Jihlavan KP-5 ASA Pilot Operating Handbook Download

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Pilot Operating Handbook KP-5 ASA

FUEL PRESSURE
EGT

(EXHAUST GAS TEMPERATURE)

1616 °F (880°C)
1652 °F (900°C)
CHT

(CYLINDER HEAD TEMPERATURE)

Labels on the lower instrument panel:

FUEL L
FUEL R

- fuel cock:

TANK L

TANK R

CLOSED

Labels on tunnel between seats (from ahead):

- label on the throttle lever:

MIN

EXTENDED

MAX

RETRACTED

Summary of Contents for KP-5 ASA

Page 1: ...O O K of KP 5 ASA Including Aircraft Operating Instructions and Flight Training Supplement Manufacturer JIHLAVAN airplanes s r o Znojemsk 64 586 01 Jihlava Czech Republic Production number 5 198 209...

Page 2: ...HE AIRCRAFT Owner of the aircraft Name Address Identity number Registration mark From To The change of the ownership Name Address Identity number Registration mark From To The change of the ownership...

Page 3: ...er of the aircraft Name Address Identity number Registration mark From To The change of the ownership Name Address Identity number Registration mark From To The change of the ownership Name Address Id...

Page 4: ...al information 5 CHAPTER 2 Operating limitations 18 CHAPTER 3 Weight and balance informations 23 CHAPTER 4 Performance 27 CHAPTER 5 Emergency procedures 31 CHAPTER 6 Standard procedures 36 CHAPTER 7 P...

Page 5: ...ATION Chapter contents Page 1 1 Introduction 6 1 2 Amendments 6 1 3 Abbreviations and definitions 8 1 4 Dimensions of the aircraft 9 1 5 Basic technical data 10 1 6 Engine 11 1 7 Propeller 12 1 8 Flui...

Page 6: ...ends an operational update with new and revised information to the owner of the Pilot Operating handbook b the holder of the Pilot Operating handbook is obliged 1 to change the original information wi...

Page 7: ...nts list Number of the change Number of amendment update Number of concerned pages Issue date of the new pages Date of new pages change and signature Note The holder of the Pilot Operating handbook fi...

Page 8: ...idering undisturbed air IFR Instrument flight rules VFR Visual flight rules ISA International standard atmosphere MAC Mean aerodynamic chord VTU Vertical tail unit fin with rudder HTU Horizontal tail...

Page 9: ...Pilot Operating Handbook KP 5 ASA 9 1 4 Dimensions of the aircraft...

Page 10: ...nstruction Tail units are self contained all metal with a forward HTU The aircraft is equiped with the fixed three wheel undercarriage 1 5 2 Dimensions of the aircraft Wing span Length Height Wing are...

Page 11: ...o 16o 1o 10o 2o 35o 2o 34o 3o 28o 2o 28o 2o 28o 2o 30o 2o 30o 2o 1 5 4 Weights Empty weight Maximum T O weight Maximum cabin baggage weight 787 lb 357 kg 1279 lb 580 kg 66 lb 30 kg 1 6 Engine Detailed...

Page 12: ...turer Engine 912 UL 912 ULS Fuel Min RON 90 Min RON 95 EN 228 Normal EN 228 Super EN 228 Super EN 228 Super plus EN 228 Super plus AVGAS 100 LL AVGAS 100 LL Canadian standard CAN CGSB 3 5 CAN CGSB 3 5...

Page 13: ...dicated by permanent light 2 x 8 45 U S gal 2 x 0 4 U S gal 5 1 3 1 9 U S gal Valid values for the aircraft equipped with additional fuel tanks Capacity Max capacity Inexhaustible volume Expansion cap...

Page 14: ...03 C308949 Oil pressure indicator ROAD 000531 CHT temp indicator XIH4 0018 00 30 11 2010 OIL temperature indicator XIH4 0010 00 11 05 2010 Fuel pressure indicator Engine hours indicator LR42455 AU1774...

Page 15: ...Pilot Operating Handbook KP 5 ASA 15 1 10 Cockpit...

Page 16: ...nder 6 Turn and bank indicator 53 Circuit breakers 7 Trim attitude indicator 54 Cooling 55 Heating 11 Engine hours indicator 12 Engine speed indicator 13 Oil pressure gauge 14 Cylinder head temperatur...

Page 17: ...Pilot Operating Handbook KP 5 ASA 17 1 10 1 Operating switches of the left control stick Key 1 Transciever 2 Trim nose down 3 Trim nose up 4 Unused button 5 Intercom...

