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Alpi Aviation Pioneer 200 Aircraft Flight Manual

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PIONEER 200 Aircraft
__________________________________________
Document N° F2-1.0/R80/F/EU Dated 20-04-2002
MANUFACTURER : ALPI AVIATION S.r.l.
Address :
City :
Country :
Web Site : www.alpiaviation.com
Telephone:
E - mail :
AIRCRAFT TYPE & MODEL
Type :
Model :
Aircraft Mark :
Aircraft S/N :
By : www.aeroprogetti.net
FLIGHT MANUAL
Cover page
Via dei Templari, 24
33080 San Quirino (PN)
Italy
+39 0434 37 04 96
info@alpiaviation.com
Pioneer
200

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Summary of Contents for Alpi Aviation Pioneer 200 Aircraft

  • Page 1 PIONEER 200 Aircraft FLIGHT MANUAL __________________________________________ Document N° F2-1.0/R80/F/EU Dated 20-04-2002 Cover page MANUFACTURER : ALPI AVIATION S.r.l. Address : Via dei Templari, 24 City : 33080 San Quirino (PN) Country : Italy Web Site : www.alpiaviation.com Telephone: +39 0434 37 04 96 E - mail : info@alpiaviation.com...
  • Page 2 Pioneer 200 Document N° : Section: 0 Flight Manual F2-1.0/R80/F/EU TABLE OF CONTENTS SECTION General Limitations Emergency Procedures Normal Procedures Performance Weight and Balance Statement This page will change with all revision issues Sect : 0 -Page: 1 of 8 Dated: 20-04-2002 REVISION : By :www.aeroprogetti.net...
  • Page 3 Pioneer 200 Document N° : Section: 0 Flight Manual F2-1.0/R80/F/EU AMENDMENT RECORD SHEET Revision No. Page(s) Signature. Date of affected Incorporation All pages 20-03-02 This page will change with all revision issues Sect : 0 -Page: 2 of 8 Dated: 20-04-2002 REVISION : By :www.aeroprogetti.net...
  • Page 4 Flight Manual for the aircraft. Amendments shall be issued by Alpi Aviation as necessary and will take the form of replacement pages, with the changes to the text indicated by a vertical line in the margin together with the amendment date at the bottom of the page.
  • Page 5 It is the responsibility of the owner to maintain this Manual in a current status when it is being used for operational purposes. Owners should contact Alpi Aviation S.r.l. whenever the revision status of their Manual is in question. A revision bar will extend the full length of new or revised text and/or illustrations added on new or presently existing pages.

