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Pilot Operating Handbook Section 0 TL-2000 Sting Introduction 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. (THIS PAGE BLANK)
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Pilot Operating Handbook Section 0 TL-2000 Sting Introduction 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. SECTION INDEX SECTION GENERAL ................
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The authority of TL Ultralight, as the original equipment manufacturer (OEM), is complete and final for all operation or maintenance of the aircraft and aircraft components. This document also incorporates some references from Rotax ®...
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If this manual is found not to be current, revisions missing, or pages removed contact our USA Continued Airworthiness Service location in accordance with ASTM for replacements. TL Ultralight, s.r.o. USA Continued Airworthiness Service 8222 Remount Road North Little Rock, AR 72118 Phone: 501.228.7777...
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Pilot Operating Handbook Section 0 TL-2000 Sting Introduction 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. LIST OF EFFECTIVE PAGES 3-18 ....
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Pilot Operating Handbook Section 0 TL-2000 Sting Introduction 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. List of changes REVISED REVISED EXTENT OF...
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. SECTION 1 GENERAL INFORMATION TABLE OF CONTENTS Page THREE VIEW DRAWINGS (Sting S3) .............
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. INTRODUCTION This manual is written and organized to conform to the ASTM F2245, Design and Performance of a Light Sport Aircraft.
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. BASIC DIMENSIONS Length ................20.33 ft. Cabin width ..............
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. Number of Blades: 3 Propeller Diameter: 63 In Propeller Type: Fixed-pitch, ground-adjustable Blade Pitch: Standard Conditions...
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. 100LL Avgas is an alternate fuel type if 91 octane unleaded auto fuel is not available.
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. Oil Specifications: Vary depending on the engine operation and may vary from one aircraft to another depending on the operation, environment and fuel type.
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. Knots True Airspeed (KTAS): KCAS corrected for non-standard temperature and pressure and is expressed in knots.
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. Standard Temperature: 15°C at sea level pressure altitude. (Decreases approximately 2°C for each 1000 feet increase of altitude.) True Altitude: The true height above mean sea level (MSL).
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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. dividing the total moment by the total weight of the airplane. Its distance from the reference datum is found by dividing the total moment by the total weight of the airplane.
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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. Maximum Forward and Maximum Aft CG Locations: A specified forward most and rear most CG location along the aircraft longitudinal axis.
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. Station: A vertical location along the airplane fuselage horizontal axis given in terms of the distance from the reference datum plane.
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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. CBS – Circuit Breaker Switch CFI –...
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NE – Never Exceed NM – Nautical Mile(s) NTSB – National Transportation Safety Board OEM – Original Equipment Manufacturer, TL Ultralight SRO POH – Pilot Operating Handbook PIC – Pilot in Command PIM – Pilot Information Manual (No longer used in LSA, PIM=POH)
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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. PSI – Pounds per Square Inch RPM –...
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Pilot Operating Handbook Section 2 TL-2000 Sting Operating Limitations 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. SECTION 2 OPERATING LIMITATIONS TABLE OF CONTENTS Page...
Pilot Operating Handbook Section 2 TL-2000 Sting Operating Limitations 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. INTRODUCTION Section 2 includes specific operating limitations and airspeed instrument markings. The limitations provided in this section should be adhered to for safe operation of the airplane.
Pilot Operating Handbook Section 2 TL-2000 Sting Operating Limitations 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. CAUTION Maximum speed for aircraft parachute deployment at gross weight: 135 Kts. AIRSPEED INDICATOR MARKINGS MARKING KIAS...
Pilot Operating Handbook Section 2 TL-2000 Sting Operating Limitations 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. WARNING Flight operations should be halted in gusts or crosswinds in excess of 25Kts. SERVICE CEILING Standard conditions, standard day: 16,000 Ft LSA altitude limits: 10,000 Ft.
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Pilot Operating Handbook Section 2 TL-2000 Sting Operating Limitations 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. CAUTION Exceeding the maximum fuel pressure may override the float valves of the carburetors and cause erratic engine operation.
Pilot Operating Handbook Section 2 TL-2000 Sting Operating Limitations 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. PROPELLER LIMITATIONS Propeller Manufacturer: Woodcomp ®...
Pilot Operating Handbook Section 2 TL-2000 Sting Operating Limitations 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. MANEUVER LIMITS This airplane is certified as a Light Sport Aircraft and is not approved for aerobatic flight, including spins.
