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.

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Quick facts

0NM

Max Range

With this range you can use it cross country.

118 kts

Max Cruise Speed

219 km/h

0

Seating

Two seats side by side,
Day VFR Flight Rule

17 l/h

Fuel Consumption

Only 4.5 US Gal  per hour,
AVGAS and MOGAS Automotive Fuel

Exterior

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.
Enjoy the P92!

Avionics

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

Standard Equipment

Flight instruments and indicators

Magnetic Compass
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/Warnings

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

Interiors

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

Product Support/Documents

Manufacturers Full Two Year Limited Warranty
Pilots Operation Handbook
Maintenance Manual
Parts Catalog
Aircraft Log Book
Engine Log Book

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

Exteriors 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

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

Paint Schemes

Optional Equipment

 

INSTRUMENTS

114/A Turn & Slip Ind. 2 1/4”

RADIO & NAVIGATION EQUIPMENT

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)

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

Other Equipment

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

Engine Equipment

201/A Special Paint Two Colours

Engine Equipment

187 Aux. Alternator

Specification

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

Specifications subject to change without notice. Always consult the Aircraft Flight Manual.

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