Wednesday, 6 March 2013

Airbus A320




The Airbus A320 family consists of short- to medium-range, narrow-body, commercial passenger jet airliners manufactured by Airbus. The family includes the A318, A319, A320 and A321, and the ACJ business jet. Final assembly of the family in Europe takes place in Toulouse, France, and Hamburg, Germany. Since 2009, a plant in Tianjin in the People's Republic of China has also started producing aircraft for Chinese airlines.In June 2012, Airbus announced plans to begin building the 319, 320, and 321 variants in Mobile, Alabama.The aircraft family can accommodate up to 220 passengers and has a range of 3,100 to 12,000 km (1,700 to 6,500 nmi), depending on model.
The first member of the A320 family—the A320—was launched in March 1984, first flew on 22 February 1987, and was first delivered in 1988. The family was soon extended to include the A321 (first delivered 1994), the A319 (1996), and the A318 (2003). The A320 family pioneered the use of digital fly-by-wire flight control systems, as well as side-stick controls, in commercial aircraft. There has been a continuous improvement process since introduction.


On 1 December 2010, Airbus officially launched the new generation of the A320 family with the A320neo "New Engine Option".The new generation offers a choice of the CFM International LEAP-X or Pratt & Whitney PW1000G, combined with airframe improvements and the addition of winglets, named Sharklets by Airbus. 
The aircraft will deliver fuel savings of up to 15%. Virgin America will be the launch customer for the aircraft in spring of 2016. As of 31 December 2011, a total of 1,196 A320neo family aircraft have been ordered by 21 airlines making it the fastest ever selling commercial aircraft.
As of December 2012, a total of 5,402 Airbus A320 family aircraft have been delivered, of which 5,234 are in service. In addition, another 3,629 airliners are on firm order. It ranked as the world's fastest-selling jet airliner family according to records from 2005 to 2007, and as the best-selling single-generation aircraft programme.The family's direct competitors are the Boeing 737, 717, 757 and the McDonnell Douglas MD-80.


#Country of origin  :  European consortium
#Type  :   Short to medium range airliner
#History  :
Perhaps the most important contributor to Airbus Industrie's success as an airliner manufacturer, the four member A320 family is a significant sales success and a technological trailblazer. The 150 seat A320 is the foundation and best selling member of the family.
The A320 is perhaps best known as the first airliner to introduce a fly-by-wire flight control system - where control inputs from the pilot are transmitted to the flying surfaces by electronic signals rather than mechanical means. Apart from a small weight saving, the advantage of Airbus' fly-by-wire is that as it is computer controlled, an inbuilt flight envelope protection makes it virtually impossible to exceed certain flight parameters such as G limits and the aircraft's maximum and minimum operating speeds and angle of attack limits.
Also integral to the A320 is the advanced electronic flightdeck, with six fully integrated EFIS colour displays and innovative sidestick controllers rather than conventional control columns. The A320 also employs a relatively high percentage of composite materials compared to earlier designs. Two engines are offered, the CFM56 and IAE V2500.

The A320 program was launched in March 1982, first flight occurred on February 22 1987, while certification was awarded on February 26 1988. Launch customer Air France took delivery of its first A320 in March that year. The first V2500 engined A320 was delivered to Adria Airways in May 1989.
The initial production version was the A320-100, which was built in only small numbers before being replaced by the definitive A320-200 (certificated in November 1988) with increased max takeoff weight, greater range and winglets. The stretched A321 and shortened A319 and A318 are described separately. All four share a common pilot type rating. Mid 2000 A320 family production was at a monthly rate of 22, to be increased to 30 units  a month by the end of 2002.
#Powerplants
Two 111.2kN to 120.1kN (25-27,000lb) CFM International CFM56-5A1 turbofans or 118kN (26,500lb) CFM56-5A3s or 120kN (27,000lb) -5B4s, or two 113.4kN (25,500lb) International Aero Engines IAE V2500-A1 or 117.9kN (26,500lb) V2527-A5s.
#Performance
A320-200 - Max cruising speed 903km/h (487kt) at 28,000ft, economical cruising speed 840km/h (454kt) at 37,000ft. Range with 150 passengers and reserves with CFM56s 4843km (2615nm), or 5639km (3045nm), or 5278km (2850nm); with V2500s 4874km (2632nm) or optionally 5463km (2950nm) or 5676km (3065nm).
#Weights  :
A320-200 - Operating empty with V2500s 42,220kg (93,079lb); with CFM56s 42,175kg (92,980lb). Standard max takeoff for both versions 73,500kg (162,040lb) or optionally 75,500kg (166,445lb) or 77,000kg (169,755lb).
#Dimensions  :  
Wing span 34.09m (111ft 10in), length 37.57m (123ft 3in), height 11.76m (38ft 7in). Wing area 122.6m2 (1319.7sq ft).
#Capacity  :
Flightcrew of two. Main cabin can accommodate a maximum of 179 passengers in a high density layout. Typical two class seating arrangement for 12 passengers at four abreast and 138 at six abreast. Seven LD3 derived LD3-46 containers or palletised cargo can be stored in the underbelly forward (four) and rear (three) freight holds.
#Production   :  
As of early 2003, firm orders for the A320 stood at 1397 with 1131 delivered.




