Some people think that they are on the web they are relatively anonymous internet surfing.   I’m afraid nothing could be further from the truth, when you request a web page all  the information is passed to your web browser in clear text, your IP address is left in the web server logs and it would be relatively trivial to find out who and were you lived from that information from your ISP.  

I’m afraid there’s more, your employer will have a full and exact list of all websites accessed, how long and when they were accessed.  I have sat in security meetings with huge charts displayed on the wall with the exact web sites that employees have accessed during the previous month and I can tell you there are some amazing sites!  Do these people know they can be traced I suspect not as they certainly wouldn’t be surfing those sort of sites at work if they did.

Anonymous Internet surfing by default simply doesn’t happen but it is possible.  The most basic way of protecting your identity is to use an anonymous proxy to hide your IP address when you are surfing.  Your communications can still be intercepted as the majority of that web traffic is in the clear but it’s less likely unless someone is deliberately targeting you, the main benefit is that your IP address is not left in the logs of the web servers and your web browsing will remain more private.

This is where many people make a really big mistake, this is what usually happens;

User decides they want keep their surfing anonymous

They search the internet for information and discover about anonymous proxies

They look for a list of free anonymous proxies and find one near them

They add the anonymous proxy settings to their internet browser and feel much more secure and private! 

Unfortunately as is often true, anything that is free on the internet often comes with a hidden cost.  Our privacy seeking internet surfer is indeed now masking their IP address from web servers they visit, all the logs will store the IP address of the proxy server as that is what is actually visiting the web site.  The Proxy server is then passing back all the requests back to the user, all the users web traffic now goes through this proxy server.

Of course many hacking groups realise the value of proxy servers for privacy and it is why you’ll often find these lists prepared by hacking groups themselves then carefully allowed to drift out onto the internet by various means.   Our hapless surfer may come across one of the many lists which are riddled by hacked servers which have had proxy servers installed onto them (usually without the owners knowledge).   These servers specifically are monitored and data logged – you are in fact sending all your web traffic directly to a bunch of criminals or hackers, not such a great idea.

This really happens and more often than you think so please if you are going to use an anonymous proxy, make sure it is legitimate and the owner can be trusted.   Don’t just use a free one you found on an internet list - not only will you have a limited anonymous internet surfing capability, you could very well be sending all data to a bunch of Eastern European Identity Thieves. 

Of course there are commercial and secure services that can secure your identity and protect your privacy.  I use a service which completely encrypts my who data stream with a US Military grade cipher (AES) and then uses a selection of high speed private proxies to make my browsing completely secure and anonymous and also safe from anyone who tries to eavesdrop.

Msndialup Yahoowebhosting

I

Aircraft manufacturers had, for some four decades, attempted to design the elusive DC-3 replacement with different powerplant types, including the piston-engined Convair 240/340/440 and Martin 2-0-2/4-0-4 series and the turboprop Vickers Viscount, Fokker F.27 Friendship, and Hawker Siddeley HS.748. The latest attempt had been made by the British aircraft industry when both de Havilland and Hawker Siddeley had conducted market research and formulated designs for a small-capacity, short-range airliner powered by pure-jet engines during 1959 and 1960.

Of the two, de Havilland, with its previous Rapide, Dove, and Heron pistonliners, had had considerable regional aircraft experience and had designed the world’s first pure-jet airliner in the form of the quad-engined DH.106 Comet. An initial study for such a DC-3 replacement, designated the DH.123, had featured a 60.6-foot overall length, an 81.3-foot wingspan, two 1,150 shp Gnone turboprops attached to a high wing, and a 22,100-pound maximum take off weight. So configured, it would have accommodated between 32 and 40 passengers, or slightly more than the DC-3’s standard 21 to 28.

De Havilland, subsequently taken over by Hawker Siddeley and redesignated the “de Havilland Division,” had forcibly discontinued design work on the DH.123 because it would have competed too closely with Hawker Siddeley’s own Rolls Royce Dart-powered Avro 748 which had seated 44. Nevertheless, existing turboprop competition, coupled with de Havilland’s belief that pure-jet technology would attract considerable passenger appeal, resulted in the mid-1960 DH.126 design proposal, which featured the later-standard configuration of most low-capacity, short-range twin-jets, such as the SE.210 Caravelle, the BAC-111, and the DC-9, with a swept wing, aft-mounted engines, and a t-tail. Powered by two 3,860 thrust-pound de Havilland PS92 jet engines, it had featured a 60.3-foot length for accommodation of 30 passengers and a 62-foot wingspan.

Several iterations had introduced progressive, although moderate wingspan, thrust, and gross weight increases by 1964, but further development had been hampered by four fundamental obstacles:

1. Suitable pure-jet engine availability.

2. Discontinuation of promising engine development because of several mid-1960s British engine manufacturer mergers.

3. Higher seat-mile costs over DC-3-like sectors for which the new design had been intended.

4. The inability to exploit a pure-jet airliner’s speed over relatively short sectors.

Hawker Siddeley, believing that the turboprop engine had only been interim-step technology, had equally embarked on a pure-jet airliner design program of its own long before the de Havilland merger, although its low-wing, aft-engined, t-tailed configurations had strongly resembled its former competitor’s.

