21080204
Descripción
Fichas por Rieul Gendron, actualizado hace más de 1 año
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Creado por Rieul Gendron
hace más de 4 años
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| Pregunta | Respuesta |
| 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 |
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