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Embraer Prodigy
®
Flight Deck 100 Pilot’s Guide
190-00728-04 Rev. A112
ENGINE & AIRFRAME SYSTEMS
ICE PROTECTION SYSTEM
When the ice protection system is operating normally, all components are shown in green on the system
diagram. Items in white indicate components which are off. A red “X” over a component indicates invalid data
or a failed unit.
1
Windshield Heaters
2
Boot Lines and Valves
3
Inboard Ejector Flow Control Valve (EFCV)
4
Outboard Ejector Flow Control Valve (EFCV)
5
Engine Anti Ice 1 Bleed Duct and Lip Skin
6
Engine Anti Ice 2 Bleed Duct and Lip Skin
7
EAI 1 Valve and Bleed Line
8
EAI 2 Valve and Bleed Line
9
Pressure Regulating Shut-Off Valve 1 (PRSOV 1)
10
Pressure Regulating Shut-Off Valve 2 (PRSOV 2)
11
STAB Ejector Flow Control Valve (EFCV)
12
Ice Protection Bleed Duct
Figure 3-19 Ice Protection Synoptics Page
1
2
4
6
5
2
3
9
10
8
7
2
11
12
1