FOM - MEP T2006P Questions and Correct Solutions A+

Propellers on piston-engine twins are driven toward the Feathered position (high pitch) by: - propeller counterweights The ineffectiveness of one engine results in asymmetric traction which tends: - to yaw and bank the aircraft towards the inoperative engine. Recommended flaps position for One Engine Inoperative landing - T/O Total usable fuel (per 2 tanks): - 194,4 l Memory items from a typical "Engine Failure After Takeoff" checklist: - Airspeed Vyse; Mixtures-RICH; Propellers-HIGH RPM; Throttles-FULL; Flaps-UP; Landing Gear-UP; Identify- Determine failed engine; Verify - Close throttle of failed engine; Propeller of failed engine - Feather. Stall speed with bank angle 0 and flaps up (VS1): - 66 KIAS Maximum allowed speed with flaps extended (T/O): - 122 KIAS Wing span: - 11.4 m For a rule, light twins should not be airborne before reaching: - Vmc Maximum baggage weight: - 80 kg The barometric pressure setting is displayed in PFD: - below the Altimeter. Engine maximum power: - 98,6 hp An airspeed indicator's green band shows: - Normal Operating Range In event of L or R ALT FAIL caution alert displayed, pilot must apply following procedure: - FIELD LH (or RH) - OFF, FIELD LH (or RH) - ON; if caution alert stay displayed: FIELD LH (or RH) - OFF, AVIONIC LH (or RH) - OFF, ADF - OFF, limit the landing light use; if caution alert stay displayed: CROSS BUS LH (or RH) - OFF Electrical system type is: - 12 V, DC The basic OEI emergency procedures common to all conventional light twins: - Control.Configure. Climb. Checklist Propeller type: - variable pitch (constant speed) Minimum oil pressure (RPM1400): - 0,8 bar In case of single generator failure the battery and another generator are able to supply electrical power necessary for: - the entire mission, but redundancy is lost. Aircraft Minimum control speed (VMC) with one engine inoperative: - 62 KIAS Recommended safe simulated OEI speed (Vsse) - 70 KIAS Who is responsible for checking the weight and CG excursion are compliant with the related limits: - Pilot Emergency gear extension access door location is: - on pilots left side floor. Minimum oil temperature (C°): - 50° Never exceed speed in any operation (VNE): - 171 KIAS For an airplane CG position calculation the Datum is: - The wing leading edge vertical After lift-of Vy should be maintained until: - a safe single engine maneuvering altitude, typically at least 400 feet AGL, has been achieved. The MFD normally displays - a full-color moving map with navigation information, while the left portion of the MFD is dedicated to the Navigation information Display. Propeller: - number of blades - 2, made of wood/composite An airspeed indicator's white band's upper limit shows: - Maximum speed with flaps FULL Engine securing in flight procedure: - Throttle - IDLE; Ignition - both OFF; Propeller - FEATHER; Fuel Selector - OFF; Electrical Fuel Pump - OFF In case of both generators failure the battery supply electrical power for at least: - 30 min.