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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.

31 December 09 / Chg 5

______

7-5

Sting flight instruments are arranged in the basic “T” configuration on the pilot (left)

side of the aircraft. Exceptions can include the absence of a particular instrument

or a variation in the order of the instruments at customer request.

Flight instruments will be arranged in this configuration (starting from the pilot-side

top left): airspeed indicator (ASI), attitude indicator (ADI), altimeter (ALT), (to the

second row from the left) turn coordinator (TC), tachometer (TACH), and vertical

speed indicator (VSI). The Sting also includes a slip indicator and remote ELT

control and front vent lever on the pilot-side panel.

Other items located on the instrument panel are the avionics stack in the center

panel. This is made up of the GPS, Engine Information System (EMS) display, (a

red EMS alert light may also be installed), a red battery discharge (low voltage)

light, a green auxiliary fuel pump “ON” light, VHF radio, and transponder.

Along the base of the center panel are the starter push button, guarded left and

right ignition switches, guarded main and instrument switches, a guarded strobe

light switch, and the unguarded aux engine fuel pump switch. Below the center

panel are the fuel shut-off valve, fuel gauge, “choke” knob, and cabin heat control.

The aux fuel pump will always be located on the last right position and will be

unguarded for immediate access. All Stings will have this switch arrangement.

A Hobbs meter, fuel pressure gauge (FP), manifold pressure gauge (MP), the

intercom control, circuit breakers, are all located on the co-pilot’s panel.

Optional glass cockpit installations may be installed. See the supplied owner’s

manuals for details and instructions on each system operation.

WING FLAP SYSTEM

The aircraft utilizes split-type flaps that are controlled by a three-position lever

positioned next to the arm rest in between the crew seats. The lever has a locking

button that prevents the flaps from being operated inadvertently. When the lever is

locked down in the first position, the flaps are totally retracted. In order to extend

the flaps to Half (15°), press the button in and move the lever up to the second

locked position. From this position, the flaps may either be extended to Full (30°)

or retracted. To fully extend the flaps (Full) the button again must be depressed

and the lever moved up to the third, locked position.

Содержание Sting TL-2000 2009

Страница 1: ...ference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 2009 Change 5 Copyright 2009 Reproduction of this document or any of...

Страница 2: ...tion 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 th...

Страница 3: ...lying and enjoyment With this Pilot Operating Handbook POH we hope to help inform you about the design and operation of your aircraft This Pilot Operating Handbook is to be used as a guide to assist t...

Страница 4: ...ation contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 ii Copyright 2009...

Страница 5: ...afe operation of this aircraft 31 December 09 Chg 5 iii Copyright 2009 Reproduction of this document or any of its parts is forbidden SECTION INDEX SECTION GENERAL 1 OPERATING LIMITATIONS 2 EMERGENCY...

Страница 6: ...conditions steps in a procedure helpful hints or useful advice This text box represents danger to equipment or operation By not observing the cautions the result could be the destruction of equipment...

Страница 7: ...to by the operator or pilot in command PIC Each aircraft is issued an FAA form 8050 15 which is a statement identifying the specific ASTM standard used in design and manufacture of that seral aircraft...

Страница 8: ...2 31 09 4 6 12 31 09 4 7 12 31 09 4 8 12 31 09 4 9 12 31 09 4 10 12 31 09 4 11 12 31 09 4 12 12 31 09 4 13 12 31 09 4 14 12 31 09 4 15 12 31 09 4 16 12 31 09 4 17 12 31 09 4 18 12 31 09 4 19 12 31 09...

Страница 9: ...ft 31 December 09 Chg 5 ____________________vii Copyright 2009 Reproduction of this document or any of its parts is forbidden List of changes CHG NR REVISED DATE REVISED PAGES EXTENT OF REVISION CHANG...

Страница 10: ...ined in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 ____________________viii Copy...

Страница 11: ...ion of this document or any of its parts is forbidden SECTION 1 GENERAL INFORMATION TABLE OF CONTENTS Page THREE VIEW DRAWINGS Sting S3 1 2 THREE VIEW DRAWINGS Sting Sport 1 3 INTRODUCTION 1 4 DESCRIP...

Страница 12: ...tained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 1 2 Copyright 2009 Reproduc...

