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ID 4235
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Use Flight Planning Manual MRJT 1 Figure 4.5.2 and 4.5.3.1
Given: Distance C - D: 3200 NM
Long Range Cruise at FL 340
Temperature Deviation from ISA: +12°C
Tailwind component: 50 kt
Gross mass at C: 55 000 kg
The fuel required from C - D is:
A
17 500 kg
B
14 200 kg
C
17 800 kg
D
14 500 kg
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