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for SPORT

STAR

Light Sport Aircraft

Document No.: S2006FTSUS Revision: -

Date of Issue: 15/01/2006

Page:

36/130

4.4.5.2.3 Directional Control – Rudder Control System

Picture: Left rudder pedal deflected
forward– airplane yaws and banks left

And corresponding deflection of
rudder to the left.

Picture: Right rudder pedal deflected
forward– airplane yaws and banks
right

And corresponding deflection of
rudder to the right.

Содержание SPORTSTAR

Страница 1: ...vektor cz Leteck 1384 686 04 Kunovice CZECH REPUBLIC http www evektor cz Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 0 130 F FL LI IG GH HT T T TR RA AI IN NI IN NG G S SU UP PP PL L...

Страница 2: ...training 9 3 1 Introduction to Flight Training 9 3 2 About the Sport Pilot certificate 10 4 Flight Training on SPORTSTAR 18 4 1 Sportstar Purpose of Use 18 4 2 Sportstar limitations 19 4 3 Ground Tra...

Страница 3: ...pecific features and characteristics which will help them to learn to fly with in the airplane or transition to it from another plane This supplement does not propose to substitute for more comprehens...

Страница 4: ...Inspection Procedures for SPORTSTAR Light Sport Aircraft Document No S2004AMIPUS Date of Issue July 22 2004 or latest 3 FAA H 8083 25 Pilot s Handbook of Aeronautical Knowledge 2003 U S Department of...

Страница 5: ...ment No S2006FTSUS Revision Date of Issue 15 01 2006 Page 5 130 1 3 Recommended Links Visit the Evektor Aerotechnik home page on http www evektor cz to see the latest news from the Sportstar manufactu...

Страница 6: ...Private Pilot certificate and a minimum of a third class medical Single non turbine engine only Fixed or ground adjustable propeller Unpressurized cabin Fixed landing gear Repositionable landing gear...

Страница 7: ...t Control Trike Land Sea and Powered Parachute U S or foreign manufacture of light sport aircraft is authorized Aircraft with a standard airworthiness certificate that meet above specifications may be...

Страница 8: ...ion with side by side seat arrangement and dual controls The airplane is fitted with a tricycle landing gear with the steerable nose wheel The standard power unit consists of four cylinder four stroke...

Страница 9: ...n pertinent to Light Sport Aircraft category may be found on web address http www sportpilot org or other web locations Some of the information available on that address is provided in section 3 2 of...

Страница 10: ...f aircraft safely Sport pilots will be limited to operating aircraft that meet the definition of a light sport aircraft That includes aircraft in the following categories Airplanes single engine only...

Страница 11: ...rate procedure being developed by FAA before being allowed to base his or her medical fitness solely on driver s license requirements 3 2 3 Restrictions on a sport pilot certificate no flights into Cl...

Страница 12: ...EAA www eaa org and its affiliate the National Association of Flight Instructors NAFI www nafinet org stand ready to assist you in this experience Visit the websites to learn more about the opportunit...

Страница 13: ...ing at least 15 hours of flight training from an authorized instructor in a single engine airplane and at least 5 hours of solo flight training in the areas of operation listed in 61 311 i 2 hours of...

Страница 14: ...Day Yes Yes Yes Yes Yes Yes Night No No No Yes No if exercising sport or recreational pilot privileges Yes VFR visibility 3 miles or more Yes Yes Yes Yes Yes Yes VFR visibility less than 3 miles Yes...

Страница 15: ...ining training additional training may be required Class E G airspace Yes Yes Yes Yes Yes Yes 10 000 MSL Yes No No Yes No if exercising sport or recreational pilot privileges Yes otherwise Yes 10 000...

Страница 16: ...s Rating N A N A Yes Yes N A Yes Class B C and D No Yes Yes No Yes if exercising sport or recreational pilot privileges No 87 knots CAS No Yes No No Yes if exercising sport or recreational pilot privi...

Страница 17: ...Certification Privileges for Which Additional Training Is Required Ultralight Pilot Sport Pilot Recreational Pilot Private Pilot CFI Sport Pilot CFI Agricultural non commercial N A No No No N A N A Ch...

Страница 18: ...ness certificate was issued may be used for sport and recreation flight training or rental 2 The Sportstar built from a kit could get an experimental airworthiness certificate and may be used only for...

