Getting to fly a jet is one of the most thrilling experiences you can have! However, before jumping in the cockpit, you probably have some questions about how it all works.
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Not to worry—our experienced pilots have all the answers to frequently asked questions about flight control instruments. Before you know it, you'll be dominating the skies!
The "six-pack" of instruments on a plane provides a pilot with the ability to fly using instrument piloting, even with limited visibility. These tools give pilots information on the aircraft’s orientation relative to the horizontal plane (attitude), altitude, vertical speed, airspeed, etc. These include the following:
A plane's altimeter measures the aircraft's height above sea level or how high in the air you are. This instrument gauges absolute pressure corrected for barometric pressure. It uses a static port to measure ambient pressure and plumbs this air into the back case.
Inside an altimeter is a sealed disc called the aneroid, or bellows. The aneroid converts the ambient pressure into
altitude¹ above sea level on the instrument dial.
The radio altimeter was invented in 1924 by Lloyd Espenschied, an American electrical engineer. He developed modern coaxial cables with his partner Herman Andrew Affel.
Modern aircraft use a sensitive altimeter. On a sensitive altimeter, there is a knob that adjusts for local barometric pressure, which has to do with weather conditions. A standard rate of 29.92 is sea level pressure, but barometric pressure can vary by one or two inches.
This impacts your altimeter reading significantly. The Kollman Window on the altimeter dial face is used to adjust for local barometric pressure, which helped to make instrument flight possible.
Jimmy Doolittle² flew the first aircraft solely by reference to instruments in 1929!
Temperature and flight correlate through a lapse rate. The lapse rate is 4.5 degrees Fahrenheit per thousand feet of altitude gained. The higher you fly, the colder it gets.
If the aircraft is intended to operate using visual flight rules (VFR), a pilot should not fly if weather conditions limit visibility. This set of regulations states that visual meteorological conditions (VMC) must allow the pilot to fly the aircraft by seeing where the plane is with visual reference to the ground and other obstructions.
Conversely, instrument meteorological conditions (IMC) mean a pilot can operate an aircraft primarily using instrument flight rules (IFR) and doesn’t need as much visibility to fly.
Calibrated altitude is your altitude after being corrected for nonstandard atmospheric conditions. This is the actual height you fly above sea level if you were to measure it with a very large tape measurer. Mountains, towers, and large structures are measured by calibrated altitude.
Altitude is measured with pressure because we haven't figured out a better way to do it yet. GPS measurements show promise, but barometric altimeter measurements are still the most prevalent. This is because barometric measurements are readily predictable as the density decreases as you gain altitude.
Yes, if you have a high-pressure weather system on a cold day, for instance, you may have altimeter readings that are below sea level. If you are at sea level and your barometric pressure is above 29.92³, your uncorrected altimeter reading will be negative. Death Valley is 200 feet below sea level, and the Dead Sea in Israel is 700 feet below sea level!
In American aviation, when flying above 18,000 feet, everyone sets their altimeter to 29.92. Therefore, everyone's altimeters match. So, if a plane is flying at flight level 31 (31,000 feet pressure altitude with 29.92 set in Kollman Window), the altimeter will match that of any other altimeters on other planes flying above 18,000 feet at the same time. This reduces the possibility of mid-air collisions.
The indicated altitude is your altitude shown on an altimeter. Your true altitude will be your height above mean sea level, or MSL. Absolute altitude is your height above ground level or AGL. Pressure altitude is your indicated altitude when your altimeter is set at 29.92.
Yes and no. It will depend on the type of aircraft. Planes must fly faster to stay in the air because the air is thinner at higher altitudes. Additionally, jets fly more efficiently and quickly at higher altitudes.
Interestingly, the airspeed indicated in an airliner at 35,000 feet may only show 220 knots when in fact, the true aircraft speed is over 450 knots since the air is so thin. Moreover, there are many changes in aviation when you climb above 18,000 feet, where the ambient pressure is half of sea level pressure.
Usually, an electronic flight display will consolidate the information that your old-school six-pack of instruments had into one simple, convenient display. Electronic flight instrument systems (EFIS) have:
A heading indicator, otherwise called a directional gyro, consists of a pressure-driven gyroscope that shows the heading an aircraft is following. There are 360 heading positions that correlate to the direction you are going or compass heading.
For example, if the 12:00 position read 090, you would be heading due east. Or, if it read 270, you would be heading due west. North is 360, and South is 180.
MSL is mean sea level, and AGL is above ground level. For example, if you were flying over Denver at 7,200 feet MSL, you would be 2,000 feet AGL. This is because Denver's altitude is already situated at 5,200 feet above sea level (MSL).
These knobs are there to correct for local barometric pressure on the altimeter. They also set the horizon line on an artificial horizon and correct for gyroscopic precession on the directional gyro. Gyroscopic precession⁴ is minute internal friction that throws off your readings over time.
Cockpit lights are red because this color has the least impact on a pilot's night vision. Red lights are also used on military vessels that operate at night.
These performance instruments use the principles of impact pressure vs static pressure to measure pressures or pressure differences. From these measurements, we derive airspeed, verticle speed, and altitude. The airspeed indicator, altimeter, and verticle speed indicator all run off the Pitot-static system.
Pitot-static tests are required for instrument-certified aircraft. These tests are taken every two years and calibrate the Pitot-static system with sensitive instruments by certified aviation mechanics.
Pitot heat is a heating element that prevents ice from forming on the Pitot tube. This tube measures airspeed. If it ices over, it will read that you are sitting still. You need to remember to turn it on.
¹FLYING Magazine. (9 March 2017). Everything Explained: All About Altitude. Retrieved 15 March 2022.
²History.com. (30 June 2020). James H. Doolittle. A&E Television Networks. Retrieved 15 March 2022.
³Gasmire, C. Why Is 29.92 The Standard Altimeter Setting? Airplane Academy. Retrieved 15 March 2022.
⁴McAdams, T. (29 January 2012). GYROSCOPIC PRECESSION. Aircraft Owners and Pilots Association (AOPA). Retrieved 15 March 2022.
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