flp2

The required time for final reserve fuel for turbojet aeroplane is:

• 45 min.

• variable with wind velocity.

• 30 min.

• 60 min.

For flight planning purposes the Landing Mass at alternate is taken as:

• Landing Mass at destination plus Alternate Fuel.

• Zero Fuel Mass plus Final Reserve Fuel.

• Zero Fuel Mass plus Final Reserve Fuel and Contingency Fuel.

• Zero Fuel Mass plus Final Reserve Fuel and Alternate Fuel.

You are required to uplift 40 US Gallons of AVGAS with specific gravity of 0.72. How many litres and kilograms is this?

• 109 litres, 151 kg.

• 182 litres, 131 kg.

• 182 litres, 289 kg.

• 151 litres, 109 kg.

A turbo-jet AC is en route to an isolated destination. On top of taxi, trip and contingency fuel, what fuel is required?

• Greater of 45 mins + 15% of trip or 2 hours.

• 2 hours at normal cruise consumption.

• 30 mins holding at 450 m AMSL.

• 30 mins holding at 450 m AAL.

Which of the following statements is relevant for forming route portions in integrated range flight planning?

• The distance from take-off up to the top of climb has to be known.

• A small change of temperature (2°C) can divide a segment.

• No segment shall be more than 30 minutes of flight time.

• Each reporting point requires a new segment.

A turbine-engined aircraft burns fuel at 200 gallons per hour (GPH) with a Fuel Density of 0.8. What is the fuel flow if Fuel Density is 0.75?

• 213 GPH

• 208 GPH

• 200 GPH

• 188 GPH

The final reserve fuel for aeroplanes with turbine engines is:

• fuel to fly for 45 minutes at holding speed at 1 000 ft (300 m) above aerodrome elevation in standard conditions.

• fuel to fly for 60 minutes at holding speed at 1 500 ft (450 m) above aerodrome elevation in standard conditions.

• fuel to fly for 45 minutes at holding speed at 1 500 ft (450 m) above aerodrome elevation in standard conditions.

• fuel to fly for 30 minutes at holding speed at 1 500 ft (450 m) above aerodrome elevation in standard conditions.

An operator shall ensure that calculation of usable fuel for an IFR flight with a turbojet aeroplane for which no destination alternate is required includes, taxi fuel, Trip Fuel, contingency fuel and fuel to fly for:

• 45 minutes plus 10% of the flight time planned to be spent at cruising level or two hours whichever is less.

• 45 minutes at holding speed at 450 m above MSL in standard conditions.

• 2 hours at normal cruise consumption.

• 45 minutes at holding speed at 450 m above aerodrome elevation in standard conditions.

The following fuel consumption figures are given for a jet aeroplane: Standard taxi fuel: 600 kg Average cruise consumption: 10 000 kg/hr Holding fuel consumption at 1.500 ft above alternate airfield elevation: 8 000 kg/hr Flight time from departure to destination: 6 hrs Fuel for diversion to alternate: 10 200 kg Forecast visibility at destination: 2 000 m The minimum ramp fuel load is:

• 77 800 kg

• 77 200 kg

• 74 800 kg

• 79 800 kg

A jet aircraft is due to fly to an isolated aerodrome. The aircraft fuel burn in the cruise is 7 500 kg/hr and 5 000 kg/hr in the hold. What is the absolute minimum additional fuel it should carry?

• 15 000 kg

• 5 625 kg

• 10 000 kg

• 3 750 kg