Страница 13: ...cument is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 1 3 Copyright 2009 Reproduction of this docu...

Страница 14: ...hich are included with the aircraft Any conflicts found in these supplier manuals are superseded by the appropriate OEM manufacturer s POH or AMM manuals The Sting is has a high cruising speed and may...

Страница 15: ...aximum Takeoff or Landing Weight 1320 Lbs Standard Empty Weight 780 Lbs Maximum Useful Load 540 Lbs Total Baggage Weight 60 Lbs Each baggage compartment can hold a maximum of 20 Lbs An additional 20 L...

Страница 16: ...RPM and may not allow a safe takeoff Loading the engine with a high propeller pitch angle high propeller angle of attack AOA or big angle above 21 5 may also result in may result in extremely long tak...

Страница 17: ...an be filled with approximately 21 5 gallons of fuel This will eliminate all fuel expansion area as the fuel expands it will be forced out of the fuel vent line and spill on to the parking area causin...

Страница 18: ...ecured against an abrupt movement Do not allow baggage to block the exit area of the aircraft parachute system nor hinder free deployment of the parachute riser cables After securing baggage assure th...

Страница 19: ...Flight VH The highest speed that can be attained in level flight at sea level under standard conditions while the engine is operating at the manufacturer designated maximum continuous power setting N...

Страница 20: ...el 91 Octane is min auto gas rating for Rotax engines Avgas 100 Octane Low Lead Aviation Fuel 100LL Max 30 use in Rotax Ballast A specific amount of weight attached in a specific location which can be...

Страница 21: ...datum for the Sting Demonstrated Crosswind Velocity The velocity of the crosswind component at which adequate control of the airplane was actually demonstrated during takeoff and landing certification...

Страница 22: ...un up fuel Maximum Takeoff Weight The maximum weight at which an airplane is approved for the start of its takeoff roll Moment The product of the weight of an item multiplied by its arm distance from...

Страница 23: ...p Weight Basic Empty Weight Useful Load The useful load will be reduced by the installation of additional equipment Usable Fuel The amount of fuel available for engine use in flight Unusable Fuel The...

Страница 24: ...e ASTM Standards Datum Location base for measurement s DC Direct Current DOT Department of Transportation US EIS Engine Information System EFIS Electronic Flight Information System EMS Engine Monitori...

Страница 25: ...nots True Kg Kilogram KM Kilometer Kt Knot nautical mile Lb s Pound s LL Low Lead as in 100LL LSA Light Sport Aircraft LSP Light Sport Plane M Meter MAC Mean Aerodynamic Chord MAG Magnetic slang engin...

Страница 26: ...orbidden PSI Pounds per Square Inch RPM Revolutions per Minute STRB Strobe switch STRT Start switch T B Turn and bank indicator Tach Tachometer TC Turn Coordinator TCP Fuel Additive Tri Cresyl Phospha...

Страница 27: ...aircraft 31 December 09 Chg 5 2 1 Copyright 2009 Reproduction of this document or any of its parts is forbidden SECTION 2 OPERATING LIMITATIONS TABLE OF CONTENTS Page INTRODUCTION 2 AIRSPEED LIMITATI...

Страница 28: ...on IFR operations See page 2 7 for further details AIRSPEED LIMITATIONS V SPEED KIAS KCAS REMARKS VNE Never Exceed Speed 164 162 Do not exceed this speed in any operation VNO Maximum Structural Cruisi...

Страница 29: ...one Takeoff Approach setting Green Arc 44 118 43 117 Normal Operating Range Lower limit is maximum weight VS at most forward CG with flaps retracted Upper limit is maximum structural cruising speed VC...

Страница 30: ...acturer s manual supplied with the aircraft for more detailed Rotax engine data Engine Manufacturer Rotax G m b H Aircraft Engines Engine Model Number 912 UL or ULS 914UL Maximum Power 80 100 or 115 B...

Страница 31: ...ation time by the engine manufacturer If 91 Octane Unleaded is not available during travel adding 100LL Avgas in any proportion to partial tanks of 91 Unleaded is acceptable Following use of Avgas dur...

Страница 32: ...n a higher cruise speed may cause the engine RPM to bog down fail to reach a sufficient ground RPM and will not allow a safe takeoff Loading the engine with a high propeller pitch high propeller angle...

