Specifications
Technical Specifications
| WEIGHT & BALANCE BASIC EMPTY WEIGHT (Standard IFR) |
2,950 LB* | 1,338 KG* |
| *The basic empty weight is defined as the complete aircraft, empty of usable fuel and without optional equipment, but including engine oil, unusable fuel and items of equipment that are an integral part of the basic aircraft. | ||
| MAXIMUM OPERATING WEIGHTS | ||
| Max. Ramp Weight | ||
| Max. Take-Off Weight (Standard) | 6,450 LB | 2,925 KG |
| Max. Take-Off Weight (Agricultural) | 8,250 LB | 3,742 KG |
| Max. Landing Weight | 6,450 LB | 2,925 KG |
| Max. Useful Load (Standard Category – 1 crew, 2.5 hrs fuel) | 2,450 LB | 1,111 KG |
| Max. Useful Load (Agricultural Category – 1 crew, 1 hrs fuel) | 4,750 LB | 2,154 KG |
| Max. Structural Hopper Load | 4,100 LB | 1,859 KG |
| SPEEDS | ||
| Never Exceed Speed (VNE) | 176 Knots | 325 KPH |
| Design Cruising Speed (VC) | 140 Knots | 259 KPH |
| Max. Manoeuvring Speed (VA) | 126 Knots | 233 KPH |
| Max. Flap Retracted Speed | 85 – 90 Knots | 157 - 166 KPH |
| Stall Speed (Idle Power) At Max. Weight | 57 Knots | 105 KPH |
| RANGE | ||
| Range - Normal | 420 Miles | 675 KM |
| Endurance – Normal Configuration | 2.7 HRS | |
| Average Fuel Consumption Per Hour | 48 US/GAL | 180 LTS |
| PERFORMANCE | ||
| TAKE-OFF & LANDING PERFORMANCE | ||
| Normal Conditions, 6,450 LB | ||
| Take-Off Distance To 15 M (50 FT) ISA | 1,065 FT | 325 M |
| Landing Distance From 15 M (50 FT) | 1,398 FT | 426 M |
| CLIMB (AT MTOW) | ||
| Max. Rate Of Climb At Sea Level | 1,560 FT/MIN | |
| Max. Rate Of Climb at 8,000 FT | 1,060 FT/MIN | |
| Max. Rate Of Climb at 14,000 FT | 680 FT/MIN | |
| ALTITUDE LIMITS | ||
| Max. Operating Altitude | 25,000 FT | |
| Service Ceiling (At Max. Weight) | 25,000FT | |
| NORMAL LOAD FACTORS | ||
| Max. Positive G | +3.56 | |
| Max. Negative G | -1.42 | |
| Wing Loading | 104 KG/M2 | 21.9 LB/FT2 |
| Power Loading | 0.25 SHP/KG | 0.11 SHP/LB |
| MAINTENANCE | ||
| Aircraft Inspection Cycle | 100 hours inspections | |
| Lifed Airframe Components | Wing spar 16,000 hours | |
| Wing strap 8,000 hours | ||
| AIRCRAFT TECHNICAL DESCRIPTION | ||
| Ailerons | Plain 25o up travel, 10o down travel | |
| Vertical Tail Surface | Fixed fin, horn balance rudder | |
| Rudder Deflection | ± 30 0 | |
| Horizontal Tail Surface | Fixed plane with elevator | |
| Elevator Deflection | 30 up 8.5 down | |
| Landing Gear Type | 12.2 FT | 3.71 M |
| Wheel and Tyre Size | 8.50 x 6 nose 8.50 x 10 main | |
| Engine | Pratt & Whitney PT6-34 Ag | |
| Propeller | Hartzell 3 Bladed fully feathering and reversible | |
| DIMENSION | ||
| Fuselage Overall Length | 36.2 FT | 10.9 M |
| Fuselage Maximum Width | 48” | 1.22 M |
| Fuselage Maximum Height | 60” | 1.52 M |
| Wing Span | 42 FT | 12.8 M |
| Wing Aspect Ratio | 6.0 | |
| CABIN DIMENSIONS & CAPACITY | ||
| Cargo Payload | 3,136 LBS | 1,435 KG |
| Large Door Size | 39” x 37” | 0.99 M x 0.94 M |
| Maximum Cabin Height | 4.21 FT | 1.28 M |
| Maximum Width | 3.5 FT | 1.06 M |
| Floor Length | 10.25 FT | 3.12 M |
| Total Compartment Length | 11.83 FT | 3.61 M |
| Total Compartment Volume | 133 FT3 | 3.79 M3 |