Evektor SportStar MAX Pilot Operating Handbook Download

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PILOT’S OPERATING HANDBOOK

Section 1

General Information

2015-07-20

1-5

Doc. No. POH-20101308

Vertical tail units

Height ................................................................... 1.28 m

VTU area .............................................................. 1.02 sq.m

Rudder area .......................................................... 0,43 sq.m

Landing gear

Wheel track ........................................................... 1.95 m

Wheel base ........................................................... 1.35 m

Main and nose landing gear wheel diameter ........ 380 mm

Summary of Contents for SportStar MAX

Page 1: ...lane board during operation This manual contains information which must be provided to the pilot and also contains supplementary information provided by the airplane manufacturer Evektor Aerotechnik a...

Page 2: ......

Page 3: ...used for airplane operation if it is not keep up to date 0 2 Warnings Cautions Notes WARNING MEANS THAT NON OBSERVATIONS OF THE CORRESPONDING PROCEDURE LEADS TO AN IMMEADIATE OR IMPORTENT DEGRADATION...

Page 4: ...3 Log of Revisions All revisions or supplements to this Manual except actual weighing data are issued in form of revisions which will have new or changed pages as an appendix and the list of which is...

Page 5: ...PILOT S OPERATING HANDBOOK Section 0 Technical Information 2015 07 20 0 3 Doc No POH 20101308 Rev No Affected Pages Description Appr Date Inserted by Date...

Page 6: ...2015 07 20 0 6 2015 07 20 2 12 2015 07 20 0 7 2015 07 20 0 8 2015 07 20 3 3 1 2015 07 20 3 2 2015 07 20 1 1 1 2015 07 20 3 3 2015 07 20 1 2 2015 07 20 3 4 2015 07 20 1 3 2015 07 20 3 5 2015 07 20 1 4...

Page 7: ...2015 07 20 4 8 2015 07 20 5 18 2015 07 20 4 9 2015 07 20 4 10 2015 07 20 4 11 2015 07 20 4 12 2015 07 20 6 6 1 2015 07 20 4 13 2015 07 20 6 2 2015 07 20 4 14 2015 07 20 6 3 2015 07 20 4 15 2015 07 20...

Page 8: ...07 20 8 6 2015 07 20 7 7 2015 07 20 8 7 2015 07 20 7 8 2015 07 20 8 8 2015 07 20 7 9 2015 07 20 8 9 2015 07 20 7 10 2015 07 20 8 10 2015 07 20 7 11 2015 07 20 7 12 2015 07 20 7 13 2015 07 20 7 14 2015...

Page 9: ...PILOT S OPERATING HANDBOOK Section 0 Technical Information 2015 07 20 0 7 Doc No POH 20101308 Section Page Date Section Page Date...

Page 10: ...OOK 0 8 2015 07 20 Doc No POH 20101308 0 5 Table of Contents Section General Information 1 Limitations 2 Emergency Procedures 3 Normal Procedures 4 Performance 5 Weight Balance 6 Airplane System Descr...

Page 11: ...Introduction 1 3 1 2 Certification Basis 1 3 1 3 Airplane Manufacturer 1 3 1 4 Flight Conditions holder for aircraft S N 2010 1308 Individual Design Holder 1 3 1 5 Descriptive Data 1 4 1 5 1 Airplane...

Page 12: ...Section 1 General Information PILOT S OPERATING HANDBOOK 1 2 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 13: ...iliar with all content of this Manual including supplements located in Section 9 1 2 Certification Basis The aircraft described herein complies with the Standard Specification for Design and Performan...

Page 14: ...e Section 7 Airplane System Description 1 5 2 Power Plant The standard power plant consists of ROTAX 912 ULS engine and 2 blade Alisport Irdovario HS propeller For further description see Section 7 Ai...

Page 15: ...n 1 General Information 2015 07 20 1 5 Doc No POH 20101308 Vertical tail units Height 1 28 m VTU area 1 02 sq m Rudder area 0 43 sq m Landing gear Wheel track 1 95 m Wheel base 1 35 m Main and nose la...

