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czech sport aircraft Piper Sport Pilot Operating Handbook

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Pilot's Operating Handbook
Airplane Registration Number:
Airplane Serial Number:
POH Copy Number:
Date of issue: 10/03/31
PS-POH-1-1-01
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Revision: -

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Summary of Contents for czech sport aircraft Piper Sport

  • Page 1 PS-POH-1-1-01 Pilot’s Operating Handbook Airplane Registration Number: Airplane Serial Number: P1001001 POH Copy Number: Date of issue: 10/03/31 Revision: -...
  • Page 2 PS-POH-1-1-01 Intentionally left blank Date of issue: 10/03/31 Revision: -...
  • Page 3 PS-POH-1-1-01 Pilot’s Operating Handbook 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.) Date of issue: 10/03/31 Revision: -...
  • Page 4 PS-POH-1-1-01 Intentionally left blank Date of issue: 10/03/31 Revision: -...
  • Page 5 RECORD OF REVISIONS PS-POH-1-1-01 RECORD OF REVISIONS Affected pages Revision name Date of Issue Signature Date of issue: 10/03/31 Revision: -...
  • Page 6 PS-POH-1-1-01 Intentionally left blank Date of issue: 10/03/31 Revision: -...
  • Page 7 LIST OF EFFECTIVE PAGES PS-POH-1-1-01 LIST OF EFFECTIVE PAGES Section Page Revision No. Section Page Revision No. 3-10 2-10 2-11 2-12 4-10 Date of issue: 10/03/31 Revision: -...
  • Page 8 PS-POH-1-1-01 LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES (Cont’d) Section Page Revision No. Section Page Revision No. Date of issue: 10/03/31 viii Revision: -...
  • Page 9 LIST OF ABBREVIATIONS PS-POH-1-1-01 LIST OF ABBREVIATIONS Attitude direction indicator Altitude or Altimeter Air Traffic Control Airspeed Indicator Pressure unit (1 bar = 14.5037 psi) BEACON Anti-collision beacon °C Temperature in degree of Celsius (1°C = (°F - 32) / 1.8) Calibrated Airspeed Course deviation indicator Cylinder head temperature...
  • Page 10 PS-POH-1-1-01 LIST OF ABBREVIATIONS Newton - force unit (1 N = 0.225 lbf) Nautical mile (1 NM = 1,852 m) System is switched off or control element is in off-position System is switched on or control element is in on-position Outside Air Temperature Pilot Operating Handbook Pressure unit - pound per square inch...
  • Page 11 ASTM STANDARDS PS-POH-1-1-01 ASTM STANDARDS The PiperSport aircraft is designed and built according to following ASTM LSA standards: ASTM F 2245 – 09 Standard Specification for Design and performance 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 –...

  • Page 12: Contact Information

    PS-POH-1-1-01 CONTACT INFORMATION CONTACT INFORMATION 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 TABLE OF CONTENTS PS-POH-1-1-01 TABLE OF CONTENTS General Information Limitations Emergency Procedures Normal Procedures Performance Weight and Balance Description of Airplane and Systems Handling and Servicing Supplements Date of issue: 10/03/31 xiii Revision: -...
  • Page 14 PS-POH-1-1-01 Intentionally left blank Date of issue: 10/03/31 Revision: -...
  • Page 15 SECTION 1 PS-POH-1-1-01 GENERAL INFORMATION SECTION 1 TABLE OF CONTENTS 1. GENERAL INFORMATION Airplane specification Summary of performances Date of issue: 10/03/31 Revision: -...

