p2002 jr

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P2002 JR CS VLA CERTIFIED

8/8/2019 P2002 jr


P2002 JR The P2002-JR is a two-seater side by side, low wing aircra t with retractablelanding gear. The P2002-JR eatures superlative per ormance and lying qualities,now con irmed by hundreds o P2002’s and P2002 RG’s

lying all over the world. The ease o piloting and maintenance make this aircra tan excellent solution or training with light schools but also an ideal plat orm orsurveillance and patrolling territory as well as, o course, or pure recreationaltourism.

The option to use AVGAS 100LL or unleaded MOGAS ASTM D4814-EN/228SUPER make the P2002 JR even more lexible and economical.The P2002-JR represents the latest development o the Tecnam aircra t as resulto the aircra t’s continued improvement, the use o advanced so tware or designwith structural and luidynamic analysis.

Thanks to the tapered wing, the laminar air oils, the slotted laps and the streamlineuselage together with the retractable gear, the P2002-JR is an outstanding

aircra t, with the per ect mix o aerodynamic and structural e iciency.

AdvAntAges• Superior per ormance and light characteristics• Low stall speed• 226 KM/H (122 KTS) cruise• Stable and responsive• High level o com ort that makes it ideal or long routes

• Excellent visibility• Sliding canopy can be opened in light• Exciting, yet easy to ly• EASA CS-VLA certi ied• Ideal or light schools

specificAtionsdesign WeigHt & LoAding Kg LB

Maximum Take-o Weight MTOW 62 1370

Standard Equipped Weight 39 0 8 60

Standard Use ul Load 230 510

Ultimate Loads +5.7 / -2.9 G

Baggage Allowance 20 44

diMension

Wing

Wing Span 8,6 m 28,2 ftWing Area 11,5 m² 124 sqftfuseLAge M ft

Length 6,63 21,7Height 2 ,4 7, 9engine

Manu acturer RotaxModel 912 s3Power 100 hpNumber o Cylinders 4pRopeLLeR

Manu acturer hoffmann

Model hoV352Number o Blades 2

Type V.p.

peRfoRMAnce MtoW 450Kg/990 LB

speed KM/H Kts

Maximum at Sea Level, Gross Weight 25 0 135Cruise, 75% power 2 26 122

Vne 267 14 4stALL speed

Flaps up, power o 83 45Flaps Down, power o 72 39Service Ceiling 4500 m 14,800 ftRate o Climb at Sea level 1200 ft/m

tAKeoff peRfoRMAnce M ftGround roll 15 0 79 2ToT. over 50 r obstacle 350 1150LAnding peRfoRMAnce

Ground roll 142 4 66Tot. over 50 r obstacle 326 1070fueL

Fuel Tank Capacity 50 x2 lt 13,2 x2 Gal

CS VLA CERTIFIED

8/8/2019 P2002 jr


constRuction• The Tecnam line employs a monocoque tail cone section with sheet aluminium over steel tubing or the

orward section.• The aluminium tapered wing has a conventional structure with a orward load bear ing spar and a conventional

rear spar. The wing halves are attached to the uselage by a very strong carry-through made o 2024-T3grade aluminium ixed to the cabin truss.

• The uel tanks hold 13.2 gal/50l each, located in the wing leading edges separated rom the uselage orsa ety.

• The sliding canopy allows 360° o vision in the cockpit. This canopy can be ully opened in light below 70knots.

• The all moving Stabilator is itted with a trim tab controlled by buttons on the control column.• The excellent lying characteristic with neutral handling makes it extremely stable and easy to ly or people

o any weight/height.• The ailerons are e ective in allowing or a quick roll rate without being overly sensitive.• All control sur aces are made out o aluminium.• The wide slotted laps, electrically activated, allow stall speed lower than 73 km/h (40 Kts).• The canopy has ull rollover protection.

inteRioR• Seats are adjustable and increase in height as they are moved orward.• The luggage area allowing or 44 pounds/20 kg o weight, located behind the seats with ample room or

several travel bags• All Tecnam aircra t have dual control sticks with a curve at the base or ease o ingress and egress.• The dual controls come standard with PTT and electric stabilator trim on both sticks with a trim indicator

on the panel.• The resh air vents are conveniently located on each side o the panel.• Heat and de rost are standard.• The aircra t comes with dual rudder pedals, connected to a steerable nose wheel.• The interior is spacious, ergonomic and com ortable.• Cabin is a roomy 44 in/112 cm wide.

• The wide conventional type instrument panel allows placement o a broad range o equipment, in additionto standard VFR training.

• Four point harness system is standard

LAnding geAR• The main landing gear is aluminium alloy with a rubber shock absorber system that is robust enough or

rough strips. Retraction is by three hydraulic cylinders.• The trailing link nose gear uses an oleo-pneumatic shock absorber that provides excellent ground load

absorption. The same system is used on the certi ied P2006.• A hydraulic Parker pump pressurises the system. In case o ailure o the electro/hydraulic system, there

is an emergency circuit with an independent tank which is constantly monitored. Should there be a totalailure, the landing gear will drop under gravity.

