AD 71-06-03

final rule

PRATT & WHITNEY Model JT4A Series Engines

AD Number
71-06-03
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 JT4A-10 PRATT & WHITNEY Model JT4A Series Engines
engine Pratt & Whitney Division JT4A-11 PRATT & WHITNEY Model JT4A Series Engines
engine Pratt & Whitney Division JT4A-12 PRATT & WHITNEY Model JT4A Series Engines
engine Pratt & Whitney Division JT4A-3 PRATT & WHITNEY Model JT4A Series Engines
engine Pratt & Whitney Division JT4A-5 PRATT & WHITNEY Model JT4A Series Engines
engine Pratt & Whitney Division JT4A-9 PRATT & WHITNEY Model JT4A Series Engines

Unsafe Condition

Twelfth stage compressor rotor disc failure as a result of suspected material deficiency.

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

Required Actions

Replace the suspect serial number twelfth stage compressor rotor disc either within the next 50 hours in service after the effective date if the disc has 18,000 hours or more in service, or prior to accumulating 18,050 hours in service if the disc has 18,000 hours or less in service. Substantiating data submission may allow compliance time adjustment.

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

Compliance Time

Within the next 50 hours in service after the effective date of this AD (May 19, 1971) for discs with 18,000 hours or more in service, or prior to accumulating 18,050 hours in service for discs with 18,000 hours or less in service.

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

Affected Aircraft

Pratt & Whitney Model JT4A series engines with 12th stage compressor rotor discs having serial numbers listed in the AD (e.g., 2G5181 to 2G6360, 5F7645 through 5F858, etc.).

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

Federal Register Abstract

Twelfth Stage Compressor Rotor Disc

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_71-06-03.html
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AD Number:
71-06-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
PRATT & WHITNEY Model JT4A Series Engines
Subject:
Twelfth Stage Compressor Rotor Disc
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/19/1971
Make:
Pratt & Whitney Division
Model:
JT4A-10 | JT4A-11 | JT4A-12 | JT4A-3 | JT4A-5 | JT4A-9
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: 71-06-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1211

AD NUMBER:   71-06-03

SUBJECT HEADING:   PRATT & WHITNEY Model JT4A Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective May 19, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-06-03 PRATT & WHITNEY: Amdt. 39-1168 as amended by Amendment 39-1211. Applies to all Pratt & Whitney Aircraft JT4A series turbojet engines which incorporate the following serial number 12th stage compressor rotor disc part number 360112.

2G5181	2G6360		
2G5182	2G6362		
2G5183	2G6363		
2G5446	2G6445		
2G5807	2G6448		
2G5812	2G6449		
2G5818	2G6454		
2G5820	2G6581		
2G5821	2G6583		
2G5825	2G6585		
2G5826	3G0201		
2G6027			
2G6030			
5F7645 7		5F858	6F8362
5F7646		5F8588	6F9707
5F8544 through		5F8695	6F9739
5F8547		6F7206	6F9751
5F8550 through		6F7207	6F9753 through
5F8553		6F7210	6F9759
5F8558		6F7214	6F9760 through
5F8576		6F7218	6F9765
5F8577		6F7501	6F9846
5F8581 through		6F7502	6F9853
5F8584		6F7504	6F9861
		6F7949	6F9866
		6F8168	7F0156
		6F8198	7F0480
			7F0556

Pratt & Whitney Aircraft telegram PSE/RS/1-3-10-1 covers this same subject.

Compliance required as indicated.

To preclude twelfth stage compressor rotor disc failure as the result of suspected material deficiency, accomplish the following:

1. For all the previously listed serial number twelfth stage compressor rotor discs:

A. With 18,000 hours or more in service within the next 50 hours in service after the effective date of this AD, replace the suspect serial number disc.

B. With 18,000 hours or less in service prior to the accumulation of 18,050 hours in service, replace the suspect serial number disc.

2. Upon submission of substantiating data by an owner or operator through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region, may adjust the compliance time.

Amendment 39-1168 was effective March 12, 1971.

This amendment 39-1211 is effective May 19, 1971 and was effective for all recipients of the telegram dated March 12, 1971 which contained this amendment.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_71-06-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
71-06-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
PRATT & WHITNEY Model JT4A Series Engines
Subject:
Twelfth Stage Compressor Rotor Disc
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/19/1971
Make:
Pratt & Whitney Division
Model:
JT4A-10 | JT4A-11 | JT4A-12 | JT4A-3 | JT4A-5 | JT4A-9
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: 71-06-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1211

AD NUMBER:   71-06-03

SUBJECT HEADING:   PRATT & WHITNEY Model JT4A Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective May 19, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-06-03 PRATT & WHITNEY: Amdt. 39-1168 as amended by Amendment 39-1211. Applies to all Pratt & Whitney Aircraft JT4A series turbojet engines which incorporate the following serial number 12th stage compressor rotor disc part number 360112.

2G5181	2G6360		
2G5182	2G6362		
2G5183	2G6363		
2G5446	2G6445		
2G5807	2G6448		
2G5812	2G6449		
2G5818	2G6454		
2G5820	2G6581		
2G5821	2G6583		
2G5825	2G6585		
2G5826	3G0201		
2G6027			
2G6030			
5F7645 7		5F858	6F8362
5F7646		5F8588	6F9707
5F8544 through		5F8695	6F9739
5F8547		6F7206	6F9751
5F8550 through		6F7207	6F9753 through
5F8553		6F7210	6F9759
5F8558		6F7214	6F9760 through
5F8576		6F7218	6F9765
5F8577		6F7501	6F9846
5F8581 through		6F7502	6F9853
5F8584		6F7504	6F9861
		6F7949	6F9866
		6F8168	7F0156
		6F8198	7F0480
			7F0556

Pratt & Whitney Aircraft telegram PSE/RS/1-3-10-1 covers this same subject.

Compliance required as indicated.

To preclude twelfth stage compressor rotor disc failure as the result of suspected material deficiency, accomplish the following:

1. For all the previously listed serial number twelfth stage compressor rotor discs:

A. With 18,000 hours or more in service within the next 50 hours in service after the effective date of this AD, replace the suspect serial number disc.

B. With 18,000 hours or less in service prior to the accumulation of 18,050 hours in service, replace the suspect serial number disc.

2. Upon submission of substantiating data by an owner or operator through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region, may adjust the compliance time.

Amendment 39-1168 was effective March 12, 1971.

This amendment 39-1211 is effective May 19, 1971 and was effective for all recipients of the telegram dated March 12, 1971 which contained this amendment.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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