  • Page 16: General Information

    SECTION 1 PS-POH-1-1-01 GENERAL INFORMATION 1. GENERAL INFORMATION This Pilot Operating Handbook has been prepared to provide pilots with information for the safe and efficient operation of the PiperSport aircraft and contains 9 sections. It also contains supplementary information considered to be important by the aircraft manufacturer.
  • Page 17 SECTION 1 PS-POH-1-1-01 GENERAL INFORMATION Aircraft layout: Date of issue: 10/03/31 Revision: -...
  • Page 18 SECTION 1 PS-POH-1-1-01 GENERAL INFORMATION Main airplane dimensions: Wing span............28.90 [ft] (8.81 [m]) Length............21.33 [ft] (6.50 [m]) Height ............7.78 [ft] (2.37 [m]) Wing area ............132.3 [sq ft] (12.3 [m Wing loading..........10 [lb/sq ft] (49 [kg/m Cockpit width ..........46 [in] (1.17 [m]) Flight control surfaces travel: Rudder............30°...
  • Page 19 SECTION 1 PS-POH-1-1-01 GENERAL INFORMATION 1.2 Summary of performances Weights: Max. takeoff and landing weight ....1,320 [lb] (600 [kg]) Max. weight of fuel.........180 [lb] (82 [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])
  • Page 20 SECTION 1 PS-POH-1-1-01 GENERAL INFORMATION Rate of climb: At sea level ............1,200 fpm Best angle of climb speed (v ) .......60 [knot] (70 [mph]) Best rate of climb speed (v ):......65 [knot] (75 [mph]) Stall speeds: – flaps down, power - idle......32 [knot] (37[mph]) –...

  • Page 21: Table Of Contents

    SECTION 2 PS-POH-1-1-01 LIMITATIONS SECTION 2 TABLE OF CONTENTS 2. LIMITATIONS Airspeed indicator range markings Stalling speeds at maximum takeoff weight Flap extended speed range Maneuvering speed Maximum structural cruising speed Never exceed speed Service ceiling Load factors Approved maneuvers 2.10 Operating weights and loading 2.11 Fuel 2.12 Engine operating speeds and limits...

  • Page 22: Limitations

    SECTION 2 PS-POH-1-1-01 LIMITATIONS 2. LIMITATIONS CAUTION Airspeeds values are valid for standard AVIATIK WA037383 pitot-static probe. 2.1 Airspeed indicator range markings NOTE The stated stall speeds are valid for all flight altitudes. IAS value or range Significance Marking knot White 32-75 37-86...

  • Page 23: Flap Extended Speed Range

    SECTION 2 PS-POH-1-1-01 LIMITATIONS 2.3 Flap extended speed range - V to V Flap operating range (IAS): 32 - 75 [knot] (37 - 86 [mph]) 2.4 Maneuvering speed - V Maneuvering speed (IAS) at 1,320 [lb]: 88 [knot] (101 [mph]) Maneuvering speed (IAS) at 900 [lb]: 70 [knot] (80 [mph]) 2.5 Maximum structural cruising speed –...

  • Page 24: Operating Weights And Loading

    SECTION 2 PS-POH-1-1-01 LIMITATIONS 2.10 Operating weights and loading Max. takeoff weight..........1,320 [lb] (600 [kg]) Max landing weight ..........1,320 [lb] (600 [kg]) Max. weight of fuel..........180 [lb] (82 [kg]) Max. baggage weight in rear fuselage ....40 [lb] (18 [kg]) Max.

  • Page 25: Fuel

    SECTION 2 PS-POH-1-1-01 LIMITATIONS 2.11 Fuel Fuel volume: Wing fuel tanks capacity ........2x15.06 [US gal] (2x57 [liter]) Total fuel capacity..........30.12 [US gal] (114 [liter]) Unusable fuel..........2x0.13 [US gal] (2x0.5 [liter]) Total usable fuel ..........29.86 [US gal] (113 [liter]) Recommended fuel type: (Refer to the ROTAX Operator’s manual section 10.2.2 Fuel, Rotax Service Instruction SI-912-016) MOGAS...

  • Page 26: Engine Operating Speeds And Limits

    SECTION 2 PS-POH-1-1-01 LIMITATIONS 2.12 Engine operating speeds and limits Engine Model: ROTAX 912 ULS Engine Manufacturer: Bombardier-Rotax GMBH Max. Takeoff: 98.6 hp (73.5 kW) at 5,800 rpm (max. 5 min.) Max. Continuous: 92.5 hp (69 kW) at 5,500 rpm Cruising (75%): 68.4 hp (51 kW) at 5,000 rpm Max.

