| AD Number | 82-26-03 | Status | Active |
| Effective Date | January 27, 1983 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-4523 |
| Product Type | ["Engine"] | Product Subtype | Not specified |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Pratt & Whitney Division |
| Model(s) | JT9D-7 JT9D-7A JT9D-7AH JT9D-7F JT9D-7H JT9D-7J |
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 notalready 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.