Avia 305 - Study guides, Class notes & Summaries

AVIA 305 Quiz: Maneuvering Performance Score for this quiz: 72.5 out of 75 Fall 2023 Score for this quiz: 72.5 out of 75 During a right crosswind landing in a tricycle gear airplane, a coordinated touchdown on the wheel first will mitigate side loading and prevent ground looping the aircraft. right left nosewheel tailwheel During a setup to a power-on stall in a single-engine propeller airplane, as IAS decreases additional input will be required to maintain coordinated flight. ri...

AVIA 305 Quiz: Maneuvering Performance Score for this quiz: 72.5 out of 75 Fall 2023 Score for this quiz: 72.5 out of 75 During a right crosswind landing in a tricycle gear airplane, a coordinated touchdown on the wheel first will mitigate side loading and prevent ground looping the aircraft. right left nosewheel tailwheel During a setup to a power-on stall in a single-engine propeller airplane, as IAS decreases additional input will be required to maintain coordinated flight. ri...

AVIA 305 Quiz: Maneuvering Performance Score for this quiz: 72.5 out of 75 Fall 2023 Score for this quiz: 72.5 out of 75 During a right crosswind landing in a tricycle gear airplane, a coordinated touchdown on the wheel first will mitigate side loading and prevent ground looping the aircraft. right left nosewheel tailwheel During a setup to a power-on stall in a single-engine propeller airplane, as IAS decreases additional input will be required to maintain coordinated flight. ri...

AVIA 305 Quiz: Maneuvering Performance Score for this quiz: 72.5 out of 75 Fall 2023 Score for this quiz: 72.5 out of 75 During a right crosswind landing in a tricycle gear airplane, a coordinated touchdown on the wheel first will mitigate side loading and prevent ground looping the aircraft. right left nosewheel tailwheel During a setup to a power-on stall in a single-engine propeller airplane, as IAS decreases additional input will be required to maintain coordinated flight. ri...

The equation Ta = Q (V2 - V1) shows thatyou can get more thrust from a jet engine by using water injection. you can get more thrust from a jet engine by decreasing the exhaust pipe area. Q in Ta = Q (V2 - V1) is the mass flow (slugs/sec). The mass flow depends onthe cross‐ sectional area of the turbojet engine inlet. the engine inlet velocity. the density of the air at the same point.

AVIA 305 Test 3 Prep Study Guide Exam. CHAPTER 12 - CORRECT ANSWER Slow‐Speed Flight The main difference between the Cl - a curves for straight‐wing aircraft is that - CORRECT ANSWER the swept‐wing aircraft has a lower value of CL(max). the straight‐wing aircraft does not fly at as high an AOA for CL(max) the swept‐wing aircraft does not have an abrupt loss of lift at CL(max) Low‐speed stall will start at the wing's trailing edge - CORRECT ANSWER Where C1/CL is a ma...

Dynamic hydroplaning Is a condition where the tire is lifted completely above the surface of the runway. Can occur at slower speeds and rather than the water lifting the tire from the pavement, the tire slips on a thin film. Is where the water turns to steam and steam pressure lifts the tire from the runway. None of the above Question 2 2.5 / 2.5 pts Directional control during a crosswind takeoff in a C172 should be maintained with coordinated use of ailerons and the rudder. True Fa...

LU AVIA 305 Test 3 • Question 1 2.5 out of 2.5 points Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift - Angle of Attack (AOA) curves. For a safe takeoff, the Critical Field Length must be no greater than the runway available An increase in density altitude has what effect on takeoff performance