• The main landing gear wheels and brakes are conventional aircra t size (5.00x5).• The brake lever control and the parking brake are located orward between the seats.

engine And pRopeLLeR• 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 or easy access to the engine compartment, withoutthe need or tools to allow e ective pre- light inspections.

• The engine’s mount is steel-tubing with shock mounts It also supports the nose wheel, while the retractioncylinder is anchored to the main uselage structure.

• The power plant is a Rotax 912 S2 series certi ied to FAR 33 our-cylinder, ourstroke engine.• The engine employs liquid and air cooling with an integrated 1:2.4286 reduction gear.• A constant speed wood and composite Ho mann propeller certi ied to FAR 33 comes as standard.• The quick drain gascolator is installed in the engine compartment with easy outside access.• Drain taps are itted to the underside o the wings to purge the tanks.• Circuit breakers are standard.• The battery is located in the rear o the uselage with easy access through a hinged door. There is also an

external power socket.

CS VLA CERTIFIED

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ZaragoZa plant

COSTRUZIONI AERONAUTICHE TECNAM S.R.L.Costruzioni Aeronautiche Tecnam operates in three acilities. The Casoria acility is located adjacent to the Napoli Capodichino Airport and covers an area o 10.8000 sq t with 43.100 sq t o enclosed acilities. The Capua

acility is located adjacent to the “Oreste Salomone” Airport, covers an area o 12.9000 sq t with 43.100 sq t o enclosed acilities. Capua has already a new area o 38.7000 sq t with 64.600 sq t o enclosed acilities.This extension will double the production capacity o the Capua plant. Modern rein orced concrete buildings are used or manu acturing processes, design activities and o ice administration. And inally the TECNAM Spain

acility located in Villanueva del Gallego, Zaragoza - Spain covers an area o 16.404 sq t with 65.661 sq t o enclosed acilities with a runway adjacent o 3.937 length/ t.

CS VLA CERTIFIED VIa MaIorISE

081043 CapUa (CE) ItalY

tEl.+39 0823 620134

FaX +39 0823 622899

WWW.tECnaM.CoM

[email protected]

CaSorIa plantCapUa plant

stAndARd equipMent

fLigHt instRuMentsAnd indicAtoRsMagnetic Compass

Airspeed Ind., Kts Altimeter (In) Vertical Speed Attitude Electric GyroDirectional Electric GyroTurn And Bank IndicatorFlaps IndicatorPitot SystemStatic SystemStabilator Trim

Position Indicator

engine instRuMents

Rpm IndicatorHour RecorderOil Press.Oil Temp.Head Temp.Fuel Press.

Voltmeter AmmeterMani old PressureLh + Rh Fuel Qty

otHeR instRuMents / WARning

ChronometerO.A.T. IndicatorGenerator Warning Light

fLigHt contRoLs

Hydraulic BrakesParking BrakeElectrical FlapsDual Flight ControlsSteerable Nose WheelStabilator Trim

(Electric Actuated From Stick)Engine Controls- Throttle, Two- Carburetor Heat- ChokeLanding Gear:- Retractable Electrohydraulic- Selector Switch- Warning Horn- Emergency ExtensionFlight Trim Controls:- Stabilator With Indicator

Fuel Control SelectorWith On/O

Panel Switches:- Starter- Fuel Pump- EngineLh And Rh Ignition SwitchesFlight Trim Controls_ Stabilator With IndicatorFuel Control Selector

With On/OPanel Switches_ Starter_ Fuel Pump_ Engine Lh And Rh IgnitionSwitches

eLectRicAL systeM

12 Volt 18A Amp. Battery12 Volt Alternators-20 Amp.Switches: - Nav. Lights- Landing Light- Strobe LightExternal Power SupplyReceptableCircuit Breaker Panel

fueL systeM

Two Integral Fuel TanksWith 100 Litres TotalCapacity

Engine Driven Fuel Pump Auxiliary Fuel Pumps,

ElectricFuel Quick DraininteRioR

Pilot And Copilot Seats(Adjustable Fore And A t)

Seat Belts& Shoulder Harness,

All SeatsWall To Wall CarpetingLuggage CompartmentsFire ExtinguisherRadio Call PlateSoundproofngFirst Aid Kit

exteRioR

Epoxy Corrosion Proofng, All Structure

Sliding CanopyWith Lock And Key

Rear WindowTie Down RingsMain Wheels,

5,00 X 5Nose Wheel,

4,00 X 6

exteRioR LigHts

Nav. Lights Vertical Tail StrobeTaxi Light

cABin confoRt systeM

Windshield De roster: Ventilator Adjustable,2 Place

Heating System: Ventilator Adjustable,2 Place

poWeRpLAnt And pRopeLLeR

Engines:1 Rotax 912S2 100 Hp,4 Cylinders Liquid/Air Cooled,

Integrated Reduction GearDual Ignition SystemThrottle Control Lh/RhTubular Steel Engine MountPropeller:

Ho mann2 Blades

Variable PitchControl Lh/RhGovernor Spinner

Air FilterOil FilterOil And Water CoolersCarburetor Heat

With Manual ControlThermostat Valve

pRoduct suppoRt/docuMents

Manu acturersFull Two YearLimited Warranty

Pilots Operation HandbookMaintenance ManualParts Catalog

Aircra t Log BookEngine Log Book

p2002 jr

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