AIRCRAFT SYSTEMS ICE AND RAIN PROTECTION
SA227‐ SERIES/FCOM/VTM
6.30.00.1
ICE AND RAIN PROTECTION
INDEX ICE AND RAIN PROTECTION……………………………………………………………………………………………………….…… 6.30.1 SURFACE DEICE SYSTEM (WING AND TAIL BOOTS) ……………………..…………………………………………………. 6.30.1 DEICE BOOT OPERATION…………………………………………………………………………………..……………………………. 6.30.1 WINDSHIELD HEAT…………………………………….…………………………………………………………………………………... 6.30.3 WINDSHIELD WIPER SYSTEM………………………………………….…………………………………………………….……….. 6.30.3 PITOT AND SAS ANTI‐ICE…………………………………………………………………….……………………………………..…... 6.30.4 PITOT HEAT WARNING SYSTEM (‐AT‐ SERIES ONLY) (XA‐USG) ……………………………………………………... 6.30.4 ENGINE INLET ANTI‐ICE…………………………………………………………………………………………………………..….….. 6.30.5 PROPELLER DEICE SYSTEM……………………………………………………………………………..………………………….….. 6.30.6 FUEL ANTI‐ICING………………………………………………………………………………………………….………………………... 6.30.6
FIGURES FIGURE 6.30‐1 DEICE BOOTS…………………………………….………………………………………….………………………... 6.30.2 FIGURE 6.30‐2 EROSION GUARDS…………………………………….…………………………………………….……………... 6.30.2 FIGURE 6.30‐3 PITOT AND PROP AMP METER AND ENGINE DUCT HEAT CYCLE LIGHTS…………..…….. 6.30.3 FIGURE 6.30‐4 ENGINE INLET ANTI‐ICE…………………………………………………………………………………………… 6.30.4
Revision: Original Aug 1,2013
GO/FCOM/SA227‐SERIES/VTM
AIRCRAFT SYSTEMS ICE AND RAIN PROTECTION
Revision: Original Aug 1,2013
SA227‐ SERIES/FCOM/VTM INTENTIONALLY LEFT BLANK
GO/FCOM/SA227‐SERIES/VTM
6.30.00.2