# STC SA00434NY - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Stolairus Aviation Inc, Canada - Description: Increase gross weight to 5370 lbs. - Applied: April 18, 1994 - Status date: June 28, 2012 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806) - Certificate PDF: https://openairdocs.org/files/sha256/ef/28/ef28b9bdae86242ba8d5c353fcf6ecaae65741fd199b315c8462e1598b2aad6a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/45325A4E34222F358625833E0059D820.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00434NY ## ADs that name it (0) None. ## 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 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 SA00434NY Stolairus Aviation Inc. 6095 Airport Way Kelowna, BC, Canada V1V1S1 Civil Air Regulations. 3 Configuration (1): Increase gross weight to 5370 lbs. in accordance with AOG Air Support Inc. Installation Instructions No. AOG-01-002-8 Revision B, dated February 12, 2001 (Wing tip fuel required)or later TCCA-accepted revision. Configuration (2): Increase gross weight to 5370 lbs. in accordance with AOG Air Support Inc. Installation Instructions No. AOG-01-002-8 Revision B, dated February 12, 2001 (No tip fuel required) or later TCCA-accepted revision. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. 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. ( See Limitations and Conditions on Page 3 of 3) Anthony E. Gallo Manager New York ACO Branch Viking Air Limited DHC-2 MK 1 June 28, 2012 June 8, 2001 April 18, 1994 May 7, 1996 IMPORT A-806 3 FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) 3 SA00434NY FAA Form 8110-2 (5/14) Page 3 of 3 Date Reissued: June 28, 2012 3. For Configuration (1), all weight above 5100 lbs. must be fuel in the wing lip tanks. AOG Air Support Inc. Airplane Flight Manual Supplement No. 3, Revision A, dated February 2, 2001, and Transport Canada approved March 1,2001, is required. Installation of STC SA 1070NE. amended October 29. 1998 (Baron STOL kit), with Flight Manual Supplement No. 1, Revision D, dated March 16, 1998, is required. The wing strut assemblies, C2W1103A, C2W1104A, and C2W1115-1 / -2, are limited to a maximum service life as defined in Section 1, paragraph 1 (a) or AOG Air Support Inc. Maintenance Manual Supplement MMS-195-01-001, Revision "New", dated February 2, 2001, from the time or installation. 4. For Configuration (2), maximum gross weight is 5370 lbs., with no fuel required in wing tip tanks. AOG Air Support Inc. Airplane Flight Manual Supplement No. 9, Revision ''New", dated February 2, 2001, and Transport Canada approved March 1, 2001, is required. Installation of STC SA1070NE, amended October 29, 1998 (Baron STOL kit), with Flight Manual Supplement No. 1, Revision D, dated March 16, 1998, is required. The wing strut assemblies, C2W1103A, C2W1104A, and C2W1115-1 / -2, are limited to a maximum service life as defined in Section 1, paragraph 1(a) of AOG Air Support Inc. Maintenance Manual Supplement MMS-196-01-001, Revision "New'', dated February 2, 2001, from the time of installation. ----------END---------- SA00434NY ## Every issue (1) - June 28, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ef/28/ef28b9bdae86242ba8d5c353fcf6ecaae65741fd199b315c8462e1598b2aad6a) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.