commander package 2013
TRANSCRIPT
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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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7/25/2019 Commander Package 2013
4/20
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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7/25/2019 Commander Package 2013
5/20
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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7/25/2019 Commander Package 2013
6/20
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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7/25/2019 Commander Package 2013
7/20
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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7/25/2019 Commander Package 2013
8/20
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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7/25/2019 Commander Package 2013
9/20
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**
-
7/25/2019 Commander Package 2013
10/20
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**
-
7/25/2019 Commander Package 2013
11/20
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
-
7/25/2019 Commander Package 2013
12/20
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**
-
7/25/2019 Commander Package 2013
13/20
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
-
7/25/2019 Commander Package 2013
14/20
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**
-
7/25/2019 Commander Package 2013
15/20
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
-
7/25/2019 Commander Package 2013
16/20
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**
-
7/25/2019 Commander Package 2013
17/20
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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7/25/2019 Commander Package 2013
18/20
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**
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7/25/2019 Commander Package 2013
19/20
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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7/25/2019 Commander Package 2013
20/20
4101 dandy trail indianapolis, in 46254 ph 317.293.6935 fx 317.297.9341
www.eagle-creek.com