Id 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:

×

New: Boost Your Preparation!

On our site, you'll now find our new PRO Simulation Panel! Here are some of the exclusive benefits you get by unlocking it:

• ✅ All official questions, none excluded
• 🧠 Explanations and predictions with Artificial Intelligence
• ♾️ No time or exam limits
• 🚫 Zero ads

💻 Discover the PRO Panel

---

You can still continue with the free version, which gives you access to 75% of the questions with a limit of 3 simulations every 2 hours.