# STC SA04175NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: MT- Propeller Entwicklung GmbH, Germany
- Description: Installation of MT-Propeller Entwicklung GmbH's Model# MTV-9-B/200-52 3-Blade constant speed propeller and spinner on Textron Aviation Inc. Model T182, T182T, and TR182 aircraft
- Applied: January 26, 2017
- Status date: September 24, 2018
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 36
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/0e/62/0e629ef5295cf36e7612d33973568984a17a0eb4ba28387b2ea9f6a261a80a5c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5C4D5536EF06292986258322005134C0.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA04175NY

## ADs that name it (0)

None.

## Approved models (3)

- Textron Aviation Inc. T182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. T182T ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. TR182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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 (5/14) Page 1 of

Part of the

Signature

Title SA04175NY MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany Civil Air/Federal Aviation Regulations.

3/23

1. Installation of MT-Propeller Entwicklung GmbH's Model# MTV-9-B/200-52 3-Blade constant speed propeller and spinner on Textron Aviation Inc. Model T182, T182T, and TR182 aircraft in accordance with the configuration stated in Master Operation Manual List, Doc. No. E-2836, Rev. 3, dated September 19, 2018 or later EASA approved revision and Installation Instructions, Doc. No. E-2834, Rev. 1, dated March 13, 2017 or later EASA approved revision.

2. Operation must be in accordance with Airplane Flight Manual Supplement, Doc. No. E-2833, Rev. 2, dated September 19, 2018 or later EASA approved revision, and is required as part of this installation.

(See Description of Type Design Change Continued on Page 3 of 3)

1. The aircraft must be operated in accordance with the "Limitations" sections of Airplane Flight Manual Supplement, Doc. No.

E-2833, Rev. 2, dated September 19, 2018, or later EASA approved revision.

2. The installer must determine whether this design change is compatible with previously approved modifications.

3. 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.

Anthony E. Gallo Acting Manager New York ACO Branch Textron Aviation Inc.

T182, T182T, TR182 January 26, 2017 September 24, 2018 IMPORT 3A13 3

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SA04175NY

FAA Form 8110-2 (5/14) Page 3 of

3 Date of Issuance: September 24, 2018

Description of Type Design Change (continued):

3. Maintenance must be in accordance with Instructions for Continued Airworthiness, Doc. No. E-2835, Rev. 0, dated December 22, 2016 or later EASA accepted revision, and is required as part of this installation.

Certification Basis:

Based on 14 CFR §21.115 and §21.101, and FAA Order 8110.48, the certification basis for this modification to Textron Aviation Inc. T182, T182T, and TR182 aircraft is as follows:

a) The type certification basis for the Textron Aviation Inc. T182, T182T, and TR182 aircraft as shown on TCDS 3A13 for parts not changed or not affected by the change.

b) The type certification basis for the Textron Aviation Inc. T182, T182T, and TR182 aircraft as shown on TCDS 3A13 for parts changed or affected by the change with the following exception:

● Compliance with 14 CFR Part 36 at Amendment 36-30.

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SA04175NY

## Every issue (1)

- September 24, 2018: Issued, Current. [certificate](https://openairdocs.org/files/sha256/0e/62/0e629ef5295cf36e7612d33973568984a17a0eb4ba28387b2ea9f6a261a80a5c)

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