P92 JS De Luxe - LY CS VLA
P92 JS De Luxe - LY SPECIFICATIONS The P92-JS is a two-seater side by side, single strut braced, high wing aircraft. The aircraft’s outstanding performance and flying qualities together with low operating costs, easy piloting and maintenance, make this aircraft an excellent choice for flying schools and training activities and also for many other missions such as touring, territory surveillance, patrol, etc. The option to use AVGAS 100LL or unleaded MOGAS ASTM D4814-EN/228 SUPER make the P92 JS even more flexible and economical. The P92-JS has been type certified in December 2001 in compliance with CS-VLA. The engine and propeller are certified to FAR 33. Several well known research institutes have chosen the JS as a platform for research into automated systems for conducting flight and environmental research and are very satisfied with it.
P92JS DE LUXE
Number of Cylinders
PROPELLER Manufacturer Model Type
r Superior performance and flight characteristics r Low stall speed r Stable and responsive r Ideal for flight schools r High level of comfort that makes it ideal for long routes r Excellent visibility r Comfortable 45 in/114 cm wide cabin r JAR-VLA certified
FIX PITCH - WOOD
FIX PITCH - WOOD
DESIGN WEIGHT & LOADING MTOW
Standard Equip. Empty Weight
Standard Equip. Useful Weight
Number of Blades
+3,8 / -1,9 G
+5,7 / -2,85 G
DIMENSION 2,5 6,4 8,7 1,11 0,91 45
Fuselage Height Fuselage Length Wing Span Cabin Width Cabin Height SEAT TO COVER Fuel Tank Capacity
m m m m m X2 lt
8,2 21 28,5 3,6 3 11,2
15°C SEA LEVEL 600 KG / 1320 LB
VMAX Cruise Speed 75% VNE Stall Speed FLAPS DOWN POWER OFF Pratical Ceiling Takeoff Run Takeoff Distance Landing Run Landing Distance Rate of Climb Range
222 200 261 76 4572 120 250 120 302 5,6
km/h km/h km/h km/h m m m m m m/sec
120 108 141 41 15000 394 820 394 991 1100
ft ft ft ft ft X2 GAL
15°C SEA LEVEL 630 KG / 1388 LB
KTS 240 KTS 220 KTS 261 KTS 78 ft 4400 ft 190 ft 295 ft 170 ft 350 ft/min 6,1 493 N.M.
km/h km/h km/h km/h m m m m m m/sec
130 118 141 42 14500 625 970 560 1150 1200
KTS KTS KTS KTS ft ft ft ft ft ft/min
r The Tecnam line employs a monocoque tail cone section with the forward fuselage using sheet aluminium
r Seats are adjustable and increase in height as they are
over steel tubing. r The wing is an all aluminium conventional structure with a single strut. r The top and bottom engine cowls are quickly and easily removable making any maintenance easier to accomplish. The top cowl has 2 large hinged openings for easy access to the engine compartment, without the need for tools to allow effective pre-flight inspections. r The top and bottom engine cowls are quickly and easily removable making any maintenance easier to accomplish. The top cowl has 2 large hinged openings for easy access to the engine compartment, without the need for tools to allow effective pre-flight inspections. r The fuel tanks hold 11.2 GAL/45 lt each, located in the wing leading edge separated from the fuselage for safety. r A wide rear window together with large side windows complete the extraordinary visibility allowing 360째 of vision in the cockpit. r The all moving Stabilator is fitted with a trim tab controlled by buttons on the control column. r The excellent flying characteristic with neutral handling makes it extremely stable and easy to fly for people of any weight/height. r The large flaps are deployed electrically and allow a stall speed lower than 41 KTS (76 km/h). r The low stall speed and the general slow flying characteristics of the aircraft allows it to operate with ease on short runways.
r The luggage area allowing for 44 pounds/20 kg of weight is located behind the seats with easy access in flight.
r All Tecnam aircraft have dual control sticks, throttles and rudder pedals. r The trim tab and the flaps are electrically activated with a position indicator on the instrument panel.
r The fresh air vents are conveniently located in the doors. r Heat and defrost are standard. r The aircraft has dual conventional rudder pedals with a steerable nose wheel. r The wide conventional instrument panel allows fitment of a broad range of IFR equipment, in addition to standard VFR training requirements.
r The interior is spacious, ergonomic and comfortable.
LANDING GEAR r The main landing gear legs are made of spring steel, directly connected to the main structure. The landing gear is robust enough for rough strips and require no maintenance.
r The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment with easy and economical maintenance.
r The main landing gear wheels and brakes are conventional aircraft size (5.00x5) r The brake lever control and the parking brake are located forward between the seats.
STANDARD EQUIPMENT FLIGHT INSTRUMENTS AND INDICATORS 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
ENGINE INSTRUMENTS Rpm Indicator Hour Recorder Oil Press Oil Temp. Head Temp. Fuel Press. Voltmeter Ammeter Lh + Rh Fuel Qty
OTHER INSTRUMENTS / WARNING Chronometer O.A.T. Indicator
Generator Warning Light Vacuum Suction Gauge
FLIGHT CONTROLS 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 with On/Off Panel Switches: - Starter - Fuel Pump - Engine Lh And Rh Ignition Switches
Two Integral Fuel Tanks with 100 Lt Tot Capacity Engine Driven Fuel Pump Auxiliary Fuel Pumps, Electric Fuel Quick Drain
INTERIOR Pilot and Copilot Seats - Adjustable Fore And Aft Seat Belts & Shoulder Harness, All Seats Wall To Wall Carpeting Luggage Compartments Fire Extinguisher Radio Call Plate Soundproofing First Aid Kit
EXTERIOR ELECTRICAL SYSTEM 12 Volt 18a Amp. Battery Switches - Nav. Lights - Landing Light - Strobe Light External Power Supply Receptable Circuit Breaker Panel
Epoxy Corrosion Proofing, All Structure Two Doors With Lock And Key (Only Lh) Rear Window Tie Down RIngs Main Wheels, 5,00 X 5 Nose Wheel, 4,00 X 6
EXTERIOR LIGHTS Nav. Lights Vertical Tail Strobe Taxi Light
CABIN CONFORT SYSTEM Windshield Defroster Ventilator Adjustable, 2 Place Heating System Ventilator Adjustable, 2 Place
POWERPLANT AND PROPELLER Option I Rotax 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 12 Volt Alternators 20 Amp. Option II Lycoming Engine 1 Lycoming Yo233b2a 115 Hp, 4 Cylinders Direct Drive Dual Ignition System Throttle Control Tubular Steel Engine Mount Propeller Gt 2 Blade Fix Propeller Spinner Air Filter Oil Filter Oil Cooler Carburetor Heat with Manual Control Thermostat Valve 12 Volt Alternators 60 Amp.
PRODUCT SUPPORT/DOCUMENTS Manufacturers Full Two Year Limited Warranty Pilots Operation Handbook Maintenance Manual Parts Catalog Aircraft Log Book Engine Log Book
COSTRUZIONI AERONAUTICHE TECNAM S.R.L. Costruzioni Aeronautiche Tecnam operates in two facilities. The Casoria facility is located adjacent to the Napoli Capodichino Airport and covers an area of about 12.000 sqm with about 4.000 sqm of enclosed facilities. The Capua facility is located adjacent to the “Oreste Salomone” Airport, covers an area of about 45.000 sqm with about 11.000 sqm of enclosed facilities.
TEL.+39 0823 620134
081043 CAPUA (CE) ITALY
FAX +39 0823 622899
CAPUA PLANT P2006T LINE PRODUCTION