czech sport aircraft PS-28 cruiser, Operating Handbook

Page 1: ...o 1 Pilot s Operating Handbook P PS S 2 28 8 C Cr ru ui is se er r equipped with Dynon SkyView System Airplane Registration Number Airplane Serial Number This Pilot s Operating Handbook is EASA approv...

Page 2: ...PS POH 1 1 13 P PS S 2 28 8 C Cr ru ui is se er r Date 2014 06 17 ii Rev No Intentionally left blank...

Page 3: ...EVISIONS Rev No Affected pages Revision name Approved Date 1 i v vii viii ix x xi xii xiii xiv xv xvi 1 4 2 6 2 7 2 8 3 14 3 15 4 5 4 6 4 8 4 11 5 2 7 3 7 7 8 5 Substitution pages for aircraft with CT...

Page 4: ...PS POH 1 1 13 P PS S 2 28 8 C Cr ru ui is se er r Date 2014 06 17 vi Rev No Intentionally left blank...

Page 5: ...2015 11 11 EASA approved 3 9 2014 06 17 xv 2015 11 11 EASA approved 3 10 2014 06 17 xvi 2015 11 11 EASA approved 3 11 2014 06 17 EASA approved 3 12 2014 06 17 1 EASA approved 3 13 2014 06 17 1 1 2014...

Page 6: ...ed 5 10 2014 06 17 7 10 2014 06 17 EASA approved 5 11 2014 06 17 7 11 2014 06 17 EASA approved 5 12 2014 06 17 7 12 2014 06 17 6 8 EASA approved 6 1 2014 06 17 8 1 2014 06 17 EASA approved 6 2 2014 06...

Page 7: ...Foot or feet 1 ft 12 in 0 305 m 305 mm fpm Vertical speed in feet per minute 1 fpm 0 0051 m s GPS Global Positioning System hp Power unit 1 hp 0 7457 kW IAS Indicated Airspeed IC Intercom IFR Instrum...

Page 8: ...psi Pressure unit pound per square inch 1psi 0 0689 bar rpm Revolutions per minute s or sec Second SM Statute Mile 1SM 1 609 m TAS True Airspeed US gal US gallon 1 US gal 0 83 UK gal 3 785 L V Volt V...

Page 9: ...ru ui is se er r Date 2015 11 11 xi Rev No 1 CS LSA STANDARD The P PS S 2 28 8 C Cr ru ui is se er r aircraft is designed and built according to CS LSA standard CS LSA Initial Issue 27 June 2011 Certi...

Page 10: ...PS POH 1 1 13 P PS S 2 28 8 C Cr ru ui is se er r Date 2015 11 11 xii Rev No 1 Intentionally left blank...

Page 11: ...se er r Date 2015 11 11 xiii Rev No 1 CONTACT INFORMATION Czech Sport Aircraft a s Na Z honech 1177 212 686 04 Kunovice Czech Republic Website www czechsportaircraft com E mail office czechsportaircr...

Page 12: ...PS POH 1 1 13 P PS S 2 28 8 C Cr ru ui is se er r Date 2015 11 11 xiv Rev No 1 Intentionally left blank...

Page 13: ...u ui is se er r Date 2015 11 11 xv Rev No 1 TABLE OF CONTENTS 1 General Information 2 Limitations 3 Emergency Procedures 4 Normal Procedures 5 Performance 6 Weight and Balance 7 Description of Airplan...

Page 14: ...PS POH 1 1 13 P PS S 2 28 8 C Cr ru ui is se er r Date 2015 11 11 xvi Rev No 1 Intentionally left blank...

Page 15: ...SECTION 1 PS POH 1 1 13 P PS S 2 28 8 C Cr ru ui is se er r GENERAL INFORMATION Date 2014 06 17 1 3 Rev No P PS S 2 28 8 C Cr ru ui is se er r aircraft layout...

Page 16: ...Aileron 15 15 1 Flaps 0 to 30 1 Aileron trim 20 20 2 Elevator trim 22 28 2 Anti balance tab 25 19 2 Engine Manufacturer BRP Powertrain GmbH Co KG Model number 912 S2 ULS2 Maximum power rating 73 5 kW...

Page 17: ...SI 912 016 latest edition MOGAS European standards min RON 95 EN 228 Super EN 228 Super plus US standard ASTM D4814 Canadian standards min AKI 91 CAN CGSB 3 5 Quality 3 CAUTION Fuels that contain more...