#SETTING THE SINGLE-AISLE STANDARDS :
The A320 is the best-selling single-aisle product
Airbus launched its best-selling single-aisle product line with the A320, which continues to set industry standards for comfort and operating economy on short- to medium-haul routes.  Typically seating 150 passengers in a two-class cabin – or up to 180 in a high-density layout for low-cost and charter flights – the A320 is in widespread service around the globe on services that vary from short commuter sectors in Europe, Asia and elsewhere to trans-continental flights across the United States.
The A320’s advanced technology includes the extensive use of weight-saving composites, an optimised wing that is 20 per cent is more efficient than previous designs, a centralised fault display for easier troubleshooting and lower maintenance costs, along with Airbus’ fly-by-wire flight controls.
Advantages of the fly-by-wire controls – which were pioneered on the A320 – are many.  They provide total flight envelope and airframe structural protection for improved safety and reduced pilot workload, along improved flight smoothness and stability, and fewer mechanical parts. 



#COCKPIT STANDARDISATION :
In addition, fly-by-wire and cockpit standardization across the A320 Family are at the heart of Airbus’ commonality, which allows a pilot qualified on one Family member to fly them all, using the same type rating.  Over 80 per cent of operators with 10 or more A320 Family jetliners in their fleets fly more than one model of the Airbus single-aisle product line – enabling them to benefit fully from the commonality concept through more effective scheduling of aircraft and crews.
Taking the Airbus commonality one step further, an A320-rated pilot can transition to any other Airbus jetliner with reduced training (known as “Cross-crew Qualification”), and is able to operate another Airbus aircraft type while still actively flying the A320 Family (a capability called “Mixed Fleet Flying”). 


#RANGE IMPROVEMENTS  :
Continuing its role as a pioneer, the A320 will be the first version in Airbus’ single-aisle product line to be delivered with the new “Sharklets” large wingtip devices, which are designed to enhance the eco-efficiency and payload-range performance of the A320 Family.  
The Sharklets – which completed their maiden flight outfitted on Airbus’ A320 development aircraft in November 2011 – are expected to result in at least a 3.5 percent reduced fuel burn over longer sectors, corresponding to an annual reduction in CO2emissions of around 700 tonnes per aircraft. Sharklets also are incorporated in the A320neo, Airbus’ fuel-efficient new engine option which brings enhanced range for its benchmark A320 jetliner.


#SIMPLY THE BEST CABIN  :
The A320’s right-sized fuselage is seven inches wider than its competitors, enhancing comfort for passengers and increasing revenue opportunities for airlines.  It enables choices of four-, five-, and six-abreast layouts with wider seats, along with opportunities for wider aisles and increased overhead storage bins.  Rapid turnaround times on the ground are further facilitated by the A320’s bigger passenger and service doors.
 Airbus has developed a new interior for the A320 and its other family members that brings a fresh new look to the cabin, a significant increase in overhead stowage, a noticeable reduction in noise, and introduces options for ambience lighting.  An added advantage is this updated interior’s lower weight.


#NAVIGATING THE FUTURE  :
Advanced navigation technology contributes to the A320’s operational flexibility.  This includes the Required Navigation Performance (RNP) capability, which reduces approach distances for landing while reducing fuel consumption and CO2 emissions; and the Global Position (GPS) landing system, allowing instrument-type approaches where ground stations are not available.Also offered are the Microwave Landing System (MLS) for increased approach capability in low visibility conditions; and the Future Air Navigation System (FANS) for optimised flight path and reduced aircraft spacing.

