DA 42 Question Bank

Question #1: What is the wing area of DA42 ?

Question #2: What is the wingspan of the DA42?

Question #3: Dihedral angle of DA 42 is :

Question #4: Aspect ratio of the DA 42 wing is :

Question #5: Angle of incidence of horizontal tail of DA 42 is :

Question #6: DA 42 rudder area is

Question #7: What is the wheel base of DA 42 ?

Question #8: How many blades does the DA 42 propeller have ?

Question #9: Datum plane is defined as :

Question #10: Minimum speed for engine restart :

Question #11: Exceeding MTOW will result in

Question #12: L/R ALTN Fail represents

Question #13: DA 42 operation is prohibited in the following area :

Question #14: VNAV information

Question #15: Maximum continuous RPM :

Question #16: Maximum oil pressure :

Question #17: GIA FAN FAIL represents

Question #18: Maximum load in the cockpit luggage compartment is

Question #19: The negative manoeuvring load factor at V𝜊

Question #20: When the seal on the emergency switch is broken

Question #21: What if the maximum landing gear extension speed of DA 42

Question #22: What is the Va for DA42 above 1800 kg

Question #23: What is the maximum landing gear retraction speed of DA42 ?

Question #24: What is the maximum emergency gear extension speed of DA42 ?

Question #25: What is the Flaps UP minimum control speed airborne of DA 42(Vmca) ?

Question #26: What is the VNO maximum structural cruising speed of DA42 ?

Question #27: What if the VNE never exceed speed in smooth air of DA42 ?

Question #28: What is the Yellow band caution range – “Only in smooth air ” of DA42 ?

Question #29: What is the Red Band minimum control speed , single engine speed of DA42 ?

Question #30: What is the Blue band Best rate of climb speed, single engine of the DA 42 ?

Question #31: The Positive Maneuvering Load Factor at Vo is

Question #32: The Positive Maneuvering Load Factor at VNE is

Question #33: The Positive Maneuvering Load Factor with Flaps down is

Question #34: The negative manoeuvring load factor at Vo is

Question #35: The permitted negative load factor at Vne is

Question #36: Total usable fuel quantity in the main fuel in DA 42 tanks is

Question #37: The landing gear unsafe warning light illuminates if the landing gear is

Question #38: If any one power lever is below___ with the landing gear retracted,the warning horn sounds to alert the pilot.

Question #39: What is the minimum number of crew required for DA42 NG?

Question #40: The red arc of voltage starts at

Question #41: The minimum and maximum fuel pressure of DA42 NG is :

Question #42: Max oil temperature of DA42 engine is

Question #43: Usable fuel in auxiliary tanks is____US Gallons.

Question #44: What is the VNE Never exceed speed in smooth air of DA42 ?

Question #45: The Engine oil used is

Question #46: The fuel used in DA42 NG aircraft is

Question #47: Aerobatics,Spinning & flight maneuvers with more than ___of bank angle are not permitted in normal category

Question #48: The maximum difference allowed in fuel quantity between LH/RH main tank is

Question #49: The Max Usable fuel in the main tanks is

Question #50: The maximum and minimum voltage of the battery is

Question #51: The maximum oil pressure

Question #52: The minimum and maximum oil quantity of DA42 NG is :

Question #53: Normal operating range of Oil Pressure is

Question #54: Maximum number of occupants of DA42 is

Question #55: VFE is the

Question #56: What is the Green band Normal operating range of DA42?

Question #57: What is VNO, maximum structural cruising speed of DA42 NG

Question #58: What is maximum flap extended speed in approach(VFELDG)

Question #59: One engine inoperative speed for best ROC( Vyse) for DA42 NG is

Question #60: What is the max speed that the landing gear wheels , VLE can be subjected to:

Question #61: What is maximum Gear box temperature?

Question #62: What is the minimum coolant temperature at start up?

Question #63: Oil temperature should be between

Question #64: The maximum landing weight of DA42 NG is :

Question #65: Reduce airspeed below____and apply moderate yawing and pitching to assist in bringing the landing gear into the locked position.

Question #66: The failure of the Attitude and Heading Reference is indicated by a

Question #67: Do not operate starter motor for more than__

Question #68: The engine instruments are available on the MFD only when

Question #69: If take-off with the canopy in the cooling gap position

Question #70: To check cross feed the engines should be run for a minimum of

Question #71: The electrically driven hydraulic pump comes on for ___ seconds when the electrical master is put on.

Question #72: If the oil pressure has not moved into the green sector within__ seconds after starting.switch off the engine Master

Question #73: In strong crosswinds use ___ to augment steering during take-off.

Question #74: What is the White band Operating range with flaps fully extended of DA42?

Question #75: Minimum Go Around Speed for DA42NG Flaps up is

Question #76: Minimum Final Approach Speed with Landing Flaps upto 1900 Kgs

Question #77: Minimum Airspeed for take-of climb with Flaps up(best rate of climb speed : Vy)upto 1900 kgs

Question #78: Minimum Airspeed for Rotation with flaps up during takeoff for DA42 (Vr) upto 1900 kgs?

Question #79: If the loss of power was due to the unintentional setting of the throttle lever

Question #80: If the Landing gear CB is pulled ____ light is illuminated

Question #81: If the fuel selector is set on CROSS FEED , the engine will be supplied with fuel

Question #82: In case of a RIGHT engine failure, to maintain lateral balance CROSS FEED must be selected on

Question #83: Depressing and holding the COM transfer button on the G1000 for___sec will tune the emergency frequency

Question #84: If the auto pilot trim is inoperative

Question #85: After six starts the starter should be allowed to cool for___minutes.

Question #86: Landing gear unsafe light should not be on for more than___ sec

Question #87: Max demonstrated airspeed for emergency opening the front canopy in flight is

Question #88: Yawing and pitching can be done to assist the landing gear to lock down in case of manual lowering of the undercarriage.The speed should be reduced to :

Question #89: Manual extension of landing gear can take___sec

Question #90: What is Best Rate-of-climb speed on one engine of DA42?

Question #91: If the oil pressure indication drops below the green sector and the oil temperature is normal

Question #92: If the oil pressure has not moved in green sector after starting