Gulfstream's Aircraft, the G280

G280 Overview


Read the Aviation Week Business & Commercial Aviation Review of the Gulfstream G280 (2.9 MB PDF) 

Gulfstream's newest aircraft, the G280 , boasts superiority in all areas of the super mid-size business jet market. It encompasses outstanding performance, comfort and advanced technology to bring together this best-in-class aircraft.

The G280 boasts the longest range at fastest cruise speed in the super mid-size business jet category. A new high-speed wing and Honeywell HTF7250G engines provide the platform for this superb performance. With excellent field performance, the G280 has the ability to obtain access into some of the most difficult airports.

With the most spacious cabin in its class, the G280 cabin can provide seating for up to ten passengers in two seating areas. The large galley and in-flight access to baggage provides the best accommodations for passengers. The 100 percent fresh air, low cabin altitude, quiet cabin and large windows reduce fatigue and promote a comfortable cabin environment.

The G280 introduces the PlaneView280™ cockpit which brings the PlaneView® philosophy from the G350® to the G650® into the super mid-size market. This advanced flight deck improves safety through reduced pilot workload and improved situational awareness. Safety during low visibility operations can be further improved with the optional HUD II heads-up guidance systems and Enhanced Vision Systems (EVS II). The introduction of auto-braking is an industry first in this market, to enhance safety, improve passenger comfort and reduce brake wear.

The Gulfstream G280 represents outstanding value in the super mid-size market. Combining improved fuel efficiency, an excellent warranty and enhancements to improve maintainability, the G280 will have low operating costs. Value is further enhanced through Gulfstream's award winning worldwide product support network.

With over 50 years experience in the business jet market, Gulfstream strives to meet your transportation needs. By combining performance with comfort, safety and affordability, the G280 upholds this Gulfstream tradition.
Gulfstream Girl spent many years in the international marketing and advertising world as an international fashion model and spokesperson, with clients including Chanel, Christian Dior, Valentino, Vogue and MTV. After many successful years in the modeling industry, she was ready for longer runways and became a licensed commercial pilot. Always looking for the next challenge, she continued on to become an FAA certified flight instructor and Gulfstream II, III & IV pilot in command. 
And that's how "Gulfstream Girl" was born.

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Sino Swearingen SJ30-2 Light Corporate Jet

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According to the company, “Sino Swearingen Aircraft Corporation
manufactures the all new SJ30-2 light business jets. Sino Swearingen
Aircraft Corporation's charter is to become the world's leading
aircraft producer by creating a family of cost-efficient, high-
performance, high-quality, superior-technology business jet aircraft
for the corporate, government and military sectors of world aviation.

The SJ30-2 has a unique blend of speed and range capability that is
unmatched in the light jets class of business jet aircraft. Sino
Swearingen Aircraft Company, a partnership between Swearingen Aircraft
Company of San Antonio, Texas and Sino Aerospace Investment
Corporation of Taiwan, was established in 1995 and incorporated in
1997. Its successor, Sino Swearingen Aircraft Corporation, is the
first all new company to develop, build, certify, and deliver a new
design business jet since 1963.

Sino Swearingen Aircraft builds the SJ30-2 Twin Engine Light business
Jet, is a six-passenger, aircraft with a top speed of some 560 mph and
a range of about 2,875 miles. The SJ30-2 was certified by the FAA in
2005, and deliveries are should begin in 2007. Major components of
thislight jet are made in Martinsburg, West Virginia; assembly takes
place in San Antonio. Sino Swearingen Aircraft also maintains a
marketing facility at the Orange County Airport in Southern
California. The company was founded in 1999 by Swearingen Aircraft of
San Antonio and Sino Aerospace Investment of Taiwan; backers include
the Taiwanese government.

Sino Swearingen Aircraft hopes the speed and the range of SJ30-2 will
prove to be selling points against models made by well-established
competitors such as Cessna and Raytheon. The company had booked about
300 orders for the plane by the time FAA certification was announced
in October 2005.

