P2006T Aircraft Limitations

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Questions and Answers

To which category does the Tecnam P2006T belong?

  • Aerobatic
  • Semi-acrobatic/Normal
  • Normal (correct)

What are the engine limitations for the Bombardier Rotax 912S3 in the Tecnam P2006T?

  • 5200 Engine RPM – 78,9 HP max continuous
  • 5800 Engine RPM – 98,6 HP max continuous
  • 5500 Engine RPM – 92,5 HP max continuous (correct)

What is the total capacity of the wing tanks in the Tecnam P2006T (in liters)?

  • 190
  • 180
  • 200 (correct)

What is the total usable capacity of the wing tanks in the Tecnam P2006T (in liters)?

<p>194,4 (A)</p> Signup and view all the answers

What are the positive limit load factors for the Tecnam P2006T in the normal category with retracted flaps?

<p>+3,8 -1,78 (B)</p> Signup and view all the answers

What is the maximum take-off weight allowed for the Tecnam P2006T in the normal category (in kg)?

<p>1180 (B)</p> Signup and view all the answers

What is the maximum landing weight allowed for the Tecnam P2006T in the normal category (in kg)?

<p>1180 (B)</p> Signup and view all the answers

What is the maximum allowable weight of the load compartment in the Tecnam P2006T (if used)?

<p>80 kg (A)</p> Signup and view all the answers

What is the design maneuvering speed of the Tecnam P2006T?

<p>118 kts (C)</p> Signup and view all the answers

What is the operating maneuvering speed of the Tecnam P2006T?

<p>118 kts (A)</p> Signup and view all the answers

What is the Vne (never exceed speed) of the Tecnam P2006T?

<p>167 kts (B)</p> Signup and view all the answers

What is the Vfe (maximum flap extended speed) in the TAKE-OFF position for the Tecnam P2006T?

<p>119 kts (B)</p> Signup and view all the answers

What is the Vfe (maximum flap extended speed) in the FULL position for the Tecnam P2006T?

<p>93 kts (A)</p> Signup and view all the answers

What is the Vle (maximum landing gear extended speed) for the Tecnam P2006T?

<p>93 kts (A)</p> Signup and view all the answers

What is the Vlo (maximum landing gear operating speed) for the Tecnam P2006T?

<p>93 kts (C)</p> Signup and view all the answers

What is the Vmc (minimum control speed with one engine inoperative) for the Tecnam P2006T?

<p>62 kts (C)</p> Signup and view all the answers

What is the Vno (maximum structural cruising speed) for the Tecnam P2006T?

<p>135 kts (A)</p> Signup and view all the answers

On the airspeed indicator, what is the speed range indicated by the white arc (flaps extended)?

<p>From 53 to 93 kts (A)</p> Signup and view all the answers

On the airspeed indicator, what is the speed range indicated by the green arc (normal operating range)?

<p>66-135 kts (B)</p> Signup and view all the answers

On the airspeed indicator, what is the speed range indicated by the yellow arc (caution range)?

<p>135-167 kts (A)</p> Signup and view all the answers

What does the red line placed in proximity of the low-speed range on the airspeed indicator correspond to?

<p>Vmc (C)</p> Signup and view all the answers

What is the Vyse (best rate-of-climb speed with one engine inoperative) for the Tecnam P2006T?

<p>80 kts (C)</p> Signup and view all the answers

What is the Vxse (best-climb-angle speed with one engine inoperative) for the Tecnam P2006T?

<p>79 kts (A)</p> Signup and view all the answers

What power do the engines of the Tecnam P2006T develop?

<p>5500 Engine RPM – 92,5 HP max continuous (B)</p> Signup and view all the answers

What is the maximum continuous power (5’) developed by the engines of the P2006T?

<p>5800 Engine RPM – 98,6 HP max continuous (A)</p> Signup and view all the answers

Regarding oil pressure in the Tecnam P2006T, what are the values for normal use?

<p>29-73 PSI (B)</p> Signup and view all the answers

What is the minimum fuel pressure required for the Tecnam P2006T?

