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Basic Six Aircraft Instruments

Updated: Sep 18

Basic Six Aircraft Instruments

*Airspeed Indicator (ASI) *Altimeter

*Vertical Speed Indicator (VSI) *Attitude Indicator (AI) *Heading Indicator (HI) *Turn Coordinator (TC)

The instruments in the six pack are powered by various aircraft systems. The ASI, altimeter, and VSI use the pitot-static system, which provides ram air pressure from the pitot tube and ambient pressure from the static port. Only the ASI uses the pitot tube; all three instruments use the static port. The AI, HI, and turn indicator are gyroscopic instruments that contain an internal gyro powered by vacuum, pressure, or electrical power


Flight Instruments ✔️✏️📘Flight instruments are the instruments in the cockpit of an aircraft that provide the pilot with information about the flight situation of that aircraft, such as altitude, airspeed, vertical speed, heading and much more other crucial information. ✔️✏️📘These instruments are vital to the operation of the aircraft, helping the pilot maintain and control the aircraft. ✔️✏️📘Flight instruments are divided into two categories: static (or pitot-static) instruments and gyroscopic instruments. ✔️✏️📘There are 6 basic Flight Instruments in the cockpit which are ➖👉Altimeter :- The altimeter uses barometric pressure obtained from the static port to display the aircraft’s approximate altitude or height above mean sea level (MSL) in feet. ➖👉Airspeed Indicator :- It uses the pressure differential in the pitot-static system to measure and display the aircraft’s speed. In most aircraft the ASI displays speed in knots or miles per hour. ➖👉Vertical Speed Indicator :- It uses internal pressure differential to provide a visual indication of how fast the aircraft is climbing or descending. ➖👉Attitude Indicator :- It uses a rigidly-mounted internal gyro to display the aircraft’s attitude relative to the horizon. ➖👉Heading Indicator :- It uses a rotating gyro to display the current compass nose direction that the aircraft is flying ➖👉Turn Coordinator :- It uses a canted internal gyro to display both initial roll rate and stabilized rate of turn.


1) Airspeed Indicator


The ASI uses the pressure differential in the pitot-static system to measure and display the aircraft’s speed. In most aircraft the ASI displays speed in knots or miles per hour. A needle points to the aircraft’s current indicated air speed (IAS). Standard color-coded markings provide various critical speed information for that model of aircraft, including stall, flap setting, normal operating, caution, and never exceed speeds. The table below shows what the colors on an airspeed indicator mean.

2) Attitude Indicator (AI)


Also known as the artificial horizon, the AI uses a rigidly-mounted internal gyro to display the aircraft’s attitude relative to the horizon. The display consists of a miniature aircraft aligned to the horizon in straight-and-level flight, with a blue sky above and brown or black ground below.

A vertical scale crossing the horizon shows degrees of pitch up or down. A curved scale across the top shows degrees of bank left or right. When the aircraft changes pitch or direction, the aircraft essentially rotates around the AI’s gyro, and the instrument display responds accordingly.

3) Altimeter


The altimeter uses barometric pressure obtained from the static port to display the aircraft’s approximate altitude or height above mean sea level (MSL) in feet. Three pointers provide the altitude information in 100, 1,000 and 10,000 foot increments.

Because barometric pressure changes with altitude and atmospheric conditions, most altimeters contain an adjustment knob to dial in the local barometric pressure (also known as the altimeter baro setting).

4) Turn Coordinator (TC)


The TC uses a canted internal gyro to display both initial roll rate and stabilized rate of turn. An aircraft silhouette mimics the aircraft to show the direction of turn, and will align with a mark on the display if the aircraft is turning in a standard rate of three degrees per second.

Note that the TC is not meant to indicate a bank angle, just rate and direction of turn. The TC may include a liquid-filled inclinometer that provides slip or skid information.

5) Heading Indicator (HI)


The HI uses a rotating gyro to display the current compass rose direction (otherwise known as the heading) that the aircraft is flying. Using a 360-degree compass card with north as zero or “N,” the HI shows headings in 5-degree increments with every 30 degrees enumerated. To reduce crowding, the last “zero” of the heading is omitted—”3” is 30 degrees, “12” is 120, etc.

An adjustment knob turns the internal HI compass card to align with the aircraft’s magnetic compass.

6) Vertical Speed Indicator (VSI)


The VSI uses internal pressure differential to provide a visual indication of how fast the aircraft is climbing or descending. A diaphragm with chambers connected to the static port expands or contracts in response to climbs and descents, causing the instrument to indicate the rate of climb or descent in hundreds of feet per minute (fpm). A hole in the diaphragm releases the pressure change to return to zero rate when no change is occurring.



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