Page 18: ...m max 5 min Max continuous 5 500 rpm Cruising 75 5 000 rpm Idling 1 400 rpm minimum Oil pressure Minimum 0 8 bar below 3 500 rpm Maximum 7 bar cold engine starting Normal 2 5 bar above 3 500 rpm Oil t...

Page 19: ...C 50 90 C 90 110 C 110 130 C 130 C Coolant Temperature CT to 50 C 50 120 C 120 C Fuel Pressure 0 14 bar 0 14 0 15 bar 0 15 0 50 bar 0 50 0 51 bar 0 51 bar Manifold Pressure 10 35 inHg 2 14 Engine ins...

Page 20: ...BITED WARNING Minimum 6 L of fuel quantity allows approximately 15 minutes of safe operation Dynon SkyView system limitations The Dynon SkyView Pilot s User Guide Document 101321 016 Revision Q or lat...

Page 21: ...ve mentioned cases there are no flight problems no vibrations good aircraft control and no change of flight characteristics It is not possible to close the canopy Recommended procedure if the canopy o...

Page 22: ...o one of three severity levels MESSAGE Advisory message CAUTION A condition which is abnormal but not critical in nature may increase pilot workload WARNING A critical condition that should be address...

Page 23: ...RATION The currently active ADAHRS has detected vibration that will affect G Meter and attitude indicator performance Troubleshoot when able BATTERY MISSING FAULT A previously connected backup battery...

Page 24: ...SECTION 3 PS POH 1 1 13 P PS S 2 28 8 C Cr ru ui is se er r EMERGENCY PROCEDURES Date 2014 06 17 3 16 EASA approved Rev No Intentionally left blank...

Page 25: ...ht controls free correct movement 2 Canopy clean close and lock 3 Safety harness fasten 4 Brakes fully applied 5 PARKING BRAKE use 4 2 2 Engine starting 1 THROTTLE IDLE 2 CHOKE cold engine ON fully pu...

Page 26: ...0 open 4 2 3 Engine warm up Prior to engine check block the main wheels using chocks Initially warm up the engine to 2 000 rpm for approximately 2 min then continue to 2 500 rpm till oil temperature r...

Page 27: ...tle IDLE 6 Engine acceleration check CAUTION To prevent impact load wait for around 3 sec after throttling back to partial load to reach constant speed before re acceleration 7 Ignition check set engi...

Page 28: ...on green mark 4 Flight controls check free movement 5 Cockpit canopy closed and locked Recommendation Before takeoff manually check the canopy is locked by pushing the canopy upwards 6 Safety harness...

Page 29: ...conditions the engine temperatures stabilize during descent taxiing and at values suitable to stop engine by switching the ignition off If necessary cool the engine at engine speed within the range 2...

Page 30: ...g only between flights during a flight day After ending the flight day or at low temperatures of ambient air do not use parking brake but use the wheel chocks instead NOTE Use anchor eyes on the wings...

Page 31: ...1 EASA approved Rev No SECTION 5 TABLE OF CONTENTS 5 PERFORMANCE 5 1 Takeoff distances 5 3 5 2 Landing distances 5 3 5 3 Rate of climb 5 3 5 4 Cruise speeds 5 4 5 5 RPM setting and fuel consumption 5...

Page 32: ...ing techniques If not stated otherwise the performance stated in this section is valid for maximum takeoff weight 600 kg and under ISA conditions The performance shown in this section is valid for air...

Page 33: ...m air cooled cylinders Dry sump forced lubrication Dual contactless capacitor discharge ignition The engine is fitted with an electric starter AC generator and mechanical fuel pump Prop drive via redu...

Page 34: ...stable propeller is installed The propeller diameter is 1 712 mm NOTE For technical data refer to documentation supplied by the propeller manufacturer 7 7 Landing gear Aircraft is equipped with tricyc...

Page 35: ...stem EMS 7 13 1 Primary Flight Display PFD Airplane is fitted with Primary Flight Display PFD DynonSkyView SV D1000 which has following functions Airspeed indicator Altimeter Attitude indicator Vertic...

Page 36: ...splay in the system can also have its own layout NOTE Screen 1 Pilot in Command seat left Screen 2 Passenger seat right The predefined layout configuration by the manufacturer is as follows The basic...

Page 37: ...ventional coolant based on ethylene glycol mixture with 50 of water NOTE With the change to a new cylinder heads design applicable for 912 ULS2 engines from S N 6 781 410 inclusive and 912 S2 engines...

Page 38: ...arm water with an adequate quantity of detergents Dry the upholstery thoroughly before insertion into the cockpit CAUTION In the case of long term parking cover the canopy to protect the cockpit inter...