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  • 7/25/2019 Commander Package 2013

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    Commander InformationEstimated Specs, Performance & Operating Costs

    Early 2014

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    Eagle Creek Aviation Services provides aircraft

    sales and service to owners and operators of Twin

    Commander, Embraer Phenom, and Cessna Cita-

    tion aircraft. Aircraft owners rely on Eagle Creek

    Aviation as their trusted partner in maximizing

    the utilization and enjoyment of their planes.

    Eagle Creeks hard-earned reputation for excel-

    lence in buying and selling aircraft is matched

    only by the companys award-winning service.

    As one of the Midwests leading aircraft service

    hubs, Eagle Creek offers a broad range of main-

    tenance, refurbishment, repair and inspection

    services.

    Eagle Creek also has a second location called

    Naples Jet Center in Naples, FL

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    DIMENSIONS FEET OPERATING SPEEDS KTAS

    Wing Span

    46.67 (at 10,250 lbs, unless otherwise noted)

    Length 44.35 Maximum Speed (100% 12,000 ft, TAS) 285

    Height 14.95 Normal Cruise (96%, 20,000 Ft., TAS) 275

    Tread 15.42 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 14.25 Minimum Control Speed, CAS 99

    Cabin Volume (Cubic ft) 224.00 Stall Speed, Clean 78

    Baggage Volume (Cubic ft) 45.00 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 FEETTake 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 38.53 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 717.5 1591 923C

    Max Continuous 717.5 1591 923C

    Overhaul Intervals 5,400 hours

    Hot Section Intervals 1,800 hours

    Gear Box intervals 3,600 hours

    Turbo Commander 690A B

    Specifications and Performance

    Performance estimations are based upon U.S. Standard (I 962) atmospheric

    conditions and performance is contingent upon engine manufacturers

    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 Manufacturers publications and is subject to

    change and buyers verification.

    Honeywell TPE331-5-251 K Single Shaft Turbo-prop

    with integral gearbox, two stage centrifugal

    compressor, three stage axial turbine, single annular

    combustion chamber.Hartzell 102 Inch Diameter, 3-Blade, Constant Speed, Full Feathering

    and Reversible

    4101 Dandy Trail

    indianapolis in 46254

    www.eagle-creek.com

    ph 317.293.6935

    fx 317.297.9341

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    Fuel 487.50$

    Fuel Costs/Gallon 6.25$

    Fuel Burn/Hour (Gallons) 78.00$

    Maintenance 648.72$

    Labor/Hour 187.20$

    Parts/Hour 262.79$

    Engine Reserves (Overhaul, Hot Section, Gearbox) 166.67$

    Prop Overhaul 24.00$

    Miscellaneous Flight Expenses 8.06$

    Total Direct Costs Per Hour 1,136.22$

    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 1,305.85$

    Cost/Statute Mile 4.66$

    Cost/Seat Mile 0.67$

    www.eagle-creek.com

    indianapolis in 46254

    ph 317.293.6935

    Turbo Commander 690A B

    Estimated Operating Costs

    4101 Dandy Trail

    **All information is subject to change and buyer's verification**

    fx 317.297.9341

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    Wing Span 46.67 feet

    Length 44.35 feet

    Height 14.95 feetTotal cabin & Baggage Vol 294.00 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 305+ KTAS (Gross) 26,000 - 27,000 feet, ISA

    Single Engine Cruise Speed 218+ KTAS (9000 lbs) 15,000 feet, ISA

    Climb: 2,824 Initial Rate of Climb, Gross, SL, ISA

    Single Engine R of C 1,003 Initial Rate of Climb, Gross, SL, ISA

    Time to Climb 12.9 minutes to 29,000 ft (9000 lbs. ISA)

    Stall Speed, Clean 77 Knots (CAS) (Gross Wt)

    Stall Speed, Gear/Flaps Dn 75 Knots (CAS) (Gross Wt)

    Take-off over 50' 1,833 Feet (Gross Wt)

    Take-off roll 1,285 Feet (Gross Wt)

    Landing Roll w/Reverse 1,240 Feet (Typical landing weight)

    Engine TBO 5,000 Hours

    Engine HSI Interval 2,500 Hours

    Nautical Miles to Overhaul Over One Million Miles!

