Pipistrel ALPHA Trainer LSA Pilot Operating Handbook
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Pipistrel ALPHA Trainer LSA Pilot Operating Handbook

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PILOT OPERATING HANDBOOK
ALPHA Trainer LSA
Document No.: POH-162-00-40-001*
REVISION A00
Date of Issue: December 3
, 2019
rd
*applicable to all ALPHA Trainer aircraft, from serial number 996 AT
912 LSA onwards, that are registered as an S-LSA or E-LSA (experi-
mental) airplane and have a MTOM of 550 kg.
Aircraft Serial Number: 1001 AT 912 LSA
Aircraft Registration Number: N221PF
PIPISTREL VERTICAL SOLUTIONS d.o.o.
Vipavska cesta 2
SI-5270 Ajdovščina
Slovenia
Tel: + 386 5 36 63 873
Fax: + 386 5 36 61 263
Email: info@pipistrel.si
All rights reserved. Reproduction or disclosure to third parties of this document or any
part thereof is not permitted, except with the prior and express written permission of
Pipistrel Group's R&D division, Pipistrel Vertical Solutions d.o.o., which is authorized to
publish technical documentation for Pipistrel Group's subsidiaries.

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  • Page 1 All rights reserved. Reproduction or disclosure to third parties of this document or any part thereof is not permitted, except with the prior and express written permission of Pipistrel Group’s R&D division, Pipistrel Vertical Solutions d.o.o., which is authorized to publish technical documentation for Pipistrel Group’s subsidiaries.
  • Page 2 ALPHA Trainer LSA Pilot Operating Handbook Pilot Operating Handbook ALPHA Trainer LSA - 550 kg Authority: Verified and approved under the authority of DOA No.: SLO.DOA.002 The airplane must be operated in compliance with information and limitations contained herein. POH-162-00-40-001 PAGE PAGE REV.
  • Page 3 SUPPLEMENTS Online updates, service notice tracking & airworthinress reporting To access all publications that pertain to your aircraft, including instructions for continued airworthiness, please visit www.pipistrel-aircraft.com and login to our technical publication portal using the following: Username: owner1 Password: ab2008...
  • Page 4 The same system applies when the header, figure or any other element inside this POH is revised. A list of revisions is located at the beginning of the log of effective pages. Pipistrel is not responsible for technical changes/updates to OEM manuals supplied with the aircraft (eg.
  • Page 5 ALPHA Trainer LSA Pilot Operating Handbook Index of document revisions Doc. Descrip- Reason for revision Affected pages Authority Rev. tion First SLO.DOA.002 POH-162-00-40-001 PAGE PAGE REV. 0...
  • Page 6 ALPHA Trainer LSA Pilot Operating Handbook List of effective pages PAGE PAGE PAGE PAGE PAGE PAGE PAGE PAGE NUMBER REV. NUMBER REV. NUMBER REV. NUMBER REV. Cover 2 - 1 3 - 12 4 - 1 2 - 2 3 - 13...
  • Page 7 ALPHA Trainer LSA Pilot Operating Handbook List of effective pages (continued) PAGE PAGE PAGE PAGE PAGE PAGE PAGE PAGE NUMBER REV. NUMBER REV. NUMBER REV. NUMBER REV. 7 - 25 9 - 1 6 - 1 4 - 29 7 - 26...
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  • Page 9 SECTION...

  • Page 10: Table Of Contents

    ALPHA Trainer LSA Pilot Operating Handbook SECTION 1 – GENERAL TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION DESCRIPTION CERTIFICATION BASIS THREE VIEW DRAWINGS AIRCRAFT OVERVIEW SYSTEMS Powerplant Propeller Fuel System Landing Gear Ballistic Parachute Rescue System (BPRS) SYMBOLS, ABBREVIATIONS and TERMINOLOGY...

  • Page 11: Introduction

    The proven low-pressure wet lay-up method from the sailplane industry is used to build the airplane structure. 1.3. CERTIFICATION BASIS ALPHA Trainer LSA complies with the following ASTM standard specifica- tions for Light Sport Aircraft: F2245 / F2746 / F2295...

  • Page 12: Three View Drawings

    ALPHA Trainer LSA SECTION 1 Pilot Operating Handbook GENERAL 1.4. THREE VIEW DRAWING Figure 01-001 ALPHA Trainer POH-162-00-40-001 PAGE PAGE REV. 0...

  • Page 13: Aircraft Overview

    ALPHA Trainer LSA SECTION 1 Pilot Operating Handbook GENERAL 1.5. AIRCRAFT OVERVIEW Basic Dimensions Metric Imperial Length 6.5 m 21’ 4” Span 10.50 m 34’ 6” Height 2.05 m 6’ 9” Wing Area 9.51 m² 102.4 ft² Mean aerodynamic chord 0.90 m...

  • Page 14: Systems

    There is also an oil cooling system. 1.6.2. PROPELLER The airplane is equipped with a Pipistrel FP02-80 propeller. It is a 2-blade, fixed pitch, wooden propeller with 1.65 m (65”) diameter. 1.6.3. FUEL SYSTEM The airplane uses single tank located in the fuselage, behind the cabin.

  • Page 15: Symbols, Abbreviations And Terminology

    ALPHA Trainer LSA SECTION 1 Pilot Operating Handbook GENERAL 1.7. SYMBOLS, ABBREVIATIONS AND TERMINOLOGY 1.7.1. GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS Knots Calibrated Airspeed is the indicated airspeed corrected for position and instrument error. Calibrated airspeed is equal to true airspeed in stan- dard atmosphere at sea level.
  • Page 16 ALPHA Trainer LSA SECTION 1 Pilot Operating Handbook GENERAL 1.7.2. METEOROLOGICAL TERMINOLOGY Instrument Meteorological Conditions are meteorological conditions expressed in terms of visibility, distance from cloud, and ceiling less than the minima for visual flight defined in FAR 91.155. International Standard Atmosphere (standard day) is an atmosphere...
  • Page 17 ALPHA Trainer LSA SECTION 1 Pilot Operating Handbook GENERAL 1.7.3. ENGINE POWER TERMINOLOGY Horsepower is the power developed by the engine. Maximum Continuous Power is the maximum power that can be used continuously. Manifold Pressure is the pressure measured in the engine’s induction system expressed as inHg.
  • Page 18 ALPHA Trainer LSA SECTION 1 Pilot Operating Handbook GENERAL Mean Aerodynamic Chord is the chord drawn through the centroid of the wing plan area. LEMAC Leading Edge of Mean Aerodynamic Chord is the forward edge of MAC aft of the reference datum.

