TECNAM P2006T Flashcards

1
Q

Wingspan

A

**11,4 m **

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2
Q

Length

A

8,7 m

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3
Q

ENGINE

A
  • Bombardier-Rotax 912 S3
  • 4 cylinders horizontally opposed 1352 c.c
  • Liquid cooled cylinder heads
  • Ram-air cooled cylinders
  • Two carburetors
  • Integrated reduction gear box
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4
Q

Maximum power

A
  • 98hp @ 5800 rpm –5 minutes maximum.
  • 92hp @ 5500 rpm (continuous)
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5
Q

Approved fuel

A

MOGAS

AVGAS 100LL

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6
Q

FUEL

A
  • Integrated tanks
  • 2 TANKS: 100 litres each one (26,42 US gallons)
  • MAXIMUM CAPACITY: 200 litres (52,8 US gallons)
  • MAXIMUM USABLE FUEL: 194.4 litres (51,35 US gallons)
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7
Q

Oil capacity

A

Max. 3.0 litres – min. 2.0 litres (per tank)

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8
Q

Maximum takeoff weight

A

1180 kg (2601 lb)

1230 kg (2712 lb)

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9
Q

Maximum landing weight

A

1180 kg (2601 lb)

1230 kg (2712 lb)

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10
Q

Maximum baggage weight

A

80 kg (176 lb)

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11
Q

Maximum zero wing fuel weight

A

1145 kg (2524 lb)

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12
Q

V<strong>NE</strong>Never exceed speed

A

167 KIAS

171 KIAS

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13
Q

V<strong>NO</strong>Maximum Structural CruisingSpeed

A

135 KIAS

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14
Q

V<strong>A</strong>Design Manoeuvring speed

A

**118 KIAS **

**122 KIAS **

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15
Q

V<strong>LE</strong>Maximum Landing Gear extended speed

A

93 KIAS

122 KIAS

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16
Q

** VLO**Maximum Landing Gear operating speed

A

**93 KIAS **

122 KIAS

17
Q

VFEMaximum flapsextended speed

A

T.O. 119/122 KIAS

FULL 93 KIAS

18
Q

V<strong>MC</strong> Aircraft minimum control speed with one engine inoperative

A

62 KIAS

19
Q

Oil normal operating range (approx.)

A

90° C / 110° C

20
Q

Oil Pressure

A
  • Min 0.8 Bar
  • Normal 2 – 5 Bar (above 1400 rpm prop)
  • Max 7 Bar
21
Q

Fuel pressure

A

Min 2.2 psi

Max 5.8 psi

22
Q

Maximum operating altitude

A

14000 ft

23
Q

Voltmeter

A
  • Min limit 10,5 Volt
  • Normal operating 12 - 14 Volt
24
Q

CENTER OF GRAVITY RANGE

A
  • Forward limit 0.221 m (16.5% MAC)
  • Aft limit 0.415 m (31% MAC) aft of datum for all weights
25
Q

MANEUVERS LOAD FACTOR LIMITS

A
  • Positive + 3.8 g
  • Negative - 1.78 g
26
Q

VRRotation SpeedT/O

A

64 KIAS @1180kg

65 KIAS @1230kg

27
Q

V<strong>X</strong>Best Angle-of-Climb Speed

A

73 KIAS FLAPS 0°

28
Q

V<strong>Y</strong>Best Rate-of-Climb speed

A

80 KIAS FLAPS 0°

84 KIAS FLAPS 0°

29
Q

Approach speed T/O FLAPS

A

90 KIAS

30
Q

Final Approach Speed FULL FLAPS

A

70 KIAS

31
Q

VSSE

A

70 KIAS

32
Q

Maximum demonstrated crosswind

A

17 Kts

33
Q

Landing gear retraction system

A

Electro-Hydraulic powered by a reversible pump

34
Q

VYSEBest rate-of-climb speed with one engine inoperative

A

80 KIAS

84 KIAS