    **All information is subject to change and buyer's verification**

    Turbo Commander 690A B Dash Ten

    Specifications and Performance

    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.

    4101 Dandy Trail

    www.eagle-creek.com

    indianapolis, in 46254

    ph 317.293.6935

    fx 317.297.9341

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    Dash Ten Turbo Commander 690A B

    Estimated Operating Costs

    Fuel 518.75$

    Fuel Costs/Gallon 6.25$

    Fuel Burn/Hour (Gallons) 83.00$

    Maintenance 622.05$

    Labor/Hour 187.20$

    Parts/Hour 262.79$

    Engine Reserves (Overhaul, Hot Section, Gearbox) 140.00$

    Prop Overhaul 24.00$

    Miscellaneous Flight Expenses 8.06$

    Total Direct Costs Per Hour 1,140.80$

    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 1,347.05$

    Cost/Statute Mile 3.95$

    Cost/Seat Mile 0.56$

    fx 317.297.9341

    www.eagle-creek.com

    4101 Dandy Trail

    **All information is subject to change and buyer's verification**

    indianapolis, in 46254

    ph 317.293.6935

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    Turbo Commander 840

    Specifications and Performance

    DIMENSIONS FEET OPERATING SPEEDS KTAS

    Wing Span 52.12 (at 10,250 lbs, unless otherwise noted)

    Length 42.98 Maximum Speed (100% 12,000 ft, TAS) 290

    Height 14.95 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 14.25 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 10375 Time to Climb to 10,000 ft (Minutes) 3.80

    Takeoff Weight 10325 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 31000

    Baggage Compartment 600 Twin Engine Service Ceiling 34000

    Twin Engine Absolute Ceiling 35100

    Single Engine Service Ceiling 21000

    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 279.37 Sq. Ft.

    Wing Loading 36.96 Lbs/Sq. Ft. LANDING FEET

    Power Loading 7.20 Lbs/SHP Landing Distance - with Reverse 1240

    Landing Distance - Over 50 ft Obstacle 2332

    POWERPLANTPROPELLERS

    Dowty-Rotol 3-Bladed with Full Feather and Reversible

    Engine Limits SHP RPM ITT PERFORMANCE CONDITIONS

    Takeoff 717.5 1591 923C

    Max Continuous 717.5 1591 923C

    Overhaul Intervals 5,400 hours

    Hot Section Intervals 1,800 hours

    Gear Box intervals 3,600 hours

    fx 317.297.9341

    www.eagle-creek.com

    Performance estimations are based upon U.S. Standard (I 962) atmospheric

    conditions and performance is contingent upon engine manufacturers

    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 Manufacturers publications and is subject to

    change and buyers verification.

    Honeywell TPE331-5-254 K Single Shaft Turbo-prop

    with integral gearbox, two stage centrifugal

    compressor, three stage axial turbine, single annular

    combustion chamber.

    4101 Dandy Trail

    indianapolis, in 46254

    ph 317.293.6935

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    Turbo Commander 840

    Estimated Operating Costs

    Fuel 487.50$

    Fuel Costs/Gallon 6.25$

    Fuel Burn/Hour (Gallons) 78.00$

    Maintenance 556.88$

    Labor/Hour 140.13$

    Parts/Hour 218.02$

    Engine Reserves (Overhaul, Hot Section, Gearbox) 166.67$

    Prop Overhaul 24.00$

    Miscellaneous Flight Expenses 8.06$

    Total Direct Costs Per Hour 1,044.38$

    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 1,223.20$

    Cost/Statute Mile 4.14$

    Cost/Seat Mile 0.59$

    ph 317.293.6935

    fx 317.297.9341

    www.eagle-creek.com

    4101 Dandy Trail

    indianapolis, in 46254

    **All information is subject to change and buyer's verification**

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    Dash Ten Turbo Commander 840

