EXAMPLE OF THE DETERMINATION OF THE FUEL AND THE NUMBER AND The above computations show that with maximum baggage, full FIGURE 16-14-Loading conditions: Determination of the fuel and the number and location of passenger permissible with maximum baggage. FIGURE 16-15-Effects of the addition of equipment items on balance. FIGURE 16-16-Example of moment and weight changes resulting from equipment changes. 1. Leveling means: level top longeron between front and rear seats. 2. Main wheel weighing point is located of datum. "FORWARD) (+ AFT 3. Actual measured distance from the main weight point centerline to the tail (or nose) point centerline_222_". 4. Oil over and above "ZERO" tank reading = (a._—_ Gals.)(b.__—_Lbs.)(c._—_In.) (a) Tail wheel airc. (Item 10a, +7.6) added to (Item 2, + 3) = ± 10.6" = C.G. (b) No se wheel airc. (Item 10b, ) added to (Item 2, COMPUTE IF AIRCRAFT WEIGHED WITH OIL (Item 4) = = C.G. FIGURE 16-17-Sample weight and balance report to determine empty weight center-of-gravity. EQUIPMENT LIST *Required or Optional Item Numbers as Shown in Aircraft Specification NM = ITEM NUMBERS WHEN LISTED IN PERTINENT AIRCRAFT SPECIFICATION MAY BE USED IN LIEU FIGURE 16-18-Sample weight and balance report including an equipment change for aircraft fully loaded. Finding Aids This Code of Federal Regulations volume contains regulations constituting Title 14, Parts 1 to 19, promulgated during 1949-1962 which were in force and effect on December 31, 1962. The following aids used in conjunction with this volume and the daily FEDERAL REGISTER, are designed to assist the user with respect to current regulations, and research concerning regulations which have expired or those which have been superseded or deleted from the Code of Federal Regulations. A subject index to the entire Code of Federal Regulations is published separately and revised annually. |