By United States. Flight Standards Service. Airman Testing Standards Branch

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Steering lines are divided into two sections; a single heavy line is attached to the steering bars. Wings and Components The powered parachute wing is unique, as compared to a fabric wing on an airplane, in that when it is not inflated it loses its ability to produce lift. When a powered parachute wing is inflated or pressurized, it becomes semi-rigid and is capable of producing lift and supporting a load. Rather than being bolted to the fuselage like an airplane, the parachute wing is attached to the cart by lines and cables which are known as risers.

Though the flightpath has changed when the climb has been established, the angle of attack of the wing with respect to the inclined flightpath reverts to practically the same value, as does the lift. The angle of attack remains relatively constant for constant weights during stabilized flight for glide, level cruise or climb. However, wind gusts, flying in turbulence, quick uncoordinated flight (as covered later), or aerobatic maneuvers can change the PPC angle of attack. PPC limitations in the POH are specifically written to avoid any maneuver that would temporarily get the PPC into a situation of too high or too low an angle of attack.

Although the EIS is a valuable tool, the ability to interpret the information is equally important. For the interperetation of any engine and flight instrument, you need to completely understand the engine limitations, parameters, and the messages the instrument provides you. Sensing the proper operation of the aircraft and engine is a key factor to the safe operation of any aircraft. Being able to interpret engine sounds and unusual vibrations is essential for any pilot. As with any aircraft or instrument operation, see the POH for each individual make and model operating instructions.

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