What it approves
Installation of modifications for gross weight increase to 9000 lb.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
FAA Form 8110-2(10-68) Page 1 of 3 IMPORT Number SA02009NY 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-815 Make : Bombardier (deHavilland) Model : DHC-3 Description of Type Design Change:
Configuration 1,2, & 3:
Installation of modifications for gross weight increase to 9000 lb. in accordance with TAG Aerospace Report 037002-10, Master Drawing List, Rev. D, dated January 2, 2007, or later Transport Canada approved revision.
1. Configuration 1: The following equipment is required:
• PZL Model ASz-621R-M18 engine, with PZL model AW-2-30 propeller, installed in accordance with STC SA327NE, amended May 22, 2000.
• Baron STOL kit installed in accordance with STC SA00287NY, dated March 10, 1995
• International Aeroproducts model 8100 floats installed in accordance with STC SA01995NY, dated September 8, 2004.
(See Continuation Sheets 2 through 3)
IMPORT Date reissued : January 6, 2006 Date of application: June 11, 2004
Date of issuance: October 14, 2004
Date amended : November 16, 2005, May 17, 2007
( Signature) Anthony Socias Manager New York Aircraft Certification Office
(Title)
FAA Form 8110-2-1(10-69) Page 2 of 3
Number SA02009NY Date of Amendment: November 16, 2005 Limitations and Conditions (Continued):
2. Configuration 2: The following equipment is required:
• PZL Engine Model ASz-621R-M18 engine, with Hamilton Standard Model 23E-50 propeller with 6477 A-O blades.
• Baron STOL kit installed in accordance with STC SA00287NY dated March 10, 1995.
• International Aeroproducts model 8100 floats installed in accordance with STC SA01995NY, dated September 8, 2004.
3. Configuration 3: The following equipment is required:
• Pratt & Whitney Canada, Model PT6A-34 or PT64-34 AG engine, with Hartzell Propeller Model HC-B3TN-3DY/T10282 +4 installed in accordance with STC SA3777NM, amended May 15, 2003.
• Baron STOL kit installed in accordance with STC SA00287NY dated March 10, 1995.
• American Aeromotive, Inc. Service Letter No. AAI-DHC-3-02-02, installation of Forward Fuselage Strengthening kit, Rev. IR, dated April 10, 2002.
4. Viking Air Limited Flight Manual Supplement BDL00004-FMS, Rev. E, Transport Canada approved February 1, 2007 is required for Configurations 1 and 2.
5. Viking Air Limited Flight Manual Supplement, Report No. 030692, Rev. D, Transport Canada approved February 1, 2007 is required for Configuration 3.
6. Tag Aerospace Report 037002-MMS, Maintenance Manual Supplement, Rev. A, dated May 4, 2007, is required with Configurations 1, 2 and 3.
7. Replacement of new wing struts and fittings in accordance with Section 7 of Tag Aerospace Report 037002-MMS, Maintenance Manual Supplement, Rev. A, dated May 4, 2007 is required with Configurations 1, 2 and 3.
8. Wing struts and fittings identified in Section 7 of Tag Aerospace Report 037002-MMS, Maintenance Manual Supplement, Rev.
A, dated May 4, 2007 are life limited parts and must be replaced after the maximum flight hours stated or maximum months stated from initial installation, whichever occurs first.
9. The installer must determine whether this design change is compatible with previously approved modifications.
10. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person written evidence of that permission.
11. Certification Basis:
Configurations 1 and 2:
CAR part 3, as Amended to November 1, 1949 and ICAO Annex 8, Second Edition, March 1951.
FAA Form 8110-2-1(10-69) Page 3 of 3
IMPORT Number SA02009NY Date of Amendment: November 16, 2005
Configuration 3:
CAR part 3, as Amended to November 1, 1949 and ICAO Annex 8, Second Edition, March 1951 plus FAR 23, including Amendment 23-31 for the following sections:
23.45 23.49 23.51 23.65 23.75 23.77
23.251 23.253 23.301 thru 23.307 23.335 23.361 23.363
23.371 23.572 23.601 thru 23.605 23.609 thru 23.627 23.629 (e) (f) 23.641
23.901 23.903 23.905 23.907 23.925 23.929
23.933 23.937 23.939 23.943 23.951 23.954
23.955 23.957 23.959 23.961 23.977 23.991
23.997 23.1013 23.1017 23.1019 23.1027 23.1041
23.1045 23.1091 23.1093 23.1103 23.1111 23.1121
23.1123 23.1141 23.1143 23.1145 23.1153 23.1155
23.1163 23.1165 23.1182 23.1183 23.1189 23.1191
23.1193 23.1301 23.1303 23.1307 23.1309 23.1321
23.1322 23.1323 23.1331 23.1337 23.1351 23.1353
23.1357 23.1416 23.1419 23.1461 23.1501 23.1505
23.1521 23.1527 23.1529 23.1545 23.1549 23.1557
23.1583 23.1585 23.1589
FAR 23, including Amendment 23-55 for the following sections:
23.251 thru 23.531 and 23.575
Special Federal Aviation Regulation 27 as amended by 27-1 and 27-2.
FAR Part 36, section 36.5014 Appendix G.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Bombardier Inc. | DHC-3 | A-815 |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| May 17, 2007 | Amended, current | Certificate |
| November 16, 2005 | Amended, earlier issue | Certificate |