  • Page 19: Conversion Table

    ALPHA Trainer LSA SECTION 1 Pilot Operating Handbook GENERAL 1.8. CONVERSION TABLE 1 bar 14.5037 psi 1 psi 0.0689 bar 1 mm2 0.0016 in2 1 in2 625 mm2 1 cm2 0.1550 in2 1 in2 6.4510 cm2 1 daN 2.2481 lbf 1 lbf 0.4448 daN...
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  • Page 21 SECTION...
  • Page 22 ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS SECTION 2 – LIMITATIONS TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION AIRSPEED LIMITATION AIRSPEED INDICATOR MARKINGS ENGINE LIMITATIONS ENGINE INSTRUMENT MARKINGS WEIGHT AND CENTER OF GRAVITY LIMITS OCCUPANCY FUEL OIL/COOLANT 2.10...

  • Page 23: Introduction

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.1 INTRODUCTION This section provides operating limitations, instrument markings and basic placards necessary for the safe operation of the airplane and its standard systems and equipment. Refer to section 9 for operating limitations for op- tional equipment.

  • Page 24: Airspeed Indicator Markings

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.3 AIRSPEED INDICATOR MARKINGS Speeds in the table below are KIAS. MARKING VALUE (KIAS) REMARKS Flap Operating Range. Lower limit is the most White adverse stall speed in the landing configuration.

  • Page 25: Engine Instrument Markings

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS Minimum Oil Temperature 50 °C (120 °F) Normal Oil Temperature 90 °C - 110 °C (190 - 230 °F) Maximum Oil Temperature 140°C (285 °F) Minimum Coolant Temperature not limited Maximum Coolant Temperature 120 °C (248 °F)

  • Page 26: Weight And Center Of Gravity Limits

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.6 WEIGHT AND CENTER OF GRAVITY LIMITS Maximum takeoff weight 550 kg / 1212 lbs Maximum landing weight 550 kg / 1212 lbs Design empty weight (typical) 279 kg / 615 lbs...

  • Page 27: Oil/Coolant

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS OIL/COOLANT Recommended oil: SAE 10W-40 (Aero Shell Oil Sport Plus 4, as per Rotax specification). Maximum oil capacity 3.5 liter Minimum oil required marked on dipstick 50/50 water/antifreeze Approved coolant* mixture...

  • Page 28: Temperature Limits

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.13 TEMPERATURE LIMITS Flight when the temperature of the aircraft’s surface is at risk of exceeding 55° C is prohibited. 2.14 MINIMUM FLIGHT CREW The minimum flight crew is one pilot.
  • Page 29 ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.15.1 MINIMUM LIST OF EQUIPMENT MLE - REQUIRED FOR KIND OF SYSTEM, OPERATION INSTRUMENT, EQUIPMENT Night VHF COM / (NAV) — — — Battery — — Ammeter / Indication — —...

  • Page 30: Operational Restrictions

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.16 OPERATIONAL RESTRICTIONS Flight into known icing conditions is prohibited. No flights in heavy rainfall or blizzard conditions. Areas with risk of thunderstorms should be avoided. Smoking is prohibited. Engine: -25°C (oil temperature) to 50°C (ambient temperature) as per Rotax OM.

  • Page 31: Placards

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.17 PLACARDS 2.17.1. PLACARDS (EXTERNAL) Next fuel tank filler neck: Next to wheel tire pressure hatches: On each main landing gear wheel fairing (if applicable) (2x): On vent/drain holes: POH-162-00-40-001 PAGE 2-11 PAGE REV.
  • Page 32 ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS Next to door opening latches: Next to fuel drain outlet on bottom engine cowling: FUEL / WATER DRAIN VALVE OPEN CLOSED Near the oil system On the fuel system breather: breather:...
  • Page 33 ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.17.3 PLACARDS (INSTRUMENT PANEL) MTOW 550 kg MTOW 1212 lbs CREW WT min. 55 kg CREW WT min. 121 lbs 1111922 1111921 CABIN LIGHT ONLY FOR DIAGNOSTICS AND UPGRADES 1111879 ONLY FOR...

  • Page 34: Placards (Center Console)

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.17.4 PLACARDS (CENTER CONSOLE) Next to fuel shut off valve: Next to choke and throttle levers (2x): On flap lever (2x): Next to cabin-air control lever: Next to brake lever (2x):...

  • Page 35: Placards (Cabin)

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.17.5 PLACARDS (CABIN) In front of control sticks - rudder pedal adjustment (2x): 1111707 Below each door to depict door handle operation: CLOSED OPEN OPEN CLOSED On upper tube in front of pilot:...

  • Page 36: Placards (Ballistic Parachute Rescue System)

    ALPHA Trainer LSA SECTION 2 Pilot Operating Handbook LIMITATIONS 2.17.6 PLACARDS (BALLISTIC PARACHUTE RESCUE SYSTEM) On/adjecent to parachute rescue system hatch and over rocket position: Next to doors (2x): Next to rocket exhaust (bottom of fuselage): Next to activation handle (cockpit):...
  • Page 37 SECTION...
  • Page 38 ALPHA Trainer LSA Pilot Operating Handbook SECTION 3 – EMERGENCY PROCEDURES TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION AIRSPEEDS FOR EMERGENCY OPERATIONS GROUND EMERGENCIES Engine Fire During Engine Start Emergency Engine Shutdown On Ground Emergency Ground Egress IN-FLIGHT EMERGENCIES...
  • Page 39 ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES PART SUBJECT PAGE NUMBER 3.12 PITOT STATIC MALFUNCTION 3-19 3.13 ELECTRIC TRIM FAILURE 3-20 3.14 BATTERY OVER-VOLTAGE / MALFUNCTION 3-20 3.15 EXCEEDING V 3-21 3.16 ICE BUILD-UP 3-21 3.17 CHECKLIST - EMERGENCY PROCEDURES...
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  • Page 41: Introduction

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES INTRODUCTION This section provides procedures for handling emergencies and critical flight situations. Although emergencies caused by airplane, systems, or engine malfunctions are extremely rare, the guidelines described in this section should be considered and applied as necessary should an emer- gency arise.

