P2008 Data/Limits Flashcards

1
Q

MTOW

A

650 kg

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2
Q

MLW

A

650 kg

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3
Q

Maximum Operating Altitude

A

13000 ft

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4
Q

Maximum Load Factor (Flaps UP)

A

+3.8/-1.9 g

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5
Q

Maximum Load Factor (Flaps LND)

A

+1.9/0 g

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6
Q

Approved Fuel

A

MOGAS + AVGAS 100LL

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7
Q

Max/Min Oil Level

A

3/2.5

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8
Q

Maximum Number of Occupants

A

2

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9
Q

Glide Ratio

A

12.8 (2 nm / 1000 ft)

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10
Q

Maximum Baggage Compartment Capacity

A

20 Kg

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11
Q

Maximum Demonstrated Crosswind Component

A

15 kn

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12
Q

Engine Model

A

ROTAX 912 S2

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13
Q

Maximum Engine Power

A

98.6 hp @ 2388 rpm

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14
Q

Maximum Continuos Engine Power

A

92.5 hp @ 2265 rpm

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15
Q

Maximum time above MCP

A

5 minutes

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16
Q

Maximum Total Fuel Tank Capacity

A

124 l

17
Q

Maximum Total Usable Fuel

A

120 l

18
Q

Maximum and Minimum Temp. for Engine Start

A

+50/-25 °C

19
Q

Va

A

98 kias

20
Q

VFE (any setting)

A

70 kias

21
Q

VR

A

50 kias

22
Q

Vx

A

63 kias

23
Q

Vy

A

67 kias

24
Q

Best glide speed (Vg)

A

71 kias

25
Q

Downwind speed

A

70 kias

26
Q

Approach speed (Flaps LND)

A

60 kias

27
Q

Approach speed (Flaps UP)

A

65 kias

28
Q

Maximum reccomended Turbulent Air Penetration Speed

A

98 kias

29
Q

Stall Speed (Flaps UP)

A

49 kias

30
Q

Stall Speed (Flaps TO)

A

46 kias

31
Q

Stall Speed (Flaps LND)

A

40 kias

32
Q

Altimeters max difference (VFR)

A

± 75 ft

33
Q

Magnetos drop max/diff

A

210/50 rpm

34
Q

Carb Heat Expected drop

A

<100 rpm

35
Q

RPM min/max (ground)

A

600/2100 rpm