|
Commander 115AT performance and specifications
Specifications
Engine |
Manufacturer |
Textron Lycoming |
Model
|
IO-540-T4B5 |
Number of Cylinders |
6
|
Displacement |
541.5
cu. in. (8.87 l) |
Maximum Power |
260
HP @ 2,700 RPM |
Recommended TBO |
2,000
hours |
|
Propeller |
Manufacturer |
McCauley |
Model
|
B3D32C419/82 NHA-5 |
Type
|
Constant-Speed, Hydraulic
|
Number of Blades |
3
|
Diameter |
77"
(1.96 m) |
|
Weights |
Maximum Ramp |
3,260
lbs. (1,478.71 kg) |
Maximum Take-off |
3,250
lbs. (1,474.17 kg) |
Standard Empty |
2,102
lbs. (953.45 kg) |
Max
Baggage Compartment |
200
lbs. (90.72 kg) |
Standard Useful Load |
1,158
lbs. (525.26 kg) |
|
Fuel & Oil Capacity
|
Fuel
|
90 US
gal./88 usable
(340.65 litres/333.08 usable)
|
Oil
|
8
quarts (7.57 l) |
|
Wing Area/Loadings
|
Wing
Area |
152
sq. ft. (14.12 sq. m) |
Wing
Loading |
21.4
lbs./sq. ft.(104.48 kg/sq. m)
|
Power
Loading |
12.5
lbs./hp. (5.67 kg/hp) |
|
Performance
Speeds |
Maximum 164 kts. |
(304
kph) |
Performance Cruise (75% Power)
|
160
kts. (297 kph) |
Economy Cruise (65% Power)
|
155
kts. (287 kph) |
Long
Range Cruise (55% Power)
|
149
kts. (276 kph) |
Stall
(Cruise Configuration)
|
60
kts. (111 kph) |
Stall
(Landing Configuration)
|
54
kts. (100 kph) |
|
Takeoff Performance
|
Ground Roll |
1,145
ft. (348.99 m) |
Distance over 50 ft. Obstacle
|
1,985
ft. (605.02 m) |
|
Climb Performance |
Initial S.L. Rate of Climb
|
1,070
ft./min.(326.14 m/min.)
|
Service Ceiling |
16,800 ft.(5,120.64 m)
|
|
Range |
Range
@ Performance Cruise |
855
NM @ 14.3 gph.(54.13 lph)
|
Range
@ Economy Cruise |
940
NM @ 12.6 gph.(47.69 lph)
|
Range
@ Long Range Cruise |
1005
NM @ 11.2 gph.(42.39 lph)
|
|
Landing Performance
|
Ground Roll |
720
ft. (219.46 m) |
Distance over 50 ft. Obstacle
|
1,200
ft. (365.77 m) |
Performance is based on a newly
manufactured aircraft, which is well
maintained and flown under standard
ISA day, sea level conditions, at
3,250 lbs. (1,474.17 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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