H3.Flight Performance.pdf-2021

Maximum Landing Mass (MLM) is best defined as: a. Maximum permissible total mass on landing under normal operating conditions. b. Maximum permissible total mass on landing. c. Maximum permissible total mass on the approach to land. d. Maximum permissible total mass on taxiing to park. 2. Helicopter Power Graph shows Rotor Profile Power and Induced Power with letters: (fig. PPL (H) FPP-2) a. “B” and “A” b. “B” and “C” c. “C” and “A” d. “C” and “B” 3. Helicopter Power Graph shows Rotor Profile Power and Parasite Power with letters: (fig. PPL(H) FPP-2) a. “B” and “C” b. “B” and “A” c. “C” and “A” d. “C” and “B” 4. What name is given to the load at which the aircraft structure will fail? a. Ultimate Load. b. Safety Factor Load. c. Limit Load. d. Maximum Load. 5. An aircraft which has been grossly overloaded will: 1. Require increased take-off and landing distances. 2. Have a reduced IGE hover ceiling. 3. Have a reduced maximum level flight speed. 4. Have increased range and endurance. 5. Have a reduced rate of climb and opMaximum Landing Mass (MLM) is best defined as: a. Maximum permissible total mass on landing under normal operating conditions. b. Maximum permissible total mass on landing. c. Maximum permissible total mass on the approach to land. d. Maximum permissible total mass on taxiing to park. 2. Helicopter Power Graph shows Rotor Profile Power and Induced Power with letters: (fig. PPL (H) FPP-2) a. “B” and “A” b. “B” and “C” c. “C” and “A” d. “C” and “B” 3. Helicopter Power Graph shows Rotor Profile Power and Parasite Power with letters: (fig. PPL(H) FPP-2) a. “B” and “C” b. “B” and “A” c. “C” and “A” d. “C” and “B” 4. What name is given to the load at which the aircraft structure will fail? a. Ultimate Load. b. Safety Factor Load. c. Limit Load. d. Maximum Load. 5. An aircraft which has been grossly overloaded will: 1. Require increased take-off and landing distances. 2. Have a reduced IGE hover ceiling. 3. Have a reduced maximum level flight speed. 4. Have increased range and endurance. 5. Have a reduced rate of climb and o