Pelegrin Tarragon Скачать руководство пользователя страница 65 | Manualshive

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Pilots Operating Handbook

65/76

YL-MFG

Revision 7, Issue 1

4/6/2016

7.19 Battery

The battery is a Super B SB12V5200P-BC lightweight lithium ion starter battery based on
lithium iron phosphate technology (LiFePO4). This lithium ion technology used in Super B
batteries is the safest lithium ion technology available today.

Technical data

Nominal Voltage

13,2

End of Charge Voltage

15,2

End of Discharge Voltage

8,0

Charge Current (A)

20,0

Discharge Current (A)

160,0

Discharge Pulse Current (A)(10 seconds)

240,0

Discharge Pulse Current (A)(1 second)

300,0

Discharge Performance at 20

0

C (rated capacity)(Ah)

4,6

Discharge Performance at -20

0

C (capacity)(Ah)

4,1

Operating Temperature Range

-30

0

C to +40

0

C

Storage Temperature Range

-50

0

C to +60

0

C

Height (mm)

84,5

Width (mm)

114,5

Thickness (mm)

62,5

Weight (g)

850,0

NOTE

: Charging the battery should be done with a special charger for lithium batteries. It is

recommended to use a charger that will test and condition the battery as well, like the
Optimate Lithium Charger (picture of charging connector in paragraph 7.21).

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Содержание Tarragon

Страница 1: ...MFG Revision 7 Issue 1 6 Apr 16 Pilot s Operating Handbook and Flight Manual YL MFG Pelegrin LIMITED LIABILITY COMPANY Identification No 50103508691 VAT No LV50103508691 Rigas gatve 8 Adazi Adazi regi...

Страница 2: ...1 2015 3 0 28 05 2015 2 1 5 23 11 2015 2 3 4 22 10 2015 4 5 5 23 11 2015 3 1 2 1 10 2015 2 8 3 10 10 2015 9 14 0 28 05 2015 4 1 4 4 22 10 2015 5 6 6 26 01 2016 7 9 3 10 10 2015 5 1 2 1 10 2015 2 3 6 2...

Страница 3: ...F GRAVITY RANGE 12 2 6 APPROVED MANEUVERS 12 2 7 SPECIFIC OPERATION LIMITS 12 2 8 FUEL 133 2 9 ENGINE 13 2 10 ENGINE AND INSTRUMENT MARKINGS 15 2 11 ENGINE OIL 15 2 12 COOLANT 15 2 13 FLAP LIMITATIONS...

Страница 4: ...0 5 2 TAKEOFF DISTANCE M 40 5 3 TAKEOFF SPEED 40 5 4 ENGINE PERFORMANCE AT STANDARD TEMPERATURES AND PRESSURES 41 5 5 LANDING DISTANCE M 41 5 6 MAXIMUM CLIMB AND GLIDE 41 5 7 ACTUAL TESTED FLIGHT PERF...

Страница 5: ...E INSTRUMENTS 59 7 14 ENGINE LUBRICATION SYSTEM 59 7 15 IGNITION SYSTEM 60 7 16 COOLING SYSTEM 61 7 17 FUEL SYSTEM 62 7 17 1 FUEL INDICATION 63 7 17 2 FUEL VENTING 63 7 17 3 FUEL DRAIN VALVES 63 7 17...

Страница 6: ...CHARTS 73 LENGTH CONVERSIONS 73 DISTANCE CONVERSIONS 74 TEMPERATURE CONVERSIONS 75 PRESSURE CONVERSIONS 75 FUEL VOLUME TO WEIGHT CONVERSIONS 76 LIST OF MANUALS 76 www tarragonaircraft com The airplan...

Страница 7: ...can result in damage to equipment if not carefully followed NOTE An operating procedure technique etc considered essential to emphasize 1 2 Basic Description The Tarragon is an all carbon composite t...

Страница 8: ...ne it is a horizontally opposed 4 cylinder engine with pushrod actuated OHV 2 valves per cylinder injector fed 2 magnetos for ignition liquid cooled heads ram air cooled cylinders reduction gear and o...

Страница 9: ...Pilots Operating Handbook 9 76 YL MFG Revision 7 Issue 1 4 6 2016 1 4 3 View and Dimensions mm...

Страница 10: ...this speed in any operation VS0 Stall speed landing configuration 46 85 Stall speed flaps full VS Stall speed clean 54 100 Stall speed flap up VFE Maximum extended flap speed Flaps 10 Flaps 20 Flaps f...

Страница 11: ...er limit is maximum weight VS at most forward C G with flaps retracted Upper limit is maximum structural cruising speed Yellow Band 124 200 Operations must be conducted with caution and only in smooth...

