czech sport aircraft Piper Sport Pilot Operating Handbook Download Page 53

Page: 53 / 98

Date of issue: 10/03/31

Revision: -

PS-POH-1-1-01

SECTION 5
PERFORMANCE

5-1

SECTION 5

TABLE OF CONTENTS

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

5-5

5.6 Airspeed indicator system calibration

5-6

Summary of Contents for Piper Sport

Page 1: ...10 03 31 Revision PS POH 1 1 01 i Pilot s Operating Handbook Airplane Registration Number Airplane Serial Number P1001001 POH Copy Number P Pi ip pe er rS Sp po or rt t D Di is st tr ri ib bu ut ti io on n I In nc c ...

Page 2: ...Date of issue 10 03 31 Revision PS POH 1 1 01 ii Intentionally left blank ...

Page 3: ... rt t a ai ir rc cr ra af ft t i is s d de es si ig gn ne ed d a an nd d m ma an nu uf fa ac ct tu ur re ed d b by y Czech sport aircraft a s Na Záhonech 1177 212 686 04 Kunovice Czech Republic www czechsportaircraft com office czechsportaircraft com Fax 420 576 519 394 Phone 420 576 514 034 Sales Dept ...

Page 4: ...Revision PS POH 1 1 01 Date of issue 10 03 31 iv Intentionally left blank ...

Page 5: ...Revision PS POH 1 1 01 RECORD OF REVISIONS Date of issue 10 03 31 v RECORD OF REVISIONS No Affected pages Revision name Date of Issue Signature ...

Page 6: ...Revision PS POH 1 1 01 Date of issue 10 03 31 vi Intentionally left blank ...

Page 7: ...issue 10 03 31 vii LIST OF EFFECTIVE PAGES Section Page Revision No Section Page Revision No 1 1 1 3 3 1 1 2 3 2 1 3 3 3 1 4 3 4 1 5 3 5 1 6 3 6 3 7 2 2 1 3 8 2 2 3 9 2 3 3 10 2 4 2 5 4 4 1 2 6 4 2 2 7 4 3 2 8 4 4 2 9 4 5 2 10 4 6 2 11 4 7 2 12 4 8 4 9 4 10 ...

Page 8: ...AGES Date of issue 10 03 31 viii LIST OF EFFECTIVE PAGES Cont d Section Page Revision No Section Page Revision No 5 5 1 8 8 1 5 2 8 2 5 3 8 3 5 4 8 4 5 5 8 5 5 6 8 6 6 6 1 9 9 1 6 2 9 2 6 3 6 4 6 5 6 6 6 7 6 8 7 7 1 7 2 7 3 7 4 7 5 7 6 7 7 7 8 ...

Page 9: ...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 Instrument Flight Rules in Inch 1 in 25 4 mm ISA International Standard Atmosphere KCAS Calibrated Airspeed in Knots kg Kilogram 1 kg 2 205 lb KIAS Indicated Airspeed in Knots km kilometer 1 km 1000 m 0 54 NM 0 621 SM km h Speed in kilometers per hour 1 km h 0 54 knots 0 62...

Page 10: ...er square inch 1psi 0 0689bar rpm Revolutions per minute s or sec Second SM Statute Mile 1SM 1 609 m US gal US gallon 1 US gal 0 83 UK gal 3 785 l V Volt VFR Visual Flight Rules VMC Visual Meteorological Conditions VSI Vertical Speed Indicator VTU Vertical tail unit VA Maneuvering airspeed VFE Maximum flap extended speed VNE Never exceed speed VNO Maximum designed cruising speed VSO Stall speed wi...

Page 11: ...ce of a Light Sport Airplane ASTM F 2279 10 Standard Practice for Quality Assurance in Manufacture of Fixed Wing Light Sport Aircraft ASTM F 2295 10 Standard Practice for Continued Operational Safety Monitoring of a Light Sport Aircraft ASTM F 2316 08 Standard Specification for Airframe Emergency Parachutes for Light Sport Aircraft ASTM F 2746 09 Standard Specification for Pilot s Operating Handbo...

Page 12: ...MATION Czech sport aircraft a s Na Záhonech 1177 212 686 04 Kunovice Czech Republic www czechsportaircraft com office czechsportaircraft com Fax 420 576 519 394 Phone 420 576 514 034 Sales Dept CONTACT INFORMATION FOR RECOVERY OF CERTIFICATION DOCUMENTATION PiperSport Distribution Inc ...

Page 13: ...0 03 31 TABLE OF CONTENTS xiii TABLE OF CONTENTS 1 General Information 2 Limitations 3 Emergency Procedures 4 Normal Procedures 5 Performance 6 Weight and Balance 7 Description of Airplane and Systems 8 Handling and Servicing 9 Supplements ...

Page 14: ...Revision PS POH 1 1 01 Date of issue 10 03 31 xiv Intentionally left blank ...

Page 15: ...SECTION 1 GENERAL INFORMATION PS POH 1 1 01 Date of issue 10 03 31 Revision 1 1 SECTION 1 TABLE OF CONTENTS 1 GENERAL INFORMATION 1 1 Airplane specification 1 2 1 2 Summary of performances 1 5 ...

