The Tecnam production line employs a monocoque tail cone section with the forward fuselage using sheet aluminum over steel tubing. The wing is an all aluminum conventional structure with a single strut. The top and bottom engine cowls are quickly and easily removable making any maintenance easier to accomplish. A wide rear window together with large side windows complete the extraordinary visibility allowing 360° of vision in the cockpit. The all moving Stabilator is fitted with a trim tab controlled by buttons on the control column. The excellent flying characteristic with neutral handling makes it extremely stable and easy to fly for people of any weight/height. The large flaps are deployed electrically and allow a stall speed lower than 41 KTS (76 km/h). The low stall speed and the general slow flying characteristics of the aircraft allows it to operate with ease on short runways.
P92 JS
Light, only in weight.
The Tecnam P92 JS is a high wing, two place, single engine airplane equipped with tricycle landing gear. But is not only that. The P92 JS is the plane for flying with a style, enjoying beauty inside and outside.
Exterior
Interior
Seats are adjustable and increase in height as they are moved forward. The luggage area allowing for 44 pounds/20 kg of weight is located behind the seats with easy access in flight. All Tecnam aircraft have dual control sticks, rudder pedals. The trim tab and the flaps are electrically activated with a position indicator on the instrument panel. The fresh air vents are conveniently located in the doors. Heat and defrost are standard. The aircraft has dual conventional rudder pedals with a steerable nose wheel. The wide conventional instrument panel allows fitment of a broad range equipment, in addition to standard VFR training requirements. The interior is spacious, ergonomic and comfortable.
Enjoy the P92!
Avionics
Standard
GMA 340 Audio Panel
GNC 255A COM/NAV
GTX 335 Transponder ADS-B OUT
ELT 406 Mhz KANNAD
Antennas:
– Transponder
– VHF
– Marker Beacon
– ELT
Speakers
Microphone
Stick Push-To-Talk Switch-Pilot/Copilot
Mic & Phone Jacks-Pilot/Copilot
Aircraft Dimensions
| Fuselage Height | 2.5 mt – 8.2 ft |
| Fuselage Length | 6.4 mt – 21 ft |
| Wingspan | 8.7 mt – 28.5 ft |
| Cabin Height (seat to cover) | 0.91 mt – 3 ft |
| Cabin Width | 1.11 mt – 3.6 ft |
| Max Seating capacity | 2 |
| Fuel tank capacity | 2 x 50 lt – 2 x 13.2 US Gal |
Powerplant
| Engine Manufacturer | ROTAX 912 S2 |
| Engine Power | 98 HP |
| Time Before Overhaul | 2000 hrs |
| Propeller | Two-Bladed Fixed Pitch |
| Fuel Consumption | 17 lt/h – 4.50 US Gal/h |
| Fuel Type | Mogas and Avgas |
Design Weight & Loading
| Maximum Take Off Weight | 600 kg – 1323 lb |
| Empty Weight, Standard | 370 kg – 816 lb |
| Useful Load | 230 kg – 507 lb |
| Baggage allowance | 20 kg – 44 lb |
Performance
| Max Cruise Speed (KTAS) | 219 km/h – 118 kts |
| Stall Speed (Flaps Down Power Off) KCAS | 72 km/h – 39 kts |
| Practical ceiling | 4267 mt – 14,000 ft |
| Take off run | 190 mt – 623 ft |
| Take off distance | 370 mt – 1213 ft |
| Landing Run | 120 mt – 394 ft |
| Landing Distance | 302 mt – 990 ft |
| Rate of climb | 1010 ft/min – 5,13 m/sec |
| Range | 469 NM – 869 km |
| Flight Rule | VFR Day |