Pipistrel 890 AT 912 LSA Скачать руководство пользователя

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ALPHA Trainer

www.pipistrel-aircraft.com

REV. 0

POH-162-00-40-050

Powerplant, fuel, oil

Engine manufacturer: ROTAX

Engine type: Rotax 912 (80 HP)

The engine

TEMPERATURE °C / ROTAX ENGINE

912 80 HP

Maximum coolant temp. (CT)

120

Maximum exhaust gas temperature (EGT)

880

Oil temperature (OIL TEMP); minimum, normal, highest

50; 90-110; 140

RPM, PRESSURE

912 80 HP

Oil pressure (OIL PRESS); lowest, highest bar (psi)

0.8; 2.0-5.0; 7.0

Maximum continuous speed (RPM)

5500

Take-off speed; maximum allowable 5 min (RPM)

5800

Magneto check at (RPM)

4000

Maximum single magneto drop (RPM)

< 300

Fuel and oil

ROTAX ENGINE

912 80 HP

Recommended fuel **

minimum 90 RON

grade,

up to 10% alcohol

content permitted,

0% is preferable*

Also approved fuels **

leaded

or AVGAS

100 LL

Recommended oil **

SAE 10 W-40

AeroShell Oil Sport

Plus 4

Oil system capacity typical

3.5 L (check dipstick)

* Engine life is reduced. If using this type of fuel is unavoidable, changing the engine oil

every 50 flight hours is crucial. Please consult the manufacturer on which type of oil to use.

** See latest edition of Rotax Service Instruction SI-912-016R10 Selection of suitable operating

fluids for Rotax Engine.

IMPORTANT!

Four-stroke engines should only be powered by unleaded fuel, for lead sedimentation inside the en-

gine shortens its life. Provided you are unable to use unleaded fuel, make sure engine oil and the oil

filter are replaced every 50 flight hours.

WARNING!

Use of fuels with alcohol content exceeding 10% is not perm

itted. See Rotax

specification - please refer to SI-912-016 “Selection of suitable operating fluids“ latest issue.

NOTE

Please refer to the applicable Rotax operator’s manual for additional engine operating limi-

rations.

1-4

General

Содержание 890 AT 912 LSA

Страница 1: ...Training Supplement REVISION B00 24th October 2019 This publication includes the material required to be supplied to the pilot by ASTM F2245 F2279 F2295 Aircraft Registration Number Aircraft Serial N...

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Страница 3: ...val ues derived from flight tests conducted by Pipistrel under the supervision of the Slovenian CAA and under carefully documented conditions Figures may vary based on numerous factors surface condi t...

Страница 4: ...pages display the same page number the page with the latest revision shall be used in the POH The revision number on the log of effective pages shall also coincide with the revision number of the page...

Страница 5: ...trel LSA s r l Revision 4 Specification changes 13th August 2013 Several Coates Pipistrel LSA s r l Revision 5 Reordering of chapters to comply with ASTM F2746 12 31st January 2014 ALL Coates Pipistre...

Страница 6: ...Rev number Cover 4 7 0 i 1 4 8 0 i 2 0 4 9 0 i 3 0 4 10 0 i 4 0 5 1 0 i 5 0 5 2 0 i 6 0 5 3 0 i 7 5 4 0 0 1 0 5 5 0 0 2 5 6 0 1 1 0 5 7 0 1 2 0 5 8 1 3 0 6 1 0 1 4 0 6 2 0 1 5 0 6 3 0 1 6 0 6 4 0 2 1...

Страница 7: ...is sold globally in more than 40 countries Many countries have their own individual requirements for information required to be shown in an aircraft manual This manual is the only official manual for...

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Страница 9: ...aft com REV 0 POH 162 00 40 050 Table of contents 1 General 2 Operating limitations 3 Emergency procedures 4 Normal procedures 5 Performance 6 Weight and balance 7 Aircraft systems 8 Handling and serv...

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Страница 11: ...www pipistrel aircraft com REV 0 POH 162 00 40 050 Introduction 1 2 Technical brief 1 2 3 view drawing 1 3 Powerplant fuel oil 1 4 Weights 1 6 Center of gravity range 1 6 G load factors 1 6 1 General...

