The early model C182 had the same fuselage as the C180 (“straight back”), without the rear window.The main operational differences of the C182 are summarised here:●manual flap lever and the limitation of 100mph (87kts) for all flap selections ●lower maximum all up weight (2550lbs)V...
LIMIT OPERATING LIMIT F L I G H T S I M U L A T I O N U S E O N L Y LIMITATIONS PAGE 2 SECTION: | 1 | 2 | 3 | 4 | 5 | 6 | SUPP | WEIGHT LIMITS NORMAL CATEGORY -Maximum Ramp Weight: 2407 lbs. -Maximum Takeoff Weight: ...
the aircraft electrical system cost and weight can be reduced without the need for a power conditioning unit, the need for which is eliminated by the ability to maintain the speed of the free-turbine generator such that power output is substantially constant. Additionally, the free-turbine generat...