AD 86-09-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 757-200 Series | BOEING Model 757-200 Airplanes |
Unsafe Condition
Failure of the slide pack release cable assemblies on Doors No. 1 and No. 2 could result in improper door opening and escape slide deployment.
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Required Actions
Modify slide pack release cable assemblies on Doors No. 1 and No. 2, left and right, per Boeing Service Bulletin 757-25A0058 or later FAA-approved revisions. An alternate means of compliance or adjustment may be approved by the Manager, Seattle Aircraft Certification Office.
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Compliance Time
within 45 days after the effective date of this amendment
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Affected Aircraft
Boeing Model 757-200 airplanes listed in Boeing Service Bulletin 757-25A0058 dated April 18, 1986
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Federal Register Abstract
Slide Pack Release Cable Assemblies
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_86-09-09.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-09-09 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 757-200 Airplanes Subject: Slide Pack Release Cable Assemblies Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/30/1986 Make: The Boeing Company Model: 757-200 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 86-09-09 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5304 AD NUMBER: 86-09-09 SUBJECT HEADING: BOEING Model 757-200 Airplanes ACTION: SUMMARY: DATES: Effective May 30, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-09-09 BOEING: Amendment 39-5304. Applies to Boeing Model 757-200 airplanes, listed in Boeing Service Bulletin 757-25A0058, dated April 18, 1986, certificated in any category. Compliance required within 45 days after the effective date of this amendment, unless already accomplished. To ensure proper door opening and escape slide deployment accomplish the following: A. Modify slide pack release cable assemblies on Doors No. 1 and No. 2, left and right, in accordance with Boeing Service Bulletin 757-25A0058, dated April 18, 1986, or later FAA-approved revisions. 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. 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 May 30, 1986. FOOTER:
Document Text
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AD Final Rules - DRS_86-09-09.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-09-09 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 757-200 Airplanes Subject: Slide Pack Release Cable Assemblies Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/30/1986 Make: The Boeing Company Model: 757-200 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: 86-09-09 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5304 AD NUMBER: 86-09-09 SUBJECT HEADING: BOEING Model 757-200 Airplanes ACTION: SUMMARY: DATES: Effective May 30, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-09-09 BOEING: Amendment 39-5304. Applies to Boeing Model 757-200 airplanes, listed in Boeing Service Bulletin 757-25A0058, dated April 18, 1986, certificated in any category. Compliance required within 45 days after the effective date of this amendment, unless already accomplished. To ensure proper door opening and escape slide deployment accomplish the following: A. Modify slide pack release cable assemblies on Doors No. 1 and No. 2, left and right, in accordance with Boeing Service Bulletin 757-25A0058, dated April 18, 1986, or later FAA-approved revisions. 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. 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 May 30, 1986. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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