Страница 33: ...ation not necessary for normal flight FLIGHT LOAD FACTOR LIMITS Flight Load Factors Flaps Up 4g 2g Flaps Down 4g 2g FLIGHT LIMITATIONS The Sting is certified only for VFR VMC or IFR VMC flight conditi...

Страница 34: ...cument or any of its parts is forbidden Limited IFR IMC operations may be approved by the OEM manufacturer for specific aircraft meeting appropriate ASTM FAA standards Such operations will continue to...

Страница 35: ...ILURES 5 ENGINE FAILURE DURING TAKEOFF ABORT 5 ENGINE FAILURE LANDING IMMEDIATELY AFTER TAKEOFF 6 ENGINE FAILURE DURING FLIGHT 6 FORCED LANDINGS 7 EMERGENCY LANDING WITHOUT ENGINE POWER 7 PRECAUTIONAR...

Страница 36: ...rmation contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 __ 3 2 Copyright...

Страница 37: ...ion should be considered and applied as necessary to correct the problem Due to the fact that emergencies can occur at any altitude or any moment procedures to follow may have to be suitably altered b...

Страница 38: ...y the Galaxy High Technology GRS Corporation It is imperative that the owner pilot of this airplane read and understand the system operating manual provided by Galaxy In most emergency scenarios the u...

Страница 39: ...a nose low attitude and sufficient airflow over the control surfaces exists limited control in flight may be accomplished If this is possible make every effort to guide the airplane toward an isolated...

Страница 40: ...Switch OFF The aircraft is capable of very high takeoff climb deck angles or AOA at low speeds Loss of engine power will result in loss of airspeed very quickly due to the nose high attitude Be prepar...

Страница 41: ...e the auxiliary fuel pump is ON for takeoff Ensure that both ignition switches are on and then engage the starter button If the engine still will not start complete the forced landing procedures detai...

Страница 42: ...anding Do not dive toward the landing zone if at too high an altitude in order to attempt a safe landing Doing so will result in a high energy high speed approach that is not likely to allow the aircr...

Страница 43: ...st Even though it may be possible to obtain a higher speed than VG do not fly the airplane faster This procedure will provide the maximum travel distance If the engine can produce sufficient thrust ma...

Страница 44: ...down procedures Add Full flaps and establish a steady slow 200fpm descent rate at an airspeed of 55 KIAS This is done to allow for a slow airspeed with a slow descent rate prior to the water surface i...

Страница 45: ...r OBTAIN 11 Airplane EVACUATE 12 Fire Extinguisher USE AS REQUIRED 13 Airplane INSPECT FOR DAMAGE If a fire occurs while starting the engine continue to crank the engine to attempt to draw the fire ba...

Страница 46: ...y DIVE the aircraft to a lower altitude to minimize the time for the fire to spread within the cockpit 1 Fuel Valve OFF 2 Throttle FULL OPEN 3 Aux Fuel Pump OFF 4 Ignition Switches OFF 5 Cabin Heat OF...

Страница 47: ...ransponder to alert ATC of the emergency Proceed with the forced landing that has been established ELECTRICAL FIRE IN FLIGHT 1 Main Switch OFF 2 All Switches Except Ignition Switches OFF 3 Cabin Heat...

Страница 48: ...s turned on Be prepared for an emergency landing and land as soon as possible If you choose to troubleshoot any problem when airborne remember that the main priority in any airborne situation is to fl...

Страница 49: ...en damaged consider using a smooth sod runway if available Touchdown on the undamaged gear first This can be accomplished by using aileron to bank into the good gear and using opposite rudder to keep...

Страница 50: ...raft to maintain 70 KIAS 6 Upon re entering VFR VMC conditions resume normal cruise operation Close the throttle to prevent any further increase in airspeed produced by the engine Because it presents...

Страница 51: ...Should an inadvertent spin occur in this airplane the following recovery procedure should be used 1 Throttle IDLE 2 Ailerons NEUTRALIZE 3 Rudder APPLY FULL in opposite direction of rotation 4 Elevator...

Страница 52: ...turning each ignition switch OFF and then back ON one at a time An obvious power loss in single ignition operation is evidence of spark plug or ignition module trouble If the problem persists proceed...