Страница 12: ...60 mm General Introduction This manual contains all information needed for appropriate and safe use of ALPHA Trainer IT IS MANDATORY TO CAREFULLY STUDY THIS MANUAL BEFORE USING THE AIRCRAFT Pipistrel...

Страница 13: ...ALPHA Trainer www pipistrel aircraft com REV 0 POH 162 00 40 050 3 view drawing General 1 3...

Страница 14: ...SAE 10 W 40 AeroShell Oil Sport Plus 4 Oil system capacity typical 3 5 L check dipstick Engine life is reduced If using this type of fuel is unavoidable changing the engine oil every 50 flight hours i...

Страница 15: ...at the vent tube remains unobstructed from contamination Propeller ALPHA Trainer Propeller Rotax 912 80 HP Pipistrel FP02 80 diameter 1660 mm Engine instrument markings Instrument Red line minimum Gre...

Страница 16: ...espected WARNING MTOM must be kept at or below 1212 lbs 550 kg Exceeding baggage weight or c g limits can shift aircraft s balance to the point when the flight becomes uncontrollable More information...

Страница 17: ...2 1 Introduction 2 2 Airspeed limitations 2 2 Powerplant limitations 2 3 Weights 2 4 Center of gravity range 2 4 G Load factors 2 5 Serviceceiling crosswind 2 5 Maneuver limits 2 5 Kinds of operation...

Страница 18: ...30 Full Flap Operating Range Lower limit is the maximum weight VS0 in landing configuration Upper limit is maxi mum speed permissible with flaps extended Green band 43 108 83 201 Normal Operating Rang...

Страница 19: ...RPM 300 Fuel and oil ROTAX ENGINE 912 UL2 80 HP Recommended fuel minimum 90 RON grade up to 10 alcohol content permitted 0 is preferable Also approved fuels leaded or AVGAS 100LL Recommended oil SAE...

Страница 20: ...cockpit crew weight 121 lbs 55 kg Baggage aft of the cabin 22 lbs 10 kg Always verify baggage allowance with a center of gravity calculation WARNING only when baggage net or solid baggage compartment...

Страница 21: ...s are permitted in this airplane The following non aerobatic maneuvers are permitted as defined Power on and off stalls not below 1500 feet 450 meters above ground level Power on and off lazy eights n...

Страница 22: ...V Main battery functional alternator functional safety belts 2x fuel shut off valve functional electric fuel pump functional Minimum equipment list IFR VMC The minimum equipment list for IFR VMC is id...

Страница 23: ...verify that the vent tube remains unobstructed from contamination Other restrictions Due to flight safety reasons it is forbidden to fly in heavy rainfall fly during thunderstorm activity fly in a bl...

Страница 24: ...system This aircraft is equipped with a rocket powered ballistic rescue system HUTE T WARNING ROCKET FOR PARACHUTE DEPLOYMENT INSIDE Next to fuel drain outlet 3 5 l OIL Refer to ROTAX manual 50 ANTIFR...

Страница 25: ...lbs min 121 lbs 55 lbs EAW MTOW kg 550 kg min 55 kg 25 15 0 37 60 kts 40 70 kts 43 135 kts Respect limits from POH 1111090_ALPHA_TRAINER_LSA CAUTION ENGAGE FUEL PUMP FOR STARTUP TAKEOFF AND LANDING V...

Страница 26: ...ow each door to depict door handle operation Next to wheel brake pull 2x Next to choke and throttle levers FUEL L R MIC OPEN CLOSED OPEN CLOSED L R HEADSET CAUTION ENGAGE FUEL PUMP FOR STARTUP TAKEOFF...

Страница 27: ...aft com REV 0 POH 162 00 40 050 Next to activation handle cockpit Placards Ballistic Parachute Rescue System Next to rocket exhaust bottom of fuselage Next to each door top aft corner 2x 2 11 Limitati...

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Страница 29: ...ecovery 3 2 Spin recovery 3 2 Engine failure 3 3 Emergency landing Outlanding 3 3 Engine fire 3 3 Smoke in cockpit 3 4 Carburetor icing 3 4 Electrical system failure 3 4 Flutter 3 5 Exceeding VNE 3 5...

Страница 30: ...lown into a spin and even so only at aft center of gravity positions However once spinning intentionally or unintentionally react as follows 1 Set throttle to idle lever in full back position 2 Push s...

