Commander Information. Estimated Specs, Performance & Operating Costs

Transcription

1 Commander Information Estimated Specs, Performance & Operating Costs Early 2014

2 Eagle Creek Aviation Services provides aircraft sales and service to owners and operators of Twin Commander, Embraer Phenom, and Cessna Citation aircraft. Aircraft owners rely on Eagle Creek Aviation as their trusted partner in maximizing the utilization and enjoyment of their planes. Eagle Creek s hard-earned reputation for excellence in buying and selling aircraft is matched only by the company s award-winning service. As one of the Midwest s leading aircraft service hubs, Eagle Creek offers a broad range of maintenance, refurbishment, repair and inspection services. Eagle Creek also has a second location called Naples Jet Center in Naples, FL

3 DIMENSIONS FEET OPERATING SPEEDS KTAS Wing Span (at 10,250 lbs, unless otherwise noted) Length Maximum Speed (100% 12,000 ft, TAS) 285 Height Normal Cruise (96%, 20,000 Ft., TAS) 275 Tread Twin Engine Best Rate of Climb, CAS 161 Cabin Entry Door 2.21 x 3.92 Twin Engine Best Angle of Climb, CAS 133 Cabin Height 4.47 Single Engine Best Rate of Climb, CAS 132 Cabin Width 4.12 Single Engine Best Angle of Climb, CAS 109 Cabin Length Minimum Control Speed, CAS 99 Cabin Volume (Cubic ft) Stall Speed, Clean 78 Baggage Volume (Cubic ft) Stall Speed, Gear & Flaps Down, CAS 75 Baggage Door Height 2.60 Baggage Door Width 1.64 CLIMB Ft/Min. Twin Engine Initial Rate of Climb (0 Flaps) 2,849 WEIGHTS POUNDS Time to Climb to 10,000 ft (Minutes) 4.0 Ramp Weight 10,375 Time to Climb to 20,000 ft (Minutes) 10.0 Takeoff Weight (690A) 10,250 Single Engine Rate of Climb (0 Flaps) 893 Takeoff Weight (690B) 10,325 Landing Weight 9,675 CEILING FEET Typical Empty Weight 6,775 Operational Ceiling Limit 31,000 Useful Load 3,575 Twin Engine Service Ceiling 33,000 Zero Fuel Weight 8,750 Twin Engine Absolute Ceiling 34,000 Baggage Compartment 600 Single Engine Service Ceiling 19,700 Single Engine Absolute Ceiling 20,600 FUEL GALLONS Maximum Pressurization Differential (PSI) 5.2 Fuel, Total Capacity (Gal) 389 Fuel, Usable (Gal) 384 TAKE OFF FEET Take Off Distance Ground Roll (0 Flaps) 1,434 LOADING Take Off Distance over 50 ft Obstacle 2,216 Wing Area 266 Sq. Ft. Short Field T.O. over 50 ft Obstacle 1,666 Wing Loading Lbs/Sq. Ft. Power Loading 7.32 Lbs/SHP LANDING FEET Landing Distance - with Reverse 1,606 POWER PLANT Landing Distance - Over 50 ft Obstacle 2,084 PROPELLERS ENGINE LIMITS SHP RPM ITT PERFORMANCE CONDITIONS Takeoff C Max Continuous C Overhaul Intervals Hot Section Intervals Gear Box intervals Turbo Commander 690A/B Specifications and Performance Honeywell TPE K Single Shaft Turbo-prop with integral gearbox, two stage centrifugal compressor, three stage axial turbine, single annular combustion chamber. 5,400 hours 1,800 hours 3,600 hours Hartzell 102 Inch Diameter, 3-Blade, Constant Speed, Full Feathering and Reversible Performance estimations are based upon U.S. Standard (I 962) atmospheric conditions and performance is contingent upon engine manufacturer s performance as indicated in FAA Type Certificate. All speeds within plus or minus 3% and all climbs, ranges and altitudes are within plus or minus 8%. All information was taken from the Manufacturer s publications and is subject to change and buyer s verification.

