Better approach: Use (common in EASA performance). Let’s verify: Moment_BEM = Index × 10,000 = 1,124,000. Then arm_BEM = Moment / Mass = 1,124,000 / 34,560 ≈ 32.5 m — plausible. Good.
Thus, is consistent.
So DOI = 112.4 + 2.4 = and DOM = 34,560 + 410 = 34,970 kg . easa atpl question bank
Given the options, correct calculation is: Better approach: Use (common in EASA performance)
Therefore, this question uses a . But in the real EASA bank, they predefine that the Dry Operating Index is directly given by loading table or simple addition of mass and index using: 000 = 1