# STC SA945NE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Viking Air Limited, Canada
- Description: Gross weight increase (6,000 lbs. when operated on wheels, wheel/skis and floats and 5950 lbs. when operatedon amphibious floats on land). (DHC-2 (L-20A) MK.III turbo Beaver)
- Applied: March 5, 1992
- Status date: November 30, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806)
- Certificate PDF: https://openairdocs.org/files/sha256/9d/5b/9d5b161561dbed2017ca1766986ba282651ab582b10861bdfeecd2e2d2be7f4f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FB57B5F6B57EA05D862571070052DA8A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA945NE

## ADs that name it (1)

- [AD 2020-16-15](https://openairdocs.org/ad/2020-16-15): Fuselage · Viking Air DHC-2 Mk.I and DHC-2 Mk.III with STC SA00299NY or SA945NE. Effective Sep 21, 2020. Named in the applicability

## Approved models (1)

- de Havilland Inc. (Canada) DHC-2 (L-20A) 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.

FAA Form 8110-2(10-68) Page 1 of 2 IMPORT Number SA945NE This certificate issued to Viking Air Limited 9574 Hampden Road Sidney, British Columbia, Canada V8L 5V5

Part 3 of the Civil Air Regulations.

Original Product -- Type Certificate Number : A-806 Make : de HAVILLAND

Model : DHC-2 MK.III (Turbo Beaver)

Gross weight increase (6,000 lbs. when operated on wheels, wheel/skis and floats and 5950 lbs. when operated on amphibious floats on land). Modification is to be carried out in accordance with Viking Air Limited Drawing VAL TB 1200 Rev. G dated March 22, 1995 and Drawing Change Note (DCN) No. 2 VAL TBW 1202, Rev. A, dated January 15, 2002, or later Transport Canada approved revision. It is applicable to all Turbo Beaver aircraft fitted with standard PT6A-6 or –20 engines, PT6A-15AG, -27 or –34 engines in accordance with STC SA620NE. Floats are installed in accordance with Wipaire, Inc. Drawing 5B1-758 Rev. A, dated March 31, 1992, or later Transport Canada approved revision.

1. Viking Air Limited Airplane Flight Manual Supplement, Report No. VAL-TB-1200-20 Rev. 7, dated May 29, 1992, DOT approved June 2, 1992, or later Transport Canada approved revisions is required with this modification.

2. Viking Air Limited Airplane Maintenance Manual Supplement, Report No. VAL-TB-1200-21, dated April 9, 1991, is required with this modification.

Date of Issuance: March 5, 1992 Date reissued :

Date amended : June 3, 1992, April 30, 2002, November 30, 2005

( Signature) Anthony Socias Manager New York Aircraft Certification Office

(Title)

Date Amended: June 3, 1992, April 30, 2002

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

Number SA945NE Date of Amendment: November 30, 2005

3. Pratt & Whitney Canada PT6A-27 engi ne installed per STC No. SA620NE dated November 10, 1988 as amended June 25, 1998.

4. Wipaire, Inc. Flow Energizers are re quired with the Seaplane and Amphibian Float installations, The Flow Energizers are installed per STC No. SA1723GL dated March 31, 1992.

5. Compatibility of this design change with previously appr oved modifications must be determined by the installer.

6. 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.

…END…

## Every issue (1)

- November 30, 2005: Amended, Current. [certificate](https://openairdocs.org/files/sha256/9d/5b/9d5b161561dbed2017ca1766986ba282651ab582b10861bdfeecd2e2d2be7f4f)

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