TL Ultralight Sting TL-2000 2009 Pilot Operating Handbook

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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 Pilot Operating Handbook must remain in the aircraft and be accessible to the pilot all times.
31 December 2009 / Change 5
Copyright © 2009
Reproduction of this document or any of its parts is forbidden.

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Summary of Contents for TL Ultralight Sting TL-2000 2009

  • Page 1 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 Pilot Operating Handbook must remain in the aircraft and be accessible to the pilot all times. 31 December 2009 / Change 5 Copyright ©...
  • Page 2 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)
  • Page 3 Feel free to contact us if you have any questions or comments regarding your Sting aircraft. Fly safe! Fly fun! (sig) Jiri Tlusty TL Ultralight, sro Letištĕ, Budova c.84 509 41 Hradec Králové Czech Republic 31 December 09 / Chg 5 Copyright ©...
  • Page 4 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) 31 December 09 / Chg 5 Copyright ©...
  • Page 5 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 ................
  • Page 6 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 ®...
  • Page 7 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...
  • Page 8 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 ....
  • Page 9 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...
  • Page 10 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.) 31 December 09 / Chg 5 ____________________viii Copyright ©...
  • Page 11: Table Of Contents

    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) .............
  • Page 12: 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. Three View Drawings Sting S3 31 December 09 / Chg 5 Copyright ©...
  • Page 13: Three View Drawings (Sting Sport)

    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. Three View Drawings Sting Sport_______________________________ 31 December 09 / Chg 5 Copyright ©...
  • Page 14: Introduction

    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.
  • Page 15: Airplane Weights

    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 ..............
  • Page 16: Fuel

    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...
  • Page 17: Oil

    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.
  • Page 18: Symbols, Abbreviations, And Terminology

    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.
  • Page 19: Meteorlogical Terminology

    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.
  • Page 20: Airplane Performance And Weight Terminology

    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).
  • Page 21 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.
  • Page 22 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.
  • Page 23: Abbreviations

    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.
  • Page 24 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 –...
  • Page 25 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)
  • Page 26 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 –...
  • Page 27 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...
  • Page 28: Introduction

    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.
  • Page 29: Airspeed Indicator Markings

    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...
  • Page 30: Service Ceiling

    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.
  • Page 31 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.
  • Page 32: Center Of Gravity Limits

    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 ®...
  • Page 33: Maneuver Limits

    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.
  • Page 34 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.
  • Page 35 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...
  • Page 36 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. (THIS PAGE BLANK) 31 December 09 / Chg 5 Copyright ©...
  • Page 37: Introduction

    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.
  • Page 38: Aircraft Parachute System

    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).
  • Page 39: Engine Failures

    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.
  • Page 40: Engine Failure During Flight

    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.
  • Page 41: Forced Landings

    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.
  • Page 42: Precautionary Landing With Engine Power

    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”...
  • Page 43: Ditching

    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.
  • Page 44 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;...
  • Page 45: Fires

    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.
  • Page 46: Engine Fire In Flight

    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.
  • Page 47: Electrical Fire In Flight

    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.
  • Page 48: Cabin 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.
  • Page 49: Landing Gear Failure

    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.
  • Page 50 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.
  • Page 51: Spin Recovery

    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.
  • Page 52: Rough Engine Operation Or Loss Of Power

    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.
  • Page 53 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.
  • Page 54 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.
  • Page 55 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...
  • Page 56 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. (THIS PAGE BLANK) 31 December 09 / Chg 5_____________________________________________2 Copyright ©...
  • Page 57: Introduction

    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.
  • Page 58: Exterior Checklist

    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.
  • Page 59 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.
  • Page 60: Right Wing

    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.
  • Page 61 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.
  • Page 62: Aft Fuselage

    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.
  • Page 63: Operating Checklist

    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.
  • Page 64 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.
  • Page 65 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.
  • Page 66: Pre-Taxi

    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.
  • Page 67: Taxi

    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.
  • Page 68: Engine Run-Up

    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.
  • Page 69: Before Takeoff

