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Serial Number
Manufacturer:
Address:
S.P. 16 km 15,150
Castelnuovo Don Bosco (AT)
ITALY
14022
The technical data and the information embodied therein are property of I.C.P. Srl and shall not be
disclosed in whole or in part to third parties, without prior written permission of I.C.P. Srl. The manual
must remain with the aircraft in case of sale.
SERIAL NUMBER:
YY-MM-62-XXXX-Z
VENTURA
Ultralight Aircraft
Pilot's Operating Handbook
YY-MM-62-XXXX-Z
ICP S.r.l.
FIRST ISSUE: 04/05/2018
REVISION 00: 04/05/2018
TM
Contacts:
Phone:
Fax:
Web:
Email:
NOT CONTROLLED COPY
VENTURA-POH-ENG
Rev. 00
Year 20YY
+39 011 9927503
+39 011 9927266
www.icp.it
info@icp.it
PAGE: 1/60
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Summary of Contents for ICP VENTURA YY-MM-62 Series
- Page 1 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Serial Number YY-MM-62-XXXX-Z Year 20YY Manufacturer: ICP S.r.l. Address: Contacts: S.P. 16 km 15,150 Phone: +39 011 9927503 Castelnuovo Don Bosco (AT) Fax: +39 011 9927266 ITALY Web: www.icp.it 14022 Email: info@icp.it...
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Page 3: Table Of Contents
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook SUMMARY GENERAL INFORMATION ....................7 1.1. CERTIFICATION CRITERIA ..................... 8 1.2. WARNING, CAUTION AND NOTE DEFINITIONS ............9 1.3. SYMBOLS, ABBREVIATIONS AND GLOSSARY ............. 9 1.4. UNIT CONVERSION TABLE ..................10 1.5. - Page 4 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook WEIGHT AND BALANCE ....................31 4.1. LIST OF STANDARD COMPONENTS INSTALLED ............31 4.2. WIGHT AND EMPTY BALANCE DETERMINATION ............32 4.3. PRE-FLIGHT WEIGHT AND BALANCE TABLE ............. 33 PERFORMANCES ......................37 5.1.
- Page 5 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 7.8. ENGINE STOP ....................... 53 7.9. PARKING / TYING-DONW ..................... 53 GROUND MANEUVERS AND SERVICE PROCESURES ..........55 8.1. TOWING / AIRCRAFT HANDLING ................. 55 8.2. AIRCRAFT GROUND MOORING ................... 55 8.3.
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Page 7: General Information
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 1. GENERAL INFORMATION The aircraft to which this manual refers is intended for recreational or tourism flying and for flight school purposes too. This ultralight aircraft can be used for aerial work only where permitted. This Pilot’s Operating Handbook provides information useful for the safe and efficient operation of Ventura aircraft. -
Page 8: Certification Criteria
Since the Italian regulations do not provide detailed design standards, construction and maintenance program of the ultralight, ICP Srl has chosen to follow the EASA CS-VLA technical specifications with the purpose of assuring flight safety. -
Page 9: Warning, Caution And Note Definitions
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 1.2. WARNING, CAUTION AND NOTE DEFINITIONS The following definitions are applied to “warning”, “caution” and “note” in the Pilot’s Operating Handbook. WARNING WARNING MEANS THAT NON- OBSERVATION CORRESPONDING PROCEDURE (PRACTICE, STATEMENT, FLIGHT BEHAVIOR, ETC...) LEADS TO AN IMMEDIATE OR IMPORTANT DEGRADATION OF THE FLIGHT SAFETY, EVEN INCLUDED PERSONAL INJURY... -
Page 10: Unit Conversion Table
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Stall speed (clean): minimum speed at which the aircraft can be maintained in level flight with the flaps retracted. Indicated by lower green arc limit on the airspeed indicator. Minimum speed at which the aircraft can be maintained in level flight with the flaps extended. -
Page 11: Installed Optional / Additional Equipment
THE “DOCUMENTATION” SECTION; ICP Srl ALSO RECOMMEND CONTACTING THE OFFICIAL ROTAX DEALER IN YOUR COUNTRY FOR ANY OTHER DETAIL. ICP Srl DOES NOT TAKE ANY RESPONSIBILITY FOR ANY DAMAGE TO PEOPLE AND/OR PROPERTY DUE TO FAILURES IN APPLYING ROTAX INSTRUCTIONS. -
Page 12: Cooling System
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 2.1. COOLING SYSTEM The engine is cooled by air, water and oil (mainly used as a lubricant) systems. The engine is equipped with water and oil radiators. Air intakes on the engine cowling ensure the correct air distribution around cylinders and radiators. -
Page 13: Fuel System
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 2.4. FUEL SYSTEM The fuel is contained in two 36 liter each plastic tanks, 72 liters in total, located in the half-wing in the first compartments behind the main spar and rear spar. The tanks are equipped with at sight level indicator and are ventilated by a vent pipe placed on the cap and a further ventilation which connects the tanks between the two wings. - Page 14 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Figure 1: Fuel system, firewall backward Figure 2: Fuel System, firewall forward SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 14/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY...
