Seabird Aviation
Australia Pty Ltd
SEABIRD SEEKER SB7L-360A
SERIES 2

NEW FOR 2007
o
ALL-UP-WEIGHT INCREASE
o
VORTEX GENERATORS
o
GARMIN AVIONICS STANDARD
o
VACUUM SYSTEM STANDARD
2007 INFORMATION PACK


Australian Made – World Leader
Designed & developed in Australia, and now operating in Australia, the
USA,
Middle-East and
Africa,
the Seeker
is a purpose built, rugged utility aircraft for private, commercial
and security operations.
At a third of the operating cost of rotary - wing equivalents,
the Seeker
provides an efficient alternative for powerline and pipeline inspection,
coast watch, environmental and stock monitoring, aerial photography and
security - where VTOL (vertical take-off and landing) is not mission
essential. Crew visibility is unrivalled by any other fixed-wing aircraft
and is superior to many helicopters.

The
SEEKER Advantage
Seabird Aviation Australia has designed and developed the SEEKER
multi-role utility aircraft for optimum effectiveness and performance in
low level observation tasks. Delivering a combination of attributes not
available with conventional helicopters or commercially available fixed
wing aircraft, the SeekeR
represents a sound business decision and offers an impressive and unique
flying experience.
SEABIRD SEEKER – A proven performer
¨
A history of thousands of hours of safe
operation
¨
A unique proven, cost-effective
airborne surveillance platform
¨
Proven
integrated infrared and video downlinked sensor options
¨
A commercially proven powerline/pipeline
patrol aircraft
¨
Proven
in harsh desert conditions of the
Middle East
¨
A unique and proven aircraft for the private owner
¨
Certified to FAR 23 in
Australia and USA
¨
Type Acceptance in
India , South Africa, Jordan
¨
Designed and manufactured under
Production Certificate 417197 in
Hervey Bay,
Queensland Australia
¨
Manufactured under license by Seabird
Aviation Jordan LLC in
Amman,
Jordan
¨
Manufactured under license by Seabird
Aviation America Inc. in
Albuquerque
New Mexico, USA


Unique features -
¨
Helicopter – like visibility
§
Crew seated forward of the wing
highlights the deficiencies of conventional fixed-wing designs and permits
unrivalled 270 degree visibility.
¨
Primary Safety
§
Responsive push - rod operated controls
and vice free stall handling – Will roll level when stalled in a turn
§
Minimal pitch change with power and flap
changes
§
Visibility from cabin and inherent
stability reduces pilot load and enhances situational awareness
§
Low stall speed and ample
power-to-weight ratio enhance low level flight safety
§
High fatigue life – metal primary
structure
§
Simple structure and systems ensure
complete and regular maintenance
¨
Secondary Safety
§
Occupants protected in tubular steel
“Safety Cell”
§
Fire hazards are minimised with fuel in
wings and no fuel lines in cabin area
§
Four point inertia reel harness standard
¨
Comfortable ride
§
Forward cabin provides the crew with a smooth ride and reduced fatigue on
extended missions
§
Well ventilated and spacious cabin with
top door-off operation approval
¨
Low vibration levels
§
With a high mounted engine and pusher prop aft of the cabin, no propeller
slipstream buffet over cabin
¨
De-rated Lycoming 0-360 engine
§
Widely acknowledged as one of the world’s most reliable piston aircraft
engines. De-rated for even greater reliability
¨
Low octane fuels
§
Min. 80/87 Avgas with Mogas approval
¨
Soft-field operation
§
Rugged spring steel main undercarriage legs. Tail wheel oleo, low pressure
tyres for rough field operations
¨
Airframe spare parts
§
Readily available direct from Australian manufacturer, with off-the–shelf
rotables commonly available
¨
Warranty
§
12 months/500 hours airframe warranty
¨
Range of sensors accommodated
§
Aperture in floor, and under-wing and
fuselage hard-points. 24 volt 70 amp electrical system
Unique Design – Proven Technology & Structure
Wings
Strut braced high-wing monoplane, with NACA 632-215 (modified)
aerofoil section with constant chord. Dihedral 2° from root.
Incidence 4° at root, 1° at tip. No sweepback. Vortex Generators and
Leading-edge Cuffs. All-metal skinned. Corrosion resistant 6061T6
aluminium alloy structure, with top-hinged ailerons and mechanical slotted
flaps. Single bracing strut, with jury strut, each side.
Fuselage
Pod and boom structure, of 4130 chrome molybdenum steel tube forward
fuselage affording maximum crew protection. FRP forward fuselage
non-load-bearing skin. Aluminium alloy semi-monocoque tail boom.
Removable doors and windows horizontally hinged.
Tail Unit
Swept fin (with dorsal fin) and balanced rudder; non-swept fixed incidence
tail plane with one-piece horn balanced elevator. Construction similar to
that of wings. Elevator trim.
Landing
Gear
Fixed, with Cleveland wheels and brakes. 8.00-6 low pressure main tyres
and cantilever spring steel legs. Scott 8 inch tailwheel with Oleo
strut.
Power
Plant
125kW (168hp) Lycoming 0-360-B2C, driving a wood-composite 2-blade fixed
pitch propeller. Fuel in two integral wing tanks, combined usable
capacity 180 litres (48 US gallons, 40 Imp gallons). MoGas
approved. Over wing flush fuel caps each tank.
SEEKER Applications

In applications requiring safe, low speed flight at low levels, Seeker
provides the operator with a platform to augment his existing fleet or tap
into new markets.
Applications:
Agriculture, Stock and Crop Monitoring
Border patrol, Crime Prevention, Detection and Pursuit
Customs Surveillance
Environmental Survey
Fisheries
Forest
Fire Detection and Control
Game Spotting
Illicit Crop Detection
News Gathering and Traffic Reporting
Photographic Platform
Pipe and Power Line Patrol
Search and Rescue
Survey and Mapping
Private Flying and Flight Training
Indicative
Overhaul Hours
Airframe life 75,000 hours
Propeller life unlimited – on condition
(suggest 5,000 hours)
Engine life 2,000 hours TBO (extendable on
condition for
private use)
Technical Specifications
|
External Dimensions |
|
|
|
Wing Span |
11.07 m |
36
ft 4 in |
|
Overall Length |
7.00 m |
23
ft 0 in |
|
Height of Vertical Stabiliser |
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 |
1342lb |
|
Maximum T/O Mass |
925 kg |
2040 lb |
|
Speeds |
|
|
|
Min Patrol Speed (CAS) |
121 km/h |
65
kts |
|
ise 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 |
|
|
|
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 & including 34 |
|
Noise Certification |
ICAO Annex 16, Volume 1, Chapter 10
FAR Part 36 Appendix G |
|
Fatigue Analysis |
FAR 23 Amendment 38 |
Performance
Standard Equipment
ENGINE Lycoming 0-360-B2C
PROPELLER Bishton 177 – wood composite