<p>2,2 PSI (C)</p> Signup and view all the answers

Are flights in icing conditions allowed in the Tecnam P2006T?

<p>False (A)</p> Signup and view all the answers

What are the front and rear center of gravity (CG) limits for the Tecnam P2006T?

<p>0,221-0,415 mt (A)</p> Signup and view all the answers

What is the maximum negative load factor that the Tecnam P2006T can bear with extended flaps?

<p>0 (C)</p> Signup and view all the answers

Which type of fuel(s) is/are approved to power the Tecnam P2006T's engine, considering any necessary precautions?

<p>All the three answers are correct but precautions must be observed. (D)</p> Signup and view all the answers

What is the crosswind velocity limitation for the Tecnam P2006T?

<p>17 kts (A)</p> Signup and view all the answers

What is the maximum cruising speed in level flight for the Tecnam P2006T?

<p>135 kts (B)</p> Signup and view all the answers

What is the minimum pressure of the landing gear hydraulic system required to guarantee extension in an emergency situation for the Tecnam P2006T?

<p>20 PSI (B)</p> Signup and view all the answers

Which definition best fits the phrase 'Land as soon as possible'?

<p>Land without delay at the nearest suitable area at which a safe approach and landing is assured. (A)</p> Signup and view all the answers

Which definition best fits the phrase 'Land as soon as practicable'?

<p>Land without delay at the nearest suitable area at which a safe approach and landing is assured. (B)</p> Signup and view all the answers

What is the maximum Cylinder Head Temperature (CHT) permitted for the Tecnam P2006T?

<p>135°C (A)</p> Signup and view all the answers

What is the maximum oil temperature permitted for the Tecnam P2006T?

<p>130°C (A)</p> Signup and view all the answers

What is the maximum oil pressure permitted for the Tecnam P2006T?

<p>7 PSI (B)</p> Signup and view all the answers

Using carburetor heating in the Tecnam P2006T, approximately how much will the propeller RPM decrease?

<p>100 (C)</p> Signup and view all the answers

If the flaps become unserviceable, and a landing without flaps is necessary, by what percentage should the landing distance be increased in the Tecnam P2006T?

<p>25% (A)</p> Signup and view all the answers

What is the best glide speed, without flaps, for the Tecnam P2006T?

<p>83 kts (A)</p> Signup and view all the answers

With retracted flaps, approximately what Calibrated Airspeed (CAS) corresponds to an Indicated Airspeed (IAS) of 100 kts in the Tecnam P2006T?

<p>98 kts (C)</p> Signup and view all the answers

What is the stall speed of the Tecnam P2006T with retracted flaps and a bank angle of 0°?

<p>66 kts (C)</p> Signup and view all the answers

What is the stall speed of the Tecnam P2006T with flaps extended in the TAKE-OFF position and a bank angle of 60°?

<p>81 kts (C)</p> Signup and view all the answers

What is the stall speed of the Tecnam P2006T with flaps extended in the FULL position and a bank angle of 30°?

<p>58 kts (C)</p> Signup and view all the answers

With the Main Bus switched off, what kind of indication does the stall speed indicator provide in the Tecnam P2006T?

<p>It does not provide any kind of indication (A)</p> Signup and view all the answers

Which of the following components are part of the fuel system in the Tecnam P2006T?

<p>Two auxiliary electric pumps and two mechanical pumps (C)</p> Signup and view all the answers

When the LEFT engine tank selector is selected to RIGHT, what occurs in the fuel system of the Tecnam P2006T?

<p>The fuel from the left tank is directed to the right tank (C)</p> Signup and view all the answers

Flashcards

P2006T category

Normal category.

Engine Limitations Bombardier Rotax 912S3

5500 Engine RPM – 92,5 HP max continuous.

Wing tanks capacity

200 liters.

Total usable wing tanks capacity

194.4 liters.

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Positive Limit Load Factor (Normal, Retracted Flaps)

+3.8, -1.78.