  • Page 27: Engine Instruments Markings

    SECTION 2 PS-POH-1-1-01 LIMITATIONS 2.13 Engine instruments markings Normal Rotax 912ULS Minimum Caution Caution Maximum Operating 73.5 [kW] Limit Range Range Range Range (98.6 [hp]) (red line) (yellow arc) (yellow arc) (red line) (green arc) Engine speed 0-1,400 5,500-5,800 5,800 1,400-5,500 [RPM] 12 psi...
  • Page 28 SECTION 2 PS-POH-1-1-01 LIMITATIONS • Minimum instruments and equipment list for Day VFR flights: • Airspeed indicator • Altimeter • Compass (is not required by ASTM F 2245) • Fuel quantity indicator • Tachometer (RPM) • Engine instruments as required by the engine manufacturer : Oil temperature indicator Oil pressure indicator Cylinder head temperature indicator...

  • Page 29: Limitation Placards And Markings

    SECTION 2 PS-POH-1-1-01 LIMITATIONS 2.15 Limitation placards and markings Operating limitation on instrument panel AIRSPEEDS: 138 kts 88 kts 75 kts 32 kts WARNING ! DO NOT EXCEED MAXIMUM TAKE-OFF WEIGHT: 600kg/1320lbs WARNING ! IFR FLIGHTS AND INTENTIONAL FLIGHTS UNDER ICING CONDITIONS ARE PROHIBITED Operating limitation in baggage space MAX.

  • Page 30: Miscellaneous Placards And Markings

    SECTION 2 PS-POH-1-1-01 LIMITATIONS 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      C   O       L    P      O    E       S    N      E   ...
  • Page 31 SECTION 2 PS-POH-1-1-01 LIMITATIONS PEDAL SETTING PEDAL SETTING CANOPY OPENED CANOPY CLOSED BAGGAGE COMPARTMENT - A BAGGAGE COMPARTMENT - B NO STEP NO PUSH Date of issue: 10/03/31 Revision: - 2-11...
  • Page 32 SECTION 2 PS-POH-1-1-01 LIMITATIONS If BRS rescue system is installed: - located on the both sides of fuselage between canopy and rear window - located in place rocket egress CAUTION The owner (operator) of this airplane is responsible for the readability of placards during the aircraft service life.
  • Page 33 SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES SECTION 3 TABLE OF CONTENTS 3. EMERGENCY PROCEDURES General information Airspeeds for Emergency procedures Engine failure during takeoff run Engine failure after takeoff Loss of engine power in flight In-flight engine starting Emergency landing without engine power Precautionary landing with engine power Engine fire during start 3.10 Engine fire in flight...

  • Page 34: Emergency Procedures

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES 3. EMERGENCY PROCEDURES 3.1 General information This section provides checklists and amplified procedures for coping with various emergencies that may occur. Emergencies caused by aircraft or engine malfunction are extremely rare if proper pre-flight inspections and maintenance are practiced.

  • Page 35: Engine Failure During Takeoff Run

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES 3.3 Engine failure during takeoff run 1. Throttle - idle 2. Ignition switch - switch OFF Brakes - apply 3.4 Engine failure after takeoff 1. Push control stick forward 2. Speed - gliding at 60 [knot] (70 [mph]) 3.

  • Page 36: In-Flight Engine Starting

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES 3.6 In-flight engine starting 1. Switches - switch OFF unnecessary electrical equipment 2. Master switch - switch ON 3. Fuel Selector - turn on (to tank with more quantity of fuel) 4. Throttle - idle 5.

  • Page 37: Engine Fire During Start

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES 3. Perform low-altitude passage into wind over the right-hand side of the chosen area with flaps extended as needed and thoroughly inspect the landing area. 4. Perform circle pattern. 5. Perform approach at increased idling with flaps fully extended at 60 [knot] (70 [mph]) 6.