Page 16: ...ilot s Operating Handbook WARNING Means that the non observation of the corresponding procedure leads to an immediate or important degradation of the flight safety i e to injury or death of persons CAUTION Means that the non observation of the corresponding procedure leads to a minor or possible long term degradation of the flight safety NOTE Draws attention to any special item not directly relate...

Page 17: ...SECTION 1 GENERAL INFORMATION PS POH 1 1 01 Date of issue 10 03 31 Revision 1 3 Aircraft layout ...

Page 18: ...udder 30 to each side Elevator 28 25 Aileron 20 15 Flaps 0 to 30 Aileron trim 20 20 Elevator trim 22 28 Engine Manufacturer BRP Rotax GmbH Co KG Model number 912ULS Maximum horsepower rating 98 6 hp 73 5 kW at 5800 RPM Cooling liquid and air Type 4 stroke 4 cylinder horizontally opposed spark ignition engine with one central camshaft push rod OHV Propeller Manufacturer WOODCOMP s r o Model number ...

Page 19: ...n each wing locker 44 lb 20 kg Empty weight minimum equipment 760 lb 345 kg NOTE Actual empty weight is shown in Section 9 Supplement No 02 Wing loading 10 lb sq ft 49 kg m 2 Power loading 13 39 lb hp 8 15 kg kW Speeds Maximum at sea level 125 knot 143 mph Cruise 75 power at 3 000 ft 97 knot 111 mph Range and endurance Range 520 NM Endurance 5 3 hours Conditions Usable fuel 29 85 US gal 113 liter ...

Page 20: ... vy 65 knot 75 mph Stall speeds VS0 flaps down power idle 32 knot 37 mph VS1 flaps up power idle 39 knot 45 mph Fuel Total fuel capacity 30 12 US gal 114 liter Total usable fuel 29 86 US gal 113 liter Approved types of fuel MOGAS min RON 95 EN 228 and EN 228 Super plus AVGAS 100 LL Engine power Maximum power at 5 800 RPM 98 6 hp 73 5 kW Max continuous power at 5 500 RPM 92 5 hp 69 kW ...

Page 21: ...ed range 2 3 2 4 Maneuvering speed 2 3 2 5 Maximum structural cruising speed 2 3 2 6 Never exceed speed 2 3 2 7 Service ceiling 2 3 2 8 Load factors 2 3 2 9 Approved maneuvers 2 3 2 10 Operating weights and loading 2 4 2 11 Fuel 2 5 2 12 Engine operating speeds and limits 2 6 2 13 Engine instruments markings 2 7 2 14 Other limitations 2 7 2 15 Limitation placards and markings 2 9 2 16 Miscellaneou...

Page 22: ...te arc 32 75 37 86 Flap Operating Range Green arc 39 108 45 124 Normal Operating Range Yellow arc 108 138 124 158 Maneuvers must be conducted with caution and only in smooth air Red line 138 158 Maximum speed for all operations 2 2 Stalling speeds at maximum takeoff weight IAS CAS Altitude loss at recovery Conditions Weight MTOW Engine idle Wing flaps pos knot mph knot mph ft 0 39 45 43 49 65 15 3...

Page 23: ...mph 2 5 Maximum structural cruising speed VNO Maximum structural cruising speed IAS 108 knot 124 mph 2 6 Never exceed speed VNE Never exceed speed IAS 138 knot 158 mph 2 7 Service ceiling Service ceiling 10 000 ft 2 8 Load factors Maximum positive limit load factor 4 g Maximum negative limit load factor 2 g 2 9 Approved maneuvers The PiperSport is approved for normal and below listed maneuvers Ste...

Page 24: ... kg Max baggage weight in rear fuselage 40 lb 18 kg Max baggage weight in each wing locker 44 lb 20 kg Empty weight minimum equipment 760 lb 345 kg NOTE Actual empty weight is shown in Section 9 Supplement No 02 WARNING Do not exceed maximum takeoff weight 1 320 lb 600 kg Number of seats 2 Minimum crew 1 pilot on the left seat Minimum crew weight 95 lb 43 kg Maximum crew weight on each seat 253 lb...

Page 25: ...l section 10 2 2 Fuel Rotax Service Instruction SI 912 016 MOGAS European standard min RON 95 EN 228 Super EN 228 Super plus US standard ASTM D4814 Canadian standard min AKI 91 CAN CGSB 3 5 Quality 3 AVGAS US standard AVGAS 100 LL ASTM D910 AVGAS 100 LL places greater stress on the valve seats due to its high lead content and forms increased deposits in the combustion chamber and lead sediments in...

Page 26: ...02 psi 7 bar cold engine starting Oil pressure Optimum 29 73 psi 2 5 bar above 3 500 rpm Minimum 122 F 50 C Maximum 266 F 130 C Oil temperature Optimum 194 230 F 90 110 C Minimum 122 F 50 C Cylinder head temper CHT Maximum 275 F 135 C Nominal 1 472 F 800 C Maximum 1 562 F 850 C Exhaust gas temperature EGT Max Takeoff 1 616 F 880 C Minimum 2 2 psi 0 15 bar Fuel press Maximum 5 8 psi 0 4 bar See the...

