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* Fuel Control The engine fuel control is a hydromechanical control. Variables sensed by the fuel control are 1) power lever angle, 2) burner pressure 3) ...
Title: Max Land Weight Author: Brian M. Carter Last modified by: Thann Created Date: 11/9/2004 2:39:24 AM Document presentation format: On-screen Show (4:3)
2 Qts Low in Press. Sump. Click to return to Table Of Contents. PROPS. Prop Brake Held Disengaged. ... Prop Aux Pump Operating limit.Static Feather Check time ...
EGT/RPM Warning light or compressor stall. Incorrect or uncommanded Engine. Fire ... uncommanded brake pressure light(s) (T-45A), or nose wheel steering failure ...
Emergency and Abnormal Procedures Cirrus SR-22 Transition Training 8/16/04 CAPS Deployment (cont) Shutting off fuel supply to engine will reduce the chances of fire ...
Min safe one engine inoperative. 227. VMO. Max dive/level flight ... Immediately prior to departing runway. Condition levers Fuel Cutoff. as soon as practical ...
Cirrus SR-20 Transition Training 8/16/04 CAPS will be covered in greater detail on another presentation. Forced Landing (Engine Out) Landing without Elevator Control ...
... Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y Y ... 333 3f f 3f3 3f33 3f33f333 3 3f f3 3ff33 ff f f fff3f f3 3 3 3ff f f3 LS*L8IDATx ...
Fail to Feather ... Airstart Prop Failed to Unfeather. Overhead CB's matter too ... Still fly to fail (i.e. not replaced during phase), but now only being replaced ...