agree with those specified in a theoretical consideration of the problem. This article describes a method used to analyse climb data whereby climb performance of an aircraft may be established for specified conditions, speed for best rate of climb determined and comparison made with theoretical ...
VYBest rate-of-climb speed74 KIASNot marked VFEMax flaps extended speedup to 10°: 110 KIASWhite arc ends at 85 KIAS more than 10°: 85 KIAS VCTypical cruising speed90 - 120 KIASNot marked VAManeuvering speed; Abrupt movement105 KIASNot marked ...
Max Rate of Climb 900 ft/min Max Rate of Climb Gross 650 ft/min Range 960 miles Hours Endurance 8 Hours Best Glide Ratio 15:1 Sevice Ceiling 15,000 Ft Fuel Consumption 2.1-3.0 gph POWERPLANT (HKS 700E) Max Power (6,200 rpm-5m) 60HP ...
Aircraft Performance Program Introduction
Rate of climb (MSL) 3.3 m/s 651 ft/min 4.0 m/s 780 ft/min Max. range (FL160, 50% PWR) incl. climb, no reserves 1,730 km 934 nm – – Max. range (10,000 ft, 55% PWR, best eco) no climb, no reserves – – 1,569 km 847 nm Fuel consumption 19.3 l/h (@60%) 5.1 ...
Too large and the rate-of-climb suffer. It may prevent the aircraft from maintaining altitude. As a rule of thumb, to achieve the maximum rate-of-climb in the OEI configuration (VYSE) a bank angle of 2° is recommended if the noncritical engine fails, and 3° if the critical engine ...
The difference that needs to be taken into account mainly concerns their performances: speed and rate of climb. – Small UAS: they will fly very low level (VLL), so it is not necessary to provide air traffic control (ATC) to those UAS. However, there is a need for airspace ...
The thrust is equal to the helicopter weight plus the air resistance of the fuselage or other parts of the craft to the vertical motion, with the oncoming stream speed V equal to the rate of climb of the helicopter. Slow, Powered Descending Flight In this case, the air approaches the ...
Move the thrust levers to the climb detent to activate it. The state of the auto thrust system is displayed in the top right corner of the primary flight display (PFD). When the text A/THR is in white color then the auto thrust is active. When the text is in cyan/blue the auto th...