Page 27: ...102 psi 7 bar Oil Temperature 122 F 50 C 122 194 F 50 90 C 194 230 F 90 110 C 230 266 F 110 130 C 266 F 130 C Cylinder head Temperature CHT 122 275 F 50 135 C 275 F 135 C Exhaust Gas Temp EGT 752 932 F 400 500 C 932 1 562 F 500 850 C 1 562 1 616 F 850 880 C 1 616 F 880 C Fuel Pressure 2 2 psi 0 15 bar 2 2 5 8 psi 0 15 0 4 bar 5 8 psi 0 4 bar 2 14 Other limitations No smoking on board of the aircra...

Page 28: ...mperature indicator Oil pressure indicator Cylinder head temperature indicator Safety harness for every used seat WARNING IFR FLIGHTS AND INTENTIONAL FLIGHTS UNDER ICING CONDITIONS ARE PROHIBITED WARNING EMERGENCY PARACHUTE APPROVED FOR UP TO MTOW 1 350 LBS AND MAX VELOCITY 120 KNOTS WARNING MINIMUM 1 58 US GAL 6 LITRES OF FUEL QUANTITY ALLOWS APPROXIMATELY 15 MINUTES OF SAFE OPERATION CAUTION Ins...

Page 29: ... VNE 138 kts VA 88 kts VFE 75 kts VSO 32 kts WARNING DO NOT EXCEED MAXIMUM TAKE OFF WEIGHT 600kg 1320lbs WARNING IFR FLIGHTS AND INTENTIONAL FLIGHTS UNDER ICING CONDITIONS ARE PROHIBITED MAX WEIGHT IN WING LOCKER 20kg 44lbs MAX BAGGAGE WEIGHT 18kg 40lbs THIS AIRCRAFT WAS MANUFACTURED IN ACCORDANCE WITH LIGHT SPORT AIRCRAFT AIRWORTHINESS STANDARDS AND DOES NOT CONFORM TO STANDARD CATEGORY AIRWORTHI...

Page 30: ...ision 2 10 Prohibited maneuvers NO INTENTIONAL SPINS AEROBATICS PROHIBITED 2 16 Miscellaneous placards and markings FUEL CAPACITY 57 Litres 15 US Gal MOGAS RON 95 AKI 91 FUEL DRAIN AEROSHELL OIL SPORT PLUS 4 MAX P O W E R IDLE OFF C H O K E ON C O L P O E S N E ª ...

Page 31: ...SECTION 2 LIMITATIONS PS POH 1 1 01 Date of issue 10 03 31 Revision 2 11 PEDAL SETTING PEDAL SETTING CANOPY OPENED CANOPY CLOSED BAGGAGE COMPARTMENT A BAGGAGE COMPARTMENT B NO STEP NO PUSH ...

Page 32: ...ion 2 12 If BRS rescue system is installed CAUTION The owner operator of this airplane is responsible for the readability of placards during the aircraft service life located on the both sides of fuselage between canopy and rear window located in place rocket egress ...

Page 33: ...ht 3 3 3 6 In flight engine starting 3 4 3 7 Emergency landing without engine power 3 4 3 8 Precautionary landing with engine power 3 4 3 9 Engine fire during start 3 5 3 10 Engine fire in flight 3 5 3 11 Electrical fire in flight 3 6 3 12 Generator failure 3 6 3 13 Inadvertent spin recovery 3 7 3 14 Inadvertent icing encounter 3 7 3 15 Obstruction of air into engine filter 3 8 3 16 Vibration 3 8 ...

Page 34: ...ed and applied as necessary to correct the problem CAUTION Airspeeds values are valid for standard AVIATIK WA037383 pitot static probe These emergency procedures are valid for WOODCOMP KLASSIC 170 3 R three composite blades ground adjustable propeller 3 2 Airspeeds for Emergency procedures Engine failure after takeoff 60 knot 70 mph flaps in T O or retracted position Maneuvering speed at 1 320 lb ...

Page 35: ...nding area choose free area without obstacles 5 Wind find direction and velocity 6 Flaps extend as necessary 7 Trim adjust 8 Safety harness tighten 9 Fuel Selector close 10 Ignition switch switch OFF 11 Master switch switch OFF before landing 12 Land 3 5 Loss of engine power in flight 1 Push control stick forward 2 Speed gliding at 60 knot 70 mph 3 Altitude in accordance with actual altitude searc...

Page 36: ...of engine failure and the engine cannot be re started 1 Speed adjust for optimum gliding 60 knot 70 mph 2 Trim adjust 3 COMM giving location and intentions if possible 4 Flaps extend as necessary 5 Fuel Selector close 6 Ignition switch switch OFF 7 Master switch switch OFF 8 Safety harness tighten 9 Perform approach without steep turns and land on chosen landing area 3 8 Precautionary landing with...

Page 37: ...OFF the fuel selector lock the airplane and seek assistance NOTE Watch the chosen area steadily during precautionary landing 3 9 Engine fire during start 1 Fuel Selector close 2 Throttle full power 3 Ignition switch switch OFF 4 Master switch OFF 5 Leave the airplane 6 Extinguish fire by fire extinguisher or call for a fire brigade if you cannot do it 3 10 Engine fire in flight 1 Heating close 2 F...

