# STC SA00438NY

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Stolairus Aviation Inc, Canada
- Description: Increase in maximum gross weight to 8367 lbs.
- Applied: January 6, 1996
- Status date: June 28, 2012
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A-815](https://openairdocs.org/tcds/A-815)
- Certificate PDF: https://openairdocs.org/files/sha256/85/da/85da66de19680867dff3beadcb60e31e1b10adc60b6deb6591492e50cb9e8cb3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/97607080FB05A063862585A1005456B8.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00438NY

## ADs that name it (1)

- [AD 2022-05-11](https://openairdocs.org/ad/2022-05-11): Wing Structure · Viking Air DHC-3. Effective Apr 13, 2022. Cited in the text

## Approved models (1)

- Viking Air Limited DHC-3 ([TCDS A-815](https://openairdocs.org/tcds/A-815))

## What the certificate says

Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA00438NY Stolairus Aviation 6095 Airport Way Kelowna, British Columbia Canada V1V 1S1 Civil Air Regulations.

1. Increase in maximum gross weight to 8,367 pounds in accordance with AOG Air Support Inc., Top Drawing No.

AOG-03-001-1, Revision A. dated December 17, 1997, or later Transport Canada approved revisions.

2. The Maintenance Manual Supplement of AOG Air Support listed in the Approved Configuration List is required for Continued Airworthiness of the aircraft following the modification described.

1. Refer to Approved Configuration List on Page 3 for limitations and required documents.

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.

Limitations and Conditions: continued on Page 3 of 3) Anthony E. Gallo Manager New York ACO Branch Viking Air Limited DHC-3 June 28, 2012 June 22, 1998, September 1, 2000, December 2, 2004 January 06, 1996 May 31, 1996 IMPORT A-815 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SA00438NY

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00438NY Date Reissued: June 28, 2012 Limitations and Conditions: (continued):

APPROVED CONFIGURATION LIST CONFIGURATION 2 ITEM Addition Required Baron STOL Kit per STC Installation SA00287NY (STA SA94-

114) Maximum Gross 8367 8367 8367 Weight (Lbs.)

Engine P&W PT6A-135 or P& W R1340-59, R1340- Pezetel PZL ASZ-62IR- PT6A-135A APPROVED 61, S1H1-G and S3H1-G M18 per CONFIGURATION per Type Certificate A- STC SA327NE LIST 815 (A-27) (STA SA83-18) or PT6A-34 per STC SA3777NM (STA SA89-32) Floats Any FAA approved float Any FAA approved float Any FAA approved float installation, up to and installation, up to and installation, up to and including EDO 7850 size, including EDO 7850 size, including EDO 7850 which provides a which provides a size, which provides a minimum buoyancy to minımum buoyancy to minimum buoyancy to 7530 floats. 7530 floats. 7530 floats.

Flight Manual No. 5, Revision C, DOT No. 6, Revision A, DOI No. 7, Revision B. DO] Supplement Approved 7/28/00 * Approved 6/6/00 * approved 6/6/00 * AOG Air Support Inc. MMS-191-95-001, Rev. MMS-191-95-001, Rev. MMS-191-95-001, Rev.

Maintenance Manual C, DOT Approved C, DOT Approved C, DOT Approved Supplement September 27, 2004** September 27, 2004 ** September 27, 2004 ** * or later Transport Canada approved revisions ** or later Transport Canada accepted revisions END

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

## Every issue (1)

- June 28, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/85/da/85da66de19680867dff3beadcb60e31e1b10adc60b6deb6591492e50cb9e8cb3)

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