AD 86-05-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-100 Series | BOEING Model 737-100, -200, and -300 Airplanes |
| aircraft | The Boeing Company | 737-200 Series | BOEING Model 737-100, -200, and -300 Airplanes |
| aircraft | The Boeing Company | 737-300 Series | BOEING Model 737-100, -200, and -300 Airplanes |
Unsafe Condition
Failure of the escape slide cover restraining straps could result in improper emergency opening characteristics of the aft door, compromising safe emergency evacuation.
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Required Actions
Install escape slide cover restraining straps per Boeing Service Bulletin 737-25A1182, Revision 2, Part II, or equivalent Revision 1. An alternate means of compliance may be approved by the FAA. Special flight permits may be issued under FAR 21.197/21.199.
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Compliance Time
within 6 months after the effective date of this amendment
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Affected Aircraft
Boeing Model 737-100, -200, and -300 airplanes as specified in Boeing Service Bulletin 737-25A1182, Revision 2, dated November 12, 1985.
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Federal Register Abstract
Escape Slide Cover Restraining Straps
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_86-05-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-05-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 737-100, -200, and -300 Airplanes Subject: Escape Slide Cover Restraining Straps Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/11/1986 Make: The Boeing Company Model: 737-100 Series | 737-200 Series | 737-300 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 86-05-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5249 AD NUMBER: 86-05-04 SUBJECT HEADING: BOEING Model 737-100, -200, and -300 Airplanes ACTION: SUMMARY: DATES: Effective April 11, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-05-04 BOEING: Amendment 39-5249. Applies to Model 737-100, -200, and -300 airplanes, as specified in Boeing Service Bulletin 737-25A1182, Revision 2, dated November 12, 1985, certificated in any category. To correct aft door emergency opening characteristics, accomplish the following within 6 months after the effective date of this amendment, unless previously accomplished: A. Install escape slide cover restraining straps in accordance with Boeing Service Bulletin 737-25A1182, Revision 2, Part II, dated November 12, 1985, or later FAA-approved revisions. NOTE: Installation of escape slide cover restraining straps in accordance with Boeing Service Bulletin 737-25A1182, Revision 1, dated September 24, 1985, is equivalent to such installation in accordance with Revision 2 of that service bulletin, and constitutes compliance with this paragraph. B. An alternate means of compliance 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 amendment who have not already received the appropriate service bulletin from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. This service bulletin 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 11, 1986. FOOTER:
Document Text
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AD Final Rules - DRS_86-05-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 86-05-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: BOEING Model 737-100, -200, and -300 Airplanes Subject: Escape Slide Cover Restraining Straps Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/11/1986 Make: The Boeing Company Model: 737-100 Series | 737-200 Series | 737-300 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: 86-05-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5249 AD NUMBER: 86-05-04 SUBJECT HEADING: BOEING Model 737-100, -200, and -300 Airplanes ACTION: SUMMARY: DATES: Effective April 11, 1986. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 86-05-04 BOEING: Amendment 39-5249. Applies to Model 737-100, -200, and -300 airplanes, as specified in Boeing Service Bulletin 737-25A1182, Revision 2, dated November 12, 1985, certificated in any category. To correct aft door emergency opening characteristics, accomplish the following within 6 months after the effective date of this amendment, unless previously accomplished: A. Install escape slide cover restraining straps in accordance with Boeing Service Bulletin 737-25A1182, Revision 2, Part II, dated November 12, 1985, or later FAA-approved revisions. NOTE: Installation of escape slide cover restraining straps in accordance with Boeing Service Bulletin 737-25A1182, Revision 1, dated September 24, 1985, is equivalent to such installation in accordance with Revision 2 of that service bulletin, and constitutes compliance with this paragraph. B. An alternate means of compliance 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 amendment who have not already received the appropriate service bulletin from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. This service bulletin 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 11, 1986. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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