P2008 Data/Limits Flashcards by Giordano Corradini

Q

MTOW

A

650 kg

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Q

MLW

A

650 kg

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Q

Maximum Operating Altitude

A

13000 ft

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Q

Maximum Load Factor (Flaps UP)

A

+3.8/-1.9 g

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Q

Maximum Load Factor (Flaps LND)

A

+1.9/0 g

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Q

Approved Fuel

A

MOGAS + AVGAS 100LL

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Q

Max/Min Oil Level

A

3/2.5

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Q

Maximum Number of Occupants

A

2

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Q

Glide Ratio

A

12.8 (2 nm / 1000 ft)

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Q

Maximum Baggage Compartment Capacity

A

20 Kg

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Q

Maximum Demonstrated Crosswind Component

A

15 kn

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Q

Engine Model

A

ROTAX 912 S2

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Q

Maximum Engine Power

A

98.6 hp @ 2388 rpm

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Q

Maximum Continuos Engine Power

A

92.5 hp @ 2265 rpm

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Q

Maximum time above MCP

A

5 minutes

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Q

Maximum Total Fuel Tank Capacity

A

124 l

Q

Maximum Total Usable Fuel

A

120 l

Q

Maximum and Minimum Temp. for Engine Start

A

+50/-25 °C

Q

Va

A

98 kias

Q

VFE (any setting)

A

70 kias

Q

VR

A

50 kias

Q

Vx

A

63 kias

Q

Vy

A

67 kias

Q

Best glide speed (Vg)

A

71 kias

Q

Downwind speed

A

70 kias

Q

Approach speed (Flaps LND)

A

60 kias

Q

Approach speed (Flaps UP)

A

65 kias

Q

Maximum reccomended Turbulent Air Penetration Speed

A

98 kias

Q

Stall Speed (Flaps UP)

A

49 kias

Q

Stall Speed (Flaps TO)

A

46 kias

Q

Stall Speed (Flaps LND)

A

40 kias

Q

Altimeters max difference (VFR)

A

± 75 ft

Q

Magnetos drop max/diff

A

210/50 rpm

Q

Carb Heat Expected drop

A

<100 rpm

Q

RPM min/max (ground)

A

600/2100 rpm