Agusta 109C
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Agusta 109C |
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| ENGINE | DIMENSIONS, EXTERNAL | FUEL CAPACITY | gallons (liters) | lbs (kg) | ||||||
| Manufacturer | Rolls Royce | Allison | Lenght, fuselage, ft (m) | 37.52 | (11.44) | Standard tank | 145 (550) | 970 (440) | ||
| Model | two | 250-C20R/1 | Lenght, T/R turning, ft (m) | 37.96 | (11.57) | Aux or ferry tank | 40 (150) | 265 (120) | ||
| Weight lbs (kg) | 158 | (72) | Lenght, both turning, ft (m) | 42.76 | (13.03) | |||||
| Width, fuselage, ft (m) | 4.72 | (1.44) | RANGE | |||||||
| POWER RATINGS | Width, widest point, ft (m) | 9.45 | (2.88) | Max fuel, nm (km) | 300 | (556) | ||||
| Takeoff, shp (kW) each | 450 | (336) | Width, landing gear, ft (m) | 7.55 | (2.30) | Max payload, nm (km) | 300 | (556) | ||
| Max continuous | 380 | (284) | Height, top, rotor hub, ft (m) | 10.17 | (3.10) | Aux fuel, no res, nm (km) | 380 | (704) | ||
| OEI 2 1/2 min | 450 | (336) | Height, top, tail fin, ft (m) | 11.48 | (3.50) | Endurance, std fuel, no reserves | 3.14 | hrs | ||
| OEI 30 min | 450 | (336) | Height, top, T/R arc, ft (m) | 10.30 | (3.14) | |||||
| OEI cont | 450 | (336) | Gr clearance, fuselage, ft (m) | 1.12 | (0.34) | PERFORMANCE | ||||
| Gr clearance, T/R, guard, ft (m) | 2.53 | (0.77) | Service ceiling, ft (m) | 15.000 | (4572) | |||||
| TRANSMISSION RATINGS | S/C, OEI, ISA, ft (m) | 7000 | (2133) | |||||||
| Takeoff, shp (kW) | 790 | (589) | DIMENSIONS, INTERNAL | CABIN | BAGGAGE | S/C, OEI, ISA+20°C, ft (m) | NA | (NA) | ||
| Continuous | 790 | (589) | Lenght, max, ft (m) | 5.35 (1.63) | 3.28 (1.00) | HIGE, ft (m) | 11400 | (3474) | ||
| OEI cont | 450 | (336) | Width, max, ft (m) | 4.72 (1.44) | 3.94 (1.20) | HIGE, ISA+20°C, ft (m) | 4000 | (1220) | ||
| Height, max, ft (m) | 4.23 (1.29) | 1.67 (0.51) | HOGE, ft (m) | 8000 | (2438) | |||||
| ROTOR SYSTEM | MAIN | TAIL | Volume, ft (m) | 113.74 (3.22) | 18.36 (0.52) | HOGE, ISA+20°C, ft (m) | 1800 | (550) | ||
| Number of blades | 4 | 2 | ROC, oblique, fpm (m/min) | 1710 | (521) | |||||
| Construction | composite | metal | ACCOMMODATION | ROC, vertical, fpm (m/min) | 940 | (286) | ||||
| Normal RPM | 384 | 2085 | Standard seating |
2 + |
3 + 3 |
ROC, OEI, fpm (m/min) | 350 | (107) | ||
| Diameter, ft (m) | 36.09 (11.00) | 6.65 (2.00) | High density |
2 + |
3 + 3 |
Econ cruise, S/L, kts (km/hr) | 147 | (273) | ||
| Chord, ft (m) | 1.15 (0.35) | 0.69 (0.21) | Vne, kts (km/hr) | 168 | (311) | |||||
| Disc area, ft² (m²) | 1022.61 (95.00) | 33.80 (3.14) | WEIGHTS | |||||||
| Disc loading, lbs/ft² (kg/m²) | 5.86 (28.63) | NA | Max gross, lbs (kg) | 5996 | (2720) | MILESTONES | ||||
| Power loading, lbs/shp (kg/kW) | 6.66 (4.05) | NA | Empty, std acft, lbs (kg) | 3461 | (1570) | Initial development | 1987 | |||
| Blabe folding | no | NA | Useful load, lbs (kg) | 2941 | (1130) | First flight (prototype) | 1988 | |||
| Useful, with full fuel, lbs (kg) | 1521 | (690) | FAA certification, VFR | Jan | 1989 | |||||
| External load, lbs (kg) | 2000 | (907) | FAA certification, IFR | Jan | 1989 | |||||
| Gross with ext load, lbs (kg) | 5997 | (2720) | ||||||||