Page 18: ...speed limitatons 19 2 3 Colour code markings of airspeed indicator 19 2 4 Engine operational limitations 20 2 5 Wind operational limitations 20 2 6 Fuel capacity 20 2 7 Weights and C G limits 20 2 8 M...

Page 19: ...aximum velocity with flaps fully extended VFE 59 68 Stalling speed in landing configuration VS0 35 40 Stalling speed with retracted flaps VS 42 48 2 3 Engine operational limitations Specifications sta...

Page 20: ...um wind speed component for take offs and landings in RWY direction headwind 23 3 kt crosswind 15 6 kt 2 5 Fuel capacity Fuel capacity in one tank 8 45 11 9 U S gal Total fuel capacity 16 9 23 8 U S g...

Page 21: ...Pilot Operating Handbook KP 5 ASA 21 2 8 Maneuvers prohibited Acrobatic intentionally driven stalls and spins are prohibited 2 9 Flight envelope For maximum take off weight of 1279 lb...

Page 22: ...aircraft on the ground always use the tow bar push the plane at the center section only do not push nor pull the aircraft via the propeller do not push nor pull the aircraft via the wings or control s...

Page 23: ...rating Handbook KP 5 ASA 23 3 0 WEIGHT AND BALANCE INFORMATION Chapter contents Page 3 1 Installed equipment list 24 3 2 Weight and Center of Gravity limits 24 3 3 Weight and Center of Gravity limits...

Page 24: ...nd Center of Gravity limits Empty weight 357 lb Maximum take off weight 1 279 lb Maximum cabin baggage weight 66 lb Minimum pilot weight 132 lb Front limit of C G position 22 MAC Rear limit of C G pos...

Page 25: ...Pilot Operating Handbook KP 5 ASA 25 3 3 Weight and Center of Gravity limits chart TOW and C G check diagram...

Page 26: ...KP 5 ASA 26 Example of using Center of Gravity limits chart Start at point of empty weight and C G position of your aircraft Start with one item and its weight then add another one to the end of previ...

Page 27: ...5 ASA 27 4 0 PERFORMANCE Chapter contents Page 4 1 Cruising speeds 28 4 2 Stalling speeds 28 4 3 Take off distance and landing distance 28 4 4 Climbing 29 4 5 Gliding 29 4 6 Flight range 29 4 7 Ceilin...

Page 28: ...Flaps extended landing position speed VS0 33 knots 38 MPH Note The airspeeds stated above are valid for idle engine speed 4 3 Take off distance and landing distance 4 3 1 Take off Concrete RWY R 912 U...

Page 29: ...4 5 Gliding Gliding velocities engine idling m 1279 lb Optimal airspeed of gliding 48 54 knost 55 62 MPH Sink rate fpm 550 Gliding velocities engine stopped flaps take off position m 1279 lb Optimal a...

Page 30: ...ROTAX 912 UL Fuel consumption at max power RPM 5500 RPM 4 76 U S gal h Fuel consumption at 75 power RPM 4300 RPM 3 17 U S gal h ROTAX 912 ULS Fuel consumption at max power RPM 5500 RPM 6 88 U S gal h...

Page 31: ...rolling 32 5 2 Engine failure after take off 32 5 3 Engine failure during flight 32 5 4 Emergency landing 33 5 5 Interrupted landing 33 5 6 Fire on ground engine not running 33 5 7 Fire on ground eng...

Page 32: ...off 4 Fuel cock close 5 Master switch off 6 Seat belts fasten 7 Flaps as needed 5 3 Engine failure during flight Insufficient height for attempt to start up the engine 1 Airspeed 48 51 knots 55 59 MPH...

Page 33: ...area 8 Magnetoes off 9 Fuel cock close 10 Master switch off 11 Seat belts fasten 12 Flaps as needed 5 4 Emergency landing 1 Airspeed 48 51 knots 55 59 MPH 2 Landing area choice landing direction surfa...

Page 34: ...help increase airspeed to the safe maximum in this situation 8 Now follow emergency landing procedures After extinguishing fire do not try to start up the engine again Note Time necessary to deplete f...

Page 35: ...tions If unnatural vibrations occur it is necessary to 1 Set the engine speed to minimize vibrations 2 Proceed with a precautionary landing to the nearest airfield or other suitable terrain 3 If vibra...

Page 36: ...ne 41 6 4 Engine warm up and engine check 42 6 5 Procedures before taxiing 43 6 6 Procedures on holding point 43 6 7 Start line procedures take off 44 6 8 Cruise 44 6 9 Down wind procedures 44 6 10 Ba...