Regards,



Monika Singh [B.Tech ] 
Web Developer / Blog Master 


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Tuesday, 5 March 2013

Pacific Aerospace Fletcher FU-24



The Fletcher FU-24 (now PAC Fletcher) is an agricultural aircraft from the American manufacturer Fletcher . It is used with the appropriate conversion kits as well as freight, passenger and degradation.



#Country of origin:     New Zealand



#History  :

Fletcher in the USA originally developed the FU-24 largely for agwork in New Zealand.The FU-24 flew for the first time in June 1954, and production and deliveries began during 1955, following certification on July 22. Seventy 195kW (260hp) Continental IO-470-D powered FU-24s and dual control FU-24As were built in the USA before Fletcher ceased production in 1964, and Air Parts (now Pacific Aerospace) of New Zealand acquired the production rights.Initial New Zealand production was of two models, one powered by a 215kW (285hp) Continental, the other a 225kW (300hp) unit. The subsequent FU-24-950 was powered by a 300kW (400hp) eight cylinder Lycoming IO-720, and was followed up by the similarly powered FU-24-954 from 1979.
Like many ag aircraft, the Fletcher was a natural candidate for conversion to turboprop power. The resulting Cresco first flew on February 28 1979 powered by a 450kW (600shp) Avco Lycoming (now Textron Lycoming) LTP-101. Nine such aircraft were built, while a tenth was fitted with a 560kW (750shp) PT6A-34AG.Although PAC announced it would cease aircraft manufacture in 1994, PAC's new owners have placed the Cresco back into production. Initial production was of the LTP-101 powered Cresco 08-600, now the focus is on the PT6A powered Cresco 08-750.PAC also offers turbine FU-24 conversions with PT6s or Walter 601s.
#Heritage Aircraft  :
Numerically the FU-24 is the aircraft model that PAL and its forerunner companies have produced the most of any aircraft model and most of these are still flying today albeit often heavily modified with more powerful engines. There is some valid argument as to the exact number produced. It is generally accepted that 300 were factory produced with around 10 assembled from spares by James Aviation and several other NZ companies.
Factory assembled examples were serial numbered 001 through to 297, 2001 and 3001 through 3003. The first completely New Zealand built example built by Airparts (NZ) Ltd in 1966 was a 300-hp variant delivered to Wanganui Aerowork. Prior to that Aircraft were assembled from detail parts produced by Fletcher Aircraft Corporation in the USA.
Fletcher Aircraft Corporation actually only ever assembled 4 complete Aircraft: the prototype s/n 001, s/n 007, s/n 089 and the first FU-24A dual s/n 102 (although this was first built as a FU-24 single control). Of these four, three eventually came to New Zealand. S/n 089 went directly to Uruguay in 1963 and is the only Fletcher FU-24 ever built that has never been to New Zealand.  It still exists today and is still powered by a 260-hp Continental Engine.
The 400-hp FU-24 which we all now know as the "950" was actually first developed in Australia by Airparts (NZ) Ltd's Sydney branch. This prototype was then abandoned in favour of another being developed by Pay's Air Service in Scone NSW. The PAS 400 was converted from 300-hp variant s/n 136 and first flew as a 400-hp in February 1970.
400-hp FU-24s were operating in Australia, all modified from 300 hp variants when the first factory example s/n 155 named FU-24-950 was produced in1970. Production of the FU-24-950 continued until s/n 248 in 1978 when it was replaced by the FU-24-954.
The prototype FU-24-954 was actually s/n 247 and it was exported to the USA where it languished unassembled for some years until it was returned to New Zealand and flew for the first time in 1988 at Wanganui Aerowork. The First FU-24-954 to be completed and fly in New Zealand was s/n 250, which first flew in May 1978. Aircraft were being built out of s/n sequence at this time, as s/n 249 did not fly until May 1979.
The last FU-24-954 was s/n 257 so numerically it was the smallest variant built with the exception of the sole FU-24-872, and the three turbine variants built in the late 1960s.
Next came the final factory variant named FU-24 post 954 with s/n 258. Production of the post 954 continued, albeit sporadically, until s/n 297, which flew in May 1992 when production was halted in favour of the 08-600 Cresco, (which itself had been in sporadic production for some 10 years). Of the final 10 FU-24 post 954s built the first Five went to Thailand and the final five to Syria.
There is confusion as to what is an FU-24-954 and what is a FU-24 post 954. The FU-24-954 is identical to an FU-24-950 but with a large Cargo Door. An FU-24 post 954 had a revised appearance including new Cowlings, Aileron fences, changed Rudder Pedals and many other refinements over an FU-24-954. What is generally accepted as an FU-24-954 is actually an FU-24 post 954.
#Powerplants :
FU-24-954 - One 300kW (400hp) Textron Lycoming IO-720-A1A or A1B fuel injected flat eight piston engine driving a three blade constant speed Hartzell propeller. Cresco 08-750 - One 560kW (750shp) Pratt & Whitney Canada PT6A-34AG turboprop.
#Performance  :  
FU-24-954 - Max speed 233km/h (126kt), max cruising speed 209km/h (113kt), typical operating speed range 165 to 210km/h (90 to 115kt). Initial rate of climb 805ft/min. Service ceiling 16,000ft. Range with max payload and reserves 709km (383nm). 
08-750 - Max speed 291km/h (157kt), max cruising speed at 75% power 261km/h (141kt). Initial rate of climb 1657ft/min. Service ceiling 26,000ft. Range with standard fuel and no reserves 726km (392nm).
#Weights
FU-24-954 - Empty equipped 1188kg (2620lb), max takeoff 2465kg (5430lb).
08-750 - Empty equipped 1315kg (2900lb), normal max takeoff 2925kg (6450lb), ag (restricted) category max takeoff 3742kg (8250lb).
#Dimensions  :  
FU-24-954 - Wing span 12.81m (42ft 0in), length 9.70m (31ft 10in), height 2.84m (9ft 4in). Wing area 27.3m2 (294.0sq ft). 
08-750 - Same except for length 11.07m (36ft 4in), height 3.63m (11ft 11in).
#Capacity  :
Typical arrangement seats pilot and passenger, and chemical hopper (capacity 1210 litres/265Imp gal/319US gal in FU-24-954, 1770 litre/391Imp gal/470US gal in Cresco). Can also be configured for freight work, or as a passenger aircraft can seat six in rear compartment (earlier models can seat five or six passengers).
#Production   :  
Almost 300 FU-24s built in the USA and New Zealand (70 in US, balance in NZ) since 1955. Approx 30 Crescos built.