  • Page 6: Flight Manual

    Pioneer 200 Document N° : Section: 0 Flight Manual F2-1.0/R80/F/EU LIST OF EFFECTIVE PAGES The dates of issue for original & revised pages are: Page Rev. Date Page Rev. Date Page Rev. Date Section 0 Section 3 Section 5 20-04-02 20-04-02 20-04-02 20-04-02...
  • Page 7 Pioneer 200 Document N° : Section: 0 Flight Manual F2-1.0/R80/F/EU DEFINITIONS AIRFIELD PRESSURE ALTITUDE The Airfield Pressure Altitude is that altitude registered at the surface of the aerodrome by an altimeter with the pressure subscale set to 1013 millibars INDICATED AIRSPEED (I.A.S.) Indicated airspeed, which is the reading obtained from an airspeed indicator having no calibration error.
  • Page 8 Pioneer 200 Document N° : Section: 0 Flight Manual F2-1.0/R80/F/EU BEST ANGLE-OF-CLIMB The speed which results in the greatest gain of altitude SPEED in a given horizontal distance. BEST RATE-OF-CLIMB SPEED The speed which results in the greatest gain in altitude in a given time.
  • Page 9 Pioneer 200 Document N° : Section: 0 Flight Manual F2-1.0/R80/F/EU WEIGHT AND BALANCE TERMINOLOGY STATION Only two load stations are specified: ie Seat Station which is the centre of the fixed seats and Fuel Station which is the centre of the fixed fuel tank. C.G.
  • Page 10 Pioneer 200 Document N° : Section: 1 Flight Manual General F2-1.0/R80/F/EU Section1 - General Table of Contents 1.1. AIRCRAFT THREE VIEW DRAWING 1.2. TECHNICAL DATA 1.2.1. ENGINE 1.2.2. PROPELLER 1.2.3. APPROVED FUEL TYPES AND GRADES 1.2.4. FUEL CAPACITY 1.2.5. APPROVED OIL GRADES 1.2.6.
  • Page 11 Pioneer 200 Document N° : Section: 1 Flight Manual General F2-1.0/R80/F/EU 1.1. AIRCRAFT THREE VIEW DRAWING Sect : 1 -Page: 2 of 6 REVISION : Dated: 20-04-2002...
  • Page 12 Pioneer 200 Document N° : Section: 1 Flight Manual General F2-1.0/R80/F/EU Ground Turning Radius = 6 metres. Sect : 1 -Page: 3 of 6 REVISION : Dated: 20-04-2002...
  • Page 13 Pioneer 200 Document N° : Section: 1 Flight Manual General F2-1.0/R80/F/EU 1.2. TECHNICAL DATA 1.2.1. ENGINE Manufacturer: ROTAX GmbH Aircraft Engine Type: 912 UL Series liquid cooled 1.2.2. PROPELLER Manufacturer: TONINI Type: Fixed Pitch Wooden GT 166X142 Diameter: 166 cm Pitch: 142 cm 1.2.3.
  • Page 14 Pioneer 200 Document N° : Section: 1 Flight Manual General F2-1.0/R80/F/EU 1.2.5. APPROVED OIL GRADES Motorcycle oil of a registered brand with gear additive Specification API classification "SJ" or "SG" Exemples : Shell - Advance VSX 4 (SAE 20W-40) Castrol - Syntetic Blend (SAE 5W-50) Shell - Synthetic Blend (SAE 10W-30) For temp.
  • Page 15 Pioneer 200 Document N° : Section: 1 Flight Manual General F2-1.0/R80/F/EU INTENTIONALLY LEFT BLANK Sect : 1 -Page: 6 of 6 REVISION : Dated: 20-04-2002...

  • Page 16: Table Of Contents

    Pioneer 200 Document N° : Section: 2 Flight Manual Limitations F2-1.0/R80/F/EU Section 2 - Limitations Table of Contents Table of contents 2.1. Introduction 2.2. Type of operation 2.3. Airspeed limitations 2.4. Weights and loading 2.5. Centre of gravity limits 2.6. Powerplant limitations 2.7.

  • Page 17: Airspeed Limitations

    Pioneer 200 Document N° : Section: 2 Flight Manual Limitations F2-1.0/R80/F/EU 2.1. INTRODUCTI0N Section 2 includes operating limitations, instrument markings and basic placards necessary for the safe operation of the airplane, its engine, standard systems and standard equipment. Observance of these operating limitations is required.

  • Page 18: Weights And Loading

    Pioneer 200 Document N° : Section: 2 Flight Manual Limitations F2-1.0/R80/F/EU Airspeed Indicator Markings and their operational significance are shown below. MARKING Km/h SIGNIFICANCE Range White Arc 65 - 100 Full-flap operating range. Lower limit is max. weight Vso in landing configuration. Upper limit is max. speed permissible with flaps extended.

  • Page 19: Powerplant Limitations

    Pioneer 200 Document N° : Section: 2 Flight Manual Limitations F2-1.0/R80/F/EU 2.6. POWERPLANT LIMITATIONS Red Radial Instrument Yellow Arc Green Arc Line/Arc Tachometer 1000 - 1400RPM 1400 - 5500 RPM 5800 RPM 90 o - 110 o C Oil Temp. 50°...

