BE9L (2)

what is the individual generator rating. 24volt 200 amp. 28 volt 250 amp. 28 volt 200 amp.

secondary flight display works with. GPU power. external power. battery.

minimum temperature for operation of deicing boots. """-""0°C". """-""10°C. """-""40°C.

propeller deice ammeter operating range green arc. 15 to 20 amp. 10 to 20 amp. 18 to 24 amp.

when a generator is off line, what indication is present. a yellow DC GEN light is on. a red DC GEN light is on. an amber DC GEN light is on.

the PT6A engine power section consist of. two-stage power turbine. a single-stage power turbine. stage power turbine.

the landing gear is held in the retracted position by. continously applied hydraulic pressure. gravity. electrical.

what indicationreflects the rate of cabin pressure altitude change. cabin despresuritation. cabin climb (cabin vertical speed) indicator. vertical speed.

when using maximum reverse power with the prop lever full forward, you expect maximum propeller RPM of. 1900 RPM. 2000 RPM. 1700 RPM.

cual es la velocidad para retraer el tren de aterrizaje. 163 kias. 156 kias. 140 kias.

air minimum control speed VMC flaps up. 85 kias. 90 kias. 82 kias.

maximum occupancy limit. 6. 13 including crew. 8 including.

en el encendido de los motores, cuanto es el tiempo limite en el que debe haber un incremento en la ITT. 10 sec. 8 sec. 1 min.

cual es la presion de la rueda del tren de nariz. 30-45 psi. 60-65 psi. 50-55 psi.

velocidad de orden tecnico para ascender de 10,000 ft a 20,000 ft. 100 kias. 130 kias. 150 kias.

one engine inoperative best angle of climb (VXSE). 90 kias. 100 kias. 130 kias.

cual es la funcion de FCU (fuel control unit). controlar el consumo de combustible. medir la presion del combustible. controlar cuanto combustible va a la camara de combustion.

to what system does the pneumatic system suply bleed air. vacuum, flight hourmeter, door seal, surface deice, rudder boost and hydraulic reservoir. vacuum systems. ice boots.

propeller rotational speed reverse limit. 1825 RPM. 1625 RPM. 1925 RPM.

operation of the engine with the FUEL PRESS light illuminated is limited to wich of the following. eight hours of engine operation before the engine driven fuel pump needs to be overhauled. ten hours of engine operation before the engine driven fuel pump needs to be overhauled. thrty hours of engine operation before the engine driven fuel pump needs to be overhauled.

if the wing flaps are beyond the approach position, the warning horn will sound if. any one gear is not down and locked, regardless of power lever setting. both power levers are retarded below a specified setting. below specified setting.

cual es la velocidad establecida para entrar en aire turbulento. 190 kias. 181 kias. 161 kias.

how much continous current should the external power unit be capable of supplying. 200 amp. 500 amp. 300 amp.

minimum airspeed for susstained icing flight. 160 kias. 130 kias. 140 kias.

when the landing gear is fully retracted, the electrically driven hydraulic pump. stops, but cycles as required. continue and cycle is not required. retract.

cual es la velocidad para realizar un planeo. 125 kias. 130 kias. 145 kias.

los HED limitan la corriente a. 275 amp. 250 amp. 24 volts.

bajo que circunstancia haremos procedimiento de crossfeed. falla de un motor. daño de la bomba boost- motor inoperativo. daño del crossfeed.

propeller rotational speed transient limit. 2000 RPM. 1800RPM. 2090 RPM.

vx speed. 101 kias. 90 kias. 110 kias.

capacidad de combustible en el tanque central. 44 galones. 40 galones. 34 galones.

cual es la temperatura mínima recomendada para incrementar la vida util del aceite del motor. 55°C. 35°C. 75°C.

propeller rotational speed reverse limit. 1700 RPM. 1925 RPM. 1825 RPM.

nacelle tank capacity. 61 gal. 40 gal. 35 gal.

falla de motor despues del VR despegue continuado VR. abortar despegue. acelerar para 112 kias. rotar aproximadamente 10°.

los limitadores de corriente de la barra triple tienen un amperaje de. 30. 20. 60.

when the auto-ignition switch is in the arm position, ignition is. inactive but armed, if torque is greater. inactive but armed, if torque is greater than 400 foort-pounds. active all the times.

the fuel panel check test electrical continuity to which items. crossfeed valve. boost pumps and crossfeed valves. firewall valves, boost pumps and the crossfeed valve-.

en caso de falla de los generadores, la batería del SFDS tiene una duración de. 30 minutos. 45 minutos. 60 minutos.

cuanto es el limitante de la temperatura de aceite del motor para el despegue. 35°C-99°C. 10°C-99°C. 55°C-99°C.

cual es el sobrevoltaje para el external power. 10 +/-,5 volts. 30+/-,5 volts. 31+/-,5 volts.

el BE9L-gti tiene una bateria de. 24 volts-42 amp. 28 volts-42 amp. 24 volts-48 amp.

maxima limitante de tiempo para el uso de los reversibles. 5 minutos. no tiene limite. 1 minuto.

maximum operating pressure altitude limit. 20,000 ft. 25,000 ft. 30,000ft.

una de las funciones del control delgenerador (GCU) es. back up. regular el voltaje.

the fuel panel check test electrical continuity to which items. boost pumups and crossfeed valve. crossfeed valve. boost pumps.

si el BE9L-GTI presenta una falla e el auto feather ese item es. no es importante. obligatorio para despegues (no go). se puede volar.

en que rango de temperatura trabajan los windshield heats. 15°C a 30°C. 20°C a 30°C. 32°C a 43°C.

one engine inoperative best angles of climb (VXSE). 90 kias. 100 kias. 140 kias.

how many continued flight hours can be operated the airplane with fuel press light. 1 hour. 10 hours. 30 hours.