# STC SA00816SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Mitsubishi Heavy Industries America Inc, United States
- Description: Installation of emergency exit placards
- Applied: May 4, 2000
- 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/sha256/9e/67/9e67a7beed9d4d287462c35dbb054a049be0f4f61975b52163bcdfea46a67187
- Approved model list and other attachments: [AML SA00816SE.pdf](https://openairdocs.org/files/sha256/25/bd/25bd768b320b164df37bfd72108349a21cda7a222226761ca6bd9289d84ec99e)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4CCE2F58D387CEF186257B9F006693A5.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00816SE

## 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.

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SA00816SE

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) SA00816SE for approved Model: aircraft models and applicable airworthiness regulations

Description of the Type Design Change: Installation of emergency exit placards in accordance with the Master Drawing List as specified on AML SA00816SE, and Installation Instructions Document as specified on AML SA00816SE.

Limitations and Conditions: Approval of this change in type design applies to the Mitsubishi aircraft models listed on AML SA00816SE only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those 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: May 4, 2000 Date reissued:

Date of issuance: June 14, 2000 Date amended: July 5, 2013

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

### AML SA00816SE.pdf

**FEDERAL AVIATION ADMINISTRATION (FAA) APPROVED MODEL LIST (AML) SA00816SE FOR**

INSTLLATION OF EMERGENCY EXIT PLACARDS ISSUE DATE: July 5, 2013

Page 1 of 1

**ITEM AIRCRAFT MAKE**

**AIRCRAFT MODEL ORIGINAL TC NUMBER**

**CERTIFICATION**

**BASIS FOR**

**ALTERATION**

**INSTALLATION**

**INSTRUCTIONS**

**FAA APPROVED MASTER**

DRAWING LIST AML REV DATE Number Revision* 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 3 CAR 10 MU2-7001 Revision A, dated May 30, 2000 MU2-7000 Revision A, dated May 30, 2000

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 MU2-7001 Revision A, dated May 30, 2000 MU2-7000 Revision A, dated May 30, 2000

* Or later FAA Approved Revision

FAA Approved:

Manager, Seattle Aircraft Certification Office AMENDED:

REISSUED:

## Every issue (2)

- July 5, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/9e/67/9e67a7beed9d4d287462c35dbb054a049be0f4f61975b52163bcdfea46a67187), [AML SA00816SE.pdf](https://openairdocs.org/files/sha256/25/bd/25bd768b320b164df37bfd72108349a21cda7a222226761ca6bd9289d84ec99e)
- June 14, 2000: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/91/ba/91ba2d5c6870f98dfcf7d640ebb83d962136352165822cce03345a4e63d7235b)

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