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Page 15: Structure
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Approved fuel types: MOGAS 912 UL/A/F 912 ULS / iS / 914 UL / 915iS EN 228 Normal European standard EN 228 Super EN 228 Super EN 228 Super plus EN 228 Super plus CAN/CGSB-3.5 CAN/CGSB-3.5 Canadian standard... -
Page 16: Landing Gear
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook The wing has a Riblett GA35A-418 profile with Junkers type flaperons that guarantee lateral controllability even at low speeds. In order to reduce stall speed, plastic vortex generators are applied to the nose of the wing. The wing has a rectangular plan, is not twisted and has a dihedral angle. The wing structure is made up of spars, ribs and coverings, all in aluminum alloy AL 6061 T6. -
Page 17: Flight Controls
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 2.7. FLIGHT CONTROLS The aircraft is equipped with single "Y" stick (double stick available as optional) and double rudder pedals. Pitch control The elevator is moved by a Ø 3.2 mm steel cable system, the tension of the cables is adjustable through a special register reachable through the inspection trapdoor located on the bottom of the rear fuselage. -
Page 18: Electrical System
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Hot Air Control for Airbox (standard on Rotax 912ULS/iS, 914UL and 915iS, optional on Rotax 912 UL); Auxiliary electric fuel pump; On/off fuel valve, placed on the floor; Magnetos Key switch 1 and 2; Master switch that connects the electrical system to the 12V battery. - Page 19 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Figure 3: Electrical system, firewall backward SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 19/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY...
- Page 20 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Figure 4: Electrical System, firewall forward Electrical system and standard panel layout in Rotax 914UL and Rotax 912iS/915iS engine installations are different. Refer to the engine installation or operator manual and/or Technical Specification for detailed scheme and configuration of the system.
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Page 21: Cabin And Instruments
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 2.9. CABIN AND INSTRUMENTS Doors Doors are locked by a central lock handle. Locked position in forward direction. WARNING DOORS AND SUPPORTING HINGES ARE NOT DESIGNED TO BE KEPT OPEN DURING THE FLIGHT. - Page 22 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Ventilation / Heating Two ventilation doors are placed in the side of front cabin compartment. Two rods located under the side of instrument panel can control the ventilation flow. Heating valve is moved by a panel-mounted lever that controls the inflow of hot air coming from the engine compartment.
- Page 23 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook WARNING INSTRUMENTS INSTALLED CERTIFIED ACCORDING TO AERONAUTICAL STANDARDS. THE INDICATIONS MAY HAVE A NON-NEGLIGIBLE ERROR. Fuel quantity and reserve indicator Fuel quantity on board is visible on the level indicators placed on the root rib of the wings. These indicators consist of a transparent pipe connected to the tank.
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Page 24: Technical Specifications
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 2.10. TECHNICAL SPECIFICATIONS Fuel system Fuel capacity 2 x 36 lt Collector tank (Nourice) Lubrication Type Engine driven oil pump Capacity Cooling Type Air-water-oil Liquid capacity 3.3/3.5 lt Electrical system Battery Minimum 9 Ah Generator 250 W... - Page 25 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Nose gear suspension Rubber pads Main gear suspension 7075 aluminium leaf spring Steering Front steerable wheel Wheels 6” x 4” (6” x 6” or Tundra, as optional) Inflation pressure 1.4 ÷ 1.6 bar for 6” and Tundra, 2.0 ÷ 2.5 bar for 4” Brakes Hydraulic disc brake Roadway...
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Page 26: Three-View Drawing
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 2.11. THREE-VIEW DRAWING Figure 5: Ventura Three view SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 26/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY... -
Page 27: Operating Limitations
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 3. OPERATING LIMITATIONS This chapter includes operating limitations of the aircraft, also reported on flight instruments with markings or listed in special cabin placards. The limits below must be respected, exceeding the limits could result in structural failures or endanger the crew. -
Page 28: Design Load Factors
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 3.6. DESIGN LOAD FACTORS Limit load factor at 600 Kg (1320 lbs): Retracted flaps +4.0 g / -2.0 g Extended flaps +2.0 g / 0 Safety factor for the ultimate load: 1.5. WARNING LOAD THE VENTURA MORE THAN 600 KG IT IS FORBIDDEN. -
Page 29: Weight And Balance Limitations
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook OIL PRESSURE 0.8 bar - 7 0.8 bar - 7 0.8 bar - 7 bar (12 (min - max) (12 psi - 102 psi) (12 psi - 102 psi) psi - 102 psi) PRESSURE 2.0 bar - 5.0 bar 2.0 bar - 5.0 bar... - Page 30 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Intentionally left blank SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 30/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY...
