Tecnam P2006T Aircraft Systems Quiz

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Questions and Answers

What material is the rudder primarily made of?

Steel Alloy

Composite material

Aluminum alloy (correct)

Light alloy

Which of the following best describes the secondary flight controls?

As in (C) and flap system (correct)

Two axis trim system

One axis trim system

As in (A) and flap system

How is the rudder trim tab operated?

Automatically during flight

Manually via control wheel

Can be adjusted on ground only

Electrically via switch (correct)

Where is the emergency light located?

Over the LH instrument panel Signup and view all the answers

What is the lubrication system of the engine?

Dry sump with oil pump and pressure regulator Signup and view all the answers

Where is the fuel gascolator located?

Between fuel tank and electric pump Signup and view all the answers

What type of retraction system does the landing gear use?

Electro-hydraulic type Signup and view all the answers

Which scenario triggers a warning horn for the pilots?

Both throttle levers are at idle and/or flaps are in LAND position Signup and view all the answers

Which statement about the engine of the Tecnam P2006T is incorrect?

All are correct Signup and view all the answers

What is the travel limit of the trailing edge of the stabilator?

Up 20° Down 17° Signup and view all the answers

Which statement regarding the propeller of the Tecnam P2006T is incorrect?

It has three blades made of metal only Signup and view all the answers

Which fuel type is NOT approved for the Tecnam P2006T?

JET A fuel Signup and view all the answers

What characterizes each main gear in the Tecnam P2006T?

An oleo-pneumatic shock absorber Signup and view all the answers

What does VYSE refer to in aviation terms?

Best Angle of Climb speed in case of one engine inoperative Signup and view all the answers

What does TOD measure in terms of aircraft performance?

Distance from start to 15m obstacle clearance Signup and view all the answers

Where are the static air sources located on the Tecnam P2006T?

At both sides of the fuselage Signup and view all the answers

What is the ambient temperature limitation for the Tecnam P2006T?

-25 degrees Celsius to 45 degrees Celsius Signup and view all the answers

Which of the following KIAS values is a correct combination for VNO, VLE, and VMC?

135, 118, 62 Signup and view all the answers

What is the maximum speed with full flaps extended in KIAS?

93 KIAS Signup and view all the answers

What is the maximum operating altitude of the Tecnam P2006T?

14500 ft MSL Signup and view all the answers

Which procedure is correct for emergency landing gear operation?

Remove access panel on pilot side and turn right control lever 90 degrees Signup and view all the answers

At what RPM is the propeller check carried out on the Tecnam P2006T?

1650 rpm Signup and view all the answers

How many times must the propeller be checked from minimum to maximum?

Three times Signup and view all the answers

Which of the following statements regarding propeller checks is true?

Both a and b are correct Signup and view all the answers

What type of cooling system do the cylinders of the Tecnam P2006T aircraft use?

Liquid cooled cylinders, liquid cooled cylinder head (closed and pressurized circuit) Signup and view all the answers

Which option describes the function of the left fuel selector in the Tecnam P2006T?

It manages the left engine's fuel supply, and allows for fuel supply from the left or right tank. Signup and view all the answers

What is the maximum continuous propeller RPM and engine RPM for maximum power in the Tecnam P2006T?

2388/5800 Signup and view all the answers

Identify the incorrect statement regarding the lighting system of the Tecnam P2006T.

Strobe lights are located on the winglets and under the fuselage. Signup and view all the answers

Where are the fuel quantity indicators and fuel pressure indicators located for each engine?

On both the LH and RH instrument panels. Signup and view all the answers

What is true about the vent valves of each wing tank in the Tecnam P2006T?

They are located on the upper wing skin. Signup and view all the answers

How is the right fuel selector configured in the Tecnam P2006T?

It allows for crossfeed from both left and right tanks. Signup and view all the answers

Which of these statements about the lighting system in the Tecnam P2006T is correct?

NAV lights help avoid collisions and are essential during flight. Signup and view all the answers

What is the standard empty weight of an aircraft?

Weight of aircraft without fuel and engine fluids Signup and view all the answers

What is the maximum oil capacity for a Tecnam P2006T?

6 liters in total Signup and view all the answers

What is the upper limit of the green arc on the Airspeed Indicator (ASI)?

66-135 Signup and view all the answers

How long can a flight operate above 12,500 ft without supplemental oxygen?

5 min Signup and view all the answers

What is the minimum limit for fuel pressure?

2.0 psi Signup and view all the answers

What consequence does excessive oil pressure lead to?

High pitch propeller configuration Signup and view all the answers

What is indicated by the yellow arc of propeller RPM?

2265-2388 Signup and view all the answers

What is the immediate action after engine failure in flight?

Autopilot- OFF and keep control using rudder and aileron Signup and view all the answers

An unwanted landing gear extension with at least one leg moving downward may indicate which of the following?

All of the above Signup and view all the answers

What is the best angle of climb speed for an aircraft with a maximum takeoff weight of 1230 kg?

84 KIAS Signup and view all the answers

When starting a cold engine, what should the throttle position be?

Fully closed, with chokes fully closed Signup and view all the answers

For a flooded engine after starting, which procedure should be followed?

