FlightStar Spyder

Flightstar Spyder

		•Pricing
		•Color
		•Specs
		•Engine

The FLIGHTSTAR SPYDER is a single seat Ultralight type aircraft. The clean light weight airframe allows maximum performance on minimum installed power. The Spyder was designed to accept the Rotax 447 and 503 engines on Flightstar’s dynafocal type engine mount. The front fairing and windshield come as standard equipment on the Spyder. The Spyder features conventional three axis controls with full span ailerons, steerable nose wheel and side mounted control stick. The standard fuel tank has a 5 gallon capacity with a 10 gallon capacity tank as an option. Equipped with the Flightstar wingfold system, the Spyder is easy to assemble and easy to care for. If you want the freedom of open cockpit Ultralight flying, the Spyder is for you!

STANDARD EQUIPMENT

OPTIONAL EQUIPMENT

• 42HP ROTAX 447 AIRCOOLED ENGINE W/COWLING

• COMPOSITE FRONT FAIRING W/TINTED LEXAN WINDSHIELD

• HIGH LIFT WING WITH STREAMLINED STRUTS

• FLIGHTSTAR WINGFOLD SYSTEM

• VIBRATION ISOLATED INSTRUMENT PANEL

• DURABLE ALUMINUM AND STAINLESS CUSTOM HARDWARE

• 5 GALLON ROTATIONAL MOLDED FUEL TANK W/SUMP

• SIDE STICK CONTROL SYSTEM

• RUGGED CHROMEMOLY CAGE AND LANDING GEAR

• HEAVY DUTY STAMPED DYNOFOCAL ENGINE MOUNT

• ANODIZED AIRFRAME FOR CORROSION PROTECTION

• 3 POINT PILOT RESTRAINT HARNESS

• YOUR CHOICE OF CUSTOM COLORS

• 48 HP ROTAX 503 AIRCOOLED ENGINE WITH SUPERCOWL

• FULL INSTRUMENT PACKAGE

• FOUR POINT HARNESS

• COMPLETE ELECTRICAL SYSTEM

• 10 GALLON ROTATIONAL MOLDED TANK

• IN-FLIGHT ADJUSTABLE TRIM

• 3 BLADE COMPOSITE PROPELLER

• AZUSA DRUM BRAKE SYSTEM

• REAR FLOOR PAN

• BRS BALLISTIC PARACHUTE SYSTEM

*FLIGHTSTAR SPYDER*
*SPECIFICATIONS*		*PERFORMANCE*
WING SPAN	30 FT.	CRUISE SPEED (@ 75%)	65 MPH.
LENGTH	16 FT.6 IN.	STALL SPEED (Vso @ Wg)	36 MPH.
HEIGHT	7 FT.10 IN.	VNE	96 MPH.
WING AREA	144 SQ. FT.	CLIMB RATE (@ Wg)	660 FPM.
ASPECT RATIO	6.25	MAX. RANGE (W/10 GAL.)	220 MILES.
EMPTY WEIGHT	280 LBS.	ROLL RATE (45 TO 45)	2.8 SEC.
GROSS WEIGHT	650 LBS.*	TAKEOFF ROLL (@ Wg)	205 FT.
FUEL CAPACITY	5 GAL.	GLIDE RATIO (ENGINE OFF)	8 TO 1.
		SINK RATE	400 FPM
*POWERPLANT:*	ROTAX 547FA (496 C.C. 42HP @ 6800 RPM) 2.58 TO1 REDUCTION RATIO.
*OPTIONAL:*	HKS 700E (680 C.C. 60 HP @ 6200 RPM) 2.58 TO 1 REDUCTION RATIO.
*PROPELLERS:*	TENNESSEE PROP. CO. 2-BLADE, 66” DIA. IVO-PROP. 3-BLADE 62”
*AIRFOIL TYPE:*	FLIGHTSTAR FS-I-2 12% THICK.
BRS-5 #500 PARACHUTE RECOVERY SYSTEM, OPTIONAL.
* STRUCTURAL LIMIT 750 LBS WITH ROTAX 503

Flightstar - Engines

HKS / ROTAX

*HPower Ltd. North American Distributor* - Website**
Version	Performance		Torque			Max RPM
	HP	RPM	Nm	ft. lb.	RPM	RPM
HKS 700E Dual Carb	60	6200	51	15.2	5000	6200



Rotax^® 503UL DCDI With Super Cowl	Rotax^® 582UL DCDI
KODIAK RESEARCH Rotax North American Website

	kW	HP	RPM	Nm	ft. lb.	RPM	RPM
503 UL-DCDI Single Carb	34.0	45.6	6500	51	37.6	5900	6800
503 UL-DCDI Dual Carb	37.0	49.6	6500	56	41.3	6000	6800
582 UL-DCDI Single Carb	40	53.6	6000	68	50.1	5500	6400
582 UL-DCDI Dual Carb	48	65.0	6500	75	55.3	6000	6800

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