Page 16: ...Section 1 General Information PILOT S OPERATING HANDBOOK 1 6 2015 07 20 Doc No POH 20101308 1 5 4 Three View Drawing Figure 1 1...

Page 17: ...ack ATC Air traffic control bar 1 bar 100 kPa C Celsius degree CAS Calibrated airspeed ELT Emergency locator transmitter fpm Foot per minute ft Foot feet 1 ft 0 305 m GEN Generator GPS Global position...

Page 18: ...sq in 1 PSI 6 89 kPa POH Pilot s Operating Handbook RON Research octane number RPM Revolutions per minute RWY Runway sq ft Foot squared sq in Inch squared sq m Meter squared U S gall U S gallons 1 U S...

Page 19: ...er Plant Instrument Marking 2 6 2 6 Miscellaneous Instrument Marking 2 6 2 7 Weight Limits 2 7 2 8 Centre of Gravity 2 7 2 9 Approved Maneuvers 2 7 2 10 Maneuvering Load Factors 2 7 2 11 Flight Crew 2...

Page 20: ...Section 2 Limitations PILOT S OPERATING HANDBOOK 2 2 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 21: ...nd their meaning for operation are stated in the table below Airspeed KIAS km h IAS Meaning VNE Never exceed speed 146 270 Do not exceed this speed in any operation VNO Maximum structural cruising spe...

Page 22: ...ne 39 72 VS0 at maxim weight flaps in landing position 50 White arc 39 70 72 130 Operating range with extended flaps Lower limit VS0 at maximum flaps in landing position 50 Upper limit VFE Green arc 4...

Page 23: ...m 130 C 266 F optimum operation 90 110 C 190 230 F Oil pressure maximum 102 PSI 7 bar for short period admissible at cold start minimum 0 8 bar 12 PSI optimum operation 2 5 bar 29 73 PSI Fuel pressure...

Page 24: ...aution range Upper limit RPM indicator RPM 1400 5500 5500 5800 5800 Oil temperature indicator C 90 110 50 90 110 130 130 Oil pressure indicator bar 0 8 2 5 0 8 2 5 7 7 PSI 12 29 73 12 29 73 102 102 Fu...

Page 25: ...eading edge WARNING DO NOT EXCEED MAXIMUM WEIGHTS AND LIMITATION OF CENTER OF GRAVITY THEIR EXCEEDING LEADS TO AIRPLANE OVERLOADING AND TO DEGRADATION OF FLIGHT CHARACTERISTICS AND DETERIORATION OF MA...

Page 26: ...pproved for VFR daylight flights WARNING NIGHT FLIGHTS ACCORDING TO VFR FLIGHTS ACCORDING TO IFR AND INTENTIONAL FLIGHTS UNDER ICING CONDITIONS ARE PROHIBITED Instruments and equipment for daylight fl...

Page 27: ...through the vents in the wing tips This should be adhered especially when cold fuel from an underground tank is tanked 2 13 2Approved Fuel Grades Automotive gasoline with octane index min RON 95 or a...

Page 28: ...otive gasoline is unavailable Risk of vapor formation if using winter fuel for summer operation 2 14 Oil Limits Performance classification SG or higher according to API Oil volume minimum 2 5 l min ma...

Page 29: ...mpty weight of the airplane with standard equipment The placard with values valid for the actual empty weight of the airplane will be placed in the cockpit MASSE Max Abflugmasse 600 kg Leermasse 348 k...

Page 30: ...nd the baggage compartment NOTE Other placards and labels are shown in Airplane Maintenance Manual for SportStar MAX airplane The following placard is located on the instrument panel The following pla...

Page 31: ...ire in Flight 3 5 3 6 Fire in the Cockpit 3 6 3 7 Emergency descent 3 7 3 8 Gliding Flight 3 7 3 9 Emergency Landing 3 7 3 9 1 Emergency Landing with Non operating Engine 3 7 3 9 2 Precautionary Landi...

