P2002 Sierra MkII AUL

Venerable classic,
reimagined.

This popular Tecnam classic low wing has gotten a major update and still retained its balanced flight soul. Great for training and enjoying the day in the sky.

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Quick facts

0NM

Max Range

1.1188 km

122 kts

Max Cruise Speed

226 km/h

0

Seating

Two seats side by side

17 l/h

Fuel Consumption

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

Exterior

The P2002 Sierra Mk2 encompasses the latest developments in Tecnam aircraft. The use of advanced software for design, structural and fluidynamics analysis, and experience in building airplanes using all types of materials, results in continuous aircraft improvement. Due to the tapered laminar airfoil and the slotted flaps the P2002 Sierra Mk2 is an outstanding aircraft with the perfect mix of aerodynamics, performance, and structural efficiency.
The wing is all light alloy built with a single spar and full metal torsion box. The wing’s leading edges are easily detachable for repairs and also incorporate the fuel tanks (110 Lt – 29 US Gal in total). They are separated from the cabin in order to maximize passive protection. The sliding canopy allows 360° of vision in the cockpit and has full rollover protection tested via inverted drop tests.
The horizontal stabilator tail design, provides remarkable longitudinal hands-off stability along with minimum drag and weight penalty. This provides balanced two finger flight control. The wide slotted flaps, are electrically activated and allow stall speed lower than 40 Kts, and allow the aircraft to perform steep approaches and easier landings. The all alloy ailerons are effective and ensure a quick roll rate without being overly sensitive. All control surfaces are made out of light alloy and all, except for flaps and tab, are mass-balanced.

Interior Details

The Cabin offers newly designed seats and seat rails which are easily operated and adjustable fore and aft via a single handle with a reinforced area between the rails to make cabin access even easier. A roomy baggage compartment accommodates voluminous items with both external and internal access. A strong automotive type seal is used on the baggage door and a courtesy lamp illuminates when opened. A wide cockpit panel provides plenty of room for glass panel avionics.
The largest selection of avionics choice is available on the P2002 Sierra Mk2 in order to allow almost any type of operation. With an extremely wide choice of rack-mounted avionics, including the latest Garmin radios and GPS, IFR training procedures (not in IMC conditions) can be possible. .

Standard Equipment

The following list of equipment is included in the standard aircraft Analog Avionics Package and does not reflect optional equipment.

Flight instruments and indicators

MAGNETIC COMPASS
AIRSPEED IND., Km
ALTIMETER
VERTICAL SPEED
BANK INDICATOR
PITOT SYSTEM
STATIC SYSTEM

Flight controls

HYDRAULIC TOE BRAKES
PARKING BRAKE
ELECTRICAL FLAPS, Preselect
DUAL FLIGHT CONTROLS
STEERABLE NOSE WHEEL
ENGINE CONTROLS:
Central Quadrant with single throttle lever
Choke
STABILATOR TRIM, electri ( Controlled from stick)
FUEL CONTROL SELECTOR WITH Lh/Rh OFF (Andair)

Electrical system

12 VOLT 18A AMP. BATTERY, ALLIANT
12 VOLT ALTERNATORS-20 AMP.
STARTER KEY ACS
SPLIT STARTER
ROCKER SWITCHES:
o   Avionic Master
o   Fuel Pump
o   Landing light
o   Nav. Light
o   Strobe light
CIRCUIT BREAKER PANEL
LANDING/TAXI LIGHT
WING TIP STROBE AND POSITION LIGHT LED
12 VOLT socket
WARNING LIGHTS:
o   Alt Out

Engine instruments

Dynon D10 Include:
TACHOMETER
HOUR RECORDER
OIL PRESS
OIL TEMP.
HEAD TEMP.
FUEL PRESS.
VOLTMETER
LH + RH FUEL QTY
STABILATOR TRIM POSITION INDICATOR
FLAP INDICATOR

Fuel system

TWO INTEGRAL FUEL TANKS WITH 55 LITRES total capacity
ENGINE DRIVEN FUEL PUMPS
AUXILIARY FUEL PUMPS, ELECTRIC
FUEL TANK QUICK DRAIN , TWO
1 X SHUT OFF VALVE

