Easy to fly, affordable, and very durable CONTACT: Walter Janner Ebnit Dornbirn Austria / Europe

Transcription

1 ZENITH STOL CH-801 SN: Easy to fly, affordable, and very durable CONTACT: Walter Janner Ebnit Dornbirn Austria / Europe info@flyingcircus.at Phone: +43-(0)664/

2 Zenith STOL CH 801 With form following function, the STOL CH 801 looks like the workhorse it is designed to be. Not designed to be just another pretty aircraft, the STOL CH 801 was developed to provide maximum short-field performance while being easy to maintain, making in a true sport utility kit aircraft. The STOL CH 801 design is based on the successful STOL CH 701 kit aircraft design, originally introduced in Aeronautical engineer Chris Heintz designed the STOL CH 801 to provide the best in performance, cost, reliability and ease of construction in a four- seat utility light aircraft design. The unique design presents some highly engineered and researched features. The STOL CH 801 design makes use of advanced technologies, while using proven design concepts and simple systems for easy maintenance. A professional design, the STOL CH 801's structure is undergoing a complete and rigorous flight test and design stress analysis. Developed for the inexperienced demanding pilot, the STOL CH 801 is designed to maximize flight performance and efficiency, using simple all-metal semi-monocoque construction - a system in use for 25 years in Zenair designs. Simple systems, modern materials, and design ingenuity minimize required maintenance, and make the STOL CH 801 easy to fly, affordable, and very durable. WING DESIGN: The STOL CH 801 uses a special airfoil design to achieve very high lift, low stall speeds, and high strength. A thick wing, full-length leading-edge slats and trailing edge "Junker" type ailerons develop a maximum wing lift coefficient of 3.10, while maintaining a short wing-span of less than 31 feet. For maximum reliability and to keep construction simple, the leading edge slats are engineered to remain in a fixed position in all flight attitudes and do not retract. TAIL DESIGN: The STOL CH 801 has an all-moving rudder tail section to provide effective and responsive rudder control, especially at low speeds. The horizontal tail features a unique inverted stabilizer to achieve adequate negative lift for sustained high angle of attack climb attitudes. The STOL CH 801's large effective control surfaces provide excellent controllability at very low flying speeds - a necessity for effective short take-off and landing performance - while being very light and balanced. CONTROL SYSTEM: The control system is developed for ease of operation and simplicity, as well as low maintenance: There are no moving parts inside the wings, and controls systems are easily accessed through a large service door on the bottom of the fuselage. Aileron Elevator Rudder Steering Aileron system; push-pull rods, easy to disconnect for wing removal. Control cables to elevator control horns. Control cables from rudder pedals to rudder control horn. Direct linkage from dual rudder pedals to nosegear strut (hydraulic disk brakes on main gear is with individual toe-brake pedals on pilot s side). LANDING GEAR: The stock tricycle gear system used on the STOL CH 801 has outstanding shock absorbing capability for rough field operation. While tailwheel aircraft have traditionally dominated in off-airport applications, the STOL CH 801's tricycle gear offers rough field capability while providing all the advantages of a tricycle-gear aircraft, such as easy ground handling and superior visibility. The STOL CH 801's gear has been developed specifically for off-airport use. The direct linkage steerable nosewheel, plus differential breaking, provide remarkably precise ground handling and steering. FUEL SYSTEM: The STOL CH 801 is equipped with 4 x 15 US gallons (56 liters) for a total fuel capacity of 60 gallons (224 liters). The welded aluminum wing fuel tanks are located inside the wing behind the main wing spar.

3 SPECIFICATIONS Aircraft Specification: Installed Additional Equipment & Parts: Airspeed Indicator (KTS/MPH) Cabin Heat Attitude Gyro (Vacuum) Fresh Air Ventilation Altimeter ( ft) External Power Port Turn Coordinator (Electric) 2 Additional Wing Fuel Tanks Directional Gyro (Vacuum) Position Light Vertical Speed Indicator (2000 ft) Strobe Light Suction Gage 1 Taxi & Landing Lights Transceiver (Becker AR 4201) Stall Warning Device Intercom 403 MC (for front Pilots Vortex Generators (for even a higher AOA) and rear Passengers) Handheld ICOM / Transceiver incl. Antenna Loudspeaker (Becker1PL042) Tire Pressure Monitoring System (Wireless) Mode S Transponder [Becker BXP (XX)] Trickle Charger incl. External Plug for Wintertime Blindencoder Becker BE (XX) Parking Brake Magnetic Compass Maintenance Free Teflon Fuel Lines Alcor Basic EGT System 12 Volt Power Plug / Cockpit Mechanical Tachometer IPAD Mount for Navigation & Flightplanning Mitchel 6 Gauge Cluster - Oil Pressure - Oil Temperatur Engine: - Fuel Pressure - Volt Meter Lycoming O-360A4M (Brand New with Kit) - Ammeter 75 A Quick Oil Drain - Cylinder Heat Temperatur Termo-Tec Exhaust Wrap Mechanical Accelorometer ( G Meter) Aviator s Flight Timer Scott Free Air Termometer Propeller: Aerospace Logic Inc. ASL-FL100 Fuel Gage (2 Qty.) NAVMAN FUEL 2100 (Fuel Flow Gages) Sensenich 76-EM (Brand New with Kit) Hobbs Hour Meter Essex Primer Carbon Monoxid Detector MAC Trim System Klixon 7277 Circuit Braker Toggle Switches ELT - Artex ME 406 MHZ Fire Extinguisher (HAL 1)