4 Turbo Commander 690A/B Estimated Operating Costs Fuel $ Fuel Costs/Gallon $ 6.25 Fuel Burn/Hour (Gallons) $ Maintenance $ Labor/Hour $ Parts/Hour $ Engine Reserves (Overhaul, Hot Section, Gearbox) $ Prop Overhaul $ Miscellaneous Flight Expenses $ 8.06 Total Direct Costs Per Hour $ 1, Average Block Speed (MPH) 280 Cost Per Statute Mile $ 4.06 Hangar Costs $ 8,500 Insurance $ 12,800 Hull $ 8,000 Legal Liability $ 4,800 Miscellaneous Overhead $ 15,000 Training $ 7,000 Aircraft Modernization $ 5,000 Navigation Equipment $ 3,000 Total Fixed Costs $ 36,300 Annual Budget Utilization Number of Seats 7 Miles 60,000 Hours 214 Direct Cost $ 243,151 Fixed Cost $ 36,300 Total Cost $ 279,451 Cost/Hour $ 1, Cost/Statute Mile $ 4.66 Cost/Seat Mile $ 0.67

5 Turbo Commander 690A/B Dash Ten Specifications and Performance Wing Span feet Length feet Height feet Total cabin & Baggage Vol cubic Feet Baggage volume and load 45 cubic feet/600 pounds Maximum Ramp weight 10,375 pounds Max gross takeoff weight 10,375 pounds Fuel Capacity, usable 384 gallons (Standard) Range 1,400+ nm Cruise Speed Single Engine Cruise Speed 305+ KTAS (Gross) 26,000-27,000 feet, ISA 218+ KTAS (9000 lbs) 15,000 feet, ISA Climb: Single Engine R of C Time to Climb 2,824 Initial Rate of Climb, Gross, SL, ISA 1,003 Initial Rate of Climb, Gross, SL, ISA 12.9 minutes to 29,000 ft (9000 lbs. ISA) Stall Speed, Clean Stall Speed, Gear/Flaps Dn Take-off over 50' Take-off roll Landing Roll w/reverse 77 Knots (CAS) (Gross Wt) 75 Knots (CAS) (Gross Wt) 1,833 Feet (Gross Wt) 1,285 Feet (Gross Wt) 1,240 Feet (Typical landing weight) Engine TBO Engine HSI Interval Nautical Miles to Overhaul 5,000 Hours 2,500 Hours Over One Million Miles! The Dash Ten 690A/B is a high performance turboprop that will rival the Citation I in climb and segment times at a fraction of the segment fuel burn. The flat rated take-off power is available up to 15,000 feet, ISA, allowing unmatched single engine safety, even at high density altitudes. This is without a doubt, a pilot's airplane.

6 Dash Ten Turbo Commander 690A/B Estimated Operating Costs Fuel $ Fuel Costs/Gallon $ 6.25 Fuel Burn/Hour (Gallons) $ Maintenance $ Labor/Hour $ Parts/Hour $ Engine Reserves (Overhaul, Hot Section, Gearbox) $ Prop Overhaul $ Miscellaneous Flight Expenses $ 8.06 Total Direct Costs Per Hour $ 1, Average Block Speed (MPH) 340 Cost Per Statute Mile $ 3.36 Hangar Costs $ 8,500 Insurance $ 12,800 Hull $ 8,000 Legal Liability $ 4,800 Miscellaneous Overhead $ 15,000 Training $ 7,000 Aircraft Modernization $ 5,000 Navigation Equipment $ 3,000 Total Fixed Costs $ 36,300 Annual Budget Utilization Number of Seats 7 Miles 60,000 Hours 176 Direct Cost $ 200,781 Fixed Cost $ 36,300 Total Cost $ 237,081 Cost/Hour $ 1, Cost/Statute Mile $ 3.95 Cost/Seat Mile $ 0.56

