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Classic Theory Meets Digital Computer; Status Quo Emerges Unscathed

Flying Magazine

For instance, in the range of cruising power settings the specific fuel consumption of my Continental TSIO-360the rate of fuel flow required to generate one horsepowerimproves by about 1 percent with each increase in speed of three knots. Again, these are indicated airspeeds. mpg drops to 10.5.

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Delta CRJ-900 Accident In Toronto: Preliminary Report Published

One Mile at a Time

At the time of the accident, winds were at an angle of 270 degrees (the runway was at an angle of 230 degrees), at 28 knots, gusting to 35 knots. degrees Less than one second before touchdown, the plane had an indicated airspeed of 134 knots, a ground speed of 111 knots, a bank angle of 7.1

Descent 101
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Airspeed and Altitude Control Simplified: Tips for Stable Flying

Pilot Institute

If you’re aiming to get comfortable with managing both airspeed and altitude in flight, you’ll need to understand the difference between indicated airspeed (IAS) and true airspeed (TAS). Key Takeaways Airspeed and altitude are directly linked to each other throughout different phases of your flight. miles per hour.

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Mach Number Explained: What It Is and Why Pilots Use It

Pilot Institute

Why don’t they use Indicated Airspeed just like the pilots who fly slower aircraft? Key Takeaways Mach number is a dimensionless ratio of true airspeed to local speed of sound. In terms of a formula, you can write it as: Mach number (M)= True Airspeed (TAS) / Speed of Sound (a) This means Mach 1 is the speed of sound, Mach 0.5

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E6B Made Easy: A Beginner’s Step-by-Step Guide

Pilot Institute

Step-by-Step: How to Use the E6B for Time and Speed Calculations Calculating Time en Route Lets say were flying at a constant airspeed of 100 knots. That means itll take 24 minutes to fly 40 miles at 100 knots. That means our groundspeed was 90 knots. Calibrated airspeed is not the same as indicated airspeed.

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Go-Around Required

Plane and Pilot

After a shallow turn from downwind, the Bonanza was positioned on base at a proper altitude and airspeed and with a constant descent rate. The wind at the surface was reported as 220 degrees at 6 knots gusting 19 knots. Increasing true airspeed makes the turn radius wider, resulting in an overshoot.

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Trial by Ice

Air Facts

This particular 172 normally cruised at 120 mph indicated airspeed, but with the ice it would barely do 90 mph and that required full throttle! The general prognosis indicated no icing in the clouds, no turbulence and a quartering headwind from the west resulting in a mere five knots of headwind component.

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