  • Page 42: Airspeeds For Emergency Operations

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES The Ballistic Parachute Rescue System (BPRS) should be activated in the event of a life-threatening emergency where BPRS deployment is deter- mined to be safer than continued flight and landing.

  • Page 43: Emergency Engine Shutdown On Ground

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES Brakes ENGAGE Once the aircraft has stopped: Starter KEEP CRANKING Throttle Lever FULL POWER If fire is estinguished: MAG L / MAG R Switches Master BAT & Master GEN If fire persist, perform Emergency Engine Shutdown on Ground and Emer- gency Ground Egress checklists.

  • Page 44: In-Flight Emergencies

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES IN-FLIGHT EMERGENCIES 3.4.1 ENGINE FAILURE AT TAKEOFF (LOW ALTITUDE) If the engine fails immediately after take-off, abort by landing on the run- way. If this is not possible and altitude is not sufficient enough to restart the engine, lower the nose to maintain airspeed and establish a glide attitude.

  • Page 45: Engine Start In Flight

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES Max. Glide (L/D) Ratio (flaps 0): 15 : 1 Best Glide speed (flaps 0): 64 KIAS Minimum sink speed (flaps 0): 58 KIAS Minimum sink rate (flaps 0): 460 ft/min...

  • Page 46: Low Oil Pressure

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES out-of-balance propeller is suspected, immediately shut down engine and perform Emergency Landing procedure. If a partial engine failure permits level flight, land at a suitable airfield as soon as possible. If conditions do not permit safe level flight, use partial power as necessary to set up a emergency landing pattern over a suitable landing field.

  • Page 47: Stall Recovery

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES WARNING: Prolonged use of high power settings after loss of oil pressure will lead to engine mechanical damage and total engine failure. Throttle Lever MINIMUM REQUIRED Land AS SOON AS POSSIBLE...

  • Page 48: Fire In Flight

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES Throttle IDLE Apply full rudder deflection in direction opposite the spin Lower the nose towards the ground to build speed (Stick forward) As rotation stops, neutralize rudder Establish horizontal flight without exceeding g-load or airspeed lim- itations 3.7 FIRE IN FLIGHT...

  • Page 49: Engine Fire In Flight

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES NOTE Door structure/hinge is not designed for intentional open-door oper- ations. Be advised that the chances of door failure occuring is higher, as the airspeed at which the door’s opened at increases.

  • Page 50: Bprs Deployment

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES WARNING If turning off the master switches eliminated the fire situation, leave the master switches OFF. Do not attempt to isolate the source of the fire by checking each individual electrical component.
  • Page 51 ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES CAUTION Expected impact in a fully stabilized deployment is equivalent to a drop from approximately 3 meters. Once it is decided to deploy BPRS, the following actions should be taken:...

  • Page 52: Landing Emergencies

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES The emergency landing body position is assumed by placing both hands on the lap, clasping one wrist with the opposite hand, and holding the up- per torso erect and against the seat backs.

  • Page 53: Ditching

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES Seat Belts SECURED Transponder SQUAWK 7700 ACTIVATE Transmit (121.5 MHz) MAYDAY, Radio giving locations and intentions Flaps (when landing is assured) 3.9.2 DITCHING Transmit (121.5 MHz) MAYDAY, Radio giving location and intentions...

  • Page 54: Landing With Defective Brakes

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES Direction should be maintained using the rudder. This should be supported by use of the brake. It is possible that the brake must be applied strongly - if necessary to the point where the wheel locks.

  • Page 55: Communication System Failure

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES generator fails, the battery should not be disconnected during flight. NOTE: If it is necessary to reduce electrical loads due to an generator mal- function, switch off electrical components and/or systems that are not essen- tial for the current flight conditions rather than pulling circuit breakers.

  • Page 56: Electric Trim Failure

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES +10 KTS for procedures, observe Groundspeed indicator winds 3.13 ELECTRIC TRIM FAILURE Any failure or malfunction of the electric trim can be overridden by use of the control stick. If runaway trim is the problem, cut the circuit by pulling the circuit breaker and land as soon as conditions permit.

  • Page 57: Exceeding

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES 3.15 EXCEEDING V Should the VNE be exceeded, pull the stick gently in order to reduce airspeed and continue flying using gentle control deflections. Land safely as soon as possible and have the aircraft verified for airworthiness by authorized service personnel.
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  • Page 59: Poh-162-00-40-001 Page