Attempting to minimize development costs by utilizing the cockpit, forward fuselage, systems, and passenger cabin of its own Avro 748, it had proposed the HS.131 in 1964, which had featured similar 62.8-foot overall lengths and 67-foot wingspans as de Havilland’s comparable DH.126, but its projected 5,000 thrust-pound Rolls Royce RB.172 engines had enabled it to offer a higher, 30,000-pound gross weight and a 32-passenger capacity.

Faced, like de Havilland, with engine unsuitability and unavailability, Hawker Siddeley devised iterations round projected powerplants. A radical configuration change, introduced by the HS.136 of 1967, for instance, had resulted in a low-wing aircraft powered by two 9,730 thrust-pound Rolls Royce Trent engines with a conventional tail accommodating 57 passengers in a five-abreast cabin and offering a 54,000-pound maximum take off weight. Although the arrangement would have eliminated the aft-mounted, t-tail’s propensity toward deep-stall and flame-out conditions, and its close ground proximity would have facilitated passenger, aircraft servicing, and maintenance access, the potential for foreign object debris (FOD) engine ingestion had yielded to the proposed HS.144 two years later, which had once again reverted to the now standard aft-engine configuration.

Progressive design evolutions and dimensional and thrust increases had intermittently resulted in an airplane whose passenger capacity had been double that of the DC-3’s, and with the Rolls Royce bankruptcy-sparked discontinuation of Trent development in 1970, the DC-3 replacement, now powerless, had become ever more elusive.

This low-capacity, short-range jetliner had, like never before, hinged upon a powerplant for its existence, and the only potential lay with a small turbofan being developed by Avco Lycoming in the US. Based upon the 7,000 thrust-pound F102 which had powered the Northrop A-9A, the engine, a derated civil derivative designated ALF-502, had been launched in 1969 for the Canadair CL-601 Challenger business jet and had first run two years later. In order to offer commercial application, it had been of modular construction.

Because the type’s 6,500 thrust-pound rating had been inadequate for the latest aircraft design, the HS.146 of 1971, and because no other suitable powerplant had been in the development stage, the ultimate DC-3 replacement had been forcibly designed round four, not two, engines and it featured neither the standard, aft engine-mounted, t-tailed nor alternative wing-mounted configuration. Instead, it would sport two high, modestly swept wings to which the four turbofans would be pylon-mounted. Accommodating 88 passengers, or three times as many as the DC-3, the airliner, with an 86.2-foot length and 84.10-foot wingspan, had a 70,000-pound gross weight and 700-nautical mile range.

Nevertheless, the HS.146 offered several advantages over the earlier, standard-arrangement de Havilland and Hawker Siddeley design studies. Short-field performance, fully the equivalent of the turboprops it had intended to replace, had been attained by its thrust-to-weight ratio and wing, which, with 78-percent coverage of its trailing edge with Fowler flaps, had obviated the need for leading edge devices, and simplification and weight reduction had been further achieved with the elimination of thrust reversers. The t-tail, remaining from the earlier designs, had been retained in order to avoid engine and wing turbulence interference.

The four engine pods, which had been interchangeable with each other, housed modular construction cores built up of the basic fan, the accessory gearbox, the gas producer/compressor, and the combustion turbine sections.

An 11.8-foot fuselage diameter had permitted an internal, six-abreast coach seating arrangement, which had been double that of the DC-3’s.

In order to cater to different route demands, Hawker Siddeley offered an initial, 88-passenger HS-146-100 and a stretched, 102-passenger HS.146-200 version, both at maximum, six-abreast densities, although capacity could be reduced with varying class, seat pitch, and abreast arrangements.

Fully intended as a pure-jet counterpart to the turboprop Viscount, HS.748, and F.27, the HS.146 had been optimized for multiple daily, high frequency, short-range sectors from short and unprepared, gravel runways, yet achieve 15-percent lower direct-operating-costs than these aircraft. Slow, controlled approach speeds, of just over 100 knots, had been attainable by its aft fuselage, petal airbrakes and 40 degrees of trailing edge flap, permitting operation from 5,000-foot runways.

Hawker Siddeley had estimated a market of 1,500 aircraft of its type by 1982.

HS.146 program launch, based upon a 40 million British pound government backing and the manufacturer’s own investment, had occurred on August 29, 1973, and the first flight, of the short-fuselage HS.146-100, had been targeted for December of that year with certification following in February of 1977, while the stretched HS.146-200, coinciding with the seventh airframe, had been targeted for certification in August of 1978. A full-scale wooden mock-up had been intermittently built at Hatfield.