    Specifications and Performance

    Wing Span 52.12 feet

    Length 42.98 feet

    Height 14.95 feet

    Total cabin & Baggage Vol 294.00 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 305+ KTAS (Gross) 26,000 - 27,000 feet, ISA

    Single Engine Cruise Speed 218+ KTAS (9000 lbs) 15,000 feet, ISA

    Climb: 2,824 Initial Rate of Climb, Gross, SL, ISA

    Single Engine R of C 1,003 Initial Rate of Climb, Gross, SL, ISA

    Time to Climb 12.9 minutes to 29,000 ft (9000 lbs. ISA)

    Stall Speed, Clean 77 Knots (CAS) (Gross Wt)

    Stall Speed, Gear/Flaps Dn 75 Knots (CAS) (Gross Wt)

    Take-off over 50' 1,833 Feet (Gross Wt)

    Take-off roll 1,285 Feet (Gross Wt)

    Landing Roll w/Reverse 1,240 Feet (Typical landing weight)

    Engine TBO 5,000 Hours

    Engine HSI Interval 2,500 Hours

    Nautical Miles to Overhaul 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.

    4101 Dandy Trail

    indianapolis, in 46254

    ph 317.293.6935

    fx 317.297.9341

    www.eagle-creek.com

    **All information is subject to change and buyer's verification**

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    Dash Ten Turbo Commander 840

    Estimated Operating Costs

    Fuel 518.75$

    Fuel Costs/Gallon 6.25$

    Fuel Burn/Hour (Gallons) 83.00$

    Maintenance 530.21$

    Labor/Hour 140.13$

    Parts/Hour 218.02$

    Engine Reserves (Overhaul, Hot Section, Gearbox) 140.00$

    Prop Overhaul 24.00$

    Miscellaneous Flight Expenses 8.06$

    Total Direct Costs Per Hour 1,048.96$

    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 1,257.58$

    Cost/Statute Mile 3.65$

    Cost/Seat Mile 0.52$

    ph 317.293.6935

    fx 317.297.9341

    www.eagle-creek.com

    4101 Dandy Trail

    indianapolis, in 46254

    **All information is subject to change and buyer's verification**

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    Turbo Commander 900

    Specifications and Performance

    DIMENSIONS FEET OPERATING SPEEDS KTAS

    Height 14.95 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 17.50 Single Engine Best Angle of Climb 97

    Cabin Volume (Cubic ft) 278.00 Minimum Control Speed 90

    Baggage Volume (Cubic ft) 46.00 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) 10.20

    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 279.37 Sq. Ft.

    Wing Loading 38.30 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

    PROPELLERS

    Dowty-Rotol 3-Bladed with Full Feather and Reversible

    Engine Limits SHP RPM ITTTakeoff 748.3 1591 923C

    Max Continuous 748.3 1591 923C

    Overhaul Intervals 5,400 hours

    Hot Section Intervals 1,800 hours

    Gear Box intervals 3,600 hours

    www.eagle-creek.com

    Honeywell TPE331-5-254 K Single Shaft Turbo-prop

    with integral gearbox, two stage centrifugal

    compressor, three stage axial turbine, single annular

    combustion chamber.

    Performance estimations are based upon U.S. Standard (I 962) atmospheric

    conditions and performance is contingent upon engine manufacturers

    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 Manufacturers publications and is subject to

    change and buyers verification.

