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Engines: PT6A-41
Left Engine
Right Engine
Time Since Overhaul:
1,820 Hours
1,820 Hours
Time Since Hot Section:
0 Hours
0 Hours
Time Between Overhaul:
3,600
3,600
Time Since Prop Overhaul:
10 Hours
10 Hours

 Avionics:
Dual Collins FGC-3000 IFCS / Pro Line 21
Collins Pro Line 21 w/AFD-3010 3-tube
IFIS 5000
Dual Collins FGC-3000 IFCS
L3 Skywatch HP TCAS-I

Dual Collins AHC-3000 AHRS
Collins NAV-4000 & NAV-4500
Dual Collins VHF-4000 w/8.33 kHz spacing
Collins TWR-850
L3 FA2100 (30-minute)
Collins FMS-3000 w/ GPS-4000A
Collins ALT-4000
Honeywell Mark VIII EGPWS
Dual Collins TDR-94 Mode S
Collins DME-4000 handset
AirCell ST-3100 w/ cordless

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Engines:
Pratt & Whitney Canada / 306B 
Engine #1
Engine #2
Serial Number:
49
51
Phase 4
Fresh from P&W in Clarksbur, WV USA
APU: Allied Signal GCTP 36-150 
Serial Number:
P213
Hobbs:
1041
TSN:
10,141
TSO:
189
TSHSI:
304

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Dimensions
Length 26 ft 7.92 m
Height 8 ft 11 in 2.71 m
Wingspan 38 ft 4 in 11.68 m
Cabin Length 130 in 330 cm
Cabin Width 49 in 124 cm
Cabin Height 50 in 127 cm
Design Weights and Loading*
Maximum Gross Weight 3050 lbs 1386 kg
Standard Empty Weight 2080 lbs 945 kg
Useful Load 970 lbs 441 kg
Usable Fuel Capacity 56 gal/336 lbs 212 litre/153 kg
Full Fuel Payload 634 lbs 288 kg
Performance**
Takeoff 1478 ft 450 m
Takeoff Over 50 ft Object 2221 ft 677 m

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SPECIFICATIONS:
Powerplant Continental O-200-D
Horse Power 100 @ 2750 rpm
Propeller Sensenich, W69EK48 Wood Prop
Prop Diameter 69 in.
Length 22.1 ft.
Height 7.7 ft.
Wingspan 33.5 ft.
Wing Area 165 sq. ft.
Wing Loading 8.0 lb. / sq. ft.
Power Loading 13.2 lb. / HP
Seats 2, Tandem
Cabin Length 8 ft. 10 in.
Cabin Width 2 ft. 6 in.
Cabin Height 3 ft. 11 in.
Empty Weight (typical) 967 lbs.
Maximum Gross Weight 1320 lbs.
Useful Load 353 lbs.
Payload with Full Fuel 251 lbs.
Fuel Capacity 17 gal. Usable
Oil Capacity 6 quarts
Baggage Capacity 100 lbs. (10.4 cubic feet)

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AT-4 The Luxury Sport Aircraft

The AT-4 is manufactured for the US market with compliance to the Light Sport Aircraft specification and sold under Gobosh G700 brand.http://gobosh.aero/G700.cfm

The AT-4 is derived from the AT-3 aircraft with the MTOW increased up to 600kg.

The AT-4 structure has a longer wingspan, altered wing profile and spar, additional winglets, and fillets between the wing leading edge and the fuselage.

The AT-4 is approved for Night-VFR and one turn spins. ILS approach procedures can be also trained on the AT-4.

The AT-4 is manufactured on the same production line that produces AT-3 certified aircraft. The certification requirements and superior craftsmanship is evident both above and below the skin of the AT series aircrafts.

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LOS ANGELES, CA – July 26, 2010 – ICON Aircraft, an early-stage, Light Sport Aircraft (LSA) manufacturer, has announced two major design enhancements to improve flight safety and the user-experience of the ICON A5 aircraft. ICON has eliminated wing flaps to simplify pilot operations. ICON has also committed to a spin-resistant design, which will include, among other things, the addition of wing cuffs. Both improvements are designed to simplify aircraft complexity and increase safety—which is especially important for new pilots. “Although these enhancements are not required by the FAA or ASTM,” says Kirk Hawkins, ICON’s CEO, “this is yet another example of ICON raising the bar to not only make the A5 one of the coolest sport planes on the planet—but to make it simultaneously one of the safest and easiest to fly. This is absolutely the right move for the customer and worth the extra work to get there.” While general aviation is inherently quite safe, when accidents do occur, it is the stall/spin scenarios that are responsible for 13.7% of all fatal accidents, according to the Aircraft Owners and Pilots Association (AOPA). Of these accidents, it is slow-speed maneuvering prior to landing that is the most common accident scenario. Making the A5 spin resistant will help ensure that the pilot maintains control of the aircraft at all times, even if the airplane is inadvertently stalled. “Spin resistance is arguably the most significant safety improvement we could add to the already docile- handling A5,” said Matthew Gionta, ICON’s CTO and VP of Engineering. One safety feature already on the A5 is the Angle of Attack (AOA) indicator (standard on modern fighter jets) that shows the pilot at any given time exactly how the wing is flying, and most importantly, how close they are to a stall. “When combined with the AOA indicator, spin resistance adds a second level of safety where, in the event of a stall, the A5 remains wings-level and the pilot does not lose control of the aircraft.” Removal of the flaps is the other improvement to the A5. Flaps are typically used to reduce an aircraft’s stall speed for landing. However, Light Sport Aircraft regulations already require that Light Sport Aircraft stall no faster than 45 knots without the use of flaps. Given this FAA requirement combined with the LSA maximum speed restriction, ICON eliminated the A5 flaps since they offer marginal benefit for their increased complexity. “When an airplane can function equally well with less complexity, the result is increased safety,” said Gionta. “The pilot of an A5 will never have to remember to set the flaps for landing, whether on water or land. This is a classic example where simplicity is elegance, and that translates directly into a safer aircraft for our pilots.” ICON Aircraft has committed itself to fielding an aircraft that offers high performance for experienced pilots, while also being safe and very accessible for novice pilots. These two design improvements confirm the company’s commitment to that philosophy. Over one third of ICON’s current orders come from individuals who are not yet pilots. 

ABOUT ICON AIRCRAFT: ICON Aircraft is a consumer sport plane manufacturer founded by Kirk Hawkins and Steen Strand while at Stanford University shortly after the Federal Aviation Administration (FAA) enacted regulation changes in 2004 that created the new sport flying category. Kirk is an engineer, former U.S. Air Force F-16 fighter pilot, and graduate of Stanford Business School. Steen, a former investment banker and Harvard graduate, holds a Masters in Engineering from Stanford in Product Design and is a serial entrepreneur. A privately funded company, ICON Aircraft’s base of operations is in Southern California, which is a hotbed for automotive design and aerospace engineering.