P92 Echo Super   click photos for larger versions   Download your Echo Super PDF files     Go to bottom of page to see VIDEO P92 Echo Super at a Farm Strip, Cooma (2:00 min) Tecnam Australia thanks this Private Owner for his video contribution.   Go to bottom of page to see VIDEO P92 Echo Super, Switzerland; includes Engine Off landing (2:08 min) This video is courtesy of Sato International AG, Mellingham, Switzerland http://www.tecnamswiss.ch/   The P92 Echo Super is an evolution of the P-92 model, the result of further improvement of the A/C, drawing on the experience of prolonged and varied use of hundreds of P-92 aircraft flying in the most diverse environmental conditions, coupled with unrelenting research in aerodynamics, structures and systems. THE P92 ECHO SUPER ATTAINS NEW GOALS OF EXCELLENCE: With its 100 Hp engine (Rotax 912ULS), superior performance, dependable systems, sturdy structure, low maintenance cost and competitive pricing, the P92 ECHO SUPER is unrivaled by a/c in similar or even higher weight category. The advantage becomes even clearer when taking into account the great ease in piloting, servicing and repair. Main variations with respect to P92-S are as follows:   More spacious cabin High efficiency slotted flaps Larger instrument panel Reduced wing surface Contoured fuselage Improved soundproofing   The aerodynamic contour of the fuselage has been improved by eliminating live edges and streamlining the nose section. The traditional landing gear that has long-been a distinctive feature of the P-92 is unvaried with the exception of small modifications of the wheel fairings. The fuel system is made up of two metal fuel tanks with a total capacity of 90 litres. The two tanks are positioned, one each, in proximity of the inboard end of half-wing's leading edge and fuel gages are mounted on cockpit instrument panel. A standby electric fuel pump insures fuel supply for any given flight attitude in case of mechanical pump malfunction. The large flapped portion of the wingspan coupled with the increased efficiency of the lower hinged slotted flaps has permitted a reduction of the wing’s surface. The resulting increase in wing loading has, in turn, yielded better performance in turbulent air and greater maneuverability. Structural load factor is increased by a factor of one.     P92 Echo Super Specifications DIMENSIONS     Wing Span 8.7 m 28' 5" Length Over-all 6.34 m 20' 8" Height Over-all 2.5 m 8' 2" Cabin Width 1.2 m 3' 9" Wing Area 12 m² 129 sq ft Transverse Dihedral 1.5º 1.5º Tailplane Span 2.9 m 9' 5" Wheel Track 1.8 m 5' 9" ENGINE AND PROPELLER   Engine Rotax 912ULS Max Power at 5000rpm 100 Hp @ 5800rpm Reduction 2.4286 : 1 Propeller Bipala GT - 172/164 Fuel Unleaded or AvGas Tanks 90 lt (2x45) WEIGHT     Max Take-off Weight 550 kg 1212 lbs Basic Empty Weight 281 kg 619 lbs Ultimate Load Factor +6 -3 +6 -3 PERFORMANCE     Max Speed s/l 235 km/h 124 kts Cruising Speed 75% 215km/h 105 kts VNE 270 km/h 140 kts Rate of Climb 5.9 m/sec 1260 ft/min Stalling Speed 63km/h 33 kts Service Ceiling 4500 m 14800 ft Take off to 50' 100 m 328' Landing Run 100 m 328' VIDEO of Echo Super at a Farm Strip (2:00 min) Click PLAY button to start   VIDEO of Echo Super in Switzerland (2:08 min) Click PLAY button to start