Страница 19: ...omplete list of limitations 4 2 2 Operating Limitations The aircraft is limited to non aerobatic flight in conditions with no icing Flight is normally according to VFR visual flight rules but IFR inst...

Страница 20: ...with caution VA Maneuvering speed 86 99 Do not make full or abrupt control movement above this speed because under certain conditions the aircraft may be overstressed by full control movement VFE Max...

Страница 21: ...ed up to 50 ft flaps in take off pos 15 55 KIAS 63 mph IAS Best rate of climb speed VY flaps in take off pos 15 55 KIAS 63 mph IAS Best rate of climb speed VY flaps retracted 0 62 KIAS 71 mph IAS Best...

Страница 22: ...ng Prior to his her initial flight in a Sportstar it is essential for the pilot to be familiar with Aircraft Operating Instructions 1 Aircraft Maintenance and Inspection Procedures 2 Manuals supplied...

Страница 23: ...t to be familiar with the aircraft cockpit layout and arrangement and use of controls instruments and equipment Refer to the Aircraft Operating Instructions 1 Aircraft Maintenance and Inspection Proce...

Страница 24: ...rior to entering the cockpit the canopy must be unlocked the key withdrawn and the canopy opened The canopy weight is counterbalanced by two gas struts that reduce the force required The strut force m...

Страница 25: ...t Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 25 130 4 4 2 Entering the Cockpit You may enter the cockpit after unlocking and opening the canopy See the pictures below for r...

Страница 26: ...T T for SPORTSTAR Light Sport Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 26 130 WARNING Exercise caution when the wing is wet or slippery with ice or snow Grasp the back of...

Страница 27: ...2006FTSUS Revision Date of Issue 15 01 2006 Page 27 130 NOTE If the aircraft is equipped with adjustable pedals it is best to make the adjustment before sitting in the seat Adjustment from the sitting...

Страница 28: ...tbelts fastened you should be able to fully deflect the stick in all directions and reach all the necessary controls Small pilots may require cushions to place them closer to controls and tall pilots...

Страница 29: ...F FL LI IG GH HT T T TR RA AI IN NI IN NG G S SU UP PP PL LE EM ME EN NT T for SPORTSTAR Light Sport Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 29 130 Strap in procedure...

Страница 30: ...FL LI IG GH HT T T TR RA AI IN NI IN NG G S SU UP PP PL LE EM ME EN NT T for SPORTSTAR Light Sport Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 30 130 4 4 4 Exiting the Cockp...

Страница 31: ...and the vertical axis see the picture on next page The Sportstar s flight control system consists of primary and secondary control system The primary control system serves to safely control the Sport...

Страница 32: ...SPORTSTAR Light Sport Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 32 130 Primary control surface Airplane movement Axes of rotation Type of stability Aileron Roll Longitudin...

Страница 33: ...ck with a grip that is dependent on the type of trim control that is installed Yaw is controlled by the rudder pedals that are also linked individually to each brake Flight control checks on the groun...

Страница 34: ...evision Date of Issue 15 01 2006 Page 34 130 4 4 5 2 1 Longitudinal Control Elevator Control system Picture Longitudinal control control stick aft airplane climbs Elevator deflection with control stic...

Страница 35: ...15 01 2006 Page 35 130 4 4 5 2 2 Lateral control Aileron Control System Picture Stick deflected left airplane banks and turns left And corresponding up deflection of the left aileron the right one de...

Страница 36: ...Date of Issue 15 01 2006 Page 36 130 4 4 5 2 3 Directional Control Rudder Control System Picture Left rudder pedal deflected forward airplane yaws and banks left And corresponding deflection of rudde...

Страница 37: ...rearward trim the airplane Nose up The trim lever neutral position coincides approximately with the Takeoff position of wing flap control lever i e if you set the flap lever to takeoff position and s...

Страница 38: ...em When installed there is an extension on the control stick with buttons to set trim tab deflection Relative position of the trim tab is indicated to the pilot by a trim position indicator on instrum...

Страница 39: ...handle depressing the button at the end of the handle and then pulling up The maximum speed for any amount of flap extension is 70 kts 81 mph The handle can be set to any of three extension positions...