Страница 53: ...E reduce power and speed immediately Do not attempt abrupt control movement or unusual attitudes Continue flight using minimum safe speed and control pressures to land as soon as possible After landin...

Страница 54: ...ircraft 31 December 09 Chg 5 __ 3 20 Copyright 2009 Reproduction of this document or any of its parts is forbidden vibration if it is a wheel spinning The nose wheel may also rotate and vibrate above...

Страница 55: ...its parts is forbidden SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS Page INTRODUCTION 3 AIRSPEEDS FOR NORMAL OPERATION 3 PREFLIGHT INSPECTION 3 COCKPIT 3 EXTERIOR CHECKLIST 4 NOSE AREA 4 RIGHT WING 6...

Страница 56: ...this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5______________________________________...

Страница 57: ...Design Cruise Speed VC 95 115 KIAS Landing and Approach Flaps Up Emergency only 70 KIAS Flaps Half Normal for all approaches 60 KIAS Flaps Full Normal for all landings 55 KIAS Balked Landing Maximum...

Страница 58: ...l panel indicator located on the instrument panel to determine the ELT s status Cross check this status with the actual ELT by removing the passenger seat back to locate the ELT Ensure the ON ARMED OF...

Страница 59: ...ne should only use a small amount of oil during normal operation For longer flights it may be advisable to add oil until it reaches its maximum limit on the dipstick to allow for some oil consumption...

Страница 60: ...eel in either direction Comply with proper environmental fuel disposal regulations and do not dump fuel onto the ground When draining the fuel sump always use a clean clear fuel sampler Pour clean fue...

Страница 61: ...screws that fasten the wheel pant bracket to the gear assembly should all be tight Confirm that the grounding wire attached inboard to the right gear assembly is securely fastened It should make suffi...

Страница 62: ...ttempt to move the rudder The rudder is directly connected to the nose wheel so there will only be slight rudder travel The horizontal stabilizer and trim tab should also be free of cracks and punctur...

Страница 63: ...are operational Inspect the wing s leading edge for flaws or damage These can impede smooth airflow over the wing The bolt and two screws that fasten the wheel pant bracket to the gear assembly shoul...

Страница 64: ...canopy remains unattended unlocked open in the wind or during taxi operations 2 Harnesses ADJUST and FASTEN 3 Headsets ON and ADJUST 4 All Switches OFF 5 Fuel Valve ON 6 Throttle IDLE 7 Main Switch ON...

Страница 65: ...nition The choke is by passed and will not be activated at high RPM throttle positions Open the fuel valve and momentarily turn on the auxiliary fuel pump to pump fuel into the engine The fuel pump wi...

Страница 66: ...warm up and then try closing the choke again Always be observant of the oil pressure temperature and cylinder head temperatures on the EMS data display during engine operation PRE TAXI 1 Oil Pressure...

Страница 67: ...latch to exit the cockpit Allow a minimum of two minutes for the engine to warm up sufficiently prior to engine run up in order to stabilize internal engine temperatures This can include time during...

Страница 68: ...min 3 Oil Pressure 29 73 PSI 4 Cylinder Head Temperature 110 F min 5 Throttle 4000 RPM 6 Ignition Switches 300 RPM DROP max 120 RPM DIFF max 7 Throttle 2000 RPM 8 Fuel Pressure CHECK 9 GRS Safety Pin...

Страница 69: ...should be determined BEFORE TAKEOFF 1 Harnesses SECURE 2 Loose Items SECURE 3 Instruments CHECK and SET 4 EMS Data CHECK 5 VHF Radio SET 6 Transponder ON ALT 7 Trim AFT 8 Flaps HALF 9 Controls FREE an...

Страница 70: ...igh engine temperatures and cause the engine to fail on full throttle application Watch for erratic rpm or rough operation when increasing the throttle Auto fuel vapor lock is the result of seasonal o...

Страница 71: ...runway Maintain elevator back pressure and when clear for takeoff add enough power to just get the airplane moving As the airplane steadily accelerates smoothly add full power As airspeed increases r...

Страница 72: ...re gravity fed They will automatically feed as the main tank is depleted The main tank will continue to indicate FULL for the time that the aux tanks are draining If installed the aux wing tank pumps...