  • Page 38: Electrical Fire In Flight

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES NOTE Estimated time to pump fuel out of carburetors is about 30 [sec]. WARNING Do not attempt to re-start the engine! 3.11 Electrical fire in flight 1. Master switch - switch OFF 2. Other switches - switch OFF 3.

  • Page 39: Inadvertent Spin Recovery

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES 3.13 Inadvertent spin recovery There is no uncontrollable tendency of the airplane to enter into a spin provided the normal piloting techniques are used. Inadvertent spin recovery technique: 1. Throttle - idle 2. Lateral control - ailerons neutralized 3.

  • Page 40: Obstruction Of Air Into Engine Filter

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES NOTE The carburetor icing and air filter icing shows itself through a decrease in engine power and an increase of engine temperatures. NOTE Use carburetor heating during lengthy descents and in areas of possible carburetor icing.

  • Page 41: Landing With A Flat Tire

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES 3.17 Landing with a flat tire 1. During landing keep the damaged wheel above ground as long as possible using the ailerons control 2. Maintain the direction on the landing roll out, applying rudder control. 3.18 Landing with a defective landing gear 4.

  • Page 42: List Of Ems Alert Alarms

    SECTION 3 PS-POH-1-1-01 EMERGENCY PROCEDURES 3.19 List of EMS alert alarms HIGH RPM ALARM HIGH MANIFOLD 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...
  • Page 43 SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES SECTION 4 TABLE OF CONTENTS 4. NORMAL PROCEDURES Preflight check Engine starting Taxiing Normal takeoff Climb Best angle of climb speed (V Best rate of climb speed (V Cruise Descend 4.10 Approach 4.11 Normal landing 4.12 Short field takeoff and landing procedures 4.13 Balked landing procedures 4.14 Airplane parking and tie-down...

  • Page 44: Normal Procedures

    SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES 4. NORMAL PROCEDURES This section provides checklists and recommended procedures for normal operation of the aircraft. CAUTION Airspeeds values are valid for standard AVIATIK WA037383 pitot-static probe. These emergency procedures are valid for standard WOODCOMP KLASSIC 170/3/R three composite blades ground adjustable propeller.
  • Page 45 SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES Inspection Check List − Ignition - OFF − Master switch - ON − Instruments switch - ON, check fuel quantity on indicators − Avionics - check condition − Control system - visual inspection, function, clearance, free movement up to stops - check wing flaps operation - check trims operation...

  • Page 46: Engine Starting

    SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES WARNING Physically check the fuel level before each takeoff to make sure you have sufficient fuel for the planned flight. WARNING In case of long-term parking it is recommended to turn the engine several times (Ignition OFF!) by turning the propeller.
  • Page 47 SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES CAUTION • The starter should be activated for a maximum of 10 [sec], followed by 2 [min] pause for starter cooling. • As soon as engine runs, adjust throttle to achieve smooth running at approx. 2,500 [rpm]. Check the oil pressure, which should increase within 10 [sec].

  • Page 48: Taxiing

    SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES 4.3 Taxiing Apply power and brakes as needed. Apply brakes to control movement on ground. Taxi carefully when wind velocity exceeds 20 [knot]. Hold the control stick in neutral position. 4.4 Normal Takeoff 4.4.1 Before takeoff 1.

  • Page 49: Climb

    SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES WARNING Takeoff is prohibited if: • Engine is running unsteadily • Engine instrument values are beyond operational limi • Aircraft systems (e.g. brakes or controls) work incorrectly • Crosswind velocity exceeds permitted limits (see section 3.6) 4.5 Climb 1.

  • Page 50: Approach

    SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES 4.10 Approach 1. Approach speed - 60 [knot] (70 [mph]) 2. Throttle - as necessary 3. Wing flaps - extend as necessary 4. Trim - as necessary 5. Safety harness - tighten CAUTION It is not advisable to reduce the engine throttle control lever to minimum on final approach and when descending from very high altitude.

