The required time for final reserve fuel for turbojet aeroplane is:4
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Refer to CAP697 Section 4 - MRJT1 Page 13 Figure 4.3.3C Simplified Flight Planning - Trip Distances Given: ground distance to destination aerodrome 1600 NM headwind component 50 KTFL 330cruise 0.78 MachISA +20 ° Cestimated landing weight 55000 kg.Find: simplified flight planning to determine estimated trip fuel and trip time.4
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Refer to CAP697 Section 4 - MRJT1 Page 17 Figure 4.4 Holding Fuel Flow - Flaps RetractedThe final reserve fuel taken from the HOLDING PLANNING table for the twin jet aeroplane is based on the following parameters:4
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Find the time to the Point of Safe Return (PSR).Given: Maximum useable fuel 15000 kg, Minimum reserve fuel 3500 kg, TAS out 425 kt, Head wind component out 30 kt, TAS return 430 kt, Tailwind component return 20 kt, Average fuel flow 2150 kg/h4
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Refer to CAP697 Section 4 - MRJT1 Page 2 Figure 4.1 / 4.2 and Page 41 Figure 4.5.3.2Given: Estimated take-off mass 57000 kg, Ground distance 150 NM, Temperature ISA -10°C, Cruise at 0.74 MachFind: Cruise altitude and expected true air speed4
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Refer to CAP697 Section 4 - MRJT1 Page 75 Figure 4.7.2 Area of Operation - Diversion Distance One Engine InoperativeUsing the above table, in ISA conditions and at a speed of M.70/280KIAS, in an elapsed time of 90 minutes an aircraft with mass at point of diversion 48000 kg could divert a distance of:4
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Given:Distance from departure to destination 140 NM GS Out 90 ktGS Home 80 kt What is the distance of the PET from the departure point?4
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Given:Distance from departure to destination 2800 NM True track 140W/V 140/100TAS 500 kt What is the distance and time of the PET from the departure point?4
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Given:Distance from departure to destination 340 NM True track 320W/V 160/40 TAS 110 ktWhat is the distance of the PET from the departure point?4
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Given:Distance from departure to destination: 400 NM Endurance: 2,5 hTAS: 115 ktGround Speed Out: 130 kt Ground Speed Home: 105 ktWhat is the distance of the PSR from the departure point?4
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