Страница 73: ...rnesses SECURE 2 Airspeed 75 KIAS 3 Fuel CHECK QUANTITY 4 Secure Loose Items 5 Aux Fuel Pump ON 6 Strobe Lights ON Prior to entering the traffic pattern ensure that the seat belts and shoulder harness...

Страница 74: ...pe On final approach 6 Airspeed 60 KIAS 7 Flaps FULL 8 Trim AFT AS REQUIRED 9 Throttle IDLE or as required 10 Airspeed 55 KIAS on short final 11 Touchdown MAIN WHEELS FIRST NOSE HIGH 12 Braking MINIMU...

Страница 75: ...y breaking may cause exceptionally fast tire and brake wear and may result in a tire failure CROSSWIND LANDING If a strong crosswind exists during landing it is practical to use the minimum flap setti...

Страница 76: ...tive rate stabilized climb 2 Flaps SET TO HALF 3 Airspeed 50 KTS VX 4 Flaps RETRACT WHEN CLEAR OF OBSTACLES 5 Airspeed 55 KTS VY 6 If a go around is executed full power should be applied a climb at VX...

Страница 77: ...hut Off Valve may attach to the metal of the valve stem if allowed to remain in a fixed position for an extended time If the aircraft is inactive for a time and the valve is quickly moved to a new pos...

Страница 78: ...headsets reinsert the GRS safety pin into the activation handle When opening the canopy reverse your method of the closing sequence It is imperative that the GRS safety pin be reinserted into its resp...

Страница 79: ...he pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 5 1 Copyright 2009 Reproduction of this document or any of its parts is forbidden SECTION...

Страница 80: ...tion contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 5 2 Copyright 2009...

Страница 81: ...eoff Distance Over a 50ft Obstacle 9400 Ft Max power Half flaps paved runway RATE OF CLIMB Rate of Climb 810FPM at 55Kts VY Max power Half flaps CRUISE SPEED Design Cruise Speed 95 115 KIAS Maximum Cr...

Страница 82: ...tion contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 5 4 Copyright 2009...

Страница 83: ...2009 Reproduction of this document or any of its parts is forbidden SECTION 6 WEIGHT BALANCE INFORMATION TABLE OF CONTENTS Page INTRODUCTION 3 STANDARD INSTALLED EQUIPMENT LIST 3 AUXILIARY ITEMS 4 WEI...

Страница 84: ...information contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 6 2 Copyrig...

Страница 85: ...WER PORT 2 AUXILIARY 12V EXTERNAL POWER CONNECTION AUXILIARY ENGINE FUEL PUMP AUX AUXILIARY WING FUELTANKS FILTER PUMP If Installed CABIN HEAT SYSTEM CARGO BAGGAGE BOXES 2 EMERGENCY LOCATOR TRANSMITTE...

Страница 86: ...result from specific weights and forces anticipated to occur in normal operations within its specified flight envelope An aircraft s handling qualities and structural integrity may be seriously compr...

Страница 87: ...aximum and Minimum Weights Due to certain balance structural and aerodynamic considerations sometimes a manufacturer may specify maximum or minimum weights for certain locations on the aircraft For ex...

Страница 88: ...alled must also be listed Ballast A specific amount of weight attached in a specific location which can be temporarily or permanently installed in an aircraft to help bring its CG within the required...

Страница 89: ...easurements For best results weigh indoors The scales must be calibrated correctly and must be set on level ground Any equipment placed on the scales when weighing the aircraft such as chocks or block...

Страница 90: ...ocation 66498 Total Moment 805 Empty Weight 82 6 inches aft of Datum Plane Figure 6 1 Example of Initial Empty Weights LOADED WEIGHT AND BALANCE CALCULATIONS Complete the Loaded CG calculations as was...

Страница 91: ...omplete this chart for each of critical test loading conditions to be sure that your final Loaded CG position falls within the allowable CG limits at all times for all operations CRITICAL LOADING COND...

Страница 92: ...performing the calculation An entry moment arm is included in the sample should any changes be made to the instrument panel This document in its entirety becomes a part of the Aircraft Legal Document...

Страница 93: ...contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 6 11 Copyright 2009 Rep...

Страница 94: ...4 2 30803 Right Gear 326 94 2 30709 Empty A C 805 82 6 66498 Instrument Changes 59 5 Main Fuel 120 68 4 8208 Wing Fuel 0 80 1 0 Pilot 1 195 90 1 17570 Pilot 2 175 90 1 15768 Baggage 25 117 0 2925 Tota...

