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) (+ 3" 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) Nose wheel airc. (Item 10b, C.G. added to (Item 2, ) = 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 FIGURE 16-18-Sample weight and balance report including an equipment change for aircraft fully loaded. FINDING AIDS In addition to the following finding aids a subject index to the entire Code of Federal Regulations is published separately and revised annually. List of Current CFR Volumes List of Superseded CFR Volumes Table of CFR Titles and Chapters Alphabetical List of CFR Subtitles and Chapters |