  • Page 20: Maximum Crosswind Velocity

    Pioneer 200 Document N° : Section: 2 Flight Manual Limitations F2-1.0/R80/F/EU Prohibited. 2.7.3. MAXIMUM AIR TEMPERATURE FOR OPERATIONS 40 o C for takeoff at gross weight. 2.7.4. MAXIMUM PERMISSIBLE NUMBER OF OCCUPANTS Two (including Pilot). MAXIMUM CROSSWIND VELOCITY 25 Km/h Dated: 20-04-2002 Sect : 2 -Page: 5 of REVISION :...
  • Page 21 Pioneer 200 Document N° : Section: 2 Flight Manual Limitations F2-1.0/R80/F/EU 2.9. PLACARDS Cockpit Placards General WARNING • Users of this aircraft do so at thei r own risk • This aircraft must be flown in acc ordance with the Owners Manual •...
  • Page 22 Pioneer 200 Document N° : Section: 2 Flight Manual Limitations F2-1.0/R80/F/EU External Fuselage STATIC VENT KEEP CLEAR EARTH ON No step Tyre pressure 32.3 Psi (2.2 Bar) FUEL AVGAS 100LL (See Sect 1) UNLEADED MOGAS 98 Octane or Higher 54 Lt capacity Earth on Post Dated: 20-04-2002 Sect : 2 -Page: 7 of...
  • Page 23 Pioneer 200 Document N° : Section: 2 Flight Manual Limitations F2-1.0/R80/F/EU INTENTIONALLY LEFT BLANK Dated: 20-04-2002 Sect : 2 -Page: 8 of REVISION :...
  • Page 24 Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU Section 3 - Emergency Procedures Table of Contents 3.1. INTRODUCTION 3.2. AIRSPEEDS FOR EMERGENCY OPERATION 3.3. OPERATIONAL CHECKLISTS 3.3.1. ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF RUN ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF 3 ENGINE FAILURE DURING FLIGHT AIRSTART &...

  • Page 25: Introduction

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU 3.1. INTRODUCTION Section 3 provides checklist and other procedures for coping with emergencies that may occur. Emergencies caused by aeroplane malfunctions are rare if proper preflight inspections and maintenance are practiced.

  • Page 26: Operational Checklists

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU 3.3. OPERATIONAL CHECKLISTS 3.3.1. ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF RUN Throttle Idle Brakes Apply Ignition Switches Master Switch ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF Move the control stick FORWARD 90-100 Km/h to mantain Airspeed : Fuel Shutoff Valve...

  • Page 27: Airstart & Limitations

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU AIRSTART & LIMITATIONS In the event that the engine is stopped during flight, it may be restarted by application of fuel & ignition, provided that the propeller is still windmilling. The following procedure addresses only airstarts by use of the Starter Motor.

  • Page 28: Fire During Start On Ground

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU 3.3.2. FIRE FIRE DURING START ON GROUND Cranking CONTINUE to get a start that would suck the flames and accumulated fuel through the carburettor and into the engine. If engine starts, Power 2500 RPM...

  • Page 29: Engine Fire In Flight

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU ENGINE FIRE IN FLIGHT Throttle CLOSED Fuel Shutoff Valve Mag Switches Master Switch Fuel Pump Switch Cabin Air Airspeed 110 Km/h (if fire is not extinguished, increase glide speed to find an airspeed which will provide an incombustible mixture).

  • Page 30: Cabin Fire

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU CABIN FIRE Master Switch Vents/Cabin Air (*) OPEN Land as soon as possible to inspect for damage. (*) Have been demonstrated possibility to open canopy in flight up to 100 mm slot, manually blocked in this position.
  • Page 31 Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU AIRFIELD OR AIRSTRIP PRECAUTIONARY LANDING WITH ENGINE POWER Airspeed 100-105 Km/h Wing Flaps 1st Stage Fuel Pump Selected Field FLY OVER Note terrain and obstructions Radio and Electrical Switches Wing Flaps FULL ( on final approach )

  • Page 32: Ditching

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU Note : IF FIRE Release canopy and seat belts just before touchdown. Cushion face at touchdown with folded coat or cushion Touchdown level attitude OPEN FIELD FORCED LANDING WITH ENGINE POWER Airspeed 100-110 Km/h Wing Flaps...

  • Page 33: Landing With A Flat Main Tyre

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU Heavy Objects SECURE Approach High winds, heavy seas INTO wind. Light winds, heavy swells Parallel to Swells Wing Flaps Power establish 15 m/min (50ft/min) descent at 90 Km/h Canopy Just before splashdown open canopy Touchdown...

  • Page 34: Maximum Glide

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU Refit magneto-thermal fuse, if again fails continue to next airport and inspect or replace. Run, after, the engine; if the fuse again fails rectify before continuing flight. 3.3.6. MAXIMUM GLIDE - For Minimum Rate of Sink: 110 KM/H...

  • Page 35: Carburettor Heat

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU 3.4.1. CARBURETTOR HEAT (IF APPLICABLE) This system serves to prevent the formation of ice within the carburettor, where it primarily forms on the throttle plates in such a manner as to obstruct the airflow, with resultant eventual engine stoppage.

