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SPECIFICATION and DESCRIPTION P92JS Introduction

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SPECIFICATION and DESCRIPTION P92JS Introduction P92JS SPECIFICATION AND DESCRIPTION P92JS Introduction SPECIFICATION AND DESCRIPTION P92JS This document applies only to the Tecnam P92JS and is published for the purpose of providing general information for the evaluation of design, powerplant, performance and equipment. Should more information be required, please contact: Costruzioni Aeronautiche Tecnam srl Via Maiorise 81043 Capua CE -Italy Tel. +39 0823 622297 Fax. +39 0823 622899 www.tecnam.com [email protected] http://www.tecnam.com/aircraft/p92-js/ Pascale Museum at Tecnam Headquarter Capua All information here applies to the Tecnam model P92JS equipped with the Rotax 912 S2 engine. 2 P92JS Introduction GENERAL DESCRIPTION General description The all moving Stabilator is fitted with a trim tab Landing Gear controlled by buttons on the control column. The The P92-JS is a two-seater side by side, single excellent flying characteristic with neutral handling The main landing gear is spring steel that is robust strut braced, high wing aircraft. The aircraft’s makes it extremely stable and easy to fly for people enough for unimproved strips and requires no outstanding performance and flying qualities of any weight/height. The large flaps are deployed service. The trailing link nose gear uses a rubber together with low operating costs, easy piloting electrically and allow a stall speed lower than shock absorber system that was designed for the and maintenance, make this aircraft an excellent 41 KTS (76 km/h). The low stall speed and the rigours of the training environment. choice for flying schools and training activities general slow flying characteristics of the aircraft The main landing gear wheels and brakes are and also for many other missions such as touring, allows it to operate with ease on short runways. conventional aircraft size (5.00x5). The brake territory surveillance, patrol, etc. control is located forward between seats. A parking The option to use AVGAS 100LL or unleaded Interior brake is between the seats and is actuated by use MOGAS ASTM D4814-EN/228 SUPER make the of a single twist. P92 JS even more flexible and economical. Seats are adjustable and increase in height as they The P92-JS was type certified in December 2001 are moved forward. The luggage area allowing Powerplant and propeller in compliance with CS-VLA. The engine and for 44 pounds/20 kg of weight is located behind propeller are certified to FAR 33. the seats with easy access in flight. All Tecnam The top and bottom engine cowls are quickly aircraft have dual control sticks, rudder pedals. and easily removable making any maintenance Construction The trim tab and the flaps are electrically activated procedure faster to accomplish. The top cowl with a position indicator on the instrument panel. has 2 large hinged openings for easy access to The Tecnam production line employs a monocoque The fresh air vents are conveniently located in the engine compartment for effective pre-flight tail cone section with the forward fuselage using the doors. Heat and defrost are standard. The inspections. sheet aluminum over steel tubing. The wing is an aircraft has dual conventional rudder pedals with The engine is set low and the cowling slopes all aluminum conventional structure with a single a steerable nose wheel. The wide conventional down from the windshield, so forward visibility is strut. The top and bottom engine cowls are quickly instrument panel allows fitment of a broad range excellent. The steel firewall is soundproofed. The and easily removable making any maintenance equipment, in addition to standard VFR training power plant is a Rotax 912S2 series four-cylinder, easier to accomplish. A wide rear window together requirements. The interior is spacious, ergonomic four- stroke engine. with large side windows complete the extraordinary and comfortable. The engine is liquid and air cooled with an visibility allowing 360° of vision in the cockpit. integrated 1:2.4286 reduction gear. The use of All information here applies to the Tecnam model P92JS equipped with the Rotax 912 S2 engine. 3 P92JS Introduction Baggage Compartment Cabin Width 2.62 ft 0,80 m ft m liquid cooled heads and air cooled cylinders allows Height 2.95 0,90 the engine to maintain safe operating temperatures Length 1.48 ft 0,45 m even if a rapid descent is performed immediately Max. permissible load 44lb 20kg Width 3.6 1,1 after a prolonged climb. An electrical fuel pump is installed to provide an effective back-up to the mechanical one. Circuit breakers are standard. The battery is located in the rear of the fuselage with easy access through an external hinged door. An external power socket allows for engine start, tests, and avionics management/training without the use of internal battery. A fixed pitch wood, composite wrapped Hoffmann propeller comes standard while the hydraulic variable pitch propeller from Hoffman is also available as an option. All information here applies to the Tecnam model P92JS equipped with the Rotax 912 S2 engine. 