103 - ATPL - The climb gradient of an aircraft after take-off is 6% in standard atmosphere, no wind, at 0' pressure altitude. Using the following corrections: '± 0.2 % / 1000' field elevation'; '± 0.1 % / °C from standard temperature' '- 1 % with wing anti-ice'; '- 0.5% with engine anti-ice'. The climb gradient after take-off from an airport situated at 1000', 17°C; QNH 1013.25 hPa, with wing and engine anti-ice operating for a functional check is:
Question 103 - Performance - ATPL - Airline Transport Pilot license
4.7 %
4.3 %
4.9 %
3.9 %
Training tests and timed exam simulations ATPL - Airline Transport Pilot license
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