2009 EMBRAER PHENOM 100
Aircraft Summary
General
Year
2009
Manufacturer
EMBRAER
Model
PHENOM 100
Serial Number
TBD-2009
Condition
New
Description
New Position - Scheduled for Delivery August 2009
Airframe
Airframe Notes
AIRFRAME 0 Hours
POWERPLANT Pratt & Whitney – PW 617F
0 Hours SINCE New
0 Hours SINCE New
ADDITIONAL • Takeoff thrust – 1,615 lb
• FADEC controlled
Avionics
Avionics/Radios
The EMBRAER Phenom 100 Executive Jet avionics will be Prodigy system wich is based on Garmin Avionics Platform. It will make extensive use of the latest technologies in a higly integrated and automated architeture. Designed with the "quiet and dark" cockipt concept, it will provide maximum safety, requiring adequate pilot workload while providing comfort during all flight phases.
The main instrument panel will incorporate 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 (Flight Management System) control.
The Prodigy will provide the following functions as baseline:
Options Chosen:
DME
Transponder #2
Weather Radar
Cockpit Flood Lights
Sunshade and Sun Visor
Life Vest
Crew Portable Breathing Equipment
Smoke Goggles
Premium Pax Door
Additional Equipment
Additional Equipment
• Display of attitude, heading, and slip/skid
• Display of air data information
• Display of engine parameters and system status / information (including synoptic)
• 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
• Flight Director (FD)
• 3 Axis CAT I Automatic Flight Control System (AFCS)
• Pitch and Mach Trim Computations
• Center Maintenance Computer (CMC), including Health Monitoring Capability for Engines
• Emergency Locator Transmiter (ELT)
(1) WAAS capability is available in GPS WAAS coverage area.
(2) Satellite Weather and Radio Receiver are available in XM service coverage area.
Exterior
Exterior Notes
EXTERIOR To Be Determined
Interior
Interior Notes
INTERIOR To be Determined
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