Q1. What is the minimum coolant temperature at start up?
Correct answer is – -30 deg C
Q2. The Maximum Emergency Gear Extension speed is
Correct answer is – 152 KIAS
Q3. Minimum Final Approach Speed with Landing Flaps upto 1900 Kgs
Correct answer is – 84 KIAS
Q4. Fuel information displayed when pushing the FUEL button
Correct answer is – Are supplemental information and requires verification by the flight crew.
Q5. Maximum continuous RPM
Correct answer is – 2300
Q6. What is the max speed that the landing gear wheels, VLE can be subjected to:
Correct answer is – 188 KIAS
Q7. The Negative Maneuvering Load Factor at Vo is
Correct answer is – -1.52
Q8. The Instrument No 09
Correct answer is – The rotary button for instrument lights
Q9. Reduce airspeed below_____ and apply moderate yawing and pitching to assist in bringing the landing gear into the locked position.
Correct answer is – 110 KIAS
Q10. When the Lower light (WHITE) is illuminated, the flaps are in
Landing position
Q11. What is VNO Max.structural cruising speed of DA42 NG
Correct answer is – 151 KIAS
Q12. 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:
Correct answer is – 110 kts
Q13. How many blades does the DA42 propeller engine have:
3 blades
Q14. The ECU backup battery provides electrical power for ECU…… minutes.
Correct answer is – 30 minutes
Q15. Normal Operating range of Oil Pressure is
Correct answer is – 2.5- 6.0 bar
Q16. L/R ALTN FAIL represents
Correct answer is – Left / Right engine generator has failed
Q17. To check cross feed the engines should be run for a minimum of ……….
Correct answer is – 30 seconds
Q18. For each 3 Knots of tailwind increase takeoff distance by______.
10%
Q19. For each 14 Knots of headwind decrease takeoff distance by______.
Correct answer is – 10%
Q20. If take-off with the canopy in the cooling gap position
Correct answer is – Land the aircraft and close
Q21. Oil temperature should be between……..to ……….Deg F for continuous operation.
50-135 Deg C
Q22. What is the maximum landing gear retraction speed of DA42
Correct answer is – 152 KIAS
Q23. The minimum and maximum fuel pressure of DA42 NG is:
Correct answer is – 4 bar, 7 bar
Q24. What is the Green band Normal operating range of DA42
68 – 151 KIAS
Q25. The permitted negative Load Factor at VNE is
Correct answer is – -1.52
Q26. What is the wing area of the DA42?
Correct answer is – 16.29 m²
Q27. The electrically driven hydraulic pump comes on for ………….seconds when the electrical master is put on.
Correct answer is – 5-20 sec
Q28. Minimum Airspeed for Rotation with flaps up during takeoff for DA42 (Vr) upto 1900 kgs?
Correct answer is – 76 KIAS
Q29. An upslope of 1% increases take off distance by
9%
Q30. Landing gear unsafe light should not be on for more than_____secs
20 secs
Q31. Take off’s are not permitted with the fuel selector knob in
Correct answer is – Both B & C
Q32. What is the Red band Minimum control speed, single engine of DA42
Correct answer is – 71 KIAS
Q33. What is Best Rate-of-Climb Speed on one engine of DA42?
90 KIAS
Q34. What is the minimum number of crew required for DA 42 NG
Correct answer is – 2
Q35. The Instrument No 2
Correct answer is – Avionics Master
Q36. The Maximum Landing Weight of DA42 NG
Correct answer is – 3979 lbs
Q37. The Datum plane is located at a distance of ………..from the wing root.
2.196m
Q38. VNAV information
Correct answer is – Use of VNAV information for Instrument Approach Procedures does not guarantee step-down fix altitude protection
Q39. Exceeding MTOW will result in
Correct answer is – all of the above
Q40. What is the Blue band Best rate of climb speed, single engine of the DA42
85 KIAS
Q41. What is the wheel base of the DA42?
1.735m
Q42. The primary function of the PFD
Correct answer is – is to provide attitude, heading, air data, navigation, and alerting information to the pilot
Q43. Aspect ratio of the DA42 wing is:
11.06
Q44. The Maximum demonstrated crosswind for flaps APP is
Correct answer is – 20 Kts
Q45. In case of strong winds, wind shear and turbulence the airspeed on approach should be:
Correct answer is – Higher
Q46. What is the Yellow band caution range – “Only in smooth air” of DA42
151 – 188 KIAS
Q47. Minimum Go Around Speed for DA42NG Flaps up is
Correct answer is – 90 KIAS
Q48. Max oil temperature of DA42 engine is
140 degrees C
Q49. The Maximum Operating altitude of DA42 is
Correct answer is – 18000
Q50. The Positive Maneuvering Load Factor with Flaps down is
Correct answer is – 2.0
Q51. Stalling speed with FLAP UP, GEAR UP
64 KIAS
Q52. The Negative Maneuvering Load Factor at Vo is
Correct answer is – -1.52
Q53. The Fuel Quantity Indicator range of DA42 NG aircraft is
Correct answer is – 1-25 Gal
Q54. What is VNO, maximum structural cruising speed of DA42 NG
151 KIAS
Q55. The engine instruments are available on the MFD only when
Correct answer is – G1000 power up completed
Q56. If the loss of power was due to the unintentional setting of the throttle lever
Correct answer is – Adjust the friction lock
Q57. Operation is prohibited in the following area:
north of 72° N and south of 70° S latitudes
Q58. One engine inoperative speed for best ROC(Vyse) for DA42 NG
Correct answer is – 85 KIAS
Q59. The Warning Message or text is shown in
Correct answer is – Red
Q60. The DA 42 has a ………..V DC system.
