AD 87-01-02

final rule

BOEING Model 747 Airplanes

AD Number
87-01-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-100B Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-100B SUD Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-200B Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-200C Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-200F Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-300 Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-400 Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-400D Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747-400F Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747SP Series BOEING Model 747 Airplanes
aircraft The Boeing Company 747SR Series BOEING Model 747 Airplanes

Unsafe Condition

The escape slide pack may not remain in proper position on Door No. 3 during a minor crash landing due to inadequate attachment.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Modify the escape slide attachment in accordance with Boeing Alert Service Bulletin 747-25A2710 or later FAA-approved revisions. 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 twelve months after the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

All Model 747 airplanes equipped with the single-piece escape slide at Door No. 3

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Escape Slide Attachment

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_87-01-02.html
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AD Number:
87-01-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 747 Airplanes
Subject:
Escape Slide Attachment
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/20/1987
Make:
The Boeing Company
Model:
747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...Show more
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: 87-01-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5494

AD NUMBER:   87-01-02

SUBJECT HEADING:   BOEING Model 747 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 20, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-01-02 BOEING: Amendment 39-5494. Applies to all Model 747 airplanes, certificated in any category, equipped with the single-piece escape slide at Door No. 3. To ensure that the escape slide pack remains in proper position on the door in the event of a minor crash landing, accomplish the following, unless already accomplished:

A. Within twelve months after the effective date of this AD, modify the escape slide attachment in accordance with Boeing Alert Service Bulletin 747-25A2710, dated July 15, 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 the modification required by this AD.

All persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. 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 January 20, 1987.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_87-01-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-01-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 747 Airplanes
Subject:
Escape Slide Attachment
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/20/1987
Make:
The Boeing Company
Model:
747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...Show more
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: 87-01-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5494

AD NUMBER:   87-01-02

SUBJECT HEADING:   BOEING Model 747 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 20, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-01-02 BOEING: Amendment 39-5494. Applies to all Model 747 airplanes, certificated in any category, equipped with the single-piece escape slide at Door No. 3. To ensure that the escape slide pack remains in proper position on the door in the event of a minor crash landing, accomplish the following, unless already accomplished:

A. Within twelve months after the effective date of this AD, modify the escape slide attachment in accordance with Boeing Alert Service Bulletin 747-25A2710, dated July 15, 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 the modification required by this AD.

All persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. 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 January 20, 1987.

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.