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Er Monika Singh [B.Tech ] 
Web Developer / Blog Master 

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Saturday, 2 March 2013

The Fokker 50 is a turboprop-powered Airliner




FOKKER 50 TURBOPROP REIONAL AIRLINER
The Fokker 50 is a turboprop-powered airliner, designed as a refinement of and successor to the highly successful Fokker F27 Friendship. The Fokker 60 is a stretched freighter version of the Fokker 50. Both aircraft were built by Fokker in the Netherlands. The Fokker 60 has also been used by the Royal Netherlands Air Force and now they are in service with the Peruvian Naval Aviation.


HISTORY  
The Fokker 50 was the successor to Fokker's highly successful and long running F-27 Friendship.
Fokker announced it was developing the 50 seat Fokker 50, together with the 100 seat jet powered Fokker 100, in November 1983. The Fokker 50 is based on the fuselage of the F-27-500 Friendship, but incorporates a number of key design changes. Foremost of the improvements was the new generation Pratt & Whitney Canada PW125 turboprops driving advanced six blade props, giving a 12% higher cruising speed and greater fuel economy, and thus range. Other improvements include new avionics and an EFIS glass cockpit, limited use of composites, small `Foklet' winglets, and more, squared, main cabin windows.
Two prototypes were built based on F-27 airframes (despite the fact that over 80% of Fokker 50 parts are new or modified), the first flying on December 28 1985. The first production aircraft flew on February 13 1987, certification was granted in May 1987, and first customer delivery, to Lufthansa Cityline, was during August that year.
The basic Fokker 50 production model is the Series 100. With three, instead of four doors, the Series 100 is designated the Series 120. The hot and high optimised Series 300 has more powerful PW127B turboprops, and was announced in 1990. It has higher cruising speeds and better field performance, particularly at altitude.
The only significant development of the Fokker 50 to see the light of day was the Fokker 60 Utility, a stretched utility transport version ordered by the Royal Netherlands Air Force. Fokker built four for the Netherlands air force and looked at offering a passenger variant. The Fokker 60 was stretched by 1.62m (5ft 4in).
Fokker collapsed due to financial problems on March 15 1996 and the last Fokker 50 was delivered to Ethiopian Airlines in May 1997.