Page 32: ...HANDBOOK 3 2 2015 07 20 Doc No POH 20101308 3 14 6 Clogging of Air Inlet to Engine Intake 3 11 3 15 Canopy Opening in Flight 3 12 3 16 Parachute Rescue System Operation 3 13 3 16 1 Using of the rescue...

Page 33: ...55 KIAS 100 km h IAS Emergency landing engine stopped flaps in LANDUNG II position 50 55 KIAS 100 km h IAS 3 3 Engine Failure 3 3 1 Engine Failure at Take off Run 1 Throttle lever GAS idle 2 Brakes as...

Page 34: ...If the engine is shut down the altitude loss during engine starting can reach up to 1000 ft 1 Gliding speed 59 KIAS 110 km h IAS 2 Altitude check 3 Master switch HAUPTSCHALTER ON 4 Unnecessary electr...

Page 35: ...OFF 8 Airplane leave 9 Portable extinguisher if available use 3 5 2 Fire at Take off 1 FUEL selector OFF 2 Throttle lever GAS full 3 Hot air knob HEIZUNG close 4 Cold air knob KALTLUFT close 5 Glidin...

Page 36: ...o complete the flight WARNING NEVER START THE ENGINE AGAIN 8 ATC report if possible 9 Emergency landing carry out according to para 3 9 1 10 Airplane leave 11 Portable extinguisher if available use 3...

Page 37: ...d for example in case of engine failure Wing flaps position Retracted 0 Take off 15 Airspeed 59 KIAS 110 km IAS 55 KIAS 100 km h IAS 3 9 Emergency Landing 3 9 1 Emergency Landing with Non operating En...

Page 38: ...Landing carry out 3 9 3 Landing with Burst Tire CAUTION WHEN LANDING AT HOLDING KEEP THE WHEEL WITH BURST TIRE ABOVE THE GROUND AS LONG AS POSSIBLE BY MEANS OF AILERONS IN CASE OF NOSE WHEEL BY MEANS...

Page 39: ...after rotation stopping set the rudder to neutral position 7 Control stick by gradual pulling recover the diving CAUTION ALTITUDE LOSS PER ONE TURN AND RECOVERING FROM THE SPIN IS 500 UP TO 1000 FT 3...

Page 40: ...ary landing see para 3 9 2 3 14 2Failure of Longitudinal Control 1 Control the airplane in longitudinal direction by means of elevator trim tab and by changing the engine power 2 Land on the nearest s...

Page 41: ...N 32 F 0 C Recommended procedure for engine power regeneration is as follows 1 Carburetor preheat knob VERGASER VORV RM OPEN 2 Throttle lever GAS set idle and cruising power again NOTE Ice coating in...

Page 42: ...ontal tail unit vibrations caused by wake behind opened canopy 2 Pull the throttle lever to reduce airspeed to approximately 65 KIAS 120 km h IAS 3 Pull opened canopy down by holding the canopy frame...

Page 43: ...loos of control of the airplane engine failure over an unlandable area health problems of the pilot prohibiting normal finishing of the flight 3 16 2Rescue System Activation NOTE The activation of the...

Page 44: ...Section 3 Emergency Procedures PILOT S OPERATING HANDBOOK 3 14 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 45: ...and Disassembly 4 3 4 4 Pre flight Check 4 4 4 5 Normal Procedures and Checklist 4 8 4 5 1 Before Engine Starting 4 8 4 5 2 Engine Starting 4 8 4 5 3 Before Taxiing 4 10 4 5 4 Taxiing 4 10 4 5 5 Befo...

Page 46: ...Section 4 Normal Procedures PILOT S OPERATING HANDBOOK 4 2 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 47: ...s 4 2 1 Take off Climbing speed up to 50 ft flaps in START pos 15 57 KIAS 106 km h IAS Best rate of climb speed VY flaps in START pos 15 57 KIAS 106 km h IAS Best rate of climb speed VY flaps retracte...