  • Page 51: Short Field Takeoff And Landing Procedures

    SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES 4.11.4 Engine shut down 1. Throttle - idle 2. Instruments - engine instruments within limits 3. Switches - switch OFF - except Instrument and Master 4. Ignition switch - turn key to switch OFF 5. Instrument switch - switch OFF 6.
  • Page 52 SECTION 4 PS-POH-1-1-01 NORMAL PROCEDURES 4.14 Aircraft parking and tie-down 1. Ignition switch - OFF 2. Master switch - OFF 3. Fuel selector - close 4. Parking brake - use it as necessary (if installed) 5. Canopy - close, lock as necessary 6.
  • Page 53 SECTION 5 PS-POH-1-1-01 PERFORMANCE SECTION 5 TABLE OF CONTENTS 5. PERFORMANCE Takeoff distances Landing distances Rate of climb Cruise speeds RPM setting and fuel consumption Airspeed indicator system calibration Date of issue: 10/03/31 Revision: -...

  • Page 54: Performance

    SECTION 5 PS-POH-1-1-01 PERFORMANCE 5. PERFORMANCE The presented data has been computed from actual flight tests with the aircraft and engine in good conditions and using average piloting techniques. If not stated otherwise, the performance stated in this section is valid for maximum take-off weight ( ) and under ISA conditions.

  • Page 55: Takeoff Distances

    SECTION 5 PS-POH-1-1-01 PERFORMANCE 5.1 Takeoff distances Conditions: - Altitude: 0 ft ISA - Engine power: max. takeoff - Flaps: 15° Takeoff distance over Takeoff run distance RUNWAY 50 ft obstacle SURFACE CONCRETE GRASS 5.2 Landing distances Conditions: - Altitude: 0 ft ISA - Engine power: idle - Flaps: 30°...

  • Page 56: Cruise Speeds

    SECTION 5 PS-POH-1-1-01 PERFORMANCE 5.4 Cruise speeds Engine Altitude speed knot knot 4200 4500 4800 1000 5000 5300 5500 5800 4200 4500 4800 3000 5000 5300 5500 5800 4200 4500 4800 5000 5000 5300 5500 5800 4200 4500 4800 7000 5000 5300 5500...

  • Page 57: Rpm Setting And Fuel Consumption

    SECTION 5 PS-POH-1-1-01 PERFORMANCE 5.5 RPM setting and fuel consumption Altitude 3,000 Engine speed 4,200 4,500 4,800 5,000 5,300 5,500 Fuel 11.5 14.0 16.5 18.5 21.0 23.0 consumption US gal/h 3.04 3.70 4.36 4.89 5.55 6.08 knot knot knot Endurance and Range at 29.85 US gal (113 liters) Endurance hh:mm 9:50...

  • Page 58: Airspeed Indicator System Calibration

    SECTION 5 PS-POH-1-1-01 PERFORMANCE 5.6 Airspeed indicator system calibration knot Date of issue: 10/03/31 Revision: -...
  • Page 59 SECTION 6 PS-POH-1-1-01 WEIGHT & BALANCE SECTION 6 TABLE OF CONTENTS 6. WEIGHT AND BALANCE Introduction Airplane weighing procedure Weight and balance C.G. layout Operating weights and loading C.G. range and determination Permitted payload range table Installed equipment list Date of issue: 10/03/31 Revision: -...

  • Page 60: Weight And Balance

    SECTION 6 PS-POH-1-1-01 WEIGHT & BALANCE 6. WEIGHT AND BALANCE 6.1 Introduction This section contains weight and balance records and the payload range for safe operation of PiperSport aircraft. Procedures for weighing the aircraft and the calculation method for establishing the permitted payload range are contained in FAA Aviation Advisory Circular AC.43.13 –...

  • Page 61: Weight And Balance C.g. Layout

    SECTION 6 PS-POH-1-1-01 WEIGHT & BALANCE 4. Measuring - Obtain measurement LR and LL by measuring horizontally (along the airplane center line) from a line stretched between the Rib No. 4. - Obtain 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.

