SPECIFICATION AND DESCRIPTION
TECNAM P92-JS · Pilot's Operating Handbook
Overview
The document provides specifications and descriptions for the Tecnam P92-JS aircraft, which is equipped with the Rotax 912 S2 engine. It covers general information about the aircraft's design, performance, and equipment, making it suitable for various missions including training and touring.
- The P92-JS is a two-seater, high wing aircraft.
- It features low operating costs and is easy to maintain.
- The aircraft can use AVGAS 100LL or unleaded MOGAS.
- Type certified in December 2001 under CS-VLA.
- The aircraft has a maximum takeoff weight of 600 kg.
- Stall speed is lower than 41 KTS.
- It has a practical ceiling of 14,000 ft.
- The interior is spacious and ergonomic.
Document
Source
Originally published by tecnam.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Pilot's Operating Handbook
- File size ·
- 657 KB
- Publisher ·
- tecnam.com
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Height (ft) ·
- 8.2
- Length (ft) ·
- 21
- Wing span (ft) ·
- 28.5
- Max baggage load (lb) ·
- 44
- Baggage compartment width (ft) ·
- 2.62
- Baggage compartment length (ft) ·
- 1.48
Performance
- Range (nm) ·
- 469
- Landing run (ft) ·
- 394
- Takeoff run (ft) ·
- 623
- Empty weight kg ·
- 370
- Stall speed kcas ·
- 39
- Max cruise speed (kt) ·
- 118
- Practical ceiling (ft) ·
- 14000
- Max takeoff weight kg ·
- 600
- Rate of climb ft per min ·
- 1010
V-speeds
- VSO_KTS ·
- 39
Weight & balance
- Useful load kg ·
- 230
- Empty weight kg ·
- 370
- Baggage allowance kg ·
- 20
- Max takeoff weight kg ·
- 600
What is the SPECIFICATION AND DESCRIPTION?
The SPECIFICATION AND DESCRIPTION is a pilot's operating handbook for the TECNAM P92-JS.
Where does the SPECIFICATION AND DESCRIPTION come from?
This copy of the SPECIFICATION AND DESCRIPTION was originally published by tecnam.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the TECNAM P92-JS.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More TECNAM P92-JSmanuals & documents
In this document
General Description
The P92-JS is designed for training and various missions, featuring excellent performance and low operating costs.
Construction
The aircraft uses a monocoque tail cone and aluminum structure, with easy maintenance features.
Powerplant and Propeller
Equipped with a Rotax 912S2 engine, the aircraft has excellent visibility and easy access for maintenance.
Performance
Performance data includes a maximum cruise speed of 118 KTAS and a range of 469 NM.
Standard Equipment
Includes flight instruments, dual controls, and a standard Garmin avionics package.
Optional Extras
Various options for instruments and equipment are available to customize the aircraft.
Full document text
P92JS SPECIFICATION AND DESCRIPTION P92JS 2 Introduction All information here applies to the Tecnam model P92JS equipped with the Rotax 912 S2 engine. P92JS SPECIFICATION AND DESCRIPTION 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. http://www.tecnam.com/aircraft/p92-js/ 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 info@tecnam.com Pascale Museum at Tecnam Headquarter Capua P92JS 3 Introduction All information here applies to the Tecnam model P92JS equipped with the Rotax 912 S2 engine. GENERAL DESCRIPTION General description 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 was type certified in December 2001 in compliance with CS-VLA. The engine and propeller are certified to FAR 33. Construction 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. 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. Landing Gear The main landing gear is spring steel that is robust enough for unimproved strips and requires no service. The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment. The main landing gear wheels and brakes are conventional aircraft size (5.00x5). The brake control is located forward between seats. A parking brake is between the seats and is actuated by use of a single twist. Powerplant and propeller The top and bottom engine cowls are quickly and easily removable making any maintenance procedure faster to accomplish. The top cowl has 2 large hinged openings for easy access to the engine compartment for effective pre-flight inspections. The engine is set low and the cowling slopes down from the windshield, so forward visibility is excellent. The steel firewall is soundproofed. The power plant is a Rotax 912S2 series