DESIGN
The Fokker 50 was based on the stretched F27-500 airframe, but with a larger number of smaller windows in the fuselage and a two-wheel nose gear.
Basic construction of the fuselage, wings and empennage (tail) remained unchanged apart from strengthening the various sections where required. The wing was equipped with upturned ailerons and wingtips, effectively acting as wing endplates or winglets.
The major design change from the Fokker F27 was in the engines, and in equipping the aircraft with an electronic flight and engine-management system. The original Rolls-Royce Darts in various marks of basically 1,268-1715 kW (1,700-2,300 hp) was replaced with two more fuel efficient Pratt & Whitney Canada PW124 powerplants of 1,864 kW (2,500 hp) each, driving six-bladed Dowty Rotol propellers.
The Fokker 50 can carry up to 62 passengers over a range of 2,000 km (1,243 mi, 1,080 nmi) at a typical speed of 530 km/h (329 mph, 286 kn), a 50 km/h (31 mph, 27 kn) increase over the Fokker F27.

VARIANTS
Interior of a Fokker 50 of Skyways Express
Fokker 50
F27 Mark 050
Marketed as the Fokker 50 (or sometimes referred to as the Fokker 50-100), based on the F27 Mark 500 with two Pratt & Whitney Canada PW125B or PW127B turboprop engines with six-bladed propellers, updated systems and cockpit instrumentations, increased use of composite structure, double the number of windows, change from pneumatic to hydraulic systems and addition of an electronic engine and propeller controls and electronic flight instrument system (EFIS) and integrated warning system.[3]
F27 Mark 0502
Marketed as the Fokker 50, same as the 050 with reconfigured interior layout and change in type of aft emergency exits, six built (two for the Royal Netherlands Air Force, two for the Singapore Air Force and two for Brunei).[3]
Fokker 60
F27 Mark 0604
Marketed as the Fokker 60, same as the 0502 with an increased fuselage length (1.02 m/3.34 ft in front of wing and 0.80 m/2.63 ft aft of wing), increased design weight and introduction of a large cargo door in the forward right side of the fuselage. Two Pratt & Whitney PW127B turboprop engines, four built.[3]

OPERATORS
As of October 2012 125 aircraft are still in operational use with airlines.[4]

Fokker 50 civil operators
airBaltic Fokker 50 at Riga International Airport

Fokker 50 - Ethiopian Airlines at Lalibela airport
Aero Condor (1)
Aero Mongolia (4)
Air Astana (2)
Air Baltic (4)
Air Iceland (6)
Air Panama (2)
Alliance Airlines (6)
Amapola Flyg (12)
Aria Air (2)
Avianca (10)
Bluebird Aviation (5)
CityJet (15)
Compagnie Africaine D'Aviation (4)
Denim Air (4)
Feeder Airlines (2)
Indonesia Air Transport (3)
Insel Air (4)
Iranian Air Transport (4)
Kish Airline (4)
Mid Airlines (3)
Minoan Air (3)
Mongolian Airlines (2)
MiniLiner (2)
Pacific Royale Airways (2)
Palestinian Airlines (2)
Sky Aviation (5)
Skywest Airlines (8)
Sonair (2)
Sudan Airways (3)

Fokker 50 military and government operators
Fokker 50 - Royal Netherlands Air Force
TGFA Fokker 50
The following governments or military operators currently fly the Fokker 50 in passenger or cargo roles:[5]
 Netherlands
Royal Netherlands Air Force.
 Republic of China
Republic of China Air Force - as VIP transport.
Republic of China Air Force Fokker 50 for VIP transport
 Singapore
Republic of Singapore Air Force - as Utility Transport Aircraft (UTA) and Maritime Patrol Aircraft (MPA).
 Tanzania
Tanzania Government Flight Agency - as VIP transport
 Thailand
Royal Thai Police
Former operators