Страница 40: ...d to the rudder pedals by push pull rods The maximum deflection of the nose wheel is 15 left or right of centre The diameter of turn at full deflection is 15m and with some assistance with brakes it c...

Страница 41: ...Revision Date of Issue 15 01 2006 Page 41 130 4 4 6 Instrument Panel Instruments are normally grouped together as follows Flight instruments left side Electrical switches and circuit breakers lower le...

Страница 42: ...indicates a range of increased caution or time limitation and a white arc on the ASI indicates the normal operating range with flaps extended All analog instruments should be checked prior to flight...

Страница 43: ...open position if the throttle cables fail Therefore as soon as the button is depressed the throttle will tend to increase with only slight pressure When making a coarse throttle movement in this mann...

Страница 44: ...Light Sport Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 44 130 Picture Throttle lever set for idle Picture Throttle lever set for max power Picture Gentle adjustment of eng...

Страница 45: ...clock position if such a type of choke lever is installed When the engine starts allow it to run with full choke for 30 sec to 1 minute and then slowly reverse the procedure and push the handle in ful...

Страница 46: ...ry starts to be charged by the alternator and should go out completely when approximately 13V is reached If the charging indicator light illuminates in flight it may indicate a failure of the alternat...

Страница 47: ...s in OFF position the fuel is closed When the selector is in LEFT position engine is fed from the left tank position for take off and landing When the selector is in RIGHT position the engine is fed f...

Страница 48: ...30 4 4 11 Fuel Tank Drain Valve The fuel drain valve is located at the bottom of the each wing Place the fuel receptacle under the valve and open the drain valve If there is contamination in the fuel...

Страница 49: ...adjustable Adjust pedals before sitting in the seat and ensure both pedals are set to the same position Brakes may be actuated by putting pressure on the top of the individual rudder pedal Brakes are...

Страница 50: ...are connected to the top of rudder pedals It is recommended that you have your heels rested on the cockpit floor and foot placed on pedal in comfortable position i e to not have the foot unnaturally d...

Страница 51: ...he left side of the instrument panel Picture Carburetor heat control knob on the right 4 4 15 Heating If installed the cockpit heat knob is a push pull knob that delivers heat to the cockpit when the...

Страница 52: ...ents operate on battery power Once the engine starts electrical power is supplied to all systems by the alternator and the battery is also recharged If a Hobbs metre is installed it begins to record a...

Страница 53: ...ge 53 130 4 4 19 Switches Electrical services may be switched on or off while airborne With a low battery charge they should be left OFF to leave all available power for the start Gyro type instrument...

Страница 54: ...l on the left side just below labels that identify each one The ACCUM label identifies the master bus If a circuit breaker pops out it may be reset once if it pops again the circuit should be consider...

Страница 55: ...rake is activated by first putting pressure on the brake pedals and then pulling the brake handle up This isolates the system and retains whatever pressure was applied by the pedals WARNING Ensure suf...

Страница 56: ...must ensure that the canopy is securely closed by checking a the guide pins located under the canopy sides fit into the holes in the cockpit sill for big bubble canopy only b the guide brackets at th...

Страница 57: ...eft sockets when the left seat transmit button is pressed and the same for the right seat transmit button If not plugged in correctly the pilot will not be able to transmit using the mic button on his...

Страница 58: ...of the canopy are optional With respect to drawing the most air into the cockpit opening the small flap is more effective than opening the whole window If the whole window is to be opened the small fl...

Страница 59: ...ight Sport Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 59 130 4 4 26 Optional Equipment We highly recommend you to familiarize yourself with information provided in the manu...

Страница 60: ...e of the instrument panel The handle is normally locked on the ground and the red REMOVE BEFORE FLIGHT flag must be removed as part of the pre take off check WARNING Pilots should keep clear of the BR...

Страница 61: ...SPORTSTAR Light Sport Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 61 130 4 5 Pre flight Inspection The pre flight inspection of Sportstar airplane is described in Aircraft O...

Страница 62: ...ply pressure to the toe brakes at least two times after releasing the parking brake There should be equal resistance pressure on both brakes This indicates that there is fluid in both brake lines and...

Страница 63: ...s the idle RPM to approximately 1600 1700 RPM ATTENTION Since the engine has a reduction gear which is equipped with a shock absorber special attention should be paid to the following To prevent impac...

