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 liters/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) |
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.