Page 38: ...ed and blinking bringing up the alarm bar at the bottom of the EMS screen with message triggering the external EMS warning light and audio alert Voltmeter on EMS screen indicates voltage under 12 5 V Ammeter on EMS screen permanently indicates negative current independently on engine RPM 1 Switch OFF all unnecessary electrical equipment 2 Switch ON Master Instruments and Avionics 3 Voltmeter monit...

Page 39: ...tent icing encounter CAUTION Aircraft is approved to operate in VMC condition only 1 Leave icing area turn back or change altitude to reach area with higher outside air temperature 2 Carburetor heating open 3 Cabin heating open 4 Increase RPM to minimize ice build up on propeller blades 5 Continue to move control surfaces to maintain their moveability 6 In case of icing on the leading edge of wing...

Page 40: ...ter can be clogged with some impurities e g dust or ice Perform 1 Carburetor heating open 2 Check engine running and monitor engine instruments 3 Land as soon as possible at nearest suitable airport If you fail to recover the engine power land on the nearest airfield if possible or depending on the circumstances perform a precautionary landing according to 3 8 3 16 Engine vibration If any forced a...

Page 41: ...the direction on the landing roll out applying rudder control 3 18 Landing with a defective landing gear 4 If the main landing gear is damaged perform touch down at the lowest practicable speed and if possible maintain direction during landing run 5 If the nose wheel is damaged perform touch down at the lowest practicable speed and hold the nose wheel above the ground by means of the elevator cont...

Page 42: ...OLD PRESSURE ALARM HIGH OIL PRESSURE ALARM LOW OIL PRESSURE ALARM HIGH OIL TEMPERATURE ALARM LOW OIL TEMPERATURE ALARM HIGH EGT 1 2 ALARM LOW EGT 1 2 ALARM HIGH CHT 1 2 ALARM LOW CHT 1 2 ALARM LOW L R FUEL TANK ALARM HIGH FUEL PRESSURE ALARM LOW FUEL PRESSURE ALARM HIGH VOLTAGE ALARM LOW VOLTAGE ALARM HIGH CURRENT ALARM LOW CURRENT ALARM ...

Page 43: ... 4 2 Engine starting 4 4 4 3 Taxiing 4 6 4 4 Normal takeoff 4 6 4 5 Climb 4 7 4 6 Best angle of climb speed Vx 4 7 4 7 Best rate of climb speed Vy 4 7 4 8 Cruise 4 7 4 9 Descend 4 7 4 10 Approach 4 8 4 11 Normal landing 4 8 4 12 Short field takeoff and landing procedures 4 9 4 13 Balked landing procedures 4 9 4 14 Airplane parking and tie down 4 10 ...

Page 44: ...ite blades ground adjustable propeller 4 1 Preflight check Carry out the pre flight inspection every day prior to the first flight or after airplane assembly Incomplete or careless inspection can cause an accident Carry out the inspection following the instructions in the Inspection Check List NOTE The word condition in the instructions means a visual inspection of surface for damage deformations ...

Page 45: ...ection of engine rotation several times to pump oil from the engine into the oil tank see the Rotax Operator s manual section 0 3 3 Coolant quantity check Visual inspection of the fuel and electrical system Fuel system draining Other actions according to the engine manual e Wing surface condition Leading edge condition Pitot head condition f Wing tip surface condition attachment Aileron surface co...

Page 46: ...e correct movement 2 Canopy clean closed and locked 3 Safety harness tighten 4 Brakes fully applied 4 2 2 Engine starting NOTE Start the engine according to procedure in Rotax Operator s manual 1 Throttle idle 2 Choke cold engine ON fully pulled and hold warm engine OFF 3 Fuel selector turn on left or right fuel tank in accordance with fuel tanks filling 4 Master switch switch ON 5 Fuel pump switc...

Page 47: ...ely 2 min then continue to 2 500 rpm till oil temperature reaches 122 F 50 C The warm up period depends on ambient air temperature Check both ignition circuits at 4 000 rpm for Rotax 912 ULS The engine speed drop during the time either magneto switched OFF should not exceed 300 rpm The max engine speed drop difference between circuits L and R should be 115 rpm NOTE Only one magneto should be switc...

Page 48: ...ation manually check by pushing the canopy upwards 5 Safety harness tighten 6 Fuel selector turn ON left or right fuel tank 7 Ignition switch switched ON both magnetos 8 Wing flaps extend as necessary 4 4 2 Takeoff 1 Brakes apply to stop wheel rotation 2 Takeoff power throttle fully forward max 5 800 rpm for max 5 min 3 Engine speed check rpm 4 Engine gauges within limits 5 Brakes release 6 Elevat...

Page 49: ... Vx 60 knot 70 mph Vy 65 knot 75 mph 3 Trim trim the airplane 4 Engine gauges oil temperature oil pressure and CHT within limits CAUTION If the cylinder head temperature or oil temperature and or coolant temperature approaches or exceeds limits reduce the climb angle to increase airspeed and possibly return within limits If readings do not improve troubleshoot causes other than high power setting ...