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Pilot Operating Handbook Section 2 TL-2000 Sting Operating Limitations 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. NOTE Limited IFR IMC operations may be approved by the OEM manufacturer for specific aircraft meeting appropriate ASTM/FAA standards.
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Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS Page...
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. INTRODUCTION Section 3 provides checklists and amplified information in the event of an emergency. Abbreviated checklists for use in the aircraft are included in Section 10.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. NOTE The items discussed in each amplified procedures are informational. None of these items or procedures are intended to replace properly qualified ground or in-flight instruction by an FAA certified flight instructor (CFI).
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. WARNING Firmly pull the parachute activation handle out 18 inches with as much as 20 pounds of force.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. Only the most time-critical items are on the checklist. These items are to be carried out quickly, in order to stop as soon as possible.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. 5. Starter -- ENGAGE If restart fails, execute a forced landing.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. NOTE If engine failure occurs at a high cruise speed, maintain the current attitude and altitude until slowing to V Do NOT attempt a “zoom”...
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. 8. Touchdown -- INTO WIND if possible, NOSE HIGH 9.
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Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. Airspeed -- 55 KIAS Flaps -- FULL Radio -- SET TO 121.5;...
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. FIRES ENGINE FIRE DURING START 1.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. ENGINE FIRE IN FLIGHT WARNING During an in-flight fire do not deploy the aircraft parachute system at high altitude.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. In the event of an in-flight engine fire, an engine restart should not be attempted. This could aggravate the emergency even further by providing more fuel for the fire.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. is needed to complete the flight, ensure that all electrical switches are still off, and check the circuit breakers.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. accumulated on the exterior surface of the hot air supply hose. Rotate both vents aft to help clear any fumes.
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Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. IF the aircraft parachute system is not deployed: Airspeed Check Throttle to IDLE if the airspeed is increasing.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. WARNING WARNING Controlled flight into terrain (CFIT) is a common occurrence following inadvertent IMC conditions.
Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. When the rotation stops, neutralize the rudder. Firmly, but cautiously pull back on the stick in order to minimize loss in altitude.
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Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. suitable field for a forced landing. Use only the minimum power required to reach the desired touchdown spot.
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Pilot Operating Handbook Section 3 TL-2000 Sting Emergency Procedures 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. vibration if it is a wheel spinning. The nose wheel may also rotate and vibrate above 110 knots.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS Page...
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. INTRODUCTION Section 4 provides checklists and amplified procedures for conducting normal operations.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. NOTE See section 9 for required aircraft documentation. 11.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. that all screws are present and tight. Clear all air inlets of debris or bird nests that could hinder engine cooling.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. NOTE Check the nose strut suspension system for evidence of nose wheel impact which can occur on high speed landings where initial runway contact is not on main landing gear.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. 13. Under wing Inspection Ports – SECURE / CHECK CONTINUITY 14.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. AFT FUSELAGE 1.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. Examine the flap slot located underneath the wing to ensure proper clearance for retracted flaps.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. CAUTION If left open for in bright sunlight, the excellent canopy optics are capable of focusing the sunlight off of the interior curved surface and causing burns in the cabin upholstery.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. 20. Intercom -- ON CAUTION Be sure to check that the safety harnesses belts or headset wires are not outside the cockpit when closing the canopy.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. When the engine fires, ensure the oil pressure rises within 10 seconds.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. Ensure that the turn coordinator’s solid state gyro is operating correctly by verifying the wings are level.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. will cause the brake pads to glaze and the brake caliper to chatter with each brake application.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. ignition switch back on. Smoothly throttle back down to 2000 RPM. The RPM drop should not have exceeded 300 RPM on either ignition nor indicate more than a 120 RPM difference between the two.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. secured and locked in all three locations, and make certain the GRS safety pin has been removed and stowed on the pilot side canopy lever.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. Accelerate to slightly above normal takeoff speed and rotate the aircraft off the ground smoothly.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. CRUISE 1. Throttle -- 5200 TO 5400 RPM 2.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. TURBULENCE IN FLIGHT If turbulent air is encountered while in flight, slow the aircraft to below 118 KIAS, (maneuver speed) in order to ensure that the airplane’s structural integrity is not compromised.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. On base leg: 4.
Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. NOTE If the AOA is not high enough (nose is low) or the speed is too high as the main wheels contact the runway, the nose wheel may drop to the runway due to the main wheels suddenly slowing the aircraft.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. rate. Allow the airplane to settle to the runway. Do not allow the nose wheel to touch down on landing.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. and the aircraft is at a slow taxi speed, retract the flaps and turn the fuel pump OFF and set the transponder back to STANDBY.