Страница 12: ...ry speed IAS Chandelles 119 Kts 220 km h Lazy Eights 119 Kts 220 km h Steep Turns 119 Kts 220 km h Stalls Except Whip Stalls Slow Deceleration Power On Stalls Slow Deceleration limit pitch to 30 nose...

Страница 13: ...7Ti ULM engine It is fuel injected for utmost safety and low fuel consumption and turbo normalized which assures constant maximum power of 100KW from sea level to the service ceiling of 15 000 feet Th...

Страница 14: ...2016 Operation outside temperature range 25 C 50 C CAUTION Engine operation with indicated oil pressure below the green band ranges while in cruise or climb configuration is considered abnormal Refer...

Страница 15: ...all the requirements These oils are normally not mineral oils but semi or full synthetic oils Use of multi grade oils is recommended Multi viscosity grade oils are less sensitive to temperature varia...

Страница 16: ...rocedures associated with optional or supplemental equipment are found in Section 9 Supplements 3 2 Airspeeds for Emergency Procedures IAS Procedure Kts km h Engine failure after take off 62 115 Desig...

Страница 17: ...ver necessary to wait for the standstill of the propeller OIL PRESSURE INDICATOR IN RED BAND RANGE RED DIGITS IN EIS 1 OIL C CHECK IF OIL C ABOVE GREEN BAND RANGE OR OIL C RISING engine failure immine...

Страница 18: ...ssured that the landing gear will not withstand the landing roll the BRS should be activated See section 7 12 DITCHING 1 Radio TRANSMIT MAYDAY on 121 5 MHz give location intentions and SQUAWK 7700 2 H...

Страница 19: ...TE BRS activation over water LDG Gear UP as it may prevent the airplane from capsizing CAUTION BRS needs at least 250FT 80M of height to properly inflate the parachute BRS activation at lower heights...

Страница 20: ...OFF If fire has not been extinguished 7 MASTER Switch ON 8 Rapid Descent EXECUTE Perform sideslip to rapidly lose altitude and shorten exposure time 9 AVN MASTER Switch ON 10 Radio ALERT ATC or TRANSM...

Страница 21: ...itch and bank b Reference GS ground speed in conjunction with GPS derived wind information to determine an approximate airspeed c Navigate using Heading Strip Lateral Deviation and GPS moving map NOTE...

Страница 22: ...PARTIALLY OPENED UNLOCKED MAIN or NOSE WHEEL 3 3 6 Abnormal Landings LANDING WITH PARTIAL OR NO FLIGHT INSTRUMENT INFORMATION 1 Transponder Select Pressure Alt display using FUNC button 2 Selected Fie...

Страница 23: ...as airplane slows to stop 7 Directional Control MAINTAIN 8 Braking Use brakes only as needed to lessen chance of prop strike Rolling drag of the flat nose tire will increase braking effect 3 3 7 Canop...

Страница 24: ...r RPM The master switch need not be recycled since an overvoltage condition has not occurred to deactivate the alternator system 1 AVN MASTER Switch OFF NOTE Radio Transponder Pitch Trim and options A...

Страница 25: ...close circuit breaker If circuit breaker opens again do not reset If closed pull open TRIM AP Circuit Breaker then reset close the circuit breaker Electric pitch trim system remains inoperative 3 Redu...

Страница 26: ...st If the engine cannot be restarted a forced landing without power must be completed 3 4 2 Forced Landings If all attempts to restart the engine fail and a forced landing is imminent select a suitabl...

Страница 27: ...race your hands against a strong support to prevent your body hurling forward onto the dashboard If it looks as if you will fall in water grip the seatbelt mechanism for immediate release on touchdown...

Страница 28: ...uation that may happen in mountainous terrain is the closing of clouds over peaks severe turbulence or descending currents in valleys This situation calls for reorientation and continued flying or lan...

Страница 29: ...ings to assure optimum recoveries 5 HOLD THESE CONTROL INPUTS UNTIL ROTATION STOPS Premature relaxation of the control inputs may extend the recovery 6 AS ROTATION STOPS NEUTRALIZE RUDDER WINGS LEVEL...

Страница 30: ...l Operation IAS Kts km h Takeoff Normal Climb 65 76 120 140 Short Field Takeoff Flaps 10 V 50feet 59 110 En route Climb Flaps Up Normal Sea Level 65 76 120 140 Best Rate of Climb 90 166 Best Angle of...

Страница 31: ...e parked in a normal ground attitude to make sure that three drain valves allow for accurate sampling In cold weather remove even small accumulations of frost ice or snow from wing tail and control su...

Страница 32: ...ch OFF 2 LEFT WING 1 Main Wheel Tire CHECK proper inflation 30 PSI and general condition weather checks tread depth and wear etc 2 Brake Line CHECK security and condition 3 LDG GEAR and gear door CHEC...