    ALPHA Trainer LSA SECTION 3 Pilot Operating Handbook EMERGENCY PROCEDURES 3.17 CHECKLISTS CHECKLISTS EMERGENCY PROCEDURES POH-162-00-40-001 PAGE 3-23 PAGE REV. 0...
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  • Page 61 GROUND EMERGENCIES ENGINE FIRE DURING ENGINE START Fuel Valve CLOSED Booster pump Brakes ENGAGE Once aircraft has stopped: Starter KEEP CRANKING Throttle Lever Full Power If flames are estinguished: MAG L / MAG R Switches Master BAT & Master GEN If flames persist: perform Emergency engine shutdown on Ground and Emergency egress checklist.
  • Page 62 EMERGENCY GROUND EGRESS Engine SHUTDOWN Brakes / Parking Brake ENGAGED Seat Belts RELEASE Airplane EXIT IN FLIGHT EMERGENCIES ENGINE FAILURE AT TAKE OFF (LOW ALT) Best Glide or Landing ESTABILISH (see POH) Speed (as appropriate) Fuel Valve CLOSED MAG L / MAG R Switches Flaps as required Booster pump...
  • Page 63 ENGINE FAILURE IN FLIGHT Best Glide Speed ESTABILISH (64 KIAS) Fuel Valve CHECK OPEN MAG L / MAG R Switches CHECK ON Restart the engine in flight: ENGINE START IN FLIGHT Master BAT Thottle Lever 10 mm OPEN Starter ENGAGE (Propeller not windmilling) Thottle Lever Slowly INCREASE...
  • Page 64 SMOKE IN THE COCKPIT Cabin Air Selector Door Vents OPEN Fan Toggle Switch Airflow Direction Knob Feet position Temperature Control Knob Cold If source of smoke is firewall forward: Cabin Air Selector/ Fan Toggle Switch Door Vents As required Land AS SOON AS POSSIBLE If airflow is not sufficient to clear smoke or fumes from cabin:...
  • Page 65 COCKPIT FIRE IN FLIGHT Cabin Air Selector Fan Toggle Switch Door Vents As required MASTER BAT Switch MASTER GEN Switch Booster pump Fire Extinguisher ACTIVATE (if available) If airflow is not sufficient to clear smoke or fumes from cabin - When fire extinguished: Cabin Air Selector Green Electrical Switches Land...
  • Page 66 SPIN RECOVERING TECHNIQUE Throttle Lever IDLE Full deflection - direction Rudder opposite to the spin Forward - lower the nose Stick to build us speed As rotation stops: Rudder Neutralize Establish horizontal flight without exceeding g-load or airspeed limitations BPRS DEPLOYMENT Airspeed MINIMUM POSSIBLE MAG L / MAG R Switches...
  • Page 67 LANDING EMERGENCIES ENMERGENCY LANDING WITHOUT ENGINE POWER Best Glide Speed ESTABLISH - 64 KIAS Transponder SQUAWK 7700 ACTIVATE Throttle Lever IDLE Fuel Valve CLOSED Booster pump MAG L / MAG R Switches Transmit (121.5 MHz) Radio MAYDAY giving location and intentions Flaps (when landing is assured) Master BAT &...
  • Page 68 LANDING WITHOUT ELEVATOR CONTROL Flaps Trim SET 60 KIAS Throttle Lever as required for glide angle LANDING WITH DEFECTIVE BRAKES Seat Belts SECURED After safe touch-down MAG L / MAG R Switches Fuel Valve CLOSED Booster pump Master BAT & Master GEN (just before touchdown) GENERATOR FAILURE Switch OFF...
  • Page 69 COMMUNICATION FAILURE Switches, Controls, CHECK Volume Frequency CHANGE Circuit Breakers CHECK Headset CHANGE Transmission ATTEMPT If unsuccessful: TRANSPONDER SQUAWK 7600 TRIM / AUTOPILOT FAILURE Graps stick - maintain Airplane Control manually If problem is not corrected: Trim Circuit Breaker PULL Throttle Lever As required Control Stick...
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  • Page 71 SECTION...
  • Page 72 ALPHA Trainer LSA Pilot Operating Handbook SECTION 4 – NORMAL PROCEDURES TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION AIRSPEEDS FOR NORMAL OPERATIONS PREFLIGHT INSPECTION Preflight Walk-Around STARTING THE ENGINE Before Starting the Engine Starting the Engine Before Taxiing Taxiing...
  • Page 73 ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES PART SUBJECT PAGE NUMBER 4.16 CHECKLIST - NORMAL PROCEDURES 4-23 POH-162-00-40-001 PAGE PAGE REV. 0...
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  • Page 75: Introduction

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES INTRODUCTION This section provides amplified procedures for normal operation. CAUTION The following procedures apply to an aircraft configured with all the optional equipment and systems. Skip steps that do not apply to the specific aircraft if the equipment is not installed.

  • Page 76: Preflight Inspection

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES 4.3 PREFLIGHT INSPECTION Before carrying out preflight inspections, ensure that all required mainte- nance has been performed. Review your flight plan and compute weight and balance. NOTE: Throughout the walk-around: check all visible hinges, hinge pins, and bolts for security;...
  • Page 77 ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Master BAT switch Master GEN switch Circuit breakers CHECK IN LEFT FUSELAGE COM/XPDR antennas Condition and attachment Wing / fuselage seal CHECK Check fuel quantity Fuel cap and secure EMPENNAGE...
  • Page 78 ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Airbrake CHECK condition RIGHT MAIN LANDING GEAR Landing gear General condition Tire Condition, inflation, and wear Fluid leaks, evidence Wheel and brakes of overheating, general condition and wear Wheel Fairing...

  • Page 79: Starting The Engine

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Wheel Fairing CHECK attachment Shock absorber CHECK functionality LEFT MAIN LANDING GEAR Landing gear General condition Tire Condition, inflation and wear Fluid leaks, evidence Wheel and brakes of overheating, general...

  • Page 80: Starting The Engine

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Seats, Pedals, Seat Belts and Baggage Adjust and Secure Doors Closed and latched CAUTION: Ensure seat belt harnesses are not twisted. 4.4.2 STARTING ENGINE If the engine is warm, no choke is required. For the first start of the day and in cold conditions, applying choke will be necessary.

  • Page 81: Before Taxiing

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Engine Parameters Monitor Ammeter/Indication Check Generator Fail Light CHECK OFF NAV/AC Lights Booster pump CAUTION: After starting, if the oil gauge does not begin to show pressure within 30 seconds in warm weather and about 60 seconds in very cold weather, shut down engine and investigate cause.
  • Page 82 ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES served, the brake system may overheat and result in brake damage or brake fire. If due to soft terrain a higher RPM setting is required, please consider not to exceed 2500 RPM before a 50° C oil temperature is achieved.

  • Page 83: Before Takeoff / Holding Point Takeoff

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Throttle lever Set to just above idle NOTE: RPM drop must not exceed 300 RPM for either ‘’magneto’’ and the difference in drop should not exceed 150 RPM If there is doubt concerning operation of the ignition system, RPM checks at higher engine speeds will usually confirm whether a deficiency exists.

  • Page 84: Power Check

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES 4.5 TAKEOFF 4.5.1 POWER CHECK Check full-throttle engine operation early in takeoff run. The engine should run smoothly and turn approximately 5300-5500 RPM. All engine parame- ters should read in the green. If power is not developed, abort take-off.

  • Page 85: Short Field Takeoff

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES SHORT FIELD TAKEOFF Flaps (+2) Airbrakes Verify Closed! * Brakes Hold Throttle Lever Full forward Engine Parameters Check Brakes Release Airspeed indication Check Elevator Control Rotate Smoothly at about 40 KIAS...

  • Page 86: Cruise

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Best Climb Speed = 76 KIAS Engine Parameters CHECK CAUTION: Avoid prolonged use of more than 75% rudder deflection as this may result in a pitch-down moment. Should this occur, first neutralize rudder to recover.

  • Page 87: Landing

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Flaps As required (+1) Booster pump Flaps (on final) (+2) below 60 KIAS Airbrakes (on final) As required * Trim As required Final Speed 55 KIAS WARNING Ensure the airbrakes are closed in event of go around maneuver! See SPOH-161-00-41-050 Electric airbrakes POH supplement for additional information about use, setting and testing.

  • Page 88: Balked Landing

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Short Field Landing For a short field landing in smooth air conditions, make an approach at 60 KIAS with full flaps and fully extended airbrakes using enough power to con- trol the glide path (slightly higher approach speeds should be used under turbulent air conditions).

