TECNAM P2006T Flashcards
(34 cards)
Wingspan
**11,4 m **
Length
8,7 m
ENGINE
- 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
Maximum power
- 98hp @ 5800 rpm –5 minutes maximum.
- 92hp @ 5500 rpm (continuous)
Approved fuel
MOGAS
AVGAS 100LL
FUEL
- 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)
Oil capacity
Max. 3.0 litres – min. 2.0 litres (per tank)
Maximum takeoff weight
1180 kg (2601 lb)
1230 kg (2712 lb)
Maximum landing weight
1180 kg (2601 lb)
1230 kg (2712 lb)
Maximum baggage weight
80 kg (176 lb)
Maximum zero wing fuel weight
1145 kg (2524 lb)
V<strong>NE</strong>Never exceed speed
167 KIAS
171 KIAS
V<strong>NO</strong>Maximum Structural CruisingSpeed
135 KIAS
V<strong>A</strong>Design Manoeuvring speed
**118 KIAS **
**122 KIAS **
V<strong>LE</strong>Maximum Landing Gear extended speed
93 KIAS
122 KIAS
** VLO**Maximum Landing Gear operating speed
**93 KIAS **
122 KIAS
VFEMaximum flapsextended speed
T.O. 119/122 KIAS
FULL 93 KIAS
V<strong>MC</strong> Aircraft minimum control speed with one engine inoperative
62 KIAS
Oil normal operating range (approx.)
90° C / 110° C
Oil Pressure
- Min 0.8 Bar
- Normal 2 – 5 Bar (above 1400 rpm prop)
- Max 7 Bar
Fuel pressure
Min 2.2 psi
Max 5.8 psi
Maximum operating altitude
14000 ft
Voltmeter
- Min limit 10,5 Volt
- Normal operating 12 - 14 Volt
CENTER OF GRAVITY RANGE
- Forward limit 0.221 m (16.5% MAC)
- Aft limit 0.415 m (31% MAC) aft of datum for all weights