7 Turbo Commander 840 Specifications and Performance DIMENSIONS FEET OPERATING SPEEDS KTAS Wing Span (at 10,250 lbs, unless otherwise noted) Length Maximum Speed (100% 12,000 ft, TAS) 290 Height Normal Cruise (FL 180) 287 Cabin Entry Door 2.21 x 3.92 Twin Engine Best Rate of Climb 135 Cabin Height 4.48 Twin Engine Best Angle of Climb 84 Cabin Width 4.12 Single Engine Best Rate of Climb 113 Cabin Length Single Engine Best Angle of Climb 97 Cabin Volume (Cubic ft) 224 Minimum Control Speed 96 Baggage Volume (Cubic ft) 70 Stall Speed, Clean 77 Baggage Door Height 2.6 Stall Speed, Gear & Flaps Down 75 Baggage Door Width 2.08 CLIMB Ft/Min. WEIGHTS POUNDS Twin Engine Initial Rate of Climb (0 Flaps) 2824 Ramp Weight Time to Climb to 10,000 ft (Minutes) 3.80 Takeoff Weight Time to Climb to 20,000 ft (Minutes) 9.50 Landing Weight 9675 Single Engine Rate of Climb (0 Flaps) 1003 Typical Empty Weight 6635 Useful Load 3740 CEILING FEET Zero Fuel Weight 8800 Operational Ceiling Limit Baggage Compartment 600 Twin Engine Service Ceiling Twin Engine Absolute Ceiling Single Engine Service Ceiling FUEL GALLONS Maximum Pressurization Differential (PSI) 5.2 Standard (Useable) 425 Optional (Useable) 474 TAKE OFF FEET Take Off Distance - Ground Roll (0 Flaps) 1285 LOADING Take Off Distance - over 50 ft Obstacle 1833 Wing Area Sq. Ft. Wing Loading Lbs/Sq. Ft. LANDING FEET Power Loading 7.20 Lbs/SHP Landing Distance - with Reverse 1240 Landing Distance - Over 50 ft Obstacle 2332 POWERPLANT Honeywell TPE K Single Shaft Turbo-prop with integral gearbox, two stage centrifugal compressor, three stage axial turbine, single annular combustion chamber. PROPELLERS Dowty-Rotol 3-Bladed with Full Feather and Reversible Engine Limits SHP RPM ITT PERFORMANCE CONDITIONS Takeoff C Max Continuous C Overhaul Intervals Hot Section Intervals Gear Box intervals 5,400 hours 1,800 hours 3,600 hours Performance estimations are based upon U.S. Standard (I 962) atmospheric conditions and performance is contingent upon engine manufacturer s performance as indicated in FAA Type Certificate. All speeds within plus or minus 3% and all climbs, ranges and altitudes are within plus or minus 8%. All information was taken from the Manufacturer s publications and is subject to change and buyer s verification.

8 Turbo Commander 840 Estimated Operating Costs Fuel $ Fuel Costs/Gallon $ 6.25 Fuel Burn/Hour (Gallons) $ Maintenance $ Labor/Hour $ Parts/Hour $ Engine Reserves (Overhaul, Hot Section, Gearbox) $ Prop Overhaul $ Miscellaneous Flight Expenses $ 8.06 Total Direct Costs Per Hour $ 1, Average Block Speed (MPH) 295 Cost Per Statute Mile $ 3.54 Hangar Costs $ 8,500 Insurance $ 12,800 Hull $ 8,000 Legal Liability $ 4,800 Miscellaneous Overhead $ 15,000 Training $ 7,000 Aircraft Modernization $ 5,000 Navigation Equipment $ 3,000 Total Fixed Costs $ 36,300 Annual Budget Utilization Number of Seats 7 Miles 60,000 Hours 203 Direct Cost $ 212,009 Fixed Cost $ 36,300 Total Cost $ 248,309 Cost/Hour $ 1, Cost/Statute Mile $ 4.14 Cost/Seat Mile $ 0.59

9 Dash Ten Turbo Commander 840 Specifications and Performance Wing Span feet Length feet Height feet Total cabin & Baggage Vol cubic Feet Baggage volume and load 70 cubic feet/600 pounds Maximum Ramp weight 10,375 pounds Max gross takeoff weight 10,375 pounds Fuel Capacity, usable 425 gallons (Standard) Range 1,700+ nm Cruise Speed Single Engine Cruise Speed 305+ KTAS (Gross) 26,000-27,000 feet, ISA 218+ KTAS (9000 lbs) 15,000 feet, ISA Climb: Single Engine R of C Time to Climb 2,824 Initial Rate of Climb, Gross, SL, ISA 1,003 Initial Rate of Climb, Gross, SL, ISA 12.9 minutes to 29,000 ft (9000 lbs. ISA) Stall Speed, Clean Stall Speed, Gear/Flaps Dn Take-off over 50' Take-off roll Landing Roll w/reverse 77 Knots (CAS) (Gross Wt) 75 Knots (CAS) (Gross Wt) 1,833 Feet (Gross Wt) 1,285 Feet (Gross Wt) 1,240 Feet (Typical landing weight) Engine TBO Engine HSI Interval Nautical Miles to Overhaul 5,000 Hours 2,500 Hours Over One Million Miles! The Dash Ten 840 is a high performance turboprop that will rival the Citation I in climb and segment times at a fraction of the segment fuel burn. The flat rated take-off power is available up to 15,000 feet, ISA, allowing unmatched single engine safety, even at high density altitudes. This is without a doubt, a pilot's airplane.

