This shows you the differences between two versions of the page.
| Next revision | Previous revision | ||
|
courses:201a:adm [2018/01/15 20:43] evan created |
courses:201a:adm [2018/04/16 21:35] (current) evan |
||
|---|---|---|---|
| Line 1: | Line 1: | ||
| - | ===== AF 201A Unit 27 Orientation Lesson 9 - Performance/WandB/ADM ===== | + | ====== AF 201A Unit 27 Orientation Lesson 9 - Performance/WandB/ADM ====== |
| Line 10: | Line 10: | ||
| aeronautical decision making. | aeronautical decision making. | ||
| - | * Takeoff and Landing Performance | + | ===== Takeoff and Landing Performance ===== |
| - | * Weight and Balance Computations | + | |
| - | * Effect of Weight and C.G. on Aircraft Performance/Flight Char. | + | ===== Weight and Balance Computations ===== |
| - | * Aeronautical Decision Making | + | |
| - | * Risk Management | + | Weight X Arm = Moment |
| - | * Hazardous Attitudes | + | |
| + | AvGas 6lb/gal | ||
| + | |||
| + | Empty weight of an aircraft (unusable fuel, undrainable oil) | ||
| + | |||
| + | ===== Effect of Weight and C.G. on Aircraft Performance/Flight Char. ===== | ||
| + | |||
| + | * Overloaded aircraft | ||
| + | * The aircraft needs a higher takeoff speed, which results in a longer takeoff run. | ||
| + | * Both the rate and angle of climb are reduced. | ||
| + | * The service ceiling is lowered. | ||
| + | * The cruising speed is reduced. | ||
| + | * The cruising range is shortened. | ||
| + | * Maneuverability is decreased. | ||
| + | * A longer landing roll is required because the landing speed is higher. | ||
| + | * Excessive loads are imposed on the structure, especially the landing gear. | ||
| + | |||
| + | Aft CG | ||
| + | * Higher cruise speed | ||
| + | * Less stability in pitch | ||
| + | * Difficult to recover from stall | ||
| + | * Shorter takeoff roll | ||
| + | |||
| + | Forward CG | ||
| + | * Longer takeoff roll | ||
| + | * Longer landing roll | ||
| + | * Slower cruise speed | ||
| + | * Difficult or impossible to land on main gear (insufficient elevator authority) | ||
| + | |||
| + | ==== Overloaded Aircraft ==== | ||
| + | |||
| + | * Higher takeoff speed | ||
| + | * Longer takeoff run | ||
| + | * Reduced rate and angle of climb | ||
| + | * Lower maximum altitude | ||
| + | * Shorter range | ||
| + | * Reduced cruising speed | ||
| + | * Reduced maneuverability | ||
| + | * Higher stalling speed | ||
| + | * Higher approach and landing speed | ||
| + | * Longer landing roll | ||
| + | * Excessive weight on the nose wheel or tail wheel | ||
| + | |||
| + | ===== Aeronautical Decision Making ===== | ||
| + | |||
| + | ===== Risk Management ===== | ||
| + | |||
| + | [[https://www.aopa.org/news-and-media/all-news/1999/september/flight-training-magazine/hazardous-attitudes|Hazardous Attitudes]] | ||