![]() |
Created by Rieul Gendron
over 4 years ago
|
|
Question | Answer |
Maximum fuel temperature and maximum ambient temperature for takeoff when using AVGAS | +25 degrees Celsius |
Maximum operating altitude when using AVGAS? | 15,000 feet |
Number of boost pump per tank that must be serviceable at all times when AVGAS is being used | ALL OF THEM |
Maximum operating altitude of the DHC-6-300 according to the POH? | 25,000 feet |
Approved flap takeoff setting(s) | 10 degrees only |
For normal operations, according to the POH, the approved flap landing setting(s) | 20 degrees and 37.5 degrees |
At a gross weight of 12,500 lbs and flaps RETRACTED, the flight load factors to which the DHC-6 airplane has been designed (normal category) | +3.17g to -1.5g |
At a gross weight of 12,500 lbs and flaps EXTENDED, the flight load factors to which the DHC-6 airplane has been designed (normal category | +2.0g to -1.5g |
The Twin Otter is certified in the Normal Category. Accordingly, which manoeuvres are NOT approved according to POH 2.12.1 | - Spins - Lazy eights - Chandelles - Turns with an angle of bank exceeding 60 degrees |
Maximum flap extension during or after flight in icing conditions | 10 degrees |
What position should the engine intake deflectors be set to during flight in icing conditions? Extended or retracted? | Extended |
In level flight, what is the low-level trigger point in pounds for usable fuel remaining for the FORWARD tank? | 75 lbs |
In level flight, what is the low-level trigger point in pounds for usable fuel remaining for the AFT tank? | 110 lbs |
The nose wheel is steerable over what range (in degrees) left and right of the centre position for purposes of low-speed ground manoeuvring? | 60 degrees to the left and right of the centre position |
Want to create your own Flashcards for free with GoConqr? Learn more.