AD 80-25-03

final rule

BOEING Model 747 Airplanes

AD Number
80-25-03
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

Failure of shear pins on B.F. Goodrich off-wing slides could result in improper deployment of escape slides during emergency evacuation.

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

Required Actions

Install shear pin mechanical restraints in accordance with B.F. Goodrich Service Bulletin 25-054 or later FAA-approved revisions. Compliance may be adjusted upon FAA inspector approval with substantiating data.

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

Compliance Time

Within three (3) years after the effective date of this AD

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

Affected Aircraft

Boeing Model 747 airplanes equipped with B.F. Goodrich off-wing slides

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

Federal Register Abstract

Shear Pin Restraints

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_80-25-03.html
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Details
AD Number:
80-25-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 747 Airplanes
Subject:
Shear Pin Restraints
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/02/1981
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: 80-25-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3982

AD NUMBER:   80-25-03

SUBJECT HEADING:   BOEING Model 747 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 2, 1981

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
80-25-03 BOEING: Amendment 39-3982. Applies to all Model 747 airplanes equipped with B.F. Goodrich off-wing slides:

A. Within three (3) years after the effective date of this AD, unless already accomplished, install shear pin mechanical restraints to affected off-wing escape slides in accordance with B.F. Goodrich Service Bulletin 25-054 dated March 4, 1980, or later FAA approved revisions, or in a manner approved by the Chief, Seattle Area Aircraft Certification Office FAA Northwest Region.

B. Upon request of the operator, an FAA maintenance inspector, subject to prior approval by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Region, may adjust the compliance date if the request contains substantiating data to justify the change.

NOTE: This installation is considered an equivalent modification to the bayonet/spring restraints required by Amendment 39-1128 (35FR19170) AD 70-26-01.

This amendment becomes effective January 2, 1981.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_80-25-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
80-25-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Model 747 Airplanes
Subject:
Shear Pin Restraints
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/02/1981
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: 80-25-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3982

AD NUMBER:   80-25-03

SUBJECT HEADING:   BOEING Model 747 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective January 2, 1981

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
80-25-03 BOEING: Amendment 39-3982. Applies to all Model 747 airplanes equipped with B.F. Goodrich off-wing slides:

A. Within three (3) years after the effective date of this AD, unless already accomplished, install shear pin mechanical restraints to affected off-wing escape slides in accordance with B.F. Goodrich Service Bulletin 25-054 dated March 4, 1980, or later FAA approved revisions, or in a manner approved by the Chief, Seattle Area Aircraft Certification Office FAA Northwest Region.

B. Upon request of the operator, an FAA maintenance inspector, subject to prior approval by the Chief, Seattle Area Aircraft Certification Office, FAA Northwest Region, may adjust the compliance date if the request contains substantiating data to justify the change.

NOTE: This installation is considered an equivalent modification to the bayonet/spring restraints required by Amendment 39-1128 (35FR19170) AD 70-26-01.

This amendment becomes effective January 2, 1981.

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.