AD 67-07-03

final rule

Airworthiness Directives; DOUGLAS DC-9 Airplanes

AD Number
67-07-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
(Federal Register: March 2, 1967)

Applicability

TypeManufacturerModelDetails
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
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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

Show stored source text (verify against official source)
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:

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.