Страница 31: ...f unsuccessful begin with the emergency landing outlanding procedure immediately Emergency landing Outlanding 1 Shut off fuel valve 2 Fuel pump switch OFF if applicable see chapter 7 3 Magneto L R OFF...

Страница 32: ...the 12 V socket is OFF as well 2 Disconnect the battery from the circuit pull battery disconnection ring on the instrument panel s switch column 3 Land as soon as possible In case you have trouble bre...

Страница 33: ...forced to land in a body of water use the same emergency procedure as above for the Emergency landing Landing out case In addition make sure to open both doors fully before hitting the water as well...

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Страница 35: ...ALPHA Trainer www pipistrel aircraft com REV 0 POH 162 00 40 050 Daily inspection 4 2 Pre flight inspection 4 2 Normal procedures and recommended speeds 4 5 4 Normal procedures Normal procedures 4 1...

Страница 36: ...mage MUST be repaired prior to engine start up Disobeying these instructions may result in serious additional damage to the plane and crew including injury and loss of life Schematic of pre flight ins...

Страница 37: ...towards the ground to verify proper nose wheel suspension operation Then lift the nose wheel off the ground and check for nose leg strut free play Bolts fastened Tire no cracks adequate pressure Wheel...

Страница 38: ...continued Surface condition pristine no cracks impact spots or bumps no paint separations Horizontal tail surfaces Surface condition pristine no cracks impact spots or bumps no paint and or edge separ...

Страница 39: ...To enter the cabin first lift the door all the way to the bottom wing surface The silver knob will grab and secure the door in position Sit on the cabin s edge and grab it to support your body Drag yo...

Страница 40: ...at 2500 RPM up to the point working temperature of oil is reached Warming up the engine you should 1 Point aircraft s nose into the wind 2 Verify the engine temperature ranges within operational limi...

Страница 41: ...nt for information about testing and use of airbrakes optional CAUTION Should the engine start to overheat because of long taxi and holding shut down the engine and wait for the engine temperatures dr...

Страница 42: ...climb out CAUTION Reduce power and lower nose to increase speed in order to cool the engine down if necessary Should you be climbing for a cross country flight consider climbing at 100 kts 185 km h a...

Страница 43: ...ime operations NOTE See SPOH 161 00 41 050 Electric airbrakes POH supplement for information about use of airbrakes optional CAUTION Crosswind landings require higher final approach speeds to ensure a...

Страница 44: ...ection of movement Balked landing Add full power establish Vy retract flaps as required WARNING If the aircraft is equipped with airbrakes optional ensure they are closed in event of go around maneuve...

Страница 45: ...0 POH 162 00 40 050 Introduction 5 2 Airspeed indicator calibration 5 2 Stall speeds 5 2 Take off performance 5 3 Climb performance 5 5 Cruise 5 5 Descent 5 6 Landing performance 5 6 Crosswind takeoff...

Страница 46: ...atures of 45 C 113 F This is not to be regarded as the limit temperature however temperatures higher than the mentioned may have an adverse effect on engine cooling and overall performance Airspeed in...

Страница 47: ...provides data about the effect of elevation on takeoff runway length Elevation ft m 0 1650 500 3280 1000 4920 1500 Atmosph pressure inHg 29 92 28 17 26 52 24 95 Atmosph pressure hPa 1013 954 898 845 O...

Страница 48: ...stances will be approximately 120 130 feet 36 40 meters longer then ones published in the manual WARNING Tailwind affects takeoff and landing performance by more than twice as much as headwind does Th...

Страница 49: ...00 ft 1020 fpm 5 1 m s NOTE Climb rate is measured at max continuous power 5500 RPM of the engine with the flaps retracted at Vy and MTOM Climb performance may vary depending on temperature altitude h...

Страница 50: ...speed 64 kts 118 km h Best lift over drag ratio flaps 0 15 1 CAUTION If the engine fails especially in climb the aircraft always loses some 100 feet 30 meters of altitude before reaching best glide s...

Страница 51: ...rel aircraft com REV 0 POH 162 00 40 050 Crosswind takeoffs landings The maximum allowed crosswind speed on takeoff and landing is 18 kts The runway length required increases by 10 for every 5 kts of...