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Pilot Operating Handbook Section 4 TL-2000 Sting Normal Procedures 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. A secondary check of the ignition system can be noted on alternate flights.
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Pilot Operating Handbook Section 5 TL-2000 Sting Performance 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. SECTION 5 PERFORMANCE TABLE OF CONTENTS Page INTRODUCTION ....................
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Pilot Operating Handbook Section 5 TL-2000 Sting Performance 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. INTRODUCTION This section contains performance information pertinent to the intended use of the airplane.
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Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. SECTION 6 WEIGHT &...
Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. INTRODUCTION Section 6 contains a standard installed equipment list information pertaining to the weight and balance calculations for the airplane.
Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. LIST OF ADDITIONAL INSTALLED EQUIPMENT (add to above): 1.
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Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. Major alteration or modification results from the addition, deletion, or redistribution of existing equipment and accessories, or from a repair which results in a significant increase of weight of the airframe or engine.
Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. Arm: The horizontal distance expressed in inches from the reference datum plane to the (CG) of an item or location along the fuselage.
Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. However, the Maximum Allowable Gross Weight should not be exceeded under any circumstances The fuel tank should be empty except for unusable fuel.
Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. 2.
Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. Write in the actual weight of the baggage in all three locations, pilot side storage, copilot side storage and aft deck area.
Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. An aircraft log book entry should be made whenever a Weight Balance calculation is performed, indicating date, and nature of change, results and name of person performing the calculation.
Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. Figure 6.2, STING MOMENT ARM DATA SHEET 31 December 09 / Chg 5 6-11...
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Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. Sting NXXX SAMPLE WEIGHT &...
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Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. Sting N_ _ _ _ _ WEIGHT &...
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Pilot Operating Handbook Section 6 TL-2000 Sting Weight & Balance Information 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. (THIS PAGE BLANK) 31 December 09 / Chg 5 6-14...
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Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. SECTION 7 AIRPLANE &...
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. INTRODUCTION Section 7 describes the different systems specific to the Sting. Some equipment described in this section may not apply to all Sting serial numbers.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. to two manually-operated flight sticks by a series of ball bearing push rods. The rudder is manually operated by two pair of control cables linked to foot pedals.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. Sting flight instruments are arranged in the basic “T” configuration on the pilot (left) side of the aircraft.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. NOTE Inflight, with air loads, the flap button may appear to lock if the flap lever is pulled sideways out-of-plane.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. CANOPY The canopy is designed to allow for a maximum outside view. It is a one-piece construction that is hinged in the front and opens upward assisted by two gas struts.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. NOTE Do not pull aft hard on the throttle to lower the engine rpm.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. drains into the crankcase. Blow-by pressure from the cylinders in compression crates a positive pressure in the crankcase which forces the oil back the reservoir, and the process repeats itself.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. CARBURETOR SYSTEM The aircraft’s Rotax ®...
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. FUEL SYSTEM The aircraft’s fuel system consists of one vented, 20.5 gallon main tank;...
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Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. tank to the top of the filler neck may cause fuel to be vented overboard due to liquid expansion.
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Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. Figure 7.1 Sting Fuel Schematic 31 December 09 / Chg 5 ______...
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. CABIN HEATING AND VENTILATION Outside air can be vented into the cockpit for cooling purposes by opening any of three vents located in the canopy.
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Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. Figure 7.2 Sting Brake System Schematic 31 December 09 / Chg 5 ______...
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. ELECTRICAL SYSTEM AND INSTRUMENTS This aircraft is equipped with a 12-volt, direct-current electrical system.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. CIRCUIT BREAKERS AND FUSES Circuit breakers and fuses are the best protection for electrical loads and malfunctions.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. On later model aircraft the static ports are located on both sides of the aft fuselage and the ports on the pitot tube are not functional.
Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. The same holds true for a descent. The indicator will show a rate of descent so long as the aircraft continues to lose altitude but will return to zero whenever level flight is reached.
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Pilot Operating Handbook Section 7 TL-2000 Sting Systems Descriptions 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. (THIS PAGE BLANK) 31 December 09 / Chg 5 ______ 7-20...
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Pilot Operating Handbook Section 8 TL-2000 Sting Required Placards & Markings 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. SECTION 8 REQUIRED PLACARDS &...
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Pilot Operating Handbook Section 8 TL-2000 Sting Required Placards & Markings 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. INTRODUCTION Section 8 contains a list of both placards and markings located inside the cockpit and on the exterior of the airplane.
