AD 80-19-03

final rule

PRATT & WHITNEY AIRCRAFT Model JT3D-1-MC7 Engines

AD Number
80-19-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division JT3D-1-MC7 PRATT & WHITNEY AIRCRAFT Model JT3D-1-MC7 Engines

Unsafe Condition

High cycle fatigue cracking of fifth stage compressor disks (P/N 426505) which could result in disk fracture.

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

Required Actions

Retire from service all fifth stage compressor disks P/N 426505 and replace with either disk P/N 697105 or P/N 749605.

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

Compliance Time

not later than December 31, 1980

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

Affected Aircraft

Pratt & Whitney Aircraft JT3D-1-MC7 turbofan engine models

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

Federal Register Abstract

Fifth Stage Compressor Disks

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_80-19-03.html
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Details
AD Number:
80-19-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
PRATT & WHITNEY AIRCRAFT Model JT3D-1-MC7 Engines
Subject:
Fifth Stage Compressor Disks
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/07/1980
Make:
Pratt & Whitney Division
Model:
JT3D-1-MC7
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 80-19-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3911

AD NUMBER:   80-19-03

SUBJECT HEADING:   PRATT & WHITNEY AIRCRAFT Model JT3D-1-MC7 Engines

ACTION:  

SUMMARY:  

DATES:   Effective October 7, 1980.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
80-19-03 PRATT & WHITNEY AIRCRAFT: Amendment 39-3911. Applies to all Pratt & Whitney Aircraft JT3D-1-MC7 turbofan engine models.

Compliance required not later than December 31, 1980.

To preclude high cycle fatigue cracking of fifth stage compressor disks which could result in disk fracture, retire from service all fifth stage compressor disks, P/N 426505, and replace with either disk P/N 697105 or P/N 749605.

Upon submission of substantiating data, through an FAA Aviation Safety Inspector, the Chief, Engineering and Manufacturing Branch, New England Region, may adjust the compliance date.

A historical file on this AD is maintained in full by the FAA at its headquarters in Washington, D.C., and at the New England Region.

This amendment becomes effective October 7, 1980.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_80-19-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
80-19-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
PRATT & WHITNEY AIRCRAFT Model JT3D-1-MC7 Engines
Subject:
Fifth Stage Compressor Disks
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/07/1980
Make:
Pratt & Whitney Division
Model:
JT3D-1-MC7
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 80-19-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3911

AD NUMBER:   80-19-03

SUBJECT HEADING:   PRATT & WHITNEY AIRCRAFT Model JT3D-1-MC7 Engines

ACTION:  

SUMMARY:  

DATES:   Effective October 7, 1980.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
80-19-03 PRATT & WHITNEY AIRCRAFT: Amendment 39-3911. Applies to all Pratt & Whitney Aircraft JT3D-1-MC7 turbofan engine models.

Compliance required not later than December 31, 1980.

To preclude high cycle fatigue cracking of fifth stage compressor disks which could result in disk fracture, retire from service all fifth stage compressor disks, P/N 426505, and replace with either disk P/N 697105 or P/N 749605.

Upon submission of substantiating data, through an FAA Aviation Safety Inspector, the Chief, Engineering and Manufacturing Branch, New England Region, may adjust the compliance date.

A historical file on this AD is maintained in full by the FAA at its headquarters in Washington, D.C., and at the New England Region.

This amendment becomes effective October 7, 1980.

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.