|
Make Embraer |
Model Phenom 300 |
Year 2013 |
Serial TBA |
Airframe New |
Engines New |
Sales Comments
Embraer Phenom 300 Position
To be delivered August 2013
Features
All performance data are for an aircraft in the baseline configuration, with no optional equipment.
Take-off field length and landing distance are for sea level, hard surface, and dry runways with zero
wind. Actual performance values may vary with individual airplanes and other factors, such as environmental conditions and aircraft configuration.
Take-off Field Length 3,138 ft (956 m) @ Sea Level, ISA, MTOW, Balanced Field Length.
Landing Distance 2,621 ft (799 m) @ Sea Level, ISA, MLW, as per FAR 91.
Range (*) 1,971 Nautical Miles, 6 occupants @ 200 lb (91 kg), MTOW, Long Range Cruise, ISA,
Reserves: 100 nm alternate + 35 minutes (NBAA IFR reserves).
Note: (*) Range considered is based on an aircraft configured with the baseline airframe, equipment, interior
layout, finishing materials, no options installed and no catering items.
Maximum Speed Cruise 453 KTAS@ ISA, Mid-cruise weight, 500 nm typical mission, 6 occupants @ 200 lb (91
kg), Reserves:100 nm alternate + 35 minutes (NBAA IFR reserves).
Selected options include: (could still be changed as explained in Optional Equipment):
- HF and SELCAL (101,700)
- Flight Data Recorder ($52,000)
- Lavatory Sink ($33,500).- Hot Jug ($8,300)
- In Flight Phone ($46,700)
- In Flight Entertainment Package- Best Value Package ($63,000)
- In Flight Entertainment Package-Premium Package ($94,800)
- Additional Individual Monitors ($12,000)
- Heating System for Baggage Compartment ($34,100)
Avionics
The EMBRAER Phenom 300 Executive Jet avionics system is the ProdigyTM system which is based on the Garmin Avionics Platform. It makes extensive use of the latesttechnologies in a highly integrated and automated architecture. Designed with the "quietand dark" cockpit concept, it provides maximum safety, requiring adequate pilot workload while providing comfort during all flight phases. The main instrument panel incorporates three 12.4 inches Active Matrix Liquid Crystal Displays (AMLCD), one Integrated Electronic Standby Instrument (IESI), two audio panels, one guidance panel and an additional panel for FMS control. The ProdigyTM provides the following functions as baseline: • Display of attitude, heading, and slip/skid • Display of air data information • Display of engine parameters and systems status information (including synoptic) • Weather Radar • Crew Alerting System (CAS) • Aural Warning (including Stall Warning Function) • Airborne Audio System • VHF Communication (COM) • Transponder functions including Traffic Information System (TIS) • VOR/ILS Navigation (NAV) • Satellite based positioning navigation (GPS-WAAS1) • Flight Management System (FMS) including Required Navigation Performance (RNP) • Vertical Navigation (VNAV) • Satellite Weather and Radio Receiver2 • Display of terrain information, including Terrain Awareness and Warning System, class B (TAWS-B) • Moving map for situational awareness • Dual Flight Director (FD) • 3 Axis CAT I Automatic Flight Control System (AFCS) • Yaw Damper through Rudder and Ventral Rudder • Central Maintenance Computer (CMC), including Health Monitoring Capability for Engines • Emergency Locator Transmitter (ELT) • Cockpit Voice & Data Recorder (CVDR) • B/PRNAV 1 WAAS capability is available in GPS WAAS coverage area. 2 Satellite Weather and Radio Receiver are available in XMTM service coverage area.
Interior
The baseline interior arrangement provides accommodations in the cockpit for two pilots, and up to six passengers in the main cabin area.
Main cabin in the baseline layout has a forward right hand side refreshment center, a forward left hand side storage space, recessed center aisle, and will provide accommodations for six passengers being two single club seats in the middle and two forward facing seats in the aft part of the cabin. The cabin is approximately 5 ft 1 in (1.55m) wide and approximately 4 ft 11 in (1.50 m) tall. Or if the selected configuration shown above is maintained, then a seven sft facing, forward seat on the right side will be added with a smaller refreshment center. Three 115 VAC / 60 Hz / 100 W AC Outlets are available for use of personal electronic devices.
These outlets are disposed one in the cockpit and two in the main cabin. Baseline in flight
entertainment system offers a CD Player, input for portable media players and XM radio. Main cabin is equipped with speakers and a subwoofer.
A chemical re-circulating externally serviced toilet is located in the aft part of the main cabin. A rigid dual sliding door installed in the partition separates the lavatory from the main cabin, increasing privacy.
Baggage compartments provides 66 ft3 (1.86 m3) of storage space in the aft fuselage area, with load capacity of 463 lb (210 kg); 8 ft3 (0.23 m3) in the forward fuselage area, with load capacity of 110 lb (50 kg); both non-pressurized.
Exterior
Colours Open as of this time.
Maintenance
- 18 months prior delivery to select optional equipment, - 12 months for interior configuration, - 09 months for paint scheme - 03 months for tail number.
Asking Price
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