Page 48: ...ding to the following procedure Figure 4 1 WARNING CHECK BEFORE PRE FLIGHT CHECK THAT IGNITION IS SWITCHED OFF NOTE The word condition used in procedures of pre flight check means visual check of surf...

Page 49: ...condition condition of the stalling speed sensor landing light condition condition of the Pitot tube 3 Left wing tip check surface condition attachment check fuel tank vent cleanness condition and at...

Page 50: ...on and cleanness of air intakes condition of the nose landing gear leg and nose wheel condition of the nose wheel control rods 15 Engine Checks before the first flight of day it is necessary to remove...

Page 51: ...h HAUPTSCHALTER ON Check canopy open close indication light LADENKONTROLE on the instrument panel All switches OFF Instrument equipment check on condition Transport safety lock of the rescue system le...

Page 52: ...heck 10 Master switch HAUPTSCHALTER ON 11 Ignition OFF 12 Canopy close 4 5 2 Engine Starting 1 Fuel gauge indicators check of fuel quantity 2 FUEL selector LEFT Pull the safety button on the fuel sele...

Page 53: ...gine adjust throttle for smooth engine running at about 2500 RPM Check oil pressure Pressure must increase within 10s Increase engine RPM until oil pressure is stabilized over 2 bar 29 PSI 13 Engine p...

Page 54: ...LLER fine low pitch 3 Ignition check carry out see NOTE NOTE Carry out ignition check in the following way Set engine speed to 4000 RPM Switch ignition gradually to L BOTH R position and return to BOT...

Page 55: ...en up the nose landing gear until airplane take off occurs 4 After take off accelerate airplane to 57 KIAS 106 km h IAS 5 Main landing gear wheels brake 6 After reaching 150 ft set flaps to retracted...

Page 56: ...tely switch the tanks during cruise to equally consume fuel from both tanks and minimize airplane tendency to bank with unbalanced tanks Do not fly with the fuel selector set to RIGHT if the left tank...

Page 57: ...E ENGINE UNDERCOOLING AND SUBSEQUENT LOSS OF POWER PERFORM DESCENDING AT INCREASED IDLE AND CHECK OBSERVANCE OF THE ALLOWED VALUES ON ENGINE INSTRUMENTS 4 5 10Before Landing 1 Fuel quantity check CAUT...

Page 58: ...IAS 3 Trim as necessary 4 Carburetor preheat knob VERGASER VORV RM OFF 4 5 11Balked Landing 1 Throttle lever GAS max take off power 2 Flaps START position 15 3 Airspeed 56 KIAS 104 km h IAS 4 Flaps a...

Page 59: ...F 5 Other electrical equipment OFF 6 Ignition OFF 7 Anticollision lights FCL OFF 8 Master switch HAUPTSCHALTER OFF 4 5 15Airplane Parking 1 Ignition check OFF 2 Master switch HAUPTSCHALTER check OFF 3...

Page 60: ...using safety harnesses during long time parking 7 Canopy close lock as necessary NOTE It is recommended to use parking brake for short time parking only between flights during a flight day After endi...

Page 61: ...ibration 5 4 5 2 2 Stall Speed 5 6 5 2 3 Take off Distance 5 7 5 2 4 Landing Distance 5 8 5 2 5 Climb Performance 5 9 5 3 Additional information 5 10 5 3 1 Cruise 5 10 5 3 2 Horizontal Speeds 5 11 5 3...

Page 62: ...Section 5 Performance PILOT S OPERATING HANDBOOK 5 2 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 63: ...provides data for airspeed calibration stall speeds take off performance and additional information provided by the airplane type certificate owner CAUTION THE PERFORMANCE STATED IN THIS SECTION IS V...

Page 64: ...LANDING I 30 LANDING II 50 IAS km h CAS km h CAS km h CAS km h CAS km h VS0 72 80 75 84 83 78 87 87 85 VS1 80 91 89 88 87 83 94 92 91 90 90 99 98 97 96 95 103 102 101 100 100 107 106 105 104 105 111...

