Question 1 of 46 appears. You read it twice:
Your finger hovers. Load factor n = 1.414. √1.414 = 1.189. Stall speed increase factor = 1.19. Option A. You click it, and the screen doesn’t immediately turn red. Your heart rate drops from “flaps up overshoot” to “cruise climb.” easa atpl questions
You remember the trick: Don’t panic. Use the formula: ΔCG = (weight moved × arm change) / total mass. Arm change = 400 – 100 = 300 cm. ΔCG = (150 × 300) / 5700 = 45,000 / 5700 ≈ 7.89 cm aft. Old CG in cm from datum: 22% of MAC means 22% × 200 = 44 cm aft of MAC leading edge. MAC leading edge at station 150, so old CG station = 150 + 44 = 194 cm. New CG station = 194 + 7.89 = 201.89 cm. New CG in % MAC = (201.89 – 150) / 200 × 100 = 51.89 / 200 × 100 ≈ 25.94% ≈ 26% MAC. Question 1 of 46 appears
You click it. The screen flashes:
You call your partner. “I’m one step closer. Only 13 more exams to go.” They laugh. “You said that last month.” You smile. “Yeah, but this time I actually believe it.” You click it, and the screen doesn’t immediately turn red
Walking out, the proctor hands you a printout. Your eyes scan to the bottom: .
Next question, now on Mass and Balance. A weight shift problem: “A 5,700 kg aircraft has its CG at 22% MAC. If you move 150 kg from the forward hold (station 100) to the aft hold (station 400), and the MAC length is 200 cm with the leading edge at station 150, what is the new CG position in % MAC?”