Like so many British commercial projects, its momentum had been abruptly arrested a little more than a year after it had been initiated. Escalating fuel prices resulting from the Arab-Israeli Yom Kippur War, changing economic conditions, and a general recession, coupled with the pending nationalization of the UK aircraft industry, had rendered the HS.146 program economically unfeasible by October of 1974. As a result, it had been halted, although small-scale engineering had continued and the aircraft’s drawings, tools, and jigs had been retained.

Three years later, on March 15, 1977, British Aerospace had been formed with the merger of Hawker Siddeley and the British Aircraft Corporation, and the design, redesignated BAe-146, had been relaunched. It had been the first to have been undertaken by the new conglomerate the following year, on July 10, 1978.

Rolled out for the first time three years later on May 20, 1981 at Hatfield, the aircraft, registered G-SSSH, became the first new British design since the BAC-111 had flown 18 years earlier.

The aircraft, in its original BAe-146-100 form, featured a pressurized, semi-monocoque, aluminum alloy/copper fuselage whose inner fuselage frames bore the aircraft’s bending loads and whose outer, notched rings carried the sheer loads, a construction technique which eliminated some 5,000 stringer/frame cleats. Its 11.8-foot diameter, permitting five- or six-abreast coach seating, had ensured that passengers would enjoy the same comfort on the type’s typical feeder routes as that offered by wide body aircraft operating long-range sectors to which they often transferred.

Single-class capacity varied from 71 in a five-abreast, 33-inch configuration to 82 at a six-abreast, 33-inch arrangement and an ultimate 93 at a six-abreast, 29-inch density. Total capacity decreased with a forward, 12-seat, first class cabin in a four-abreast configuration.

The aircraft had an 85-foot, 11½-inch overall length.

The wings, with an 86-foot span and 832-square-foot area, had featured a 15-degree sweepback and three degrees of anhedral at their leading edges. Due to the aircraft’s short, 150-nautical mile sectors, cruise speeds higher than its optimized Mach 0.7 had not been necessary and had therefore obviated the need for greater sweepback. Low-speed, short-field performance had been attained by means of its single-section, tabbed, trailing edge Fowler flaps which, with a 210-square-foot area, had covered 78 percent of the span and had been hydraulically operated by Dowty Rotol actuators. Roll control had been provided by manually-operated, trim- and servo tab-equipped ailerons, which operated in conjunction with each outer wing’s hydraulically-actuated roll spoilers. Three additional inboard spoilers served as lift dumpers after touch down.

Power had been provided by four Textron Lycoming ALF-502R-5 turbofans, each rated at 6,970 pounds of thrust, and these had replaced the lower-thrust, 6,700-pound ALF-502Hs originally intended for the design. Avco Lycoming had since become “Textron Lycoming.”

A total of 3,098 US gallons of fuel could be carried in two wing integral and one center section tank, the latter located above the passenger cabin and equipped with a vented and drained sealing diaphragm. The single-point pressure fueling had been located on the right wing, outboard of the number four engine.

The fixed horizontal tailplane, mounted atop the vertical fin, had not required the standard variable-incidence geometry because the absence of wing leading edge devices had eliminated the balance-out requirements ordinarily associated with the latter’s pitch changes. Its location, avoiding wing downwash and engine thrust interference, provided the greatest moment-arm, thus reducing required area and weight. Its elevators had been manually operated, while the vertical fin’s rudder had been hydraulically actuated.

Key to the BAe-146 design had been the 40-square-foot, hydraulically-actuated petal air brakes forming an integral, aerodynamic part of the tailcone at the extreme end of the fuselage and deployable to a maximum 60-degree position. Augmenting slow, controlled, increased descent rates, they had enabled the aircraft to descend at 7,000 fpm above 10,000 feet and 4,000 fpm below it, facilitating short-runway operation and eliminating the need for thrust reversers.

The aircraft’s hydraulically-operated, tricycle undercarriage had been comprised of a steerable, telescope strut-attached, forward-retracting nose wheel and two outboard-displaced main units which retracted inwards into blister-type fairings on the fuselage’s sides. All featured Dunlop wheels, while the main gear’s multi-disc carbon brakes had only been previously employed by Concorde.

Two 3,000-psi hydraulic systems powered the trailing edge flaps, the petal air brakes, the undercarriage, and the wheel brakes. A Garrett AiResearch GTCP 36-100M auxiliary power unit had provided cabin conditioning and engine starting power and had been operable up to 20,000 feet.

With an 84,000-pound maximum take off weight, the BAe-146-100 had an 880-nautical mile range with its maximum payload and a 1,620-nautical mile range with its maximum fuel.

First flying on September 3, 1981, on a one-hour, 35-minute fight at a 64,000-pound take off weight, the BAe-146-100 had been pronounced as “remarkably stable, very responsive, and delightfully quiet” by its test pilot and had been awarded its Civil Aviation Authority (CAA) type certificate on February 4, 1983. FAA certification followed three months later, on May 20.

