Eclipse 500 User Manual

Section 5. Oxygen Eclipse 5OO Systems Manual
Copyright © — Eclipse Aviation Corporation
Version 2.0 April 2007 87
Table 6. Oxygen Duration 40 cu ft Cylinder – Part 91
# Pass # Pilots
Total Useable
Cylinder Capacity
(LITERS)
Oxygen Used
in Preflight
(LITERS)
Emergency Oxygen
Consumed in 10 min
Descent (Pilot+Pass)
(LITERS)
Pilot Cruise
Consumption
Above 35K ft.
(Mask in "NORM")
(LITERS)
Maximum Oxygen
Consumption Time
Above 35K ft for Pilot
(Mask in "NORM")
(MINUTES)
0 1 1005 2.32 32.84 969.84 444.88
1 1 1005 2.32 78.84 923.84 423.78
2 1 1005 2.32 124.84 877.84 402.68
3 1 1005 2.32 170.84 831.84 381.58
4 1 1005 2.32 216.84 785.84 360.48
5 1 1005 2.32 262.84 739.84 339.38
Table 7. Oxygen Duration 40 cu ft Cylinder – Part 135
# Pass
#
Pilots
Total Useable
Cylinder
Capacity
(LITERS)
Oxygen
Used in
Preflight
(LITERS)
Crew Emergency
Descent
Requirement 10 min
(LITERS)
30-Minute Rule
for Passenger
Oxygen Reserve
Above 15K ft
(LITERS)
Single Pilot Cruise
Consumption
Above 25K ft.
(Mask in "NORM")
(LITERS)
Maximum Oxygen
Consumption
Time Above 25K ft
for Pilot
(Mask in "NORM")
(MINUTES)
0 1 1005 2.32 32.84 0.00 969.84 444.88
1 1 1005 2.32 32.84 139.88 829.965 380.72
2 1 1005 2.32 32.84 279.75 690.09 316.56
3 1 1005 2.32 32.84 419.63 550.215 252.39
4 1 1005 2.32 32.84 559.50 410.34 188.23
5 1 1005 2.32 32.84 699.38 270.465 124.07
0 2 1005 4.64 65.68 0.00 934.68 428.75
1 2 1005 4.64 65.68 139.88 794.805 364.59
2 2 1005 4.64 65.68 279.75 654.93 300.43
3 2 1005 4.64 65.68 419.63 515.055 236.26
4 2 1005 4.64 65.68 559.50 375.18 172.10
0 2 1005 4.64 65.68 0.00 934.68 428.75
NOTE:
Refer to the onboard oxygen duration chart for oxygen requirements for a
particular flight
5.6.3 Oxygen System Post-Flight
When the engines are shut down, push in the oxygen control knob to shut off the
oxygen system and prevent inadvertent oxygen depletion.

Eclipse 500 Specifications

General

Manufacturer	Eclipse Aerospace
Model	Eclipse 500
Type	Very Light Jet
Engines	2 × Pratt & Whitney Canada PW610F turbofans
Thrust per engine	900 lbf (4.0 kN)
Wingspan	37.9 ft (11.6 m)
Height	11.0 ft (3.4 m)
Avionics	Avio NG
First Flight	August 26, 2002
Maximum Speed	430 mph
Range	1, 125 nautical miles
Service Ceiling	41, 000 ft (12, 500 m)
Crew	1 or 2
Max Takeoff Weight	6, 000 pounds
Seating Capacity	4-6
Length	33 feet 6 inches
Empty Weight	3, 550 pounds
Payload	Varies with configuration and fuel load