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.
Cere o oferta de pret!
The Tecnam line employs a monocoque construction style using sheet aluminium over steel tubing. The wing is all aluminium and constructed in a conventional way with a single spar and metal torsion box. The airfoil is a Gottinga 398 modified for better low speed handling characteristics. The standard fuel tanks hold 45 Lt. (11.9 gal) in each wing and are located in the leading edge separated from the fuselage for safety. A rear window completes the extraordinary visibility allowing 360 degre of vision in the cockpit. The stabilator provides remarkable longitudinal hands-off stability along with minimum drag and weight penalty providing balanced, 2 finger, flight control. The wide slotted flaps, electrically activated, allow stall speed lower than 38 Kts. The P92 JS has 35 degrees of flaps making steep approach landings easier.
Seats are adjustable in flight 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 ample room for several travel bags. All Tecnam aircraft have dual control sticks with a curve at the base for ease of ingress and egress. The dual controls come standard with PTT and electric stabilator trim on the stick with a trim indicator on the panel. The interior is spacious, ergonomic and comfortable. Dual throttles allow the pilot to fly either left or right handed. Heat and defrost are standard. The fresh air vents are conveniently located in the doors. All Tecnam aircraft provide excellent forward visibility over the cowling. The planes come with dual conventional rudder pedals with a steerable nose wheel. The wide conventional type instrument panel allows placement of a broad range of equipment.Enjoy the P92!
Magnetic Compass
Airspeed Ind., Kts
Altimeter (In)
Vertical Speed
Attitude Gyro
Directional Gyro
Turn And Bank Indicator
Flaps Indicator
Pitot System
Static System
Stabilator Trim Position Indicator
Rpm Indicator
Hour Recorder
Oil Press
Oil Temp.
Head Temp.
Fuel Press.
Voltmeter
Ammeter
Lh+Rh fuel qty
Chronometer
O.A.T. Indicator
Generator Warning Light
Vacuum Suction Gauge
Trim Indicator
Warning Light:
– Alt. Out
– Fuel Pump On
Hydraulic Brakes
Parking Brake
Electrical Flaps
Dual Flight Controls
Steerable Nose Wheel
Stabilator Trim (Electric Actuated From Stick)
Engine Controls
– Throttle, Two
– Carburetor Heat
– Choke
Flight Trim Controls
– Stabilator With Indicator
– Fuel Control Selector Andair
12 Volt 18A Amp. Battery
12 Volt Alternators-20 Amp.
Switches:
– Avionic Master
– Fuel Press
– Nav. Lights
– Landing Light
– Strobe Light
12 Volt Socket
External Power Supply Receptable
Circuit Breaker Panel
Two – Integral Fuel Tanks, 100 Lt Tot Capacity
Engine Driven Fuel Pump
Fuel Quick Drain
Auxiliary Fuel Pump, Electric
Fuel Selector Rh & Lh
Pilot And Copilot Seats
– Adjustable Fore And Aft
Seat Belts & Shoulder Harness, All Seats
Wall T – Wall Carpeting
Map E Storage Pockets
Luggage Compartments
Fire Extinguisher
Radi – Call Plate
Soundproofing
First Aid Kit
Emergency Hammer
Manufacturer's Full Two – Year Limited Warranty
Pilot's Operation Handbook
Maintenance Manual
Parts Catalog
?Aircraft Log Book
Engine Log Book
Epoxy Corrosion Proofing, All Structure
Lh/Rh Front Door Pilot/Copilot With Lock And Key
Rear Window
Tie Down Rings
Main Wheels, 5,00 X 5 Cleveland
Nose Wheel, 5,00 X 5
Stall Warning
Nav. Lights Led With Strobe Ave – Full Led Tso
Taxi Light Led
Windshield Defroster
Ventilator Adjustable 2 Place
Heating System
Engine – 1 Rotax 912S2 100 Hp, 4 Cylinders
Liquid/Air Cooled, Integrated Reduction Gear
Dual Ignition System
Throttle Control Lh/Rh
Tubular Steel Engine Mount
Propeller – Hoffmann, 2 Blade Fix
Propeller Spinner
Air Filter
Oil Filter
Oil And Water Coolers
Carburetor Heat With Manual Control
Thermostat Valve
Gma 340 Audi – Panel
Gnc 255A Com/Nav
Gtx 328 Tdx
Elt 406 Mhz
Antennas:
– Transponder
– Vhf
– Elt
– Marker Bacon
Speakers
Microphone
Stick Push-To-Talk Switch-Pilot/Copilot
Mic& Phone Jacks-Pilot/Copilot
GMA 35 Audio Panel with Antenna and inst. Only for GTN750 Exchange for Std. GMA340)
MD200 VOR Indicator Only for GNC255A
GARMIN GTR225A Com 8.33 Khz with Ant. & Inst. (From Nov. 2013 mandatory for EU)
GARMIN GTR225A COM 8.33 Khz with Antenna and Inst. (Exch for Standard GNC255A)
GTN 650 Com/Nav/Gps with Antennas, Triplex and inst. With GI106A Ind.
GTN 650 Com/Nav/Gps with Antennas, Triplex. & inst. With GI106A Ind.(Exch. for Std. GNC255A)
GTN 750 Com/Nav/Gps with Antennas, Triplex and inst. With GI106A Ind.
GTN 750 Com/Nav/Gps with Antennas, Triplex & inst. With GI106A Ind.(Exch for Std. GNC255A)
GTX 330 Transponder mode S with Antenna and Inst. Exchange for Std. GTX23)
GTX 330 Transponder mode S with Antenna and Inst. Exchange for Std. GTX328)
GTX 33 Transponder mode S remote mounted with Antenna and Inst. (Requires option 122)
GTX 33 Transponder mode S remote mounted with Ant. and Inst. (Requires option 122) Exch. For Std. GTX328
RA3502 ADF with AN3500 Indicator
KR 87 ADF with KI227 Indicator
DME KN63-14
Two Head Sets
BOSE A 20 Two Head Sets
Tinted Windows
Toe Brakes
Central Quadrant with single throttle level (requires Toe Brakes opt. 176)
Fuselage Cover
Spinner Polished Alluminum Look
Battery Gill G25 (Exchange for standard battery)
Special paint two colors
Aux alternator
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 45 lt – 2 x 11.9 US Gal |
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 |
Maximum Take Off Weight | 600 kg – 1320 lb |
Std. Empty Weight | 350 kg – 771 lb |
Useful Load | 250 kg – 551 lb |
Baggage allowance | 20 kg – 44 lb |
Vmax | 222 km/h – 120 kts |
Cruise Speed 75% | 200 km/h – 108 kts |
Stall Speed (Flaps Down Power Off) | 76 km/h – 41 kts |
Pratical ceiling | 4572 mt – 15,000 ft |
Take off run | 120 mt – 394 ft |
Take off distance | 250 mt – 820 ft |
Landing Run | 120 mt – 394 ft |
Landing Distance | 302 mt – 991 ft |
Rate of climb | 5.1 m/sec – 1000 ft/min |
Range | 493 NM |
Flight Rule | VFR Day |