Page 65: ...DING II 50 KIAS KCAS KCAS KCAS KCAS VS0 39 43 40 44 41 46 45 42 47 47 46 VS1 43 49 48 48 47 44 50 49 48 48 45 51 50 49 48 50 55 54 53 53 55 59 58 58 57 60 63 62 62 62 65 67 67 66 66 VFE 70 71 71 70 70...

Page 66: ...cted 0 80 91 Take off 15 78 87 Landing 50 72 80 Retracted 0 92 105 Take off 15 90 100 Landing 50 83 92 600 kg Altitude loss 1323 lb KIAS KCAS ft Retracted 0 43 49 Take off 15 42 47 Landing 50 39 43 Re...

Page 67: ...0 630 6000 ft ISA 13 1 290 660 340 710 8000 ft ISA 9 2 330 750 380 800 10000 ft ISA 5 2 370 850 430 910 ISA 20 C Airport altitude H ft Temperature tH C Takeoff Run m Distance over 50 ft obstacle m Tak...

Page 68: ...ISA 13 1 223 496 198 471 8000 ft ISA 9 2 237 528 211 501 10000 ft ISA 5 2 253 562 225 534 ISA 20 C Airport altitude H ft Temperat ure tH C Landing Run m Distance over 50 ft obstacle m Landing Run m Di...

Page 69: ...heating OFF airplane weight 600 kg ambient air temperature ISA SportStar MAX RATE OF CLIMB Rotax 912 ULS Idrovario Alisport prop 0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800 850 90...

Page 70: ...aximum Horizontal Speeds Rotax 912 ULS Idrovario Alisport prop 130 135 140 145 150 155 160 165 170 175 180 185 190 195 200 205 210 3000 3100 3200 3300 3400 3500 3600 3700 3800 3900 4000 4100 4200 4300...

Page 71: ...6 200 TAS km h 170 179 183 190 194 199 202 206 IAS km h 166 175 181 187 192 197 200 204 27 0 inHg CAS km h 164 172 177 183 187 192 195 199 TAS km h 169 177 182 189 193 198 201 205 IAS km h 159 168 173...

Page 72: ...Hg CAS km h 148 154 157 161 164 167 169 170 TAS km h 167 173 177 182 185 188 190 192 IAS km h 137 144 148 153 155 159 161 163 20 0 inHg CAS km h 138 144 147 152 154 157 159 161 TAS km h 156 162 166 17...

Page 73: ...9 Fuel cons l hour 16 4 17 5 18 1 19 0 19 6 Endurance h m 7 10 6 45 6 31 6 13 6 01 Range km h 1240 1210 1190 1160 1140 IAS km h 156 162 166 171 174 CAS km h 155 160 164 168 171 TAS km h 164 170 174 17...

Page 74: ...km h 1420 1360 1310 1240 1200 IAS km h 114 118 121 123 125 CAS km h 118 122 124 126 128 TAS km h 138 142 144 147 149 Fuel cons l hour 10 8 11 7 12 4 13 5 14 1 Endurance h m 10 56 10 03 9 29 8 45 8 20...

Page 75: ...plane weight 600 kg ambient air temperature ISA SportStar MAX BALKED LANDING ROC with the flaps extended to the Takeoff position 0 ft min 100 ft min 200 ft min 300 ft min 400 ft min 500 ft min 600 ft...

Page 76: ...mance and Characteristics Flight performances and characteristics are not considerably affected by rain or insect stuck on the airplane surface 5 3 6 Demonstrated Crosswind Performance Maximum demonst...

Page 77: ...PILOT S OPERATING HANDBOOK Section 5 Performance 2015 07 20 5 17 Doc No POH 20101302 5 3 7 Ceiling Service ceiling 14 700 ft 5 3 8 Noise data Not measured...