Powerplant and Propeller

INOX FIREWALL
ENGINE – 1 ROTAX 912ULS2 100 HP
o   4 Cylinders
o   Liquid/air cooled
o   Integrated reduction gear
DUAL IGNITION SYSTEM
THROTTLE CONTROL (Central)
TUBULAR STEEL ENGINE MOUNT
PROPELLER: Sensenich 2 Blade Fix Pitch
PROPELLER SPINNER
TWO AIR FILTER
OIL FILTER
OIL AND WATER COOLERS
FIRE SLEEVE FUEL AND OIL TUBES
TERMOSTATIC OIL VALVE

Exterior

EPOXY CORROSION PROOFING, All structure
CANOPY, LOCK AND KEY
TIE DOWN RINGS
MAIN WHEELS, 5.00 X 5 – NOSE 5,00 X 5

Exteriors lights

WING TIP STROBE AND POSITION LIGHT LED
LANDING/TAXI LIGHT

Interior

PILOT and CO-PILOT SEATS, simulated leatheradjustable fore and aft
SEAT BELTS 4 points, All Seats
WALL TO WALL CARPETING
MAP & STORAGE POCKETS
RADIO CALL PLATE
SOUNDPROOFING
LUGGAGE COMPARTMENTS
EMERGENCY HAMMER

Cabin comfort system

WINDSHIELD DEFROSTER
VENTILATOR ADJUSTABLE
HEATING SYSTEM

Product Support and Documents

MANUFACTURER’S FULL TWO YEAR LIMITED WARRANTY
PILOT’S OPERATION HANDBOOK
MAINTENANCE MANUAL
PARTS CATALOG

Avionics

Analog Standard


FLIGHT INSTRUMENTS AND INDICATORS

MAGNETIC COMPASS
AIRSPEED IND., Kt
ALTIMETER
VERTICAL SPEED
SIDESLIP INDICATOR
PITOT SYSTEM
STATIC SYSTEM

ENGINE INSTRUMENTS

Dynon D10 Includes:
-TACHOMETER
-HOUR RECORDER
-OIL PRESS
-OIL TEMP.
-CYLINDER HEAD TEMP.
-FUEL PRESS.
-VOLTMETER
-ELEVATOR TRIM POSITION INDICATOR -FLAP INDICATOR
-LH + RH FUEL QTY

ELECTRICAL SYSTEM

3,2V 7 AMP ALLIANT BATTERY
14V Alternator-20 AMP.
STARTER KEY ACS
SPLIT STARTER
SWITCHES : Avionic Master Fuel Pump Landing light Nav light Strobe light
CIRCUIT BREAKER PANEL
12V SOCKET
Flap three positions
WARNING LIGHT: ALT OUT

Six Pack

replaces standard equipment and avionics


FLIGHT INSTRUMENTS AND INDICATORS

ATTITUDE, electric
DIRECTIONAL, electric
TURN & BANK Indicator

ENGINE INSTRUMENTS

TACHOMETER
HOUR RECORDER
OIL PRESS
OIL TEMP.
HEAD TEMP.
FUEL PRESS.
VOLTMETER
AMMETER
LH + RH FUEL QTY

AVIONICS PACKAGE

GARMIN GMA 240 Audio Panel
GARMIN GTR 200 COM
GARMIN GTX 335 TRANSPONDER with GPS
GARMIN 796 GPS XM VERSION
STICK PUSH-TO-TALK SWITCH-PILOT/COPILOT
MIC & PHONE JACKS-PILOT/COPILOT
ANTENNAS:
o   TRANSPONDER
o   VHF
o   GPS
ELT KANNAD 406 Mhz WITH ANTENNA & REMOTE MOUNTED SWITCH

DYNON SKY VIEW

replaces standard equipment and avionics


Dynon Sky View Sv1000 Two Screens Avionics Pack For Rotax 912 Uls2 & IS

SKYVIEW SV 1000 10” 2 SCREEN DISPLAY (includes main wiring harness)
SV-ADAHRS-200
SV-ADAHRS-201
SV-EMS-221/A ENGINE MONITORING MODULE FOR ROTAX 912
SV-GPS-250
SV-BAT-320

SV-EMS CONFIGURATION
• AMPS (AMMETER SHUNT OR HALL EFFECT)
• MONITOR CHT
• AIRCRAFT BUS VOLTAGES
• OIL TEMPERATURE
• OAT
• OIL PRESSURE
• MANIFOLD PRESSURE
• FUEL PRESSURE
• RPM
• TRIM INDICATOR
• FUEL INDICATOR LH/RHù
• WARNING LIGHTS:
– Fuel pump ON
– ALT OUT

