Final Environmental Assessment for E-2/C-2 Field Carrier Landing Practice Operations at Emporia-Greensville Regional Airport, Greensville County, Virginia, and National Aeronautics and Space Administration Wallops Flight Facility, Accomack County, Virginia. ICP SrI - Via Torino 12, 14020 PIOVA' MASSAlA (AT) - lta1y Phone +39-0141-996503. Fax +39-0141-996506 1 I.C.P. SrI I Savannah'TMVG FLIGHT MANUAL I Pag.
The Ventura-4 is the latest in a prestigious series of aircrafts and is the result of extensive studies by the ICP R&D department aimed at satisfying the growing market demand for a larger aircraft with more space and a larger load capacity. All metal construction and manufactured with cutting edge industrial technologies. The Ventura-4 is a high wing aircraft that can accommodate engines with power ranging from 140 hp Turbo charged Rotax 915is to 180 hp Lycoming O-360
By virtue of the new wing with Riblett GA 35-418 airfoil, The Ventura-4 can approach for landing as slow as 50 mph at maximum weight and with its high propeller clearance, can operate from semi-prepared runways shorter than 250 meters with a large margin of safety. Combining such excellent STOL characteristics with high cruising speed and brilliant manoeuvrability with brisk roll response, the aircraft offers optimal performance in any situation giving the pilot full control and a lot of fun!
Space. Reliability. Performance. These are the buzz words of The Ventura-4
Details
- The Ventura 4 is a monoplane type, with 4 seats, fitted with a high wing supported by struts.
- All metal structure with load resisting panels.
- High lift GA 35 418 Aerofoil with Junkers type flaperon (aileron + flap) with electrical control.
- Trim with electrical control on the elevator and with manual control on the rudder.
- Wing fuel tanks with 2×36 litres capacity in each wing. The tanks are connected and flow into a 16ltr collection sump placed in the fuselage. A single drain valve at the bottom of the fuselage is provided for fuel sampling.
Details
- The two large removable lateral doors allow easy independent access to the cabin.
- The cockpit is insulated, has upholstery covered seats and a fitted carpet.
- Doors are fully transparent allowing good visibility.
- The cabin arrangement features two upholstery adjustable front seats and 2 rear upholstered seats.
- The luggage compartment situated behind the rear seats is accessible during the flight and can hold up to 45 lbs (20 kilograms).
- The cabin’s ventilation is provided by cabin adjustable air scoops on the side of the forward fuselage. A dynamic air scoop intended to extract the cabin air is fitted at the top of the baggage compartment.
- Heating system can be orientated on feet or on windshield with control on the dashboard.
- Cabin light.
Details
- Air speed indicator, 3 1/8” with coloured arcs.
- Altimeter, 3 1/8” with setting window.
- Vertical speed indicator, 3 1/8”.
- Magnetic Compass
- Slip and skid indicator
MGL iEfis Explorer Lite with the following functions:
- Full engine monitoring
- Moving Maps display
- Remote transponder compatible.
- 2 Axis auto pilot compatible.
- 6 pack back up instruments.
- Airspeed ribbon
- Altitude ribbon
- Barometric pressure reading
- Tachometer and Hobbs.
- Fuel level indicator
Details
- LENGTH – 7.3m
- HEIGHT – 2.7m
- VCRUISE – 120mph
- WING SPAN – 9M
- VSO STALL CLEAN – 40MPH
- STALL FULL FLAP – 38MPH
- WING CHORD – 1.5M
- VNE – 162MPH
- WING SURFACE- 13.5M2
- CLIMB RATE – 1500fpm (Rotax 915is/Airmaster Propeller)
- ASPECT RATIO- 6
- CABIN WIDTH – 1.16M
- FUEL CONSUMPTION – @5000RPM = 25LTR P/H (ROTAX 915is)
- EMPTY MASS – 400KG
- USEFULL LOAD = 400KG
- ENDURANCE – 6.4 HR TO EMPTY
- MTOW – 800KG
- TAKE OFF DISTANCE GRASS MSL – 150M
- LANDING DISTANCE GRASS MSL – 100M
- RANGE TO EMPTY – 768MILES
- FUEL CAPACITY 156LTRS
- MAX OP ALT – 23,000FT
- STRUCTURAL LOAD – +3.8/-1.5
- CROSS WIND LIMITATION – 30MPH
Details
PROPELLER – Airmaster 3 blade AP430CTF-WWR72B Electric Variable pitch, Constant Speed Feathering with panel mount controller OR AX Sport AX3R Electric variable pitch, constant speed with panel mount controller.
ENGINE –
- Rotax 915is 141hp (Turbo charged) with redundant electronic fuel injection and ignition or Rotax 914UL 115hp (Turbo charged) with dual carburettors and dual ignition and back up fuel pump.