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Maximum Take-Off Weight (Normal Category)

1180 kg.

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Maximum Landing Weight (Normal Category)

1180 kg.

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Maximum Allowable Load Compartment Weight

80 kg.

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Design Maneuvering Speed

118 kts.

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Operating maneuvering speed

118 kts

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Vne

167 kts.

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Vfe (Take-off)

119 kts.

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Vfe (Full)

93 kts.

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Vle

93 kts.

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Vlo

93 kts.

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Vmc

62 kts.

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Vno

135 kts.

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Airspeed Indicator White Arc

From 53 to 93 kts.

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Airspeed Indicator Green Arc

66-135 kts.

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Airspeed Indicator Yellow Arc

135-167 kts.

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Red Line (Low Speed)

Vmc

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Blue Line (Low Speed)

Vyse

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Vyse

80 kts.

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Vxse

79 kts.

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P2006T Engine Power

5500 Engine RPM – 92,5 HP max continuous

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P2006T Engine Power (5')

5800 Engine RPM – 98,6 HP max continuous

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Normal Oil Pressure

29-73 PSI

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Minimum Fuel Pressure

2,2 PSI.

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Flight in icing condition allowed?

False

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CG limits

0,221-0,415 mt

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Max Negative Load Factor (Flaps Extended)

0

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Acceptable fuel types

the three answers are all correct but precautions must be observed.

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Crosswind velocity limitation

17 kts

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Max Cruising Speed

135 kts.

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Minimum Hydraulic Pressure (Emergency Gear)

20 PSI

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Land as soon as possible

land without delay at the nearest suitable area at which a safe approach and landing is assured.

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Land as soon as practicable

land at the nearest approved landing area where suitable repairs can be made.

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Maximum CHT value

135°C

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Maximum oil temperature value

