# STC SA09565SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Intercontinental Jet Service Corporation
- Description: Installation of TPE331-10AV-511M engines.
- Status date: March 30, 2012
- Data sheets: A10SW, A10SW, A10SW, A2PC, A2PC, A2PC, A2PC
- Certificate PDF: https://openairdocs.org/files/sha256/70/28/70280cd92ba1e37df26b2395922b6762126486ae6e16b16bf07887136269d7b6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D89B15E38B018CFB862579D50055DA31.0001
- Page: https://openairdocs.org/stc/SA09565SC

## ADs that name it

None.

## Approved models (7)

- Mitsubishi Heavy Industries Ltd. MU-2B-25 (TCDS A10SW)
- Mitsubishi Heavy Industries Ltd. MU-2B-25 (TCDS A2PC)
- Mitsubishi Heavy Industries Ltd. MU-2B-26 (TCDS A10SW)
- Mitsubishi Heavy Industries Ltd. MU-2B-26 (TCDS A2PC)
- Mitsubishi Heavy Industries Ltd. MU-2B-35 (TCDS A10SW)
- Mitsubishi Heavy Industries Ltd. MU-2B-35 (TCDS A2PC)
- Mitsubishi Heavy Industries Ltd. MU-2B-36 (TCDS A2PC)

## 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 1 Number SA09565SC This Certificate issued to Intercontinental Jet Service Corporation a Delaware Corporation 3322 N. 74th East Avenue Tulsa, OK 74115

Part 23 of the Federal Aviation Regulations.

Original Product Type Certificate Number : [See attached FAA approved model list (AML) Make : for list of approved models and applicable

Model : airworthiness regulations]

Description of Type Design Change: Installation of TPE331-10AV-511M engines in accordance with “STC Instructions”, Revision 1, dated January 4, 1999, and “Engine Installation, Turboprop TPE331-10AV”, Drawing No.

3108201, dated October 20, 1997, or later FAA approved revision. FAA approved Flight Manual Supplement dated July 22, 1999, or later FAA approved revision required.

Limitations and Conditions: Installation only on aircraft which have TPE331-6-251M or –252M engines installed.

Hartzell Propeller, model number HC-B3TN-5( )/T10178NS( )-11R, with “N” style shot peened blades will be used with the replacement engine. The propeller diameter limits are 90.375 to 89.375 inches. The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Date of application : September 21, 1998

Date of issuance : July 22, 1999 Date reissued : 10/29/99; 9/11/06; 3/30/12

( Signature) M. Monica Merritt, Manager Airplane Certification Office, Southwest Region

( Title)

## Every issue (2)

- March 30, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/70/28/70280cd92ba1e37df26b2395922b6762126486ae6e16b16bf07887136269d7b6)
- September 11, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/d2/ad/d2ad48c9bea895a3f1935db894c4b7937d0d7c660f12541ecd28c5124fe5fceb)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.