Pica 22021-04-14T09:26:23+04:30

Pica 2

Two – Seat UL/LSA Aircraft

Pica 2 is a two seat, side by side, low wing aircraft with full composite structure. It has one of the best cockpit design, layout and space among the aircrafts of this class.

Pica2 is powered by Rotax 912 ULS2 engine with a 3blade ground ground adjustable propeller.

This aircraft is designed base on ASTM of USA regulation which allows this aircraft to take more structural load on maneuvers and landing for pilot training.

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Pica2 Dorna Aircraft

APPLICATIONS

SPECIFICATIONS

Weight and Loading

Empty Weight, Equipped 390 kg
Max Takeoff Weight 600kg
Usable Fuel 2×45 liter
Wing Loading 54.25 kg/m2
G Limits +4 and -2

External Dimensions

Wing Chord, Constant 1.17 m
Wing Aspect Ratio 8.08
Length Overall 6.25 m
Fuselage Max Width 1.21 m
Height Overall 2.33 m
Wheel Track 1.94 m
Wheel Base 1.51 m
Propeller Diameter 1.72 m
Wing Span 9.45 m

Interior Dimensions

Cockpit Max Width 1.17 m
Cockpit Max Length 1.55 m

Areas

Wing Gross 11.06 m2
Ailerons (total) 0.952 m2
Trailing Edge Flaps (total) 1.54 m2
Fin 0.96 m2
Rudder 0.46 m2
Tail 2.02 m2
Elevator (total) 0.9 m2
side pica2
top pica 2
front pica 2

Power Plant

Engine Manufacturer BRP - Rotax
Model 912 ULS2
Max Takeoff Power 100 HP
Fuel Type Automotive Super 95% Octane Unleaded or Avgas 100 LL

Propeller

Manufacturer WOODCOMP
Type SR200B
Specifications WOODCOMP Three Blades on Ground Adjustable Propeller
rotax 912 ULS2

Performance

Max Level Speed at 14,000 ft.(TAS) 120 Knot (225 km/h)
Stall Speed (Flap Down) 40 Knot (75 km/h)
Max Rate of Climb 300 m/min (1000 ft/min)
Service Ceiling 14,000 ft. (4265 m)
Takeoff Run (To 50 ft. obstacle) 1000 ft. (305 m)
Landing Run (From 50 ft. obstacle) 850 ft. (260 m)
Max Range 650 nm (1200 km)
pica2 performace
Pica 2
&
Competition
Pica 2 Dynamic WT9 P2002 Sierra ZODIAC CH601XL
Pica 2 Dynamic WT9 P2002 Sierra ZODIAC CH601XL
Wing Span 9.45 m 8.6 m 8.6 m 8.23 m
Wing Aera 10.96 m2 10.3 m2 11.5 m2 12.26 m2
Length Overall 6.25 m 6.4 m 6.61 m 6.10 m
Height 2.32 m 1.98 m 2.41 m 1.98 m
Cockpit Width 1.17 m 1.17 m 1.09 m 1.12 m
Empty Weight 380 Kg 300 kg 331 kg 312 kg
Max Take-Off Weight 600 kg 550 kg 600 kg 600 kg
Useful Load 218 kg - 368 kg -
Total Fuel Capacity 70.00 lit 100 lit - 92 lit
Engine Power 100 hp 100 hp 100 hp 100 hp
Stall Speed(With Flaps) 46 mph 32 mph 43.73 mph 44 mph
Stall Speed(No Flaps) 56 mph - 51.79 mph 51 mph
Service Ceiling 14000 ft - 13110 ft -
Rate of Climb 1000 ft/min 1200 ft/min 1200 ft/min 900 ft/min
Range(Cruise Reserved) 684.00 km - 836.86 km -
Endurance(Fuel Reserve) 3.5 hr - - 4.9 hr
Take-off Distance(On Ground) 141 m 186 m - 168 m
G Limits (+4 / -2g) - (+4 / -2g) (+6 / -4g)

Basic Equipment

  • Air Speed lnd.

  • Altimeter

  • Vertical Speed lnd.

  • Magnetic Compass

  • Slip lnd.

  • Annunciator Panel

  • COM Radio

  • Manifold Pressure lnd.

  • Circuit Breaker Panel

  • Fuel Pressure lnd.

  • Voltmeter / Ammeter

  • Fuel Quantity (R/L)

  • Throttle

  • Battery Switch

  • Aux. Fuel Pump Switch

  • Ignition Switch

  • Radio Master switch

  • Dual Control Stick

  • Dual Breake

  • Shoulder Harness

Optional Equipment

  • ELT

  • GPS

  • Trim Switch & Lnd.

  • Turn & Bank lnd.

  • Attitude Gyro.

  • Heading lnd.

  • Transponder Radio

  • Encoder

  • Flydat

  • Radio NAV/COM Hand Held

  • Clock

  • Stall lnd.

  • Nav/Strobe Light

  • Landing Light

  • Beacon Light

  • Fire Extinguisher

  • Cabin Heater

  • Parking Brake

  • Static discharger

  • Fuselage Cover

  • External Generator

  • Engine EMS System

  • Flight EFIS System

  • BRS System

FAQ

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