories. Compliance required within 30 days after the effective date of this AD unless previously accomplished. To determine wire harness condition and ensure proper wire routing, accomplish the following: A. Inspect both the left-hand and right-hand wiring bundles beneath the cockpit glareshield for chafing and proper routing in accordance with Douglas All Operators Letter 10-1759, dated May 30, 1984, and Service Sketch 3597. B. Repair all chafed wires by replacement or use of methods outlined in the Douglas DC-10 Maintenance Manual. C. Verify proper routing of both the left-hand and right-hand wire bundles beneath the cockpit glareshield over the fluorescent light shroud in accordance with Douglas All Operators Letter 10-1759, dated May 30, 1984, and Service Sketch 3597. D. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. E. 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. All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to 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 the Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California. This amendment becomes effective August 20, 1984. FOOTER:
Document Text
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AD Final Rules - DRS_84-15-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-15-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes Subject: Wiring Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/20/1984 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: 84-15-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4896 AD NUMBER: 84-15-06 SUBJECT HEADING: Airworthiness Directives; McDONNELL DOUGLAS DC-10 and KC-10A (military) Airplanes ACTION: SUMMARY: DATES: Effective August 20, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-15-06 McDONNELL DOUGLAS: Amendment 39-4896. Applies to McDonnell Douglas DC-10 and KC-10A (military) airplanes, certificated in all categories. Compliance required within 30 days after the effective date of this AD unless previously accomplished. To determine wire harness condition and ensure proper wire routing, accomplish the following: A. Inspect both the left-hand and right-hand wiring bundles beneath the cockpit glareshield for chafing and proper routing in accordance with Douglas All Operators Letter 10-1759, dated May 30, 1984, and Service Sketch 3597. B. Repair all chafed wires by replacement or use of methods outlined in the Douglas DC-10 Maintenance Manual. C. Verify proper routing of both the left-hand and right-hand wire bundles beneath the cockpit glareshield over the fluorescent light shroud in accordance with Douglas All Operators Letter 10-1759, dated May 30, 1984, and Service Sketch 3597. D. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. E. 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. All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to 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 the Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California. This amendment becomes effective August 20, 1984. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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