Regional services were flown by Malaysia Airlines using Fokker 50s until the takeover by FlyAsianXpress and subsequently MASwings
Fokker 50 of Ansett Express at Perth Airport (mid 1990s).
 Angola
TAAG Angola Airlines
 Australia
Airlines of New South Wales
Ansett Australia
Flight West Airlines
 Austria
Austrian Airlines/Tyrolean Airways
 Brazil
Nordeste Linhas Aéreas Regionais
Rio Sul
TAM Airlines
 Estonia
Estonian Air (1996–2003)
 Germany
Lufthansa CityLine
Contact Air
 India
Rajair
 Ireland
Aer lingus
 Kenya
Kenya Airways
 Luxembourg
Luxair
 Malaysia
Firefly
FlyAsianXpress
Malaysia Airlines
MASwings
 Netherlands
KLM Cityhopper
KLM uk
 Nigeria
Virgin Nigeria Airways
 Norway
Busy Bee
Norwegian Air Shuttle (2000-2004)
 Philippines
Philippine Airlines
 Spain
Iberia/Air Nostrum
 Taiwan
Formosa Airlines/Mandarin Airlines
 United Kingdom
Air UK
Fokker 60 Military Operators
 Peru
Peruvian Naval Aviation - 2 as Utility Transport Aircraft (UTA) and 2 as Maritime Patrol Aircraft (MPA).

FORMER OPERATORS
 Netherlands
Royal Netherlands Air Force.

POWERPLANTS  
Series 100 - Two 1864kW (2500shp) Pratt & Whitney Canada PW125B turboprops driving six blade Dowty propellers. Series 300 - Two 2050kW (2750shp) PW127Bs.

PERFORMANCE  
Series 100 - Max cruising speed 532km/h (287kt), economical cruising speed 454km/h (245kt). Max operating altitude 25,000ft. Range with 50 passengers and reserves 2055km (1110nm), or 2822km (1524nm) for optional high gross weight version. Series 300 - Typical cruising speed 526km/h (284kt). Range with 50 passengers and reserves at high speed cruise 2033km (1097nm), or 3017km (1628nm) for high gross weight option at long range cruise.

WEIGHTS 
Series 100 & 300 - Operating empty 12,520kg (27,602lb), max takeoff 19,950kg (43,980lb), or optionally 20,820kg (45,900lb).

DIMENSIONS  
Wing span 29.00m (95ft 2in), length 25.25m (82ft 10in), height 8.32m (27ft 4in). Wing area 70.0m2 (753.5sq ft).

CAPACITY  
Flightcrew of two. Standard seating for 50 at four abreast and 81cm (32in) pitch. Max high density seating for 58. Available with convertible passenger/freight configurations.



PRODUCTION  
205 Fokker 50s built. Last machine delivered in May 1997.



SPECIFICATIONS
General characteristics
Crew: 2 (flight deck crew)
Capacity: up to 58 passengers
Length: 25.25 m (82 ft 10 in)
Fokker 60: 26.87 m (88.16 ft)
Wingspan: 29 m (95 ft 2 in)
Height: 8.32 m (27 ft 4 in)
Wing area: 70 m2 (750 sq ft)
Empty weight: 12,250 kg (27,007 lb)
zero fuel weight: 18,600 kg (41,006 lb)
Gross weight: 18,597 kg (41,000 lb)
Max takeoff weight: 20,820 kg (45,900 lb)
Fokker 60: 22,950 kg (50,596 lb)
Powerplant: 2 × Pratt & Whitney Canada PW125B turboprop engines, 1,864 kW (2,500 hp) each
Fokker 60: 2x 1,953 kW (2,619 hp) Pratt & Whitney Canada PW127B turboprop engines
Propellers: 6-bladed Dowty Rotol composite propellers
Performance
Maximum speed: 560 km/h (348 mph; 302 kn)
Cruising speed: 530 km/h (329 mph; 286 kn)
Fokker 60: 469 km/h (291 mph)
Range: 2,055 km (1,277 mi; 1,110 nmi)
Service ceiling: 7,620 m (25,000 ft)
Armament
2 × AGM-84D Harpoon missiles and radar, sonar systems (Republic of Singapore Air Force Fokker 50s)

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Ayushi  Singh [B.Tech ] 
Software Engineer/Blog Master 


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The AS/SA 202 Bravo is a two to three-seat civil light Aircraft