    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.
  • Page 70: Takeoff

    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.
  • Page 71: Soft Field Takeoff

    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.
  • Page 72: Cruise

    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.
  • Page 73: Before Landing

    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.
  • Page 74 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.
  • Page 75: Crosswind Landing

    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.
  • Page 76 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.
  • Page 77 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.
  • Page 78 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.
  • Page 79 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 ....................
  • Page 80 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. (THIS PAGE BLANK) 31 December 09 / Chg 5 Copyright ©...
  • Page 81 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.
  • Page 82 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. (This Page Blank.) 31 December 09 / Chg 5 Copyright ©...
  • Page 83 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 &...
  • Page 84 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 Copyright ©...
  • Page 85: Introduction

    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.
  • Page 86: Auxiliary Items

    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.
  • Page 87 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.
  • Page 88: Procedure

    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.
  • Page 89: Empty Weight Center Of Gravity Calculations

    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.
  • Page 90: Loaded Weight And Balance Calculations

    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.
  • Page 91: Critical Loading Conditions

    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.
  • Page 92: Weight & Balance Data Worksheet Notes

    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.
  • Page 93: Sting Moment Arm Data Sheet

    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...
  • Page 94 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 &...
  • Page 95 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 &...
  • Page 96 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...
  • Page 97 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 &...
  • Page 98 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 ______ Copyright ©...
  • Page 99: Introduction

    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.
  • Page 100: Trim 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. 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.
  • Page 101: Wing Flap 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. Sting flight instruments are arranged in the basic “T” configuration on the pilot (left) side of the aircraft.
  • Page 102: Landing Gear

    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.
  • Page 103: Canopy

    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.
  • Page 104: Engine Instruments

    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.
  • Page 105: Ignition-Starter 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. 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.
  • Page 106: Carburetor 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. CARBURETOR SYSTEM The aircraft’s Rotax ®...
  • Page 107: Fuel 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. FUEL SYSTEM The aircraft’s fuel system consists of one vented, 20.5 gallon main tank;...
  • Page 108 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.
  • Page 109 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 ______...
  • Page 110: Brake 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. 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.
  • Page 111 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 ______...
  • Page 112: Electrical System And Instruments

    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.
  • Page 113: Circuit Breakers And Fuses

    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.
  • Page 114: Airspeed Indicator

    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.
  • Page 115: Avionics Equipment

    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.
  • Page 116 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...
  • Page 117 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 &...
  • Page 118 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. (THIS PAGE BLANK) 31 December 09 / Chg 5 Copyright ©...
  • Page 119 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.
  • Page 120 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...
  • Page 121 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):...
  • Page 122 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...
  • Page 123 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 &...
  • Page 124 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. (THIS PAGE BLANK) 31 December 09 / Chg 5 Copyright ©...
  • Page 125: Introduction

    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.
  • Page 126: Ground Handling

    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...
  • Page 127: Servicing

    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...
  • Page 128 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...
  • Page 129 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.
  • Page 130 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.
  • Page 131: Engine Coolant

    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.
  • Page 132: Fuel

    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.
  • Page 133: Tire Pressures

    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.
  • Page 134: Propeller Care

    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.
  • Page 135 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...
  • Page 136 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. (THIS PAGE BLANK) 31 December 09 / Chg 5 10-2 Copyright ©...
  • Page 137: Introduction

    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.
  • Page 138: Takeoff

    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.
  • Page 139: Descent

    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.
  • Page 140: Base

    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.
  • Page 141: Landing

    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.
  • Page 142: Turn 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. 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.
  • Page 143: Air Manuvers

    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.
  • Page 144: Bounce Recovery On Landing

    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.
  • Page 145 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...
  • Page 146: Emergency Proceedures

    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...
  • Page 147 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...
  • Page 148 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...
  • Page 149 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...
  • Page 150: Normal Proceedures

    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...
  • Page 151 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 –...
  • Page 152 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...
  • Page 153 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 –...
  • Page 154 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)
  • Page 155 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:...
  • Page 156 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. (This Page Blank.) 31 December 09 / Chg 5 10-22 Copyright ©...

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