  • Page 89: After Landing

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES Flaps Airspeed Best climb speed V (76 KIAS) WARNING Ensure the airbrakes are closed immediately after the go around is initiated! See SPOH-161-00-41-050 Electric airbrakes POH supplement for additional information about use, setting and testing.

  • Page 90: Parking

    ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES 4.14 PARKING BPRS safety pin CHECK Inserted, secured Parking brake Engaged only if necessary Fuel Valve CLOSED Chocks, Tie-downs, Pitot Covers As required 4.15 SOFT FIELD OPERATIONS As described in 4.5.2. and 4.10.
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  • Page 93 ALPHA Trainer LSA SECTION 4 Pilot Operating Handbook NORMAL PROCEDURES 4.16 CHECKLISTS CHECKLISTS NORMAL PROCEDURES POH-162-00-40-001 PAGE 4-23 PAGE REV. 0...
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  • Page 95 PREFLIGHT WALK-AROUND CABIN UNLOCK/OPEN/ Doors CLOSE/SECURE BPRS Handle / Pin CHECK, Pin inserted MAG L / MAG R Switches CHECK OFF Green Electrical Switches ALL OFF Required Documents On Board Flight Controls, Flaps Free and Correct Circuit Breakers Master BAT Master GEN Generator Fail light Verify ON...
  • Page 96 LEFT FUSELAGE COM/XPDR antennas Condition and attachment Wing / Fuselage Seal CHECK condition CHECK fuel quantity and Fuel cap secure EMPENNAGE Tiedown Rope Remove Horizontal and Vertical CHECK condition Stabilizers Elevator and Elevator Condition and movement U-Piece Rudder Condition and movement Hinges, Bolts, Springs and Secure Pins...
  • Page 97 RIGHT WING Flaperon Condition and movement CHECK condition, no Flaperon Gap Seal wrinkles CHECK condition and Hinges, Bolts, Safety Nuts secured NAV/AC lights CHECK condition Leading Edge CHECK condition Water Drain Holes Clean CHECK quantity and Fuel Cap secure Cover REMOVED Pitot Tube Tube clear Airbrake...
  • Page 98 ENGINE AND NOSE LANDING GEAR AREA CHECK quantity, leaks, Engine Oil cap and door secured Exhaust Pipe CHECK and condition Gascolator Drain 1 cup, sample Landing Light Attachment and condition Nose Landing Gear CHECK condition Strut CHECK condition Condition, inflation and Wheel and Tire wear Wheel Fairing...
  • Page 99 LEFT WING Leading edge Condition NAV/AC lights Condition and attachment Condition, attachment, Flaperon movement Flaperon gap seal Condition, no wrinkles Hinges, bolts and safety Secure nuts Airbrake CHECK condition POH-162-00-40-001 PAGE 4-29 PAGE REV. 0...
  • Page 100 STARTING ENGINE BEFORE STARTING ENGINE Preflight Inspection / Completed Logbook Fuel Quantity Sufficient Emergency Equipment On board Passenger Briefed BPRS Safety Pin Removed Seats, Pedals, Seat belts Adjust and Secure and Baggage Doors Closed and latched STARTING ENGINE Parking Brake ENGAGE Fuel Valve OPEN...
  • Page 101 STARTING ENGINE (continue) 2000 RPM for 2 mins then Throttle Lever 2500 RPM for warm up Oil Pressure CHECK Choke Slowly close Engine Parameters Monitor Ammeter / Indication CHECK Generator Fail Light CHECK OFF NAV/AC Lights Booster pump BEFORE TAXIING Flaps NAV/COM, GPS, XPDR SET as required...
  • Page 102 BEFORE TAKEOFF ENGINE TEST Brakes HOLD Doors Latched Choke Verify CLOSED Throttle Lever 4000 RPM Generator Fail Light CHECK OFF Voltage CHECK Value OFF, note RPM, MAG L switch then ON OFF, note RPM, MAG R switch then ON Engine Parameters CHECK Throttle Lever Set to just above idle...
  • Page 103 BEFORE TAKEOFF (continue) NAV / Strobe / Landing As required Lights Circuit Breakers CHECK NAV/COM, GPS, XPDR Altimeter Engine Parameters CHECK Flight Controls Unobstructed and Correct TAKEOFF NORMAL TAKEOFF Brakes Release Throttle Lever Full Forward Engine Parameters CHECK Airspeed Indication CHECK Rotate smoothly Elevator Control...
  • Page 104 SHORT FIELD TAKEOFF Flaps (+2) Brakes HOLD Throttle Lever Full Forward Engine Parameters CHECK Brakes Release Airspeed Indication CHECK Rotate smoothly Elevator Control at about 40 KIAS Airspeed at Obstacle 58 KIAS at 60 KIAS, FLAPS (+1) at 70 KIAS, FLAPS CLIMB Climb Power / RPM Flaps...
  • Page 105 CRUISE (continue) Flaps Verify (0) Booster pump Cruise Power Engine Parameters CHECK DESCENT / APPROACH Altimeter Cabin heating As required Landing Light Fuel System CHECK Engine Parameters CHECK Parking Brake CHECK Disengaged Seat Belts Secure BEFORE LANDING/LANDING Approach Speed Reduce below 70 KIAS Flaps As required (+1) Booster pump...
  • Page 106 BALKED LANDING Throttle Lever Full Forward Airbrakes CLOSE Flaps (+1) Airspeed 57 - 60 KIAS After Clear of Obstacles: Flaps Airspeed V 76 KIAS AFTER LANDING Throttle Lever IDLE Flaps Booster pump Transponder STBY Lights As required Airbrakes Close at taxi speed PAGE POH-162-00-40-001 4-36...
  • Page 107 SHUT DOWN Green electrical switches All OFF Throttle lever IDLE MAG L / MAG R Switches Master GEN switch Master BAT switch BPRS safety pin Insert Transmit Light OUT PARKING BPRS Safety Pin CHECK Inserted / Secured ENGAGED Parking Brake Only if necessary Fuel Valve CLOSED...
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  • Page 109 SECTION...
  • Page 110 ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA SECTION 5 – PERFORMANCE DATA TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION OUTSIDE AIR TEMPERATURE FOR ISA-CONDITION WIND COMPONENT AIRSPEED CALIBRATION STALL SPEED TAKE-OFF Take-off Performance Effects of Elevation...