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Page 31: Weight And Balance
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 4. WEIGHT AND BALANCE The following paragraphs describe how to do the aircraft weighing and how to calculate the center of gravity position. WARNING IT IS THE PILOT'S RESPONSIBILITY TO VERIFY THAT THE TAKE-OFF CENTER OF GRAVITY IS WITHIN THE LIMITS SHOWN IN THE FOLLOWING CHAPTER. -
Page 32: Wight And Empty Balance Determination
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 4.2. WIGHT AND EMPTY BALANCE DETERMINATION Depending on the quantity of options and the configuration of the Ventura, there may be variations in the empty weight. It is necessary to perform this measurement before the first flight and whenever the configuration and the installed accessories are changed. -
Page 33: Pre-Flight Weight And Balance Table
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Figure 6: Ventura empty weighing and balancing scheme 4.3. PRE-FLIGHT WEIGHT AND BALANCE TABLE C.G. front limit: 19% +/- 0.9 % C.G. rear limit: 35% +/- 0.9 % The aircraft tolerates a wide variation of its center of gravity position, this facilitate the loading of the aircraft itself and its balancing. - Page 34 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Fill out the weight column by entering the values relating to the items actually boarded before the flight (Pilot, Passenger, Fuel, Baggage); Multiply the weight of each row for the related arm and write the value of the Moment in the third column;...
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Page 35: Tm W&B [Kg X M]
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Figure 7: Ventura W&B [kg x m] Figure 8: Ventura W&B [lbs x ft] SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 35/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY... - Page 36 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Intentionally left blank SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 36/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY...
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Page 37: Performances
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 5. PERFORMANCES This paragraph gives information regarding take-off, climb, cruising and landing performances. All the speeds shown are indicated on the airspeed (IAS). WARNING AIRCRAFT PERFORMANCES ARE INFLUENCED BY WEATHER CONDITIONS AND ALTITUDE (TEMPERATURE AND HUMIDITY). -
Page 38: Rate Of Climb (Rotax 912Uls)
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 5.1. RATE OF CLIMB (ROTAX 912ULS) Best rate of climb speed V Weight 992 Lbs / 450 kg 1320 Lbs / 600 kg Speed Vy 63 Mph / 100 km/h / 54 kt 73 Mph / 118 km/h / 64 kt Best angle of climb speed V Weight... -
Page 39: Stall Speed
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 5.3. STALL SPEED WARNING THE SPEEDS SHOWN IN THE TABLE ARE SPEEDS INDICATED AIRSPEEDS (IAS). Mass 992 Lbs / 450 kg 1320 Lbs / 600 kg Retracted Flaps 41 Mph / 65 km/h / 35 kt 47 Mph / 75 km/h / 41 kt Flaps 1/2 38 Mph / 61 km/h / 33 kt... -
Page 40: Fuel Consumption
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 5.5. FUEL CONSUMPTION The following table shows the fuel consumption referred to the standard atmosphere condition (ISA) at sea level. Performance 912UL 912ULS 912iS 914UL Take-off 24 lt/h 27 lt/h 26.1 lt/h 33 lt/h Maximum continuous power 22.6 lt/h... -
Page 41: Emergency Procedures
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 6. EMERGENCY PROCEDURES This chapter provides checklist and amplified procedures for coping with emergencies that may occur. Emergencies caused by aeroplane or engine malfunctions are extremely rare if proper pre- flight inspections and maintenance are practised properly. However, should an emergency arise, the basic guidelines described in this section should be considered and applied as necessary to correct the problem. -
Page 42: Engine Falure In Flight
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 6.3. ENGINE FALURE IN FLIGHT Set and maintain the best glide speed; Weight 992 Lbs / 450 kg 1320 Lbs / 600 kg Best Glide speed 63 Mph / 100 km/h / 54 kt 73 Mph / 118 km/h / 64 kt FLAP retracted;... -
Page 43: Fire In Flight
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 6.4.2. FIRE IN FLIGHT Close the fuel shut-off valve; Set the maximum power; Electric fuel pump OFF; o When the engine stops; Magnetos OFF; Master switch OFF; Perform an emergency landing with the engine off. 6.5. -
Page 44: Emergency Landing With Engine Off
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook CAUTION WHEN THE BATTERY WILL BE DEAD, RADIO COMMUNICATIONS WILL NOT BE POSSIBLE. THE ENGINE CAN NOT BE RESTARTED. THE ELECTRICAL INSTRUMENTS WILL NOT BE AVAILABLE. 6.9. EMERGENCY LANDING WITH ENGINE OFF Maintain the maximum efficiency speed;... -
Page 45: Unintentional Spin Recovery
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 6.11. UNINTENTIONAL SPIN RECOVERY Apply full rudder on the side opposite the rotation and keep until the rotation stops; Apply slightly pitch down stick with centered ailerons; Engine to idle; o When the rotation stops; Return the aircraft in level flight and return engine. - Page 46 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Intentionally left blank SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 46/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY...
