DA-42 Austro

⚡ Cheat Sheet
 

Results

⚡ Cheat Sheet
⚡ Cheat Sheet

Q1. Minimum Airspeed for take-off climb with Flaps up(best rate of climb speed: Vy) upto 1900 kgs

90 KIAS

Q2. What is the VNE Never exceed speed in smooth air of DA42

188 KIAS

Q3. Normal Operating range of Oil Pressure is

Correct answer is – 2.5- 6.0 bar

Q4. The red arc of voltage starts at

Correct answer is – 24.1 V

Q5. If the auto pilot trim is inoperative

Correct answer is – Both B & C

Q6. Aspect ratio of the DA42 wing is:

11.06

Q7. What is the Green band Normal operating range of DA42

68 – 151 KIAS

Q8. L/R ALTN FAIL represents

Correct answer is – Left / Right engine generator has failed

Q9. The ECU backup battery provides electrical power for ECU…… minutes.

Correct answer is – 30 minutes

Q10. The primary function of the PFD

Correct answer is – is to provide attitude, heading, air data, navigation, and alerting information to the pilot

Q11. In strong crosswinds use …………to augment steering during take-off.

Correct answer is – Toe brakes

Q12. In case of strong winds, wind shear and turbulence the airspeed on approach should be:

Correct answer is – Higher

Q13. L/R Oil Pressure Low

Correct answer is – Left either Right engine oil pressure is less than 0.9 bar

Q14. Take off’s are not permitted with the fuel selector knob in

Correct answer is – Both B & C

Q15. What is Minimum speed for engine restart

Correct answer is – 100 KIAS

Q16. The Instrument No 27

Correct answer is – Auto Pilot control

Q17. The Warning Message or text is shown in

Correct answer is – Red

Q18. The Negative Maneuvering Load Factor at Vo is

Correct answer is – -1.52

Q19. The Fuel Quantity Indicator range of DA42 NG aircraft is

Correct answer is – 1-25 Gal

Q20. What is the wheel base of the DA42?

1.735m

Q21. if the oil pressure has not moved in green sector after starting

Correct answer is – Shut down engine immediately.

Q22. The Max.Usable fuel in the main tanks is

Correct answer is – 2x 25 US gal

Q23. For each 3 Knots of tailwind increase takeoff distance by______.

10%

Q24. What is the Yellow band caution range – “Only in smooth air” of DA42

151 – 188 KIAS

Q25. Dihedral Angle of the DA42 wing is:

Correct answer is – 5 degrees

Q26. What is VNO Max.structural cruising speed of DA42 NG

Correct answer is – 151 KIAS

Q27. Maximum continuous RPM

Correct answer is – 2300

Q28. Aerobatics, Spinning, & flight maneuvers with more than_____ of bank angle are not permitted in normal category.

Correct answer is – 60°

Q29. Operation is prohibited in the following area:

north of 72° N and south of 70° S latitudes

Q30. The failure of the Attitude and Heading Reference is indicated by a

Correct answer is – All of the above

Q31. Max oil temperature of DA42 engine is

140 degrees C

Q32. Depressing and holding the COM transfer button on the G1000 for___secs will tune the emergency frequency

Correct answer is – 2

Q33. 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

Q34. Max demonstrated airspeed for emergency opening the front canopy in flight is

117 KIAS

Q35. The Maximum demonstrated crosswind for flaps APP is

Correct answer is – 20 Kts

Q36. Before moving the fuel selector knob from CROSSFEED-ON or ON-CROSSFEED ensure

Correct answer is – The fuel pump is switched OFF

Q37. For each 14 Knots of headwind decrease takeoff distance by______.

Correct answer is – 10%

Q38. VNAV information

Correct answer is – Use of VNAV information for Instrument Approach Procedures does not guarantee step-down fix altitude protection

Q39. The maximum and minimum voltage of the battery is

Correct answer is – 32.0 V , 24.1 V

Q40. The electrically driven hydraulic pump comes on for ………….seconds when the electrical master is put on.

Correct answer is – 5-20 sec

Q41. The permitted negative Load Factor at VNE is

Correct answer is – -1.52

Q42. When the Lower light (WHITE) is illuminated, the flaps are in

Landing position

Q43. 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

Q44. Minimum Airspeed for Rotation with flaps up during takeoff for DA42 (Vr) upto 1900 kgs?

Correct answer is – 76 KIAS

Q45. The Instrument No 21 is

Correct answer is – Emergency Compass

Q46. The Maximum Operating altitude of DA42 is

Correct answer is – 18000

Q47. The staling speed with flaps up and landing gear up is______kts at a weight of 1900 Kgs is______.

Correct answer is – 68 Kts

Q48. DA42 has which of the following structures

Correct answer is – Semi-Monocoque

Q49. What is Va for the DA42 above 1800 kgs

122 KIAS

Q50. What is the White band Operating range with flaps fully extended of DA42

Correct answer is – 62 -113 KIAS

Q51. The Positive Maneuvering Load Factor with Flaps down is

Correct answer is – 2.0

Q52. What is the Maximum flap extended speed in approach(VFE LDG)

Correct answer is – 113 KIAS

Q53. In case of a RIGHT engine failure, to maintain lateral balance CROSS FEED must be selected on

Correct answer is – Left fuel selector

Q54. The Maximum Landing Weight of DA42 NG

Correct answer is – 3979 lbs

Q55. One engine inoperative speed for best ROC(Vyse) for DA42 NG

Correct answer is – 85 KIAS

Q56. Stalling speed with FLAPS LAND, GEAR DOWN

Correct answer is – 57 KIAS

Q57. What is the minimum number of crew required for DA 42 NG

Correct answer is – 2

Q58. What is the maximum landing gear retraction speed of DA42

Correct answer is – 152 KIAS

Q59. How many blades does the DA42 propeller engine have:

3 blades

Q60. Max. Load in Cockpit Baggage Compartment

45 kg

Q61. Maximum number of occupants of DA42 is

Correct answer is – 4

Q62. The minimum and maximum oil quantity of DA42 NG is:

Correct answer is – 5 Ltr, 7 Ltr

Q63. The Total usable fuel quantity of the main fuel tanks is of DA42 in gallons is

Correct answer is – 25×2

Q64. Maximum oil pressure

6.5 psi

Q65. Angle of incidence of horizontal tail of DA42 is:

Correct answer is – -1.1 degrees

Q66. What is the maximum landing gear extension speed of DA42

Correct answer is – 188 KIAS

Q67. Stalling speed with FLAP UP, GEAR UP

64 KIAS

Q68. The maximum oil pressure

Correct answer is – 6.5 bar

Q69. The DA 42 has a ………..V DC system.

28 V

Q70. The minimum propeller RPM for feathering is

Correct answer is – 1300 RPM

Q71. After six starts the starter should be allowed to cool for_____minutes.

30 minutes

Q72. 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

Q73. GIA FAN FAIL represents

Correct answer is – Cooling fan for the GIA is inoperative.

Q74. 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

Q75. If the oil pressure has not moved into the green sector within ____seconds after starting, switch off the engine Master

Correct answer is – 3

Q76. What is the max speed that the landing gear wheels, VLE can be subjected to:

Correct answer is – 188 KIAS

Q77. What is the minimum coolant temperature at start up?

Correct answer is – -30 deg C

Q78. Manual extension of landing gear can take_____secs

Correct answer is – 20 secs

Q79. The Negative Maneuvering Load Factor at Vo is

Correct answer is – -1.52

Q80. The Instrument No 2

Correct answer is – Avionics Master

Q81. Landing gear unsafe light should not be on for more than_____secs

20 secs

Q82. What is the Red band Minimum control speed, single engine of DA42

Correct answer is – 71 KIAS

Q83. If the loss of power was due to the unintentional setting of the throttle lever

Correct answer is – Adjust the friction lock

Q84. If the Landing gear CB is pulled _____ light is illuminated

Correct answer is – Red

Q85. What is Best Rate-of-Climb Speed on one engine of DA42?

90 KIAS

Q86. The Positive Maneuvering Load Factor at Vo is

Correct answer is – 3.8

Q87. The Positive Maneuvering Load Factor at VNE is

Correct answer is – 3.8

Q88. The Engine oil used is

SAE Grade 5W-30

Q89. Minimum Go Around Speed for DA42NG Flaps up is

Correct answer is – 90 KIAS

Q90. Minimum Final Approach Speed with Landing Flaps upto 1900 Kgs

Correct answer is – 84 KIAS

Q91. The maximum difference allowed in fuel quantity between LH/RH main tanks is

Correct answer is – 5 USG

Q92. What is the Flaps UP, Minimum control speed airborne of DA42 NG (Vmca)

71 KIAS

Q93. The minimum and maximum fuel pressure of DA42 NG is:

Correct answer is – 4 bar, 7 bar

Q94. What is the VNE Never exceed speed in smooth air of DA42 NG

Correct answer is – 188 KIAS

Q95. DA42 rudder area is:

0.78 m2

Q96. If take-off with the canopy in the cooling gap position

Correct answer is – Land the aircraft and close

Q97. If any one power level is below…….with the landing gear retracted,the warning horn sounds to alert the pilot.

25%

Q98. The Instrument No 09

Correct answer is – The rotary button for instrument lights

Q99. Oil temperature should be between……..to ……….Deg F for continuous operation.

50-135 Deg C

Q100. Usable fuel in auxiliary tanks is ………….. Us Gallons

Correct answer is – 2X13

Q101. The Maximum Emergency Gear Extension speed is

Correct answer is – 152 KIAS

Q102. An upslope of 1% increases take off distance by

9%

Q103. The fuel used in DA 42 NG aircraft is

Correct answer is – JET A, JET A1

Q104. What is VNO, maximum structural cruising speed of DA42 NG

151 KIAS

Q105. Exceeding MTOW will result in

Correct answer is – all of the above

Q106. When the seal on the emergency switch is broken.

VFR flights can be taken

Q107. The Datum plane is located at a distance of ………..from the wing root.

2.196m

Q108. What is the wingspan of the DA42?

Correct answer is – 13.42 m

Q109. The Maximum demonstrated crosswind for flaps UP is ______.

Correct answer is – 25 Kts

Q110. What is maximum Gear box temperature?

Correct answer is – 120 deg C

Q111. Fuel information displayed when pushing the FUEL button

Correct answer is – Are supplemental information and requires verification by the flight crew.

Q112. The landing gear unsafe warning light illuminates if the landing gear is

Correct answer is – All the above

Q113. Do not operate the starter motor for more than_____.

30 Seconds

Q114. What is the Blue band Best rate of climb speed, single engine of the DA42

85 KIAS

Q115. The engine instruments are available on the MFD only when

Correct answer is – G1000 power up completed

Q116. The Design of the Prop Feathering System does not allow the feathering of a prop

Correct answer is – With speed below 1300 RPM

Q117. What is the wing area of the DA42?

Correct answer is – 16.29 m²

Q118. To check cross feed the engines should be run for a minimum of ……….

Correct answer is – 30 seconds

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