# STC SA04714NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Viking Air Limited, Canada
- Description: Installation of MT-Propeller model MTV-16-1-E-C-F-R(P)/CFR240-55a propeller
- Applied: September 11, 2020
- Status date: March 3, 2022
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806)
- Certificate PDF: https://openairdocs.org/files/sha256/a0/b5/a0b523bea7117422a0a701ea618832bfead9bf4c259073c35543452be603f899
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/896AD6DDEC6F3408862587FE00547653.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA04714NY

## ADs that name it (0)

None.

## Approved models (1)

- Viking Air Limited DHC-2 Mk.III ([TCDS A-806](https://openairdocs.org/tcds/A-806))

## 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.

IMPORT SA04714NY Viking Air Limited 1959 de Havilland Way Sidney, British Columbia Canada V8L 5V5 Part 3 A-806 Viking Air Limited DHC-2 Mk. III

1. Installation of MT-Propeller model MTV-16-1-E-C-F-R(P)/CFR240-55a propeller in accordance with MT-Propeller Operation and Installation Manual E-610, Revision 43, dated April 30, 2020, or later European Union Aviation Safety Agency (EASA) approved revisions.

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

1. 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.

(Limitations and Conditions Continued on Page 3 of 3) September 11, 2020 March 3, 2022 Anthony E. Gallo Manager, International Validation Branch (AIR-730) Compliance & Airworthiness Division Aircraft Certification Service (AIR) 3 the Civil Air Regulations

**IMPORT SA04714NY SA04714NY 3**

IMPORT SA04714NY Date of Issuance: March 3, 2022

Description of Type Design Change (continued):

2. Operation must be done in accordance with in accordance with MT-Propeller Operation and Installation Manual E-610, Revision 43, dated April 30, 2020, or later EASA approved revisions.

3. Maintenance must be done in accordance with MT-Propeller Operation and Installation Manual E-610, Revision 43, dated April 30, 2020, or later EASA approved revisions.

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

3. This STC is applicable to all serial numbers for this Make-Model.

4. The aircraft must be equipped with a PT6A-27 or -34 engine installed in accordance with FAA STC No. SA620NE.

5. The aircraft may be optionally equipped with 6000 pound gross weight increase installed in accordance with FAA STC No. SA945NE.

----------END---------- 3 3

## Every issue (1)

- March 3, 2022: Issued, Current. [certificate](https://openairdocs.org/files/sha256/a0/b5/a0b523bea7117422a0a701ea618832bfead9bf4c259073c35543452be603f899)

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