  • Page 111: Introduction

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.1. INTRODUCTION The performance tables and diagrams on the following pages show the per- formance of the airplane. The data presented in these tables and diagrams has been derived from test–flights using an airplane and engine in good operating condition, and was corrected to standard atmospheric conditions 15˚...

  • Page 112: Outside Air Temperature For Isa-Condition

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.2. OUTSIDE AIR TEMPERATURE FOR ISA-CONDITION Pressure ISA-40° C ISA-20° C ISA+10° C ISA+20° C Altitude [ft] 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 11000 12000 13000...

  • Page 113: Wind Component

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.3. WIND COMPONENT EXAMPLE: Runway Heading: 10° Wind Direction: 60° Angle between wind and runway: 50° Wind Velocity: 15 Knots Component parallel: ~9,6 Knots Component perpendicular: ~11,5 Knots POH-162-00-40-001 PAGE...

  • Page 114: Airspeed Calibration

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.4. AIRSPEED CALIBRATION KIAS/KCAS Diagram Conditions Power: power level for level flight, or max. continuous power whichever is less The IAS-CAS relation is shown in the graph below: POH-162-00-40-001 PAGE...

  • Page 115: Stall Speed

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.5. STALL SPEED Conditions Power: idle Attitude: level flight Weight: MTOM ( 1212 lbs / 550 kg) NOTE: The recovery altitude necessary is very dependent on the tempo of recovery.

  • Page 116: Take-Off

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.6. TAKE-OFF 5.6.1. TAKE-OFF PERFORMANCE Conditions Weight: MTOM ( 1212 lbs / 550 kg) Power: throttle full open Flaps: (+1) Runway: dry, paved and level Wind: calm DISTANCE Conditions [ft] / [m]...

  • Page 117: Effects Of Elevation

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.6.2. EFFECTS OF ELEVATION The table below provides data about the effect of elevation on takeoff runway lenght. UNWAY ELEVATION DISTANCE 1650 ft/ 3280 ft/ 4920 ft/ [ft] / [m]...

  • Page 118: Effects Of The Wind

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.6.4. EFFECTS OF THE WIND Wind (head, cross or tailwind) affects aircraft’s ground speed (GS). Headwind on takeoff or landing causes the takeoff and landing distance length to shorten as the GS is slower during these two flight stages. The opposite holds true for tailwind on takeoff and landing as tailwind increases takeoff and landing distances significantly.

  • Page 119: Climb

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.7. CLIMB 5.7.1. CLIMB PERFORMANCE Climb performance may vary depending on, temperature, altitude, humidity and wing propeller surface condition. Conditions Power: throttle full open Weight: MTOM ( 1212 lbs / 550 kg)

  • Page 120: Cruise

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.8. CRUISE 5.8.1. CRUISE PERFORMANCE Conditions Weight: MTOM ( 1212 lbs / 550 kg) Temperature: ISA Wind: zero Altitude: sea level Flaps: Reference cruise parameters: KIAS FF [US gal] / [liter/h]...

  • Page 121: Landing

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.10. LANDING 5.10.1. LANDING PERFORMANCE Conditions Weight: MTOM ( 1212 lbs / 550 kg) Wind: zero Runway: dry, level and paved Flaps: (+2) Airspeed: 55 KIAS CAUTION: Minimum recommended runway length for approaches is 1640 feet (500 m) with no obstacles inside the 3 deg glide slope area and runway heading in order ensure safe flying activity.

  • Page 122: Noise Characteristics

    ALPHA Trainer LSA SECTION 5 Pilot Operating Handbook PERFORMANCE DATA 5.11. NOISE CHARACTERISTICS According to independent testing performed by German LBA-LTF noise reg- ulations the airplanes, the equivalent exhibited noise measures 55.8 dBa. Noise is measured on the ground when the airplane overflies at 500 ft at full power, at speed of best climb.
  • Page 123 SECTION...
  • Page 124 ALPHA Trainer LSA SECTION 6 Pilot Operating Handbook WEIGHT AND BALANCE SECTION 6 – WEIGHT AND BALANCE TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION C.G. SAMPLE CALCULATION WEIGHT AND BALANCE CHART POH-162-00-40-001 PAGE PAGE REV. 0...
  • Page 125 ALPHA Trainer LSA SECTION 6 Pilot Operating Handbook WEIGHT AND BALANCE INTRODUCTION This section provides information about how to calculate the takeoff weight and C.G. of the aircraft. Once calculated, these two values can be used to find a point on the weight and balance chart (see section 6.3) and thus de- termine whether aircraft is within the flight limits (see section 2.6).
  • Page 126 ALPHA Trainer LSA SECTION 6 Pilot Operating Handbook WEIGHT AND BALANCE 6.2 C.G. SAMPLE CALCULATION The calculation below is an example of how to calculate the aircraft’s takeoff weight and C.G.. Except for the arm values in italic font, the values do not apply to any particular aircraft and are for illustration purposes only.
  • Page 127 ALPHA Trainer LSA SECTION 6 Pilot Operating Handbook WEIGHT AND BALANCE 6.3 WEIGHT AND BALANCE CHART The chart below shows the ALPHA Trainer’s mass-CG envelope. Once the aircraft’s takeoff weight and C.G. have been calculated, they can be used to find a point in the chart and determine whether or not the aircraft is within the flight limits.
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  • Page 129 SECTION...
  • Page 130 ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION SECTION 7 – AIRPLANE DESCRIPTION TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION AIRCRAFT STRUCTURE Fuselage Wings Empennage FLIGHT CONTROL SYSTEM Elevator Control System Aileron Control System Rudder Control System...
  • Page 131 ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION PART SUBJECT PAGE NUMBER Engine Monitoring Instruments Propeller FUEL SYSTEM 7-14 ELECTRICAL SYSTEM 7-15 Electrical System Power Generation Power Distribution Switches Warning Lights Circuit Breakers and Fuses Miscellaneous Components LIGHTNING...
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  • Page 133: Introduction

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION INTRODUCTION This section provides a basic description and operation of the standard air- plane and its systems. Optional equipment described within this section is identified as optional. AIRCRAFT STRUCTURE 7.2.1...
  • Page 134 ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION The wings attach with shear pins to bushes at the fuselage root ribs. Each wing half can be optionally equipped with glider type electric airbrakes. 7.2.3 EMPENNAGE The empennage consists of a horizontal stabilizer, a single piece elevator, a vertical fin and a rudder.

