AUF logo

   TL 2000 Sting Carbon   

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
AUF CATEGORY:
•   CAO 95.55 para 1.6 AUF accepted European certificated factory built aircraft manufactured by the TL Ultralight Company of the Czech Republic.

GENERAL DESCRIPTION:
Normally configured two seat carbon fibre reinforced plastic construction, low wing with two stage split flaps and fixed tricycle landing gear.

Star This TL96 Star is very similar to the standard TL2000 Sting Carbon except that the construction is glass fibre reinforced plastic.
Sting The TL2000 Sting Carbon sporting the retractable undercarriage option.

ENGINE & PROPELLER OPTIONS
  • Standard 100 hp Rotax 912 ULS liquid cooled 4 cyl engine .

  • Optional Rotax 582, 80 hp Rotax 912 and 115 hp Rotax 914 engines.

  • Propeller: Woodcomp 3 blade carbon fiber – 1600 mm diameter, in-flight adjustable with computer controlled CSU.

OTHER MAJOR OPTIONS AVAILABLE:
  • Retractable undercarriage
  • 125 litre long range fuel tanks
  • The Sting is supplied custom built with instrumentation to customer specification.


PRICE & DELIVERY
Please refer to the website www.mcp.com.au for more details. Delivery varies on factory workload but generally expect around 5 months with another 5 weeks for shipping.



PERFORMANCE SPECIFICATIONS

[Standard model with 100 hp Rotax 912]
  • Performance figures are for MTOW = 544 kg

  • Performance cruise – 75% power (@ 5200 rpm): 135 knots TAS (@ sea level)
  • Cruise – 65% power (@ 5000 rpm): 127 knots TAS (@ sea level)
  • Economy cruise – 55% power (@ 4800 rpm): 115 knots TAS (@ sea level)

  • Range (at 75% power with 30 min reserve fuel): 405 nm
  • Endurance (economy cruise with 30 min reserve): 5.1 hours
  • Fuel consumption (75% power): 19.5 l/hr
  • Fuel consumption (65% power): 15.6 l/hr
  • Fuel consumption (55% power): 12.4 l/hr

  • Vne: 165 knots*
  • Va: 132 knots*
  • Vx: 68 knots*
  • Vy: 75 knots*
  • Stall - Vso: 35 knots CAS
  • Stall - Vs1: 44 knots CAS
  • Glide ratio - max. weight, engine idle: 16.8:1
  • Glide ratio - max. weight, propeller stopped: 15.2:1
  • Initial rate of climb (sea level): 1150 ft/min
  • Service ceiling: 22,000 feet ???

  • Take-off ground roll (short,dry grass): 75 m
  • Take-off over 15 m screen (still air from rest): 220 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): 200 m
* V speeds defined
DIMENSIONAL SPECIFICATIONS
Sting standard UL model, with 100 hp Rotax 912
No options included:
  • Rotax 912 ULS 100 hp engine
  • Propeller: 3 blade variable pitch with CSU
  • Overall height: 2.3 m
  • Length: 5.93 m
  • Wingspan: 8.44 m
  • Wing area: 9.85m²
  • Aspect ratio: 7.26
  • Cabin width - shoulder height: 1250 mm
  • Empty weight : 290 kg
  • Maximum take off weight: 544 kg
  • Maximum load with full fuel: 205 kg
  • Wing loading: 55.5 kg/m² mtow
  • Design load limit: +6G and -4G
  • Fuel capacity: 71 liters - usable: 69 liters[standard tank]
  • VHF radio: XCOM VHF 760 [as an option]
  • Standard instrumentation included: not stated
  • Tyre size (main):14 x 4 (350 x 100)
  • Tyre size (nose): 14 x 4 (350 x 100)
  • Track: 1.65 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