A modified Cessna 310 has a stall speed of (80 mph), a cruise speed of (200 mph), and a dive speed of (215 mph) when it is flying near Denver (air density = 0.002 lb-sec2/ft4). FAA spec load factors includes a maximum positive load factor of 4.00 and a minimum negative load factor of -1.5. The aircraft is undergoing a push-down maneuver at (200 mph), calculate the wing lift load at the top of the maneuver (i.e. aircraft is horizontal). Assume a flight path radius of ( 1,203 ft) and a CG offset of delta =6 inches.

Answer rating: 100% (QA)

According to the information provided the aircraft is a modified Cessna 310 with specific speeds and ... View the full answer