Dan-Air Services, Ltd., the type’s launch customer, had placed two firm and two optioned orders the previous September, and inaugurated it into scheduled service on March 1, 1983, with an intermittently-provided aircraft from British Aerospace, on the London/Gatwick-Berne, Switzerland route, before it deployed its own aircraft on the route as of May 27. The BAe-146 had been the only pure-jet airliner which had been capable of operating from Berne’s short runway.

The larger, BAe-146-200, with a five-frame stretch, featured a new, 93.10-foot overall length and could accommodate 100 passengers in a six-abreast configuration at a 33-inch seat pitch or a maximum of 112 at a 29-inch pitch, but otherwise retained the BAe-146-100’s wingspan. The aircraft, with a 93,000-pound maximum take off weight, had a 1,130-nautical mile range with a full payload or a 1,570-nautical mile range with full fuel.

First flying on August 1, 1982 and registered G-WISC, the type had been inaugurated into service the following year, on June 27, by Air Wisconsin, which had placed an order for four firm and four optioned aircraft, configured for 100, on May 20, 1981, the same day that the shorter-fuselage variant had first rolled out. Joining a fleet of Fairchild Swearingen Metro IIs and de Havilland of Canada DHC-7 turboprops, the BAe-146-200 had been deployed on average, 127-mile route sectors, rarely climbing higher than 17,000 feet, and by the spring of 1984, it had served 16 mid-western cities, operating 14 daily sectors per day. It ultimately replaced the turboprops.

The largest single order, for 20 firm and 25 options, had been placed by another US regional carrier, Pacific Southwest Airlines (PSA), while other US operators had included Air-Pac of the Aleutian Islands in Alaska, Aspen Airways, Air-Cal, American Airlines, Discovery Airways of Hawaii, Presidential Airways, Royal West, USAir, and WestAir Commuter.

The BAe-146 had been the first pure-jet to have been certified to operate from London City STOLport, located in the docklands region, because of its steep approach capability, short-runway performance, and low noise emission.

In order to further expand its product line, offer increased passenger capacity, and more adequately compete with Fokker’s own advanced, stretched F.100, British Aerospace offered a second stretch over its original BAe-146-100, which had entailed 8.1-foot forward and 7.8-foot aft fuselage plugs in comparison to the BAe-146-200. The resultant version, the BAe-146-300, featured a strengthened center section fuselage and a new 100-foot, 8 ¼-inch overall length, but otherwise employed the same wingspan and ALF-502R-5 turbofans. Single-class, five-abreast capacity, at a 31-inch seat pitch, had been 103, although 128 high-density passengers, at a 29-inch seat pitch, could be accommodated with the addition of type III emergency exits installed in the center fuselage. The 97,500-pound variant, with a 1,040-nautical mile range with a full payload and a 1,520-nautical mile range with full fuel, had first flown on May 1, 1987, after the BAe-146-100 prototype (G-SSSH) had been converted to this standard and reregistered G-LUXE.

Air Wisconsin, again launch customer for the version, had taken delivery of its first longer-fuselage BAe-146-300 on December 10, 1988, one of five which had comprised its previous order for -200s.

A freighter version, the BAe-146-QT Quiet Trader, had been available in all three passenger versions. Incorporating an upward-opening, hydraulically-operated, 10.11-by-6.4 foot door on its aft, left side; a strengthened floor; and a loading system; the aircraft, devoid of passenger windows and facilities, could accommodate nine LD-3 containers or six 108-by-88 inch pallets of up to 6,000 pounds each and a single 53-by-88 inch half pallet. The prototype, a BAe-146-200 converted by Hayes International Corporation, had first flown on March 20, 1986 and had been inaugurated into service by TNT International Aviation Services the following year on May 5. The operator had subsequently acquired a considerable number of them.

II

A representative BAe-146-200 flight, operated by Air Zimbabwe from Hwange to Kariba, had been taken in September of 1994.

Founded in 1967 as Air Rhodesia to operate the Rhodesian routes of Central African Airways, the carrier, continually changing as a result of increased black majority rule, had been redesignated Air Rhodesia-Zimbabwe in 1979 and, simply, Air Zimbabwe the following year after the country had attained independence. The transition period, fraught with political instability, had sparked constant route structure realignment, which had only encompassed South Africa.

When the internal situation had ultimately been restabilized, the route system had been gradually reestablished, once again offering connections between Zimbabwe and many regional African nations, as well as those in Europe. In 1982, Air Zimbabwe had operated eight Viscounts, three 720Bs, and three 707-320Bs, although additional 707s had later replaced the 720s.

Due to deregulation-spawned competition, the small carrier had increased its efforts to remain competitive with improved passenger service and a more modern, three-type fleet which had included one BAe-146-200, three 737-200s, and two 767-200ERs, serving the five Zimbabwean domestic destinations of Bulawayo, Harare, Hwange, Kariba, and Victoria Falls; the 11 African international destinations of Dar-es-Salaam, Durban, Gabarone, Johannesburg, Lilongwe, Lusaka, Manzini, Maputo, Mauritius, Nairobi, and Windhoek; and the three European intercontinental destinations of Frankfurt, Larnaca, and London.