  • Page 62: Operating Weights And Loading

    SECTION 6 PS-POH-1-1-01 WEIGHT & BALANCE 6.4 Operating weights and loading Max. takeoff weight..........1,320 [lb] (600 [kg]) Max. landing weight ..........1,320 [lb] (600 [kg]) Max. weight of fuel..........180 [lb] (82 [kg]) Max. baggage weight in rear fuselage ....40 [lb] (18 [kg]) Max.
  • Page 63 SECTION 6 PS-POH-1-1-01 WEIGHT & BALANCE Blank form of Weight & Balance record WEIGHT MOMENT ITEM [lb/kg] [in/mm] (WEIGHT x ARM) RIGHT MAIN WHEEL LEFT MAIN WHEEL NOSE WHEEL negative arm Empty weight: Aircraft moment: C.G.= [in/mm] COMPUTED C.G. EMPTY [lb/kg] [%]MAC WEIGHT...

  • Page 64: Permitted Payload Range Table

    SECTION 6 PS-POH-1-1-01 WEIGHT & BALANCE 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.
  • Page 65 SECTION 6 PS-POH-1-1-01 WEIGHT & BALANCE Blank form of Permitted payload range table PiperSport Serial number : for 30 gauges together 1 / 4 1 / 2 3 / 4 min flight 15.1 22.6 30.1 US gal volume liter 28.5 85.5 22.2 45.1...

  • Page 66: Installed Equipment List

    SECTION 6 PS-POH-1-1-01 WEIGHT & BALANCE 6.7 Installed equipment list NOTE Actual Installed equipment list is shown in Section 9, Supplement No. 02. Date of issue: 10/03/31 Revision: -...
  • Page 67 PS-POH-1-1-01 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS SECTION 7 TABLE OF CONTENTS 7. DESCRIPTION OF AIRPLANE AND SYSTEMS General Airframe Flight controls Instrument panel Engine Propeller Landing gear Baggage compartment Seats and safety harnesses 7.10 Canopy 7.11 Fuel system 7.12 Electrical system 7.13 Pitot-static system Date of issue: 10/03/31...

  • Page 68: Description Of Airplane And Systems

    PS-POH-1-1-01 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS 7. DESCRIPTION OF AIRPLANE AND SYSTEMS 7.1 General This section provides description and operation of the aircraft and its systems. PiperSport aircraft is a single-engine, all metal, low-wing monoplane of semi- monocoque structure with two side-by-side seats. The airplane is equipped with a fixed tricycle undercarriage with castering nose wheel.

  • Page 69: Instrument Panel

    PS-POH-1-1-01 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS 7.4 Instrument panel Actual picture, description and data for follow items are shown in Section 9, Supplement No.02 • Instrument panel layout • Description of instrumentation and controls in the cockpit • Instruments and Avionics NOTE For instrument and avionics operating instructions refer to the documentation supplied with the instruments and avionics.

  • Page 70: Propeller

    PS-POH-1-1-01 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS Carburetor preheating Heated air streaming from a heat exchanger to the carburetor through the airbox. The control lever is installed on the middle panel. Ignition switch Ignition switch must be on “BOTH” position to operate the engine. For safety remove the key when engine is not running.

  • Page 71: Landing Gear

    PS-POH-1-1-01 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS 7.7 Landing gear Aircraft is equipped with tricycle landing gear. Main landing gear uses two fiberglass spring elements. Each main gear wheel is equipped with an independent, hydraulically operated, disc type brakes. Nose wheel is free castering.

  • Page 72: Canopy

    PS-POH-1-1-01 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS 7.10 Canopy Access to the cabin is from both sides. Make sure that the canopy is latched and mechanism is securely locked into position on both sides before operating the aircraft. 7.11 Fuel system Each tank is equipped with a vent outlet, finger screen filter and float sensor.

  • Page 73: Electrical System

    PS-POH-1-1-01 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS 7.12 Electrical system Battery The 12 [V] battery is mounted on 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.
  • Page 74 PS-POH-1-1-01 SECTION 7 DESCRIPTION OF AIRPLANE AND SYSTEMS Intentionally left blank Date of issue: 10/03/31 Revision: -...
  • Page 75 SECTION 8 PS-POH-1-1-01 HANDLING AND SERVICING SECTION 8 TABLE OF CONTENTS 8. HANDLING AND SERVICING Introduction Ground handling Towing instructions Tie-down instructions Servicing operating fluids Cleaning and care Assembly and disassembly Aircraft inspection periods Aircraft alterations or repairs Date of issue: 10/03/31 Revision: -...

