AD 67-07-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-9-11 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-12 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-13 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-14 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-15 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-15F | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-21 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-31 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-32 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-32 (VC-9C) | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-32F | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-32F (C-9A) | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-32F (C-9B) | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-33F | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-34 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-34F | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-41 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-51 | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-81 (MD-81) | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-82 (MD-82) | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-83 (MD-83) | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
| aircraft | The Boeing Company | DC-9-87 (MD-87) | Airworthiness Directives; DOUGLAS DC-9 Airplanes |
Unsafe Condition
The autopilot may not disengage when the control wheel disconnect button is used.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install a placard in clear view of the pilot with specific instructions. The placard may be removed if Sperry SP-50A autopilot control panel switches are reworked to Sperry Service Bulletin TA-693-37.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to completing the next 50 hours' time in service (for panels with 1,500+ hours) or prior to completing 1,550 hours' total time in service (for panels with less than 1,500 hours).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Douglas DC-9 Airplanes equipped with the Sperry SP-50A Autopilot, including models DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, and others as listed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Sperry SP-50 Autopilot
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-07-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-07-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; DOUGLAS DC-9 Airplanes Subject: Sperry SP-50 Autopilot Status: Current Citation: (Federal Register: March 2, 1967) Citation Publish Date: 03/02/1967 Effective Date: 03/02/1967 Make: The Boeing Company Model: DC-9-11 | DC-9-12 | DC-9-13 | DC-9-14 | DC-9-15 | DC-9-15F | DC-9-21 | DC-9-31 | DC-9-32 | DC-9-32 (...Show more 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: 67-07-03 CITATION: [Federal Register: March 2, 1967] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-356 AD NUMBER: 67-07-03 SUBJECT HEADING: Airworthiness Directives; DOUGLAS DC-9 Airplanes ACTION: SUMMARY: DATES: Effective March 2, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-07-03 DOUGLAS: Amdt. 39-356 Part 39 Federal Register March 2, 1967. Applies to Model DC-9 Airplanes Equipped With the Sperry SP-50A Autopilot. Compliance required as indicated unless already accomplished. To prevent an unsafe condition which may result when the autopilot does not disengage when the control wheel disconnect button is used, accomplish the following: (a) For airplanes having Sperry SP-50A autopilot control panels with 1,500 or more hours' time in service on the effective date of this AD, comply with (d) prior to completing the next 50 hours' time in service. (b) For airplanes having Sperry SP-50A autopilot control panels with less than 1,500 hours' time in service on the effective date of this AD, comply with (d) prior to completing 1,550 hours' total time in service. (c) Operators who have not kept records of hours' time in service of individual Sperry SP-50A autopilot control panels shall substitute hours' time in service for the airplane or airplanes in which the individual autopilot control panel was installed. (d) Install a placard in clear view of the pilot with the following information: Autopilot(s) must be turned off when operating below 3,000 feet above ground level in a terminal area. Verify by position of the control panel engage lever. (e) The placard installed in accordance with (d) may be removed when the Sperry SP- 50A autopilot control panel switches have been reworked to Sperry Service Bulletin TA-693-37. This directive effective March 2, 1967. FOOTER:
Document Text
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AD Final Rules - DRS_67-07-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-07-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; DOUGLAS DC-9 Airplanes Subject: Sperry SP-50 Autopilot Status: Current Citation: (Federal Register: March 2, 1967) Citation Publish Date: 03/02/1967 Effective Date: 03/02/1967 Make: The Boeing Company Model: DC-9-11 | DC-9-12 | DC-9-13 | DC-9-14 | DC-9-15 | DC-9-15F | DC-9-21 | DC-9-31 | DC-9-32 | DC-9-32 (...Show more 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: 67-07-03 CITATION: [Federal Register: March 2, 1967] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-356 AD NUMBER: 67-07-03 SUBJECT HEADING: Airworthiness Directives; DOUGLAS DC-9 Airplanes ACTION: SUMMARY: DATES: Effective March 2, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-07-03 DOUGLAS: Amdt. 39-356 Part 39 Federal Register March 2, 1967. Applies to Model DC-9 Airplanes Equipped With the Sperry SP-50A Autopilot. Compliance required as indicated unless already accomplished. To prevent an unsafe condition which may result when the autopilot does not disengage when the control wheel disconnect button is used, accomplish the following: (a) For airplanes having Sperry SP-50A autopilot control panels with 1,500 or more hours' time in service on the effective date of this AD, comply with (d) prior to completing the next 50 hours' time in service. (b) For airplanes having Sperry SP-50A autopilot control panels with less than 1,500 hours' time in service on the effective date of this AD, comply with (d) prior to completing 1,550 hours' total time in service. (c) Operators who have not kept records of hours' time in service of individual Sperry SP-50A autopilot control panels shall substitute hours' time in service for the airplane or airplanes in which the individual autopilot control panel was installed. (d) Install a placard in clear view of the pilot with the following information: Autopilot(s) must be turned off when operating below 3,000 feet above ground level in a terminal area. Verify by position of the control panel engage lever. (e) The placard installed in accordance with (d) may be removed when the Sperry SP- 50A autopilot control panel switches have been reworked to Sperry Service Bulletin TA-693-37. This directive effective March 2, 1967. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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