Страница 95: ...Item Weight Arm Moment Nose Wheel 32 8 Left Gear 94 2 Right Gear 94 2 __________ Empty A C Instrument Changes 59 5 Main Fuel 68 4 Wing Fuel 80 1 Pilot 1 90 1 Pilot 2 90 1 Baggage 117 0 __________ Tota...

Страница 96: ...information contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 6 14 Copyrig...

Страница 97: ...ON 3 AIRFRAME 3 FLIGHT CONTROLS 3 TRIM SYSTEM 4 GROUND CONTROL 4 INSTRUMENT PANEL 4 WING FLAP SYSTEM 5 LANDING GEAR 6 SAFETY HARNESSES 6 CANOPY 7 ENGINE 7 ENGINE CONTROLS 7 ENGINE INSTRUMENTS 8 ENGINE...

Страница 98: ...ation contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 ______ 7 2 Copyrig...

Страница 99: ...the wing tip and is about a foot longer The area of both wings is exactly the same The wings are attached to the fuselage by two interlocking box type spars that cross beneath the cockpit and interlo...

Страница 100: ...is operated by two control rods connected between each of the rudder pedals to either side of the nose wheel hinge The rudder and nose wheel steering operate as follows to turn left the left pedal is...

Страница 101: ...ON light VHF radio and transponder Along the base of the center panel are the starter push button guarded left and right ignition switches guarded main and instrument switches a guarded strobe light s...

Страница 102: ...nd the right toe pedal will actuate the right main landing gear brake SAFETY HARNESSES Each seat in the aircraft is equipped with a four point safety harness Each of the shoulder harnesses is latched...

Страница 103: ...powered by a normally aspirated liquid air cooled gear reduced drive dual carburetor equipped four cylinder four stroke horizontally opposed Rotax 912UL S engine and is rated at 80 100 BHP at 5800 RP...

Страница 104: ...ed the EMS will alert with a light or change color to illuminate affected display If installed a difference of as much as 200 RPM can exist between the Rotax tachometer and the RPM indication on the E...

Страница 105: ...in isolating engine deficiencies Starter operation is controlled by a momentary push button The starter solenoid is then energized which in turn activates the starter AIR INDUCTION EXHAUST SYSTEM Unli...

Страница 106: ...ith a small starting carburetor commonly referred to as a choke for starting Starting a cold engine may be difficult and the cylinders may need more fuel than air to burn A starting carburetor is used...

Страница 107: ...n requires it to be off The fuel shut off can remain in the ON position to prevent damage of the rubber O ring by quick rotation Fuel will not drain overboard with the fuel shut off in the ON position...

Страница 108: ...sion To break the siphon open the main tank cap lock lever don t remove the cap and raise the nose by pushing down on the tail area ahead of the vertical fin Do not sit on the horizontal tail surfaces...

Страница 109: ...ntained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 ______ 7 13 Copyright 2009...

Страница 110: ...pull knob is located forward of the left pilot s armrest which is connected to the vent by a Bowden cable control wire By pulling the knob aft the vent opens to close the vent push the knob forward Wa...

Страница 111: ...ned in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 ______ 7 15 Copyright 2009 Rep...

Страница 112: ...t and left vertical surface of each seat The pilot side port is directly hot wired to the battery and can be used to charge the battery without the pilot having to connect additional leads directly to...

Страница 113: ...nd decreased drag The center panel has a STRB ON OFF circuit breaker switch CBS for the strobe lights Night lighting for the instruments is provided and dimmable Internal lighting of the cockpit is pr...

Страница 114: ...As altitude decreases the aneroid wafers will contract Atmospheric pressure is supplied to the altimeter by the static ports on the pitot tube or aft on the fuselage Mechanical linkages attached to th...

Страница 115: ...he transponder contains a computerized altimeter connected to the pitot static system that allows it to calculate the aircraft s altitude This data is then transmitted to the ground radar of ATC This...

Страница 116: ...ation contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 ______ 7 20 Copyri...

Страница 117: ...s for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 8 1 Copyright 2009 Reproduction of this document or...

Страница 118: ...information contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 8 2 Copyrig...