  • Page 76: Handling And Servicing

    SECTION 8 PS-POH-1-1-01 HANDLING AND SERVICING 8. HANDLING AND SERVICING 8.1 Introduction This section contains factory-recommended procedures for proper ground handling and servicing of the airplane. It also identifies certain inspection and maintenance requirements, which must be followed if the airplane is to retain that new-plane performance and dependability.

  • Page 77: Towing Instructions

    SECTION 8 PS-POH-1-1-01 HANDLING AND SERVICING 8.3 Towing instructions To handle the airplane on ground use the Tow Bar, or if pushing the airplane by hand, push on the aft fuselage, placing your hands over an area of skin supported by a bulkhead. CAUTION Avoid excessive pressure at the airplane airframe-especially at control surfaces.

  • Page 78: Supplements

    SECTION 8 PS-POH-1-1-01 HANDLING AND SERVICING 8.5.1 Approved fuel grades and specifications Recommended fuel type: (refer to the ROTAX Operator’s manual 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.

  • Page 79: Cleaning And Care

    SECTION 8 PS-POH-1-1-01 HANDLING AND SERVICING 8.5.3 Approved coolant grades and specifications Recommended coolant type: (refer to the Rotax Operator’s manual section 10.1.2 Operating speeds and limits and section 10.2.1 Coolant, Rotax Installation manual section 12 Cooling system, Rotax Service Instruction SI-912-016) In principle, 2 different types of coolant are permitted: •...

  • Page 80: Assembly And Disassembly

    SECTION 8 PS-POH-1-1-01 HANDLING AND SERVICING CAUTION In the case of long term parking, cover the canopy to protect the cockpit interior from direct sunshine. 8.7 Assembly and disassembly Refer to the PiperSport aircraft Maintenance manual and the PiperSport aircraft Assembly photo manual.
  • Page 81 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS SECTION 9 TABLE OF CONTENTS 9. SUPPLEMENTS 9.1 List of inserted supplements 9.2 Inserted supplements Date of issue: 10/03/31 Revision: -...
  • Page 82 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS 9. SUPPLEMENTS This section contains the appropriate supplements necessary to 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 Suppl. Revision Date Title of inserted supplement...
  • Page 83 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Supplement No. 01 Aircraft Flight Training Supplement Introduction The PiperSport flying characteristics and behavior are similar to other single engine aircraft. Following training procedure is applicable if the pilot is holder of PPL or LSA Pilot License. The training flight hours are recommended minimum and depends on the Flight Instructor if student pilot is ready to continue on in next training step.
  • Page 84 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Flight training program (recommended): Dual Solo Flight Training Procedure Flights Time Flights Time Check flight 30’ Pattern training flights up to 20’ 15’ 1,000 ft AGL Pattern training flights up to 20’ 15’ 500 ft AGL Stall speed, 45°turns, side slips 30’...

