Aeronaves

Model: EMBRAER PHENOM 100
Engine Takeoff Power: P&W 1615 lb thr • PW617F
Engine TBO Hours: 3500

Embraer Phenom 100 Speed:

• Maximum Operating Speed: 463 Knots (kts), 532 mph or Mach 0.70
• High Speed Cruse: 390 Knots (kts) or 722 km/h

Airspeed Limitations:

• V_MO (max operating speed): 275 Knots Indicated Airspeed (KIAS) from sea level to 28,000 feet.
• M_MO (Max Mach Speed): 0.7 Mach above 28,000 feet

V_FE (Maximum Flaps Extended Speed):

• 10 degrees (takeoff): 200 KIAS
• 26 degrees (takoff and landing): 160 KIAS
• 36 degress (landing): 145 KIAS

V_MC (minimum control speed):

• 10 degrees (takeoff): 97 KIAS
• 26 degrees (takeoff): 92 KIAS
• 26 degrees (landing): 86 KIAS
• 36 degrees (landing: 86 KIAS
• Speeds above can change due to temperature and altitude. Do not use for flight, refer to official aircraft operating manual.

V_LO (landing gear operating)

• Gear Retract and Extend: 180 KIAS
• VLE (landing gear extended): 275 KIAS
• Maximum tire ground speed: 139 Knots

Embraer Phenom 100 Landing and Takeoff Distances:

• Phenom 100 Takeoff Distance: 3,125 feet (ft) or 952 meters (m) (MTOW, SL, ISA)
• Landing Distance: 2,699 feet (ft) or 823 meters (m) (MLW, SL, ISA)
• Service Ceiling – Maximum Operating Altitude: 41,000 feet (ft) or 12,497 meters (m)
• Maximum Takeoff and Landing Altitude: 10,000 ft

Engines:

• Embraer Phenom 100 Engines: Pratt & Whitney PW617F-E (2 Total)
• Engine Thrust and Flat Rating: 1,695 lb ISA + 10 degrees Celsius
• Both Phenom 100 Engines are FADEC controlled
• External Noise: 33 EPNdB below stage 4

Engine Limitations:
During standard day, sea level and static thrust

• Takeoff (5 Minutes): Standard Version: 1,695 pounds of thrust. Enhanced Version (Possibly Phenom 100E): 1,695 pounds of thrust.
• Automatic Thrust Reserve (ATR, 10 minutes): Standard Version: 1,720 pounds of thrust. Enhanced Version (Phenom 100E): 1,820 pounds of thrust.

Maximum engine rotor operating speeds, permissible (Takeoff and Maximum Continuous)

• N₁ (fan): 100% = 19,845 revolutions per minute (RPM)
• N₂ (Gas Gen): 100.4% = 40,200 RPM
• N₁ Transient (20 seconds): 101% = 20,043 RPM
• N₂ Transient (20 seconds): 102% = 40,840 RPM

Maximum interturbine gas temperatures (IGT), permissible

• Takeoff: 830° Celsius
• ATR: 845° Celsius
• Maximum Continuous: 830° Celsius
• Transient (starting 5 seconds): 892° Celsius or 950° Celsius with Post SB 500-73-0001 incorporated (SB = Service Bulletin)
• Transient (20 seconds): 862° Celsius

Seating Configuration and Seating Capacity:

• 1 crew and 7 passengers (9 total persons)

Avionics: Prodigy Flight Deck 100 based on the Garmin G1000 avionics suite

Embraer Phenom 100 Dimensions:

External Dimensions:

• Height 14 ft 3 in
• Wing Span 40 ft 4 in (Wing Area: 160 ft2 (squared))
• Length 42 ft 1 in

Cabin / Interior Dimensions:

• Max. Height 4 ft 11 in
• Max. Width 5 ft 1 in
• Length 11 ft
• Floorline Width 3 ft 7 in

Cabin Door Dimensions:

• Height 4 ft 10 in (1.48m) Width 2 ft (0.62m)

Phenom 100 Cabin Volume: 282 cu ft