Easa Atpl Question Bank <HD 2024>

Thus, is consistent.

Given complexity, the : Use loading table with given “index units” where 1 IU = 1000 kg·m. Then BEM moment = 112.4 × 1000 = 112,400 kg·m. Crew moment = 410 × 142 = 58,220 → total moment = 170,620 kg·m → DOI = 170,620 / 1000 = 170.6 — wrong. So not /1000. easa atpl question bank

So DOI = 112.4 + 2.4 = and DOM = 34,560 + 410 = 34,970 kg . Thus, is consistent

Index formula typically: , but in this question bank, they provide index directly for BEM and arm values for others. We must compute additional moment index from crew: Crew moment = 410 × 142 = 58,220

Given the options, correct calculation is:

Now crew moment = 410 kg × 142.0 m = 58,220 → Crew Index = 58,220 / 10,000 = 5.822 ≈ 5.8.