Eclipse 500 - Table 1.Performance Data

Section 1. Aircraft Overview Eclipse 5OO Systems Manual
Copyright © — Eclipse Aviation Corporation
6 Version 2.0 April 2007
1.4 Performance and Capabilities
1.4.1 Performance
Below is a table of key performance data of interest to the pilot.
Table 1. Performance Data
Performance Design Speeds
Max Cruise Speed (at 4,950 lbs,
ISA conditions, 35,000 ft)
370 KTAS V
s
(Stall speed clean configuration) 90
NBAA IFR Range, 4 Occupants
(at high speed, 200 lb Pilot +
3 170 lb Passengers)
1,155 nm
V
SO
(Stall Speed landing configuration) 70
Time to Climb, 35,000 ft 19 min. V
o
(Operating maneuvering speed) 180
Max Climb rate (Both Engines,
Takeoff Power)
3,314 fpm V
MO
(Max Operating Limit Speed) 275
Single engine climb rate 888 fpm M
MO
(Max Operating Mach Number) 0.64 M
V
FE
(Flaps TO) 200
V
FE
(Flaps LDG) 120
V
LE
275
V
LO
200
Limit Load Factors Operational Limitations
Flaps UP +3.62/-1.45 g’s Max operating altitude 41,000 ft
Max Cabin Pressure Differential 8.7 PSI
Single engine service ceiling 25,000 ft