four-cylinder, four- stroke engine. The engine is liquid and air cooled with an integrated 1:2.4286 reduction gear. The use of P92JS 4 Introduction All information here applies to the Tecnam model P92JS equipped with the Rotax 912 S2 engine. liquid cooled heads and air cooled cylinders allows the engine to maintain safe operating temperatures even if a rapid descent is performed immediately 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. Cabin ft m Height 2.95 0,90 Width 3.6 1,1 Baggage Compartment Width 2.62 ft 0,80 m Length 1.48 ft 0,45 m Max. permissible load 44lb 20kg P92JS 5 Views P92JS 6 Weight & Performance PERFORMANCE All estimated performance data are based on aeroplane weights at MTOW; standard atmospheric conditions; level, hard surface, dry runways, no wind. P92JS kg lb Maximum Take Off Weight 600 1,320 Empty Weight, Standard 370 815 Useful Load 230 507 Baggage allowance 20 44 P92JS 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 Dimensions ft m Height 8.2 2,5 Length 21 6,4 Wing ft m Span 28.5 8,7 Area 129 ft 2 12 m 2 Dihedral 1.5° Aspect ratio 6.31 DIMENSIONS DESIGN WEIGHT AND LOADING P92JS 7 Standard STANDARD EQUIPMENT FLIGHT INSTRUMENTS and INDICATORS Magnetic Compass
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Airspeed Ind., Kts Altimeter (In) Vertical Speed Attitude Gyro Directional Gyro Turn And Slip Indicator Flaps Indicator Pitot System Static System Stabilator Trim Position Indicator ENGINE INSTRUMENTS RPM Indicator Hour Recorder Oil Press Oil Temp. Coolant Temp. Fuel Press. Voltmeter Ammeter LH+ RH Fuel Q.ty OTHER INSTRUMENTS / WARNING Chronometer O.A.T. Indicator Generator Warning Light Vacuum Suction Gauge FLIGHT CONTROLS Hydraulic Hand Brakes Parking Brake Electrical Flaps Dual Flight Controls Steerable Nose Wheel Stabilator Trim (electric actuated from stick) Engine Controls _ Throttle, Two _ Carburettor 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 ELECTRICAL SYSTEM 12 VOLT 18A AMP. Battery 12 VOLT Alternator - 20 AMP. Switches: _Nav. Lights _Landing Light _Strobe Light External Power Supply Receptical Circuit Breaker Panel FUEL SYSTEM Two Integral Fuel Tanks with 100 Litres Total Capacity Engine Driven Fuel Pump Auxiliary Fuel Pump, Electric Fuel Quick Drain INTERIOR Pilot And Copilot Seats _ Adjustable Fore and Aft Seat Belts & Shoulder Harness, all Seats wall to wall Carpeting Luggage Compartment Fire Extinguisher Radio Call Plate Soundproofing First Aid Kit EXTERIOR 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, 5,00 X 5 P92JS 8 Standard EXTERIOR LIGHTS Nav. Lights LED with strobe Aveo full LED TSO Taxi Light LED CABIN COMFORT SYSTEM Windshield Defroster Ventilator adjustable, 2 Place Heating System POWERPLANT AND PROPELLER 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 Fixed Pitch Propeller Spinner Air Filter Oil Filter Oil And Water Coolers Carburettor Heat with Manual Control Thermostat Valves Oil And Water PRODUCT SUPPORT/DOCUMENTS Manufacturers Full Two Year Limited Warranty Pilots Operation Handbook Maintenance Manual Parts Catalog Aircraft Log Book Engine Log Book STANDARD GARMIN AVIONICS 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 • 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 ROTAX 912 S2 P92JS 9 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 P92JS 10 PAINT SCHEMES Paint Many colours options for your to choose: from base Standard livery to the Special Paint Two colours. More info on: colors.tecnam.com P92JS 11 Optional ExtrasOPTIONS 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. GNC255A) RADIO & NAVIGATION EQUIPMENT GARMIN-GPS 128 AERA 500 with Antenna, Panel Support and Installation 132 795 with Antenna, Panel Support and Installation BENDIX KING 137 KR 87 ADF with KI227 Indicator 139 DME KN63-14 with KDI 572 Indicator OTHERS 157 Head Sets, Two 157/A BOSE A 20 Head Sets, Two AIRCRAFT EQUIPMENT 174 Tinted Windows 176 Toe Brakes (see note #1) 178 Central Quadrant with single throttle lever 182 Fuselage Cover 185 Battery Gill G25 (Exchange for standard battery) 209 Control Lock 210 Towing Bar EXTERIOR 201/A Special Paint Two Colours ENGINE and PROPELLER EQUIPMENT 187 Aux. Alternator #1 - 176 TOE BRAKES includes: • New Pedals • 4 Brakes Pumps • Parking Brake Selector Costruzioni Aeronautiche Tecnam srl Via Maiorise 81043 Capua CE - Italy Tel. +39 0823 622297 Fax. +39 0823 622899 www.tecnam.com info@tecnam.com http://www.tecnam.com/aircraft/p92-js/ 17050819