AD 89-24-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300 Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300F Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
Unsafe Condition
Binding of the pilot's control wheel due to the Aircraft Integrated Data System (AIDS) position transducer, crank assembly, and rod assembly.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Deactivate the control wheel AIDS by removing the position transducer, crank assembly, and rod assembly as per Boeing Alert Service Bulletin 767-31A0029. An alternate means of compliance or adjustment may be used if approved by the FAA Manager, Seattle Aircraft Certification Office.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 45 days after the effective date of this AD (December 1, 1989), unless previously accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BOEING Model 767-200 Series, 767-300 Series, 767-300F Series airplanes listed in Boeing Alert Service Bulletin 767-31A0029 dated March 23, 1989.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Aircraft Integrated Data System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_89-24-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-24-05 Document Type: AD Final Rules Docket Number: 89-NM-213-AD Subject Heading: Airworthiness Directives; BOEING Model 767 Series Airplanes Subject: Aircraft Integrated Data System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/01/1989 Make: The Boeing Company Model: 767-200 Series | 767-300 Series | 767-300F Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 89-24-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 89-NM-213-AD AMENDMENT: 39-6395 AD NUMBER: 89-24-05 SUBJECT HEADING: Airworthiness Directives; BOEING Model 767 Series Airplanes ACTION: SUMMARY: DATES: Effective December 1, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-24-05 BOEING: Amendment 39-6395. Docket No. 89-NM-213-AD. Applicability: Model 767 series airplanes, listed in Boeing Alert Service Bulletin 767- 31A0029, dated March 23, 1989, certificated in any category. Compliance: Required within 45 days after the effective date of this AD, unless previously accomplished. To prevent binding of the pilot's control wheel, accomplish the following: A. Deactivate the control wheel Aircraft Integrated Data System (AIDS) by removing the position transducer, crank assembly, and rod assembly in accordance with Boeing Alert Service Bulletin 767-31A0029, dated March 23, 1989. B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office. C. 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 directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment (39-6395, AD 89-24-05) becomes effective on December 1, 1989. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_89-24-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-24-05 Document Type: AD Final Rules Docket Number: 89-NM-213-AD Subject Heading: Airworthiness Directives; BOEING Model 767 Series Airplanes Subject: Aircraft Integrated Data System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 12/01/1989 Make: The Boeing Company Model: 767-200 Series | 767-300 Series | 767-300F Series 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: 89-24-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 89-NM-213-AD AMENDMENT: 39-6395 AD NUMBER: 89-24-05 SUBJECT HEADING: Airworthiness Directives; BOEING Model 767 Series Airplanes ACTION: SUMMARY: DATES: Effective December 1, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-24-05 BOEING: Amendment 39-6395. Docket No. 89-NM-213-AD. Applicability: Model 767 series airplanes, listed in Boeing Alert Service Bulletin 767- 31A0029, dated March 23, 1989, certificated in any category. Compliance: Required within 45 days after the effective date of this AD, unless previously accomplished. To prevent binding of the pilot's control wheel, accomplish the following: A. Deactivate the control wheel Aircraft Integrated Data System (AIDS) by removing the position transducer, crank assembly, and rod assembly in accordance with Boeing Alert Service Bulletin 767-31A0029, dated March 23, 1989. B. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office. C. 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 directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment (39-6395, AD 89-24-05) becomes effective on December 1, 1989. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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