Страница 64: ...efore then the engine must be shut down Failure for the oil pressure to rise means that the engine is not being lubricated and can seize One reason that the oil pressure gauge may not indicate a rise...

Страница 65: ...up test with the aircraft on a rough surface e g small stones or sand The propeller rotation creates a suction below it which can lift contamination into the prop This can cause damage to the blades...

Страница 66: ...rough or loose surface e g such as small stones or sand etc because the suction created under the propeller can lift contamination into the propeller and cause damage In light wind conditions the airp...

Страница 67: ...mmunication with the proper ATC facility and receive clearances When taxiing at an uncontrolled airport then verify the current status of the airport s communication requirements Some uncontrolled air...

Страница 68: ...lease the toe brake pedals 7 Turn the throttle lever to smoothly increase engine power The airplane should slowly start to move The rpm required to make the airplane move forward depends on the condit...

Страница 69: ...ulled back the airplane could slide towards the outside of the turn and the radius of the could unintentionally become larger Also when taxiing against a strong wind with the control stick held back t...

Страница 70: ...s not recommended to taxi into grass that is too high over 2 3 ft 200 mm because of risk of damage to the prop blades Also the surface of the airplane can become contaminated landing gear engine cowli...

Страница 71: ...e and adding power slowly by turning the throttle clockwise Do not brake against power during taxiing Taxiing speed is controlled with power and if braking is required then first reduce the power then...

Страница 72: ...he Main Wheel Brakes The pilot can use the main wheel brakes to reduce the taxiing speed or to turn tighter refer to the recommendations in the previous text To execute a turn of the smallest possible...

Страница 73: ...peller strike Crossing a deeper ditch must be done very slowly and at an angle not exceeding 45 degrees in order to avoid prop damage 4 7 10 Taxiing on Wet Runway When taxiing on a wet runway it is re...

Страница 74: ...the airplane at higher speeds should be controlled by the rudder pedals without using the brakes to avoid the risk of putting the airplane into a skid If such a situation occurs then release the toe b...

Страница 75: ...nated by the aileron system by placing the upwind aileron up Since the Sportstar is a low wing monoplane its wing is not too affected by quartering crosswinds The effect of applying aileron is slight...

Страница 76: ...way The crosswind limit is 10 knots 5 m s which is easy for the average skilled pilot a well trained pilot may safely take off and land at 20 knots 10m s When an unskilled pilot starts under a strong...

Страница 77: ...3 Set the trim lever to be coaxial with the flap lever in neutral position If the electric trim system is installed in your airplane set the trim slightly to the nose heavy position the third diode f...

Страница 78: ...will have enough time to stabilize the rotation of the Gyros If an auxiliary fuel pump is installed then switch it on using a switch on the instrument panel switch off the pump after take off and aft...

Страница 79: ...he neutral position the pilot can correct the left turning tendency by a gradual deflection of the right rudder pedal the required rudder pedal deflection is about 2 inches 50mm 20 Maintain direction...

Страница 80: ...e recommend for you to practice the take off roll and transition to the climb not with full power setting but with power slightly reduced throttle lever set to between up to of its full travel to have...

Страница 81: ...imb at maximum Takeoff power 5800 rpm for 5 minutes When a fixed or ground adjustable prop is installed you will not be able to reach this rpm so you are not limited by that time however observe oil a...

Страница 82: ...execute the shortest possible takeoff then set the wing flaps to the Landing 1 position 30 degrees or Landing 2 50 degrees fully extended The elevator trim lever should be set to a position to be par...

Страница 83: ...tle does not exceed 5500 rpm maximum continuous power In this case you are not limited by the duration of the climb as in the case of an in flight adjustable prop However oil temperature and pressure...

Страница 84: ...the case of a longer climb which has resulted in the engine temperatures being in the yellow arcs it is not recommended to suddenly reduce the engine power to idle and transit to a descent because en...

Страница 85: ...r trim then the trim should be adjusted to stabilize flight 10 of your lookout should be used to pay attention to your flight and engine instruments look at them from time to time Use the elevator tri...

Страница 86: ...lane with in flight variable pitch prop at 3 various altitudes and in each case at 3 various manifold pressures to get data for the Aircraft Operating Instructions However you may find better engine p...

Страница 87: ...rim as necessary 4 11 2 Transition from Level Flight to a Descent Pull the throttle lever to reduce engine power and airspeed and then push the control stick to go into a descent Adjust descent angle...

