Agusta 109E
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Agusta 109E |
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| ENGINE | DIMENSIONS, EXTERNAL | FUEL CAPACITY | gallons (liters) | lbs (kg) | ||||||
| Manufacturer | Pratt & Whitney | of Canada | Lenght, fuselage, ft (m) | 37.52 | (11.44) | Standard tank | 160 (606) | 1080 (490) | ||
| Model | two | 206C | Lenght, T/R turning, ft (m) | 37.96 | (11.57) | |||||
| Weight lbs (kg) | NA | NA | Lenght, both turning, ft (m) | 42.78 | (13.04) | |||||
| Width, fuselage, ft (m) | 5.28 | (1.61) | RANGE | |||||||
| POWER RATINGS | Width, widest point, ft (m) | 9.45 | (2.88) | Max fuel, nm (km) | 521 | (965) | ||||
| Takeoff, shp (kW) each | 640 | (477) | Width, landing gear, ft (m) | 8.03 | (2.45) | Max payload, nm (km) | 1361 | (2522) | ||
| Max continuous | 567 | (423) | Height, top, rotor hub, ft (m) | 10.17 | (3.10) | Aux fuel, no res, nm (km) | 521 | (965) | ||
| OEI 2 1/2 min | 732 | (546) | Height, top, tail fin, ft (m) | 11.48 | (3.50) | Endurance, std fuel, no reserves | 5.04 | hrs | ||
| OEI 30 min | 670 | (500) | Height, top, T/R arc, ft (m) | 10.30 | (3.14) | |||||
| OEI cont | 670 | (500) | Gr clearance, fuselage, ft (m) | 1.38 | (0.42) | PERFORMANCE | ||||
| Gr clearance, T/R, guard, ft (m) | 3.18 | (0.97) | Service ceiling, ft (m) | 20.000 | (6096) | |||||
| TRANSMISSION RATINGS | HIGE, ft (m) | 16600 | (5060) | |||||||
| Takeoff, shp (kW) | 900 | (671) | DIMENSIONS, INTERNAL | CABIN | BAGGAGE | HIGE, ISA+20°C, ft (m) | NA | (NA) | ||
| Continuous | 900 | (671) | Lenght, max, ft (m) | 11.58 (3.53) | 7.55 (2.30) | HOGE, ft (m) | 11800 | (3597) | ||
| OEI cont | 640 | (477) | Width, max, ft (m) | 5.28 (1.61) | NA (NA) | HOGE, ISA+20°C, ft (m) | NA | (NA) | ||
| Height, max, ft (m) | 4.20 (1.28) | NA (NA) | ROC, oblique, fpm (m/min) | NA | (NA) | |||||
| ROTOR SYSTEM | MAIN | TAIL | Volume, ft (m) | 180.08 (5.10) | 33.55 (0.95) | ROC, vertical, fpm (m/min) | 1930 | (588) | ||
| Number of blades | 4 | 2 | Econ cruise, S/L, kts (km/hr) | 154 | (285) | |||||
| Construction | composite | metal | ACCOMMODATION | Vne, kts (km/hr) | 168 | (311) | ||||
| Normal RPM | 384 | 2085 | Standard seating | 1 + 7 | ||||||
| Diameter, ft (m) | 36.09 (11.00) | 6.56 (2.00) | High density | 1 + 7 | ||||||
| Chord, ft (m) | 1.15 (0.35) | 0.69 (0.21) | ||||||||
| Disc area, ft² (m²) | 1022.60 (95.00) | 33.80 (3.14) | WEIGHTS | |||||||
| Disc loading, lbs/ft² (kg/m²) | 6.14 (29.99) | NA | Max gross, lbs (kg) | 6283 | (NA) | MILESTONES | ||||
| Power loading, lbs/shp (kg/kW) | 4.91 (2.99) | NA | Empty, std acft, lbs (kg) | 2910 | (1570) | Initial development | NA | |||
| Blabe folding | no | NA | Useful load, lbs (kg) | 2645 | (1200) | First flight (prototype) | NA | |||
| Useful, with full fuel, lbs (kg) | 2645 | (1200) | FAA certification, VFR | NA | ||||||
| External load, lbs (kg) | NA | (3000) | FAA certification, IFR | NA | ||||||
| Gross with ext load, lbs (kg) | 5730 | (2599) | ||||||||