In June of 1983, it had embarked on a “Customer Care Program” to improve service and introduce a new Executive Business Class on its two widebody aircraft in order to more effectively compete with the larger, international carriers which had operated between Europe and Africa.

It had toted three slogans: “A Tradition of Caring,” in 1989; “Above All, We Care,” in 1992; and “Experience our Commitment to Excellence,” in 1994.

Its self-stated goal had been “to be the airline that best meets the needs of the customer, to operate profitably, and to contribute to the development of Zimbabwe using the skills and talents of a committed workforce.”

The BAe-146-200 operating the day’s flight, registered Z-WPD and named “Jungwe,” had been configured with 91 single-class, six-abreast seats and had been fitted with a passenger audio system. Routed from Victoria Falls to Hwange, Kariba, and Harare under flight number “UM 229,” it operated three sectors spanning 30 minutes, one hour, and 45 minutes in duration.

After boarding from the single terminal by means of its forward, left airstair, the high-wing, quad-engined British regional jet, sporting its colorful black, red, yellow, and green striped livery, executed a lengthy taxi roll on the concrete runway flanked on either side by Hwange National Park’s dry, brown grass and scrub expanses, periodically interspersed by feeding herds of impalas.

Completing its “Before Take Off” checklist, and extending its trailing edge Fowler flaps to their 24-degree position, the aircraft throttled into its acceleration roll, its four ALF-502R-5 turbofans propelling its 35,500-kilo mass with their 6,970 pounds of thrust into life-generating speed. Leveraging itself into rotation at 112 knots with its horizontal tail-hinged elevator, the BAe-146 surrendered itself to the hot African atmosphere at a 118-knot V2 velocity, retracting its tricycle undercarriage and accelerating through a 171-knot VFTO speed toward the gray, obscuring ceiling.

Leaning into a right bank over the brown and tan African expanse at 4,200 feet, the BAe-146 retracted its flaps from the 24- to the 0-degree position, completing its “After Take Off” checklist. Ascending through 7,600 feet, at which time a 291-knot ground speed had been registered, it maintained a 1,800-fpm climb rate. Its NAV indicated a 135.4-mile distance to Kariba.

Plunging through the dirty opaque obscurity at 15,780 feet, Fight 229 triumphed over white, mountainous-appearing cumulous, now unrestrictedly bulleting through the illustriously-blue mid-afternoon purity at 18,640 feet.

Inching the throttle back a moment later, the British regional liner settled into its 21,000-foot level off plateau at a 354-knot ground speed with 97.7 miles remaining to its destination.

Cabin service on the one-hour domestic sector had included a selection of sodas, mineral water, orange juice, and lemonade and a snack try of potato chips and peanuts.

The ground speed had pinnacled at 411 knots.

Descent, initiated with 54 miles remaining on its flight plan, had been attained by dialing in 5,500 feet in the cockpit’s “ALT SEL” autopilot, resulting in a 2,000-fpm descent rate.

Surrendering once again to the dense, reference-losing obscurity of the cloud deck, the aircraft plunged through 10,000 feet at a 260-knot speed with 21 miles remaining to Kariba, extending its petal air brakes at 7,000 feet, which produced a very controlled, but drag-induced profile. An altitude of 4,500 feet had been intermittently dialed into the “ALT SEL” window.

Emerging from the ceiling mist over the baby blue of Lake Kariba, which had been outlined by its dry, tan and brown scrub shoreline, the captain consulted his landing flap chart corresponding to a 34,500-kilo weight.

Extending its Fowler flaps to the 18-degree position at 3,600 feet, at which time 6.4 miles had remained on its flight plan, the airliner unleashed its undercarriage at a 162-knot ground speed and actuated its high-lift devices into the 24-degree position while arcing into a left bank over the parched expanse of desert. Black mountain silhouettes rolled into view ahead of the cockpit windows.

Descending through 2,600 feet at a 161-knot ground speed, the BAe-146-200, now sporting 33 degrees of trailing edge flap, maintained a 270-degree heading, the runway, seemingly plowed between brown straw, visible through the windshield.

Extending its petal air brakes to the 60-degree position, the aircraft, at a negligible descent rate, passed over Runway 27’s threshold at 120 knots, retarding its throttle and flaring into main undercarriage contact with the sizzilingly hot concrete. Decelerating with significant brake applications, and with its spoiler handle already deployed to the “LIFT SPLR” position, the thrust reverser-devoid quad-jet consumed the centerline with its nose wheel until it had reached its other threshold and could execute a 180-degree turn.

Taxiing toward the single terminal’s ramp amid the sweltering, 94-degree heat, the high-wing, t-tailed airliner, although ordinarily minuscule next to an intercontinental wide body, dwarfed the United Air PA-23 Aztec and collection of private pistons now parked around it.