Sino Swearingen currently employs more than 400 people at its
facilities in San Antonio, Texas and Martinsburg, West Virginia. The
company is headquartered at the San Antonio International Airport
(KSAT) in San Antonio, Texas. The headquarters building has over
220,000 sq. ft of hangar and office space and is home to the
engineering, executive, marketing & sales, final assembly/production
line, quality assurance, flight test, and finance departments.”
SJ30
The Emivest SJ30 is an American business jet built by the Emivest
Aerospace. The SJ30 has been under development since the late 1980s
and has been the subject of investment and partnership with a number
of companies.
Development
Ed Swearingen announced a new design for a light twin business jet in
October 1986, the SA-30 Fanjet. The SA-30 was to be a 6 to 8 person
aircraft powered by two Williams FJ44 turbofans and with a highly
swept wing of relatively small area. It was planned to be more
efficient than contemporary business jets, and to sell for $2 million.
In October 1988 an agreement was signed with Gulfstream Aerospace with
the SA-30 to be manufactured and sold by Gulfstream as the Gulfstream
Gulfjet. Gulfstream withdrew from the project in September 1989,
causing Swearingen to get backing from the Jaffe Group of San Antonio,
with the aircraft to be built in a factory next to Dover Air Force
Base, Delaware. This resulted in the aircraft again being redesignated
as the SJ-30 (later "SJ30-1"). The first SJ-30 flew on 13 February
1991, and was demonstrated at the 1991 Paris Air Show, but development
ground to a halt when withdrawal of financial support from the state
of Delaware.

The program was rescued by Lockheed, who arranged a joint venture
between Swearington and Taiwanese investors as part of the offset
agreement for Taiwan's purchase of the F-16 fighters. The Sino
Swearingen Aircraft Corporation was set up, with the aircraft now to
be built at Martinsburg, West Virginia.

It was subsequently decided to modify the original design as the
SJ30-2, with a 4 ft 4in (1.32 m) longer fuselage and wingspan
increased by six foot (1.83 m).This promised a signifiant increase in
range.The prototype was modified and flew in the new configuration on
8 November 1996, and with the intended FJ44-2a engines on 4 September
1997.Amidst construction delays caused by funding issues, two
"as-designed" pre-production aircraft (serial numbers 002, performing
the aerodynamics/stability & control testing; and 003, performing
systems testing) were built and the design entered certification
testing. However, in April 2003, S/N 002 crashed during flight
testing, causing further delays in the certification program. After a
series of additional design changes, S/N 004, originally slated as the
functionality & maintainability (F & M) test article, took over the
testing role of S/N 002 (with S/N 005 taking on the F & M role), and
after years of flight testing, the SJ30-2 was finally certified by the
FAA in October 2005. The first customer delivery took place in early
2007.

The SJ30 is in the "light" jet class, and has the fastest cruise
speeds and longest range of any aircraft in that class. The aircraft
can seat up to six passengers plus one pilot. A unique feature of this
aircraft is that it maintains a 'sea level cabin' up to 41,000 ft (due
to its 12 psi differential pressure) thereby reducing fatigue due to
high cabin altitude on long journeys.

Sino Swearingen was acquired by investors from Dubai in 2008. The
Dubai-based company will become the majority shareholder in Sino
Swearingen, with the Taiwanese government and private investors taking
minority stakes. The company name was changed to the Emivest Aerospace
Corporation.

The order book for the $7.5 million aircraft was reported to be
largely unaffected by the funding setbacks, with the tally reportedly
exceeding 300 units including 159 from Action Aviation.

On October 26, 2010, Emivest filed for bankruptcy after being unable
to find further funds to continue operations.

The original SJ30-1 prototype was on display at the Lone Star Flight
Museum in Galveston, Texas when it was flooded by Hurricane Ike.

