21078246
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 |
| Minimum control speed (VMC) flaps 10 | 64 KIAS |
| Best angle of climb speed (VX), flaps 0 | 87 KIAS |
| Best rate of climb speed (VY), flaps 0 | 100 KIAS |
| Best single-engine rate of climb speed (VYSE), flaps 10 | 80 KIAS |
| Maximum flaps extended speed (VFE) for flaps 10 | 103 KIAS |
| Maximum flaps extended speed (VFE) for GREATER THAN flaps 10 | 93 KIAS |
| Maximum operating speed (VMO) for the following altitudes: Sea level to 6,700 feet | 166 KIAS |
| Maximum operating speed (VMO) for the following altitudes: 6,701 feet to 10,000 feet | 156 KIAS |
| Maximum operating speed (VMO) for the following altitudes: 10,001 feet to 15,000 feet | 141 KIAS |
| Maneuvring speed (VA) between sea level and 18,000 feet | 132 KIAS |
| Gust penetration speed (VB) between sea level and 18,000 feet | 132 KIAS |
| Maximum takeoff weight | 12,500 lbs |
| Maximum landing weight | 12,300 lbs |
| Maximum permissible baggage compartment load for the FORWARD baggage compartment | 300 lbs |
| Maximum permissible baggage compartment load for the (entire) AFT baggage compartment | 500 lbs |
| Maximum weight on the EXTENSION SHELF in the aft baggage compartment | 150 lbs |
| TRUE or FALSE? The maximum permissible baggage compartment load for the lower portion of the aft baggage compartment (i.e., the area NOT on the shelf) is 350 lbs. | FALSE. See POH 2.8.3 The total limit for the aft baggage compartment is 500 lbs. The shelf limit is 150 lbs. However, there is no limit for the lower portion of the aft baggage compartment, so you could have, for example, 400 lbs on the lower portion and 0 pounds on the shelf. |
| Maximum permissible floor loading value for the forward and rear baggage compartments | 100 lbs per square foot |
| Maximum permissible floor loading value for the cabin | 200 lbs per square foot |
| At the maximum permitted weight during the phase of flight described, what is the airspeed? VYSE Engine Failure after Take-off, Flaps at 10 degrees | 80 KIAS |
| At the maximum permitted weight during the phase of flight described, what is the airspeed? VSO Stall speed, landing configuration (Flaps 37.5 degrees) | 56 KIAS |
| At the maximum permitted weight during the phase of flight described, what is the airspeed? VS1 Stall speed, take-off configuration (Flaps 10 degrees) | 66 KIAS |
| At the maximum permitted weight during the phase of flight described, what is the airspeed? VS Stall speed, flaps up | 73 KIAS |
| Glide Speed (both propellers feathered) for best RANGE | 100 KIAS |
| Glide Speed (both propellers feathered) for best ENDURANCE | 77 KIAS |
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