28 V
Q61. The Max.Usable fuel in the main tanks is
Correct answer is – 2x 25 US gal
Q62. Before moving the fuel selector knob from CROSSFEED-ON or ON-CROSSFEED ensure
Correct answer is – The fuel pump is switched OFF
Q63. Max. Load in Cockpit Baggage Compartment
45 kg
Q64. Maximum oil pressure
6.5 psi
Q65. The Maximum demonstrated crosswind for flaps UP is ______.
Correct answer is – 25 Kts
Q66. Max demonstrated airspeed for emergency opening the front canopy in flight is
117 KIAS
Q67. Stalling speed with FLAPS LAND, GEAR DOWN
Correct answer is – 57 KIAS
Q68. What is Minimum speed for engine restart
Correct answer is – 100 KIAS
Q69. What is the VNE Never exceed speed in smooth air of DA42 NG
Correct answer is – 188 KIAS
Q70. The Engine oil used is
SAE Grade 5W-30
Q71. DA42 has which of the following structures
Correct answer is – Semi-Monocoque
Q72. When the seal on the emergency switch is broken.
VFR flights can be taken
Q73. In strong crosswinds use …………to augment steering during take-off.
Correct answer is – Toe brakes
Q74. The landing gear unsafe warning light illuminates if the landing gear is
Correct answer is – All the above
Q75. Dihedral Angle of the DA42 wing is:
Correct answer is – 5 degrees
Q76. if the oil pressure has not moved in green sector after starting
Correct answer is – Shut down engine immediately.
Q77. Aerobatics, Spinning, & flight maneuvers with more than_____ of bank angle are not permitted in normal category.
Correct answer is – 60°
Q78. If the Landing gear CB is pulled _____ light is illuminated
Correct answer is – Red
Q79. If any one power level is below…….with the landing gear retracted,the warning horn sounds to alert the pilot.
25%
Q80. The failure of the Attitude and Heading Reference is indicated by a
Correct answer is – All of the above
Q81. What is maximum Gear box temperature?
Correct answer is – 120 deg C
Q82. What is the maximum landing gear extension speed of DA42
Correct answer is – 188 KIAS
Q83. What is the Flaps UP, Minimum control speed airborne of DA42 NG (Vmca)
71 KIAS
Q84. If the oil pressure has not moved into the green sector within ____seconds after starting, switch off the engine Master
Correct answer is – 3
Q85. What is Va for the DA42 above 1800 kgs
122 KIAS
Q86. The fuel used in DA 42 NG aircraft is
Correct answer is – JET A, JET A1
Q87. Do not operate the starter motor for more than_____.
30 Seconds
Q88. The Instrument No 21 is
Correct answer is – Emergency Compass
Q89. What is the VNE Never exceed speed in smooth air of DA42
188 KIAS
Q90. Depressing and holding the COM transfer button on the G1000 for___secs will tune the emergency frequency
Correct answer is – 2
Q91. The staling speed with flaps up and landing gear up is______kts at a weight of 1900 Kgs is______.
Correct answer is – 68 Kts
Q92. What is the White band Operating range with flaps fully extended of DA42
Correct answer is – 62 -113 KIAS
Q93. After six starts the starter should be allowed to cool for_____minutes.
30 minutes
Q94. L/R Oil Pressure Low
Correct answer is – Left either Right engine oil pressure is less than 0.9 bar
Q95. Maximum number of occupants of DA42 is
Correct answer is – 4
Q96. The Total usable fuel quantity of the main fuel tanks is of DA42 in gallons is
Correct answer is – 25×2
Q97. The Positive Maneuvering Load Factor at Vo is
Correct answer is – 3.8
Q98. The Instrument No 27
Correct answer is – Auto Pilot control
Q99. The maximum difference allowed in fuel quantity between LH/RH main tanks is
Correct answer is – 5 USG
Q100. What is the wingspan of the DA42?
Correct answer is – 13.42 m
Q101. The maximum and minimum voltage of the battery is
Correct answer is – 32.0 V , 24.1 V
Q102. If the oil pressure indication drops below the green sector and the oil temperature is normal
it is probable that the oil pressure indication is defective
Q103. The red arc of voltage starts at
Correct answer is – 24.1 V
Q104. DA42 rudder area is:
0.78 m2
Q105. The minimum and maximum oil quantity of DA42 NG is:
Correct answer is – 5 Ltr, 7 Ltr
Q106. The Design of the Prop Feathering System does not allow the feathering of a prop
Correct answer is – With speed below 1300 RPM
Q107. The maximum oil pressure
Correct answer is – 6.5 bar
Q108. If the fuel selector is set on CROSS FEED ,the engine will be supplied with fuel
Correct answer is – From the main tank on the opposite side
Q109. Usable fuel in auxiliary tanks is ………….. Us Gallons
Correct answer is – 2X13
Q110. The minimum propeller RPM for feathering is
Correct answer is – 1300 RPM
Q111. What is the Maximum flap extended speed in approach(VFE LDG)
Correct answer is – 113 KIAS
Q112. The Positive Maneuvering Load Factor at VNE is
Correct answer is – 3.8
Q113. In case of a RIGHT engine failure, to maintain lateral balance CROSS FEED must be selected on
Correct answer is – Left fuel selector
Q114. Minimum Airspeed for take-off climb with Flaps up(best rate of climb speed: Vy) upto 1900 kgs
90 KIAS
Q115. Angle of incidence of horizontal tail of DA42 is:
Correct answer is – -1.1 degrees
Q116. GIA FAN FAIL represents
Correct answer is – Cooling fan for the GIA is inoperative.
Q117. Manual extension of landing gear can take_____secs
Correct answer is – 20 secs
Q118. If the auto pilot trim is inoperative
Correct answer is – Both B & C