Страница 33: ...CHECK security verify tab is faired with elevator when trimmed in T O position 4 Tail cone CHECK for security 5 RIGHT WING Trailing Edge 1 GRS bay cover CHECK security 2 Flap Gust Lock if installed RE...

Страница 34: ...ave approx 30 of free movement 3 Engine Top Cowl REMOVE put in safe location so that wind does not damage it 4 Propeller TURN in direction of rotation until oil in the tank blurbs 5 Engine Oil Dipstic...

Страница 35: ...n both tanks and top up both tanks Each tank is designed for 42 5 liters but real world application can vary by a small amount NOTE When fuel is just visible through the fuel filling hole near bottom...

Страница 36: ...safe distance from the propeller 9 IGNITION Switch START max 10 seconds release when engine starts after each start attempt 2 minute starter cool down is necessary NOTE If the engine is flooded push C...

Страница 37: ...ither ignition or 120 RPM differential between ignitions b Engine Indicators CHECK c AMPS and VOLTS CHECK 13 THROTTLE Control CHECK IDLE 1600 RPM 14 COM Frequency SET 15 GPS Flight Plan AS DESIRED 16...

Страница 38: ...if necessary DESCENT 1 Power AS DESIRED 2 Altimeter SET 3 Wing Flaps AS DESIRED 10 below 81 Kts 150 km h IAS 20 below 74 Kts 137 km h IAS FULL below 74 Kts 137 km h IAS 4 9 Landing APPROACH 1 Seat Bel...

Страница 39: ...control 9 Wing Flaps UP GO AROUND 1 THROTTLE Control FULL 2 Wing Flaps RETRACT to 10 3 LDG GEAR UP 4 Climb Speed 65 Kts 120 km h IAS until obstacle is cleared 5 Climb Speed 65 76 Kts 120 140 km h IAS...

Страница 40: ...46 85 WARNING Altitude loss during a stall recovery may be as much as 500 feet 5 2 Takeoff Distance m Distances stated are valid at sea level and MTOW 660 kg equipped with EPA Power SA R917Ti engine...

Страница 41: ...T tailwind Increase distance by 30 when landing with flaps UP Increase distance by 10 if concrete surface is wet and by 30 if grass is wet 5 6 Maximum Climb and Glide Sea Level 660 kg Rate ft min Spee...

Страница 42: ...d the test was performed at Vy 90 Kts IAS Minutes Press Alt OAT o C MAP RPM 0 2000 10 35 5500 1 3500 11 35 5500 2 4300 10 35 5500 3 5300 9 35 5500 4 6300 7 35 5500 5 7350 5 35 5500 6 8350 4 35 5500 7...

Страница 43: ...spinner tip The Design CG Range of 9 30 of Mean Average Wing Chord MAC or 3499 3760 mm aft of datum The length of MAC is 1243 mm The nose wheel center is located 2048 mm aft of datum and main gear whe...

Страница 44: ...rm All weights and moments are added up The Basic Empty CG Arm is obtained by dividing the sum of all three moments by the Basic Empty Weight Basic Empty Weight and CG Arm Table Position Weight kg Arm...

Страница 45: ...ng Weight 565 3 550 2005 62 This sample forward loading problem puts the sample airplane to the forward limit of the CG range 3 50 3 76m Loading Table 2 Sample Problem with Very AFT CG ITEM DESCRIPTIO...

Страница 46: ...2 kg l Standard fuel 85l max 3 492 Reduced fuel e g 42l 30 3 492 104 70 3 Pilot 80 3 488 279 04 4 Passenger 65 4 272 276 68 5 Baggage 4 955 6 Ramp Weight 579 3 591 2079 30 7 Fuel for start taxi run up...

Страница 47: ...elevator trim tab Attaching on either side the fuselage the wing contains fuel tanks at the wing root Aft of the rear wing spar are mounted the flaps inboard and ailerons outboard The wing empennage a...

Страница 48: ...6 2016 Dual control sticks are used for aileron and elevator control The control stick location is designed so that the pilot s right hand naturally falls on the control stick The rudder is held cent...

Страница 49: ...Pilots Operating Handbook 49 76 YL MFG Revision 7 Issue 1 4 6 2016...

Страница 50: ...el indicator 7 4 Wing Flap System The double slot type wing flaps are electrically operated by a flap control switch on the FlyBox Flap control unit located on the instrument panel A single electric s...

Страница 51: ...are located in the front The electrical system switch circuit breaker panel cabin heat and radiator flap control levers various switches and emergency gear lowering system are located on the middle c...

Страница 52: ...operate the COM separately 7 5 3 Cockpit Layout Description 1 Master Switch 5 ASI 13 Heater Control 2 Ignition Switch Key 6 ELT 14 Handbrake 3 Avionics switch 7 BRS Handle 15 USB Charging Port 4 Dyno...

