Apis/Bee

APIS/BEE technical data

Model Apis/Bee
Wing span (m) 14.97
Wing area (m2) 12.24
Aspect ratio 18.33
Fuselage length (m) 6.26
Overall height (m) 1.3
Empty weight (kg) 215
Single wing weight (kg) 40
Max. takeoff weight (kg) 322.5
Min. takeoff weight (kg) 250
Max. speed VNE (km/h) 220
Max. airspeed in rough air (km/h) 144
Max. airspeed in aero-tow (km/h) 144
Manouvering airspeed (km/h) 144
Max. speed with air-brakes (km/h) 220
Min. speed MTOW (km//h) 60
Airfoil type and ratio IMD 029
17.01 %
Best glide ratio @ 94 km/h 39
Min. sinking rate @ 84 km/h (m/s) 0.59
G load limits +5.3 -2.65
Best climb rate 2 m/sec

BASIC PRICE INCLUDES:

14.97 M WING-SPAN TAIL-WHEEL SINGLE SEATER UL CLASS GLIDER WITH INTEGRATED WINGLETS, T - TAIL
READY TO FLY, TEST FLOWN
INTEGRAL INNER-SHELL BONDED TO FUSELAGE SHELL - SAFETY COCKPIT CONCEPT
OUTSIDE SURFACES IN WHITE, CABINE INTERIOR IN GREY
ACRYLIC PAINT, FINISHING AND POLISHING OF JOINTS ON ALL PLASTIC PARTS
LIGHT CABIN UPHOLSTERY IN BLUE COLOUR WITH LARGE SIDE POCKETS
IN-FLIGHT ADJUSTABLE BACKREST WITH HEADREST
4 POINT SEAT BELTS WITH AUTOMATIC CLOSURE
SLIDING AIR VENT WINDOW
DEFOGGING SYSTEM FOR CANOPY
ADJUSTABLE CABIN FRESH AIR VENT SYSTEM
MIRROR ON INSTRUMENT PANEL (FOR PROP POSITION MONITORING)
NOISE REDUCING FIREWALL
6 STAGE POSITIVE AND NEGATIVE DEFLECTING FLAPERONS
FLAPERON, ELEVATOR & RUDDER GAPS INSIDE SEALED
SCHEMPP-HIRTH TYPE AIRBRAKES, SELF LOCKING
SPRING-TYPE ELEVATOR TRIM
IN FLIGHT ADJUSTABLE RUDDER PEDALS
AUTOMATIC FITTING OF WING AND TAIL MECHANIC CONTROLS
TRANSPARENT CANOPY
FIXED MAIN LANDING GEAR
4˝ MAIN WHEEL WITH DISC BRAKE AND FAIRING
TWO WINGTIP WHEELS, 2 ½ ˝x 1 ˝, WITH FAIRINGS
STEERABLE TAIL WHEEL 180 x 45 mm ( 7˝x 1 ¾Ë)
14 - LITER FUEL TANK
VISUAL CONTROL OF THE FUEL LEVEL
FUEL GASCOLATOR / SUMP
ENGINE HIRTH F33BS or ROTAX 447 BELT DRIVE, AIR CLEANERS ETC
ALL THROTTLE CONTROL BOWDENS IN TEFLON
FULLY AUTOMATIC ENGINE CONTROL AND PROPELLER POSITIONING SYSTEM
HIGH CAPACITY DRY-TYPE BATTERY 12 V / 10Ah
MODULAR ELECTRIC SYSTEM WITH FUSES ON PRIMARY AND SECUNDARY CIRCUIT
ELECTRIC STARTER
REGULATOR-RECTIFIER
2 BLADE WOODEN PROPELLER REINFORCED WITH FIBERGLASS
INSTRUMENT PANEL WITH:
master switch key, switches with fuses and warning lights, magnetos switches,
INSTRUMENTS: MULTIFUNCTION INSTRUMENT TO CONTROL THE ENGINE OPERATIOM AND THE SYSTEM
TO RETRACT THE ENGINE, ENGINE HOURS COUNTER, RPM COUNTER, CHT, EGT, ALTIMETER,
AIRSPEED INDICATOR, VARIOMETER, LIBELLE (SLIP INDICATOR) & MAGNETIC COMPASS WITH MOUNT
AIRCRAFT TOOL KIT FLIGHT AND MAINTENENCE MANUALS

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