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Commander 115TC performance and specifications
Specifications
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Engine |
|
Manufacturer |
Textron Lycoming |
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Model
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TIO-540-AG1A |
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Number of Cylinders |
6
|
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Displacement |
541.5
cu. in. (8.87 l) |
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Maximum Power |
270
HP @ 2,575 RPM |
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Recommended TBO |
2,000
hours |
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Propeller |
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Manufacturer |
McCauley |
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Model
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B3D32C419/82 NHA-5 |
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Type
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Constant-Speed, Hydraulic
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Number of Blades |
3
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Diameter |
77"
(1.96 m) |
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Weights |
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Maximum Ramp |
3,305
lbs. (1,499.12 kg) |
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Maximum Take-off |
3,305
lbs. (1,499.12 kg) |
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Standard Empty |
2,152
lbs. (976.13 kg) |
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Max
Baggage Compartment |
200
lbs. (90.72 kg) |
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Standard Useful Load |
1,152
lbs. (522.54 kg) |
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Fuel & Oil Capacity
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Fuel
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90 US
gal./88 usable
(340.65 litres/333.08 usable)
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Oil
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10
quarts (9.46 l) |
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Wing Area/Loadings
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Wing
Area |
152
sq. ft. (14.12 sq. m) |
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Wing
Loading |
21.8
lbs./sq. ft.(105.94 kg/sq. m)
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Power
Loading |
12.2
lbs./hp.(5.53 kg/hp) |
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Performance
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Speeds |
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Maximum |
197
kts.(365 kph) |
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Performance Cruise (75%) @ 25,000
ft. |
187
kts.(347 kph) |
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Performance Cruise (75%) @ 17,500
ft. |
177
kts.(328 kph) |
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Performance Cruise (75%) @ 12,500
ft. |
170
kts.(315 kph) |
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Stall
(Cruise Configuration)
|
66
kts.(122 kph) |
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Stall
(Landing Configuration)
|
59
kts.(109 kph) |
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Takeoff Performance
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Ground Roll |
1,408
ft. (429.15 m) |
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Distance over 50 ft. Obstacle
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2,223
ft. (677.56 m) |
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Climb Performance |
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Initial S.L. Rate of Climb
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1,050
ft./min.(320.04 m/min.)
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Maximum Authorized Altitude
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25,000 ft.(7,620 m) |
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Range |
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Range
@ Performance Cruise (75%)
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670
NM @ 16.3 gph.(61.70 lph)
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Range
@ Economy Cruise (65%)
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780
NM @ 14.1 gph.(53.37 lph)
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Range
@ Long Range Cruise (55%)
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870
NM @ 12.0 gph.(45.42 lph)
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Landing Performance
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Ground Roll |
734
ft. (223.73 m) |
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Distance over 50 ft. Obstacle
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1,312
ft. (399.90 m) |
Performance is based on a newly
manufactured aircraft, which is well
maintained and flown under standard
ISA day, sea level conditions, at
3,305 lbs. (1,499.12 kg), cruise
speeds at mid-weight, based on the
latest data available at the time of
publication of this document. The
performance of any particular aircraft
will depend in part on actual
conditions, aircraft status, and pilot
technique. Cruise range figures
include allowances for start, taxi,
climb, cruise descent, and 45-minute
reserve at maximum endurance.
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