Brake Components
- – The Savannah™ S is a monoplane type, with two side-by-side seats, fitted with a high wing supported by struts. – The airframe structure is a full-metal one with load-resisting panels. – The wing presents a “high lift” NACA 650-18 modified airfoil with Junkers type flaperon (aileron + flap) with manual or electrical (optional) control.
- Flight Dynamics by D.G. New gauges by Dennis Seeley. The ICP Savannah is one of the top selling ultralights in Europe. It is dependable and easy to fly. Its STOL performance makes it easy to operate from any airfield. The Savannah is also a very good airplane for cross-country flights during which one can appreciate its great stability.
- The ICP Savannah S has the latest technology and the intergrating of all improvements introduced by the world renowned Savannah aircraft. The sporty controls, superior handling and super STOL performance allows you to fly to any destination, and more importantly, fly out of the shortest runways.
Savannah™VG FLIGHT MANUAL I.C.P. 17 FLIGHT CONTROLS Figure nr.3 Issue 1/Revision 03 ICP Srl – S.P.16 km 15,150 14022 Castelnuovo Don Bosco (AT) Jan.2012 Tel.
ICP Brake Calipers
New for 2003, we have totally redesigned our popular calipers to be even better than before, with a 36% weight reduction, and 50% increase in stiffness.
Icp Savannah Flight Manual Online
The new crossover bridge design allows us to make the maximum use of the minimum amount of material, and the optional “radial mount” feature will allow you to adapt this caliper to replace any of the popular calipers used in the past just by using the proper adapter bracket. Rotors of larger diameters or different thickness are easily accommodated.
All ICP calipers are cast using 80 kpsi tensile strength ductile cast iron – 20 kpsi stronger than our competitors. All body parts are Yellow Zinc plated for long lasting corrosion protection.
Pistons are machined from 304 Stainless Steel to a tolerance of .0002, and polished to a sub-20 micron finish. The use of stainless steel gives our pistons a heat insulating value nearly that of titanium, at a fraction of the cost.
Piston seals are custom made for us in Ethylene Propylene – one of the best brake caliper piston seal materials available.
All calipers incorporate 2 bleed screws – one per piston – for reliability in proper system bleeding. Fluid crossover passages are internal – no external pipes to break or leak.
All calipers are available set up for a variety of rotor thicknesses. Standard width for the LD20 is 3/8”. Special kits are available to upgrade your car to larger diameter rotors.
| Weights: | Standard ICP20 Leg or Radial mount for 3/8” rotor | 2.5 lbs (4.25 lbs less than AP LD20) |
| Narrowed for ¼” rotor | 2.4 lbs | |
| Radial mount LD65 replacement for .812 vented rotor, with bracket | 2.65 lbs (4.5 lbs less than the LD65) | |
| Radial mount replacement for Girling 14LF, with bracket | 2.45 lbs (4.5 lbs less than the Girling) | |
| Price: | Standard ICP20 Leg mount or Radial mount for 3/8” rotor | $200 each |
| Narrowed ICP20 Leg or Radial for 1/4” rotor | $200 each | |
| Girling 14LF replacement with bracket | $225 each | |
| LD65 .812 rotor replacement with bracket | $250 each |
ROUND IS COOL!!!!
The Savannah™ S is I.C.P.’s 2010 innovation. It was born from the wish to make the Savannah™ more refined and elegant and complete the aesthetical improvement process already started last year with the Savannah™ XL, whose front part fuselage was completely modified.
This year we have paid attention to the back side of the aircraft. We have left the wings unchanged, because they have always proved to be the key force of the Savannah™, above all in VG (vortex generators) version, thanks to the combination of the wide wing surface with the high lift profile.
The object of restyling 2010 has been the tail trunk; we have removed the corners, so the typical squared shape has been replaced by a sinuous bending that gives harmony and completeness to the whole aircraft, without taking away the well known features of solidity and safety.
The new Savannah™ S joins inside all the previous versions’ improvement:
The wings with vortex generators, that imply a cruise speed increase up to180 Km/h, without compromising the very low stalling speed
The cockpit wider dimensions, able to lodge comfortably also the taller pilots
The adjustable rudder pedals, standard or advanced position of 10 cm
The panoramic view thanks to the canopy and the doors fully transparent
Aerodynamic profiling improved thanks to the streamlined engine cowling and to the major slope of the windscreen
Wider and higher positioned instruments panel, to leave more space to the knees.
Description ↓
Structure
– The airframe structure is a full-metal one with load-resisting panels.
– The wing presents a “high lift” NACA 650-18 modified airfoil with Junkers type flaperon (aileron + flap) with manual or electrical (optional) control.
– Trim with electrical control on the elevator and with manual control on the rudder.
– It’s possible to install a parachute “Junkers 500” type.
– The tanks are installed into the wings and have 36 litres capacity each. They are communicating and flow into a collection sump, placed in the fuselage, provided with drain valve and with fuel reserve indicator connected to a push-to-test light.
Cockpit
– The cockpit is completely sound insulated and covered with upholstery or fitted carpet.
– For a better visibility, the doors and the roof are fully transparent.
– The cabin arrangement features two canvas or upholstery covered side-by-side seats.
– The luggage van, situated behind the seats and accessible during the flight, may contain up to 45 lbs (20 kilograms)
– The cabin’s ventilation is provided by an opening between the doors and the upper part of the cabin door frame. A dynamic air scoop intended to extract the cabin air is fitted at the bottom of the baggage compartment. It’s possible to improve the cabin ventilation by using two rotating air scoops in the doors windows.
– Heating system can be orientated on feet or on windshield with control on the dashboard.
– Cabin light.
Landing Gear
– The nose landing gear (in tri-cycle configuration) is fitted with a telescopic, elastic chord shock absorber, and is steerable in order to ease the taxiing.
– The hydraulic drum brakes are independent and operate on the main landing gear’s wheels.
Engine-propeller group
– On the upper cowling has been inserted a little door that allows an easy inspection of the oil level.
– It’s possible to choose between two different engines:
Rotax 912 UL 2 – 80 Hp with two-blade prop “Duc” with adjustable pitch on the ground;
Rotax 912 ULS 2 – 100 Hp with three-blade prop “Duc” with adjustable pitch on the ground;
– The nose is completed with a glass fiber spinner 260 mm diameter.
– The new ring engine mount, that supports the engine by the rear, makes possible to have less vibrations.
– The fuel system is provided with an additional electric pump shielded anti-heat.
Icp Savannah Flight Manual Pdf
Standard Instrumentation
Altimeter D. 3 1/8” with setting window
Variometer D. 3 1/8”
Compass
Sljp and skid indicator
Tachometer
Fuel pressure
Oil pressure
Oil temperature
Hourmeter
Voltmeter
External temperature indicator + airbox (for Rotax 912 ULS only)
Water temperature in front left engine head
Water temperature in back right engine head
Icp Savannah Flight Manuals
Aircraft Three View
Specifications
