The P92 Echo Classic is a
two-seat, single strut braced high wing aircraft.
The P92 Echo Classic was designed and manufactured according to the
international
airworthness standards. This has been accomplised by one of the most renowed
European Designers in the general aviation field,
with the aid of modern planning insturments.
The P92's performance and flying qualities are so superiour that it compares to
aircraft Certified under FAR/CS 23.
ADVANTAGES:
* Superior performance and flight characteristics
* 205 km/h (100 kts) cruise speed
* stable and responsive
* ideal for flight schools
* Excellent visibility
SPECIFICATIONS:
|
Design Weight & Loading |
||
| Designed MTOW | 600 KG | 1320 LB |
| Limit loads | +4 / -2 G | |
| Ultimate loads | +6 / -3 G | |
| Baggage Allowance | 20 KG | 44 LB |
|
Dimension |
||
| Wing Span | 9,4 m³ | 30,8 IN³ |
| Length Over-all | 6,5 m | 21,3 IN |
| Height Over-all | 2,5 m | 8,2 IN |
| Width Cabin | 1,1 m | 3,6 IN |
| Wing Area | 13,4 m³ | 144 SQFT |
| Transv. Dihedral | 1,5° | |
| Tailplane Span | 2,9 m | 9,5 IN |
| Wheel Track | 1,8 m | 5,9 IN |
| Wheel Tyres | AIR TRAC 5.00-5 (Main Gear) | |
| Engine and Propeller | Rotax 100 HP | Rotax 80 HP |
| Power Max@580M0 Rinpumte (Sm) Ax.5 | 73,5 KW (98,5 HP) | 59,6 KW (80 HP) |
| Reduction | 2,4286:1 | 2,273:1 |
| Propeller | GT Tonini | |
| Fuel | Auto fuel: min. RON 95 (AKI 91 Premium USA) / AVGAS: 100LL | |
| Tanks | 45 x 2 liters | 11,8 x 2 GAL |
| Performance | 100 HP | 80 HP |
| Max Speed S/L | 230 KM/H - 124 KTS | 219 KM/H - 117 KTS |
| Cruise speed 75% 5250 RPM | 205 KM/H - 110 KTS | 190 KM/H - 102 KTS |
| Vne | 260 KM/H - 140 KTS | |
| Rate of climb | 6,2 M/sec - 1220 FT/Min | 6 KM/H - 1180 FT/MIN |
| Stalling Speed (with Flap) | 64 KM/H - 34,5 KTS | |
| Service Celling | 4500 M - 15000 FT | 4000 M - 13000 FT |
| Max Range (without reserve) 65% | 750 KM - 466 N.M. | 720 KM - 447 N.M. |
| Take Off Run & Landing Run | 100 M - 328 FT | 110 M - 360 FT |
| Construction | Interior |
|
* The tecnam line
employs a monocoque tail cone with sheet aluminium over steel tubing * The wing is an all aluminium conventional structure with a single strut * The fuel tanks hold 11,9 gal/45 L each, located in the wing leading edge separated from the fuselage for safety. * A wide rear window together with large side windows complete the extraodinary visibility allowing 360° of vision in the cockpit. * The all moving Stabilator is fitted with a trim tab controlled by buttons on the control column. * The excellent flying charateristic with neutral handling makes it extremely stable and easy to fly for people of any weight/height. * The large flaps are deployed electrically * The low stall speed and the general slow flying characteristics of the aircraft allo it to operate on short runways. |
* Seats
are adjustable and increase in height as they are moved forward. |
| Landing Gear | Engine and Propeller |
|
* The main landing gear
legs are made of spring steel, directly connected to the main
structure. The landing gear is robust enough for rough strips and
requires no maintenance. * The trailing link nose gear uses a rubber shock absorber system that was designed for the rigours of the training environment with easy and economical maintenance. * The main landing gear wheels and brakes are conventional aircraft size (5.00 x 5) * The brake lever control and the parking brake are located forward between the seats. |
* The top and bottom
engine cowls are quickly and easily removable making any maintenance
easier to accomplish. The top cowl has 2 large hinged openings for
easy acces to the engine compartement, without the need for tools to
allow effective pre-flight inspections. * The engine's mount is steel-tubing with shock mounts. It also supports the nosewheel that is not anchored directly to the cabin's structure. * Two powerplant options are available: Rotax 912 UL 80 HP four-cylinder, four-stroke engine and Rotax 912 ULS 100 HP four-cylinder, four-stroke engine. Both engines come withan integrated 1:2.4286 Reduction. * A fixed pitch wood and composite propeller comes as standard. * The quick drain gascolator is installed in the engine compartement with eeasy outside access. * The fuel system uses a mechanical engine driven pump along with an electrical backup pump. * The battery is easily accesible through a hinged door in the rear fuselage. |
| Flight instruments and indicators | Electrical Flaps | Fuel Quick Drain | Cabin Confort System |
| Magnetic compass | Dual Flight controls | Interior | Ventilator Adjustable, 2 place |
| Airspeed ind., Kts | Steerable Nose Wheel | Pilot and copilot seats: | Powerplant and propeller |
| Altimeter (ln) | Stabilator trim (between seats) | Adjustable for and aft-Arm Rest | Engines: |
| Vertical speed | Engine controls: | Seat belts & shoulder harness, all seats | 1 Rotax 912ULS2 80/100HP |
| Bank indicator | - Throttle, two | Wall to wall carpeting | 4 cylinders liquid/air colled, integrated |
| Flaps indicator | - Choke | Luggage compartement -Map pockets | Reduction Gear |
| Pitot system | Flight Trim controls: | Exterior | Dual Ignition System |
| Static system | - Stabilator with indicator | Sliding canopy with lock and key | Throttle control LH/RH |
| Stabilator Trim position indicator | Fuel control selector with on/off | Rear window | Tubular steel engine mount |
| Engine Instruments | Panel switches: | Tie down rings | Propeller |
| Tachometer | - Starter | Main wheels 5.00 x 5 | GT Propeller, 2 blade fix |
| Hour recorder | - Engine Lh + Rh ignition switches | Nose wheel 4.00 x 6 | Propeller Spinner |
| Oil press | Exterior | Air filter | |
| Oil temp | Electrical system | Rear Window | Oil filter |
| Head temp | 12 volt 18 Amp. battery | Tie Down Rings | Oil and water coolers |
| Lh + Rh Fuel Qty | 12 volt alternator 20 Amp. | Main Wheels, 5,00 x 5 | |
| Switches: landing light | Nose Wheel, 4,00 x 6 | ||
| Circuit fuses panel | Wheel pants | Product Support/Docs | |
| Flight Controls | Fuel System | Manufactures full 2 year limited warranty | |
| Hydraulic brakes | Two integral tanks with 90 L capacity | Pilots operation handbook | |
| Parking brake | Engine driven fuel pump | Maintenance manual |