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(For this question use annex 033-012 rev. 05.11.2004 or Flight Planning Manual MRJT 1 Figure 4.5.1).
Given:

Brake release mass 57500 kg,
Temperature ISA -10° C,
Average headwind component 16 kt,
Initial FL280

Find: Climb fuel for enroute climb 280/.74

  • A
    1138 kg
  • B
    1238 kg
  • C
    1040 kg
  • D
    1387 kg
In the schedule attached:
Interpolate between airplane mass 56000 kg and 58000 kg to find the fuel consumption for airplane mass 57500 kg: 1138 kg

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