Страница 53: ...evers The throttle control lever is on the left hand side in the cockpit for both pilot and passenger To operate push forward for more throttle and pull backwards for less throttle Brake lever works b...

Страница 54: ...s PITOT operates pitot heating INSTR powers all instruments MASTER main switch for all electric bus 7 5 8 Equipment Switch Panel There are 4 warning lights on top of front instrument panel ALT1 and AL...

Страница 55: ...Front Dynon Skyview for exporting flight logs and updating has a USB port built above the Skyview into the instrument panel To access the USB port on rear cockpit Dynon Skyview remove the 4 screws ho...

Страница 56: ...y pressing down on the tail cone bulkhead just forward of the horizontal stabilizer to raise the nose wheel off the ground Care should be exercised to ensure that pressure is exerted on a wide area Pr...

Страница 57: ...nding gear on the Tarragon features gas hydraulic shock absorbers and electric retraction system The nose wheel is steerable with directional control done via rudder pedals This permits very tight tur...

Страница 58: ...ositive locking has occurred when a distinctive snap sound is heard Tighten belt as needed to achieve proper fit Then attach the shoulder straps to the buckle in the same manner Proper installation of...

Страница 59: ...aph 2 9 for the engine limitations 7 14 Engine Lubrication System The engine is provided with a dry sump forced lubrication system with a main oil pump with integrated pressure regulator 1 and oil pre...

Страница 60: ...needs no external power supply Two independent charging coils 1 located on the generator stator supply one ignition circuit each The energy is stored in capacitors of the electronic modules 2 At the...

Страница 61: ...the standard location of the radiator 2 is below engine level the expansion tank located on top of the engine allows for coolant expansion The expansion tank is closed by a pressure cap 3 with excess...

Страница 62: ...through a fine fuel filter and to a return line with a pressure regulator The fuel system needs to hold a specific and accurate pressure CAUTION The injectors are sensitive to fuel pressure in the fu...

Страница 63: ...ked 7 17 3 Fuel Drain Valves The fuel system is equipped with 2 drain valves in the fuel tanks under each wing to provide a means for the examination of fuel in the system for contamination and grade...

Страница 64: ...Pilots Operating Handbook 64 76 YL MFG Revision 7 Issue 1 4 6 2016 7 18 Electrical Wiring Diagram...

Страница 65: ...A 20 0 Discharge Current A 160 0 Discharge Pulse Current A 10 seconds 240 0 Discharge Pulse Current A 1 second 300 0 Discharge Performance at 20 0 C rated capacity Ah 4 6 Discharge Performance at 20...

Страница 66: ...arachute is pulled from the container then the bag of parachute is discarded and parachute canopy is filled with air For proper operation it is necessary to remove the locking pin for the handle befor...

Страница 67: ...hat is clamped to the oil tank The Reiff is FAA approved and includes a thermostat to keep the oil from exceeding 150 o F The connector for the heater charger is located on the lower left side of the...

Страница 68: ...endum Special attention must be devoted to areas which are affected by the high vibrations and high temperatures from the engine These include Propeller attachment Exhaust system Engine attachment Wir...

Страница 69: ...neuvering Speed Maximum speed the airplane may be stalled without exceeding structural limitations VFE Maximum Flap Extended Speed Highest speed permissible with wing flaps in a prescribed extended po...

Страница 70: ...ccepted as a measure of the applied power or thrust MCP Maximum Continuous Power Maximum power for abnormal or emergency operations BHP Brake Horsepower Power developed by the engine RPM Revolutions P...

Страница 71: ...m Moment Product of the weight of an item multiplied by its arm Moment divided by the constant 1000 is used in this POH to simplify balance calculations by reducing the number of digits C G Center of...

Страница 72: ...ginary rectangular airfoil having the same pitching moments throughout the flight range as that of the actual wing Electrical and Avionics Terminology EFIS Electronic Flight Information System AVN Avi...

Страница 73: ...Pilots Operating Handbook 73 76 YL MFG Revision 7 Issue 1 4 6 2016 Metric Imperial U S Conversion Charts Length Conversions...

Страница 74: ...Pilots Operating Handbook 74 76 YL MFG Revision 7 Issue 1 4 6 2016 Distance Conversions...

Страница 75: ...Pilots Operating Handbook 75 76 YL MFG Revision 7 Issue 1 4 6 2016 Temperature Conversions Pressure Conversions...

Страница 76: ...ating Handbook 76 76 YL MFG Revision 7 Issue 1 4 6 2016 Fuel Volume To Weight Conversions List of Manuals 1 Maintenance Manual 2 EPA Power Engine Manual 3 Skyview Pilot s User s Guide 4 Manual for EFI...

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