 
|
Specifications
In
the relentless pursuit of safety and quality, CPAC reserves the right to change
specifications, performance estimates, material, and/or prices, and may
discontinue models and introduce new models, at any time and without prior
notice.
|
Engine
|
|
Manufacturer
|
Textron Lycoming
| |
Model
|
TIO-540-AG1A
| |
Number of Cylinders
|
6
| |
Displacement
|
541.5 cu. in. (8.87 l)
| |
Maximum Power
|
270 HP @ 2,575 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
|
3,305 lbs. (1,499.12 kg)
| |
Maximum Take-off
|
3,305 lbs. (1,499.12 kg)
| |
Standard Empty
|
2,152 lbs. (976.13 kg)
| |
Max Baggage Compartment
|
200 lbs. (90.72 kg)
| |
Standard Useful Load
|
1,152 lbs. (522.54 kg)
|
| |
|
Fuel & Oil Capacity
|
|
Fuel
|
90 US gal./88 usable
(340.65 liters/333.08 usable)
| |
Oil
|
10 quarts (9.46 l)
|
| |
|
Wing Area/Loadings
|
|
Wing Area
|
152 sq. ft. (14.12 sq. m)
| |
Wing Loading
|
21.8 lbs./sq. ft.(105.94 kg/sq. m)
| |
Power Loading
|
12.2 lbs./hp.(5.53 kg/hp)
|
| |
Performance
|
Speeds
|
|
Maximum
|
197 kts.(365 kph)
| |
Performance Cruise (75%) @ 25,000 ft.
|
187 kts.(347 kph)
| |
Performance Cruise (75%) @ 17,500 ft.
|
177 kts.(328 kph)
| |
Performance Cruise (75%) @ 12,500 ft.
|
170 kts.(315 kph)
| |
Stall (Cruise Configuration)
|
66 kts.(122 kph)
| |
Stall (Landing Configuration)
|
59 kts.(109 kph)
|
| |
|
Takeoff Performance
|
|
Ground Roll
|
1,408 ft. (429.15 m)
| |
Distance over 50 ft. Obstacle
|
2,223 ft. (677.56 m)
|
| |
|
Climb Performance
|
|
Initial S.L. Rate of Climb
|
1,050 ft./min.(320.04 m/min.)
| |
Maximum Authorized Altitude
|
25,000 ft.(7,620 m)
|
| |
|
Range
|
|
Range @ Performance Cruise (75%)
|
670 NM @ 16.3 gph.(61.70 lph)
| |
Range @ Economy Cruise (65%)
|
780 NM @ 14.1 gph.(53.37 lph)
| |
Range @ Long Range Cruise (55%)
|
870 NM @ 12.0 gph.(45.42 lph)
|
| |
|
Landing Performance
|
|
Ground Roll
|
734 ft. (223.73 m)
| |
Distance over 50 ft. Obstacle
|
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. |
