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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 |
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Wing Span |
11.07 m |
36 ft 4 in |
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Overall Length |
7.00 m |
23 ft 0 in |
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Height of Vertical Stabilizer |
2.03 m |
6 ft 7 in |
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Wheelbase |
2.04 m |
6 ft 8 in |
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Internal Dimensions |
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Cabin Width |
1.12 m |
3 ft 8 in |
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Doors - Long Axis |
1.07 m |
3 ft 6 in |
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Weights |
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Empty weight |
610kg |
1342 lb |
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Maximum T/O Mass |
925 kg |
2040 lb |
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Speeds |
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Min Patrol Speed (CAS) |
121 km/h |
65 kts |
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Cruise 75% Power (CAS) |
208 km/h |
112 kts |
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Never Exceed (CAS) |
239 km/h |
129 kts |
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Stall (40° Flap)(IAS) |
89 km/h |
48 kts |
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Fuel Capacity |
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Usable |
180 litres |
47.5 US gal |
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Endurance (incl. reserve) |
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Min. Patrol Speed |
65 kts |
7 h 15 min |
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Cruise (65% Power) |
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4 h 30 min |
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Range |
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Patrol Speed (65 kts) |
880 km |
476 nm |
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Cruise (65% Power) |
869 km |
470 nm |
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Fuel Flow |
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Patrol Speed (65 kts) |
22 l/h |
5.80 US gal/h |
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Cruise (65% Power) |
34 l/h |
9.00 US gal/h |
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Take-off/Landing |
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T-O run |
264 m |
870 ft |
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Landing run |
198 m |
654 ft |
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Stressing |
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Limit Load Factor |
+3.8 |
-1.52 |
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Certification |
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Certification Basis |
FAR 23 up to and including Amdt 34 |
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Noise Certification |
ICAO Annex 16, Volume 1, Chapter 10 |
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Fatigue Analysis |
FAR 23 Amendment 38 |
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