Page 78: ...Section 5 Performance PILOT S OPERATING HANDBOOK 5 18 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 79: ...Balance Record 6 4 6 3 Permitted Payload Range 6 5 6 4 Operational Weight and Balance Computation 6 6 6 4 1 Computation Procedure 6 6 6 5 Airplane Loading Schedule Chart 6 7 6 6 Table of Static Momen...

Page 80: ...Section 6 Weight Balance PILOT S OPERATING HANDBOOK 6 2 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 81: ...ane Permitted Payload Range within which the airplane may be safely operated and a method to determine whether the operational weight and CG location will be within the permitted limits range Procedur...

Page 82: ...20101308 6 2 Weight and Balance Record Basic weight of empty airplane Moment kg mm Weight kg Weight change Removed Moment kg mm Arm mm Weight kg Added Moment kg mm Serial No Arm mm Serial No Weight k...

Page 83: ...ayload Range Maximum weight of crew kg Approved Signature Date F U E L L I N G 0 2 25 l 18 kg 0 4 50 l 36 kg 0 6 75 l 54 kg 0 8 100 l 72 kg 1 120 l 86 kg Fuel volume Fuel volume Fuel weight 25 kg 12 k...

Page 84: ...6 or Airplane Loading Graph para 6 7 to read static moments for given weights of crew fuel and baggage 4 Record found moments into the Airplane Loading Schedule Chart para 6 5 5 Determine Take off we...

Page 85: ...hange weight of some of the useful load items crew fuel baggage and perform the computation again WARNING SAFETY OF FLIGHT PERFORMED WITH THE AIRPLANE LOADED OUTSIDE PERMITTED LIMITS OF WEIGHT AND STA...

Page 86: ...6 Table of Static Moments Crew Baggage Weight kg Moment kg m Weight kg Moment kg m 0 0 0 0 50 27 3 5 5 4 60 32 7 10 10 8 70 38 2 15 16 2 80 43 6 20 21 7 90 49 1 25 27 1 100 54 5 110 60 0 120 65 4 130...

Page 87: ...alance 2015 07 20 6 9 Doc No POH 20151308 Fuel Fuel volume l Weight kg Moment kg m 0 0 0 10 7 2 4 9 20 14 4 9 8 30 21 6 14 7 40 28 8 19 6 50 36 0 24 5 60 43 2 29 4 70 50 4 34 3 80 57 6 39 2 90 64 8 44...

Page 88: ...60 70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 230 240 250 260 270 280 290 300 310 320 330 340 0 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 230 24...

Page 89: ...rtStar MAX Airplane SportStar MAX CG Moment Envelope SAMPLE 350 360 370 380 390 400 410 420 430 440 450 460 470 480 490 500 510 520 530 540 550 560 570 580 590 600 610 620 50 60 70 80 90 100 110 120 1...

Page 90: ...eight and CG Envelope SportStar MAX Operational Weight and CG Envelope SAMPLE 350 360 370 380 390 400 410 420 430 440 450 460 470 480 490 500 510 520 530 540 550 560 570 580 590 600 610 620 18 19 20 2...

Page 91: ...re the datum plane If there is no sign indicated then the item lies in an appropriate distance after the datum plane The sign in the column Installed means that the item is physically located on the a...

Page 92: ...97 1 21 18 Turn and bank indc BZW 4B 1 0 46 0 014 19 Engine speed ind D1 211 5021 1 0 20 0 014 20 Oil press indicator D1 211 5055 1 0 14 0 014 21 Oil temperature ind D1 211 5091 1 0 14 0 014 22 CHT in...

Page 93: ...7 3 4 Elevator Trim Tab Control 7 5 7 3 5 Aireron Trim Tab Control 7 5 7 3 6 Wing Flaps Control 7 5 7 4 Controls in the Cockpit and Instrument Panel 7 6 7 5 Inside and Outside Marking and Placards 7...