Page 50: ...becomes under cooled and a loss of power may occur Descent at increased idle approximately 3 000 rpm speed between 60 75 knot 70 86 mph and check that the engine instruments indicate values within permitted limits 4 11 Normal landing 4 11 1 Before landing 1 Throttle as necessary 2 Airspeed 60 knot 70 mph 3 Wing flaps extend as necessary 4 Trim as necessary 4 11 2 Landing 1 Throttle idle 2 Touch do...

Page 51: ...g and low engine rpm or at engine shutdown immediately after landing Under normal 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 idle rpm to stabilize the temperatures prior to engine shut down 4 12 Short field takeoff and landing procedures None 4 13 Balked landing procedures 1...

Page 52: ...ke if installed for short time parking 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 and fuselage rear section to fix the airplane Move control stick forward and fix it together with the rudder pedals Make sure that the cockpit canopy is properly ...

Page 53: ...ECTION 5 PERFORMANCE 5 1 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 5 5 6 Airspeed indicator system calibration 5 6 ...

Page 54: ...s If not stated otherwise the performance stated in this section is valid for maximum take off weight 600 kg 1 320 lb and under ISA conditions The performance shown in this section is valid for aircraft fitted with given ROTAX 912 ULS 98 6 hp 73 5 kW engine and WOODCOMP KLASSIC 170 3 R three composite blades ground adjustable propeller as delivered CAUTION Airspeeds values are valid for standard A...

Page 55: ...anding distances Conditions Altitude 0 ft ISA Engine power idle Flaps 30 Brakes fully depressed immediately after touch down Landing distance over 50 ft obstacle Landing run distance braked RUNWAY SURFACE ft ft CONCRETE 591 180 GRASS 558 197 5 3 Rate of climb Best rate of climb speed Rate of climb Vz Conditions Max continuous power 5 500 rpm Max takeoff weight 1 320 lb 600 kg knot mph fpm 0 ft 65 ...

Page 56: ...2 94 4800 92 106 90 104 5000 97 112 95 109 5300 106 122 103 118 5500 112 129 108 124 3000 5800 120 139 116 133 4200 72 83 72 83 4500 80 92 79 91 4800 88 101 86 99 5000 94 108 92 106 5300 102 117 99 114 5500 107 124 104 120 5000 5800 116 134 112 129 4200 69 79 70 80 4500 77 88 77 88 4800 84 97 83 96 5000 90 103 88 101 5300 97 112 95 109 5500 103 118 100 115 7000 5800 111 127 107 123 4200 65 75 66 7...

Page 57: ...ance hh mm 9 50 8 04 6 51 6 06 5 23 4 55 NM 766 686 637 599 570 545 Range SM 881 789 732 688 656 627 Endurance and Range at 23 77 US gal 90 liters Endurance hh mm 7 50 6 26 5 27 4 52 4 17 3 55 NM 610 546 507 477 454 434 Range SM 702 628 583 548 522 500 Endurance and Range at 15 85 US gal 60 liters Endurance hh mm 5 13 4 17 3 38 3 14 2 52 2 37 NM 407 364 338 318 303 290 Range SM 468 419 389 366 348...

Page 58: ...39 40 44 45 48 50 53 55 57 60 62 65 66 70 71 75 75 80 79 85 84 90 88 95 93 100 97 105 102 110 106 115 111 120 115 125 120 130 124 135 129 140 133 IAS CAS mph 35 41 40 45 45 49 50 54 55 58 60 63 65 67 70 72 75 76 80 81 85 85 90 89 95 94 100 98 105 103 110 107 115 112 120 116 125 121 130 125 135 130 140 134 145 139 150 143 155 148 160 152 ...

Page 59: ...N 6 TABLE OF CONTENTS 6 WEIGHT AND BALANCE 6 1 Introduction 6 2 6 2 Airplane weighing procedure 6 2 6 3 Weight and balance C G layout 6 3 6 4 Operating weights and loading 6 4 6 5 C G range and determination 6 4 6 6 Permitted payload range table 6 6 6 7 Installed equipment list 6 8 ...

Page 60: ...ft as well as further undesirable objects inflate tires to recommended operating pressure drain fuel from fuel installation add oil hydraulic and cooling liquid up to the maximum specified value retract wing flaps close the canopy and other lids and covers remove control surfaces blocking level the airplane according to the rivet line located on the fuselage on LH and RH sides under the canopy fra...

Page 61: ... measurement LN by measuring horizontally and parallel to the airplane center line from center of nose wheel axle left sides to a plumb bob dropped from the Rib No 4 Repeat on right side and average the measurements 5 Using weights from item 3 and measurements from item 4 the airplane weight and C G can be determined 6 Basic Empty Weight may be determined by completing appropriate table 6 3 Weight...

Page 62: ... equipment 760 lb 345 kg NOTE Actual Empty weight is shown in Section 9 Supplement No 02 Number of seats 2 Minimum crew 1 pilot on the left seat Minimum crew weight 95 lb 43 kg Maximum crew weight on each seat 253 lb 115 kg 6 5 C G range and determination Aircraft C G range Operating C G range 27 to 38 of MAC 15 94 to 22 44 in 405 to 570 mm of MAC Empty weight C G range 28 to 32 of MAC 16 54 to 18...

