# STC SA01220NY - Type: Supplemental type certificate - Status: Current, Issued - Holder: Viking Air Limited, Canada - Description: Installation of right hand wing landing light and floor track. - Applied: February 24, 2000 - Status date: June 21, 2000 - Product: Aircraft, Single-Engine - Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806) - Certificate PDF: https://openairdocs.org/files/sha256/e2/45/e245423447079180ab25a28c6717c70253f39d10e2850db49bda6dd11606a0cf - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125148509620250227181943.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01220NY ## ADs that name it (0) None. ## Approved models (2) - de Havilland Inc. (Canada) DHC-2 (L-20A) MK.I ([TCDS A-806](https://openairdocs.org/tcds/A-806)) - de Havilland Inc. (Canada) DHC-2 (L-20A) MK.III ([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 SA0122ONY This certificate issued to: Viking Air Limited 1962 Canso Road Sidney, B.C. V&L SV5 Canada Purt 3 of the Civil Ais Regulations. Original Product -- Type Certificate Number: A-806 Make: deHavilland Model: DHC-2 MK.I; DHC-2 MK.III Description of Type Design Change: 1. Installation of Right Hand Wing Landing Light is in accordance with DOT approved Viking Air Ltd. drawing VAL BVS 1052, Revision C, approved 16 February 2000. 2. Installation of Floor Track is in accordance with DOT Approved Viking Air Ltd. Installation Instruction P/N VAL TBS 1274-14, Revision 1, approved February 16, 2000. 1. The Fioor Track installation is limited to the DHC-2 MK III Turbo Beaver only. 2. The Fuel Cap installation is limited to the DHC-2 MK III Turbo Beaver only. 3. The Storage Tube is limited to the DHC-2 MK III models which have been previously modified with a cabin extension per either Sealand Aviation STC SA90-2 or Wipaire STC SA714GL. Date of Application: February 24, 2000 Date Reissued: Date of Issuance: June 21,2000 Date Amended: FEDERAL AVIATION By Direction of the Administrator Signature) Vito A. Pullera TOMMISFRATO Manager New York Aircraft Certification Office (Title) Signature ul krantur (in inal: _ Date ul Trander:. Extent of luchurity lif licensing acresment):. (Aldress «f granior) from (Niame of prantor) (Print me type) •buman une lines, 1. Address of iransleree). 10 (Nume yf iransferee). Transfer the ownership of Supplemental Type Cariñcate Vumber TRANSFER ENDORSEMENT The fA will reissue the sentineare in the name vi the transierce and ion ard is 1o him. the transier «i inıs Supplemental Type Certiñcate. INSTRUCTIONS: The transier nilorsement Irion mav be used co nursiv she agoropriare FAt Repional Crice oi Hutted Siales of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01220NY Date of Issuance: June 21, 2000 Description of Type Design Change: (Continued): 3. Installation of Flush Fuel Caps is in accordance with DOT approved Viking Air Ltd. Drawing No. VAL TBF 1249, New Issue, approved February 16, 2000. 4. Installation of the Storage Tube is in accordance with DOT approved Viking Air Ltd. Drawing VAL TBS 1269, New Issue, approved February 16, 2000. 5. Installation of the Radio Shelves is in accordance with DOT approved Viking Air Ltd. Drawing VAL BVS 1238, Issue A, approved February 16, 2000. 6. Installation of the Battery Structural Support at stn. 104 is in accordance with DOT approved Viking Air Ltd. Drawing VAL TBS 1239, Issue D, approved February 16, 2000. Limitations and Conditions: (Continued): 1. The Radio Shelves are limited to the DHC-2 MK III models which have been previously modified with a cabin extension per either Sealand Aviation STC SA90-2 or Wipaire STC SA714GL. 2. The Battery Structural Support is limited to the DHC-2 MK III models which have been previously modified with a cabin extension per either Sealand Aviation STC SA90-2 or Wipaire STC SA714GL. 3. Compatibility of this design change with previously approved modifications must be determined by the installer. 4. 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) - June 21, 2000: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e2/45/e245423447079180ab25a28c6717c70253f39d10e2850db49bda6dd11606a0cf) --- 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.