Page 94: ...Selector 7 13 7 12 3 Fuel Filter 7 13 7 12 4 Indication of Fuel Quantity 7 13 7 12 5 Fuel Tank Draining 7 13 7 13 Electrical System 7 15 7 13 1 Lighting 7 15 7 13 2 Electrical System Scheme 7 15 7 14...

Page 95: ...ember crew is located in the middle part of the fuselage that is accessible after uncovering the single piece organic glass canopy The engine compartment in the front part of the fuselage is separated...

Page 96: ...evator by mechanical system of pull rods and levers 7 3 2 Lateral Control Lateral control is actuated by the control stick From the control stick the movements is transferred through the system of lev...

Page 97: ...Control There is an electric trim tab installed on the left aileron Control switches are located on the control stick trim tabs position indicator is located on the left side of the instrument panel 7...

Page 98: ...gine hours indicator 11 Oil temperature indicator 12 Cylinder head indicator 13 Fuel pressure indicator 14 Oil pressure indicator 15 Fuel quantity indicator left tank 16 Fuel quantity indicator right...

Page 99: ...7 6 1 Landing Gear The airplane is equipped with a sort of fixed nose landing gear Main landing gear legs are produced from composite spring Nose landing gear leg is welded from two pieces the tube a...

Page 100: ...d of safety belts shoulder straps and lock The safety harness is anchored in the fuselage sides behind the seats and on the seat sides 7 8 Baggage Compartment Baggage compartment is positioned behind...

Page 101: ...e power If the lever is fully pulled out then this position corresponds to idle Rapid changes in engine power setting can be made by pressing down the round button on the lever body and by its pulling...

Page 102: ...is 50 150 C Color code is stated in section 2 page 2 6 Oil pressure indicator Oil pressure on the oil input into engine is measured by means of sensor which is located behind the oil filter Working r...

Page 103: ...ipped with oil pump 1 ensuring oil feeding from reservoir 4 located on the fire wall through the oil cooler 5 and the oil cleaner 6 to the lubricated points of engine The pressure sensor 2 is located...

Page 104: ...s are controlled by the ignition switch on the instrument panel Positions of ignition switch OFF engine ignition is off R only ignition circuit B is on L only ignition circuit A is on BOTH both circui...

Page 105: ...pull the safety button on the fuel selector turn the handle to the OFF position and then release safety button Now the handle is blocked in the OFF position Safety button prevents unintentionally swi...

Page 106: ...Section 7 Airplane and System Description PILOT S OPERATING HANDBOOK 7 14 2015 07 20 Doc No POH 20101308 Figure 7 5 Scheme of fuel system...

Page 107: ...ers are listed in the Aircraft Maintenance and Inspection Procedures CAUTION DO NOT USE CIRCUIT BREAKERS FOR NORMAL SWITCHING OFF OF THE SYSTEMS After switching Master switch HAUPTSCHALTER on and by t...

Page 108: ...is led to the airspeed indicator Transparent draining reservoirs are located in the pressure branch of static and total pressure on the left fuselage side by the wing leading edge It is necessary to...

Page 109: ...PILOT S OPERATING HANDBOOK Section 7 Airplane and System Description 2015 07 20 7 17 Doc No POH 20101308 Figure 7 5 Scheme of pitot static system...

Page 110: ...anopy frame Vents are connected to the NACA scoops through tip up canopy frame front flaps Cockpit heating is ensured by hot air from the heat exchanger The heat exchanger is located on the exhaust pi...

Page 111: ...Becker AR 4201 is an efficient transceiver for communication It is equipped with the two line display which is able to indicate active and standby frequencies The control elements of the transceiver...

Page 112: ...equency selector knob inner Switches the indicated frequency in 25 kHz steps or the storage channel by 1 step in each case upwards or downwards without carry over Technical parameters 760 communicatio...

Page 113: ...teps By turning the small knob inner you will change frequency with 25 kHz steps Storage operation Press the STO key The active frequency remains displayed in the top line The preset frequency appears...

Page 114: ...ree channel no frequency stored will be skipped when selected NOTE Further operation modes and detailed description transceiver handling are shown in Operating instructions Becker AR 6201 VHF Transcei...

