Rieul Gendron
Quiz by , created more than 1 year ago

Quiz: DHC-6-300 Other Limitations for the Grand Canyon Scenic operation. This is not an official source of information.

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Rieul Gendron
Created by Rieul Gendron almost 5 years ago
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Quiz: DHC-6-300 Other Limitations

Question 1 of 14

1

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

Select one of the following:

  • True
  • False

Explanation

Question 2 of 14

1

What is the maximum fuel temperature and maximum ambient temperature for takeoff when using AVGAS?

Select one of the following:

  • 20 degrees Celsius

  • 25 degrees Celsius

  • 30 degrees Celsius

  • 35 degrees Celsius

Explanation

Question 3 of 14

1

What is the maximum operating altitude when using AVGAS?

Select one of the following:

  • 8,000 feet

  • 10,000 feet

  • 12,000 feet

  • 15,000 feet

Explanation

Question 4 of 14

1

At least one boost pump per tank must be serviceable at all times when AVGAS is being used.

Select one of the following:

  • True
  • False

Explanation

Question 5 of 14

1

What is the maximum operating altitude of the DHC-6-300 according to the POH?

Select one of the following:

  • 10,000 feet

  • 15,000 feet

  • 20,000 feet

  • 25,000 feet

Explanation

Question 6 of 14

1

Select all that apply.
The approved flap takeoff setting(s) is/are:

Select one or more of the following:

  • 0

  • 10

  • 20

  • 37.5

Explanation

Question 7 of 14

1

Select all that apply.
For normal operations, according to the POH, the approved flap landing setting(s) is/are:

Select one or more of the following:

  • 0

  • 10

  • 20

  • 37.5

Explanation

Question 8 of 14

1

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):

Select one of the following:

  • +3.17g to -1.5g

  • +2.0g to -1.5g

  • +1.5g to -3.17g

  • +1.5g to -2.0g

Explanation

Question 9 of 14

1

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):

Select one of the following:

  • +2.0g to -1.5g

  • +3.17g to -1.5g

  • +1.5g to -3.17g

  • +3.17g to -2.0g

Explanation

Question 10 of 14

1

Select ALL that apply.
The Twin Otter is certified in the Normal Category.
Accordingly, the following are NOT approved:

Select one or more of the following:

  • Spins

  • Lazy eights

  • Chandelles

  • Turns with an angle of bank exceeding 45 degrees

  • Turns with an angle of bank exceeding 60 degrees

  • Stalls

Explanation

Question 11 of 14

1

Fill the blank space to complete the text.

Fill in the blank with no spaces or commas.
Flap extension must not exceed ° during or after flight in icing conditions.

Explanation

Question 12 of 14

1

Select from the dropdown list to complete the text.

Engine intake deflectors must be ( extended, retracted ) during flight in icing conditions.

Explanation

Question 13 of 14

1

Fill the blank spaces to complete the text.

Fill in the blanks with numbers only.

In level flight, the low-level trigger point is pounds usable fuel remaining for the forward tank and pounds usable fuel remaining for the aft tank.

Explanation

Question 14 of 14

1

Fill the blank space to complete the text.

Fill in the blanks with numbers only.

The nose wheel is steerable over a range of degrees to left and right of the centre position for purposes of low-speed ground manoeuvring.

Explanation

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