AD 86-07-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 757-200 Series | BOEING Model 757 Airplanes |
| aircraft | The Boeing Company | 757-200CB Series | BOEING Model 757 Airplanes |
| aircraft | The Boeing Company | 757-200PF Series | BOEING Model 757 Airplanes |
| aircraft | The Boeing Company | 757-300 Series | BOEING Model 757 Airplanes |
Unsafe Condition
Improper engagement of the upper pinch bolt on left and right side Number 1, 2, and 4 passenger doors could result in door opening failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the left and right side Number 1, 2, and 4 passenger doors to verify proper engagement of the upper pinch bolt, and reinstall if necessary in accordance with Boeing Service Bulletin 757-52A0019 or later FAA-approved revisions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 30 days after the effective date of this amendment
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 757 airplanes, line numbers 1 through 90, certificated in any category
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Passenger Doors
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_86-07-11.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-07-11 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 757 Airplanes Subject: Passenger Doors Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/28/1986 Make: The Boeing Company Model: 757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 86-07-11 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5285 AD NUMBER: 86-07-11 SUBJECT HEADING: BOEING Model 757 Airplanes ACTION: SUMMARY: DATES: Effective April 28, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-07-11 BOEING: Amendment 39-5285. Applies to Boeing Model 757 airplanes, line numbers 1 through 90, certificated in any category. Compliance is required within 30 days after the effective date of this amendment. To ensure proper door opening, accomplish the following, unless already accomplished: A. Inspect the left and right side Number 1, 2, and 4 passenger doors to verify proper engagement of the upper pinch bolt, and reinstall, if necessary, in accordance with Boeing Service Bulletin 757-52A0019, dated February 27, 1986, or later FAA-approved revisions. B. Alternate means of compliance or adjustment of 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. 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 April 28, 1986. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_86-07-11.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-07-11 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 757 Airplanes Subject: Passenger Doors Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/28/1986 Make: The Boeing Company Model: 757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 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: 86-07-11 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5285 AD NUMBER: 86-07-11 SUBJECT HEADING: BOEING Model 757 Airplanes ACTION: SUMMARY: DATES: Effective April 28, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-07-11 BOEING: Amendment 39-5285. Applies to Boeing Model 757 airplanes, line numbers 1 through 90, certificated in any category. Compliance is required within 30 days after the effective date of this amendment. To ensure proper door opening, accomplish the following, unless already accomplished: A. Inspect the left and right side Number 1, 2, and 4 passenger doors to verify proper engagement of the upper pinch bolt, and reinstall, if necessary, in accordance with Boeing Service Bulletin 757-52A0019, dated February 27, 1986, or later FAA-approved revisions. B. Alternate means of compliance or adjustment of 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. 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 April 28, 1986. 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.