Page 37: ...guy ropes chock the wheels Carry out the fuel tanks mud discharging Mud traps are placed at the bottom of both fuel tanks There are numbered checking points on the drawing These numbers are presented...

Page 38: ...ition and attachment of engine engine screws and engine mounting screws shock absorbers condition The spiral springs condition on exhaust system and their security lock with binding wire exhaust gas t...

Page 39: ...om side of fuel tank Fuel tank filler caps seals Free passage of fuel tank ventilation e Wings 1 5 6 7 8 15 16 17 18 19 check the following Leading edge cover check and whole wing cover Winglets rivet...

Page 40: ...chanical brakes hydraulic hose and brake check liquid emission for hydraulic brakes i Fuselage 1 8 9 11 12 14 15 19 check the following Fuselage covers Cable covers belts and casing of emergency parac...

Page 41: ...n 5 Control stick free movement 6 Flaps free movement retract 7 Brakes function 8 Master switch on 9 Instruments check values and settings lock positions of gyroscopic instruments 10 Trim function tes...

Page 42: ...e start up is 10 sec It is possible to repeat starting up process with 2min delay for starting gear cooling Oil pressure must rise within 10 sec of start When oil pressure is steady above 2 bars it is...

Page 43: ...brake and directional control range when taxiing 6 Adjust speed of taxiing to airfield surface condition and wind direction and speed Warning Max taxiing speed is 8 kt 9 MPH 6 6 Procedures on holding...

Page 44: ...1 min 8 Flaps up height 500 ft 9 Engine instruments check 10 Trim as needed 6 8 Cruise 1 Fuel cock check fuel tank with sufficient fuel quantity 2 Throttle 75 of max power 4300 RPM 3 Speed 105 knots...

Page 45: ...ft 7 Lose speed by gradually pulling control stick and touch down on main landing gear 8 Brake as needed hold direction with control 6 12 Procedures after landing 1 Vacate RWY time 2 Engine speed idle...

Page 46: ...stop 3 Full throttle 4 After stop rotation take airplane to horizontal flight by longitudinal control 6 14 2 Right spin If airplane came on to right spin 1 Resolutely push stick to the front 2 Press l...

Page 47: ...Chapter contents Page 7 1 Airspeed indicator range markings 48 7 2 Operating limitations on instrument panel 49 7 3 Passenger warning on instrument panel 49 7 4 Flight warning on instrument panel 49 7...

Page 48: ...nal range with flaps down Green arc 44 117 knots 51 138 MPH normal range of operating Yellow arc 117 140 knots 138 162 MPH range of operating in calm air and with greater attention The first red radia...

Page 49: ...ake off weight 1279 lb Max total baggage weight on board 66 lb Min pilot weight 132 lb Never exceed speed VNE 162 MPH Minimum permitted speed in landing configuration VSO 40 MPH Never exceed speed wit...

Page 50: ...rcraft equipment 7 5 1 Limitations restrictions warnings Notices are placed on the instrument panel within view of the pilot NO SMOKING 7 5 2 Regitration mark XX YYY 00 7 5 3 Labeling operating and co...

Page 51: ...erating Handbook KP 5 ASA 51 Controls CHOKE HEATING PULL TO OPEN COOLING L PULL ON COOLING R PULL ON Engine instruments OIL PRESSURE oil pressure range OIL TEMPERATURE oil temperature range R912UL R91...

Page 52: ...RATURE 1616 F 880 C 1652 F 900 C CHT CYLINDER HEAD TEMPERATURE Labels on the lower instrument panel FUEL L FUEL R fuel cock TANK L TANK R CLOSED Labels on tunnel between seats from ahead label on the...

Page 53: ...Pilot Operating Handbook KP 5 ASA 53 Labels on back wall of cockpit marking of headsets inlets CO PILOT PILOT External labels DO NOT PUSH DO NOT STEP DO NOT TOUCH 36 psi FUEL 8 45 11 9 U S gal...

Page 54: ...Pilot Operating Handbook KP 5 ASA 54 8 0 AIRCRAFT GROUND HANDLING AND SERVICING Chapter contents Page 8 1 Towing and tie down instructions 55 8 2 Servicing fuel oil and coolant anb brake fluid 55...

Page 55: ...laced on blocks it is prohibited to enter the cockpit except for training purposes or and possible repairs 8 2 Servicing fuel oil and coolant Fuel and oil are highly flammable Do not manipulate with f...

Page 56: ...stated in this handbook 8 2 3 Coollant Cooling liquid Mr Vif Antifreeze BC distilled water 1 1 Max cooling liquid volume 0 71 U S gal Oil servicing by Operator s Manual for all versions of ROTAX 912 I...

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