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Страница 53: ...iner www pipistrel aircraft com REV 0 POH 162 00 40 050 Weight and balance Introduction 6 2 Weighing procedure 6 2 Equipment list 6 3 Determination of CG 6 3 Sample CG calculation 6 4 6 Weight and bal...

Страница 54: ...aft parts and appliances are installed and in position Remove all other objects e g tools rugs tie downs and other items Empty fuel tanks except for the unusable fuel inflate tires to recommended oper...

Страница 55: ...iance must be registered in the upper table Also new total weight and lever arm of CG values must be entered and position of CG re determined Furthermore the moment must be recalculated This is rather...

Страница 56: ...down values of G1 sum of scale readings at main wheels and G2 scale reading at tail front wheel Then calculate the position of c g in millimeters mm from the datum wing s leading edge at wing root Us...

Страница 57: ...e aircraft with 10 kgs 22 lbs of baggage You can recalcu late the formulas using the weights and c g of your empty aircraft and the planned amount of bag gage aft of the cabin for your flight CAUTION...

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Страница 59: ...ypical instrument panel 7 4 Undercarriage 7 6 Seats and safety harnesses 7 6 Pitot static system 7 6 Propeller 7 6 Powerplant 7 7 Fuel system 7 8 Electrical system 7 9 Engine cooling system 7 10 Engin...

Страница 60: ...nd also in flight to suit your size and needs The fuel tank is located in the fuselage with the fuel shut off valve located in the cockpit The gascolator is located beneath the lower engine cover Refu...

Страница 61: ...NGINE COVERS FRONT WHEEL PEDALS LEFT WHEEL LANDING GEAR RUDDER CABLES ELEVATOR CONTROL TUBE LEFT WING LEFT FLAPERON RUDDER ELEVATOR STICK RIGHT FLAPERON RIGHT WHEEL Aircraft systems 7 3 INSTRUMENT PAN...

Страница 62: ...ndbrake lever choke lever flap lever trim lever door handles battery disconnection lever ring and emergency parachute release handle Typical Instrument panel RIGHT SEAT FLAP LEVER LEFT SEAT RIGHT PEDA...

Страница 63: ...ockpit electrical system panel switch panel incorporates a separate master switch avionics switch and engine starter push button separate magneto control There are fuses located in the il luminated re...

Страница 64: ...andbrake lever firmly hold it engage and use the lock latch to activate parking brake function To release simply release the lock latch and push handbrake lever to full forward position Seats and safe...

Страница 65: ...g parts oilcooled own radiator and pump Lubrication centrally oiled own oil pump and radiator Reduction gearbox integrated Reduction ratio 1 2 27 El generator output power 250 W at 5800 RPM Starter el...

Страница 66: ...ual fuel consumption flow and fuel quantity remaining are calculations based on en gine rpm and manifold pressure These settings are to be used as a guide only and are NOT to be relied upon for the sa...

Страница 67: ...cket and the Pitot heat are connected to the avionics bus via push pull circuit breakers For loads which are engaged and disengaged more often fused rocker switches are used Electrical fuel pump 12 V...

Страница 68: ...The overflow tank fluid level must always be inside the designated limits The engine does not feature a cooling fan therefore cooling is entirely dependent on moving air cur rents and airspeed CAUTION...

Страница 69: ...hin limits at all times CAUTION Oil temperature pressure and quality is strictly defined and must not under any circumstances vary from its safe values Schematic of engine lubrication system Wheel bra...

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Страница 71: ...0 POH 162 00 40 050 Special inspections 8 2 Draining and refueling 8 2 Connecting auxiliary power supplies 8 3 Tie down 8 4 Storage 8 4 Cleaning 8 4 Keeping your aircraft in perfect shape 8 5 8 Handli...

Страница 72: ...witch is set to OFF Draining the fuel system The gascolator is located beneath the bottom engine cover on the left hand side of the fuselage To drain the fuel system open the drain valve on the gascol...

Страница 73: ...relay mounted top right of the aircraft s battery on the firewall This relay has 3 nipples the positive wire must be connected to the upper left nipple the only one to which 2 cables are connected to...

Страница 74: ...scue system is installed in your aircraft so make sure the activation handle safety pin is inserted every time you leave the aircraft Also disconnect the battery from the circuit to prevent battery se...