    4101 Dandy Trail

    indianapolis, in 46254

    ph 317.293.6935

    fx 317.297.9341

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    Turbo Commander 900

    Estimated Operating Costs

    Fuel 487.50$

    Fuel Costs/Gallon 6.25$

    Fuel Burn/Hour (Gallons) 78.00$

    Maintenance 556.88$

    Labor/Hour 140.13$

    Parts/Hour 218.02$

    Engine Reserves (Overhaul, Hot Section, Gearbox) 166.67$

    Prop Overhaul 24.00$

    Miscellaneous Flight Expenses 8.06$

    Total Direct Costs Per Hour 1,044.38$

    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 1,250.88$

    Cost/Statute Mile 4.17$

    Cost/Seat Mile 0.60$

    ph 317.293.6935

    fx 317.297.9341

    www.eagle-creek.com

    4101 Dandy Trail

    indianapolis, in 46254

    **All information is subject to change and buyer's verification**

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    Dash Ten Turbo Commander 900

    Specifications and Performance

    Wing Span 52.12 feet

    Length 42.98 feet

    Height 14.95 feet

    Total cabin & Baggage Vol 294.00 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 305+ KTAS (Gross) 26,000 - 27,000 feet, ISA

    Single Engine Cruise Speed 218+ KTAS (9000 lbs) 15,000 feet, ISA

    Climb: 2,824 Initial Rate of Climb, Gross, SL, ISA

    Single Engine R of C 1,003 Initial Rate of Climb, Gross, SL, ISA

    Time to Climb 12.9 minutes to 29,000 ft (9000 lbs. ISA)

    Stall Speed, Clean 77 Knots (CAS) (Gross Wt)

    Stall Speed, Gear/Flaps Dn 75 Knots (CAS) (Gross Wt)

    Take-off over 50' 1,833 Feet (Gross Wt)

    Take-off roll 1,285 Feet (Gross Wt)

    Landing Roll w/Reverse 1,240 Feet (Typical landing weight)

    Engine TBO 5,000 Hours

    Engine HSI Interval 2,500 Hours

    Nautical Miles to Overhaul Over One Million Miles!

    www.eagle-creek.com

    **All information is subject to change and buyer's verification**

    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.

    4101 Dandy Trail

    indianapolis, in 46254

    ph 317.293.6935

    fx 317.297.9341

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    Turbo Commander 900 Dash Ten

    Estimated Operating Costs

    Fuel 518.75$

    Fuel Costs/Gallon 6.25$

    Fuel Burn/Hour (Gallons) 83

    Maintenance 530.21$

    Labor/Hour 140.13$

    Parts/Hour 218.02$

    Engine Reserves (Overhaul, Hot Section, Gearbox) 140.00$

    Prop Overhaul 24.00$

    Miscellaneous Flight Expenses 8.06$

    Total Direct Costs Per Hour 1,048.96$

    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 1,286.32$

    Cost/Statute Mile 3.73$

    Cost/Seat Mile 0.53$

    ph 317.293.6935

    fx 317.297.9341

    www.eagle-creek.com

    4101 Dandy Trail

    indianapolis, in 46254

    **All information is subject to change and buyer's verification**

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    Turbo Commander 980

    Specifications and Performance

    DIMENSIONS FEET OPERATING SPEEDS KTAS

    Wing Span 52.12 (at 10,250 lbs, unless otherwise noted)

    Length 42.98 Maximum Speed (100% 12,000 ft, TAS) 309

    Height 14.95 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 14.25 Single Engine Best Angle of Climb 97

    Cabin Volume (Cubic ft) 224.00 Minimum Control Speed 93

    Baggage Volume (Cubic ft) 70.00 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 279.37 Sq. Ft.

    Wing Loading 36.96 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

    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

    www.eagle-creek.com

    Performance estimations are based upon U.S. Standard (I 962) atmospheric

    conditions and performance is contingent upon engine manufacturers

    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 Manufacturers publications and is subject to

    change and buyers verification.

    Honeywell TPE331-10-501K Single Shaft Turbo-prop with

    integral gearbox, two stage centrifugal compressor, three stage

    axial turbine, single annular combustion chamber.

