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Lockheed L-188 Electra

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Lockheed L-188 Electra
NameLockheed L-188 Electra
TypeTurboprop airliner
National originUnited States
ManufacturerLockheed Corporation
First flightDecember 6, 1957
IntroductionJanuary 12, 1959 with Eastern Air Lines
StatusIn limited service
Primary usersEastern Air Lines (historical), American Airlines (historical), National Airlines (historical), KLM (historical)
Produced1957–1961
Number built170
Unit cost$2.4 million (1960)

Lockheed L-188 Electra is a American turboprop airliner designed and built by the Lockheed Corporation in the late 1950s. It was the first large turboprop airliner produced in the United States and entered service with Eastern Air Lines in early 1959. The aircraft was developed to compete with the Vickers Viscount and other emerging jetliners, featuring a low-wing design and four powerful Allison 501-D13 engines.

Development and design

The Lockheed Corporation initiated the L-188 project in 1955 following a request from American Airlines for a high-speed, medium-range airliner. The design team, led by renowned engineer Willis Hawkins, opted for a turboprop configuration to balance operating economics with performance, competing against the British Vickers Viscount. The aircraft's airframe was entirely new, featuring a semi-monocoque fuselage and a T-tail empennage for improved control. Key design goals included short-field performance for operations at airports like LaGuardia Airport and the ability to carry over 90 passengers. The Electra was powered by four Allison 501-D13 turboprop engines, each driving a distinctive three-bladed Aeroproducts propeller. The first prototype, registered N1881, made its maiden flight from Lockheed Air Terminal in Burbank, California on December 6, 1957, piloted by Herman "Fish" Salmon and Roy Wimmer.

Operational history

The Lockheed L-188 Electra entered commercial service with Eastern Air Lines on the New York to Miami route on January 12, 1959, followed quickly by American Airlines. Other major operators included National Airlines, Western Airlines, and Braniff International Airways. Internationally, carriers like KLM, Garuda Indonesia, and Ansett-ANA also utilized the type. Its speed and comfort were praised, but its career was significantly impacted by a series of early catastrophic accidents, leading to an extensive and costly modification program known as the "LEAP" (Lockheed Electra Achievement Program). After being phased out of major passenger service by the late 1960s due to the arrival of jets like the Boeing 727, many airframes were converted into dedicated cargo aircraft. A significant number were modified into P-3 Orion-like configurations for firefighting and reconnaissance roles, with companies like Hemet Valley Flying Service and Aero Union operating them extensively. Several remain in service today in these specialized roles.

Variants

* L-188A: The initial production model, certified for up to 99 passengers. * L-188C: A longer-range variant introduced in 1959, featuring increased fuel capacity and a higher maximum takeoff weight. This model was operated by carriers such as KLM and Pacific Southwest Airlines on longer overwater routes. * L-188AF (All Freight): A factory-produced cargo variant. * L-188PF (Passenger/Freight): A convertible passenger/freight model. * Numerous aftermarket conversions were performed, most notably the "Electra Freighter" and various firefighting conversions like the "Aero Firefighter" and "Orion 200" by companies including Marshall Aerospace and Hemet Valley Flying Service.

Operators

Primary civil airline operators included Eastern Air Lines, American Airlines, National Airlines, Western Airlines, Braniff International Airways, Pacific Southwest Airlines, KLM, Garuda Indonesia, Ansett-ANA, and Air New Zealand. Military operators included the United States Navy and the Argentine Air Force. In its later cargo and firefighting career, major operators have been Hemet Valley Flying Service, Aero Union, Buffalo Airways, and Conair Aviation.

Accidents and incidents

The Electra's service history was marred by several high-profile crashes shortly after introduction. The most significant were Braniff International Airways Flight 542 near Buffalo, Texas in September 1959 and Northwest Orient Airlines Flight 710 near Tell City, Indiana in March 1960. Investigations, led by the Civil Aeronautics Board, determined these were caused by a previously unknown phenomenon called "whirl-mode" aeroelastic instability, which led to catastrophic engine nacelle and wing failure. This prompted the Federal Aviation Administration to mandate the extensive "LEAP" program, which involved structural reinforcements to the engine mounts and wing. The modifications were successful, and the aircraft returned to service with a strong safety record thereafter.

Specifications (L-188A)

* **Crew:** 3–4 flight deck + cabin crew * **Capacity:** 85–99 passengers (typical) * **Length:** 104 ft 6 in (31.85 m) * **Wingspan:** 99 ft 0 in (30.18 m) * **Height:** 32 ft 10 in (10.00 m) * **Empty weight:** 61,500 lb (27,895 kg) * **Max takeoff weight:** 113,000 lb (51,256 kg) * **Powerplant:** 4 × Allison 501-D13 turboprop engines, 3,750 shp (2,800 kW) each * **Propellers:** 3-bladed Aeroproducts constant-speed fully-feathering propellers * **Maximum speed:** 448 mph (721 km/h, 389 kn) * **Cruise speed:** 405 mph (652 km/h, 352 kn) * **Range:** 2,200 mi (3,500 km, 1,900 nmi) * **Service ceiling:** 28,400 ft (8,700 m) * **Rate of climb:** 1,800 ft/min (9.1 m/s)

Category:Airliners Category:United States airliners 1950–1959 Category:Four-engined turboprop aircraft