Страница 75: ...wel chamois artificial leather skin To save time soak all the leading edges of the airframe fist Make sure to wipe ALL of the aircraft s surface until it is com pletely dry at the end Clean the propel...

Страница 76: ...ine polishing requires more skills and has its own particularities therefore it is recommended to leave it to a professional Cleaning the Lexan transparent surfaces It is most important to use really...

Страница 77: ...ALPHA Trainer www pipistrel aircraft com REV 0 POH 162 00 40 050 Parachute rescue system use handling and servicing 9 2 Training supplement 9 4 Conversion tables 9 8 9 Appendix Appendix 9 1...

Страница 78: ...ty pin should be inserted when the aircraft is parked or stored in a hangar to prevent accidental deployment However the instant pilot boards the air craft safety pin MUST be removed Use of parachute...

Страница 79: ...assist you After the parachute rescue system has been used or if you suspect any possible damage to the sys tem do not hesitate and immediately contact the manufacturer Handling and servicing Prior to...

Страница 80: ...up to 10 km s 5 kts while holding the stick back fully to ease the pressure of the nose wheel During taxiing monitor engine temperatures Due to low airflow around the radiators the CHT and Oil tempera...

Страница 81: ...urns Above 85 kts 160 km h the rudder becomes almost insignificant in comparison to aileron deflections when it comes to making a turn Cruising fast it is important to fly coordinated ball in the midd...

Страница 82: ...be a constant 55 kts 100 km h throughout the final with the descent path constant as well At a height of 10 meters 25 feet start a gentle flare and approach the aircraft must touch down with the main...

Страница 83: ...st cannot be damaged due to side forces on cross wind landings Landing in strong turbulence and or gusty winds First of all airspeed must be increased for half of the value of wind gusts e g if the wi...

Страница 84: ...0295 in Hg 1 in Hg 33 898 hPa 1 kg 2 2046 lb 1 lb 0 4536 kg min 1 kg min 2 2046 lb min 1 lb min 0 4536 kg min 1 l 0 2641 US gal 1 US gal 3 7864 l min 1 l 1 057 US quart 1 US quart 0 9461 l 1 l min 0 2...

Страница 85: ...ALPHA Trainer www pipistrel aircraft com REV 0 POH 162 00 40 050 Operators Manual for the Instrument panel 10 2 Checklist 10 8 Warranty statement 10 10 10 Supplements Supplements 10 1...

Страница 86: ...ALPHA Trainer www pipistrel aircraft com REV 0 POH 162 00 40 050 Pipistrel ALPHA Trainer Instrument Panel Operators Manual Supplements 10 2...

Страница 87: ...nts 10 3 1 Variometer 2 Air Speed Indicator ASI 3 HORIS 4 Garmin AERA GPS 5 Altimeter 6 Engine Data display 7 Airbrakes control switch optional 8 RPM indicator 9 COM Radio 10 Slip indicator 11 Transpo...

Страница 88: ...sensors and an LCD display Majority of sensors are built into its compact hous ing static pressure dynamic pressure 3 axis ac celerometer 3 axis angular rate and GPS receiver Only GPS antenna and OAT...

Страница 89: ...arly marked with a red line 3 Altimeter The Altimeter is a 80 mm 3 1 8 unit which shows aircraft altitude based on QNH The Altimeter consists of familiar mechani cal double needle The large OLED digit...

Страница 90: ...Oil temperature Water Temperature Manifold pressure CT EGT Fuel Pressure Instant fuel flow Fuel remaining Battery voltage Outside air temperature The Engine Data instrument displays the following read...

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Страница 92: ...rm up at 2000 RPM for 2 mins then 2500 RPM Magneto RPM drop VERIFIED MAX 300 RPM Engine Propeller check CHECK parameters NAV AC lights ON as required NAV COM GPS XPDR SET Before takeoff Fuel valve CHE...

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Страница 94: ...ALPHA Trainer www pipistrel aircraft com REV 0 POH 162 00 40 050 Warranty statement voids For applicable warranty terms and conditions please refer to www pipistrel aircraft com 10 10...

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Страница 96: ...pipistrel si www pipistrel aircraft com Pipistrel Italia Via Fratelli Rusjan 26 34070 Savogna d Isonzo GO Italia EU t 39 3703207623 info pipistrel si www pipistrel aircraft com Pipistrel Vertical Sol...

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