4 INTERIOR Leather for the Interior Carpet for the Interior The Leather was used on all sides and on the top of the inside of the cockpit and cabin. The Carpet was used on the floor and on the side of the food areas.

5 EXTERIOR The complete parts from the Zenith/Janner STOL CH801 was first primed with Zinc Chromate to make it very durable. The complete airframe was sprayed from a professional paint shop. The color range is from a dark blue on the front to a very bright blue to the rear of the aircraft.

6 The following performance and specification figures are based on the production prototype STOL CH 801 equipped with the Lycoming O-360-A engine (180 BHP: 400 lbs. with accessories and fixed-pitch Sensenich 76-EM Metal Propeller). SPECIFICATIONS STOL CH 801 LENGTH 24 Ft. 6 In. 7.5 m. HEIGHT 10 Ft. 0 In. 3.0 m. WING SPAN 31 Ft. 4 In m. WING AREA 167 SQ.FT m.sq. WING CHORD 5 Ft. 3 In. 1.6 m. HORIZONTAL TAIL SPAN 8 Ft. 4 In m. HORIZONTAL TAIL AREA 25 SQ.FT. 2.7 m.sq.. EMPTY WEIGHT 1,3710 LBS. 622 kg. DESIGN GROSS WEIGHT 2,150 LBS. 975 kg. USEFUL LOAD 779 LBS. 353 kg. FUEL CAPACITY (Extended Range Option) - Fuel weight (Extended Range Option) 60 Gal. (4 x 15) = 352 LBS. 224 l. (4 x 56) = 160 kg. WING LOADING 12.9 LBS/FT² 62.9 kg/m² POWER LOADING LBS/BHP 5.44 kg/bhp CABIN WIDTH 44 INCHES 112 cm. CABIN LENGTH 78 INCHES 198 cm. DESIGN LIMITATIONS: POWER BHP. MAX. INSTALLED POWERPLANT WEIGHT 440 lbs. 200 kg. MAX. TAKE-OFF WEIGHT (MTOW) 2,200 lbs. 998 kg. DESIGN LOAD FACTOR 2,200 lbs , MAX. WING LOADING (@ 2,200 lbs.) 13.2 PSF 64.4 kg/m² MAX. CRUISE SPEED - VC 120 MPH 193 km/h NEVER EXCEED SPEED (VNE) 150 MPH 240 km/h PERFORMANCE Lycoming O-360, 180-hp Typical Load: 500 Lbs 1,650 Lbs. Gross Weight 2,150 Lbs. TAKE-OFF ROLL 290 Ft. 88 m. 390 Ft. 119 m. MAX LEVEL SPEED 112 MPH 181 km/h 110 MPH 178 km/h CRUISE SPEED (75% 7,000 Ft.) 106 MPH 170 km/h 105 MPH 169 km/h STALL SPEED 43 MPH 69 km/h 48 MPH 77 km/h RATE OF CLIMB 1,200 FPM 6.1 m/s 720 FPM 3.7 m/s SERVICE CEILING 16,000+ 4,875+ m. 14,000 Ft 4,267 m. ENDURANCE (Extended Range 6.0 Hrs. 6.0 Hrs. RANGE (Standard) 320 Miles 515 km. 315 Miles 507 km. RANGE (Extended Range Option) 640 Miles 1,030 km. 630 Miles 1,015 km. Above performance figures with the Lycoming O-360-A engine (180 BHP: 400 lbs. with accessories and fixed-pitch Sensenich 76-EM metal propeller). Standard atmosphere, sea level, no wind. All technical data, specification and performance figures subject to change without notice.

7 ZENITH STOL CH 801 /ON DESCENT AFTER SKYWRITING LEFT INSTRUMENT PENAL OF CH 801

8 RIGHT INSTRUMENT PANAL OF CH 801 VORTEX GENERATORS ON TAIL FOR EVEN LOWER STALL SPEED S

9 FINE COLOR IN COLLOR LEADER INTERIOR OF CH 801

10 REAR PASSANGER / CARGO AREA OF CH 801 / SMOKE SYSTEM

11 PRICE: Make offer!