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TL ULTRALIGHT
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T L - 2000 Sting Carbon RG Manual
Flight and operational manual
1st Published in December 2000 Translated to English - January 2001

Serial number:

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T L - 2000 Sting Carbon RG Manual

1.GENERAL INFORMATION ...................................................................................................... 7
1.1. Important Information ..........................................................................................................................................7 1.2. Description of theaircraft....................................................................................................................................7 1.2.1. Airframe...........................................................................................................................................................7 1.2.2. Fuel system.....................................................................................................................................................8 1.2.3. Propeller ..........................................................................................................................................................8 1.2.4. Engine .............................................................................................................................................................8 1.2.5. Control movements.........................................................................................................................................8 1.2.6. Basic technical data of the airplane ................................................................................................................9 1.3. Layout of the airplane..........................................................................................................................................9 1.4. Detecting the center of gravity position, allowed and measured values......................................................10 1.4.1. Weighing the airplane for the foreword center of gravity position.................................................................10 1.4.2. Weighing the airplane for the backmost center of gravity.............................................................................11

2. OPERATING RESTRICTIONS............................................................................................... 11
2.1. Flight operation speeds and position fault of the Air Speed Indicator.........................................................11 2.1.1. Air-speed data and position fault of Pitot tube..............................................................................................12 2.1.2. Reparation table of real and indicated air-velocity in km/h ...........................................................................12 2.2. Weights and loads ..............................................................................................................................................12 2.2.1.Maximum and minimum weights...................................................................................................................12 2.2.2. Weight of the empty airplane and detected position of the point of balance ................................................12 2.2.3. Positioning of the load...................................................................................................................................12 2.3. Engine operating restrictions............................................................................................................................13 2.3. Propeller operating restrictions ........................................................................................................................13 2.4. Fuel and lubricant oil...