On April 7, 2011, a judge approved sale of Emivest assets to MT LLC of
Utah, an ownership group affiliated with Metalcraft Technologies, Inc.
of Cedar City, Utah, a parts supplier for the SJ30. According to a
news article, Emivest vice president Mark Fairchild stated that
according to his understanding, MT planned to maintain Emivest as a
jet manufacturer, though he didn't know any details.

As of June 15, 2011, Metalcraft Technologies, the Cedar City,
Utah-based company that purchased Emivest out of bankruptcy, MT LC,
announced that the new company name would be SyberJet Aircraft.
Metalcraft also owns the SJ30 type certificate.
Variants
SJ-30-1
    Prototype later modified to SJ-30-2 standard.
SJ-30-2
    Stretched production variant.
Specifications (SJ30)
General characteristics

    Crew: 1 or 2 pilots (the SJ30 is certified as single pilot)
    Capacity: 6 passengers (including one passenger in the cockpit if
there is no co-pilot)
    Length: 46 ft 9½ in (14.26 m)
    Wingspan: 42 ft 4 in (12.90 m)
    Height: 14 ft 3 in (4.34 m)
    Wing area: 190.7 sq ft (17.72 m²)
    Empty weight: 7,700 lb (3,493 kg)
    Max. takeoff weight: 13,500 lbs (6,123 kg)
    Powerplant: 2 × Williams International FJ44-2A turbofan, 2,300 lbs
(10.23 kN) each

Performance

    Never exceed speed: M .83
    Maximum speed: 486 knots (528 mph, 850 km/h)
    Stall speed: 91 knots (104 mph) (105 mph, 169 km/h)
    Range: 2,500 nmi (2,887 mi, 4,626 km)
    Service ceiling: 49,000 ft (14,935 m)
    Rate of climb: 1,000 ft/min (5.1 m/s)

Avionics

    Honeywell Epic Control Display System





    Sino Swearingen San Antonio
    Sino Swearingen SJ30 for Sale
    Sino Swearingen Aircraft Corp
    Sino Swearingen Jobs
    SJ30 Jet Review
    SyberJet
    SJ30-2
    Swearingen SJ30
    SJ30 Price
    SJ30 2 Jet
    SJ30 for Sale
    Sino Swearingen Aircraft Corporation
    SJ30-2 Airplane for Sale
    Emivest SJ30-2
    Emivest SJ30 Jet
    Emivest SJ30 for Sale


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Toyota TA-1 Prototype Single Engine, 4-place Aircraft

Toyota TA-1 Prototype Single Engine, 4-place Aircraft:

The Toyota TAA-1 (also referred to in the press as the TA-1) was a
prototype general aviation aircraft substantially built and test flown
by Burt Rutan's Scaled Composites under contract with Toyota.
First flight of the aircraft took place at the Mojave Airport on May
31, 2002. The project was a joint effort of Toyota Motor Corporation
(TMC) and Toyota Motor Sales, USA, Inc (TMS) to determine if "Toyota's
aerodynamics and low-cost production technologies could be applied to
the small aircraft sector." Although Toyota announced the first
flight, Company executives have remained relatively silent about the
project, and many in the general aviation industry were unaware that
the aircraft was even being built.
              The prototype TAA-1 is a 4-place, single piston engine
aircraft powered by an "engine produced by an outside manufacturer",
according to Toyota, and presumably built by Textron Lycoming. (in the
1990s, Toyota attempted to adapt one of their Lexus engines for
aviation purposes, but eventually shelved the project due to an
industry downturn). The wing, as well as the fuselage, of the aircraft
is carbon fiber, constructed in a one piece co-cured single-molded
configuration. The fuselage was fabricated by Rocky Mountain
Composites, Inc. using a proprietary fiber wetting and placement
technique, the wings were produced by Radius Engineering, Inc. with a
modified resin transfer molding process. The project was unique for
Scaled Composites as never before had an aircraft been completed there
using composite wing and fuselage structures that were designed and
fabricated elsewhere.
The empty weight of the prototype was significantly beyond predictions
and the unsubstantiated rumors within the industry are that the
aircraft's performance during the test flight was below what was
expected, and it does not appear that much flight test activity
followed the initial flight. The prototype aircraft remains stored in
a Scaled Composites hangar. A follow-on design, TAA-2, (substantially
similar airframe with retractable landing gear, upgraded avionics and
higher performance engine with constant speed propeller) was also
envisioned however never made it to the prototype stage.
After several years of negotiation for a potential joint venture with
the general aviation piston aircraft market leader of that time,
interest in the TAA-1 declined after the initial flight test and that
outside partnership development evaporated shortly thereafter.
The Toyota TA-1 was a prototype general aviation aircraft built by
Burt Rutan's Scaled Composites under contract.
First flight of the aircraft took place at the Mojave Spaceport on May
31, 2002. The project was a joint effort of Toyota Motor Corporation
(TMC) and Toyota Motor Sales, USA, Inc (TMS) to determine if "Toyota's
aerodynamics and low-cost production technologies could be applied to
the small aircraft sector." Although Toyota announced the first
flight, Company executives have remained relatively silent about the
project, and many in the general aviation industry were unaware that
the aircraft was even being built.
                The first flight was the culmination of fours years'
design work by a team of 40 engineers, many formerly of Boeing and
Raytheon, at TMS's Long Beach facilities. A Toyota official would only
say, "We are studying the potential for a single-engine piston plane
but there is not a lot we can say." Scaled Composites turned the
Toyota engineers' design work into reality and hosted the flight test
program at Mojave. Rutan, in a public address, called the aircraft
"the aeronautical equivalent to the Lexus LS400."The prototype TA-1 is
a 4-place, single piston engine aircraft powered by an "engine
produced by an outside manufacturer", according to Toyota, and
presumably built by Textron Lycoming (in the 1990s, Toyota attempted
to adapt one of their Lexus engines for aviation purposes, but
eventually shelved the project due to an industry downturn). The
fuselage of the aircraft is carbon-fiber, constructed in a one-piece
co-cured single-molded configuration. Unsubstantiated rumors within
the industry are that the aircraft's performance during the test
flight was below what was expected, and it does not appear that much
flight test activity followed the initial flight. The prototype
aircraft remains stored in a Scaled Composites hangar.


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New Toyota Tacoma 2012 Redesign,
2011 Toyota Tacoma Winch Bumper,
Toyota Dealership Seattle Washington,
Toyota Ta 22,
2014 Toyota Ta,
TA22 Celica,
Stride for Breast Cancer Walk,

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Er Ayushi Saxena  [ B E CS, MBA ]
Management Trainee / Software Engineer / Webmaster
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Transavia Airtruk & Skyfarmer Agricultural aircraft:

The Transavia PL-12 Airtruk is a single-engine agricultural aircraft
designed and built by the Transavia Corporation in Australia. The
Airtruk is a shoulder-wing strut braced sesquiplane of all-metal
construction, with the cockpit mounted above a tractor engine and
short pod fuselage with rear door. The engine cowling, rear fuselage
and top decking are of fibreglass. It has a tricycle undercarriage,
the main units of which are carried on stub wings. It has twin tail
booms with two unconnected tails. Its first flight was in 22 April
1965, and was certified on 10 February 1966.

