# STC SA02064SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Mitsubishi Heavy Industries America Inc, United States
- Description: Fabrication and installation of a Test Instrumentation, Inc., Tip Fuel Tank Pressure-Vacuum Relief Valve
- Applied: February 10, 2010
- Status date: July 5, 2013
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A2PC](https://openairdocs.org/tcds/A2PC), [TCDS A10SW](https://openairdocs.org/tcds/A10SW)
- Certificate PDF: https://openairdocs.org/files/sha256/fd/93/fd935b36ef8b71d50253911dcd84c8d329da27ecca843cb00c7fd41931337d59
- Approved model list and other attachments: [AML SA02064SE.pdf](https://openairdocs.org/files/sha256/f7/4d/f74d923f5e59a504bce3883cdea2cac5b9c980c53a56295041b62cd3c642931e)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D83CDC7B03FA0F9586257B9F00676678.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02064SE

## ADs that name it (0)

None.

## Approved models (17)

- Mitsubishi Heavy Industries Ltd. MU-2B ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-10 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-15 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-20 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-26A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-30 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-36A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-40 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-60 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))

## 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.

Number SA02064SE

This certificate, issued to Mitsubishi Heavy Industries America, Inc.

4951 Airport Parkway, Suite 530 Addison, TX 75001-6045

Part * of the * Regulations.

Original ProductType Certificate Number: * See attached Federal Aviation Administration (FAA) Make: Approved Model List (AML) SA02064SE for approved Model: aircraft models and applicable airworthiness regulations

Description of the Type Design Change: Fabrication and installation of a Test Instrumentation, Inc., Tip Fuel Tank Pressure-Vacuum Relief Valve in accordance with Test Instrumentation Master Drawing List (MDL) as specified on AML SA02064SE.

Limitations and Conditions: Approval of this change in type design applies to the Mitsubishi aircraft models listed on AML SA02064SE only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of the other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

A copy of this certificate and AML must be maintained as part of the permanent records for the modified aircraft.

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: February 10, 2010 Date reissued:

Date of issuance: May 6, 2010 Date amended: July 5, 2013####

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

### AML SA02064SE.pdf

FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA02064SE FOR FABRICATION AND INSTALLATION OF A TEST INSTRUMENTATION, INC., TIP FUEL TANK PRESSURE-VACUUM RELIEF VALVE ISSUE DATE: May 6, 2010

Page 1 of 1

**ITEM AIRCRAFT MAKE**

**AIRCRAFT MODEL ORIGINAL TC NUMBER**

**CERTIFICATION**

**BASIS FOR**

**ALTERATION**

**FAA APPROVED MASTER**

DRAWING LIST AML REV DATE Drawing Revision*

1. Mitsubishi MU-2B, MU-2B-10, MU-2B-20, MU-2B-15, MU-2B-30, MU-2B-35, MU-2B-25, MU-2B-36, MU-2B-26 A2PC CAR 10 CAR 3 TII-10003 Revision 1, dated April 20 2010 7/5/13

2. Mitsubishi MU-2B-25, MU-2B-35, MU-2B-26, MU-2B-36, MU-2B-26A, MU2B-36A, MU-2B-40, MU-2B-60 A10SW CAR 3 TII-10003 Revision 1, dated April 20 2010 7/5/13 * Or later FAA Approved Revision

FAA Approved:

Manager, Seattle Aircraft Certification Office AMENDED: July 5, 2013 REISSUED:

## Every issue (2)

- July 5, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/fd/93/fd935b36ef8b71d50253911dcd84c8d329da27ecca843cb00c7fd41931337d59), [AML SA02064SE.pdf](https://openairdocs.org/files/sha256/f7/4d/f74d923f5e59a504bce3883cdea2cac5b9c980c53a56295041b62cd3c642931e)
- May 6, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/07/e0/07e08bccd8b94e37efa95ae9445a80ef4b6cb89e7779996ae776d575b5da0638), [SA02064SE_AML.pdf](https://openairdocs.org/files/sha256/ec/5e/ec5e3be602c919ae7717a03dcfe15ec44905d70b2802d6e5532f6d087d65a800)

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