Page 115: ...ransmitting identification codes Mode A and Mode C In this mode the responder will respond to requests for transmitting identification code and will transmit data on pressure flight altitude Code Sett...

Page 116: ...hen required by ATC controller VFR Button By pressing VFR button the preset code for VFR operation is set on the responder no code preset by instrument producer By second pressing within 3 sec from th...

Page 117: ...ode Mode switch ISO The pilot is isolated from the intercom and is connected only to the airplane VHF transceiver ALL Mode Mode switch ALL Pilot and other crew member can hear the airplane VHF transce...

Page 118: ...ersatile color aviation automotive and marine navigator perfect for air land or water This portable navigator features a 256 color TFT screen that is easy to read in bright sun a nuilt in base map Jep...

Page 119: ...rn off the unit press and hols the POWER key again Using the GPSMAP 496 See Owners s Manual of the GPSMAP 496 P N 190 00722 00 Rev C or later valid version 7 17 Parachute Rescue System Parachute emerg...

Page 120: ...Section 7 Airplane and System Description PILOT S OPERATING HANDBOOK 7 28 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 121: ...oring 8 5 8 4 4 Airplane Jacking 8 5 8 4 5 Leveling 8 6 8 4 6 Road Transport 8 6 8 5 Airplane Servicing 8 7 8 5 1 Airplane Fuelling 8 7 8 5 1 1 Approved Fuel Grades 8 7 8 5 1 2 Fuelling Procedure 8 7...

Page 122: ...Section 8 Airplane Handling Servic and Maintenance PILOT S OPERATING HANDBOOK 8 2 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 123: ...ory although they do not come into effect before Airworthiness Directive is issued by aviation authority of user s country All correspondence with the airplane manufacturer distributor or service cent...

Page 124: ...is possible to move the airplane on a short distance by holding the fuselage end in the position before the fin eventually by holding the root part of wings The hand towing bar can be used for airpla...

Page 125: ...with fixing eyes on the lower side of wings Procedure 1 Check of fuel selector off position of all switches ignition and master switch 2 Lock manual control e g by using safety belts 3 Release parking...

Page 126: ...skid and by pushing from below and then the lower part of fuselage can be supported by the rest located in the area of the skid Wings van is jacked by pushing on the wing from below in the area of the...

Page 127: ...PERSON ALLOWED IN THE COCKPIT DURING FUELING 1 Connect the airplane to ground 2 Open fuel tank cap 3 Fill airplane with necessary amount of fuel 4 After fuelling wipe the remaining fuel out of the fu...

Page 128: ...l quantity in the oil tank NOTE Before the check oil quantity turn the propeller by hand ignition must be switched OFF in the sense of engine rotation so that oil can fill in the engine space or opera...

Page 129: ...approx 25 mm in the reservoir 3 Step repeatedly on the pedal during refilling 4 Bleed the system after refilling 5 Install the upper engine cowling 8 6 Cleaning and Care Always use appropriate cleani...

Page 130: ...Section 8 Airplane Handling Servic and Maintenance PILOT S OPERATING HANDBOOK 8 10 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 131: ...ILOT S OPERATING HANDBOOK Section 9 Supplements 2015 07 20 9 1 Doc No POH 20101308 TABLE OF CONTENTS 9 Supplements 9 1 Introduction 9 3 9 2 List of Inserted Supplements 9 3 9 3 Supplement Inserted 9 4...

Page 132: ...Section 9 Supplements PILOT S OPERATING HANDBOOK 9 2 2015 07 20 Doc No POH 20101308 Intentionally Left Blank...

Page 133: ...ction This section contains the appropriate supplements necessary to safely and efficiently operate the airplane when equipped with various optional systems and equipment not provided with the standar...

Page 134: ...Section 9 Supplements PILOT S OPERATING HANDBOOK 9 4 2015 07 20 Doc No POH 20101308 9 3 Supplement Inserted...

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