# STC SE2338SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Jet Avion Corporation, United States
- Description: Installation of an oil tank safety cap adapter which prevents oil loss in the event of loss or damage to the filler cap.
- Applied: May 2, 1988
- Status date: September 8, 2006
- Product: Engine
- Certification basis: Part 21, Part 33
- Data sheets: [TCDS E20EA](https://openairdocs.org/tcds/E20EA), [TCDS E3NE](https://openairdocs.org/tcds/E3NE)
- Certificate PDF: https://openairdocs.org/files/sha256/18/4d/184d3faf0864b20bdda075c12e80f3813e4bf2ef7c050a8d04d4a1427370ce28
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FD021012FC1B63E9862571FD0063459F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SE2338SO

## ADs that name it (0)

None.

## Approved models (7)

- Pratt & Whitney Division JT9D-20 ([TCDS E20EA](https://openairdocs.org/tcds/E20EA))
- Pratt & Whitney Division JT9D-59A ([TCDS E3NE](https://openairdocs.org/tcds/E3NE))
- Pratt & Whitney Division JT9D-7 ([TCDS E20EA](https://openairdocs.org/tcds/E20EA))
- Pratt & Whitney Division JT9D-7A ([TCDS E20EA](https://openairdocs.org/tcds/E20EA))
- Pratt & Whitney Division JT9D-7F ([TCDS E20EA](https://openairdocs.org/tcds/E20EA))
- Pratt & Whitney Division JT9D-7J ([TCDS E20EA](https://openairdocs.org/tcds/E20EA))
- Pratt & Whitney Division JT9D-7Q ([TCDS E3NE](https://openairdocs.org/tcds/E3NE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA FORM 8110-2(10-68) PAGE 1 of 2 PAGES Number SE2338SO This certificate issued to Jet Avion Corporation 3000 Taft Street Hollywood, FL 33021

Part 33 of the Federal Aviation Regulations.

Original Product--Type Certificate Number : E20EA, E3NE Make : Pratt & Whitney Model : JT9D-7,-7A,-7F,-7J,-20,-7Q,-59A

Installation of an oil tank safety cap adapter which prevents oil loss in the event of loss or damage to the filler cap, per Propulsion Technology Corp. (PTC) Drawing PT020001, Revision D, Sheet 5 of 7, dated August 15, 1988, or PTM International, Inc. Drawing PT020001 Revision F, dated May 26, 1993, or later FAA approved drawing.

Limitations and Conditions: This approval is limited to the above JT9D engine models when installed in aircraft nacelles which meet the clearance requirements shown on Propulsion Technology Corp. (PTC) drawing PT020001, Revision D, Sheet 5 of 7 dated August 15, 1988, or PTM International, Inc. Drawing PT020001 Rev. F, sheet 4 of 4 dated May 26, 1993, or later FAA approved drawing. Also this approval should not be extended to other engines of this model that incorporate any other previously approved modifications, unless it is determined that the interrelationship between this change and any other previously approved modifications will introduce no adverse effect upon the airworthiness of that engine. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application : May 02, 1988

Date of issuance : May 18, 1988 Date reissued : November 16, 1998; September 08, 2006

Date amended : June 07, 1993; October 06, 1999

( Signature) Melvin D. Taylor Manager Atlanta Aircraft Certification Office

(Title)

## Every issue (1)

- September 8, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/18/4d/184d3faf0864b20bdda075c12e80f3813e4bf2ef7c050a8d04d4a1427370ce28)

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