130°C

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Maximum oil pressure value

7 PSI

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Study Notes

  • P2006T belongs to the normal category.
  • The Bombardier Rotax 912S3 engine limitations are 5500 Engine RPM and 92.5 HP max continuous.
  • Total wing tanks capacity is 200 liters.
  • Total usable capacity of the wing tanks is 194.4 liters.
  • Positive limits load factor for normal category with retracted flaps is +3.8/-1.78.
  • Maximum take-off weight allowed in normal category is 1180 kg.
  • Maximum landing weight allowed in normal category is 1180 kg.
  • Maximum allowable weight of the load compartment is 80 kg.
  • Design Maneuvering Speed is 118 kts.
  • Operating Maneuvering Speed is 118 kts.
  • Vne (Never Exceed Speed) is 167 kts.
  • Vfe (max flap extended speed) in TAKE-OFF position is 119 kts.
  • Vfe (max flap extended speed) in FULL position is 93 kts.
  • Vle (max landing gear extended speed) is 93 kts.
  • Vlo (max landing gear operating speed) is 93 kts.
  • Vmc (minimum control speed with one engine inoperative) is 62 kts.
  • Vno (max structural cruising speed) is 135 kts.
  • The white arc on the airspeed indicator (flaps extended range) is from 53 to 93 kts.
  • The green arc on the airspeed indicator (normal use range) is from 66-135 kts.
  • The yellow arc on the airspeed indicator (smooth air range) is from 135-167 kts.
  • A red line on the airspeed indicator corresponds to Vmc.
  • A blue line on the airspeed indicator corresponds to Vyse.
  • Vyse (best rate-of-climb speed with one engine inoperative) is 80 kts.
  • Vxse (best-climb-angle with one engine inoperative) is 79 kts.
  • The engines develop 92.5 HP max continuous at 5500 Engine RPM.
  • The engines develop 92.5 HP max continuous (5’) at 5500 Engine RPM.
  • The normal oil pressure range is 29-73 PSI.
  • Minimum fuel pressure is 2.2 PSI.
  • Flights in icing conditions are not allowed.
  • Center of gravity limits are 0.221-0.415 mt.
  • The max negative load factor with extended flap is 0.
  • AVGAS 100LL, MOGAS ASTM D4814, and MOGAS EN 228 Super/Super plus (min. RON 95) can power the engine with precautions.
  • The crosswind velocity limitation is 17 kts.
  • Maximum cruising speed in level flight is 135 kts.
  • The minimum pressure of the landing gear hydraulic system for emergency extension is 20 PSI.
  • “Land as soon as possible” means land without delay at the nearest suitable area with a safe approach and landing assured.
  • “Land as soon as practicable” means land without delay at the nearest suitable area with a safe approach and landing assured.
  • Maximum permitted CHT (Cylinder Head Temperature) is 135°C.
  • Maximum permitted oil temperature is 130°C.
  • Maximum permitted oil pressure is 7 PSI.
  • Using carburetor heating, propeller RPM decreases by 100.
  • If landing without flaps, the landing distance must be increased by 25%.
  • Best glide speed without flaps is 83 kts.
  • IAS of 100 kts with retracted flaps corresponds to a CAS of 98 kts.
  • Stall speed with retracted flap and 0° bank angle is 66 kts.
  • Stall speed with extended flap in TO position and 60° bank angle is 81 kts.
  • Stall speed with extended flap in FULL position and 30° bank angle is 58 kts.
  • With the Main Bus switched off, the stall speed indicator does not provide any kind of indication.
  • The fuel system includes two auxiliary electric pumps and two mechanical pumps.
  • When the LEFT engine tank selector is selected to RIGHT, fuel from the left tank is directed to the right tank.
  • When the RIGHT engine's tank selector is selected on LEFT, fuel from the right tank is directed to the left tank.
  • The brake system is hydraulic.
  • At 1180 kg, 4000 ft PA, 25°C, with 15 kts tailwind, the take-off run and distance are 468 - 610 mt.
  • At 1080 kg, sea level, 0°C, with 25 kts headwind, the take-off run and distance are 125.5 – 183.5 mt.
  • At 930 kg, 14000 ft PA, 0°C, with Vy at 62 kts, the climb rate is +404 ft/m.
  • At 1180 kg, 4000 ft PA, TISA, with Vy at 79 kts, the climb rate is +818 ft/m.
  • At 1080 kg, 500 ft PA, 0°C, with Vx at 72 kts, the climb rate is +766 ft/m.
  • At 1180 kg, 1000 ft PA, 50°C, with Vx at 76 kts, the climb rate is +729 ft/m.
  • At 1180 kg, 4000 ft PA, 0°C, with Vx at 72 kts, the en route climb rate is +729 ft/m.
  • At 1180 kg, one engine inoperative, 2000 ft PA, 25°C, with Vyse at 80 kts, the en route climb rate is +97 ft/m.
  • At 1180 kg, one engine inoperative, 2000 ft PA, 25°C, with Vxse at 79 kts, the en route climb rate is +69 ft/m.
  • At 1150 kg, 6000 ft PA, ISA+30, 2250 RPM/22” HG MAP, the parameters are: 57% Power, 119 ktas, 22.6 lt/h fuel flow.
  • At 1150 kg, 12000 ft PA, ISA, 2250 RPM/18” HG MAP, the parameters are: 60% Power, 129 ktas, 16.8 lt/h fuel flow per engine.
  • At 1180 kg, 3000 ft PA, +25°C, the landing distance and run are 261 - 378.
  • With a 2.5% uphill gradient, landing distances become 276 - 393.
  • With a paved surface and uphill gradient, the landing run is 235.
  • With a 20 kts headwind, the landing distances are 145- 279.
  • The electrical system is powered by alternators with operating characteristics of 14 VDC/40 A.
  • Each engine has 4 cylinders, double electronic injection, forced lubrication, and liquid cooling.
  • The voltmeter indication for correct electrical system operation is between 12 – 14 V.
  • The aircraft's anti-ice system consists of Pitot tube electric heating.
  • The temperature range for aircraft operation is -25°C to +50°C.
  • The maximum allowed altitude of the aircraft is 14000 ft.

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