  • Page 135: Flight Control System

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION FLIGHT CONTROL SYSTEM The aircraft uses conventional flight controls for ailerons, elevator and rud- der. The control surfaces are pilot controlled through either of two control sticks positioned centrally in front of each pilot. The location and design of the control sticks allow easy, natural use by the pilots.

  • Page 136: Wing Flaps Control System

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION The nose wheel is part of the yaw control system and is moved whenever the pedal is pressed. Cables for nosewheel steering run from the bellcranks be- hind the seats forward to the nosewheel hinge element, where a anti-shim- my damper is also connected to.

  • Page 137: Nose Gear

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION less type wheel tire is 4.00 x 6. Wheel track is 1.60 m, wheel base 1.58 m. Inflate to 40 psi (2.8 bar). 7.4.2 NOSE GEAR The nose landing gear is supported from the main engine frame. The nose landing gear is steerable, connected to the rudder pedal control system and incorporates an oil-spring damper element.

  • Page 138: Airplane Cabin

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION AIRPLANE CABIN 7.5.1 CABIN DOORS Windshield, upper window and doors’- windows are made from Lexan shat- ter-resistant polycarbonate. The fuselage has two cabin doors made out of CFRP frames. Doors are locked in the closed position via 3 locking pins operated simulta- neously by rotating a common central handle.

  • Page 139: Powerplant

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION POWERPLANT 7.6.1 ENGINE The engine installed is a Rotax 912 UL (A2 version offered as option) engine providing 59.6 kW takeoff power. All limits as defined by the engine manu- facturer apply.

  • Page 140: Engine Operating Controls

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION Engine Fuel Ignition Dual self-powered electronic ignition drive two spark plugs in each cylin- der. The system is denominated as Magnetos, as it mimics the typical func- tionality of mechanical magnetos. Normal operation is conducted with both magnetos, as more complete burning of the fuel-air mixture occurs with dual ignition.

  • Page 141: Engine Monitoring Instruments

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION 7.6.4 ENGINE MONITORING INSTRUMENTS The aircraft is equipped with electronic engine instrumentation, which is part of the Engine Management System display. NOTE: For additional information on instrument limit markings, refer to Sec- tion 2, Limitations.

  • Page 142: Fuel System

    AIRPLANE DESCRIPTION 7.6.5 PROPELLER The airplane is equipped with a Pipistrel FP02-80 propeller. It is a 2-blade, fixed pitch, wooden propeller with 1.65 m (65”) diameter. FUEL SYSTEM The airplane has single 13.2 US gal (50 L) polyamide fuel tank in the fuse- lage, positioned behind the cabin.

  • Page 143: Electrical System

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION Thereafter fuel enters the fuel shut-off valve, activated from the cabin, which has two positions: OPEN and CLOSED. When CLOSED position is selected the valve shuts off the fuel feed line. Once the fuel leaves the fuel valve it is fed through a gascolator, which has a drain valve.

  • Page 144: Power Distribution

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION is capable of delivering max. 12A at 14V which feeds the onboard battery (12V, 11Ah or 12.4Ah for EarthX). In case of emergency, the battery will sup- ply reduced number of necessary direct-current loads with power for 30 minutes.

  • Page 145: Warning Lights

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION Kanardia Horis 0.23 A 0.51 A (Typical) Garmin GTR200 transceiver 2.6 A (Max) 0.72 A (Typical) Garmin GTX335 transponder 1.22 A (Max) Landing light 1 A (steady) NAV/AC lights 2 A (Peak) Electrical trim 0.3 A...

  • Page 146: Circuit Breakers And Fuses

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION connected to the voltage regulator. When ON, this means that the generator is not operating. Normal state (generator operating) is when this LED light is OFF. NOTE: Engine RPM below 1600 will typically result in GENERATOR FAIL warning light to come ON, however this is not a failure but a case of insuffi- cient RPM to generate electrical power.

  • Page 147: Interior Lightning

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION panel. 12 VDC for navigation light operation is supplied through the NAV/ STROBE light switch, which includes a resettable circuit breaker element. Strobe Light Anti-collision strobe lights can be installed integral with the standard naviga- tion light and controlled by the same switch.

  • Page 148: Pitot System

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION steel heat muff fastened to the exhaust system muffler that serves as the system’s source of hot air. Air from the oil cooler enters the engine bay and is directed into the heat muff. Hot air leaving the heat muff is then directed through scat tubing to a mixer where it meets fresh air coming from a NACA inlet positioned on the upper engine cowling.

  • Page 149: Flight Deck Arrangement

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION 7.12 FLIGHT DECK ARRANGEMENT Instrument Panel A typical instrument panel arrangement consists of a set of analogue gauges for airspeed, altitude, vertical speed and rpm. Each instrument features a LCD display showing the values indicated by the instrument pointers. The upper portion of the panel is occupied by a Kanardia Horis.
  • Page 150 ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION Switch Panel A switch panel located in the “dash board” bolster below the flight instru- ments contains the BAT and GEN master switches, magneto switches, starter button, Booster pump, lighting switches and circuit breakers.

  • Page 151: Flight Instruments

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION Center Console The center console contains (front-to-back) throttle and choke lever, elevator trim switch, brake lever and the flap lever. 7.13 FLIGHT INSTRUMENTS The following paragraph lists a typical avionic configuration offered for the aircraft.

  • Page 152: Emergency Locator Transmitter (Elt)

    ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION 7.14 EMERGENCY LOCATOR TRANSMITTER The airplane is optionally equipped with a self-contained emergency locator transmitter (ELT). The transmitter and antenna are installed immediately be- hind the aft cabin wall to the right of the airplane centerline. The main trans- mitter control switch, labeled ON-OFF-ARMED, on the transmitter is in the armed position for normal operations.
  • Page 153 ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION the baggage compartment. There is an exhaust tube leading the activation gasses from the rocket to the outside (bottom) of the fuselage, the exhaust is placarded. The type of BPRS is Galaxy Rescue System GRS 6/473. The parachute sys- tem attaches with 2 belts to the aft fuselage/wings pins and belonging bulk- head.
  • Page 154 ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION Before Flight” streamer is attached to the pin. WARNING: Always remove the safety pin of the BPRS before engine start-up and re-insert before leaving the aircraft. WARNING: After maintenance has been performed or any other time the system has been safe tied, operators must verify that the pin has been removed before further flight.
  • Page 155 ALPHA Trainer LSA SECTION 7 Pilot Operating Handbook AIRPLANE DESCRIPTION BPRS installation: hatch and belt positioning BPRS installation: belts attachment points to fuselage structure POH-162-00-40-001 PAGE 7-27 PAGE REV. 0...
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  • Page 157 SECTION...
  • Page 158 ALPHA Trainer LSA Pilot Operating Handbook SECTION 8 – HANDLING AND SERVICING TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION AIRPLANE INSPECTION PERIODS PILOT CONDUCTED MAINTENANCE CHANGES AND REPAIRS SERVICING Tire Servicing Brake Servicing Propeller Servicing Oil Servicing Fuel System Servicing...

