AD 75-07-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-30 Series Airplanes |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-30 Series Airplanes |
Unsafe Condition
Installation of Autothrottle/Speed Control Computer Part Number 2593342-910C could lead to unreliable operation of the autothrottle system, resulting in potential loss of thrust control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Do not install Autothrottle/Speed Control Computer Part Number 2593342-910C. Refer to McDonnell Douglas Service Bulletin No. 22-67 dated February 21, 1975 or later FAA-approved revision for compliance.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
After the effective date of this airworthiness directive
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
MCDONNELL DOUGLAS DC-10-30 series airplanes, including DC-10-30, DC-10-30F (KC-10A, KDC-10), certificated in all categories.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Autothrottle/Speed Control
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_75-07-12.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-07-12 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; MCDONNELL DOUGLAS DC-10-30 Series Airplanes Subject: Autothrottle/Speed Control Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/07/1975 Make: The Boeing Company Model: DC-10-30 | DC-10-30F (KC-10A, KDC-10) Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-07-12 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2151 AD NUMBER: 75-07-12 SUBJECT HEADING: Airworthiness Directives; MCDONNELL DOUGLAS DC-10-30 Series Airplanes ACTION: SUMMARY: DATES: Effective April 7, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-07-12 MCDONNELL DOUGLAS: Amendment 39-2151. Applies to all Douglas Aircraft Company DC-10-30 series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished. After the effective date of this airworthiness directive do not install Autothrottle/Speed Control Computer Part Number 2593342-910C. Note: Refer to paragraph 2 of McDonnell Douglas DC-10 Service Bulletin No. 22-67 dated February 21, 1975 or later FAA-approved revision. This amendment becomes effective April 7, 1975. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_75-07-12.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-07-12 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; MCDONNELL DOUGLAS DC-10-30 Series Airplanes Subject: Autothrottle/Speed Control Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/07/1975 Make: The Boeing Company Model: DC-10-30 | DC-10-30F (KC-10A, KDC-10) 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: 75-07-12 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2151 AD NUMBER: 75-07-12 SUBJECT HEADING: Airworthiness Directives; MCDONNELL DOUGLAS DC-10-30 Series Airplanes ACTION: SUMMARY: DATES: Effective April 7, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-07-12 MCDONNELL DOUGLAS: Amendment 39-2151. Applies to all Douglas Aircraft Company DC-10-30 series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished. After the effective date of this airworthiness directive do not install Autothrottle/Speed Control Computer Part Number 2593342-910C. Note: Refer to paragraph 2 of McDonnell Douglas DC-10 Service Bulletin No. 22-67 dated February 21, 1975 or later FAA-approved revision. This amendment becomes effective April 7, 1975. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.