The BAe-146 had, as evidenced by this sector, served as Zimbabwe’s link between its often road-unconnected cities and communities.

III

Although the British Aerospace BAe-146 had only sold 219 examples of all of its versions to 45 world airlines, it had nevertheless formed the basis of its later, more advanced, Textron Lycoming LF507-powered Avro RJ70, RJ85, and RJ100 derivatives.

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Cyprus is the third largest island in the Mediterranean and Northern Cyprus is almost half of the coastline of Cyprus.

About the ideal climate of Northern Cyprus and pleasures, which long ago for visitors!

North Cyprus lies about 70 miles south of Turkey and enjoys a fantastic eastern Mediterranean climate with long hot summers and short mild winters, the average water temperature is above 20 º C for more than half of the years , for which North Cyprusan average of 320-340 days of sunshine a year make it a favorite for years tourists.

The coastline of North Cyprus offers some of the best and safest bathing in the Mediterranean Sea, and the clear waters of the Mediterranean Sea offers delights for swimmers, snorkeling, scuba divers, sailors, water skiing and fishing are.

Precipitation of Northern Cyprus' is low and is concentrated in December and January – and the rain, there is a good thing, unlike the rain in Northern Europe! Rainbring the wild flowers, for which North Cyprus is also known, they carpet the island in spring and varieties are diverse and include more than 38 species of orchids alone! In addition, the fragrance of orange, lemon, lime and grapefruit blossoms and your senses will be found by the aromatic and visual beauty of North Cyprus.

About Northern Cyprus, its scenery and attractions.

The fertile northern coastal strip is now considered one of the most beautiful natural AcceptedAreas in the world to live in too. It offers lush scenery and behind the spectacular backdrop of mountains Besparmak is also known as the Kyrenia or Girne Mountains are.

The mountains are steep and breathtaking and decorated with medieval castles and ruins. The steep slopes are those for pine forests, olive and carob trees and you'll find many a picturesque village in!

In the land behind the rocky mountainRange and the imposing Five Finger Mountain you will find the enormous level Mesaoria fertile. From here you reach Ercan airport and the island's capital Nicosia, or Lefkosa.

If you travel along the east coast is the walled city of Famagusta or Gazimagosa find and near the ruins of Salamis. In the north-east, the landscape turns into small pastures enclosed by stone walls and dotted with olive trees and rocks. The beaches along the coastHere are a blend of rock pools and sheltered sandy bays.

Simply put, the contrasting landscapes in North Cyprus breathtaking – from the delicate jewel of the port of Kyrenia Besparmak to the imposing mountains, its beautiful coastline of pristine stretches of beach and isolated secret coves, Northern Cyprus is an incredible place.

You'll be spoiled when you visit, and you will need more and more! When you visit Northern Cyprus is the turkishPeople of Cyprus in the warmer, more generous and welcoming people, is legendary, in fact, their friendship. And if you decide to Northern Cyprus at home – whether permanently or declare in a few weeks a year for the holidays – they are, they are generally happy.

About Northern Cyprus, accessibility, and knowledge of Northern Cyprus.

Since the Republic of Cyprus joined the EU in May 2004, the Green Line between the north and south of the 'island is open forThe holders of the EU – is to visit not only free for EU citizens in the north and south of the island.

Northern Cyprus has an airport called Ercan – You can fly from here to Istanbul and in collaboration with international flights, or you can by here in the UK and Germany, flying for example. You can also navigate and the northern part of Cyprus by Turkey. The airports of Larnaca and Paphos are also accessible if you want to travel to Northern Cyprus and there are many taxi companies, which willTransfer destination of choice in the northern part of Cyprus.

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Cyprus is famous for its year-round So so only one of many reasons that make this beautiful island popular with tourists. When the holidays with family and are looking for a goal that all parties are satisfied you have problems, you can find a better place. If you are chilling on the beach, climb a mountain, or test your skills on some of the best golf courses in Europe, is everything.

Cyprus holidays offer excellent opportunities to play golf with the mostOf course, Aphrodite Hills is the most popular, and it is easy to see why. This beautiful championship course offers a surprising, particularly the 7th hole, which is the T-pieces of a large ravine to a green surrounded by olive trees.

If hiking is your thing, you are sure to love the mountain roads of Cyprus. Mount Olympus is the highest and most central zone and has much to offer, including, traditional villages, vineyards and beautiful scenery. Of course, if all that sounds just abit 'too much like hard work, you can only dream of days away on the beaches of the upper class, able to offer rental Cyprus. In particular, the area of Protaras has some of the best beaches in Cyprus has a wonderful golden sand and crystal clear water that stretches for miles along the coast.

Cyprus holidays offer a lot of fun for the younger members of the family including the wonderful Mazotos Golden Mile, between Limassol and Larnaca, isFeatures camel, the Ark of Noah, with a variety of animals, a playground for adults and a restaurant open for business. To speak of a journey for the whole family believes that there is nothing better than a holiday in Cyprus.