Page 63: ...TY AIRCRAFT PILOT 27 56 700 PASSENGER 27 56 700 BAGGAGE COMPARTMENT A 51 58 1 310 BAGGAGE COMPARTMENT B 70 87 1 800 WING LOCKERS 23 62 600 FUEL TANKS 7 09 180 TOTAL WT lb kg MT TAKEOFF WEIGHT lb kg C G in mm MAC NOTE EMPTY WEIGHT INCLUDING OIL COOLANT AND HYDRAULIC FLUID MAXIMUM FUEL QUANTITY IN WING TANKS 180 62LB 30 1US GAL 82 1KG 114L IS USED FOR MOST FORWARD C G CALCULATION MINIMUM FUEL QUANTI...

Page 64: ...to 32 of MAC Operating C G range 15 94 to 22 4 4 in 405 to 570 mm 27 to 38 of MAC Maximum useful weight W Max Useful W Max TakeOff WE W Max Useful 1 320 lb 600 kg lb kg This useful weight must be never exceeded NOTE MAXIMUM USEFUL WEIGHT INCLUDING PILOT PASSENGER BAGGAGE AND FUEL MT ME 100 Aircraft C G in mm x WT WE MAC 6 6 Permitted payload range table NOTE Actual Permitted payload range table is...

Page 65: ... 5 41 61 6 82 1 Permitted crew weight lb No baggage kg lb rear A 20 lb 9 kg kg lb rear A 40 lb 18 kg kg lb wing lockers 44 lb 20 kg kg lb rear A wing lockers 64 lb 29 kg kg lb rear A wing lockers 84 lb 38 kg kg lb wing lockers 88 lb 40 kg kg lb rear A wing lockers 108 lb 49 kg kg lb B A G G A G E rear A wing lockers 128 lb 58 kg kg Crew weight Max TakeOff weight Empty weight Baggage weight Fuel we...

Page 66: ...SECTION 6 WEIGHT BALANCE PS POH 1 1 01 Date of issue 10 03 31 Revision 6 8 6 7 Installed equipment list NOTE Actual Installed equipment list is shown in Section 9 Supplement No 02 ...

Page 67: ...DESCRIPTION OF AIRPLANE AND SYSTEMS 7 1 General 7 2 7 2 Airframe 7 2 7 3 Flight controls 7 2 7 4 Instrument panel 7 3 7 5 Engine 7 3 7 6 Propeller 7 4 7 7 Landing gear 7 5 7 8 Baggage compartment 7 5 7 9 Seats and safety harnesses 7 5 7 10 Canopy 7 6 7 11 Fuel system 7 6 7 12 Electrical system 7 7 7 13 Pitot static system 7 7 ...

Page 68: ...metal riveted to aluminum angles with Avex rivets This high strength aluminum alloy construction provides long life and low maintenance costs thanks to its durability and corrosion resistance characteristics The wing has a high lift airfoil equipped with flaps 7 3 Flight controls The plane is equipped with a dual stick control the adjustable rudder pedals with pedal hydraulic brakes for easy groun...

Page 69: ...OHV Liquid cooled cylinder heads ram 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 reduction gear with integrated shock absorber For information about engine performance speeds and limits see Section 2 chapter 2 12 Engine operating speeds and limits in...

Page 70: ...dependent of the power source and will operate even with Master switch and or breaker OFF Engine instruments EMS screen displays all Engine Instruments as follows engine speed manifold pressure oil pressure and temperature exhaust gas temperature cylinder head temperature fuel pressure and flow For information about engine instruments range and markings see Section 2 chapter 2 13 Engine instrument...

Page 71: ... of the baggage compartment further from seats Baggage compartment is fitted with four tie down straps for baggage fixation Load heavy items in compartment A and lighter items in compartment B Baggage may also be loaded into the baggage compartment inside each wing up to 44 lb 20 kg in each wing locker Make sure that baggage does not exceed maximum allowable weight and that the aircraft C G is wit...

Page 72: ...al console in the cockpit The electric fuel pump is located on bulkhead and it is used for fuel line filling before engine starting Fuel return hose goes from the fuel pump into the left tank CAUTION During operation fuel valve shall be in LEFT or RIGHT tank position position on green mark Left green mark Right green mark NOTE If left tank is full start engine with the fuel selector set to LEFT If...

Page 73: ...n the front side of forward bulkhead Master switch Master switch connects the electrical system to the 12 V battery 7 13 Pitot static system Standard AVIATIK WA037383 pitot static probe is located below the left wing Pressure distribution to the instruments is through flexible plastic hoses Keep the pitot head clean to ensure proper function of the system ...

Page 74: ...SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS PS POH 1 1 01 Date of issue 10 03 31 Revision 7 8 Intentionally left blank ...

Page 75: ...ONTENTS 8 HANDLING AND SERVICING 8 1 Introduction 8 2 8 2 Ground handling 8 2 8 3 Towing instructions 8 3 8 4 Tie down instructions 8 3 8 5 Servicing operating fluids 8 3 8 6 Cleaning and care 8 5 8 7 Assembly and disassembly 8 6 8 8 Aircraft inspection periods 8 6 8 9 Aircraft alterations or repairs 8 6 ...