Keep chokes closed, open throttle fully and start engine then reduce throttle to idle Signup and view all the answers

What is the minimum oil temperature that the engine should be warmed up to, and at what rpm?

60°C at 1200 rpm Signup and view all the answers

Maximum takeoff power must be limited to which of the following durations?

5 minutes Signup and view all the answers

The aircraft has a trim tab on which aileron and how is it operated?

Right; operated mechanically via control wheel Signup and view all the answers

How many outlets are there in the Tecnam P2006T for entering ram air for ventilation?

Two Signup and view all the answers

Study Notes

Tecnam P2006T Study Notes

Engine Model and Type: The engine model is 912 S3, a four-cylinder horizontally opposed engine with air-cooled cylinders and heads.
Stabiliator Travel Limit: The trailing edge of the stabilator travels up to 20 degrees and down to 17 degrees.
Propeller Details: The propeller diameter is 1780 mm and is a three-bladed wood/composite propeller with an aluminum hub. It's hydraulically controlled variable pitch. The manufacturer is MT propeller.
Approved Fuel Type: The approved fuel type for the Tecnam P2006T is MOGAS ASTM D4814. Note: Check if DGCA has approved MOGAS; MOGAS EN228 Super/Super plus; or AVGAS 100LL (ASTM D910).
VYSE Definition: VYSE refers to the Best Rate of Climb speed in case of one engine inoperative.
Take-off Distance (TOD): TOD is the distance measured from the start to 15m obstacle clearance.
VNO, VLE, VMC (KIAS):
- VNO: 135 KIAS, VLE: 118 KIAS, and VMC: 93 KIAS (or 62 KIAS depending on the source)
Maximum Full Flaps Extended Speed: The maximum full flaps extended speed is not explicitly stated in the provided text, but some value is given
ASI Blue Line Significance: The blue line on the ASI indicates the Minimum Control Speed with one engine inoperative.
Maximum CHT: The maximum CHT (cylinder head temperature) is 135°F.
Normal Oil Pressure Range: The normal range for oil pressure is 29-73 PSI.
Maximum Oil Pressure: The maximum oil pressure is 107 PSI.
Landing Gear Hydraulic System Low Pressure Limit: The low pressure limit for the landing gear hydraulic system is 20 bar.
Emergency Exit Procedure: To bypass the door lock system, push and hold the red tab down to open the door with the handle.
Magneto Check: A magneto check should be performed at 1650 RPM, with a maximum RPM difference between right and left less than 150.
Maximum Demonstrated Crosswind: The maximum demonstrated crosswind is 17 knots.
Fuselage, Skin Panel & Fairing: The fuselage is a semi-monocoque structure made of light alloy with stressed skin panels; the radome and stern fairing are also made of light alloy.
Rudder Material: The rudder is made of light alloy.
Secondary Flight Controls: Secondary flight controls consist of one-axis trim system and flap system, or two-axis trim system and flap system .
Landing Gear Emergency Operation: Emergency operation of the landing gear can be performed with hydraulic jacks.
Cabin Heat Control Knobs Position: The heat control knobs are located on the lower side of the left instrument panel.
Maximum Baggage Weight: The maximum baggage weight allowed is 80 kg (or 130 pounds).
Generators: Each generator is rated at 12 VDC, 20 amps (or 14.2-14.8 VDC, 40 amps).
Cockpit Lights: Cockpit lights are supplied by the battery bus or LH Avionics bus during normal operations.
Landing Gear System Type in P2006T: The Landing gear retraction system in the Tecnam P2006T is electro-hydraulic.
Aural warnings: aural warnings of a gear up landing are given in terms of different configurations of flaps, throttles, and landing gear position.
Engine Cylinders: The P2006T engine has four cylinders arranged horizontally in an opposed configuration.
Oil Type: Approved oil for the engines is Aviation Grade Mineral Oil (Red Can) or Aviation Grade Synthetic Oil (Blue Can), with API Classification "SG" or higher.
Fire Extinguisher: The aircraft has Carbon Dioxide fire extinguishers.
Propeller Positions: The P2006T flap indicator shows four positions (0, takeoff (T/O), 15°, and full).
RPM Indicator: The RPM indicator shows propeller revolutions.
Fuel System: Each wing tank has a vent valve located on the upper wing skin, and the fuel system uses electric pumps for safety and normal operation.
Gascolator: The fuel filter/gascolator is located beneath the engine nacelle, between the fuel tank and electric pump.
Starting procedure for cold engines: Throttle is fully closed, chokes fully closed; then advance throttle to approximately 800 rpm after starting.
Maximum Take off Power: The maximum take-off power must be limited to 10 minutes.
Engine Warm-up: The engine requires warmup time at 900 rpm to minimum oil temperature of 60 or 50 °C
Ground Ram Air Inlet: There are one or two outlets for the entry of ram air for ventilation in Tecnam P2006T.

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Description

Test your knowledge on the key systems and specifications of the Tecnam P2006T aircraft. This quiz covers a range of topics including the engine, control surfaces, landing gear, and performance metrics. Perfect for aviation enthusiasts or those studying aircraft systems.