Tecnam P92 Eaglet - Descriptive Data; Airframe; Powerplant; Engine

P92 Eaglet
Flight Manual
Revision Date: 12-14-2007
Revision Number: 1.00
Doc n° 27-13-100-00
13
1.3 Descriptive Data
1.3.1 Airframe
1.3.1.1 Wing
Wing span 8.7m (28.5’)
Wing area 12 m
2
(129 sq ft)
Aspect ratio 6.31
Taper ratio 1.00
Dihedral 1.5º
Wing chord 1.400 m (4.6’)
1.3.1.2 Fuselage
Overall length 6.5m (21,3’)
Overall width 1.143 m (45”)
Overall height 2.5m (8.2’)
1.3.1.3 Empennage
Stabilator span 2.9 m (9.5’)
Stabilator area 1.972 m
2
(21.2 ft
2
)
1.3.1.4 Landing Gear
Wheel track 1.8 m (5.9’)
Wheel base 1.6 m (5.2’)
Main gear tires 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 Bombardier-Rotax GmbH
Model 912 ULS or 912 S2
Certification basis ASTM F2239 or FAR Part 33
Type 4 stroke carburetor engine
Maximum power 73.5 kW (98.5 hp) @ 5800 rpm (max. 5 minutes)
69.0 kW (92.5 hp) @ 5500 rpm (cont.)
1.4.2 Propeller
Manufacturer GT Tonini
Model GT-2/173/VRR- FW101 SRTC
Number of blades 2
Diameter 1730 mm (68”) (no reduction permitted)
Type Fixed pitch – wood / composite