# STC SA00299NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Viking Air Limited, Canada
- Description: Modification of the airplane to provide for an increase in maximum gross weight.
- Applied: January 25, 1993
- Status date: May 26, 1998
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806)
- Certificate PDF: https://openairdocs.org/files/sha256/dd/2a/dd2a8251076236d10659f852af2d3bd6e626d17de2954957247610a947565292
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156388664020250227181252.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00299NY

## 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.I ([TCDS A-806](https://openairdocs.org/tcds/A-806))

## 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: SA00290NY This certificate issued to: VIKING AIR LIMITED 9574 Hampden Road SIDNEY, B.C., CN V&L SV5 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirement's of Part 3/10.10 of the Civil Air Poegulations.

Original Product -- Typo Certificato Number A806 Make: DEHA VILLAND Model: DHC-2 MK.I Description of Type Design Change: Modification of the Airplane in accordance with Viking Air Limited Drawing VAL-BVS- 1256, issue C, dated January 6, 1998 or later FAA approved revisions, to provide for an increase in maximum gross weight from 5100 pounds to 5600 pounds, for airplanes configured with Wipline 6000/6100 seaplane or amphibian floats, or for airplanes configured with wheels or wheel/skis; increase to 5500 pounds for airplanes equipped with EDO 679-4930 floats or EDO 58-4580 floats modified in accordance with Supplemental Type certificate SF 92-1.

1. Flight Manual Supplement VAL-BVS-1256-20, revision D, dated December 30, 1992, when operated on wheels, wheel/skis, EDO 679-4930 floats or EDO 58-4580 floats, is required with this installation.

2. Flight Manual Supplement for opcration of Dellavilland DHC-2 Mk.I (HEAVY WEIGHT) Piston Beaver equipped with Wipline Model 6000 or 6100 Amphibian Floats, at a Gross Weight of 5600 pounds, dated January 15, 1998, is required with such an installation.

Date of Application: January 25, 1993 Date Reissued:

Date of Issuance: April 07, 1995 Date Amended: May 26, 1998 FEDERAL AVIATION By directign of the Sodmisistaton (Signature) * Ar Vito A. Pulera TOMINISTRATIO Manager, New York Aircraft Certification Office (Title)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) - (Address of grantor) (Number and streel) (City, State, and SIP code ) Extent of Authority (if licensing agreement):

Date of Transfer: _ Signature of grantor (In ink): _

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Cantinuatian Sheet) Number: SA00290NY Date of Issuance: April 07, 1995 Date Amended: May 26, 1998 Limitations and Conditions: (Continued):

3. Flight Manual Supplement for operation of DeHavilland DHC-2 Mk.I (HEAVY WEIGHT) Piston Beaver equipped with Wipline Model 6000 or 6100 Seaplane Floats, at a Gross Weight of 5600 pounds, dated January 15, 1998, is required with such an installation.

4. Maintenance Manual Supplement VAL-TB-1256-21, dated December 30, 1992, or later approved revisions, is required with this installation.

5. Compatibility of this design change with previously approved 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..

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

## Every issue (1)

- May 26, 1998: Amended, Current. [certificate](https://openairdocs.org/files/sha256/dd/2a/dd2a8251076236d10659f852af2d3bd6e626d17de2954957247610a947565292)

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