TECNAM P2006T Flashcards
1
Q
Wingspan
A
**11,4 m **
2
Q
Length
A
8,7 m
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
4
Q
Maximum power
A
- 98hp @ 5800 rpm –5 minutes maximum.
- 92hp @ 5500 rpm (continuous)
5
Q
Approved fuel
A
MOGAS
AVGAS 100LL
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)
7
Q
Oil capacity
A
Max. 3.0 litres – min. 2.0 litres (per tank)
8
Q
Maximum takeoff weight
A
1180 kg (2601 lb)
1230 kg (2712 lb)
9
Q
Maximum landing weight
A
1180 kg (2601 lb)
1230 kg (2712 lb)
10
Q
Maximum baggage weight
A
80 kg (176 lb)
11
Q
Maximum zero wing fuel weight
A
1145 kg (2524 lb)
12
Q
V<strong>NE</strong>Never exceed speed
A
167 KIAS
171 KIAS
13
Q
V<strong>NO</strong>Maximum Structural CruisingSpeed
A
135 KIAS
14
Q
V<strong>A</strong>Design Manoeuvring speed
A
**118 KIAS **
**122 KIAS **
15
Q
V<strong>LE</strong>Maximum Landing Gear extended speed
A
93 KIAS
122 KIAS