AD 86-07-12

final rule

PRATT & WHITNEY Models JT9D-7R4G2 Engines

AD Number
86-07-12
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division JT9D-7R4G2 PRATT & WHITNEY Models JT9D-7R4G2 Engines

Unsafe Condition

Possible engine support clevis failure due to fatigue cracking in P/N 5006482-01 engine support clevis on PW JT9D-7R4G2 engines.

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

Required Actions

Remove P/N 5006482-01 engine support clevis at or before 3,000 cycles per PW SB JT9D-7R4-72-119, Rev 3. Replace any engine support clevis with greater than 3,000 cycles prior to next flight.

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

Compliance Time

at or before 3,000 cycles

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

Affected Aircraft

Pratt & Whitney Division JT9D-7R4G2 engines

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

Federal Register Abstract

Engine Support Clevis

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_86-07-12.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
86-07-12
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
PRATT & WHITNEY Models JT9D-7R4G2 Engines
Subject:
Engine Support Clevis
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/11/1986
Make:
Pratt & Whitney Division
Model:
JT9D-7R4G2
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Superseded AD: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Superseded By: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: 86-07-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5267

AD NUMBER:   86-07-12

SUBJECT HEADING:   PRATT & WHITNEY Models JT9D-7R4G2 Engines

ACTION:  

SUMMARY:  

DATES:   Effective April 11, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
86-07-12 PRATT & WHITNEY: Amendment 39-5267. Applies to PW JT9D-7R4G2 engines. Compliance is required as indicated unless already accomplished.

To prevent possible engine support clevis failure, accomplish the following:

(a) Remove P/N 5006482-01 engine support clevis on PW JT9D-7R4G2 at or before 3,000 cycles in accordance with PW SB JT9D-7R4-72-119, Revision 3, dated November 5, 1985, or FAA approved equivalent.

(b) Replace any engine support clevis with greater than 3,000 cycles prior to next flight.

NOTES: (1) For the purpose of this AD, the number of flight cycles equals the number of flights that involve an engine operating sequence consisting of engine starting, takeoff operation, landing and engine shutdown.

(2) The hourly life limit is not affected by this AD.

Aircraft may be ferried in accordance with the provisions of FAR 21.197 and 21.199 to a base where the AD can be accomplished.

SB JT9D-7R4-72-119, Revision 3, dated November 5, 1985, identified and described in this document, is incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received this document from the manufacturer may obtain copies upon request to Pratt & Whitney, Commercial Products Division, 400 Main Street, East Hartford, Connecticut 06108. These documents also may be examined at the Office of the Regional Counsel, New England Region, Federal Aviation Administration, 12 New England Executive Park, Burlington, Massachusetts 01803.

This amendment becomes effective on April 11, 1986.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_86-07-12.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
86-07-12
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
PRATT & WHITNEY Models JT9D-7R4G2 Engines
Subject:
Engine Support Clevis
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/11/1986
Make:
Pratt & Whitney Division
Model:
JT9D-7R4G2
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: 86-07-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5267

AD NUMBER:   86-07-12

SUBJECT HEADING:   PRATT & WHITNEY Models JT9D-7R4G2 Engines

ACTION:  

SUMMARY:  

DATES:   Effective April 11, 1986.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
86-07-12 PRATT & WHITNEY: Amendment 39-5267. Applies to PW JT9D-7R4G2 engines. Compliance is required as indicated unless already accomplished.

To prevent possible engine support clevis failure, accomplish the following:

(a) Remove P/N 5006482-01 engine support clevis on PW JT9D-7R4G2 at or before 3,000 cycles in accordance with PW SB JT9D-7R4-72-119, Revision 3, dated November 5, 1985, or FAA approved equivalent.

(b) Replace any engine support clevis with greater than 3,000 cycles prior to next flight.

NOTES: (1) For the purpose of this AD, the number of flight cycles equals the number of flights that involve an engine operating sequence consisting of engine starting, takeoff operation, landing and engine shutdown.

(2) The hourly life limit is not affected by this AD.

Aircraft may be ferried in accordance with the provisions of FAR 21.197 and 21.199 to a base where the AD can be accomplished.

SB JT9D-7R4-72-119, Revision 3, dated November 5, 1985, identified and described in this document, is incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received this document from the manufacturer may obtain copies upon request to Pratt & Whitney, Commercial Products Division, 400 Main Street, East Hartford, Connecticut 06108. These documents also may be examined at the Office of the Regional Counsel, New England Region, Federal Aviation Administration, 12 New England Executive Park, Burlington, Massachusetts 01803.

This amendment becomes effective on April 11, 1986.

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.