    4101 Dandy Trail

    indianapolis, in 46254

    ph 317.293.6935

    fx 317.297.9341

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    Turbo Commander 980 Dash Ten

    Estimated Operating Costs

    Fuel 518.75$

    Fuel Costs/Gallon 6.25$

    Fuel Burn/Hour (Gallons) 83

    Maintenance 511.81$

    Labor/Hour 140.13$

    Parts/Hour 218.02$

    Engine Reserves (Overhaul, Hot Section, Gearbox) 121.60$

    Prop Overhaul 24.00$

    Miscellaneous Flight Expenses 8.06$

    Total Direct Costs Per Hour 1,030.56$

    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 1,239.18$

    Cost/Statute Mile 3.59$

    Cost/Seat Mile 0.51$

    ph 317.293.6935

    fx 317.297.9341

    www.eagle-creek.com

    4101 Dandy Trail

    indianapolis, in 46254

    **All information is subject to change and buyer's verification**

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    DIMENSIONS FEET OPERATING SPEEDS KTAS

    Wing Span 52.12 (at 10,250 lbs, unless otherwise noted)

    Length 42.98 Maximum Speed (100% 22,000 ft, TAS) 308

    Height 14.95 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 17.25 Single Engine Best Angle of Climb 102

    Cabin Volume (Cubic ft) 278.00 Minimum Control Speed 95

    Baggage Volume (Cubic ft) 46.00 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 279.37 Sq. Ft.

    Wing Loading 40.09 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

    PROPELLERSDowty-Rotol 3-Bladed with Full Feather and Reversible

    Engine Limits SHP RPM EGT PERFORMANCE CONDITIONS

    Takeoff 820.00 1591 650

    Max Continuous 820.00 1591 650

    Overhaul Intervals 5,400 hours (opt. 5000)

    Hot Section Intervals 1,800 hours (opt. 2500)

    Gear Box intervals 3,600 hours (opt 5000)

    www.eagle-creek.com

    Honeywell TPE331-10-501K Single Shaft Turbo-prop

    with integral gearbox, two stage centrifugal

    compressor, three stage axial turbine, single annular

    combustion chamber.

    Turbo Commander 1000

    Specifications and Performance

    4101 Dandy Trail

    Performance estimations are based upon U.S. Standard (I 962) atmospheric

    conditions and performance is contingent upon engine manufacturers

    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 Manufacturers publications and is subject to

    change and buyers verification.

    indianapolis, in 46254

    ph 317.293.6935

    fx 317.297.9341

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    Turbo Commander 1000 Dash Ten

    Estimated Operating Costs

    Fuel 518.75$

    Fuel Costs/Gallon 6.25$

    Fuel Burn/Hour (Gallons) 83

    Maintenance 511.81$

    Labor/Hour 140.13$

    Parts/Hour 218.02$

    Engine Reserves (Overhaul, Hot Section, Gearbox) 121.60$

    Prop Overhaul 24.00$

    Miscellaneous Flight Expenses 8.06$

    Total Direct Costs Per Hour 1,030.56$

    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 1,267.92$

    Cost/Statute Mile 3.68$

    Cost/Seat Mile 0.53$

    ph 317.293.6935

    fx 317.297.9341

    www.eagle-creek.com

    4101 Dandy Trail

    indianapolis, in 46254

    **All information is subject to change and buyer's verification**

  • 7/25/2019 Commander Package 2013

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    We are known for our unmatched after-sales support, uniquely structured to keep you ying

    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 y with you for 10-20 hours in your aircraft, then y with you to Flight

    Safety for their 5 day school, and afterwards, y 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 ying 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 todays 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 1982..Yes,

    3000.you can rest assured we are up to the task! No one else has Eagle Creeks one-stop

    solutions.

    Selling an aircraft is just the rst 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.

    supportafter-sales

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    4101 dandy trail indianapolis, in 46254 ph 317.293.6935 fx 317.297.9341

    www.eagle-creek.com