AIRCRAFT SYSTEMS FLIGHT CONTROLS
SA227‐ SERIES/FCOM/VTM
6.27.00.1
FLIGHT CONTROLS
INDEX FLIGHT CONTROLS……………………………………………………………………………………….…..……………………………. 6.27.1 AILERONS……………………………………………………………..……………………………………………………..………………... 6.27.1 AILERON TRIM TABS………………………………………………………………………………………………………………………. 6.27.1 RUDDER…………………………………………………………………………………………………………………………….…………… 6.27.2 RUDDER TRIM TAB…………………………………………………….…………………………………………………………………… 6.27.3 ELEVATOR…………………………………………………………………………………………….………………………………………… 6.27.4 HORIZONTAL STABILIZER………………………………..……………………………………………………………………………… 6.27.5 TRIM CONTROLS……………………………………………………………………….……………………………………………………. 6.27.5 PILOT’S AUXILIARY PITCH TRIM……………………………..………………………………………………………….…………… 6.27.5 POSITION INDICATING SYSTEM………………………………………………………………………………………………………. 6.27.5 WING FLAPS………………………………………………………………………………………………………..…………………………. 6.27.7 GUST LOCK SYSTEM…………………………………………………………..……………………..……………………………………. 6.27.8 ELEVATOR GUST LOCK…………………………………………………………..……………………..…………………………. 6.27.9 STALL AVOIDANCE SYSTEM…………………….……….…………………………………………….…………………………….. 6.27.10 FIGURES FIGURE 6.27‐1 AILERON CONTROL…………………………………………………………………………………………………. 6.27.1 FIGURE 6.27‐2 RUDDER CONTROL………….…………………………………………………………………………………..…. 6.27.2 FIGURE 6.27‐3 RUDDER PEDALS……………………………………………………………………………………………………… 6.27.2 FIGURE 6.27‐4 RUDDER TRIM……………………………………………………………………………………………………..…. 6.27.3 FIGURE 6.27‐5 ELEVATOR………………………………………………………………………………………………………………. 6.27.4 FIGURE 6.27‐6 HORIZONTAL STABILIZER…………………………………………………………………………………….…. 6.27.5 FIGURE 6.27‐7 PITCH TRIM AND CONTROL…………………………………………………………………………….....…. 6.27.6 FIGURE 6.27‐8 FLAP CONTROL AND INDICATOR………………………………………………………………………..…. 6.27.7 FIGURE 6.27‐9 GUST LOCK……………………………………………………………………………………………………..………. 6.27.9 FIGURE 6.27‐10 ELEVATOR GUST LOCK…………………………………………………………………………………….……. 6.27.9 FIGURE 6.27‐11 SAS INDICATOR……………………………………………………………………………………………….……. 6.27.9 FIGURE 6.27‐12 STALL AVOIDANCE……………………………………………………………………….……………………... 6.27.10
Revision: Original Aug 1,2013
GO/FCOM/SA227‐SERIES/VTM
AIRCRAFT SYSTEMS FLIGHT CONTROLS
SA227‐ SERIES/FCOM/VTM
INTENTIONALLY LEFT BLANK
Revision: Original Aug 1,2013
GO/FCOM/SA227‐SERIES/VTM
6.27.00.2