Eclipse 500 User Manual

Section 6. Ice Protection Eclipse 5OO Systems Manual
Copyright © — Eclipse Aviation Corporation
110 Version 2.0 April 2007
6.7.7 Pressure Regulating Shut-Off Valve Fault
A failure of a pressure regulating shut off valve causes a L (R) ENG A/ICE VLV
FAULT to appear. This valve fails open allowing pneumatic de-ice to remain
available.
6.7.8 De-ice Pressure Sensor Fault
Should a wing de-ice pressure sensor malfunction be detected on the ground, a
WING DEICE MON FAULT advisory message appears and flight into icing conditions
is prohibited. Should this fault occur in flight, wing de-ice is unavailable and a WING
DEICE FAIL caution appears.
6.7.9 Engine Anti-Ice Sensor Fault
Should an engine anti-ice sensor malfunction be detected on the ground, an ENG
ANTI-ICE MON FAULT advisory message appears and flight into icing conditions is
prohibited. Should this fault occur in flight, engine anti-ice is unavailable and a WING
DEICE FAIL caution appears.
6.7.10 Static Heater Monitor Fault
Should the ACS be unable to monitor the function of the static heaters, a STATIC
HTR MON FLT advisory message appears. The heaters will still operate.

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