FFA AS-202 BRAVO TWO-SEAT BASIC TRAINER AND AEROBATIC LIGHT AIRCRAFT

The AS/SA 202 Bravo is a two to three-seat civil light Aircraft jointly designed and manufactured by the Swiss company Flug- und Fahrzeugwerke Altenrhein (FFA) and the Italian company Savoia-Marchetti. The aircraft was designated the AS 202 in Switzerland, and the SA 202 in Italy.
Savoia-Marchetti manufactured the wings, undercarriage and engine installation, while FFA manufactured the fuselage, tail and controls, while both companies had assembly plants manufacturing the complete aircraft.
The first Swiss model flew on 9 March 1969, the first Italian aircraft following on 8 May.
Bravo is a rugged all-metal low-wing monoplane with a full vision canopy. Its tricycle landing gear is fixed.
34 15s and 180 18s were built, with most in service with military customers. The biggest civil operator is Patria Pilot Training at Helsinki-Malmi Airport, Finland.


HISTORY  
Although largely in operation with military air arms as a basic trainer, small numbers of the FFA Bravo are also in civilian hands, used primarily as aerobatic and basic pilot trainers.
Design of the Bravo dates back to the late 1960s, with original design work undertaken by SIAI-Marchetti of Italy, but with production and subsequent development work the responsibility of FFA (a company originally established by Dornier as its Swiss subsidiary).
The first prototype to fly was Swiss built, it took to the air for the first time on March 7 1969. An Italian built prototype followed soon after on May 7, while the first production standard aircraft flew on December 22 1971.
Initial production concentrated on the AS-202/15 and 34 were built through to the early 1980s. The definitive production model was the AS-202/18A-4, which first flew in August 1974 and received its certification in late 1975. This version differs from the original 15 in having a more powerful 135kW (180hp) engine. The principle civil Bravo operator was British Aerospace Flight Training (Prestwick) in Scotland which operated 11 (named Wrens). One crashed, but the remaining 10 were sold to Finland where they now fly with Pilot Factory Flight Training (Helsinki).
Two other models have been developed, although single aircraft of each have flown only. The first was the 195kW (260hp) Textron Lycoming AEIO-540 powered Bravo AS-202/26A, which first flew in 1979, the second was the 240kW (320shp) Allison 250-B17C turbine powered Bravo AS-202/32TP which flew in 1991. Swiss certification was awarded in 1995.
The Bravo is still offered for sale although none have been delivered since 1989. In the absence of Bravo production FFA builds components for other manufacturers under subcontract.

VARIANTS
There are a number of versions of the basic AS-202; depending on the engine horsepower and certain customer avionics packages. 
1)AS-202/15 
Two/three seat light trainer and sporting aircraft, with 112 kW (150 hp) Lycoming O-320-E2A engine. The prototype first flew in March 1969, and the first production aircraft in December 1971. Swiss certification granted on 15 August 1972; FAA certification awarded on 16 November 1973. FAA Type Certificate no. A34EU.

2)AS-202/18A 
As AS-202/15 model, but with a 134 kW (180 hp) Lycoming AEIO-360-B1F engine. The first example first flew in August 1974. Swiss certification granted on 12 December 1975; FAA certification awarded on 17 December 1976.

3)AS-202/18A2 
As model /18A with higher maximum take-off/landing weight, extended canopy, electric trim.

4)AS-202/18A3 
As model /18A2 but mechanical trim, 24 Volt electrical system.

5)AS-202/18A4 
As model /18A2 but with British CAA approved special instrumentation. FAA certification awarded on 4 February 1993.

6)AS-202/26A 
Modified aircraft flew as prototype only with a 194 kW (260 hp) Lycoming AEIO-540-D4B5 engine in 1978, 24 Volt electrical system as in model /18A3, air condition to be available as option. Designed for higher performance, especially in hot/high locations. Did not go in production.

7)AS-202/32TP 
Turboprop version of the AS-202/18A4 with 313 kW (420 shp) Allison 250-B17D turboprop, with three bladed constant speed propeller, plus two additional fueltanks at the wingtips. First flight in July 1992. Only one built.

8)AS-202/15-1/16M 
AS-202/15 aircraft with STC from MecanAir. The original engine (150 hp) is removed and a Lycoming O-320-D2A with 160 hp is installed. 

