What is the takeoff distance at 705 kg takeoff mass? OAT 20°C QNH 1013 HPA at an elevation of 3500 feet with 5 kt

Given the following information what range can be achieved: outside air temperature 20°C pressure altitude MSL power 55%

What is the true airspeed TASKT and feel consumption for a cruise flight with 60% power in flight level 60 under the following conditions temperature ISA -20 Celsius degrees QNH980 HPA

What is the required fuel to climb from flight level 65 to flight level 95 under the following conditions: aircraft mess 3000 pounds OAT in flight level 65:-5°C, OAT in flight level 95:-15°C

Calculated takeoff mass 746 kg calculated CG equals 0.371 fuel burn 30 1/2 L on station 0.45 m where is the CG situated after the lending?

A pilot want to takeoff on runway 36. The reported wind is 240° 12 kt what is the value of the wind component acting on the aircraft on takeoff and landing?

Giving the following conditions, the TAS equals outside air temperature 10°C pressure altitude 6000 feet power 65%

Which maximum rate of climb can the aircraft reach at 9000 feet pressure altitude and OAT 12°C

What is the true airspeed in fuel consumption for co-flight with 70% power in flight level 60 under the following conditions temperature ISA -20 degrees Celsius QNH980 HPA

What is the fuel flow in the true airspeed for cruise flight with 70% power in flight level 75 at an OAT of 0°C?

What is the required distance to climb to flight level 75 after a departure for an airfield which is located at the pressure altitude of 3000 feet with an initial mass of 3000 pounds 0AT at airfield 25°C OAT in flight level 75 0°C

Deposition of the center of gravity equals see (PFP052E)

The position of the center of gravity, including fuel equal see figure (PFP053E)

A pilot wants to takeoff on runway 36. The reported wind is 240 degrees 12 kt what are the wind components acting on the aircraft on the takeoff and landing?

Given the following conditions, the TAS equals outside air temperature -2°C pressure altitude 8000 feet power 75% see annex PFP014

Which is the maximum rate of climb for the aircraft at 6500 feet pressure altitude, and and OAT 0°C

What is the maximum rate of climb considering the following conditions outside air temperature 20°C pressure altitude 4000 feet aircraft mass 530 KG see annex PFP010

At which airspeed do you climb to flight level 75 after a departure form an airfield which is located at the pressure altitude of 3000 feet with an initial mass oh 3000 pounds OAT at airfield 25°C OAT in flight level 75 0°C see annex PFP023

Considering The following field data how much tree fuel is needed fuel for startup and taxi 5 L fuel for takeoff and climb 12 L fuel for cruise 25 L fuel for descent in approach and lending 7 L fuel for taxi in parking 3 L fuel to return to alternate 13 L final reserve fuel 10 L

Calculated takeoff mass 2300 pounds calculated CG 95.75 inches fuel burn 170 pounds on station 87.00 inches where is the CG situated after the lending

Given the following conditions, the takeoff distance equals outside air temperature -20°C pressure altitude 5000 feet airplane mass 750 KG headwind 10 see annex PFP009

The takeoff distance at 750 KG takeoff mass standard ISA condition at elevation of 4000 feet with 5KT tailwind see annex PFP009

Which maximum rate of climb can the Elkridge it 2200 feet pressure altitude and OAT 15°C see annex (PFP-011)

What is the maximum rate of climb considering the following conditions outside air temperature OAT -15°C pressure altitude 11,000 feet aircraft mass 500 KG see annex (PFP010)

What is the required distance to climb from flight level 65 to flight level 95 under the following conditions aircraft mass 3000 LB OAT in flight level 65 -5°C OAT in flight level 95: -15 c See annex PFP023

What is the meaning of the “Z” in METER

Calculated takeoff mass equal 1082 KG calculated CG equals 0.254 m fuel burn 55 L on station 0.40 m. Where is the CG situated after the landing?

For a takeoff from runway 22 in the reported wind of 250° 10 KT, the longitude wind component equals

What range can be achieved at the following conditions outside air temperature 6°C pressure altitude 6000 feet power 65% see annex (PFP013)

What is the range (nm) for cruise flight with 60% power in flight level 65 at an OAT of -15°C see annex (PFP013)

How much taxi fuel must be consumed before takeoff to reduce the aircraft mass to the maximum takeoff mass maximum ramp mess (MRM) 1150 KG actual ramp mess 1148 KG maximum takeoff mass (MTOM) 1145 KG

What is the range for a cruise flight with 70% power in flight level 75 at OAT of -20

What is the fuel flow and the true airspeed for cruise flight with 60% power in flight level 85 at an OAT -25

Given the following condition the fuel consumption equals pressure altitude 2000 ft temperature 31 RPM 2400