Page 76: ...ly the whole airplane by means of a suitable tarpaulin 8 2 2 Jacking Since the empty weight of this aircraft is relatively low two people can lift the aircraft easily First of all prepare two suitable supports to support the aircraft It is possible to lift the aircraft by handling the following parts By pushing the fuselage rear section down in the place of a bulkhead the fuselage front section ma...

Page 77: ... this reason the aircraft is equipped with mooring eyes located on the lower surfaces of the wings Tie down procedures 1 Fuel Selector close Master switch and other switches switched OFF Ignition switch switched OFF 2 Fix the hand control using e g safety harness 3 Close air vent 4 Close and lock canopy 5 Moor the aircraft to the ground by means of a mooring rope passed through the mooring eyes lo...

Page 78: ...n chamber and lead sediments in the oil system Thus it should only be used in case of problems with vapor lock or when other types of gasoline are unavailable Fuel volume Wing fuel tanks volume 2x15 06 US gal 2x57 liter Unusable fuel quantity 2x0 13 US gal 2x0 5 liter 8 5 2 Approved oil grades and specifications Recommended oil type refer to the Rotax Operator s manual section 10 2 3 Lubricants Ro...

Page 79: ...the cooling system and engine Type of coolant used by aircrafts manufacturer see Section 9 Supplement No 02 Coolant liquid volume It is approximately 0 66 US gal 2 5 liter 8 6 Cleaning and care Use efficient cleaning detergents to clean the aircraft surface Oil spots on the aircraft surface except the canopy may be cleaned with petrol The canopy may only be cleaned by washing it with a sufficient ...

Page 80: ... every 100 flight hours or at least annual inspection Refer to the PiperSport aircraft Maintenance manual for aircraft maintenance Refer to the Rotax engine Maintenance manual for engine maintenance Maintain the propeller according to its manual All repairs and maintenance should be made in accordance with AC 43 13 1B 8 9 Aircraft alterations or repairs It is recommended to contact the airplane ma...

Page 81: ...PS POH 1 1 01 SECTION 9 SUPPLEMENTS Revision Date of issue 10 03 31 9 1 SECTION 9 TABLE OF CONTENTS 9 SUPPLEMENTS 9 1 List of inserted supplements 9 2 9 2 Inserted supplements 9 2 ...

Page 82: ...safely and efficiently operate the aircraft when equipped with various optional systems and equipment not provided with the standard airplane 9 1 List of inserted supplements Date Suppl No Title of inserted supplement Revision No 10 03 31 01 Aircraft Flight Training Supplement 10 03 31 02 Aircraft specification S N P1001001 9 2 Inserted Supplements ...

Page 83: ... the Flight Instructor if student pilot is ready to continue on in next training step Training can be performed by Flight Instructor or by the experienced pilot who has minimum 20 hours on the PiperSport Type Rating Training Procedure Ground Training Before practical Flight Training the pilot has to get familiar with following procedures and documentation Pilot s Operating Handbook POH Aircraft Ma...

Page 84: ...airplane in local flight instructor giving advice as necessary 2 Pattern training flights up to 1 000 feet AGL High pattern procedures instructor giving advice as necessary 3 Pattern training flights up to 500 feet AGL High pattern procedures instructor giving advice as necessary 4 Stall speed 45 turns sideslips Stall speed flaps retracted and extended landing configuration sideslips at landing co...

Page 85: ...s Supplement must be contained in the Pilot s Operating Handbook during operation of the airplane Information contained in this Supplement adds to or replaces information from the basic Pilot s Operating Handbook in the parts mentioned only Limitations procedures and information not mentioned in this Supplement are contained in the basic Pilot s Operating Handbook This Supplement adds information ...

Page 86: ...weight 1 320 lb Maximum useful weight W Max Useful W Max TakeOff WE W Max Useful 1 320 lb 853 6 lb 466 4 lb This useful weight must be never exceeded NOTE MAXIMUM USEFUL WEIGHT INCLUDING PILOT PASSENGER BAGGAGE AND FUEL MT ME 100 Aircraft C G in x WT WE MAC 2010 03 02 ITEM WEIGHT lb ARM in MOMENT WEIGHT x ARM RIGHT MAIN WHEEL WR 325 38 LR 31 42 10 223 44 LEFT MAIN WHEEL WL 322 96 LL 30 91 9 982 69...

Page 87: ... 0 0 51 58 0 0 BAGGAGE COMPARTMENT B 0 0 70 87 0 0 WING LOCKERS 0 0 23 62 0 0 FUEL TANKS 180 62 7 09 1 280 60 TOTAL WT 1 122 22 lb MT 18 166 78 TAKEOFF WEIGHT 1 122 22 lb C G 16 19 in 27 4 MAC NOTE MAXIMUM FUEL QUANTITY IN WING TANKS 180 62LB 30 1US GAL IS USED FOR MOST FORWARD C G CALCULATION Max TakeOff weight 1 320 lb Max weight in baggage compartment A B 40 lb Max weight in wing lockers togeth...

