# STC SA00056DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: AeroProducts Intl Inc, United States
- Description: Expansion of temperature restricted operational envelope.
- Applied: August 18, 1993
- Status date: January 14, 1994
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A10SW](https://openairdocs.org/tcds/A10SW)
- Certificate PDF: https://openairdocs.org/files/sha256/46/e5/46e5158fd3425a0cf5ca9d677d201297e32e0c4dc5e6c99c2e36b9fc899c3746
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/13E0C8E706321CB585256CC1007DC74B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00056DE

## ADs that name it (0)

None.

## Approved models (1)

- Mitsubishi Heavy Industries Ltd. MU-2B-60 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00056DE This certificate issued to: AeroProducts International, InC.

Part 3 of the Civil Air Regulations.

Original Product - Type Certificate Number: A 10SW Make: Mitsubishi Heavy Industries, LTD.

Model: MU-2B-60 Description of Type Design Change:

Expansion of temperature restricted operational envelope in accordance with FAA approved AeroProducts International, Inc. Report No. MU2-001, initial release, dated October 6, 1993, or later FAA approved revision.

1. FAA approved Airplane Flight Manual Supplement dated January 14, 1994, or later FAA approved revision is required.

2. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft on which other previously approved modifications are incorporated unless it is determined that the interrelationship 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 the aircraft. A copy of this Certificate must be maintained as part of the permanent records for the Toditied sire a tid the supperting dalu which is the basis for appreval shall remain in effect until sur vendered, suspended, revoked, or a lermination date is otherwise established by the Adminisbrater of the Federal Aviation Administration .

Date of Application: August 18, 1993 Sinte weissued:

Date of Issuance: . January 14, 1994 I ate unended:

FEDERAL AVIATION VAINISTRAIO RICHARD E. JENNINGS (Signature) Denver Aircraft Certification Field Office Manager Northwest Mountain Region, Denver, Colorado (Title)

## Every issue (1)

- January 14, 1994: Issued, Current. [certificate](https://openairdocs.org/files/sha256/46/e5/46e5158fd3425a0cf5ca9d677d201297e32e0c4dc5e6c99c2e36b9fc899c3746)

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