Dornier 328-100 aircraft MSN 3012 Detailed Specification Sheet --------------------------------------------------------------------------------------------------------------------- SPECIFICATION SUMMARY Reg. Manufacturer Serial Current Current Delivery Date Number Hours Cycles N334PH 1994 3012 16354 21266 Prepared by Ray Mosses, with best knowledge of 24 th April 2013 Revision 1 N334PH MSN 3012 Contents Chapter Title Page 1. General 3 2. Certification 3 3. Power Plant / APU 3 4. Operation Weights 3 5. Cockpit Layout 4 6. Cabin Layout 4 7. Cargo Layout / Volumes 4 8. Fuel System 4 9. Avionics 4 10. Wheels and Brakes 5 11. Maintenance System 5 12. Drawings (LOPA ) - current 5 2 N334PH MSN 3012 1. GENERAL This Aircraft was delivered new by Fairchild Dornier in Germany (Former Dornier) to Horizon Airways. Aircraft has new all white paint scheme recently applied Aircraft is currently parked in USA. 2. CERTIFICATION Aircraft is currently on FAA register 3. POWER PLANT / PROPELLERS PW119C with a thrust of 6.050 lbs. The engines are operated “on-condition”, Serial TSN CSN TSO CSO Cycles remaining Number 116025 16000 20929 5702 7003 7990 Various 116024 14220 17529 3859 4661 10332 various Hartzell model HD-E6C-3B Serial TSN TSO TBO Blade Life Number remaining HL264 8304 2666 6000 TBD HL205 10867 15 6000 TBD 4. CURRENT OPERATION WEIGHTS Basic Operational Weights are: Max Gross Taxi Weight (MGTW) 31019 lbs 14070 kg Max Take-Off Weight (MTOW) 30843 lbs 13990 kg Max Landing Weight (MLW) 29167 lbs 13154 kg Max Zero Fuel Weight (MZFW) 27800 lbs 12538 kg 5. COCKPIT LAYOUT a) Two Crew seats, b) One Observer Seat The aircraft is equipped with EASA approved bullet proof (Cascade) door 3 N334PH MSN 3012 6. CABIN LAYOUT Aircraft has been converted to a cargo aircraft but a standard 32 seat interior can be installed prior to delivery. This conversion will be at additional cost to the selling price and would be subject to a separate contract. Current Configuration a) Full cargo layout b) Galley Not applicable d) Lavatories Poratable toilet e) Seating Manufactured by B/E Aerospace 7. CARGO LAYOUT / VOLUMES Max. Comp. Capacity (aft1/bulk) 400 kg Max. Comp. Capacity (aft2/bulk) 350 kg In addition the following cargo areas are available 8. FUEL SYSTEM The usable fuel tank capacity is 4.542 liters, in wings and feeder tanks. Each wing tank has a capacity inner tank 1.341 liters and outer 826 liters and each feeder tank has a capacity of 104 liters.The fuel quantity indication system is calibrated in lbs. This can be converted to Kgs prior to delivery if required. 4 N334PH MSN 3012 9 AVIONICS 10. WHEELS AND BRAKES a) Nose Wheel Tyres: Goodyear P/N: 2225 b) Main Wheel Tyres: Goodyear P/N: 2226-2 c) Brakes: Bendix P/N: HA2227-4 5 N334PH MSN 3012 11. MAINTENANCE SYSTEM 11.1 Aircraft Maintenance Aircraft is sold “as is where is” Last check performed C1 - completed December 2012 Next Due CP2.5 – Due December 2013 SSI 2.5 Due December 2013 Further details on request 11.2 Landing Gear Maintenance Overhaul Interval Landing Gears(NLG& MLG): 22.000 Flight Cycles or 10 Years. Gear Data (MLG and NLG) Assy Partnummer Serial nr Next Gear Overhaul 22.000 FC (Remaining Time in FC ) Barrel Assy LH22730-000-8 U-9 21994 FC/ 83 months remaining Barrel Assy RH22731-000-7 U-57 21994 FC/ 95 months remaining Barrel Assy 231000-000-2 IL085 21994 FC/ 83 months remaining 12 LOPA – current 6 N334PH MSN 3012 7 N334PH MSN 3012 8 N334PH MSN 3012 For information contact: Ray Mosses Director- Sales – 328 Aircraft Trade GmbH 0049 8153 88111 2512 0049 171 583 9374 [email protected] 9 .