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Commercial Pilot Ground Course (or Private Pilot Ground Course) > Tecnam P2002JF > Flashcards

Tecnam P2002JF Flashcards

You may prefer our related Brainscape-certified flashcards:
Charter Pilot (Part 135) - Oral flashcards
1
Q

Wing span of the tecnam?

A

8.6 meters

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2
Q

Aircraft length of the tecnam?

A

6.61 meters

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3
Q

Aircraft height of the tech?

A

2.43 meters

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4
Q

Wing taper of tecnam?

A

0.6 taper ratio

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5
Q

Propeller grand clearance of the tecnam ?

A

320 mm

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6
Q

Aspect ratio of tecnam?

A

6.4

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7
Q

Dihedral of tecnam?

A

5 degrees

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8
Q

Wing area of tecnam?

A

11.5 m2

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9
Q

Number of engines?

A

1

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10
Q

Engine manufacturer of tecnam?

A

Bombardier - rotax GmbH

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11
Q

Engine model number of tecnam?

A

912 -s2

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12
Q

State the engine type of the tecnam

A

4 cylinder horizontally - opposed twins with overall displacement of 1352 c.c, mixed cooling, (water-cooled heads and air-cooled cylinders), twin carburetors,integrated reduction gear with torque damper

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13
Q

State the hp rating and engine speed for maximum 5 minutes

A

73.5 kW (98.5 hp) @5800 rpm (max.5’)

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14
Q

State the hp rating and engine speed for cont.

A

69.0 kW (92.5 hp) @5500 rpm (cont.)

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15
Q

Manufacturer of the tecnam’s propeller

A

Hoffmann propeller

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16
Q

Number of the tecnam’s propeller

A

HO17GHM A 174 177 C

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17
Q

Number of blades of the tecnam’s propeller

A

2

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18
Q

Propeller diameter

A

1740 mm

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19
Q

Propeller type

A

Fixed pitch

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20
Q

Propeller material

A

Wood

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21
Q

Total capacity of fuel

A

100 liters

22
Q

Total capacity (each tanks )

A

50 liters

23
Q

Total usable fuel

A

99 liters

24
Q

Total unusable fuel

A

1 liter

25
Q

State the approved fuel grades

A
  • MOGAS ASTM D4814
  • MOGAS EN 228 Super/Super Plus (Min RON 95)
  • AVGAS 100LL (ASTM D910)
26
Q

Lubrication system

A

Forced type with external reservoir

27
Q

Oil capacity

A

2 Liters (min) - 3 Liters (max)

28
Q

Maximum Oil Temperature

A

130°C

29
Q

Minimum Oil Pressure

A

0.8 bar

30
Q

Maximum Oil Pressure

A

7 bar

31
Q

State the MTOW/ MLW (Takeoff Weight and Landing Weight under Normal category)

A

580 kg

32
Q

Standard Empty Weight

A

337 kg

33
Q

Useful Load

A

243 kg

34
Q

Baggage Allowance

A

20 kg

35
Q

Service Ceiling

A

Maximum operating altitude is 14,000 ft (4260m) MSL

36
Q

Fuel Consumption

A

4.5 gal/hr or 17 l/hr

37
Q

Fuel Endurance

A

4 Hrs

38
Q

Takeoff Rotation Speed

A

42 KIAS

39
Q

Enroute Climb, Flaps up:

Best Rate of Climb, Sea Level

A

66 KIAS

40
Q

Enroute Climb, Flaps up:

Best Angle of Climb, Sea Level

A

56 KIAS

41
Q

Stall Speeds

A

Bank Angle at 0°

42
Q

Stall Speed with Flaps 0°

A

40 KIAS

43
Q

Stall Speed with Flaps T/O (15°)

A

35 KIAS

44
Q

Stall Speed with Flaps Full (40°)

A

30 KIAS

45
Q

Approach Speed, Flaps T/O

A

66 KIAS

46
Q

Final Approach Speed Speed, Flaps FULL (40°)

A

51 KIAS

47
Q

Balked Landing

A

keep over 61 KIAS, climb to VY or VX as applicable

48
Q

Maneuvering Speed

A

96 KIAS

49
Q

Never Exceed Speed

A

138 KIAS

50
Q

Maximum Demonstrated Crosswind Velocity:

Takeoff and Landing

A

22 Knots

51
Q

Engine Failure After T/O

A

51 KIAS minimum

52
Q

Maximum Glide Speed

A

69 KIAS

Commercial Pilot Ground Course (or Private Pilot Ground Course) (21 decks)

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