Страница 88: ...urn of 60 degrees angle of bank So watch the airspeed during turns at high angles of bank The load factor in a turn at a stabilized 60 degree angle of bank reaches 2g and the stall speed in this turn...

Страница 89: ...ver from a steep turn onto the desired heading you should start the recovery earlier than in the case of a shallow turn at a low speed 4 12 2 Climbing Turns It will be necessary to increase the engine...

Страница 90: ...d but a descent at a slightly increased idle When selecting the airspeed to descend at the turbulence should be taken into consideration In smooth air the descent speed can be much faster than in turb...

Страница 91: ...a climb just slightly deflect the left pedal to keep the ball of the turn indicator in the middle This is because a fixed trim tab attached to the rudder which the deflection is set for cruise regime...

Страница 92: ...ightly clockwise and then turn the ignition key fully clockwise and release it The engine should start If you would like the engine to start from the prop rotation then turn the ignition key to the BO...

Страница 93: ...left slip a decreased application of the left stick the airplane will have a tendency to yaw to the right and to keep the direction straight you will be required to decrease the deflection of the rig...

Страница 94: ...is necessary Even a small change of airplane pitch is clearly recognizable against the horizon After you descend to the height of 1 ft 0 5 m above ground turn the throttle lever knob fully anticlockw...

Страница 95: ...ween a downwind landing and a normal landing which is executed up wind is that a larger distance of runway will be required in a downwind landing This should be taken into consideration when planning...

Страница 96: ...uring a crosswind does not differ from a normal approach and should be approximately 59 62 KIAS 110 115km h 68 71 mph Start the roundout at approximately 20 30 ft 7 10 m with the airplane still yawed...

Страница 97: ...in a crosswind does not have a significant effect on the Sportstar low wing monoplane and moreover the airplane has a wide main wheel track However holding the aileron control towards the upwind side...

Страница 98: ...ected towards the downwind side and the control stick deflected towards the upwind side Slightly pull back on the control stick during the landing roll to keep the nose wheel above the ground as long...

Страница 99: ...ommended Hold the airplane in level flight at 1 ft 0 5 m above ground as long as possible until it touches down on the main wheels Then keep in mind that due to increased drag on the main wheels norma...

Страница 100: ...nt Practicing the techniques during rotation to lift the nose wheel and lift off Experiencing the airplane s characteristics after takeoff Pilot technique during the acceleration and during the climb...

Страница 101: ...it pattern If you operate at a non controlled airport then you are not required to ask for clearances it is just a matter of reporting your intentions to the traffic by means of a traffic frequency CO...

Страница 102: ...b performance is very high the rate of climb is above 880 ft min and you would reach the required circuit height very soon the first turn after takeoff is usually done at 300ft 100m and the circuit he...

Страница 103: ...at the position to make the second turn again keep a good lookout for traffic both on the inside and on the outside of the turn to make sure that no other aircraft are arriving Listening to the air tr...

Страница 104: ...hecks completed If you are close enough to the airport to be able to glide back to the runway in case the engine fails then reduce the power to idle after executing the base leg turn If you are too fa...

Страница 105: ...trolling the airplane s attitude against the horizon and the height above ground then looking at the instruments Just only check very quickly to make sure that there is enough airspeed 62 KIAS 115 km...

Страница 106: ...e and its nose wheel touch the ground set the flaps to the takeoff position they were probably in Landing position 1 or 2 set the trim lever to neutral to be parallel with the flap control lever glanc...

Страница 107: ...2 Minimum Safe Speed It may become necessary to fly at the minimum safe speed in order to get to a landing spot with an emergency problem like engine overheat damaged canopy etc Minimum safe speed is...

Страница 108: ...entry Power requirement is quite high with the flap up configuration and with flaps down it is even greater so practice with flap up 4 17 5 Flight in Turbulence Flight in turbulence is a compromise be...

Страница 109: ...55 60 KIAS 100 110 km h 65 70 mph This will allow you to get into the manoeuvre right away rather than wait while you slow down after rolling out of the turn Once you are straight and level set the f...

Страница 110: ...peed build to about 65 KIAS 120 km h 75 mph and then smoothly pull back to level flight If you try to pull too soon and too vigorously you could induce a secondary stall If the wing dropped at the sta...