10 Dash Ten Turbo Commander 840 Estimated Operating Costs Fuel $ Fuel Costs/Gallon $ 6.25 Fuel Burn/Hour (Gallons) $ Maintenance $ Labor/Hour $ Parts/Hour $ Engine Reserves (Overhaul, Hot Section, Gearbox) $ Prop Overhaul $ Miscellaneous Flight Expenses $ 8.06 Total Direct Costs Per Hour $ 1, Average Block Speed (MPH) 345 Cost Per Statute Mile $ 3.04 Hangar Costs $ 8,500 Insurance $ 12,800 Hull $ 8,000 Legal Liability $ 4,800 Miscellaneous Overhead $ 15,000 Training $ 7,000 Aircraft Modernization $ 5,000 Navigation Equipment $ 3,000 Total Fixed Costs $ 36,300 Annual Budget Utilization Number of Seats 7 Miles 60,000 Hours 174 Direct Cost $ 182,519 Fixed Cost $ 36,300 Total Cost $ 218,819 Cost/Hour $ 1, Cost/Statute Mile $ 3.65 Cost/Seat Mile $ 0.52

11 Turbo Commander 900 Specifications and Performance DIMENSIONS FEET OPERATING SPEEDS KTAS Height Normal Cruise (FL 150) 284 Cabin Entry Door 2.21 x 3.92 Twin Engine Best Rate of Climb 135 Cabin Height 4.77 Twin Engine Best Angle of Climb 93 Cabin Width 4.17 Single Engine Best Rate of Climb 112 Cabin Length Single Engine Best Angle of Climb 97 Cabin Volume (Cubic ft) Minimum Control Speed 90 Baggage Volume (Cubic ft) Stall Speed, Clean 79 Baggage Door Height 2.58 Stall Speed, Gear & Flaps Down 77 Baggage Door Width 1.83 CLIMB Ft/Min. WEIGHTS POUNDS Twin Engine Initial Rate of Climb (0 Flaps) 2,779 Ramp Weight 10,775 Time to Climb to 1 0,000 ft (Minutes) 4.00 Takeoff Weight 10,700 Time to Climb to 20,000 ft (Minutes) Landing Weight 10,550 Single Engine Rate of Climb (0 Flaps) 924 Typical Empty Weight 7,000 Useful Load 3,775 CEILING FEET Zero Fuel Weight 9,000 Operational Ceiling Limit 31,000 Baggage Compartment 600 Twin Engine Service Ceiling 32,245 Twin Engine Absolute Ceiling 33,401 Single Engine Service Ceiling 18,140 FUEL GALLONS Maximum Pressurization Differential (PSI) 6.7 Standard (Useable) 425 Optional (Useable) 474 TAKE OFF FEET Take Off Distance - Ground Roll (0 Flaps) 1,387 LOADING Take Off Distance - Over 50 ft Obstacle 1,937 Wing Area Sq. Ft. Wing Loading Lbs/Sq. Ft. LANDING FEET Power Loading 7.15 Lbs/SHP Landing Distance - with Reverse 1,411 Landing Distance - Over 50 ft Obstacle 2,698 POWER PLANT Honeywell TPE K Single Shaft Turbo-prop with integral gearbox, two stage centrifugal compressor, three stage axial turbine, single annular combustion chamber. PROPELLERS Dowty-Rotol 3-Bladed with Full Feather and Reversible Engine Limits SHP RPM ITT Takeoff C Max Continuous C Overhaul Intervals 5,400 hours Hot Section Intervals 1,800 hours Gear Box intervals 3,600 hours Performance estimations are based upon U.S. Standard (I 962) atmospheric conditions and performance is contingent upon engine manufacturer s performance as indicated in FAA Type Certificate. All speeds within plus or minus 3% and all climbs, ranges and altitudes are within plus or minus 8%. All information was taken from the Manufacturer s publications and is subject to change and buyer s verification.

