AD 82-26-03

final rule

PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J

AD Number
82-26-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
engine Pratt & Whitney Division JT9D-7 PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J
engine Pratt & Whitney Division JT9D-7A PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J
engine Pratt & Whitney Division JT9D-7AH PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J
engine Pratt & Whitney Division JT9D-7F PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J
engine Pratt & Whitney Division JT9D-7H PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J
engine Pratt & Whitney Division JT9D-7J PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J

Unsafe Condition

Fuel signal manifold cracking in operation

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

Required Actions

Replace manifold assembly P/N 711391 with assembly P/N 783391, bracket P/N 5003038-01, and clamp P/N ST1104-06 in accordance with Pratt & Whitney Aircraft Service Bulletin Number 5202, Revision 2, dated August 16, 1982, or later revision approved by the Manager, Engine Certification Branch, New England Region.

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

Compliance Time

prior to February 27, 1983

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

Affected Aircraft

Pratt & Whitney Aircraft models JT9D-7, -7H, -7A, -7AH Engines prior to and including S/N 695827; JT9D-7F Engine S/Ns 695600 through 695614, S/N 702000, S/N 702001, S/N 702550 through 702557 and all engines prior to and including S/N 689635; JT9D-7J Engines prior to S/N 701697. Excluded: JT9D engines obtained by conversion without Service Bulletin 3741.

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

Federal Register Abstract

Manifold Assembly

Applicability Source Text

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AD Final Rules - DRS_82-26-03.html
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AD Number:
82-26-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J
Subject:
Manifold Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/27/1983
Make:
Pratt & Whitney Division
Model:
JT9D-7 | JT9D-7A | JT9D-7AH | JT9D-7F | JT9D-7H | JT9D-7J
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: 82-26-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4523

AD NUMBER:   82-26-03

SUBJECT HEADING:   PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J

ACTION:  

SUMMARY:  

DATES:   Effective January 27, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-26-03 PRATT & WHITNEY AIRCRAFT: Amendment 39-4523. Applies to Pratt & Whitney Aircraft models.

JT9D-7, -7H, -7A, -7AH	Engines prior to and including S/N 695827.
JT9D-7F	Engine S/Ns 695600 through 695614, S/N 702000, S/N 702001, S/N 702550 through 702557 and all engines prior to and including S/N 689635.
JT9D-7J	Engines prior to S/N 701697.

NOTE: This directive does not apply to JT9D engines obtained by conversion which do not incorporate Service Bulletin 3741.

Compliance required prior to February 27, 1983, unless already accomplished.

To prevent fuel signal manifold cracking in operation replace manifold assembly P/N 711391 with assembly P/N 783391, bracket P/N 5003038-01, and clamp P/N ST1104-06 in accordance with Pratt & Whitney Aircraft Service Bulletin Number 5202, Revision 2, dated August 16, 1982, or later revision approved by the Manager, Engine Certification Branch, New England Region.

All persons affected by this directive who have not already received the referenced service bulletin from the manufacturer may obtain copies upon request to Pratt & Whitney Aircraft, Division of United Technologies Corporation, 400 Main Street, East Hartford, Connecticut 06108. This document may also be examined at FAA, New England Region, 12 New England Executive Park, Burlington, Massachusetts 01803. A historical file on this AD which includes the material in full is maintained by the FAA at the New England Region office.

This amendment becomes effective on January 27, 1983.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_82-26-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-26-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J
Subject:
Manifold Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
01/27/1983
Make:
Pratt & Whitney Division
Model:
JT9D-7 | JT9D-7A | JT9D-7AH | JT9D-7F | JT9D-7H | JT9D-7J
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: 82-26-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4523

AD NUMBER:   82-26-03

SUBJECT HEADING:   PRATT & WHITNEY AIRCRAFT Models JT9D-7, -7H, -7A, -7AH and JT9D-7F and JT9D-7J

ACTION:  

SUMMARY:  

DATES:   Effective January 27, 1983.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-26-03 PRATT & WHITNEY AIRCRAFT: Amendment 39-4523. Applies to Pratt & Whitney Aircraft models.

JT9D-7, -7H, -7A, -7AH	Engines prior to and including S/N 695827.
JT9D-7F	Engine S/Ns 695600 through 695614, S/N 702000, S/N 702001, S/N 702550 through 702557 and all engines prior to and including S/N 689635.
JT9D-7J	Engines prior to S/N 701697.

NOTE: This directive does not apply to JT9D engines obtained by conversion which do not incorporate Service Bulletin 3741.

Compliance required prior to February 27, 1983, unless already accomplished.

To prevent fuel signal manifold cracking in operation replace manifold assembly P/N 711391 with assembly P/N 783391, bracket P/N 5003038-01, and clamp P/N ST1104-06 in accordance with Pratt & Whitney Aircraft Service Bulletin Number 5202, Revision 2, dated August 16, 1982, or later revision approved by the Manager, Engine Certification Branch, New England Region.

All persons affected by this directive who have not already received the referenced service bulletin from the manufacturer may obtain copies upon request to Pratt & Whitney Aircraft, Division of United Technologies Corporation, 400 Main Street, East Hartford, Connecticut 06108. This document may also be examined at FAA, New England Region, 12 New England Executive Park, Burlington, Massachusetts 01803. A historical file on this AD which includes the material in full is maintained by the FAA at the New England Region office.

This amendment becomes effective on January 27, 1983.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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