Страница 111: ...nose up just enough to gradually reduce the speed toward the stall When the nose drops push the stick forward to neutral or slightly forward of neutral The throttle is already at full power and recov...

Страница 112: ...airplane s downward motion Generally speaking the stalls in clean configuration flaps up are more comfortable than stalls with the flaps extended Recovery from that stall can be accomplished by relea...

Страница 113: ...can feel in the stick prior to a stall The airspeed which the airplane should reach for non problematic stall recovery varies around 54 KIAS 100 km h 62 mph During stall recovery once the aircraft re...

Страница 114: ...both the flaps retracted and flaps extended conditions the applicable airspeed limit and positive limit maneuvering load factor may not be exceeded 2 There may be no excessive back pressure during the...

Страница 115: ...s long enough that you can simulate the threshold at about 1 3 of the way from the real threshold If you do this and make a mistake that would make you land short you can always continue to touchdown...

Страница 116: ...e pushed too far forward and airspeed cannot likely be increased because there just isn t enough altitude available It would be more like an initial stick forward followed soon after by aft stick as y...

Страница 117: ...ng the turn because the typical mistake is for the pilot to allow the airspeed to decrease in the turn to the point of stall use a bit too much rudder to increase the turn rate and the aircraft enters...

Страница 118: ...nevertheless failed then do not try to repeat the takeoff Taxi back to hangar to conduct a thorough inspection of fuel system to find the cause of the engine failure impurities or debris in fuel syste...

Страница 119: ...k too much you risk that the airplane will quickly enter into descent You would not have enough time to pull the control stick and roundout and the airplane would hit the ground on the nose wheel at h...

Страница 120: ...ailure both near the ground and at higher altitude The emergency procedures to be used in these cases have been already discussed in the chapter 4 20 2 1 The basic rule is always to immediately push t...

Страница 121: ...oing to do 4 inform circuit traffic that you have an engine failure and what your intentions are 5 when it comes time to lower flap do so in stages Lowering flap all at once could put you into a low s...

Страница 122: ...port You will loose some height by this maneuver and will arrive to the airport from longer distance so would not over fly the airport even when landing downwind After you will push the control stick...

Страница 123: ...tor is LEFT or RIGHT and fuel quantity enough And that Master switch and ignition key in Both position is ON And again if everything this was OK it is not recommended to restart the engine because a f...

Страница 124: ...5 Engine Failure after 4th Turn or During Final If an engine failure occurs at final approach leg when you have already low height above ground then there is always a risk that you will be short not...

Страница 125: ...ick forward to correct the control stick forces The stick should be pushed a bit more than in previous case aborting at final so that the airspeed will not decrease By applying engine power the airpla...

Страница 126: ...Certification 10 3 2 3 Restrictions on a sport pilot certificate 11 3 2 4 New Sport Pilots 12 3 2 5 Airman Certification Operating Privileges and Limitations 14 3 2 6 Airman Certification Privileges...

Страница 127: ...oe brake Pedals 50 4 4 14 Carburetor Heat 51 4 4 15 Heating 51 4 4 16 Defrost 51 4 4 17 Master Switch 52 4 4 18 Ignition Switch 52 4 4 19 Switches 53 4 4 20 Circuit Breakers 54 4 4 21 Parking Brake 55...

Страница 128: ...ight to a Descent 87 4 12 Turns 88 4 12 1 Level Flight Turns 88 4 12 2 Climbing Turns 89 4 12 3 Descent Turns 89 4 13 Descent 90 4 13 1 Straight Descent Flight 90 4 13 2 Power off Descent 91 4 13 3 In...

Страница 129: ...109 4 18 3 Stall Warning 111 4 18 4 Wing Level PowerOn Stalls 111 4 18 5 Turning Flight Stalls 112 4 18 6 PowerOff Turning Flight Stalls 112 4 18 7 PowerOn Turning Flight Stalls 112 4 18 8 Accelerated...

Страница 130: ...FL LI IG GH HT T T TR RA AI IN NI IN NG G S SU UP PP PL LE EM ME EN NT T for SPORTSTAR Light Sport Aircraft Document No S2006FTSUS Revision Date of Issue 15 01 2006 Page 130 130 5 Table of Contents 12...

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