Performance Flashcards
The Power Assurance Check chart indicates minimum percent torque that must be available for an engine meeting minimum Rolls-Royce specification.
a) True.
b) False.
A) True.
The Power Assurance Check chart indicates maximum percent torque that must be available for an engine meeting minimum Roll-Royce specification.
a) True.
b) False.
B) False.
The Height-Velocity Diagram defines conditions
a) From which a safe landing can be made on a smooth, level, firm surface following an engine failure.
b) From which a safe landing can be made on a rough, sloping, soft surface following an engine failure.
c) In which a safe takeoff profile must be maintained; this is a limitation and must be complied with.
A) From which a safe landing can be made on a smooth, level, firm surface following an engine failure.
For the BH206L4, VH is
a) 130 KIAS; maximum airspeed at the maximum operating ceiling.
b) 60 KIAS; maximum airspeed for hydraulics OFF.
c) 110 KTAS; the airspeed in level flight obtained using the minimum specification engine torque corresponding to maximum continuous power for sea level, 25°C ambient conditions at the relevant maximum certificated weight.
C) 110 KTAS; the airspeed in level flight obtained using the minimum specification engine torque corresponding to maximum continuous power for sea level, 25°C ambient conditions at the relevant maximum certificated weight.
Some performance charts may be found in the Flight Manual Supplement section of the flight manual, depending on installed equipment.
a) True.
b) False.
A) True.
When calculating aircraft performance, it is important to ensure that the correct chart(s) are utilized for the specific equipment/systems installed in the aircraft.
a) True.
b) False.
A) True.
