Tecnam P2008 - Descriptive Data; Airframe; Powerplant; Engine

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1.3 Descriptive Data
1.3.1 Airframe
1.3.1.1 Wing
Wing Span
9.00 m (29.5 ft)
Wing Area
12.16 m
2
(130.9 ft
2
)
Aspect Ratio
6.7
Taper Ratio
0.8
Wing chord
1.373 m (4.5 ft)
1.3.1.2 Fuselage
Overall length
6.93 m (22.7 ft)
Overall width
1.20 m (3.9 ft)
Overall height
2.46 m (8.07 ft)
1.3.1.3 Empennage
Stabilator span
2.90 m (9.51 ft)
Stabilator area
2.03 m
2
(21.8 ft
2
)
Vertical tail area
1.06 m
2
(11.4 ft
2
)
1.3.1.4 Landing Gear
Wheel track
1.8 m (5.9 ft)
Wheel base
1.94 m (6.4 ft) - 1.74 m (5.7 ft steerable nose landing gear)
Main gear tire
Air Trac 5.00-5
Nose Gear tire
Sava 4.00-6
Wheel brakes
Marc Ingegno 199-102
1.4 Powerplant
1.4.1 Engine
Manufacturer
Model
Certification basis
Type
Bombardier-Rotax GmbH
912 ULS
ASTM F2339-06
4 stroke carburetor engine
73.5 kW (98.5 hp) @ 5800 rpm (max. 5 minutes)
Maximum power
69.0 kW (92.5 hp) @ 5500 rpm (cont.)
1.4.2 Allowed Propellers
Manufacturer
Model
Number of blades
Diameter
Type
GT Tonini
GT-2/173/VRR- FW101
2
1730 mm (68”) (no reduction permitted)
Fixed pitch – wood / composite
Manufacturer
Model
Number of blades
Diameter
Type
Spacer
Sensenich
2A0R5R70EN
2
1778 mm (70”) (no reduction permitted)
Fixed - ground adjustable pitch
B-1805-81 TECNAM Spacer