Design and development:
It was developed from the Bennett Airtruck designed in New Zealand by
Luigi Pellarini. It has a 1 metric ton capacity hopper and is able to
ferry two passengers as a topdresser. Other versions can be used as
cargo, ambulance or aerial survey aircraft, and carry one passenger in
the top deck and four in the lower deck.
The Airtruk is also sometimes known as the Airtruck. Because the name
"Airtruck" was registered by the New Zealand companies Bennett
Aviation Ltd and Waitomo Aircraft Ltd, for their PL-11, Transavia
found another name for their PL-12 ("Airtruk").
July 1978 saw the first flight of an improved model, the T-300
Skyfarmer, which was powered by a Textron Lycoming IO-540-engine. This
was followed in 1981 by the T-300A with improved aerodynamics

Variants:
PL-12 Airtruk
Single-engined agricultural aircraft. Powered by 300 hp (224 kW) Rolls
Royce Continental IO-520-D
PL-12U
Multi-purpose utility transport, air ambulance, aerial survey aircraft.
T-320 Airtruk
Powered by a 320-hp Continental/Rolls-Royce Tiara 6-320-2B piston engine.
Skyfarmer T-300
Powered by Lycoming O-540 engine.
Skyfarmer T-300A
Improved version of the T-300.
Skyfarmer T-400
Enlarged, more powerful (400 hp (298 kW) Lycoming O-720 engine.

Specifications:
General characteristics
Crew: 1
Capacity: 907 kg (2,000 lb) dry chemicals or 818 litres (216 US
Gallons, 180 Imp Gallons) liquids. Two passengers.
Length: 6.35 m (20 ft 10 in)
Wingspan: 11.98 m (39 ft 3½ in)
Height: 2.79 m (9 ft 2 in)
Wing area: 24.5 m² (264 ft²)
Airfoil: NACA 23012
Empty weight: 1,017 kg (2,242 lb)
Max. takeoff weight: 1,925 kg (4,244 lb)
Powerplant: 1 × Textron Lycoming IO-540-K1A5 flat-six piston engine,
224 kW (300 hp)

Performance:
Never exceed speed: 274 km/h (148 knots, 170 mph)
Maximum speed: 196 km/h (106 knots, 122 mph) at 915 m (3,000 ft)
Cruise speed: 188 km/h (102 knots, 117 mph) (max cruise -75% power)
Stall speed: 73 km/h (39 knots, 45 mph)
Range: 1297 km (700 nm, 806 mi)
Service ceiling: 6,890 m (22,600 ft)
Rate of climb: 7.62 m/s (1,500 ft/min)
Wing loading: 78.6 kg/m² (16.1 lb/ft²)
Power/mass: 0.12 kW/kg (0.071 hp/lb)


Regards,

Er Ayushi Saxena  [ B E CS, MBA ]
Management Trainee / Software Engineer / Webmaster
www.AeroSoftCorp.com
www.AeroSoft.in
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Tupolev Tu-444 Supersonic Business Jets

