Appendix G Figure G-4. Plot to Determine VMCA for Derate Thrust
3000 Fna - lbs 2900 2800 2700 2600 2500 2400 Maximum Thrust Derated Thrust (5%) 80 KEAS 2686 lbs 50 100 150 200 Ve - kts G.1.9 For a given weight and bank angle, rudder pedal force is determined solely by asymmetric thrust; consequently, takeoff thrust should be limited to a value that results in a pedal force no greater than 150 lbs (180 lbs prior to amendment 25-42).
G-6
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