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.
Pregunta 2
Pregunta
What is the maximum fuel temperature and maximum ambient temperature for takeoff when using AVGAS?
Respuesta
-
20 degrees Celsius
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25 degrees Celsius
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30 degrees Celsius
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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
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15,000 feet
Pregunta 4
Pregunta
At least one boost pump per tank must be serviceable at all times when AVGAS is being used.
Pregunta 5
Pregunta
What is the maximum operating altitude of the DHC-6-300 according to the POH?
Respuesta
-
10,000 feet
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15,000 feet
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20,000 feet
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25,000 feet
Pregunta 6
Pregunta
Select all that apply.
The approved flap takeoff setting(s) is/are:
Pregunta 7
Pregunta
Select all that apply.
For normal operations, according to the POH, the approved flap landing setting(s) is/are:
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
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+2.0g to -1.5g
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+1.5g to -3.17g
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+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:
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.
Pregunta 12
Pregunta
Engine intake deflectors must be [blank_start]extended[blank_end] during flight in icing conditions.
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.
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.