Tupolev  is a Russian aerospace and defence company, headquartered in
Moscow, Russia. Basmanny District, Central Administrative Okrug,
Moscow,Russia.Known officially as Public Stock Company Tupolev, it is
the successor of the Tupolev OKB or Tupolev Design Bureau (OKB-156,
design office prefix Tu) headed by the Soviet aerospace engineer A.N.
Tupolev.The capabilities of PSC Tupolev include development,
manufacturing and overhaul for both civil and military aerospace
products such as aircraft and weapons systems. It is also active with
missile and naval aviation technologies. More than 18,000 Tupolev
aircraft were produced for the USSR and the Eastern Bloc.
               The Tupolev Tu-444 is a concept for a supersonic
business jet from the Russian firm Tupolev. Tupolev has had previous
experience developing supersonic transport aircraft with projects such
as the Tu-144, Tu-144LL and other experience with supersonic aircraft
in the bombers Tu-22, Tu-22M and Tu-160.Tupolev OKB was founded by
Andrei Nikolayevich Tupolev in 1922. Its facilities are tailored for
aeronautics research and aircraft design only, manufacturing is
handled by other firms. It researched all-metal airplanes during the
1920s, based directly on the pioneering work already done by Hugo
Junkers during World War I.The Supersonic Business Jet (SSBJ) has long
been a fantasy of aerospace engineers and business executives alike.
For many decades designs have been floated, but for one reason or
another, the projects have withered and died on the vine. Currently
there are half a dozen or so aircraft manufacturers with an eye on
fielding the first SSBJ including the Tupolev Design Bureau. With a
long history of supersonic capable military bombers, Tupolev has a
vast depth of knowledge to draw from.  Whether the market will ever
accept the utility and cost of a SSBJ, however, remains to be seen.
For fans of the concept, Ramzzess recently released his concept of
what the Tu-444 SSBJ might eventually look like. While the external
model is based on actual design plans released by Tupolev, the
interior, avionics, and panels are strictly from the mind of
Ramzzess.It would be difficult to find as exotic looking an aircraft
as the Tu-444. With massive cigar shaped engines, a sleek delta wing,
drooping nose, and a slim body, the Tu-444 advertises that she is
built for speed. Borrowing from the Tu-144 “Concordski” and the
military side of the house, the Tu-444 features the retractable visor
similar to that found on the Concorde to aid in low speed, high angle
of attack visibility. With a total max gross takeoff weight of about
90,000 lbs, the Tu-444 isn’t a small aircraft by any measure. All of
that mass and complexity is designed to carry less than 10 passengers
at better than Mach 2 a bit over 4,000nm. No doubt traveling on a
Tu-444 would be an order of magnitude more glitzy than arriving in
something as sedentary as a Gulfstream.The cockpit, as envisioned by
Ramzzess, is a cool interpretation of what the real Tu-444 panel might
actually look like. Ultra modern, crammed with information and
displays, the panel is pleasant to look at and highlights all of the
special capabilities of the Tu-444. The virtual cockpit is smooth and
nicely rendered. The overhead panels work great and the layout makes
good sense. There are some significant labeling misspellings
throughout the aircraft which clue us in that Ramzzess isn’t a native
English speaker, but the mistakes are actually quite charming and lend
an air of Russian “experimentality” to the Tu-444. Once airborne, the
Tu-444 will (as expected) blow you away with its performance. Climb
rates are in the astronomical range, and care must be taken to keep
the aircraft under Mach 1 over populated areas. The noise footprint of
supersonic aircraft remains one of the bigger challenges that
designers face and I don’t know how effective Tupolev has been at
mitigating the noise factor of the Tu-444. Hand flying the Tu-444 can
be done effectively below Mach 1, but above that I would recommend
slaving the controls to the autopilot since small control movements
can lead to large flight path deviations if you are clumsy on the
controls.

Extremely detailed 3D Model - in and out:
Custom cockpit with advanced touch-screen
Detailed interior with business seats, tables and kitchen
Animated flight controls, nose, gear, rotating fans, etc..
Shutters on passenger windows and in the cockpit
Animated doors
Many liveries

Advanced systems with plugin:
several systems are plugin enhanced, such as fuel consumptions,
lighting, temperature etc.
several original built in systems, like air-conditioning and
autopilot-artificial stability synchronization system
flight model has been also plugin enhanced with randomization
algorithms producing destabilization failures.

General characteristics:
Crew: 2 pilots, 1 flight attendant
Capacity: 6–10
Length: 36 m (118 ft 1 in)
Wingspan: 16.2 m (53 ft 1 in)
Height: 6.51 m (21 ft 4 in)
Wing area: 136 m² (1,460 ft²)
Empty weight: 19,300 kg (42,550 lb)
Max. takeoff weight: 41,000 kg (90,400 lb)
Powerplant: 2 × NPO Saturn AL-32M turbofan, 95 kN (21,400 lbf) each

Performance:
Cruise speed: Mach 2, 2125 km/h (1,320 mph)
Range: 7,500 km (4,660 mi)
Wing loading: 300 kg/m² (29 lb/ft²)
Thrust/weight: 0.48



Regards,

Er Ayushi Saxena  [ B E CS, MBA ]
Management Trainee / Software Engineer / Webmaster
www.AeroSoftCorp.com
www.AeroSoft.in
www.AeroSoft.co.in
www.AeroSoftseo.com
On Line Assistence :
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