AM.I.C.S12

From the FAA library

• Aircraft Weight and Balance Handbookp. 2-3
  Chapter 2: Weight and Balance Theory › The Law of the Lever

  important; it may be in various locations, but all of the measurements must be made from the same datum location. The procedure for finding the balance point is the same anywhere the datum is located. In Figure ... datum is located at C. Weight A has an arm of –100 inches (negative because it is to the left) of the datum and weight B has an arm of –60 inches from the datum. The table in Figure…

• Aircraft Weight and Balance Handbookp. 3-7
  Chapter 3: Weighing the Aircraft and Determining the Empty Weight Center of Gravity › Location of Datum › Datum Forward of the Main Wheels—Tailwheel Landing Gear

  inches forward of the main wheels, exactly the same location as when it was measured from other datum locations. Figure 3-11. Determining the CG with datum aft of the main wheels of an airplane with nosewheel landing gear. Location ... Datum The location of the datum is not important, but all measurements must be made from the same location. Datum Forward of the Main Wheels—Tailwheel Landing Gear Locating the CG of a tailwheel airplane is done in the same…

• Aviation Maintenance Technician Handbook - Generalp. 6-32
  Chapter 6: Aircraft Weight & Balance › Weight & Balance for Large Airplanes › Weight & Balance Records

  Serial # Datum Location Leveling Means Scale Arms: Nose Tail Scale Weights: Nose Tail Tare Weights: Nose Tail Model N# Left Main Right Main Left Main Right Main Left Main Right Main Aircraft Current Empty Weight: Aircraft Current Empty Weight ... Aircraft Maximum Weight: Aircraft Useful Load: Computed By: Certificate #: Date: Figure 6-55. Aircraft weight and balance report. (print name) (signature) (A&P, Repair Station, etc.) item names must be changed to reflect the weight locations. If an equipment change…