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Page 47: Normal Procedures
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 7. NORMAL PROCEDURES The procedures below provide a guide to flight preparation, execution and, moreover, provide a method to control the efficiency of the aircraft and its systems. The pilot must familiarize and fully understand these procedures. - Page 48 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Cooling system (water and glycol), CHECK for leakages or damages; Water cooler, CHECK; Coolant level, CHECK; Lubrication system (oil), CHECK for leakages or damages; Oil cooler, CHECK; WARNING BEFORE TURNING THE PROPELLER, CHECK MAGNETOS OFF.
- Page 49 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Rear fuselage Antennas, CHECK; Integrity of panels and static ports, CHECK; Inspection doors, CHECK present and closed (under the fuselage and near the tail); Tail tab surface, CHECK. Horizontal empennage ...
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Page 50: Engine Start
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 7.2. ENGINE START Pedals Brake, APPLY. Do not use the parking brake (optional); Choke, APPLY (not necessary with engine hot or if outside air temperature is above 15° C); Throttle, CLOSED (1 cm open with engine hot); Master switch, ON;... -
Page 51: Normal Take-Off
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook o Maximum difference 150 RPM; Oil pressure, CHECK rise in green arc within 10’’; Fuel pressure, CHECK. Flap ½, SET; Trim neutral, SET; Electric fuel pump, ON; Carburettor Heat, OFF; 7.5. NORMAL TAKE-OFF Communication, PERFORM if required;... -
Page 52: Short Take-Off / Soft Ground Runway
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 7.6. SHORT TAKE-OFF / SOFT GROUND RUNWAY Communication, PERFORM if required; Runway and Final, CHECK free; Flap Full, SET; Neutral Trim, SET; Electric fuel pump, ON; Carburettor heat, OFF; Throttle, push FULL power gradually to the maximum; Take-off RPM, CHECK min 5200;... -
Page 53: Engine Stop
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Full Flap, SET; Communication, PERFORM if required; Wind-cone, CHECK; Runway, CHECK free. Flaire, PERFORM; Brake, APPLY as required; Runway, VACATE. 7.8. ENGINE STOP Flaps, RETRACT; Electric fuel pump, OFF; Avionics and electrical switches, OFF; Throttle idle;... - Page 54 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Intentionally left blank SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 54/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY...
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Page 55: Ground Maneuvers And Service Procesures
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 8. GROUND MANEUVERS AND SERVICE PROCESURES 8.1. TOWING / AIRCRAFT HANDLING Before towing the aircraft, check MAGNETOS OFF and parking brake deactivated. Pull the aircraft out of the propeller. Never lift or pull the aircraft from the spinner. To move the airplane backward is possible to push from wing struts, on both side. -
Page 56: Aircraft Refueling
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook NOTE The aircraft is not watertight. Rain could enter from the roof or from the passages of the parachute straps. In case of rain cover the cabin. 8.3. AIRCRAFT REFUELING Check Master switch OFF and brake the aircraft with parking brake or wheel chocks. Connect the grounding cable to the aircraft exhaust pipe. -
Page 57: Labels And Indictions Required
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook 9. LABELS AND INDICTIONS REQUIRED 9.1. AIRSPEED INDICATOR MARKINGS SPEED SPEED RANGE SPEED RANGE MARKING RANGE NOTES [Km/h] [Kt] [Mph] White arc 41-81 67-130 36-70 Extended flaps Green arc 46-112 75-180 46-97 Normal Operating Range Manoeuvres... -
Page 58: Identification Plate
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook HEATING SYSTEM PULL TO OPEN 9.4. IDENTIFICATION PLATE The aircraft must have the identification plate attached with rivets on the right side of the rear fuselage, under the horizontal stabilizer. The main information is the Aircraft Serial Number, composed as follows: S/N code: YY-MM-Model-XXXX-Z Year of construction;... -
Page 59: List Of Revisions
VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook LIST OF REVISIONS The list of revisions is updated every time a revision is issued. The list of all the revisions made to the Pilot’s Operating Handbook since its issuance is summarized in the following table. - Page 60 VENTURA Ultralight Aircraft VENTURA-POH-ENG Rev. 00 Pilot’s Operating Handbook Intentionally left blank SERIAL NUMBER: FIRST ISSUE: 04/05/2018 PAGE: 60/60 YY-MM-62-XXXX-Z REVISION 00: 04/05/2018 NOT CONTROLLED COPY...