Pilot Operating Handbook
Section 1
TL-2000
Sting
General
Notice! The information contained in this document is for reference and information only.
The pilot is the final and only responsible party for the safe operation of this aircraft.
31 December 09 / Chg 5
1-5
Copyright © 2009 Reproduction of this document or any of its parts is forbidden.
BASIC DIMENSIONS
Length .......................................................................... 20.33 ft.
Cabin width .................................................................. 44 in.
Wingspan - Sport - (S3) ................................................ 28.2 ft. - (29.3 ft.)
Height .......................................................................... 78 in.
Areas
Wing ............................................................................. 121.4 ft
2
Flap .............................................................................. 18.6 ft
2
Aspect ratio .................................................................. 7.26
Glide ratio ..................................................................... 12:1
AIRPLANE WEIGHTS
Maximum Calculated Structural Weight: 1430 Lbs
Maximum Ramp Weight: 1340 Lbs
Maximum Takeoff or Landing Weight: 1320 Lbs
Standard Empty Weight: 780 Lbs
Maximum Useful Load: 540 Lbs
Total Baggage Weight: 60 Lbs.
Each baggage compartment can hold a maximum of 20
Lbs. An additional 20 Lbs may be loaded on the surface
of deck aft of the seats if properly secured against an
abrupt movement. Total baggage limit is 60 lbs (20-20-
20).
ENGINE
Number of Engines: 1
Engine Manufacturer: Rotax
®
G.m.b.H. Aircraft Engines
Engine Model Number: 912 UL(S), Standard Equipment
Engine Type: Normally-aspirated, liquid/air-cooled, dry sump, gear-reduced drive,
dual carburetor-equipped, four-cylinder, four-stroke, electronic dual
ignition, horizontally-opposed engine.
Horsepower Rating and Engine Speed: 80(100) BHP at 5800 RPM
PROPELLER
Propeller Manufacturer: Woodcomp
®
Propellers, SRO
Propeller Model Number: SR 200
NOTE