Seeker equipment includes: Lycoming 0-360-B2C Engine 2- Blade timber-composite propeller Sigma-Tek instruments Garmin Avionics 28V Electrical system, 70A alternator Cantilever spring steel main landing gear Cleveland wheels and brakes Oleo strut tail landing gear Scott 8”Steerable tail wheel 8.00 x 6.00 low pressure tires Dual primary flight controls Dual differential toe-brakes Double longitudinally hinged windows and doors Baggage/cargo area with tie down points 4-point inertia-reel seatbelts Wing tip Nav/Strobe lights Ground power receptacle Floor aperture provision Windscreen demister Vacuum system (optional) Heated pitot tube (optional)   Once you fly the SEEKER you will immediately realize its unique attractiveness and outstanding effectiveness in providing a safe, cost-efficient alternative to many conventional fixed-wing and rotary wing aircraft.	External Dimensions
	Wing Span	11.07 m	36 ft 4 in
	Overall Length	7.00 m	23 ft 0 in
	Height of Vertical Stabilizer	2.03 m	6 ft 7 in
	Wheelbase	2.04 m	6 ft 8 in
	Internal Dimensions
	Cabin Width	1.12 m	3 ft 8 in
	Doors - Long Axis	1.07 m	3 ft 6 in
	Weights
	Empty weight	610kg	1342 lb
	Maximum T/O Mass	925 kg	2040 lb
	Speeds
	Min Patrol Speed (CAS)	121 km/h	65 kts
	Cruise 75% Power (CAS)	208 km/h	112 kts
	Never Exceed (CAS)	239 km/h	129 kts
	Stall (40° Flap)(IAS)	89 km/h	48 kts
	Fuel Capacity
	Usable	180 litres	47.5 US gal
	Endurance (inc. reserve)
	Min. Patrol Speed	65 kts	7 h 15 min
	Cruise (65% Power)		4 h 30 min
	Range
	Patrol Speed (65 kts)	880 km	476 nm
	Cruise (65% Power)	869 km	470 nm
	Fuel Flow
	Patrol Speed (65 kts)	22 l/h	5.80 US gal/h
	Cruise (65% Power)	34 l/h	9.00 US gal/h
	Take-off/Landing run at AUW
	T-O run	264 m	870 ft
	Landing run	198 m	654 ft
	Stressing
	Limit Load Factor	+3.8	-1.52
	Certification
	Certification Basis	FAR 23 up to and including Amdt 34
	Noise Certification	ICAO Annex 16, Volume 1, Chapter 10 FAR Part 36 Appendix G
	Fatigue Analysis	FAR 23 Amendment 38