Larger aircraft have landing weights much less than takeoff weights since they are designed to burn hundreds (or thousands) of pounds of fuel during flight. This is not always published, or it may be published as equal to takeoff weight. Maximum landing weight - Maximum weight you can land with. Maximum takeoff weight - Maximum weight you can take off with. This will be a few pounds heavier than maximum takeoff weight because it assumes you will burn some for taxi and run-up. Maximum ramp weight - Total loaded aircraft weight only published for some airplanes. Licensed empty weight - An older term than “standard empty weight,” which does not include engine oil Standard empty weight - The weight of the airframe, engines, and permanently installed fixtures and fluids (including unusable fuel and full engine oil)īasic empty weight - Standard empty weight plus any accessories your airplane might have added Should the airplane begin pitching up and slowing, as in a stall scenario, it may be impossible for the pilot to lower the nose, reduce the angle of attack, and recover.Ī rearward out-of-limits CG is associated with unrecoverable stalls and spins.Ĭheck out these 7 private pilot books to help you become a better pilot! Weight and Balance Terms The aircraft will have a noticeably higher cruise speed, but the aircraft will be much less stable. This typically is the most dangerous situation. If the CG is located too far aft, the airplane will have a nose-up tendency. The nose-down tendency will increase the airplane’s stall speed and make cruise flight much slower. If the loading is severe enough, the elevator travel may not produce enough force to allow the airplane to flare or rotate. Either situation will make the airplane dangerous and potentially unstable.Ī CG located forward of the forward limit will cause the airplane to have a nose-down tendency. The CG cannot be too far forward nor too far back. Once you have this, you can compare it to the charts or tables the manufacturer gives you to ensure that it is within acceptable limits. More load put on the structure of the aircraft then it was designed forįinding whether or not your airplane is in balance is all about finding the loaded airplane Center of Gravity or CG. ![]()
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