4 P92JS Views 5 P92JS Weight & Performance DIMENSIONS Wing ft m Dimensions ft m Span 28.5 8,7 Height 8.2 2,5 Area 129 ft2 12 m2 Length 21 6,4 Dihedral 1.5° Aspect ratio 6.31 P92JS DESIGN WEIGHT AND LOADING kg lb Maximum Take Off Weight 600 1,320 Empty Weight, Standard 370 815 Useful Load 230 507 Baggage allowance 20 44 P92JS PERFORMANCE Fixed Propeller Max Cruise Speed KTAS 118 kts 219 km/h Stall Speed (Flaps Down Power Off) KCAS 39 kts 72 km/h Practical ceiling 14000 ft 4267 m Take off run 623 ft 190 m Take off distance 1213 ft 370 m Landing Run 394 ft 120 m Landing Distance 990 ft 302 m Rate of climb 1010 ft/min 5,13 m/sec Range 469 NM 869 km 6 All estimated performance data are based on aeroplane weights at MTOW; standard atmospheric conditions; level, hard surface, dry runways, no wind. P92JS Standard STANDARD EQUIPMENT FLIGHT INSTRUMENTS and INDICATORS FLIGHT CONTROLS FUEL SYSTEM Magnetic Compass Hydraulic Hand Brakes Two Integral Fuel Tanks with 100 Litres Total Airspeed Ind., Kts Parking Brake Capacity Altimeter (In) Electrical Flaps Vertical Speed Dual Flight Controls Engine Driven Fuel Pump Attitude Gyro Steerable Nose Wheel Auxiliary Fuel Pump, Electric Directional Gyro Stabilator Trim (electric actuated from stick) Fuel Quick Drain Turn And Slip Indicator Engine Controls Flaps Indicator _ Throttle, Two INTERIOR Pitot System _ Carburettor Heat Pilot And Copilot Seats Static System _ Choke _ Adjustable Fore and Aft Stabilator Trim Position Indicator Flight Trim Controls Seat Belts & Shoulder Harness, all Seats _ Stabilator with Indicator wall to wall Carpeting ENGINE INSTRUMENTS Fuel Control Selector with On/Off Luggage Compartment RPM Indicator Fire Extinguisher Hour Recorder Panel Switches: Radio Call Plate Oil Press _ Starter Soundproofing Oil Temp. _ Fuel Pump First Aid Kit Coolant Temp. _ Engine LH And RH Ignition Switches Fuel Press. EXTERIOR Voltmeter ELECTRICAL SYSTEM Epoxy Corrosion Proofing, all Structure Ammeter 12 VOLT 18A AMP. Battery Two Doors with Lock and Key (Only LH) LH+ RH Fuel Q.ty 12 VOLT Alternator - 20 AMP. Rear Window Switches: Tie Down Rings OTHER INSTRUMENTS / WARNING _Nav. Lights Main Wheels, 5,00 X 5 Chronometer _Landing Light Nose Wheel, 5,00 X 5 O.A.T. Indicator _Strobe Light Generator Warning Light External Power Supply Receptical Vacuum Suction Gauge Circuit Breaker Panel 7 P92JS Standard EXTERIOR LIGHTS Propeller - Hoffmann, 2 Blade Fixed Pitch STANDARD GARMIN AVIONICS PACKAGE Nav. Lights LED with strobe Aveo full LED TSO Propeller Spinner GMA 340 Audio Panel Taxi Light LED Air Filter GNC 255A COM/NAV Oil Filter GTX 335 Transponder ADS-B OUT CABIN COMFORT SYSTEM Oil And Water Coolers ELT 406 Mhz KANNAD Windshield Defroster Carburettor Heat with Manual Control Antennas: Ventilator adjustable, 2 Place Thermostat Valves Oil And Water - Transponder Heating System - VHF PRODUCT SUPPORT/DOCUMENTS - Marker Beacon POWERPLANT AND PROPELLER Manufacturers Full Two Year Limited Warranty - ELT ENGINE - 1 ROTAX 912S2 100 HP, 4 Cylinders Pilots Operation Handbook Speakers liquid/air cooled, integrated reduction gear Maintenance Manual Microphone Dual Ignition System Parts Catalog Stick Push-To-Talk Switch-Pilot/Copilot Throttle Control LH/RH Aircraft Log Book Mic & Phone Jacks-Pilot/Copilot Tubular Steel Engine Mount Engine Log Book ROTAX 912 S2 • 4-cylinders • 4-stroke liquid-/air-cooled engine with opposed cylinders • Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet • Mechanical fuel pump • Dual electronic ignition • Air intake system • Gearbox Reduction Ratio 2,43:1 8 P92JS Standard STANDARD AVIONICS STANDARD GARMIN AVIONIC PACKAGE • 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 Empty Weight 389 kg 9 P92JS Paint PAINT SCHEMES Many colours options for your to choose: from base Standard livery to the Special Paint Two colours. More info on: colors.tecnam.com 10 P92JS OPTIONS Optional Extras Code Description INSTRUMENTS 114/A Turn & Slip Ind. 2 1/4” RADIO & NAVIGATION EQUIPMENTS GARMIN-COM/NAV/GPS 120/A GTR225 COM 25 Mhz with Antenna and Installation. 120/B GTR225A COM 8.33 Khz with Antenna and Installation. 119 MD200 VOR Indicator Only for GNC255A 121 GTN 650 Com/Nav/Gps with Antennas, Triplex and inst. With GI106A Ind. 121/A GTN 650 Com/Nav/Gps with Antennas, Triplex. & inst. With GI106A Ind.(Exch. for Std. GNC255A) 122 GTN 750 Com/Nav/Gps with Antennas, Triplex and inst. With GI106A Ind. 122/A GTN 750 Com/Nav/Gps with Antennas, Triplex & inst. With GI106A Ind.(Exch. for Std.
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