BE9L

Máximum cabin differential pressure?. 4,1 PSI. 5,1 PSI. 6,2 PSI.

minimum airspeed for susstained icing flight?. 135 kias. 140 kias. 145 kias.

landing gear retraction speed VLO. 163. 160. 150.

air minimum control speed VMC flaps up. 83 kias. 85 kias. 82 kias.

maximum operating speed?. 200. 210. 226.

maximum crosswind?. 15 kts. 20 kts. 25 kts.

one engine inoperative best angle of climb (VXSE). 85 kias. 100 kias. 105 kias.

itt for start. 820 C. 700 C. 1090 C.

oil pressure for take off and maximum continous power?. 35 to 102 PSI. 85 to 105 PSI. 45 to 105 PSI.

external power limits in volts. 28 volts. 20 volts. 15 volts.

total usable fuel. 340 gal. 384 gal. 300 gal.

minimum fuel for take off. 100 lbs. 200 lbs. 265 lbs.

maximum take off weight. 10,000 lbs. 10,485 lbs. 12,000 lbs.

maximum rear compartment door weight. 200 lbs. 100 lbs. 350 lbs.

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

maximum outside air temperature limit. ISA+20. ISA+10. ISA+33.

continued flight with a cracked windshield is limited to. 10 hours. 40 hours. 25 hours.

horse power for each engine. 200 shp. 300 shp. 550 shp.

how many fuel pumps can be inoperative for take off. 1. 2. 0.

at what altitude the cabin altitude light will illuminate. 20,000 fts. 5,000 ft. 12,500 ft.

flaps are elictrical powered and _______ operated. mechanic. electrical. hidraulic.

how many tanks does the plane have for each wing. 8. 5. 1.

how many fuel drain holes does the plane have for each wing. 15. 1. 5.

how much fuel is lost with a failure of a transfer pump. 28 gal. 61 gal. 100 gal.

maximum ITT for transient condition. 500 C. 300 C. 880 C.

how many axial flow stages does each engine have. 10. 3. 4.

oil quarters capacity. 14 quarters. 5 quarters. 10 quarters.

how many emergency exits does the plane have. 2. 1. 5.

whats the rating for the battery. 28 volts 24 amp. 20 volts 10 amp. 24 volts 42 amp.

engine model number. pt6a-135a. pta10b-35. pt1c-2a.

secondary flght display sistem works with. independent battery. generator power. gpu power.

how many continued hours we can operate with fuel press light. 10 hours. 30 hours. 100 hours.

fuel aproved for flight. JET A, JETA1, JET B, JP. JP8 JP10. military N20.

maximum fuel inbalance. 500 lbs. 300 lbs. 200 lbs.

recomendable oil temperature. 10 C. 20 C. 55 C.

torque for take off maximum continous. 1800 lbs. 1520 lbs. 2000 lbs.

oil pressure low idle. 40 PSI. 80 PSI. 100 PSI.

primary gobernors works with. P3 air. oxygen. oil.

emergency descend speed. 200 kias. 182 kias. 250 kias.

glide speed. 130 kias. 200 kias. 125 kias.

turbulence speed. 161 kias. 164 kias. 180 kias.

maximum tailwind capacity. 18 kts. 12 kts. 25 kts.

VX speed. 110 kias. 120 kias. 101 kias.

maximum landing weight. 9832 lbs. 9000 lbs. 10500 lbs.

nacelle tank capacity. 80 gal. 20 gal. 61 gal.

dihedral angle of the plane. 10°. 7°. 15°.

fuel crossfeed is authorized with. boost pump failure and engine failure. boost pump failure. over ride failure.

max operating pressure altitude with yaw damper off. 20,000 ft. 24,000 ft. 15,000 ft.

answer for the memory item cabbin door unlocked is. all occupants seatbelts off. close door open inmediately. all occupants seated with seatbelts secured.

answer for the memory item rudder boost failure is. landing gear down. rudder boost off. rudder boost reset.