Section 9. Climate Control Eclipse 5OO Systems Manual
Copyright © — Eclipse Aviation Corporation
186 Version 2.0 April 2007
9.3 Limitations and Specifications
9.3.1 Cabin Pressurization Limitations
Maximum Regulated Cabin Pressure Differential (∆P) ....................................8.33 PSI
Maximum Regulated Negative Cabin Pressure Differential (ΔP) ......................-0.5 PSI
Positive Pressure Relief, Primary Outflow Valve ................................................8.6 PSI
Positive Pressure Relief, Secondary Outflow Valve............................................8.7 PSI
Maximum Bleed Air Muffler Duct Temperature. ....................................... 185°F (85° C)
Maximum Evaporator Temperature.......................................................... 176°F (80° C)
Maximum Pylon Temperature .................................................................. 350°F(177°C)
Landing with cabin pressurized is not approved
When operating in the Manual mode, negative entries of Selected Cabin Altitude
are not approved.
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