Company type | Private |
---|---|
Industry | Aerospace Logging |
Founded | 1963 |
Headquarters | Perkasie, Pennsylvania, U.S. |
Products | Commercial helicopters |
Website | carsonhelicopters.com |
Carson Helicopters, Inc is a helicopter operating company based in Perkasie, Pennsylvania, United States. Carson operates a fleet of Sikorsky S-61 helicopters in aerial lift services and aerial firefighting. Carson is known for its development of the "Carson Blade" for the S-61 and H-3 Sea King. [1] In 2010, Carson Helicopters, Inc. partnered with Sikorsky Aircraft to develop and manufacture the S-61T, an upgraded version of the S-61 helicopter. [2]
In 2015 former VP Steve Metheny was sentenced to prison for falsifying documents that led to a 2008 crash that killed seven firefighters and two pilots. [3] A federal jury had earlier found that the primary cause of the crash was the failure of the GE designed engine, specifically issues with the engine's fuel control, of which GE had previously been notified. [4]
In 2007, Carson Helicopters partnered with the British Royal Navy to modernize its British HC4 Sea King Helicopters because British forces faced issues operating the Sea Kings in Afghanistan due to the country’s altitude above sea level and lower air density which contributed to a dramatic decrease in lift and forward speed. [5]
The upgrades included the replacement of the aircraft’s legacy metal main rotor blades with the Carson Composite Main Rotor Blade and to use Agusta Wesland’s five-bladed composite tail rotor. Within 12 months after installation, the upgrades were tested and deployed after receiving a UOR from the MoD.
The increased performance provided by the Carson Composite Main Rotor Blades enabled the aircraft to operate at its operational and design capability in hot-and-high environments without having to strip weight or decrease defensive aids, such as armor or weaponry and its associated ammunition. [6]
In February 2010, the U.S. State Department signed an open-ended contract for as many as 110 Sikorsky S-61 Triton Helicopters ("S-61T") for U.S. diplomatic transportation and cargo services. [7]
The S-61T, which was an upgraded SH3H, included a fully modernized glass cockpit with digital screens and avionics, crashworthy seats, a modular wiring harness derived from the UH-60 Black Hawk, as well as engine and transmission improvements. Upgrades also included the Carson Composite Main Rotor Blades which provided a 10 knot increase in cruising speed using the same horsepower and a 1750 lb. increase in lift. [6]
The CarterCopter is an experimental compound autogyro developed by Carter Aviation Technologies in the United States to demonstrate slowed rotor technology. On 17 June 2005, the CarterCopter became the first rotorcraft to achieve mu-1 (μ=1), an equal ratio of airspeed to rotor tip speed, but crashed on the next flight and has been inoperable since. It is being replaced by the Carter Personal Air Vehicle.
The Sikorsky CH-53E Super Stallion is a heavy lift helicopter operated by the United States military. As the Sikorsky S-80, it was developed from the CH-53 Sea Stallion, mainly by adding a third engine, adding a seventh blade to the main rotor, and canting the tail rotor 20°. It was built by Sikorsky Aircraft for the United States Marine Corps. Developed in the 1970s, it entered service in 1981, and is planned to be in service into the 2030s. It is one of the largest helicopters, and military helicopters in service, and is operated from U.S. Navy ships or from land.
The CH-53 Sea Stallion is an American family of heavy-lift transport helicopters designed and built by the American manufacturer Sikorsky Aircraft. The Sea Stallion was originally developed in response to a request from the United States Navy's Bureau of Naval Weapons made in March 1962 for a replacement for the Sikorsky CH-37 Mojave helicopters flown by the United States Marine Corps (USMC).
The Sikorsky S-76 is a medium-size commercial utility helicopter designed and produced by the American helicopter manufacturer Sikorsky Aircraft. It is the company's first helicopter specifically developed for the civilian market.
The Sikorsky CH-148 Cyclone is a twin-engine, multi-role shipborne helicopter developed by the Sikorsky Aircraft Corporation for the Canadian Armed Forces. A military variant of the Sikorsky S-92, the CH-148 is designed for shipboard operations and replaced the CH-124 Sea King, which was in Canadian Armed Forces operation from 1963 to 2018.
The Sikorsky S-92 is an American twin-engine medium-lift helicopter built by Sikorsky Aircraft for the civil and military helicopter markets. The S-92 was developed from the Sikorsky S-70 helicopter and has similar parts such as flight control and rotor systems.
Copterline Flight 103 (AAQ103) was a Copterline helicopter flight en route to Helsinki, Finland from Tallinn, Estonia that crashed into the Tallinn Bay on 10 August 2005, at 12:45 local time.
