Aviators Toll Free # 180042577777
Tel No. : +91 80 22219838 / 9839
Email : aviators@vsnl.com
Email : aviators@vsnl.com
Phenom 100
Performance
Payloads vs Range
Characteristics
| Design Goals | Final Results | |||
| Range with IFR (1) reserves | 1,160 nm | 1,178 nm | √ | 18 miles more |
| MMO | 0.70 | 0.70 | √ | on the mark |
| Maximum Ceiling | 41,000 ft | 41,000 ft | √ | with direct climb at MTOW |
| High Speed Cruise | 380 kt | 390 kt | √ | 10 ktas faster |
| Landing Distance (2) | 3,000 ft | 2,699 ft | √ | 301 ft shorter |
| Standard Take-off Field Length (3) | 3,400 ft | 3,400 ft | √ | on the mark |
| Enhanced Take-off Field Length (3) | n/a | 3,125 ft | √ | 275 ft shorter |
| Engine Thrust | 1,615 lb | 1,695 lb | √ | 5% more thrust |
| Block Fuel for 1,000 nm | 1,960 lb | 1,892 lb | √ | up to 3.6% fuel savings |
| External noise | Stage IV | Stage IV | √ | with 33 EPNdB margin |
| Main baggage compartment | 45 ft 3 | 53 ft 3 | √ | 22% more space |
- NBAA IFR reserves (35 min) with 100 nm alternate; 4 occupants @ 200 lb each
- MLW, SL, ISA
- MTOW, SL, ISA
Structural and Operational Weight
| Imperial (lb) | Metric (kg) | |
| Maximum Ramp | 10,516 | 4,770 |
| Maximum Takeoff | 10,472 | 4,750 |
| Maximum Landing | 9,766 | 4,430 |
| Maximum Zero Fuel | 8,444 | 3,830 |
| Basic Operating (1) (2) | 7,132 | 3,235 |
| Useful Load | 3,384 | 1,535 |
| Maximum Payload (2) | 1,312 | 595 |
| Maximum Usable Fuel (3) | 2,804 | 1,272 |
- BOW considering 1 crew (91kg)
- Standard configuration (weights may vary according to optional equipment installed or interior layouts).
- Adopted fuel density 6.70 lb/US gal (0.803 kg/l).