AUF logo

   Allegro 2000   

www.mcp.com.au

Buyer's Guide
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IMPORTER & DISTRIBUTOR:
X-Air Australia

Factory 4
24 Leda Drive
Burleigh Heads
Queensland, Australia

AIRFIELD:
Heck Field [YJCW]
Jacobs Well
Gold Coast, Qld

SALES MANAGER:
Michael Coates

07 5568 7770 or 0418 168 665
mcoates@mcp.com.au
DEALER – ACT and Victoria:
Phil Allen

0417 040 052
phila@bigpond.net.au
Allegro
AUF CATEGORY:
•   CAO 95.55 para 1.6 AUF accepted European certificated factory built aircraft manufactured in the Czech Republic.



Star
GENERAL DESCRIPTION:
Normally configured two seat, high wing monoplane with two stage flaps, T tail and fixed tricycle landing gear. Construction: metal wings and tail, composite fuselage.


ENGINE & PROPELLER OPTIONS
  • Available with Rotax 582, 80 hp Rotax 912 or 100 hp Rotax 912 ULS engines.
  • 105 litre long range wing tank

OTHER MAJOR OPTIONS AVAILABLE:
  • The standard factory built aircraft is equipped with ASI, VSI, altimeter, slip and skid indicator, flap position indicator, fuel gauge, oil pressure gauge, oil temperature gauge, CHT, fuel pressure and tachometer. Additional instruments may be ordered for fitting at the factory or the importer's workshop.


PRICE & DELIVERY
Please refer to the website www.mcp.com.au for more details. Delivery is 10 to 12 weeks with another 5 weeks for shipping.



PERFORMANCE SPECIFICATIONS

[Standard model with 80 hp Rotax 912 ULS]
  • Performance figures are for MTOW = 520 kg

  • Performance cruise – 75% power (@ 5000 rpm): 95 knots TAS (@ sea level)
  • Cruise – 65% power (@ 4800 rpm): 85 knots TAS (@ sea level)
  • Economy cruise – 55% power (@ 4300 rpm): 74 knots TAS (@ sea level)

  • Range (at 75% power with 30 min reserve fuel): 325 nm
  • Endurance (economy cruise with 30 min reserve): 4.9 hours
  • Fuel consumption (75% power): 14.5 l/hr
  • Fuel consumption (65% power): 13.5 l/hr
  • Fuel consumption (55% power): 10.1 l/hr

  • Vne: 118 knots*
  • Va: 86 knots*
  • Vx: 60 knots*
  • Vy: 66 knots*
  • Stall - Vso: 35 knots CAS
  • Stall - Vs1: 43 knots CAS
  • Glide ratio - max. weight, propeller stopped: 12:1
  • Initial rate of climb (sea level): 985 ft/min
  • Service ceiling: 12,500 feet

  • Take-off ground roll (short,dry grass): 150 m
  • Take-off over 15 m screen (still air from rest): 250 m
  • Demonstrated maximum crosswind capability: 15 knots
  • Landing ground roll (short, dry grass): 100 m
  • Landing distance to full stop over 15 m screen (still air): 220 m
* V speeds defined
DIMENSIONAL SPECIFICATIONS
Allegro 2000 standard UL model, with 80 hp Rotax 912
No options included:
  • Rotax 912 ULS 80 hp engine
  • Propeller: Woodcomp 3 blade carbon fibre – 1600 mm diameter
  • Overall height: 2.05 m
  • Length: 6.36 m
  • Wingspan: 10.81 m
  • Wing area: 10.37m²
  • Aspect ratio: 9.5
  • Cabin width - shoulder height: 1100 mm
  • Empty weight : 275 kg
  • Maximum take off weight: 520 kg
  • Maximum load with full fuel: 206 kg
  • Wing loading: 45.73 kg/m² mtow
  • Design load limit: +4g and -2g
  • Fuel capacity: 56 liters - usable: 55 liters[standard tank]
  • VHF radio: XCOM VHF 760 [as an option]
  • Standard instrumentation included: ASI, VSI, altimeter, slip and skid indicator, flap position indicator, fuel gauge, oil pressure gauge, oil temperature gauge, CHT, fuel pressure and tachometer. Additional instruments may be ordered for fitting at the factory or the importer's workshop.
  • Tyre size (main):14 x 4 (350 x 100)
  • Tyre size (nose): 14 x 4 (350 x 100)
  • Track: 1.55 m




X-Air Australia

telephone: international +61 7 5568 7770     national: 07 5568 7770    

or : EMAIL X-Air Australia      Web address:www.mcp.com.au


Currency of information – this page last updated with company supplied data – April, 2004