OPERATORS

1)Civil Operators
 Finland
Patria Pilot Training - 7 aircraft. Patria's Bravos are ex-British Aerospace Flying College aircraft. BAE Flying College owned 11 aircraft, but 1 was lost in Scotland claiming 2 lives. Remaining 10 aircraft were sold to private Finnish flying school Pilot Factory, which merged with Patria in 2004-2005.
7 aircraft out of original 10 remain in service. During merger with Patria, one aircraft was sold to private owner. Night-time accident at Helsinki-Malmi airport in 2002 claimed no lives but hull was damaged beyond repair. In August 2010 one aircraft veered off the runway at Helsinki-Malmi and was written off.
 Morocco
Royal Air Maroc - 5 aircraft.
 Oman
Royal Flight of Oman - 4 aircraft.
 Uganda
Uganda Central Flying School - 8 aircraft.

2)Military Operators
 Indonesia
Indonesian Air Force - 40 aircraft. To be replaced by G 120TP in 2013 - 2014
 Iraq
Iraqi Air Force - 48 aircraft.
 Jordan
Royal Jordanian Air Force
 Morocco
Royal Moroccan Air Force - 10 aircraft.
 Oman
Royal Air Force of Oman - Former operator.
 Uganda
Ugandan Air Force - 1 aircraft in 2012

POWERPLANTS  
AS-202/15 - One 110kW (150hp) Lycoming O-320-E2A flat four piston engine driving a two blade fixed pitch McCauley propeller. 
AS-202/18A-4 - One 135kW (180hp) fuel injected Textron Lycoming AEIO-360-B1F driving a two blade constant speed Hartzell propeller, or optionally a three blade Hoffmann prop.

PERFORMANCE  
AS-202/15 - Max cruising speed 210km/h (114kt), economical cruising speed 203km/h (110kt). Initial rate of climb 633ft/min. Service ceiling 14,000ft. Range with max fuel and no reserves 890km (480nm). 
AS-202/18A-4 - Max speed 240km/h (130kt), max cruising speed 226km/h (122kt), economical cruising speed 205km/h (110kt). Initial rate of climb 800ft/min. Service ceiling 17,000ft. Range with max fuel and no reserves 1140km (615nm).

WEIGHTS  
AS-202/15 - Empty equipped 630kg (1388lb), max takeoff 999kg (2202lb) for Utility category, 885kg (1951lb) for Aerobatic. 
AS-202/18A-4 - Operating empty 710kg (1565lb), max takeoff 1080kg (2380lb) for Utility category, 1050kg (2315lb) for Aerobatic category.

DIMENSIONS 
Wing span 9.75m (32ft 0in), length 7.50m (24ft 7in), height 2.81m (9ft 3in). Wing area 13.9m2 (149.2sq ft).

CAPACITY
Two pilots side by side, plus one passenger in rear.

PRODUCTION
Approximately 34 15s and 180 18s built, with most in service with military customers.

SPECIFICATIONS
General characteristics
Crew: One, pilot
Capacity: One or two passengers
Length: 6.65 m (21 ft 9¾ in)
Wingspan: 9.8 m (32 ft 2 in)
Height: 2.51 m (8 ft 2¾ in)
Wing area: 13.16 m² (141.58 ft²)
Empty weight: 486 kg (AS 202-18A4 742 kg[2]) (1,069 lb)
Max. takeoff weight: 852 kg (AS 202-18A4 1,080 kg[2]) (1,874 lb)
Powerplant: 1 × Lycoming O-235-C2A 4-cylinder air-cooled horizontally-opposed piston engine, 86 kW (115 hp)
Max landing weight : AS 202-18A4 1,050 kg[2]
Performance
Never exceed speed: 175 knots[2]
Maximum speed: 227 km/h (122 knots, 141 mph)
Cruise speed: 211 km/h (114 knots, 131 mph)
Stall speed: Flaps 0° 60 KIAS. Flaps 15° 56 KIAS. Flaps 41° 49 KIAS[2] ()
Rate of climb: 3.66 m/s (720 ft/min)
Endurance : 4½ hrs for 202-18A4[2]



Regards,

Ayushi  Singh [B.Tech ] 
Software Engineer/Blog Master 


On Line Assistence :
Y! Messenger : Ayushi.AeroSoft@yahoo.com