FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 869 | Status | Valid |
| Manufacturer Name | VIKING AIR LIMITED | Certificate Issue Date | 12/21/2017 |
| Model | DHC-6-400 | Expiration Date | 12/31/2027 |
| Type Aircraft | Fixed Wing Multi-Engine | Type Engine | Turbo-prop |
| Pending Number Change | None | Dealer | No |
| Date Change Authorized | None | Mode S Code (base 8 / Oct) | 50153303 |
| MFR Year | 2013 | Mode S Code (Base 16 / Hex) | A0D6C3 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | BANK OF UTAH TRUSTEE | ||
| Street | 50 S 200 E STE 110 | ||
| City | SALT LAKE CITY | State | UTAH |
| County | SALT LAKE | Zip Code | 84111-1617 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | P&W CANADA | Classification | Restricted |
| Engine Model | PT6A-34 | Category | Patrolling, Aerial Surveying, Other |
| A/W Date | 12/16/2015 | Exception Code | Yes |
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The information contained in this record should be the most current Airworthiness information available in the historical aircraft record. However, this data alone does not provide the basis
for a determination regarding the airworthiness of an aircraft or the current aircraft configuration. For specific information, you may request a copy of the aircraft record at https://aircraft.faa.gov/e.gov/ND/ |
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| None |
| Certificate Number | T178862 | Issue Date | 12/21/2017 | Expiration Date | 01/20/2018 |
| Mod Code | 28 | Mod Date | 20151228 |
| NO CHANGES FROM PREVIOUS FUEL MOD DATED 4/4/2015 | |||
| Mod Code | 28 | Mod Date | 20130809 |
| FERRY FUEL SYSTEM P/N C6G1241-13 INSTALLATION CARRIED OUT AS PER AIRCRAFT MANUFACTURERS APPROVED DATA CONTAINED IN ENGINEERING ORDER 66596 REVISION H FOR THE DHC-6 SERIES 300 AND 400 AIRCRAFT. MAIN WHEELTIE INFLATION INCREASE PRESSUR TO 45 PSI CARRIED OUT AS PER PSM 1-63-1FLIGHT MANUAL SUPPLEMENT 14. FLIGHT MANUAL SUPPLEMENT PSM 1-63-1 SUPPLEMENT 14 PLACED IN THE APPROVED FLIGHT MANUAL PSM 1-64-1A PER AIRCRAFT FLIGHT MANUAL PSM 1-64-POH SECTION 7.27.4 REQUIREMENT. WEIGHTAND BALANCE PSM 1-64-8 SUPPLEMENT 1 PLACED IN THE APPROVED FLIGHT MANUAL PSM 1-64-1A. AIRCRAFT REWEIGH CARREIDD OUT - FERRY FUEL SYSTEM WEIGHT AND BALANCE REPORT INITIATED. A COPY FO THIS 337 IT TO BE PLACED ONBOARD THE MODIFIED AIRCRAFT IN ACCORDANCE WITH FAA PART913417(D) AND FAA PART 43 (D)(1). | |||
| Mod Code | 28 | Mod Date | 20150404 |
| THIS AIRCRAFT HAS BEEN RE-FITTED WITH AN AUXILIARY FERRY FUEL SYSTEM, TO ENABLE OVERSEAS DELIVERY, IN ACCORDANCE WITH SOUTHERN CROSS AVIA TION, INC., FERRY FUEL SYSTEM ENGINEERING DOCUMENTS, DEHAVILLAND DHC-6COMMUTER SERIES AIRCRAFT, REPORT NO. SCA A005, PAGES, 1-20 DATED 6/1/1996, WITH DEVIATIONS TO USE TURTLE PAC 160-300 GALLLON TANKS PER PACIFIC RIM AEROSPACE CORPORATION, DOCUMENTS NO. PRA13006BE, REV. B DATED 9/13/13 AND FAA 8110-3 DATED 9/13/2013 FOR THIS AIRCRAFT. THE FUEL TANKS ARE MANUFACTURED BY TURTLE-PAC PTY, LTD. THE BLADDER TANKS WERE TESTED TO 24 PSI, WITHOUT FAILURE AND TANKS WERE LEAK TESTED TO 5.0 PSI. THE TANKS MEET THE REQUIREMENTS FOR FAR 23.965 AND FAR 25.965THE TANKS ARE LOCATED IN THE CABIN AT FLOOR LEVEL FOR EVEN LOAD DISTRIBUTION. THEY ARE SECURED IN PLACE USING 6 - 3333 LBS RATED CARGO STAPSAND EXISTING SEAT ATTACHMENT POINTS USING PN 78101 TRACK FITTINGS. FUEL IS ROUTED THROUGH THE INDIVIDUAL TANK OUTLET AND FITTINGS, THROUGH AEROQUIP, MIL-6000 TYPE 3/4" ID HOSE AND AN FITTINGS TO THE PUMP AND AFT TANK VENT. FUEL ENTERS IN THE TOP OF THE AIRCRAFT FUEL CELLS, LOCATED IN THE BELLY OF THE AIRCRAFT, NUMBER ONE AND/OR SEVEN. THIS FILLS FRONT AND /OR REAR AIRCRAFT FUEL TANKS. THE FLOW OF FUEL FROM THE FERRY SYSTEM TO THE AIRCRAFT TANKS IS BY GRAVITY AND/OR PUMP PRESSURE, ADEQUATE AT ALL POWER SETTINGS. THE FUEL SUPPLY WILL ENABLE UTILIZATION OF ALL BUT ONE(1) GALLON OF FUEL PER INDIVIDUAL CELL. A PLACARD DETAILING OPERAITON OF THE FERRY FUEL SYSTEM IS DISPLAYED IN THE AIRCRAFT. THE GWTO IN THE FERRY CONFIGURATION DOES NOT EXCEED 140%OF THE NORMAL GWTO, IN ACCORDANCE WITH DEHAVILLAND DHC-6-300 OPERATINGDATA MANUAL, PMS 1-163-1, REV. 7 DATED 11/16/2005, PART 6, SUPPLEMENT | |||
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