STANDARD INSTRUMENT PANEL – Dual screen MGL 8.5in Explorer with dual battery back-up, full engine monitoring, moving maps GPS, digital 6 pack, remote transponder and Auto pilot compatible or Single screen CF2000 7in Efis with battery backup, full engine monitor and digital 6 pack together with analogue instrument backup and separate Garmin Aera 660 GPS.
RADIO – Dittle KRT2 + 4 place intercom
RUBBER BOOTS – For easy switch identification.
CONTROL COLUMN – Centre Y stick with Ray Allen G205 stick grip (PTT and elevator trim)
RUDDER PEDALS – Both sides with toe brakes.
FLAP CONTROL – Electric operated via panel toggle switch.
ELEVATOR TRIM – Electric operated via G205 stick grip.
THROTTLE FRICTION – Wicks A820 on both throttles.
PARK BRAKE – Panel mounted.
INTERIOR – Grey epoxy coated with upholstered baggage compartment and floor carpets or rubberised floor.
EXTERIOR AND INTERIOR PRIME AND PAINT – Spray painted with primer, painted with a standard two-tone design.
SEAT BELTS – Lap and shoulder harness for rear seats and car type belts for front seats.
LUGGAGE COMPARTMENT – Luggage compartment behind rear seats with 20kgs capacity.
BAGGAGE NET – Covers bag compartment opening.
DOORS – Gull wing type with snap vents in the windows.
TYRES & TUBES – Deli 15×6 with spats.
FUEL TANKS – 70Ltr tanks in each wing with locking caps with 16Ltr accumulator behind the seat for total of 156Ltr (6 hr endurance)
LEATHER BOOT – For centre control Y stick.
LIGHTS – LED landing light on left wing and interior cabin light.
Details
- Transponder + antenna
UPGRADES/OPTIONAL EXTRAS
- Auto pilot servos
- Custom paint & decals
- Wing tip strobes
- Tail strobe
- High-intensity landing light
Details
- The main landing gear is made up of a single piece aluminium alloy leaf leg.
- The nose landing gear is fitted with a high density rubber ring shock absorber and is steerable during taxiing.
- The Ventura is fitted with disc brakes, with independent left/right toe brakes for the pilot and co-pilot (optional).
- 4-stroke liquid/air-cooled engine with horizontally opposed cylinders
- Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
- Redundant electronic fuel injection and ignition
- Engine management system (EMS)
- Electric starter (12 or 24 volt)
- Propeller speed reduction gearbox
- Air intake system with intercooler
- Turbocharger with stainless steel exhaust
- TBO (Time between overhauls) 1,200 hours
- Service ceiling of 23,000 feet
104 Kw @ 5800rpm
Max Rpm – 5800
Bore – 84mm
Icp Savannah Flight Manual Pdf
Stroke – 61mm
Displacement – 1352cm3
Weight – 84.6kg-Engine with gearbox, turbocharger, intercooler, cooling air baffle, wiring harness, sensors, flange with overboost valve, air hoses, clamps, magneto valve block with hoses, ECU, fusebox with regulators, oil tank, exhaust system without fuel pumps assembly, radiator and oil cooler.
Icp Savannah Flight Manual
- 4 cylinder, with auto-waste gate control
- 4-stroke liquid-/air-cooled engine with opposed cylinders
- Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
- Two carburettors with dual electronic ignition
- Engine management system (EMS)
- Electric starter (12 or 24 volt)
- Propeller speed reduction gearbox
- Air intake system with intercooler
- Turbocharger with stainless steel exhaust
- TBO (Time between overhauls) 2,000 hours
- Service ceiling of 23,000 feet
84.5 Kw @ 5800rpm 115 HP
Max Rpm – 5800
Bore – 79.8mm
Stroke – 61mm
Displacement – 1211.2cm3
Weight – 64kg-Engine with gearbox, turbocharger, intercooler, cooling air baffle, wiring harness, sensors, flange with overboost valve, air hoses, clamps, magneto valve block with hoses, ECU, fusebox with regulators, oil tank, exhaust system without fuel pumps assembly, radiator and oil cooler.
The Savannah is a two seater high wing Light Sport Aircraft (LSA). The newly introduced Savannah to our fleet now enables us to further extend our array of flying courses, like the National Pilots License (NPL).
- Short field landing & take off
- NPL Training
- Hire & Fly
- Conversion to type
Used for initial training, this two seater aircraft has excellent handling qualities. The Savannah locally built here in East London is simple, robust and easy to fly. Offering flight training at a lower cost.
Capacity;
1 pilot + 1 passenger
Length:
6.6 m
Wingspan:
9 m
Height:
2.58 m
Empty weight:
320.3 kg
Useful load:
260 kg
Max All Up Weight:
560 kg
Max speed:
125 mph
Cruise speed:
90 mph
Stall speed:
30 mph
Range:
4.5 hrs