AD 93-15-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | MD-11 | Airworthiness Directives; MCDONNELL DOUGLAS MD-11 Series Airplanes |
| aircraft | The Boeing Company | MD-11F | Airworthiness Directives; MCDONNELL DOUGLAS MD-11 Series Airplanes |
Unsafe Condition
Inadvertent slat deployment during flight at cruise altitude.
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Required Actions
Install a retainer assembly on the upper pedestal flap/slat control module quadrant in the flight compartment within 15 days after the effective date of this AD, in accordance with McDonnell Douglas MD-11 Alert Service Bulletin A27-38. Alternative methods of compliance or adjustments to the compliance time may be approved by the Manager, Los Angeles Aircraft Certification Office.
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Compliance Time
Within 15 days after the effective date of this AD
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Affected Aircraft
Model MD-11 series airplanes; fuselage numbers 447 through 546 inclusive; certificated in any category.
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Federal Register Abstract
Slat Control Module
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_93-15-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 93-15-03 Document Type: AD Final Rules Docket Number: 93-NM-114-AD Subject Heading: Airworthiness Directives; MCDONNELL DOUGLAS MD-11 Series Airplanes Subject: Slat Control Module Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/04/1993 Make: The Boeing Company Model: MD-11 | MD-11F Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 93-15-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 93-NM-114-AD AMENDMENT: 39-8649 AD NUMBER: 93-15-03 SUBJECT HEADING: Airworthiness Directives; MCDONNELL DOUGLAS MD-11 Series Airplanes ACTION: SUMMARY: DATES: Effective August 4, 1993. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 93-15-03 MCDONNELL DOUGLAS: Amendment 39-8649. Docket 93-NM-114-AD. Applicability: Model MD-11 series airplanes; fuselage numbers 447 through 546 inclusive; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent inadvertent slat deployment during flight at cruise altitude, accomplish the following: (a) Within 15 days after the effective date of this AD, install a retainer assembly on the upper pedestal flap/slat control module quadrant in the flight compartment, in accordance with McDonnell Douglas MD-11 Alert Service Bulletin A27-38, dated July 8, 1993. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Los Angeles ACO. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO. (c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. (d) The installation shall be done in accordance with McDonnell Douglas MD-11 Alert Service Bulletin A27-38, dated July 8, 1993. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from McDonnell Douglas Corporation, P.O. Box 1771, Long Beach, California 90801-1771, Attention: Business Unit Manager, Technical Publications - Technical Administrative Support, C1-L5B. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Transport Airplane Directorate, Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment becomes effective on August 4, 1993. FOOTER:
Document Text
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AD Final Rules - DRS_93-15-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 93-15-03 Document Type: AD Final Rules Docket Number: 93-NM-114-AD Subject Heading: Airworthiness Directives; MCDONNELL DOUGLAS MD-11 Series Airplanes Subject: Slat Control Module Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/04/1993 Make: The Boeing Company Model: MD-11 | MD-11F 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: 93-15-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 93-NM-114-AD AMENDMENT: 39-8649 AD NUMBER: 93-15-03 SUBJECT HEADING: Airworthiness Directives; MCDONNELL DOUGLAS MD-11 Series Airplanes ACTION: SUMMARY: DATES: Effective August 4, 1993. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 93-15-03 MCDONNELL DOUGLAS: Amendment 39-8649. Docket 93-NM-114-AD. Applicability: Model MD-11 series airplanes; fuselage numbers 447 through 546 inclusive; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent inadvertent slat deployment during flight at cruise altitude, accomplish the following: (a) Within 15 days after the effective date of this AD, install a retainer assembly on the upper pedestal flap/slat control module quadrant in the flight compartment, in accordance with McDonnell Douglas MD-11 Alert Service Bulletin A27-38, dated July 8, 1993. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Los Angeles Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Los Angeles ACO. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Los Angeles ACO. (c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. (d) The installation shall be done in accordance with McDonnell Douglas MD-11 Alert Service Bulletin A27-38, dated July 8, 1993. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from McDonnell Douglas Corporation, P.O. Box 1771, Long Beach, California 90801-1771, Attention: Business Unit Manager, Technical Publications - Technical Administrative Support, C1-L5B. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Transport Airplane Directorate, Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment becomes effective on August 4, 1993. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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