12 Turbo Commander 900 Estimated Operating Costs Fuel $ Fuel Costs/Gallon $ 6.25 Fuel Burn/Hour (Gallons) $ Maintenance $ Labor/Hour $ Parts/Hour $ Engine Reserves (Overhaul, Hot Section, Gearbox) $ Prop Overhaul $ Miscellaneous Flight Expenses $ 8.06 Total Direct Costs Per Hour $ 1, Average Block Speed (MPH) 300 Cost Per Statute Mile $ 3.48 Hangar Costs $ 8,500 Insurance $ 17,800 Hull $ 13,000 Legal Liability $ 4,800 Miscellaneous Overhead $ 15,000 Training $ 7,000 Aircraft Modernization $ 5,000 Navigation Equipment $ 3,000 Total Fixed Costs $ 41,300 Annual Budget Utilization Number of Seats 7 Miles 60,000 Hours 200 Direct Cost $ 208,876 Fixed Cost $ 41,300 Total Cost $ 250,176 Cost/Hour $ 1, Cost/Statute Mile $ 4.17 Cost/Seat Mile $ 0.60

13 Dash Ten Turbo Commander 900 Specifications and Performance Wing Span feet Length feet Height feet Total cabin & Baggage Vol cubic Feet Baggage volume and load 70 cubic feet/600 pounds Maximum Ramp weight 10,775 pounds Max gross takeoff weight 10,700 pounds Fuel Capacity, usable 425 gallons (Standard) Range 1,700+ nm Cruise Speed Single Engine Cruise Speed 305+ KTAS (Gross) 26,000-27,000 feet, ISA 218+ KTAS (9000 lbs) 15,000 feet, ISA Climb: Single Engine R of C Time to Climb 2,824 Initial Rate of Climb, Gross, SL, ISA 1,003 Initial Rate of Climb, Gross, SL, ISA 12.9 minutes to 29,000 ft (9000 lbs. ISA) Stall Speed, Clean Stall Speed, Gear/Flaps Dn Take-off over 50' Take-off roll Landing Roll w/reverse 77 Knots (CAS) (Gross Wt) 75 Knots (CAS) (Gross Wt) 1,833 Feet (Gross Wt) 1,285 Feet (Gross Wt) 1,240 Feet (Typical landing weight) Engine TBO Engine HSI Interval Nautical Miles to Overhaul 5,000 Hours 2,500 Hours Over One Million Miles! The Dash Ten 900 is a high performance turboprop that will rival the Citation I in climb and segment times at a fraction of the segment fuel burn. The flat rated take-off power is available up to 15,000 feet, ISA, allowing unmatched single engine safety, even at high density altitudes. This is without a doubt, a pilot's airplane.

14 Turbo Commander 900 Dash Ten Estimated Operating Costs Fuel $ Fuel Costs/Gallon $ 6.25 Fuel Burn/Hour (Gallons) 83 Maintenance $ Labor/Hour $ Parts/Hour $ Engine Reserves (Overhaul, Hot Section, Gearbox) $ Prop Overhaul $ Miscellaneous Flight Expenses $ 8.06 Total Direct Costs Per Hour $ 1, Average Block Speed (MPH) 345 Cost Per Statute Mile $ 3.04 Hangar Costs $ 8,500 Insurance $ 17,800 Hull $ 13,000 Legal Liability $ 4,800 Miscellaneous Overhead $ 15,000 Training $ 7,000 Aircraft Modernization $ 5,000 Navigation Equipment $ 3,000 Total Fixed Costs $ 41,300 Annual Budget Utilization Number of Seats 7 Miles 60,000 Hours 174 Direct Cost $ 182,519 Fixed Cost $ 41,300 Total Cost $ 223,819 Cost/Hour $ 1, Cost/Statute Mile $ 3.73 Cost/Seat Mile $ 0.53