Page 88: ...NG LOCKERS 24 42 23 62 576 80 FUEL TANKS 0 0 7 09 0 0 TOTAL WT 1 297 78 lb MT 27 684 80 TAKEOFF WEIGHT 1 297 78 lb CG 21 33 in 36 1 MAC NOTE MINIMUM FUEL QUANTITY IN WING TANKS FOR 30MINUTE FLIGHT 22 2LB 3 7US GAL IS SUBTRACTED FROM MTOW 1 320LB MOST REARWARD C G CALCULATION IS DONE WITH ZERO FUEL QUANTITY AFTER FUEL DEPLETION Max TakeOff weight 1 320 lb Max weight in baggage compartment A B 40 lb...

Page 89: ...rear A 40 lb 18 kg kg 184 173 153 132 112 lb 400 377 332 287 242 wing lockers 44 lb 20 kg kg 182 172 151 130 110 lb 380 357 312 267 222 rear A wing lockers 64 lb 29 kg kg 173 162 142 121 101 lb 360 337 292 247 202 rear A wing lockers 84 lb 38 kg kg 164 153 133 112 92 lb 356 333 288 243 198 wing lockers 88 lb 40 kg kg 162 152 131 110 90 lb 336 313 268 223 178 rear A wing lockers 108 lb 49 kg kg 153...

Page 90: ...g PM3000 intercom Garmin GTX328 transponder King AK451 ELT AirGizmos Garmin 495 GPS Dynon HS34 HSI expansion module Dynon AP74 autopilot control unit Electric autopilot servos Antennas G 205 trim control and PTT on the control sticks Trims and flaps electrically actuated Kuntzleman wing tips strobe nav lights Landing light in cowl Adjustable pedals Dual hydraulic brakes Parking brake Wheel fairing...

Page 91: ...evision Date of issue 10 03 31 7 of 14 7 DESCRIPTION OF AIRPLANE AND SYSTEMS 7 4 Instrument panel Instrument panel layout of PiperSport aircraft S N P1001001 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 15 ...

Page 92: ... HS34 HSI expansion module 20 Flaps control switch 6 Backup Airspeed indicator 21 Flaps position indicator 7 Transceiver 22 Throttle 8 Garmin GPS 23 Choke 9 Compass 24 Fuel selector valve 10 Transponder 25 Socket 12V 11 Dynon AP74 autopilot control unit 26 Carburetor preheating 12 Dynon EMS 27 Cabin heating 13 ELT control unit and buzzer 28 BRS release handle 14 Circuit breakers 29 PS Intercom 15 ...

Page 93: ... module Dynon AP74 autopilot control unit Electric autopilot servos Antennas NOTE For instrument and avionics operating instructions refer to the documentation supplied with the instruments and avionics Miscellaneous equipment G 205 trim control and PTT on the control sticks Trims and flaps electrically actuated Kuntzleman wing tip strobe nav lights Landing light in cowl Adjustable pedals Dual hyd...

Page 94: ...it breaker LDG L landing light circuit breaker FUEL P fuel pump circuit breaker 8 HANDLING AND SERVICING 8 5 Servicing operating fluids 8 5 2 Approved oil grades and specifications Type of oil used by aircrafts manufacturer AeroShell Oil Sport Plus 4 SAE 10W 40 API SL 8 5 3 Approved coolant grades and specifications Type of coolant used by aircrafts manufacturer Specification ASTM D 3306 VW TL 774...

Page 95: ...SECTION 9 SUPPLEMENTS PS POH 1 1 01 Revision Date of issue 10 03 31 11 of 14 Intentionally left blank ...

Page 96: ...C G COMPUTED C G EMPTY Empty weight WE lb kg C G in mm MAC Aircraft moment ME NOTE EMPTY WEIGHT INCLUDING OIL COOLANT AND HYDRAULIC FLUID MAXIMUM FUEL QUANTITY IN WING TANKS 180 62LB 30 1US GAL 82 1KG 114L IS USED FOR MOST FORWARD C G CALCULATION MINIMUM FUEL QUANTITY IN WING TANKS FOR 30 MINUTE FLIGHT 22 2LB 3 7US GAL 10 1KG 14L IS SUBTRACTED FROM MTOW 1 320LB 600KG MOST REARWARD C G CALCULATION ...

Page 97: ...mm MAC Max TakeOff weight 1 320 lb 600 kg Max weight in baggage compartment A B 40 lb 18 kg Max weight in wing lockers together 88 lb 40 kg Empty weight C G range 16 54 to 18 90 in 420 to 480 mm 28 to 32 of MAC Operating C G range 15 94 to 22 4 4 in 405 to 570 mm 27 to 38 of MAC Maximum useful weight W Max Useful W Max TakeOff WE W Max Useful 1 320 lb 600 kg lb kg This useful weight must be never ...

Page 98: ...5 41 61 6 82 1 Permitted crew weight lb No baggage kg lb rear A 20 lb 9 kg kg lb rear A 40 lb 18 kg kg lb wing lockers 44 lb 20 kg kg lb rear A wing lockers 64 lb 29 kg kg lb rear A wing lockers 84 lb 38 kg kg lb wing lockers 88 lb 40 kg kg lb rear A wing lockers 108 lb 49 kg kg lb B A G G A G E rear A wing lockers 128 lb 58 kg kg Crew weight Max TakeOff weight Empty weight Baggage weight Fuel wei...

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