Страница 119: ...ds and markings located inside the cockpit and on the exterior of the airplane These placards and markings provide guidance instruction or caution It is the responsibility of the owner pilot to unders...

Страница 120: ...f this aircraft 31 December 09 Chg 5 8 4 Copyright 2009 Reproduction of this document or any of its parts is forbidden Aux wing fuel tank filler neck rims FUEL CAPACITY 6 US GALLONS Main landing gear...

Страница 121: ...formation only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 8 5 Copyright 2009 Reproduction of this document or any of its parts is fo...

Страница 122: ...rmation only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 8 6 Copyright 2009 Reproduction of this document or any of its parts is forb...

Страница 123: ...Copyright 2009 Reproduction of this document or any of its parts is forbidden SECTION 9 AIRPLANE HANDLING SERVICE MAINTENANCE TABLE OF CONTENTS Page INTRODUCTION 3 AIRPLANE FILES 3 AIRPLANE INSPECTION...

Страница 124: ...e The information contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 9 2 Co...

Страница 125: ...Pilot Operating Handbook POH 2 Weight and Balance Data 3 Operating Limitations issued by FAA at airworthiness inspection 4 Aircraft Airworthiness Certificate FAA Form 8130 7 5 Aircraft Registration Ce...

Страница 126: ...he best precaution to prevent damage Metal screw rings are located underneath each wing tip for fastening tie down straps or ropes The nose gear can be tied down by attaching a rope or strap around an...

Страница 127: ...ted with leaded Avgas fuels The lead contained in Avgas will deposit in the piston rings and in the rocker arms of the valve train Use Avgas only while traveling when unleaded fuel is not available Wh...

Страница 128: ...aded unleaded fuel SHELL Advance VSX 4 APISG SAE 15W 50 Semi synthetic motorcycle oil w gear additives for normal high temps leaded unleaded fuel SHELL Advance Ultra 4 APISJ SAE 10W 40 Full synthetic...

Страница 129: ...s leaded unleaded fuel SHELL Formula Shell APISJ SAE 10W 30 Petroleum based oil for normal temps leaded fuel only SHELL Formula Shell APISJ SAE 20W 50 Petroleum based oil for normal temps leaded fuel...

Страница 130: ...ated at the rear of the firewall Remove the dipstick to check the oil level A flattened segment at the end of the dipstick represents the oil capacity range The top of this segment is the MAX limit an...

Страница 131: ...engine oil before installation To ensure a better seal rub fresh oil around the sealing ring of the new oil filter 8 Snuggly screw on new oil filter by hand Turn until hand tight and the seal is comp...

Страница 132: ...is a waterless coolant and may not be recognized by line personnel prior to the addition of water to top off the system To add engine coolant 1 Remove the cap and inner screen of the coolant system s...

Страница 133: ...torage Run the engine long enough on Avgas to fill the carb bowls before storage TIRE PRESSURES Nose Wheel Tire Pressure 30 psi 2 bar Main Gear Wheel Tire Pressure 30 psi 2 bar CLEANING AND CARE CANOP...

Страница 134: ...electric problems Check coolant brake fluid and engine oil levels to determine if there are any losses Clean the radiator vanes from bugs and debris using a low pressure water hose and a cloth Never...

Страница 135: ...mber 09 Chg 5 10 1 Copyright 2009 Reproduction of this document or any of its parts is forbidden SECTION 10 SUPPLEMENTARY INFORMATION TABLE OF CONTENTS Page INTRODUCTION 3 FAMILIARIZATION FLIGHT PROCE...

Страница 136: ...information contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 10 2 Copyrig...

Страница 137: ...attering noise if you unintentionally ride the brakes while taxiing It is an irritant not a serious problem and can be fixed by removing the pads and scrubbing them with a file to remove the glaze Use...

Страница 138: ...er the nose if the engine performance diminishes It is better to climb at a higher speed than a lower speed for safety So don t continue a Vy climb any longer than necessary to clear any obstacle Main...

Страница 139: ...in that situation and plan the decent to remain well below Vne If you anticipate the descent you will also be in a good position to handle any turbulence at a reasonable airspeed that is not high int...

Страница 140: ...turns you have to make If you find that you are overshooting the final approach course don t tighten the turn just continue the turn through the runway heading to an intercept angle from the other sid...