15 Turbo Commander 980 Specifications and Performance DIMENSIONS FEET OPERATING SPEEDS KTAS Wing Span (at 10,250 lbs, unless otherwise noted) Length Maximum Speed (100% 12,000 ft, TAS) 309 Height Normal Cruise 303 Cabin Entry Door 2.21 x 3.92 Twin Engine Best Rate of Climb 135 Cabin Height 4.48 Twin Engine Best Angle of Climb 93 Cabin Width 4.12 Single Engine Best Rate of Climb 113 Cabin Length Single Engine Best Angle of Climb 97 Cabin Volume (Cubic ft) Minimum Control Speed 93 Baggage Volume (Cubic ft) Stall Speed, Clean 77 Baggage Door Height 2.60 Stall Speed, Gear & Flaps Down 75 Baggage Door Width 2.08 CLIMB Ft/Min. WEIGHTS POUNDS Twin Engine Initial Rate of Climb (0 Flaps) 2,777 Ramp Weight 10,375 Time to Climb to 10,000 ft (Minutes) 4.00 Takeoff Weight 10,325 Time to Climb to 20,000 ft (Minutes) 8.00 Landing Weight 9,675 Single Engine Rate of Climb (0 Flaps) 982 Typical Empty Weight 6,733 Useful Load 3,642 CEILING FEET Zero Fuel Weight 8,800 Operational Ceiling Limit 31,000 Baggage Compartment 600 Twin Engine Service Ceiling 37,369 Twin Engine Absolute Ceiling 34,000 Single Engine Service Ceiling 24,850 FUEL GALLONS Maximum Pressurization Differential (PSI) 5.2 Standard (Useable) 474 TAKE OFF FEET Take Off Distance - Ground Roll (0 Flaps) 1,299 LOADING Take Off Distance - Over 50 ft Obstacle 1,854 Wing Area Sq. Ft. Wing Loading Lbs/Sq. Ft. LANDING FEET Power Loading 7.04 Lbs/SHP Landing Distance - with Reverse 1,277 Landing Distance - Over 50 ft Obstacle 2,310 POWER PLANT Honeywell TPE K Single Shaft Turbo-prop with integral gearbox, two stage centrifugal compressor, three stage axial turbine, single annular combustion chamber. PROPELLERS Dowty-Rotol 3-Bladed with Full Feather and Reversible ENGINE LIMITS: SHP RPM PERFORMANCE CONDITIONS Takeoff 733 1,591 Max Continuous 733 1,591 Overhaul Intervals 5,400 hours (opt. 5000) Hot Section Intervals 1,800 hours Gear Box intervals 3,600 hours Performance estimations are based upon U.S. Standard (I 962) atmospheric conditions and performance is contingent upon engine manufacturer s performance as indicated in FAA Type Certificate. All speeds within plus or minus 3% and all climbs, ranges and altitudes are within plus or minus 8%. All information was taken from the Manufacturer s publications and is subject to change and buyer s verification.

16 Turbo Commander 980 Dash Ten Estimated Operating Costs Fuel $ Fuel Costs/Gallon $ 6.25 Fuel Burn/Hour (Gallons) 83 Maintenance $ Labor/Hour $ Parts/Hour $ Engine Reserves (Overhaul, Hot Section, Gearbox) $ Prop Overhaul $ Miscellaneous Flight Expenses $ 8.06 Total Direct Costs Per Hour $ 1, Average Block Speed (MPH) 345 Cost Per Statute Mile $ 2.99 Hangar Costs $ 8,500 Insurance $ 12,800 Hull $ 8,000 Legal Liability $ 4,800 Miscellaneous Overhead $ 15,000 Training $ 7,000 Aircraft Modernization $ 5,000 Navigation Equipment $ 3,000 Total Fixed Costs $ 36,300 Annual Budget Utilization Number of Seats 7 Miles 60,000 Hours 174 Direct Cost $ 179,317 Fixed Cost $ 36,300 Total Cost $ 215,617 Cost/Hour $ 1, Cost/Statute Mile $ 3.59 Cost/Seat Mile $ 0.51