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Create a site of an act is not much, if we equate for the breeding of other technical achievements. Many people tend to leave, and to pack just find the word "programming" and "technical". Estimate it `sa bit 'far from a really worthwhile to buy a full computer language." Hypertext Markup Language, the most common computer language on site is actually pretty easy to interpret, take all the time that we have theParticipation in the acquisition of new questions.

What is Hypertext Markup Language?

HTML stands for Hyper Text Markup Language. The acquisition, you only think of them as a language of communication that the computer reads. For example, as humans, we were brought another linguistic process *, that is, as the nomenclature HTML is primarily and specifically used for the production of a website. The Web browser such as Microsoft Internet Explorer or Mozilla Firefox, will thenTranslate encrypt and decrypt, or better, Language (HTML) and displays them in a sense, we can see exactly the same thing in a simple website.

Written in code.

Encrypting the HTML language might be a little 'difficult * for a few people, so that we can actually buy software like Macromedia Dreamweaver or Microsoft FrontPage. These programs are only that individuals make in the design of professional qualificationsWeb pages / websites.

Additionally, you may also access the online web-builders, manufacturers, which are linked to the website and can be manipulated by the World Wide Web There are many different manufacturers, especially online.

To complement the guides and magazines that offer support in the extension exercises and know-how to our own personal sites. Internet tutorials also are compelling, as in the modern world, information technology is the cheapest and mostAgency costs of professional training, especially abnormally in this area.

Then, you start and build immediately. If you enjoy coding, it could also last for a free time.

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The safety of the consumer product information on the card account for the success of the company e-commerce is essential. Before moving products and services online, consumers want to be sure that their account information is safe and not be questioned and abused. This need is a credit card and forces companies to create a program that regulates the procedures that are e-commerce merchants can implement in their businesses to protect sensitive personal data, ad.

AllDealers are required to meet the requirements established in the Payment Card Industry (PCI) Data Security Standard (DSS). The default is the result of a collaboration between Visa and MasterCard to create common industry security requirements for protecting sensitive information of the cardholder. Other credit card companies are the norm in their respective programs. The CIP is composed of twelve basic requirements, grouped into seven standards.

Create and maintainSecure Network:
Installation and maintenance of a firewall to protect data.
Do not use vendor-supplied passwords and other security parameters.
Protect cardholder data:
Protection of stored data.
Encrypt transmission of card data and sensitive information across public networks.
Maintain a Vulnerability Management Program:
Use and regularly update anti-virus software.
Develop and maintain secure applications.
Strong Access Control ImplementationActions:
Restrict access to data on a need-to-know basis.
Assign a unique ID to each person who has access to computers.
Restrict physical access to cardholder data.
Regularly monitor and test networks:
Track and monitor all access to network resources and cardholder data.
Be regularly tested security systems and processes.
Maintain an Information Security Policy:
Maintaining a policy that addresses information security.

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Web-based or hosted CRM applications have come as a big advantage for small businesses, which have so far been reluctant to even consider CRM to their business. This is because the cost of CRM on-premise was too much for SMEs.

The advent of Web-based CRM, has small and medium enterprises, the benefits of CRM in a fraction of the cost of enjoying CRM on-premise. Companies, large or small, essentially the same requirements of a CRM system. Small and medium businesses now have a requestSuites available, can play the big players in their activities.

Past, small businesses were forced to their society based on rules of thumb and the game by ear regarding the marketing strategies of the customers. Small and medium-sized businesses have had with spreadsheets and discrete software on different machines that are loaded very difficult to extract information on the data.

Benefits of Web-based CRM software for SMB include

Low Cost 1)Installation and low TCO – The offer interesting for a SMB. Low cost of entry, because the costs with the selected number of users and modules. Similarly, you should question the costs over a number of people using the software hosted.

2) Ease of application – much easier to implement, compared to CRM on-premise. You can adjust the forms for your company. There are vendors offering hosted CRM is already customized for various industries. Businesses would be more time for the user safelyBuy-in.

3) accessibility – a big advantage in hosted CRM is that you can conduct your business in motion, until you have an Internet connection. Sales force the right information at the right time. Conversion of lead can be rationalized. Telemarketing is facilitated.

4) the minimum or servers – Web-based CRM is the infrastructure requirements of an SMB. This gives space that can be used for other purposes. IT staff requirement is minimized, which is an additional costSave.

5) Security – An SMB can not be better equipped to manage the security of confidential company information and customer data. But a hosted CRM vendors is to ensure the ability to encrypt data and data security, avoiding any kind of hacker attacks

Small and medium-sized enterprises now have the resources to companies on the move with the help of a behavior online CRM. Whether you're a high-growth companies or mid-market, a seller or provider of online services provides access to a CRM,Able to optimize your employees. Take a look around before you sign for CRM to better organization. Many CRM solutions on-line, notably the open source ones are offered for free. Some manufacturers offer a solution to single-user for free.