  • Page 36: Low Oil Pressure

    Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU 3.4.3. LOW OIL PRESSURE 1 A rapid drop from normal indicated pressure to indication "0” Action Observe for smell of oil Open cabin air vents Observe for signs of spilt oil on cowls, windscreen, wing surface.
  • Page 37 Pioneer 200 Section: 3 Document N° : Flight Manual Emergency Procedures F2-1.0/R80/F/EU Intentionally left blank Sect : 3 -Page: 14 of 144 Dated: 20-04-2002 REVISION :...
  • Page 38 Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU Section 4 - Normal Operations Table of Contents 4.1. INTRODUCTION 4.2. SPEEDS FOR NORMAL OPERATION 4.3. CHECKLIST & PROCEDURES 4.3.1. PREFLIGHT INSPECTION 4.3.2. BEFORE STARTING ENGINE 4.3.3. STARTING ENGINE - COLD ENGINE. 4.3.4.

  • Page 39: Introduction

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.1. INTRODUCTION Section 4 provides checklist and other procedures for the conduct of normal operations. 4.2. SPEEDS FOR NORMAL OPERATION The following speeds are based on a maximum weight of 450 Kg and may be used for any lesser weight.

  • Page 40: Checklist & Procedures

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.3. CHECKLIST & PROCEDURES 4.3.1. PREFLIGHT INSPECTION Prior to flight, the aircraft should be inspected in accordance with the following checklists and in the sequence shown in the following diagram: Sect : 4 -Page: 3 of 38 Dated: 20-04-2002...
  • Page 41 Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU NOTE Visually check airplane for general condition during walk-around inspection. In cold weather, remove even small accumulations of frost, ice or snow from wing, tail and control surfaces. Also, make sure that control rods and cables are free of ice and move freely.

  • Page 42: Preflight Inspection Checklists

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU PREFLIGHT INSPECTION CHECKLISTS 1 - FUEL Fuel Quantity CHECK level in tank through visual or little rod. Chech instrument for security Water Check Before first flight of the day & after each refueling, use sampler cup &...
  • Page 43 Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 5 - RIGHT WING Wing Tie-down DISCONNECT. Main Wheel & Tyre CHECK for security. Proper tyre inflation & wear or damage. Wing Root Mount Bolts CHECK for security. 6 - NOSE Propeller &...
  • Page 44 Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU Flap CHECK security. Control Rods CHECK aileron & flap control bolts & nuts & flap & Cables control rod for security. CHECK rod ends for freedom of rotation & excessive movement 9 - CABIN Flight manual AVAILABLE IN THE AIRCRAFT.

  • Page 45: Before Starting Engine

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.3.2. BEFORE STARTING ENGINE Preflight Inspection COMPLETE Seatbelts & Harness ADJUST & LOCK Fuel Shutoff Valve Radio/Intercom Brakes TEST & SET 4.3.3. STARTING ENGINE - COLD ENGINE. Carburettor Heat COLD Choke Throttle...

  • Page 46: Starting Engine - Hot Engine

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.3.4. STARTING ENGINE - HOT ENGINE. Proceed as for cold engine above, but eliminate the priming operation 3. Instead, open throttle to 1/4. 4.3.5. WARM-UP and FUNCTIONAL CHECK Warm-up the engine with a fast idle of 1500 - 2500 RPM until the oil temperature reaches 50 degrees C.
  • Page 47 Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU either system. If drop is excessive, shut down & determine the reason. Switch No. 2 Ignition ON. NOTE During the check with one system only, the inactive sparkplugs may tend to load up slightly.

  • Page 48: Takeoff

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.3.7. TAKEOFF Normal Takeoff Wing Flaps 1st Stage Carburettor Heat COLD Throttle FULL..OPEN Elevator Control LIFT NOSE WHEEL AT 45-55 Km/h and wait for aircraft to fly itself off (at around 75 Km/h) Climb Speed 100 Km/h until Flaps retracted, then 110...

  • Page 49: Enroute Climb

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.3.8. ENROUTE CLIMB Airspeed 100 Km/h Throttle FULL OPEN NOTE : During climb, monitor the water & oil temperatures to avoid exceeding their limits. The aircraft has been tested to ensure adequate cooling in climb, therefore any excessive readings may indicate a malfunction.

  • Page 50: After Landing

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU Short Field Landing Airspeed 90 Km/h Wing Flaps FULL DOWN ( below 100 Km/h) Power REDUCE to idle as obstacle is cleared Touchdown MAIN WHEELS FIRST Brakes APPLY AS REQUIRED Wing Flaps RETRACT when convenient for better braking...