AVIONICS PACKAGE

Dynon SV-INTERCOM-2S
Dynon SV-COM-C25 COM (25 KhZ)
Dynon SV-XPNDR-261 TRANSPONDER
STICK PUSH-TO-TALK SWITCH-PILOT/COPILOT
MIC & PHONE JACKS-PILOT/COPILOT
ANTENNAS:
o   TRANSPONDER
o   VHF
o   GPS

GARMIN G3X

replaces standard equipment and avionics

Astore-opt3-G3x
Garmin G3X two screens Avionics Package for Rotax 912 ULS2

Two Display GDU 460 With EIS
GDU460
GDU460
ADAHRS GSU 25
GEA 24 Engine Instrument Module
GMU 22 Magnetometer
GTP 59 Temperature Probe
LRU KIT
INSTALLATION KIT
G3X SENSOR KIT
GA 56 Antenna

GSU Configuration

AMPS (AMMETER SHUNT OR HALL EFFECT)
MONITOR CHT
AIRCRAFT BUS VOLTAGES
OIL TEMPERATURE
OAT
OIL PRESSURE
MANIFOLD PRESSURE
FUEL PRESSURE
RPM
TRIM INDICATOR
LH + RH FUEL QTY

AVIONICS PACKAGE

GARMIN GMA 240 AUDIOPANEL
GARMIN GTR 200 COM
GTX 35R Transponder mode S remote mounted
STICK PUSH-TO-TALK SWITCH-PILOT/COPILOT
MIC & PHONE JACKS-PILOT/COPILOT
ANTENNAS:
o   TRANSPONDER
o   VHF
ELT KANNAD 406 Mhz WITH ANTENNA & REMOTE MOUNTED SWITCH

Category Upgrades

A-1002 Advanced

Includes:

Radio ICA210 installed
GARMIN GTX 335 TRANSPONDER with GPS
ELT KANNAD 406 Mhz WITH ANTENNA & REMOTE MOUNTED SWITCH
Paracadute Junkers 600 KG

A-1003 US-LSA

Non-Additive. Replaces all Standard Equipment.- Also Includes the following equipment:

Includes:
EXTENDED WARRANTY FOR ROTAX ENGINE ( 1 year extention)
LANDING LIGHT LED
EXTERNAL POWER RECEPTABLE
BAGGAGE COMPARTMENT NET
ELT KANNAD 406 Mhz WITH ANTENNA & REMOTE MOUNTED SWITCH

A-1004 US LSA – ADSB OUT (Only for A-OPT. 3)

Non-Additive. Replaces all Standard Equipment.- Also Includes the following equipment:
Includes:
GDU465 (Exchange for Std. GDU460)
GPS 20A – ADSB OUT
GA 37 Antenna (ADSB & XM)

A-1005 US LSA – ADSB IN/OUT (Only for A-OPT. 3)

Non-Additive. Replaces all Standard Equipment.- Also Includes the following equipment:
Includes:
GDU465 (Exchange for Std. GDU460)
GTX345R GPS (P/N dash -41) (Exch. For Std. GTX23S)
GA 37 Antenna (ADSB & XM)

Paint Options

MkII-Paint & Interior options

 

 

 

 

 

Interior Options


 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Video

 

Specification

Aircraft Dimensions

Fuselage Height 2.4 mt – 8.0ft
Fuselage Length 6.74 mt – 22.11ft
Wingspan 8.56 mt – 28.08 ft
Cabin Height (seat to cover) 0.95 mt – 3.1 ft
Cabin Width 1.11 mt – 3.6 ft
Max Seating capacity 2
Fuel tank capacity 2 x 55 lt – 2 x 14.5 US Gal

Powerplant

Engine Manufacturer ROTAX 912ULS2
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

Baggage allowance 20 kg – 44 lb
Design Weight 620 kg – 1367 lb

Performance

Max Cruise Speed (KTAS) 122 kts- 226 km/h KTAS
Stall Speed (Flaps Down Power Off) KCAS 40 kt – 74 km/h KCAS
Practical ceiling 14,000 ft – 4267 mt
Take off run 489 ft – 149 mt
Take off distance 984 ft – 300 mt
Landing Run 620 ft – 189 mt
Landing Distance 1100 ft – 335 mt
Rate of climb 923 ft/min – 4,69 m/sec
Range 642 NM – 1189 km

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

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