Quiz: DHC-6-300 Other Limitations

Descripción

Quiz: DHC-6-300 Other Limitations for the Grand Canyon Scenic operation. This is not an official source of information.
Rieul Gendron
Test por Rieul Gendron, actualizado hace más de 1 año
Rieul Gendron
Creado por Rieul Gendron hace casi 5 años
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Resumen del Recurso

Pregunta 1

Pregunta
In an emergency when jet fuel is not available, any grade of AVGAS may be used, but only at specific mixture ratios.
Respuesta
  • True
  • False

Pregunta 2

Pregunta
What is the maximum fuel temperature and maximum ambient temperature for takeoff when using AVGAS?
Respuesta
  • 20 degrees Celsius
  • 25 degrees Celsius
  • 30 degrees Celsius
  • 35 degrees Celsius

Pregunta 3

Pregunta
What is the maximum operating altitude when using AVGAS?
Respuesta
  • 8,000 feet
  • 10,000 feet
  • 12,000 feet
  • 15,000 feet

Pregunta 4

Pregunta
At least one boost pump per tank must be serviceable at all times when AVGAS is being used.
Respuesta
  • True
  • False

Pregunta 5

Pregunta
What is the maximum operating altitude of the DHC-6-300 according to the POH?
Respuesta
  • 10,000 feet
  • 15,000 feet
  • 20,000 feet
  • 25,000 feet

Pregunta 6

Pregunta
Select all that apply. The approved flap takeoff setting(s) is/are:
Respuesta
  • 0
  • 10
  • 20
  • 37.5

Pregunta 7

Pregunta
Select all that apply. For normal operations, according to the POH, the approved flap landing setting(s) is/are:
Respuesta
  • 0
  • 10
  • 20
  • 37.5

Pregunta 8

Pregunta
Choose the correct answer. At a gross weight of 12,500 lbs and flaps RETRACTED, the flight load factors to which the DHC-6 airplane has been designed are (normal category):
Respuesta
  • +3.17g to -1.5g
  • +2.0g to -1.5g
  • +1.5g to -3.17g
  • +1.5g to -2.0g

Pregunta 9

Pregunta
Choose the correct answer. At a gross weight of 12,500 lbs and flaps EXTENDED, the flight load factors to which the DHC-6 airplane has been designed are (normal category):
Respuesta
  • +2.0g to -1.5g
  • +3.17g to -1.5g
  • +1.5g to -3.17g
  • +3.17g to -2.0g

Pregunta 10

Pregunta
Select ALL that apply. The Twin Otter is certified in the Normal Category. Accordingly, the following are NOT approved:
Respuesta
  • Spins
  • Lazy eights
  • Chandelles
  • Turns with an angle of bank exceeding 45 degrees
  • Turns with an angle of bank exceeding 60 degrees
  • Stalls

Pregunta 11

Pregunta
Fill in the blank with no spaces or commas. Flap extension must not exceed [blank_start]10[blank_end]° during or after flight in icing conditions.
Respuesta
  • 10

Pregunta 12

Pregunta
Engine intake deflectors must be [blank_start]extended[blank_end] during flight in icing conditions.
Respuesta
  • extended
  • retracted

Pregunta 13

Pregunta
Fill in the blanks with numbers only. In level flight, the low-level trigger point is [blank_start]75[blank_end] pounds usable fuel remaining for the forward tank and [blank_start]110[blank_end] pounds usable fuel remaining for the aft tank.
Respuesta
  • 75
  • 110

Pregunta 14

Pregunta
Fill in the blanks with numbers only. The nose wheel is steerable over a range of [blank_start]60[blank_end] degrees to left and right of the centre position for purposes of low-speed ground manoeuvring.
Respuesta
  • 60
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