P2002 Sierra

Perfection with Low Wing

To design the P2002 Sierra we used the most advanced systems in 3D design, fluid dynamics and structural analysis, resulting in one of the best two-seater low wing aircraft in its category. Tapered laminar flow wing, slotted flaps, up turned wing tips and a streamlined fuselage give to the P2002 superlative performance, a complete harmony of controls and style. Designed with the pilot in mind, this aircraft will delight even the most discerning pilot while still keeping the not so experienced pilot safe and comfortable.

Contacteaza-ne acum la 021-22.22.55.4!

Cere o oferta de pret!

589NM

Max Range

With this range you can use if cross country.
124kts

Cruise Speed

244 km/h Sea Level
2

Seating

Two seats side by side.
17l/h

Fuel Consumption

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

Exteriors

The P2002 Sierra is a two-seater side by side, low wing aircraft. The P2002 Sierra features superlative performance and flying qualities, now confirmed by hundreds of P2002 ultralights, Light Sport and VLA aircraft sold throughout the world and validated in 15 countries other than Europe. The ease of piloting and maintenance make this aircraft an excellent solution for training in flight schools. It is also an ideal platform for surveillance and as well as, of course, for pure recreational and private use. The option to use 100LL AVGas or unleaded automotive fuel (with up to 10% ethanol content) makes this aircraft even more flexible and cost effective. The P2002 Sierra encompasses the latest developments of Tecnam aircraft. The use of advanced software for design, structural and fluidynamics analysis, and experience in building airplanes with all types of materials results in continuous aircraft improvement. Due to the tapered laminar airfoil and the slotted flaps the P2002 Sierra is an outstanding aircraft, with the perfect mix of aerodynamics, performances, and structural efficiency.

Interiors Details

Seats are adjustable in flight 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 ample room for several travel bags. All Tecnam aircraft have dual control sticks with a curve at the base for ease of ingress and egress. The dual controls come standard with PTT and electric stabilator trim on the stick with a trim indicator on the panel. The interior is spacious, ergonomic and comfortable: cabin is roomy: 36 in/111 cm wide. Dual throttles allow the pilot to fly either left or right handed. Heat and defrost are standard. All Tecnam aircraft provide excellent forward visibility over the cowling.

Avionics

Standard GARMIN Avionics Package

GMA 340 Audio – Panel
GNC 255A Com/Nav
GTX 328 Tdx
ELT 406 Mhz
Antennas:
– Transponder
– Vhf
– ELT
– Marker Bacon
Speakers
Microphone
Stick Push-To-Talk Switch-Pilot/Copilot

Standard Equipment

Flight instruments and indicators

Magnetic Compass
Airspeed Ind., Kts
Altimeter (In)
Vertical Speed
Bank Indicator
Flaps Indicator
Pitot System
Static System
Stabilator Trim Position Indicator

Engine instruments

Tachometer
Hour Recorder
Oil Press.
Oil Temp.
Head Temp.
Fuel Press. Voltmeter
Lh + Rh Fuel Qty

Other instruments / Warnings

Chronometer
O.A.T. Indicator
Generator Warning Light
Vacuum Suction Gauge
Trim Indicator
Warning Light:
– Alt. Out
– Fuel Pump On

Flight controls

Hydraulic Brakes
Parking Brake
Electrical Flaps
Dual Flight Controls
Steerable Nose Wheel
Stabilator Trim (Electric Actuated From Stick) Engine Controls:
_ Throttle, Two
_ Choke
Flight Trim Controls: _ Stabilator With Indicator Fuel Control Selector With On/Off
Panel Switches:
_ Starter
_ Fuel Pump
_ Engine LH + RH Ignition Switches

Electrical system

12 Volt 18A Amp. Battery
12 Volt Alternators-20 Amp.
Switches:
– Landing Light
– Strobe Light
Circuit Fuses Panel

Fuel system

Two Integral Fuel Tanks With 100 Lt Total Capacity
Engine Driven Fuel Pump
Auxiliary Fuel Pumps, Electric
Fuel Quick Drain

Interiors

Pilot And Copilot Seats:
Adjustable
Fore And Aft
Seat Belts & Shoulder Harness,
All Seats
Wall To Wall Carpeting
Luggage Compartments

Product Support/Documents

Manufacturer's Full Two – Year Limited Warranty
Pilot's Operation Handbook
Maintenance Manual
Parts Catalog
Aircraft Log Book
Engine Log Book

Exterior

Sliding Canopy With Lock And Key Rear Window
Tie Down Rings
Main Wheels, 5,00 x 5
Nose Wheel, 4,00 x 6

Exteriors lights

Vertical Tail Strobe
Taxi Light

Cabin comfort system

Ventilator Adjustable, 2 Place

Powerplant and Propeller

Rotax 912ULS2 100 Hp,
4 Cylinders Liquid/Air Cooled,
Integrated Reduction Gear

Rotax 912UL2 115 Hp,
4 Cylinders Liquid/Air Cooled,
Integrated Reduction Gear
Dual Ignition System
Throttle Control Lh/Rh
Tubular Steel Engine Mount
P2002 SIERRA DELUxE:
Gt Propeller, 2 Blade Fix
P2002 SIERRA TURBO:
Gt Propeller, 2 Blade Variable Pitch Propeller Spinner
Air Filter
Oil Filter
Oil And Water Coolers

