To fly the aircraft, Lift must be higher than (Weight + Tail down force). The more forward the CG, the higher the tail down force. The higher the tail down force, the higher the lift necessary to …

2013年1月15日 · CG - center of gravity. Why would it be changed when changing the ZFW? In real life, as far as I know, pilots get sheets where CG is written according to cargo, …

I have read a320's optimum CG position is 25% MAC. But, the aerodynamic center is also at 25% of chord. So since CG and aerodynamic center at the same position, there would be no …

The aft CG limit of the aircraft for takeoff and landing must be restricted according to the aft CG limit shown in the CG envelopes below. Note: The CG envelopes shown below correspond to …

2019年5月5日 · Tech Log - A320 CG - Just want someone to check if I have understood it correctly. According to FCOM, if we are using the RTOW charts based on CG being at 25% …

If TO CG < 27 % then decrease flex temperature by 2oC and increase V1, VR and V2 by 1 kt. This will give you the final flex temperature and associated speeds. Download the Excel …

2007年8月22日 · A CG of 25 % is a FORWARD CG, which is called nose heavy. If you support the aircraft at its' CG, it will be in balance. If the balance point is forward, the nose must be …

2024年5月16日 · 2019年8月29日A320飞机航前出港进入跑道后机组反馈按压起飞构型测试不通过，ECAM有信息F/CTL PITCH TRIM/MCDU/CG DISAGREE。 协调机组重新输入无燃油重量 …

2009年1月19日 · Anybody knows which method is used to calculate the take-off CG. Is it an extrapolation from the ZFW CG entered in the MCDU or a result from measurements via …

For a smaller aircraft as the A320neo, most operators would favor an AFT CG loading for fuel consumption benefits when considering the lifetime of the fleet and how easy the benefits can …