Weight & Balance Cessna 182L N42565 S/N 18259080  Removed the following equipment: 1. Turn coordinator P/N C661003-0201 2. Directional gyro P/N 0706000 Installed the following equipment: 1. S-TEC System 40 autopilot, includes turn coordinator and directional gyro *REVISED LICENSED EMPTY WEIGHT NEW USEFUL LOAD 1,216.62 Forward check (Limit +33.0) Wt. × Arm =  Moment A/C empty  Fwd. seats Aft seats Fuel (min.) Baggage A Baggage B Jeseph P. Kline A&P 123456789 Supersedes computations of FAA Form 337 dated 10/02/07. Weight x Arm = Moment 2.50 lb  15.0  37.50 +3.12 lb  13.5  +42.12 5.62  79.62 1,876.00  36.14  67,798.64 −5.62  −79.62 1,870.38  36.20  67,719.02  Weight x Arm = Moment 13 lb  32.70  425.13 1,870.38  36.20  67,719.02 +13.00  + 425.13 1,883.38  36.18  68,144.15  Rearward check (Limit +46.0) A/C empty  Fwd. seats Aft seats Fuel (min.) Baggage A Baggage B 1,883.38  36.18  68,144.15 170.00  37.00  6,290.00 115.00  48.00  5,520.00 2,168.38  +36.87  79,954.15 Total Aircraft after removal: Wt. × Arm = Moment  1,883.38  36.18  68,144.15 170.00  37.00  6,290.00 340.00  74.00  25,160.00 528.00  48.20  25,449.60 100.00  97.00  9,700.00 60.00  116.00  6,960.00 3,081.38 45.98 141,703.75 Date: 08/07/09 Figure 7-3.  A typical airplane weight and balance revision record. 7-4