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This article refers to inflight determination of maximum landing weight in order to remain within the available landing distance (LDA) without compromising the landing safety margins. Check your LDA from Charts / Bulletins / NOTMAS etc. and call it A.
Enter the Field Limit Weight table to find the appropriate limit using corrected field length and pressure altitude. Result: 88100 kg of landing field limit weight. Go to FCOM - Performance Dispatch -- Landing -- Landing Climb Limit Weight.
How to calculate Landing Distance using the Table. Flip to the Landing Distance chart in your POH/AFM. Identify the landing type (i.e. short field) and associated conditions. Identify the field pressure altitude. Identify the temperature at time of landing and locate the column nearest to that temperature.
25 maj 2024 · Key Takeaways. Learn why weight and balance management is so critical – and what you need to do to stay legal. See how an aircraft’s flight characteristics change just by moving the CG a few inches. Learn how to use the computational method to determine the aircraft’s CG and see if it’s within safe limits.
4 kwi 2020 · Find the point at which your drawn line intercepts the vertical graph line representing the actual total weight of your aircraft at the point the performance data would be used (takeoff weight or landing weight).
26 cze 2014 · Introduction. This article introduces the first step in the preliminary sizing process, which is to determine the so-called aircraft design point in terms of wing loading and thrust-to-weight ratio.
The classical equation to calculate gyroscopic stability is as follows. ( Sg) is the gyroscopic stability factor, and must be above 1.0 if the bullet is to remain stable. Sg = 8π ρairt2d5CMαA2 B. The variables are as follows: The first four variables are easy to measure and/or calculate. The last two can be troublesome.