17 DIMENSIONS FEET OPERATING SPEEDS KTAS Wing Span (at 10,250 lbs, unless otherwise noted) Length Maximum Speed (100% 22,000 ft, TAS) 308 Height Normal Cruise (FL 180) 302 Cabin Entry Door 2.21 x 3.92 Twin Engine Best Rate of Climb 138 Cabin Height 4.77 Twin Engine Best Angle of Climb 98 Cabin Width 4.17 Single Engine Best Rate of Climb 120 Cabin Length Single Engine Best Angle of Climb 102 Cabin Volume (Cubic ft) Minimum Control Speed 95 Baggage Volume (Cubic ft) Stall Speed, Clean 81 Baggage Door Height 2.58 Stall Speed, Gear & Flaps Down 77 Baggage Door Width 1.83 CLIMB Ft/Min. WEIGHTS POUNDS Twin Engine Initial Rate of Climb (0 Flaps) 2,802 Ramp Weight 11,250 Time to Climb to 10,000 ft (Minutes) 3.5 Takeoff Weight 11,200 Time to Climb to 20,000 ft (Minutes) 8.8 Landing Weight 10,550 Single Engine Rate of Climb (0 Flaps) 929 Typical Empty Weight 7,210 Useful Load 4,040 CEILING FEET Zero Fuel Weight 9,000 Operational Ceiling Limit 35,000 Baggage Compartment 600 Twin Engine Service Ceiling 35,000 Twin Engine Absolute Ceiling 36,000 Single Engine Service Ceiling 24,850 FUEL GALLONS Maximum Pressurization Differential (PSI) 6.7 Standard (Useable) 474 TAKE OFF FEET Take Off Distance - Ground Roll 1,407 LOADING Take Off Distance - Over 50 ft Obstacle 2,131 Wing Area Sq. Ft. Wing Loading Lbs/Sq. Ft. LANDING FEET Power Loading 6.83 Lbs/SHP Landing Distance - with Reverse 1,395 Landing Distance - Over 50 ft Obstacle 2,670 POWER PLANT Turbo Commander 1000 Specifications and Performance Honeywell TPE K Single Shaft Turbo-prop with integral gearbox, two stage centrifugal compressor, three stage axial turbine, single annular combustion chamber. PROPELLERS Dowty-Rotol 3-Bladed with Full Feather and Reversible Engine Limits SHP RPM EGT PERFORMANCE CONDITIONS Takeoff Max Continuous Overhaul Intervals 5,400 hours (opt. 5000) Hot Section Intervals 1,800 hours (opt. 2500) Gear Box intervals 3,600 hours (opt 5000) Performance estimations are based upon U.S. Standard (I 962) atmospheric conditions and performance is contingent upon engine manufacturer s performance as indicated in FAA Type Certificate. All speeds within plus or minus 3% and all climbs, ranges and altitudes are within plus or minus 8%. All information was taken from the Manufacturer s publications and is subject to change and buyer s verification.

18 Turbo Commander 1000 Dash Ten Estimated Operating Costs Fuel $ Fuel Costs/Gallon $ 6.25 Fuel Burn/Hour (Gallons) 83 Maintenance $ Labor/Hour $ Parts/Hour $ Engine Reserves (Overhaul, Hot Section, Gearbox) $ Prop Overhaul $ Miscellaneous Flight Expenses $ 8.06 Total Direct Costs Per Hour $ 1, Average Block Speed (MPH) 345 Cost Per Statute Mile $ 2.99 Hangar Costs $ 8,500 Insurance $ 17,800 Hull $ 13,000 Legal Liability $ 4,800 Miscellaneous Overhead $ 15,000 Training $ 7,000 Aircraft Modernization $ 5,000 Navigation Equipment $ 3,000 Total Fixed Costs $ 41,300 Annual Budget Utilization Number of Seats 7 Miles 60,000 Hours 174 Direct Cost $ 179,317 Fixed Cost $ 41,300 Total Cost $ 220,617 Cost/Hour $ 1, Cost/Statute Mile $ 3.68 Cost/Seat Mile $ 0.53

19 Selling an aircraft is just the first step in what we hope is a long and rewarding relationship. At Eagle Creek, our customers are treated with just as much care after a sale as before. We are known for our unmatched after-sales support, uniquely structured to keep you flying even when your aircraft is in for maintenance. We have a full staff of pilots who can pick-up and deliver your airplane virtually anywhere. We are able to proved loaner airplanes (when available) so you experience as little disruption to your schedule as possible. Our extensive parts inventory provides us access to replacement components faster than anyone in the business. And you have access to someone that can help with a problem or answer questions 24/7. Transition Pilot Training - Experienced on-staff ATP instructors with literally thousands of hours in Turbine Commanders fly with you for hours in your aircraft, then fly with you to Flight Safety for their 5 day school, and afterwards, fly with you or your pilot until you are ready to go it alone! This method of using the simulator-based training coupled with real world flying with Commander experts result in a safe, fully knowledgeable professional Turbine Commander pilot. In addition, Flight Safety discounts are available with Aircraft purchases through Eagle Creek. In today s complex maze of I.R.S. and F.A.A. regulations, proper ownership structure and design, along with detailed record keeping are critical. We can assist with Aircraft Financing, Trade- Ins and Like Kind Exchange Support. With over 3000 aircraft transactions since Yes, 3000.you can rest assured we are up to the task! No one else has Eagle Creek s one-stop solutions. after-sales support

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