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What is the big thing in less than a version of Windows 7 more than the others? Whichever version you need? Second, it is better for you?

In this article, my goal is to show the hidden and the obvious differences between the three versions of Windows 7, the fans: Home Premium includes Windows 7, Windows 7 Professional, and Windows 7 Ultimate.

First, how do I start with my hand in front of hidden. The most obvious is the color ofPackaging (Home Premium is the orange, green is the professional and the Ultimate is black) and the price. The Ultimate version is the most expensive of the three, followed by the professional then the Home Premium.

The Ultimate is the most versatile and powerful Windows-7 combines remarkable ease of use with the entertainment features of Home Premium and the business of professional skills, including the ability to remove the productivity running in Windows XP. Formay introduce additional security with BitLocker to encrypt the data. And for added flexibility, it is possible in each of 35 languages.

Let us now perform the functions of Windows 7 and what version of these functions is possible.

Windows-7 do things that are not consumed every day more easily, more desktop menu that allows you to display files that are used regularly in only two clicks. The snap navigation that lets you organize two widows side by side only pullingtheir opposite sides of the screen. The obtained Aero Peek, which allows you to look behind the window open at a quick glance at your desktop. Finally, the search for Windows that allows you to open any file on your PC, documents, emails, allowing songs directly from the Start menu. These functions are included in all three versions of Windows 7

Now the next feature is … makes the Web experience faster, easier and safer than ever with Internet Explorer 8 All three versionscan.

Watch many of your favorite TV shows for free, anytime, anyplace with Internet TV. You can also pause and rewind TV programs record. This function can be preserved in all three versions.

Another function of the share with three others, have in common is the ability to create a home network and connect your PC to a printer with Home Group.

Now that the three common characteristics and the difference between the beginning has come to a.

The ability to perform manyWindows XP productivity applications in Windows XP mode is no longer in Windows 7 Professional and Ultimate.

Connect to corporate networks, it's easy and secure with more entering the domain, and ending on the Professional and Ultimate.

Easy Data Recovery Automatic Backup on your home or office network can be found only on professional and Ultimate.

There are, what we have in common the following services:

The possibility of protecting your data on your PC and laptopStorage devices against loss or theft with BitLocker.

Work in the language of your choice, or switch between any of 35 languages.

The last two functions can be found only in Windows 7 Ultimate.

Now we're talking about the difference in hidden … Obviously, there is no other obvious difference in hidden, because all important functions have been explored. The only thing I might add, as it is, is that unless you plan to encrypt the hard drive, now or in the future andWorking with multiple languages, which are found only in Windows 7 Ultimate, then I suggest you stick to Windows 7 Professional, all the media capabilities of Windows 7 and Home Premium and Business features in Windows 7 Ultimate.

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Software anti-spyware, anti-virus and a good personal firewall offers the best protection against most types of threats that exist today. Although each of the Internet should use these products, I find that most casual users of the Internet to run only one antivirus program. Without the added protection of a software firewall and anti-spyware software, there are some things you can do to ensure that your personal information receivedTheft by spyware, and you are not a victim of identity theft through phishing attacks.

The following is a list of computer security tips to help people, and / or minimize the damage, if your personal information is stolen:
Never use the same user ID that you e-mail or the Internet to record something else. Maintaining separate user ID for the key accounts to minimize the risk to safety in case someone gets hold of your identity.
Never useYour e-mail password for everything else. This prevents unauthorized access to your email account.
Passwords in an encrypted file or a program manager with password encryption. This will ensure that your passwords in any case an intruder or password to get spyware application list.
Never click on links in emails, especially from banks. Manual Go to the site and recorded this is one of the most common phishing scams. Unscrupulous people, sending emails,Look legitimate. The links they give you usually get a copy of a legitimate site. Enter your account information to these fraudulent websites allow thieves access to your account real gain.
If you absolutely must download and install freeware ever. If you download our software free for download from the developer. Imitators there are many sites that are fraudulent. Download one of them will certainly be able to install spyware on your system.
Use the parentsControl software, if children use the computer. This prevents access to objectionable sites where spyware can be installed on the sly.
Browser (Internet Explorer, Firefox, etc …) the security setting should be too high. This prevents many sites to install certain types of spyware and adware on your PC.
Never click on pop-up ads, as this spyware may be installed on your system. One click is enough to have secretly installed spyware.
Avoid browsing questionable Web sites. SitesThat no illegal, immoral or indecent, are also havens for spyware. Just some of these pages is all that is needed to infect your computer with spyware.
Excessive pop-ups usually say, adware is installed on your system. Use an adware remover to locate and destroy. A good rule is to not click on an advertisement pop-ups, they may install spyware on your system.
If your computer seems to be very slow, suspect spyware. Install a spyware remover and a PC.

These suggestionsare not a substitute for anti-spyware software and a personal firewall, but it should help to ensure that it remains secure until you reach the computers are properly protected.

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