2015 EVEKTOR HARMONY

2015

EVEKTOR

HARMONY

New

IFR

2

Order NOW for 2015. GLOBAL AIRCRAFT - U.S EVEKTOR DEALER. The Harmony LSA is setting a new standard in flight training and travel comfort. The Harmony LSA is continuation of the worldwide successful SportStar - the first S-LSA certified in the USA - and brings further performance and comfort enhancements. Elegant sporty look, tapered wing and great performance Tapered wing & HTU, prolonged fuselage and sleek lines from prop to tail express elegant and sporty look of the new Harmony LSA and together with aerodynamic optimization bring further enhancement of performance parameters. Superb cockpit comfort & spaciousness Amazing cockpit spaciousness providing 46.5' shoulder room and extra leg room for tall and large pilots, sporty high seats and optimized cockpit ergonomic bring superb cockpit comfort for your long cross country flights. Excellent strength & reliability proven in flight school operations The new Harmony LSA has origin in Evektor´s EASA JAR-VLA certified pilot training airplane. Excellent strength and operation reliability of the Harmony LSA have been proven in flight schools operations worldwide. GA quality from EASA, LAMA and ISO 9001 certified manufacturer Uncompromising build quality of the Harmony LSA is based on Evektor´s certified aircraft production by EASA (European Aviation Safety Agency), LAMA and ISO 9001:2008 Quality Management System. This means the airplane is assembled according to the very best of aviation standards. Advanced airframe The Harmony LSA has a robust all metal anodized and corrosion-proofed aluminum airframe which delivers significantly more durability and longer service life than most of the airplanes in the category. As all the SportStar line, also the Harmony has metal airframe with all joints of construction riveted as well as bonded for high durability and long fatigue life. All heads of pop rivets are sealed with mastic for further enhancement of durability of riveted joints. Such build provides also better crash characteristics and smoother and quitter flight because drumming and flexing are absent. Using composite parts for enhancement of aerodynamic cleanness of the airplane is limited just to non-structural parts of construction. Technical data Dimensions & Performance Dimensions Length 20 ft 6.11 m Height 8 ft 2" 2.48 m Wing span 30 ft 4" 9.25 m Cabin width 46 1/2" 1.18 m Baggage compartment volume 10.1 cu.ft 285 l Weight & Quantities Useful load 634 lb 289 kg Max take-off weight 1320 lb 600 kg Empty weight (standard a/c) 686 lb 311 kg Max. baggage 55 lb 25 kg Design load factors +6 / -3 g +6 / - 3 g Operation load factors +4 / -2 g +4 / - 2 g Wing tank capacity 31.7 USgal 120 l Flight performance Rotax 912 ULS Rotax 912 ULS (100 HP) (100 HP) Never exceed speed 146 kts 270 km/h Maximum level speed 120 kts 222km/h Cruising speed 110 kts 212 km/h Stall speed VS1 45 kts 83 km/h Stall speed VS0 (full flaps) 40 kts 74 km/h Rate of climb 1 020 ft / min 5.2 m/s Service ceiling 15 500 ft 4 720 m Take-off run (concrete RWY) 620 ft 190 m Landing run (concrete RWY) 590 ft 180 m Range 700 nm 1 300 km Under ISA conditions. All information can change without prior notice.

Engine instruments RPM indicator Cylinder head temperature indicator (°C or °F) Electric fuel indicator Oil temperature indicator (°C or °F) Oil pressure indicator (MPa or psi) Firewall forward Rotax 912 ULS (100 HP inclusive slip clutch and Airbox) optional engines: Rotax 914UL2 Turbo (115 hp), Rotax 912iS (100 hp) Propeller Propuls AES 1700/3/R, composite, ground adjustable, spinner 12 V battery Exhaust system Combined engine cooling Dry sump forced engine lubrication Two spark electronic ignition system Electric starter AC generator Engine oil check cup

Controls Dual hydraulic brakes (4 pumps) Dual control sticks Mechanical flaps Longitudinal, lateral, flaps and nose wheel control through push / pull rods Throttle control with friction lock Adjustable pedals New design of instrument panel Press-button circuit breaker Nose wheel steering Combined starting switch Choke lever

Flights instruments Air speed indicator (knots or km/h) Altimeter (feet or m) Magnetic compass Vertical speed indicator (ft/min or m/s) Bank ndicator

Advanced all metal anodised and corrosion-proofed airframe All joints of construction riveted as well as bonded for long service life All heads of pop rivets filled with mastic for longevity of riveted joints White colour painting Tricycle landing gear with steerable nose wheel Main Tires 15x6 Nose Tire 15x6 Tinted canopy with UV protection Automotive type latching mechanism with separate canopy lock Integral wing tanks 120 l (2x 60 l) Vortex generators on the wings for US market

Ventilation system with NACA inlets and canopy side eye-ball vents Standard seats with low back rests De luxe lined interior Four points seat belts Padded seat belt shoulder straps Side map pockets Arm rests Aft baggage compartment with luggage nets „Open / Closed" canopy alert 12 volt auxiliary outlet