Standard GARMIN Avionics Package

GMA 340 Audio – Panel
GNC 255A Com/Nav
GTX 328 Tdx
ELT 406 Mhz
Antennas:
– Transponder
– Vhf
– ELT
– Marker Bacon
Speakers
Microphone
Stick Push-To-Talk Switch-Pilot/Copilot
Mic& Phone Jacks-Pilot/Copilot

Packages

1002 P2002 Sierra VP CS/VLA includes:

Non additive, replaces standard equipment and Avionics
ROTAX 912 S3 100HP ENGINE WITH GOVERNOR
CENTRAL QUADRANT WITH SINGLE THROTTLE AND PITCH LEVER
HOFFMANN VARIABLE PITCH PROPELLER
MANIFOLD PRESSURE INDICATOR
ATTITUDE AND DIRECTIONAL ELECTRIC

1003 VFR NIGHT VERSION includes:

Non additive, replaces standard equipment and Avionics
HEATED PITOT
GILL 25A BATTERY
INSTRUMENTS LIGHT
MAP LIGHT
DIMMER
AUX ALTERNATOR

1004 GLASS COCKPIT G500 includes:

Non additive, replaces standard equipment and Avionics
GARMIN G500 PFD
GTN 650 COM/NAV/GPS WITH ANTENNAS AND INST. (EXCH. FOR GNC225A) BACKUP AIRSPEED IND. AND ALTIMETER TSO
AUX ALTERNATOR

1005 GLASS COCKPIT G500 + VFR NIGHT includes:

Non additive, replaces standard equipment and Avionics
GARMIN G500 PFD
GTN 650 COM/NAV/GPS WITH ANTENNAS AND INST. (EXCH. FOR GNC225A)
BACKUP AIRSPEED IND. AND ALTIMETER TSO
HEATED PITOT
GILL 25A BATTERY
INSTRUMENTS LIGHT
MAP LIGHT
DIMMER
AUX ALTERNATOR

1006 RUDDER, THROTTLE AND BRAKE HAND CONTROLS includes:

Non additive, replaces standard equipment and Avionics
FULLY REMOVABLE AND AIRFRAME INTEGRATE HAND CONTROLS FOR RUDDER AND BRAKES

Optional Equipment

Radio And Navigation

GARMIN

GMA 35 Audio Panel with Antenna and inst. Only for GTN750 Exchange for Std. GMA340)
MD200 VOR Indicator Only for GNC255A
GARMIN GTR225A Com 8.33 Khz with Ant. & Inst. (From Nov. 2013 mandatory for EU)
GARMIN GTR225A COM 8.33 Khz with Antenna and Inst. (Exch for Standard GNC255A)
GTN 650 Com/Nav/Gps with Antennas, Triplex and inst. With GI106A Ind.
GTN 650 Com/Nav/Gps with Antennas, Triplex. & inst. With GI106A Ind.(Exch. for Std. GNC255A)
GTN 750 Com/Nav/Gps with Antennas, Triplex and inst. With GI106A Ind.
GTN 750 Com/Nav/Gps with Antennas, Triplex & inst. With GI106A Ind.(Exch for Std. GNC255A)
GTX 330 Transponder mode S with Antenna and Inst. Exchange for Std. GTX23)
GTX 330 Transponder mode S with Antenna and Inst. Exchange for Std. GTX328)
GTX 33 Transponder mode S remote mounted with Antenna and Inst. (Requires option 122)
GTX 33 Transponder mode S remote mounted with Ant. and Inst. (Requires option 122) Exch. For Std. GTX328

BECKER

RA3502 ADF with AN3500 Indicator

BENDIX KING

KR 87 ADF with KI227 Indicator
DME KN63-14

Other Equipment

Two Head Sets
BOSE A 20 Two Head Sets

Aircraft Equipment

  • Tinted Windows
  • Toe Brakes
  • Central Quadrant with single throttle level (requires Toe Brakes opt. 176)
  • Fuselage Cover
  • Spinner Polished Alluminum Look
  • Battery Gill G25 (Exchange for standard battery)
  • Special paint two colors

 

Engine Equipment

  • Aux alternator

Specification

Aircraft Dimensions

Fuselage Height 2.43 mt – 8 ft
Fuselage Length 6.65 mt – 21.8 ft
Wingspan 8.6 mt – 28.2 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 ULS
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 Design Weight: 600 kg – 1320 lb
Std. Empty Weight
Useful Load 250 kg – 551 lb
Baggage allowance 20 kg – 44 lb

Performance

Vmax 244 km/h – 132 kts
Cruise Speed 75% 226 km/h – 122 kts
Stall Speed (Flaps Down Power Off) 65 km/h – 35 kts
Pratical ceiling 4572 mt – 15,000 ft
Take off run 105 mt – 344 ft
Take off distance 200 mt – 656 ft
Landing Run 90 mt – 295 ft
Landing Distance 200 mt – 656 ft
Rate of climb 6.1 m/sec – 1200 ft/min
Range 636 NM
Flight Rule

Afla mai multe despre acest tip de avion, descarcand brosura de prezentare!