Страница 141: ...t the Sting will continue to fly well below the speed of the approach and flare You will be using that difference in speed energy to maneuver the plane during the last few inches above the runway The...

Страница 142: ...ent at some uncontrolled runways does not allow direct vision of all the exit taxiways from the runway hold position PARKING As in the taxi for takeoff do not let the ground speed increase as you retu...

Страница 143: ...tall and the other will continue to produce lift The result can be a roll into the stalled wing that is initially disturbing to new pilots because the large canopy gives you no sense of enclosure Do n...

Страница 144: ...RECOVERY ON LANDING Occasionally an airplane will bounce when forced into a hard landing The primary concern after an initial bounce on the runway is to recover go around and attempt a second landing...

Страница 145: ...and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 10 11 Copyright 2009 Reproduction of this document or any of its pa...

Страница 146: ...Ignition OFF 2 Harnesses TIGHTEN 3 GRS Activation Handle PULL FIRMLY 25 POUNDS 4 Radio SET TO 121 5 TRANSMIT MAYDAY MAYDAY MAYDAY with AIRCRAFT ID and CURRENT POSITION 5 Transponder SET TO 7700 6 Gli...

Страница 147: ...O 7700 7 Landing Zone CIRCLE OVER if possible BEFORE LANDING 8 All Switches OFF 9 Harnesses TIGHTEN 10 Flaps FULL on final 11 Touchdown PREFERABLY INTO WIND NOSE HIGH 12 Brakes APPLY AS REQUIRED PRECA...

Страница 148: ...EVACUATE 13 Anticipate that the aircraft may be inverted FIRES ENGINE FIRE DURING START 1 Starter CONTINUE CRANKING If engine starts 2 Power 2000 RPM for a few seconds 3 Fuel Valve OFF 4 Engine SHUTD...

Страница 149: ...inues 7 Land ASAP If fire appears out and electrical power is necessary for extended flight 8 Main Switch OFF 9 All Switches Except Ignition Switches OFF 10 Circuit Breakers CHECK for faulty circuit d...

Страница 150: ...T Control Panel Indicator CHECK STATUS 6 Main Switch OFF 7 Flight Controls PROPER OPERATION 8 Flaps PROPER OPERATION SET FULL 9 Trim CENTERED 10 Required Documentation ON BOARD 11 Baggage SECURED 12 S...

Страница 151: ...LATION and WEAR 9 Chock REMOVE 10 Wing Leading Edge CHECK 11 Wing Aux Tank if installed CHECK QUANTITIY FUEL TYPE 12 Wing Aux Tank Cap SECURE 13 Under wing Inspection Ports SECURE CHECK CONTINUITY 14...

Страница 152: ...CONTINUITY 7 Wing Aux Tank if installed CHECK QUANTITIY FUEL TYPE 8 Wing Aux Tank Cap SECURE 9 Gear Leg and Brake Line CHECK 10 Wheel Pant and Bracket SECURE 11 Brake Pads and Disk CHECK FOR WEAR 12 T...

Страница 153: ...Safety Pin REMOVED and STOWED TAXI 1 Area CLEAR 2 Brakes CHECK and APPLY AS NEEDED 3 Steering CHECK 4 Compass CHECK 5 attitude reference Track Display CHECK 6 Turn Coordinator CHECK in turns 7 GRS Sa...

Страница 154: ...ps RETRACT SMOOTHLY AT 500 AGL CLIMB 1 Throttle SET TO 5500 RPM or as required 2 Climb 75 KIAS 3 Trim ADJUST AS NEEDED 4 EMS Data CHECK 5 Aux Fuel Pump ON CRUISE 1 Throttle 5200 TO 5400 RPM 2 Trim LEV...

Страница 155: ...9 Throttle IDLE or as required 10 Airspeed 55 KIAS on short final 11 Touchdown MAIN WHEELS FIRST NOSE HIGH 12 Braking MINIMUM BALKED GO AROUND LANDING 1 Throttle FULL 2 Flaps SET TO HALF 3 Airspeed 5...

Страница 156: ...information contained in this document is for reference and information only The pilot is the final and only responsible party for the safe operation of this aircraft 31 December 09 Chg 5 10 22 Copyri...

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