AD 86-04-03
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
The latent failure of the monitoring circuit of the antiskid system could lead to potential operational hazards.
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Required Actions
Within 3,000 flight hours after the effective date, and every 3,000 flight hours thereafter, perform a parking brake shut-off valve monitoring circuitry test per DC-10 Maintenance Manual Section 32-45-05. Optional modifications include installing a parking brake valve fault isolation relay per SB 32-155 and revising antiskid control wiring per SB 32-155 or SB 32-198.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 3,000 flight hours after the effective date of this AD, and thereafter at intervals not to exceed 3,000 flight hours
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas DC-10 and KC-10A (Military) series airplanes listed in Service Bulletins 32-155 (Rev 2) and 32-198.
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Federal Register Abstract
Brake Anti-Skid System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_86-04-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-04-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes Subject: Brake Anti-Skid System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/13/1986 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: 86-04-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5227 AD NUMBER: 86-04-03 SUBJECT HEADING: Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes ACTION: SUMMARY: DATES: Effective March 13, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-04-03 MCDONNELL DOUGLAS: Amendment 39-5227. Applies to Model DC-10 and KC-10A (Military) series airplanes, certificated in any category, which are listed in McDonnell Douglas DC-10 Service Bulletin 32-155, Revision 2, dated July 28, 1983, and Service Bulletin 32-198 dated January 17, 1984. Compliance required as indicated, unless previously accomplished. To minimize the potential operational hazard associated with the latent failure of the monitoring circuit of the antiskid system, accomplish the following: A. Within the next 3,000 flight hours after the effective date of this AD, and thereafter at intervals not to exceed 3,000 flight hours, accomplish a parking brake shut-off valve monitoring circuitry test in accordance with McDonnell Douglas DC-10 Maintenance Manual Section 32-45-05. B. Modifications listed below in paragraphs C. and D. are optional and constitute terminating action for this AD when incorporated. C. Install a parking brake valve fault isolation relay in accordance with McDonnell Douglas DC-10 Service Bulletin 32-155, Revision 2, dated July 28, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. D. Revise the antiskid control wiring in accordance with McDonnell Douglas DC-10 Service Bulletin 32-155, Revision 2, dated July 28, 1983, or Service Bulletin 32-198, dated January 17, 1984, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. E. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. F. 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 proposal who have not already received the appropriate service 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 13, 1986. FOOTER:
Document Text
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AD Final Rules - DRS_86-04-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-04-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes Subject: Brake Anti-Skid System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/13/1986 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: 86-04-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5227 AD NUMBER: 86-04-03 SUBJECT HEADING: Airworthiness Directives; MCDONNELL DOUGLAS DC-10 and KC-10A (Military) Series Airplanes ACTION: SUMMARY: DATES: Effective March 13, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-04-03 MCDONNELL DOUGLAS: Amendment 39-5227. Applies to Model DC-10 and KC-10A (Military) series airplanes, certificated in any category, which are listed in McDonnell Douglas DC-10 Service Bulletin 32-155, Revision 2, dated July 28, 1983, and Service Bulletin 32-198 dated January 17, 1984. Compliance required as indicated, unless previously accomplished. To minimize the potential operational hazard associated with the latent failure of the monitoring circuit of the antiskid system, accomplish the following: A. Within the next 3,000 flight hours after the effective date of this AD, and thereafter at intervals not to exceed 3,000 flight hours, accomplish a parking brake shut-off valve monitoring circuitry test in accordance with McDonnell Douglas DC-10 Maintenance Manual Section 32-45-05. B. Modifications listed below in paragraphs C. and D. are optional and constitute terminating action for this AD when incorporated. C. Install a parking brake valve fault isolation relay in accordance with McDonnell Douglas DC-10 Service Bulletin 32-155, Revision 2, dated July 28, 1983, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. D. Revise the antiskid control wiring in accordance with McDonnell Douglas DC-10 Service Bulletin 32-155, Revision 2, dated July 28, 1983, or Service Bulletin 32-198, dated January 17, 1984, or later revisions approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. E. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. F. 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 proposal who have not already received the appropriate service 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 13, 1986. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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