  • Page 51: Securing Airplane

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.3.13. SECURING AIRPLANE Radio/Intercom Ignition Switches Master Switch Controls LOCK with seatbelt Fuel 4.4. OTHER PROCEDURES 4.4.1. FUELING SAFETY WARNINGS > Never prepare fuel in an area that is enclosed or where fumes could reach ignition point.

  • Page 52: Taxiing

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU > Before first flight of the day, and after each refueling, use a sampler cup and drain a small quantity of fuel from the fuel tank sump quick drain valve -check for water, sediment and contamination.

  • Page 53: Propellor Care

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.4.3. PROPELLER CARE Full throttle run up over loose gravel is especially harmful to propeller tips. When takeoffs must be made over a gravel surface, it is very important that the throttle is advanced slowly.

  • Page 54: Baulked Landing

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.4.7. BAULKED LANDING In a baulked landing (go-around) climb, the wing flap setting should be reduced to the First Stage and landing gears retracted, immediately after full power is applied and the aircraft has accelerated to a safe climb speed. Upon reaching a safe airspeed, the flaps should be slowly retracted to the full up position, whilst allowing the aircraft to accelerate to the best climb speed.

  • Page 55: Stopping The Engine

    Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU 4.4.10. STOPPING THE ENGINE To stop the engine, turn OFF the ignition switches and turn OFF the Master Switch. Carburettor Heat should be returned to the Full IN or cold position. 4.4.11.
  • Page 56 Pioneer 200 Document N° : Section: 4 Flight Manual Normal Operations F2-1.0/R80/F/EU INTENTIONALLY LEFT BLANK Sect : 4 -Page: 19 of 198 Dated: 20-04-2002 REVISION :...
  • Page 57 Pioneer 200 Document N° Section: 5 Flight Manual Performance F2-1.0/R80/F/EU Section 5 - Performance Table of Contents Table of Contents 5.1. STALLING 5.1.1. STALL SPEEDS 5.1.2. NATURE OF STALL WARNING 5.2. TAKEOFF & LANDING DISTANCES 5.3. MAXIMUM CROSSWIND FOR TAKEOFF & LANDING Sect : 5 -Page: 1 of 2 Dated: 20-04-2002 REVISION :...
  • Page 58 Pioneer 200 Document N° Section: 5 Flight Manual Performance F2-1.0/R80/F/EU 5.1. STALLING 5.1.1. STALL SPEEDS (In Km/h and power off condition - Maximum Takeoff & Landing Weight) Stage 1 Stage 2 Flap Setting Zero Takeoff Landing 5.1.2. NATURE OF STALL Aircraft buffeting announce the stall.
  • Page 59 Pioneer 200 Document N° Section: 6 Flight Manual Weight and Balance F2-1.0/R80/F/EU Section 6 - Weight and Balance Table of Contents 6.1. Introduction 6.2. Aircraft Weight Record 6.3. Center of Gravity Limits 6.3.1. Operational Aircraft Center of Gravity 6.4. Aircraft Equipment List Sect : 6 -Page: 1 of 4 Dated: 20-04-2002 REVISION :...

  • Page 60: Introduction

    Pioneer 200 Document N° Section: 6 Flight Manual Weight and Balance F2-1.0/R80/F/EU 6.1. Introduction This section contains basic weight and center of gravity information necessary to ensure correct loading. It records the weight and balance of the empty aircraft, together with the Aircraft Weight & Balance diagram. These documents are to be carried in the Flight Manual at all times.

  • Page 61: Center Of Gravity Limits

    Pioneer 200 Document N° Section: 6 Flight Manual Weight and Balance F2-1.0/R80/F/EU Maximum takeoff and landing weight 450 Kg) 6.3. Center of Gravity Limits 6.3.1. Operational Aircraft Center of Gravity 20% MAC = 670 mm aft of datum up to & including 350 kg Forward Limit: 26% MAC = 685 mm aft of datum @ 450 Kg.

  • Page 62: Aircraft Equipment List

    Pioneer 200 Document N° Section: 6 Flight Manual Weight and Balance F2-1.0/R80/F/EU 6.4. Aircraft Equipment List Items listed in the following table were fitted to the standard aircraft at manufacture and were included in the aircraft basic weight. Generic Item Specific Item Engine Rotax 912 UL...

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