The Schweizer S300 series family of light utility helicopters was originally produced by Hughes Helicopters, as a development of the Hughes 269. Later manufactured by Schweizer Aircraft, and currently produced by Schweizer RSG, the basic design has been in production for over 50 years. The single, three-bladed main rotor and piston-powered S300 is mostly used as a cost-effective platform for training and agriculture.
A coaxial-rotor aircraft is an aircraft whose rotors are mounted one above the other on concentric shafts, with the same axis of rotation, but turning in opposite directions (contra-rotating).
The Sikorsky S-64 Skycrane is an American twin-engine heavy-lift helicopter. It is the civilian version of the United States Army's CH-54 Tarhe. It is currently produced as the S-64 Aircrane by Erickson Inc.
The Sikorsky CH-53K King Stallion is a heavy transport helicopter designed and produced by Sikorsky Aircraft. The King Stallion is an evolution of the long running CH-53 series of helicopters which has been in continuous service since 1966, and features three up-rated 7,500 shp (5,590 kW) engines, new composite rotor blades, and a wider aircraft cabin than its predecessors. It is the largest and heaviest helicopter in the U.S. military.
A helicopter is a type of rotorcraft in which lift and thrust are supplied by horizontally spinning rotors. This allows the helicopter to take off and land vertically, to hover, and to fly forward, backward and laterally. These attributes allow helicopters to be used in congested or isolated areas where fixed-wing aircraft and many forms of short take-off and landing (STOL) or short take-off and vertical landing (STOVL) aircraft cannot perform without a runway.
The Sikorsky H-53 is a family of military helicopters built by Sikorsky Aircraft. H-53 is its United States military designation; the company has several designations for it including S-65, S80, and S-95.
The Sikorsky S-61L and S-61N are civil variants of the SH-3 Sea King military helicopter. They were developed and produced by the American helicopter manufacturer Sikorsky Aircraft.
Los Angeles Airways Flight 417 was a Sikorsky S-61 helicopter that crashed on August 14, 1968 in the city of Compton, California. All eighteen passengers and three crew members were killed. The aircraft was destroyed by impact and fire. According to the National Transportation Safety Board the probable cause of the accident was fatigue failure. The accident happened when the yellow blade, one of five main rotor blades, separated from the spindle that attached the blade to the rotor head. Following failure, the helicopter was uncontrollable and it fell to the ground. The fatigue crack originated in an area of substandard hardness and inadequate shot peening.
Los Angeles Airways Flight 841 was a Sikorsky S-61 helicopter that crashed at 5:50 p.m. on Wednesday, May 22, 1968, in the city of Paramount, California. All twenty passengers and three crew members were killed. The aircraft was destroyed by impact and fire. The probable cause of the accident was a mechanical failure in the blade rotor system, which then allowed one blade to strike the side of the fuselage. As a result, the other four blades were thrown out of balance. All five rotor blades then broke and the rear fuselage and tail separated from the rest of the airframe. The cause of the mechanical failure is undetermined. At the time, it was the worst helicopter-related accident in U.S. aviation history, not to be surpassed until the 1986 Grand Canyon mid-air collision which killed 25.
The Sikorsky S-97 Raider is a high-speed scout and attack compound helicopter based on the Advancing Blade Concept (ABC) with a coaxial rotor system under development by Sikorsky Aircraft. Sikorsky planned to offer it for the United States Army's Armed Aerial Scout program, along with other possible uses. The S-97 made its maiden flight on 22 May 2015.
The Bell 525 Relentless is an American super-medium-lift helicopter, under development by Bell Textron. The Bell 525 was unveiled at the 2012 Heli-Expo in Dallas, Texas in February 2012. The helicopter first flew on 1 July 2015. It is designed to transport up to 19 passengers. The aircraft is the first fly-by-wire civilian aircraft and suffered a crash of its prototype, and is still slowly working towards certification. As of 2024, Bell is still working towards completing flight certification it has secured its first order.
The Sikorsky S-73 was a proposed aircraft design to meet the United States Army requirement in 1970 for a Heavy Lift Helicopter (HLH) capable of carrying 45,000 lb, a lifting capacity more than twice that of Sikorsky's most powerful helicopter at that time.
The 2016 Bell 525 Relentless prototype crash occurred during a test flight on July 6, 2016, near Italy, Texas, destroying the prototype Bell 525 Relentless helicopter and killing the two occupants. The helicopter broke up in flight while traveling about 229 mph (199 kn) at an altitude of about 2,000 feet (610 m); the main rotor contacted and severed the tail boom due to severe vertical oscillations. The crew were performing one engine inoperative (OEI) recovery testing; the test induced a scissors-mode vibration in the main rotor, which resulted in involuntary collective control input. The unintended biomechanical feedback loop exacerbated the vibration, until the rotor contacted the tail-boom.