# STC SA03315NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: MT- Propeller Entwicklung GmbH, Germany
- Description: Installation of Model MTV-27-1-E-C-F-R(G)/CFR210-58d 5-bladed, full feathering composite propellers
- Applied: April 18, 2013
- Status date: July 31, 2013
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21, Part 23, Part 36
- Data sheets: [TCDS A2PC](https://openairdocs.org/tcds/A2PC), [TCDS A10SW](https://openairdocs.org/tcds/A10SW)
- Certificate PDF: https://openairdocs.org/files/sha256/a5/00/a500629bcd1db694572688de55626011ff358471ea7ec81bd68be2ecf4f73270
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C3A51B92638741AB86257BEC006F1918.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA03315NY

## ADs that name it (0)

None.

## Approved models (10)

- Mitsubishi Heavy Industries Ltd. MU-2B-20 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- 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 A2PC](https://openairdocs.org/tcds/A2PC))
- 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.

Part 3 of the Civil Air Regulations.

“2000 RPM Engine” Configuration, (Applicable to MU-2B-20, -25, -26, -30, -35, and -36 aircraft):

Installation of Model MTV-27-1-E-C-F-R(G)/CFR210-58d 5-bladed, full feathering composite propellers. The installation must be in accordance with MT-Propeller documents Master Operation Manual List, Doc. No. E-2244, Revision 0, dated January 28, 2013, and Installation Instructions, Doc. No. E-2246, Revision 0, dated January 28, 2013. Required documents included in this installation are FAA and EASA approved Airplane Flight Manual Supplement and Pilots Operating Manual Supplement, Doc. No. E-2245, Revision 0, dated January 28, 2013, and Instructions for Continued Airworthiness, Doc. No. E-2247, Revision 0, dated January 28, 2013.

“1591 RPM Engine” Configuration, (Applicable to MU-2B-26A, 36A, -40, and -60 aircraft):

Installation of Model MTV-27-1-E-C-F-R(G)/CFRL240-55d 5-bladed, full feathering composite propellers. The installation must be in accordance with MT-Propeller documents Master Operation Manual List, Doc. No. E-2304, Revision 0, dated January 28, 2013, and Installation Instructions, Doc. No. E-2306, Revision 0, dated January 28, 2013. Required documents included in this installation are FAA and EASA approved Airplane Flight Manual Supplement and Pilots Operating Manual Supplement, Doc. No. E-2305, Revision 0, dated January 28, 2013 and Instructions for Continued Airworthiness, Doc. No. E-2307, Revision 0, dated January 28, 2013.

1. The Installer must determine whether this design change is compatible with previously approved modifications.

MT- Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany

No. A2PC No. A10SW Make: Mitsubishi Heavy Industries, Ltd.

Model: MU-2B-20, MU-2B-25, MU-2B-26, MU-2B-30, MU-2B-35, and MU-2B-36 MU-2B-26A, MU-2B-36A, MU-2B-40, and MU-2B-60 Date reissued:

(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office

(Title)

Date of application: April 18, 2013

Date of issuance: July 31, 2013

FAA Form 8110-2-1(10-69) Page 3 of 3

Number SA03315NY Issuance date: July 31, 2013

Limitations and Conditions: Continued

2. 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.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for this modification are as follows:

• The type certification basis for the Mitsubishi Heavy Industries, Ltd. Model MU-2B-20, -25, -26, -30, -35, and -36 aircraft is shown on TCDS No. A2PC and A10SW, and for Mitsubishi Heavy Industries, Ltd. Model MU-2B-26A, -36A, -40, and - 60 aircraft is shown on TCDS No. A10SW for parts not changed or not affected by the change.

• The type certification basis for the Mitsubishi Heavy Industries, Ltd. Model MU-2B-20, -25, -26, -30, -35, and -36 aircraft is shown on TCDS No. A2PC and A10SW, and for Mitsubishi Heavy Industries, Ltd. Model MU-2B-26A, -36A, -40, and - 60 aircraft is shown on TCDS No. A10SW for parts changed or affected by the change with the following 14 CFR exceptions:

Section 23.1529 Amendment 23-26 Part 36 Amendment 36-28

………………………..END…………………….

## Every issue (1)

- July 31, 2013: Issued, Current. [certificate](https://openairdocs.org/files/sha256/a5/00/a500629bcd1db694572688de55626011ff358471ea7ec81bd68be2ecf4f73270)

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