AD 86-02-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | BOEING Model 767 Airplanes |
| aircraft | The Boeing Company | 767-300 Series | BOEING Model 767 Airplanes |
| aircraft | The Boeing Company | 767-300F Series | BOEING Model 767 Airplanes |
Unsafe Condition
Failure of the entry/service door operating mechanisms due to lack of integrity in the upper and lower pushrod installations could result in improper door opening.
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Required Actions
Inspect all entry/service door operating mechanisms for integrity of the upper and lower pushrod installations and repair if necessary, in accordance with Boeing Service Bulletin 767-52-0041 dated December 13, 1985, or later FAA-approved revisions. Alternate means of compliance may be used if approved by the FAA Manager, Seattle Aircraft Certification Office.
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Compliance Time
within 30 days after the effective date of this AD
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Affected Aircraft
Boeing Model 767-200 Series, 767-300 Series, 767-300F Series airplanes listed in Boeing Service Bulletin 767-52-0041 dated December 13, 1985
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Federal Register Abstract
Entry/Service Door Operating Mechanisms
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_86-02-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-02-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 767 Airplanes Subject: Entry/Service Door Operating Mechanisms Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/03/1986 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767-200 Series | 767-300 Series | 767-300F Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 86-02-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5214 AD NUMBER: 86-02-01 SUBJECT HEADING: BOEING Model 767 Airplanes ACTION: SUMMARY: DATES: Effective February 3, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-02-01 BOEING: Amendment 39-5214. Applies to Model 767 airplanes, as listed in Boeing Service Bulletin 767-52-0041, dated December 13, 1985, certificated in any category. Compliance is required within 30 days after the effective date of this AD. To ensure proper door opening, accomplish the following, unless already accomplished: A. Inspect all entry/service door operating mechanisms for integrity of the upper and lower pushrod installations and repair, if necessary, in accordance with Boeing Service Bulletin 767-52-0041 dated December 13, 1985, or later FAA-approved revisions. B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. All persons affected by this AD who have not already received copies of the service bulletin cited herein may obtain copies upon request from the Boeing Commercial Airplane Company, P. O. Box 3707, Seattle, Washington 98124. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This Amendment becomes effective February 3, 1986. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_86-02-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-02-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 767 Airplanes Subject: Entry/Service Door Operating Mechanisms Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/03/1986 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: 86-02-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5214 AD NUMBER: 86-02-01 SUBJECT HEADING: BOEING Model 767 Airplanes ACTION: SUMMARY: DATES: Effective February 3, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-02-01 BOEING: Amendment 39-5214. Applies to Model 767 airplanes, as listed in Boeing Service Bulletin 767-52-0041, dated December 13, 1985, certificated in any category. Compliance is required within 30 days after the effective date of this AD. To ensure proper door opening, accomplish the following, unless already accomplished: A. Inspect all entry/service door operating mechanisms for integrity of the upper and lower pushrod installations and repair, if necessary, in accordance with Boeing Service Bulletin 767-52-0041 dated December 13, 1985, or later FAA-approved revisions. B. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. All persons affected by this AD who have not already received copies of the service bulletin cited herein may obtain copies upon request from the Boeing Commercial Airplane Company, P. O. Box 3707, Seattle, Washington 98124. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This Amendment becomes effective February 3, 1986. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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