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Pilot Operating Handbook Section 8 TL-2000 Sting Required Placards & Markings 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. Aux wing fuel tank filler neck rims: FUEL CAPACITY 6 US GALLONS...
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Pilot Operating Handbook Section 8 TL-2000 Sting Required Placards & Markings 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. Aircraft parachute warning labels Interior co-pilot panel: (may be separated if required) Below aft canopy (x2):...
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Pilot Operating Handbook Section 8 TL-2000 Sting Required Placards & Markings 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. Aft Fuselage behind aft canopy: GRS rocket interior front of rocket motor: PUSH...
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Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. SECTION 9 AIRPLANE HANDLING, SERVICE &...
Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. INTRODUCTION Section 9 provides instruction and procedures for handling and care of the airplane.
Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. GROUND HANDLING TOWING The best way for maneuvering the aircraft on the ground is by use of the included tow...
Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. SERVICING ENGINE OIL Servicing the oil of the Rotax...
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Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. Engine Oils Recommended for Use with Unleaded Fuel (92 OCTANE AUTO GAS, not 87 Octane ‘MoGas’) Brand...
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Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. Fig.
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Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. WARNING Before hand-turning the propeller, ENSURE THAT BOTH IGNITION SWITCHES ARE OFF.
Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. WARNING The careless draining of hot engine oil may cause scalds or burns.
Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. engine is hot.
Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. CAUTION The main tank has a 21.5 gallon total capacity when completely filled to the neck.
Pilot Operating Handbook Section 9 TL-2000 Sting Airplane Handling, Service & Maintenance 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. Do not use a canvas cover on the canopy unless freezing rain or sleet is anticipated because the cover may scratch the plastic surface.
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. SECTION 10 SUPPLEMENTARY INFORMATION Page TABLE OF CONTENTS...
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. INTRODUCTION This section includes informal advice and familiarization procedures; a mention of some flight characteristics and a copy of checklist procedures, for operating the Sting which are available in Appendix A.
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. Complete the pre-take-off checks and confirm that the safety pin is removed from the aircraft (GRS) ballistic recovery system.
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. Once at your altitude, set power to 75% and enjoy the flight. High cruise power is about 5200 to 5400 RPM.
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. Keep the power at idle and use pitch to keep your speed at 65Kts. Cross check the VVI.
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. Small throttle movements will generate large increases in speed and may cause you to over-shoot the glide path or the 65Kt flap limit.
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. on. Apply the brakes as firmly and evenly as is required for the desired stopping distance in coordination with the nose wheel steering to a perfect stop.
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. AIR MANUVERS STALL RECOVERY The primary indication of a stall in a Sting is a BURBLE and vibration of the airframe caused as the air begins to separate from the wing surface.
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. Pulling back abruptly could also result in a (high speed) secondary stall.
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. APPENDIX A STING OPERATIONAL CHECKLISTS THE FOLLOWING PAGES MAY BE...
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. EMERGENCY PROCEDURES AIRCRAFT PARACHUTE SYSTEM Slow the Aircraft, If Possible Ignition -- OFF...
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. FORCED LANDINGS EMERGENCY LANDING WITHOUT ENGINE POWER Airspeed -- 70 KIAS Landing Zone -- DETERMINE and FLY TOWARDS...
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. Power -- ESTABLISH MIN DESCENT RATE AT MIN SPEED Approach -- INTO WIND with high winds PARALLEL TO SWELLS with light winds Canopy -- UNLATCH...
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. ELECTRICAL FIRE IN FLIGHT Main Switch -- OFF All Switches Except Ignition Switches -- OFF Cabin Heat -- OFF...
Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. NORMAL PROCEDURES PREFLIGHT INSPECTION COCKPIT All Switches -- OFF...
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. RIGHT WING Main Fuel Tank -- CHECK QUANTITY / CORRECT FUEL TYPE Main Fuel Cap -- SECURE ELT –...
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. LEFT WING Flap and Hinges -- CHECK Aileron and Hinges -- CHECK Wing Tip Cover and Enclosed Lights -- CHECK...
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. PRE-TAXI Oil Pressure -- CHECK Transponder -- STANDBY VHF –...
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. TAKEOFF Flaps -- CHECK (HALF) Throttle -- FULL Rotate -- 45 KIAS Throttle -- MONITOR (5800 RPM maximum)
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Pilot Operating Handbook Section 10 TL-2000 Sting Supplementary Information 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. On base leg: Airspeed -- 65 KIAS Trim -- ADJUST TO AFT On final approach:...
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