  • Page 159: Introduction

    ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING INTRODUCTION The airplane owner should establish contact with the dealer or certified ser- vice station for service and information. All correspondence regarding the airplane must include its serial number (see tail-mounted type dataplate).

  • Page 160: Servicing

    ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING SERVICING 8.5.1 TIRE SERVICING The main landing gear wheel assemblies use 4.00 x 6 tires. The nose wheel assembly uses a 4.00 x 4 tire. For maximum service from the tires, keep...

  • Page 161: Oil Servicing

    ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING 8.5.4 OIL SERVICING Oil must be changed every 100 hours and sooner under unfavorable (AVGAS) operating conditions. An oil filler cap and dipstick are located at the right side of the engine, accessible through an access door on the top right side of the engine cowl- ing.
  • Page 162 ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING To refuel airplane: Place fire extinguisher near fuel tank being filled. Connect ground wire from refuel nozzle to airplane exhaust, from airplane exhaust to fuel truck or cart, and from fuel truck or cart to a suitable earth ground.

  • Page 163: Ground Handling

    ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING rotating in the opposite direction. CAUTION: Make sure the gascolator sampling outlet has been closed and is not leaking fuel before flight. Fuel/water drain outlet GROUND HANDLING 8.6.1 APPLICATION OF EXTERNAL POWER...
  • Page 164 ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING MASTER BAT switch to ON. 14 VDC from the external power unit will energize the main distribution and essential distribution buses. The airplane may now be started or electrical equipment operated.
  • Page 165 ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING Shut down airplane and install chocks and tie-downs. 8.6.3 PARKING For parking: Head airplane into the wind if possible. Choose even terrain so that fuel does not spill because of sloped wings.

  • Page 166: Cleaning

    ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING CLEANING 8.7.1. CLEANING EXTERIOR SURFACES The airplane should be washed with a mild soap and water. Harsh abrasives or alkaline soaps or detergents could make scratches on painted or plastic surfaces.

  • Page 167: Cleaning Interior Surfaces

    ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING accumulated on the cloth, fold cloth to expose a clean area after each pass. Remove grease or oil using a soft cloth saturated mild detergent, then rinse with clean, fresh water.
  • Page 168 ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING Dry the windows using a dry nonabrasive cotton cloth or chamois. Instrument Panel and Electronic Display Screens The instrument panel, control knobs, and plastic trim need only to be wiped clean with a soft damp cloth.
  • Page 169 ALPHA Trainer LSA SECTION 8 Pilot Operating Handbook HANDLING AND SERVICING Wipe leather upholstery with a soft, damp cloth. For deeper cleaning, use a mix of mild detergent and water. Do not use soaps as they contain alkaline which will cause the leather to age prematurely. Cover areas where cleaning solution could cause damage.
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  • Page 171 SECTION...
  • Page 172 ALPHA Trainer LSA SECTION 9 Pilot Operating Handbook SUPPLEMENTS SECTION 9 – SUPPLEMENTS LIST OF SUPPLEMENTS PART SUBJECT REVISION 9-S1 TRAINING SUPPLEMENT POH-162-00-40-001 PAGE 9-02 PAGE REV. 0...
  • Page 173 SUPPLEMENT 9-S1...
  • Page 174 ALPHA Trainer LSA SECTION 9 Pilot Operating Handbook SUPPLEMENTS SECTION 9 – SUPPLEMENT 9-S1 TRAINING SUPPLEMENT TABLE OF CONTENTS PART SUBJECT PAGE NUMBER INTRODUCTION 9-S1-3 ENGINE START-UP 9-S1-3 TAXI 9-S1-3 TAKE OFF AND INITIAL CLIMB 9-S1-4 CLIMB 9-S1-4 CRUISE 9-S1-5...
  • Page 175 ALPHA Trainer LSA SECTION 9 Pilot Operating Handbook SUPPLEMENTS INTRODUCTION This chapter has been written to assist owners/pilots/instructors of ALPHA Trainer on their quest to learn how to safely and efficiently fly this aircraft in addition to the information already assembled in the rest of this POH. This section will cover most operations the aircraft offers in an order established in section Normal procedures and recommended speeds.
  • Page 176 ALPHA Trainer LSA SECTION 9 Pilot Operating Handbook SUPPLEMENTS some 2500 RPM as this will provide some airflow from the propeller to the radiators and the temperatures will not rise so quickly. Should you see en- gine temperatures exceed safe operational values, shut off the engine, point the aircraft’s nose into the wind and wait for the temperatures to reduce.
  • Page 177 ALPHA Trainer LSA SECTION 9 Pilot Operating Handbook SUPPLEMENTS CRUISE Make sure flaps are retracted. A comfortable cruise setting is 5300 engine RPM. Cruising fast, do not kick-in rudder for turns! Above 85 kts (160 km/h) the rud- der becomes almost insignificant in comparison to aileron deflections when it comes to making a turn.
  • Page 178 ALPHA Trainer LSA SECTION 9 Pilot Operating Handbook SUPPLEMENTS Before turning to base-leg, reduce power to idle and set flaps to 1st stage at 70 kts (130 km/h). Once out of the turn, reduce speed towards 60 kts (110 km/h). Power remains idle from the point of turning base all the way to touch- down.
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  • Page 182 Via Fratelli Rusjan, 26 34070 Savogna d’Isonzo (GO) Italia - EU t +39 3703207623 info@pipistrel.si www.pipistrel-aircraft.com Pipistrel Vertical Solutions d.o.o. Vipavska cesta 2 SI-5270 Ajdovščina Slovenija - EU t +386 5 366 38 73 f +386 5 366 12 63 info@pipistrel.si...

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