Tecnam P2006T Aircraft Systems Quiz

The model number of the engine used in the Tecnam P2006T is 912 S3.

The Tecnam P2006T's engine is a four-cylinder, horizontally opposed configuration. This means the cylinders are arranged in a flat line and face each other.

The Tecnam P2006T uses a variable pitch propeller that is controlled hydraulically.

The Tecnam P2006T can be fueled with AVGAS 100LL, MOGAS (ASTM D4814) or MOGAS EN228 Super/ Super plus.

VYSE is the minimum control speed, which is the speed at which the aircraft can be controlled with one engine inoperative.

TOD refers to the distance measured from the start of takeoff roll to when the aircraft reaches 15m obstacle clearance.

The maximum flap extended speed for the Tecnam P2006T is 118 kIAS.

The blue line on the ASI (Airspeed Indicator) represents the best angle of climb (AOC) speed, with one engine inoperative. This is the speed that provides the steepest climb in a single-engine scenario.

The Tecnam P2006T uses a combined cooling system: the cylinders are air-cooled using ram air, while the cylinder heads are liquid-cooled by a closed, pressurized system.

Each fuel selector controls its respective engine's fuel supply. They can switch between the left and right fuel tanks or be set to OFF.

The maximum continuous propeller RPM is 2265, and the maximum continuous engine RPM is 5500. These are the limits for maximum power.

Taxi and landing lights are actually located on the left wing leading edge, not on the right as some might assume.

Fuel quantity and pressure indicators are displayed on the left instrument panel, providing crucial information about the fuel system.

Each wing tank has a vent valve located on the upper wing skin, ensuring proper ventilation for the fuel tank.

The Tecnam P2006T uses a combined cooling system, where the engine cylinders are air-cooled and the engine cylinder heads are liquid-cooled.

The Tecnam P2006T fuel selector allows for crossfeeding, which means that fuel from one tank can be supplied to the other engine if necessary.

A composite material is a material made from two or more constituent materials with significantly different properties. Each material retains its identity in the final product. The composite material is stronger and lighter than the individual original materials.

Secondary flight controls are controls that assist in maintaining a stable flight path. They include: trim systems which adjust the aircraft's trim, and flaps that alter the airfoil shape for improved performance.

Rudder trim tab is a small, movable section on the rudder that helps adjust the rudder's position. This is usually manually operated via the control wheel, allowing the pilot to trim the rudder for stable flight without having to hold constant pressure on the rudder pedals.

The emergency light is a bright light that helps pilots see in the event that the main cabin lights fail. It is located on the overhead panel, making it easily accessible in an emergency.

A dry sump system is a lubrication system that separates the engine oil from the engine crankcase. It uses a separate tank to store oil and relies on an oil pump to circulate oil to the engine. This system is often favored for higher performance engines because it prevents oil from sloshing around in the crankcase creating turbulence.

The fuel gascolator is a device that filters out contaminants from fuel before it reaches the engine. It's located before the engine driven pump, ensuring that the engine receives clean fuel.

The landing gear retraction system uses hydraulic power to move the landing gear up and down. This system is reliable, efficient, and offers a smooth operation.

The warning horn is a safety feature that alerts pilots to potential dangers. It sounds when the landing gear control knob is in the 'UP' position, and at least one throttle lever is at idle or the flaps are in the 'LAND' position.

The Tecnam P2006T's main landing gear is designed with a single axle unit featuring an oleo-pneumatic shock absorber to absorb landing impacts.

The static air sources on the Tecnam P2006T are strategically located on both sides of the fuselage. They are used to supply static air pressure for various aircraft instruments and systems.

The Tecnam P2006T can operate within a temperature range of -25 degrees Celsius to 45 degrees Celsius for safe and optimal performance.

The maximum operating altitude for a Tecnam P2006T is 14,000 feet above sea level.

In an emergency landing gear deployment, access the panel on the co-pilot side floor and turn the upper right hand control lever 90 degrees counter-clockwise. Wait for 20 seconds and then turn the left hand lever 90 degrees counter-clockwise. This procedure extends the landing gear.

When performing propeller checks for the Tecnam P2006T, the engine rpm should be set to 1650 rpm. The check involves moving the propeller from minimum to maximum pitch three times to ensure proper operation.

Propeller revolution is the number of rotations the propeller makes in a given period of time, typically measured in RPM (revolutions per minute). This is a key parameter for determining how much thrust the propeller generates.

Engine revolution refers to the speed at which the engine crankshaft rotates. It is also measured in RPM. A higher engine revolution typically indicates an increased power output, but may also lead to higher fuel consumption and wear.

The weight of the aircraft without fuel and engine fluids. It's essentially the basic weight of the plane, excluding consumables.

The maximum amount of oil the Tecnam P2006T engine can hold.

The range of airspeeds displayed on the ASI (Airspeed Indicator) that are safe for flight, indicated by a green arc on the gauge.

The maximum time you can fly above 12,500 ft without supplemental oxygen due to the thinner air and lower oxygen levels.

Minimum limit for fuel pressure in the Tecnam P2006T, typically measured in pounds per square inch (psi).

The normal operating range for the voltmeter, which measures the electrical voltage in the aircraft's system.

Excessive oil pressure can lead to a high pitch propeller configuration, potentially resulting in propeller feathering, which stops the propeller from spinning for safety reasons.

The range of engine RPM (Revolutions Per Minute) that indicates the safe operating zone for the propeller, displayed on the engine tachometer.

An unwanted extension of the landing gear, where at least one leg moves downward, often caused by hydraulic fluid loss.

The best angle of climb speed for a maximum takeoff weight of 1230 kg is 72 KIAS.

To start a cold engine, the throttle should be fully closed, the chokes fully closed, and after starting, the throttle should be advanced to approximately 800 rpm.

To address a flooded engine after starting, keep the chokes closed, open the throttle fully, and start the engine. Then, quickly reduce the throttle to idle.

The engine should be warmed up to a minimum oil temperature of 50°C at 900 rpm.

The maximum takeoff power for the Tecnam P2006T should be limited to 5 minutes.

The Tecnam P2006T has a trim tab on the left aileron. It is operated electrically via a switch.

The Tecnam P2006T has two outlets for entering ram air for ventilation, which is essential for cooling and cabin pressurization.