Using the proven P92, (an all metal, two seats, single strut braced high wing aeroplane, as the base platform) and paying particular attention to the needs of the new American LSA category, Tecnam has delivered the best high wing training and cross country aircraft to date in the light general aviation category.
The Eaglet combines the best features of their existing high wing aircraft line merged into a single platform. The Eaglet’s increased side visibility, smooth aerodynamic lines, a low profile modular panel able to accommodate a wide range of avionics, while still maintaining excellent visibility over the nose, a trait of all TECNAM models.
The doors which are lined with automotive type door seals, seats that give full support with excellent leg room, side map pockets as well as pockets in the back of the seats all combine to make the Eaglet a very comfortable aircraft.
Some of the advantages: Superior performance and flight characteristics. Low stall speed with excellent response at all speeds. Stable and Responsive with uncompromising build quality (based on CS/VLA certified Aircraft). Excellent visibility, roomy, quiet and ergonomic.
All this makes the Eaglet the natural choice for discriminating buyers of all ages and levels of flight experience.
P92 Eaglet US-LSA
Exteriors
Interiors Details
The generous interior dimensions of the Tecnam P92 Eaglet allow maximum space for Pilot and passenger alike.
With two wide doors and eco leather seats adjustable fore and aft, the cabin provides great flexibility for pilots of varying physical size to optimize their comfort. Each seat is provided with a three point seat belt. Dual controls come as standard with PTT and electric stabilator trim on the stick with a trim indicator on the panel. The plane comes with dual conventional rudder pedals with steerable nose wheel and toe brakes.
Avionics
Non additive, replace standard equipment and avionics
Option 1 – GARMIN SIX PACK
Flight instruments and indicators
• Attitude, Electric
• Directional, Electric
• Turn & Bank
• Trim Position Indicator
• Flap Indicator
Engine analog instruments:
• Tachometer
• Hour Recorder
• Oil Press
• Oil Temp.
• Head Temp.
• Fuel Press.
• Voltmeter
• Ammeter
AVIONICS PACKAGE
• Garmin GMA 240 Audio Panel
• Garmin GTR 200 Com
• Garmin GTX 327 Transponder
• Garmin 796 Gps XM Version
• Stick Pushp-To-Talk Switch Pilot/Copilot
• Mic & Phone Jacks Pilot/Copilot
• Antennas:
– Transponder
– Vhf
– Gps
Option 2 – GARMIN G3X
Garmin G3X two screens Avionics Package for For Rotax 912 Uls2 & Is
• GDU460
• GDU465
• ADAHRS GSU 25
• ADAHRS GSU 25 2Nd ADAHRS
• GEA 24 Engine Instrument Module
• GMU 22 Magnetometer
• GtGTPp 59 Temperature Probe
• GA 35 Gps/Waas Antenna
• GA55 Xm Antenna (Tso’d-GDU 375 Only)
• LRU Kit
• Installation Kit
• G3X Sensor Kit
• Back Up Airspeed. And Altimeter
GSU CONFIGURATION
• Amps
• Monitor Cht
• Aircraft Bus Voltages
• Oil Temperature
• Oat
• Oil Pressure
• Manifold Pressure
• Fuel Pressure
• Rpm
• Trim Indicator
AVIONICS PACKAGE
• Garmin GMA 240 Audio – Panel
• Garmin GTR 200 Com
• Gtx 23 Transponder Mode S Remote Mounted
• Stick Push-top-talk Switch-pilot/Copilot
• Mic & Phone Jacks-pilot/Copilot
• Antennas:
– Transponder
– Vhf
– Gps
Aircraft Dimensions
| Fuselage Height | 8.2 ft – 2.5 mt |
| Fuselage Length | 21.3 ft – 6.5 mt |
| Wingspan | 28.5 ft – 8.70 mt |
| Cabin Height (seat to cover) | 3 ft – 0.91 mt |
| Cabin Width | 3.7 ft – 1.14 mt |
| Max Seating capacity | 2 |
| Fuel tank capacity | 22.4 US – Gal 90 lt |
Powerplant
| Engine Manufacturer | ROTAX 912ULS/912is / LYCOMING YO-233-B2A |
| Engine Power | 90 to 115 hp |
| Time Before Overhaul | 2000 hrs |
| Propeller | Senseniich |
| Fuel Consumption | 4.50 US Gal/h – 17 lt/h |
| Fuel Type | Avgas and Mogas |
Design Weight & Loading
| Maximum Take Off Weight | Design Weight: 1320 lb – 600 kg |
| Empty Weight, Standard | 780 lb – 355 kg |
| Useful Load | 540 lb – 245 kg |
Performance
| Max Cruise Speed (KTAS) | 118 kts – 219 km/h KTAS |
| Stall Speed (Flaps Down Power Off) KCAS | 39 kts – 72 km/h KCAS |
| Practical ceiling | 13,120 ft – 4.000 mt |
| Take off run | 459 ft – 140 mt |
| Take off distance | 918 ft – 280 mt |
| Landing Run | 377 ft -115 mt |
| Landing Distance | 935 ft – 285 mt |
| Rate of climb | 1100 ft/min – 5.6 m/sec |
| Range | 530 NM |