  • Page 85: Limitations

    SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Supplement No. 02 AIRCRAFT SPECIFICATION In this Supplement No. 02 – the Weight & Balance & Equipment is shown for real S/N of the aircraft. Aircraft Registration number : P1001001 Aircraft Serial Number : This Supplement must be contained in the Pilot’s Operating Handbook during operation of the airplane.
  • Page 86 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS 6. WEIGHT AND BALANCE 6.5 C.G. range and determination Aircraft C.G. determination WEIGHT & BALANCE RECORD Empty Weight C.G. Check of PiperSport aircraft S/N : P1001001 WEIGHT MOMENT ITEM [lb] [in] (WEIGHT x ARM) RIGHT MAIN = 325.38 31.42 10,223.44...
  • Page 87 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS WEIGHT & BALANCE RECORD Forward C.G. Check of PiperSport aircraft S/N : P1001001 WEIGHT MOMENT FORWARD C.G. [lb] [in] (WEIGHTxARM) 853.60 -------- 14,460.91 EMPTY AIRCRAFT 88.00 27.56 2,425.28 PILOT 27.56 PASSENGER BAGGAGE 51.58 COMPARTMENT - A BAGGAGE 70.87 COMPARTMENT - B...
  • Page 88 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS WEIGHT & BALANCE RECORD Rearward C.G. Check of PiperSport aircraft S/N : P1001001 WEIGHT MOMENT REARWARD C.G. [lb] [in] (WEIGHT x ARM) 853.60 -------- 14,460.91 EMPTY AIRCRAFT 190.08 27.56 5,238.60 PILOT 190.08 27.56 5,238.60 PASSENGER BAGGAGE 33.00 51.58 1,702.14...
  • Page 89 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS 6.6 Permitted payload range table PiperSport Serial number : P1001001 for 30 min gauges together 1 / 4 1 / 2 3 / 4 flight 15.1 22.6 30.1 US gal volume 28.5 85.5 liter 22.2 45.1 90.3 135.4 180.6...
  • Page 90 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS 6.7 Installed equipment list of PiperSport aircraft S/N : P1001001 • Rotax 912 ULS • Woodcomp KLASSIC 170/3/R • Dynon D100 EFIS • Dynon D120 EMS • Backup Airspeed indicator • Backup Altimeter • Magnetic compass •...
  • Page 91 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS 7. DESCRIPTION OF AIRPLANE AND SYSTEMS 7.4 Instrument panel Instrument panel layout of PiperSport aircraft S/N: P1001001 Date of issue: 10/03/31 Revision: - 7 of 14...
  • Page 92 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Description of instrumentation and controls in the cockpit Autopilot disconnection Parking brake button Backup Altimeter Switches / Circuit breakers Dynon EFIS Ignition switch Dynon Alerts volume EMS warning light control Dynon HS34 Flaps control switch HSI expansion module Backup Airspeed indicator Flaps position indicator Transceiver...
  • Page 93 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Instruments and Avionics • Dynon D100 EFIS • Dynon D120 EMS • Backup Airspeed indicator • Backup Altimeter • Magnetic compass • Garmin SL30 transceiver • PS Engineering PM3000 intercom • Garmin GTX328 transponder • King AK451 ELT •...
  • Page 94 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Description of switches and circuit breakers circuit breaker MASTER INSTR. engine instruments switch AVIONICS switch AUTOPIL. autopilot switch circuit breaker STROBE NAV. L. navigation lights circuit breaker LDG. L. landing light circuit breaker fuel pump circuit breaker FUEL P.
  • Page 95 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Intentionally left blank Date of issue: 10/03/31 Revision: - 11 of 14...
  • Page 96 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Blank form of Weight & Balance record WEIGHT MOMENT ITEM [lb/kg] [in/mm] (WEIGHT x ARM) RIGHT MAIN WHEEL LEFT MAIN WHEEL NOSE WHEEL negative arm Empty weight: Aircraft moment: C.G.= [in/mm] COMPUTED C.G. EMPTY [lb/kg] [%]MAC NOTE: EMPTY WEIGHT INCLUDING OIL, COOLANT AND HYDRAULIC FLUID.
  • Page 97 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS WEIGHT MOMENT AIRCRAFT C.G. [lb/kg] [in/mm] (WEIGHTxARM) -------- EMPTY AIRCRAFT 27.56 PILOT 27.56 PASSENGER BAGGAGE 51.58 1 310 COMPARTMENT - A BAGGAGE 70.87 1 800 COMPARTMENT - B 23.62 WING LOCKERS 7.09 FUEL TANKS TOTAL [lb/kg] C.G.
  • Page 98 SECTION 9 PS-POH-1-1-01 SUPPLEMENTS Blank form of Permitted payload range PiperSport Serial number : for 30 1 / 4 1 / 2 3 / 4 gauges together min flight 15.1 22.6 30.1 US gal volume liter 28.5 85.5 22.2 45.1 90.3 135.4 180.6...

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