P92 Eaglet G5 - LY PDF Imprimir E-mail
Productos y Servicios - Categoría VLA

 

Especificaciones, prestaciones, equipamiento estándar y fotografías del avión P92 Eaglet G5 - LY.

 

 

FOTOGRAFÍAS DEL AVIÓN


ESPECIFICACIONES Y PRESTACIONES

MOTOR P92 EAGLET G5 P92 EAGLET LY
Fabricante Rotax   Lycoming
Modelo 912 ULS2   YO -233-B2A
Potencia 98 hp   115 hp
Cilindros 4   4
HÉLICE
Fabricante GT Propeller   GT Propeller
Modelo GT -2/173/VRR-SRTC FW101   GT -2
Palas 2   2
Tipo Fix pitch - wood   Fix pitch - wood
DESIGN WEIGHT & LOADING      
MTOW 600 kg / 1320 lb   600 kg / 1320 lb
Standard Equip. Empty Weight 355 kg / 780 lb   380 kg / 840 lb
Standard Equip. Useful Weight 245 kg / 540 lb   220 kg / 480 lb
Baggage Allowance 20 kg / 44 lb   20 kg / 44 lb
Limit Loads +3,8 / -1,9 G
Ultimate Loads +5,7 / -2,85 G
DIMENSIONES
Ala      
Wing span 8,7 m   28,5 ft
Fuselaje:      
Largo 6,4 m   21 ft
Alto 2,5 m   8,2 ft
       
Cabin Width 1,11 m   3,6 ft
Cabin Height Seat to Cover 0,91 m   3 ft
Fuel Tank Capacity 45 x2 lt   11,2 x2 GAL
CARACTERÍSTICAS 15°C Sea Level 600 KG / 1320 LB
VMAX 222 km/h - 120 kts   240 km/h - 130 kts
Cruise Speed 75% 200 km/h - 108 kts   220 km/h - 118 kts
Vne 261 km/h - 141 kts   261 km/h - 141 kts
Stall Speed FLAPS down POWER OFF 76 km/h - 41 kts   76 km/h - 41 kts
Pratical Ceiling 4572 m - 15000 ft   4400 m -14500 ft
Takeoff Run 120 m - 394 ft   190 m - 625 ft
Takeoff Distance 250 m - 820 ft   295 m - 970 ft
Landing Run 120 m - 394 ft   170 m - 560 ft
Landing Distance 302 m - 991 ft   350 m - 1150 ft
Rate of Climb 5,6 m/sec - 1100 ft/min   5,6 m/sec - 1100 ft/min
Range 493 n.M.   493 n.M.

EQUIPAMIENTO ESTÁNDAR


Flight Instruments And Indicators

  • Magnetic Compass
  • Airspeed Ind.,
  • Altimeter Dual Mode (In/Mb)
  • Vertical Speed
  • Bank Indicator
  • Flap 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

 

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:
  • Avionic Master

 

Electrical System

  • 12 Volt 18a Amp. Battery
  • Switches
         ·· Landing Light
         ··Strobe Light
  • 12 Volt Socket
  • Circuit Breakers Panel

 

Fuel System

  • Two Integral Fuel Tanks with 92 Litres Total Capacity
  • Engine Driven Fuel Pump
  • Fuel Quick Drain

 

Interior

  • Pilot And Copilot Seats
         ··Adjustable Fore And Aft
         ··Arm Rest
  • Seat Belts & Shoulder Harness, All Seats
  • Wall To Wall Carpeting
  • Map and Storage Pockets
  • Luggage Compartments

 

Exterior

  • Epoxy Corrosion Proofing, All Structure
  • Lh/Rh Front Door Pilot/Copilot,
  • Lock And Key
  • Rear Window
  • All Windows Tinted
  • Main Wheels, 5,00 X 5
  • Nose Wheel, 4,00 X 6

 

Exterior Lights

  • Vertical Tail Strobe
  • Taxi Light

 

Cabin Confort System

  • Windshield Defroster
  • Ventilator Adjustable, 2 Place
  • Heating System With Defrost

 

Powerplant And Propeller

  •      ··Opion I ROTA X
  • 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 Gt 2 Blade Fix
  • Propeller Spinner
  • Air Filter
  • Oil Filter
  • 12 Volt Alternators 20 Amp.
  • Opion Ii Lycoming
  • Engine 1 Lycoming Yo-233-B2a 115 Hp,
  • 4 Cylinders
  • Direct Drive
  • Dual Ignition System
  • Throttle Control
  • Tubular Steel Engine Mount
  • Propeller Gt 2 Blade Fix
  • Propeller Spinner
  • Air Filter
  • Oil Filter
  • Oil Cooler
  • 12 Volt Alternators 60 Amp

 

Product Support/Documents

  • Manufacturers Full Two Year
  • Limited Warranty
  • Pilots Operation Handbook
  • Maintenance Manual
 

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