Convair CV-240 family

From Wikipedia, the free encyclopedia
Jump to: navigation, search
CV-240 family
CV-240 / CV-300 / CV-340 / CV-440 Metropolitan / CV-540 / CV-580 / CV-600 / CV-640 / CV5800
Convair-240-color.jpg
A restored Convair CV-240 in Western Air Lines livery, at the Planes of Fame Museum in Chino, California, USA
Role Airliner
Manufacturer Convair
First flight March 16, 1947[1]
Introduction February 29, 1948 with American Airlines
Primary user American Airlines[1]
Produced 1947–1954[1]
Number built 1,181[1]
Variants Convair C-131 Samaritan
Canadair CC-109 Cosmopolitan[1]

The Convair CV-240 is an American airliner produced by Convair from 1947 to 1954, initially as a possible replacement of the ubiquitous Douglas DC-3. While featuring a more modern design, the 240 series was able to make some inroads as a commercial airliner and also had a long development cycle which resulted in a number of civil and military variants. Although reduced in numbers through attrition, the "Convairliners" in various forms continue to fly into the 21st century.[1]

Design and development[edit]

The design began life in a requirement by American Airlines for an airliner to replace its Douglas DC-3s. Convair's original design, the unpressurised Model 110 was a twin-engined low-wing monoplane of all-metal construction, with 30 seats. It was powered by Pratt & Whitney R-2800 Double Wasp radial engines and had a tricycle landing gear and a ventral airstair for passenger boarding.[2] The prototype Model 110, registration NX90653 first flew on July 8, 1946.[2] By this time, American had changed their requirements to require pressurization and deemed the design too small. The first prototype was used by Convair for development work for the 240 series before being broken up in 1947.[3]

A 1949-built Convair 240 of Swiss Air Lines at Manchester, England, in March 1950.

To meet the requirements of airlines for a pressurized airliner Convair produced a revised design, the Model 240. This had a longer but thinner fuselage than the Model 110, accommodating 40 passengers in the first pressurized twin-engined airliner.[4] The 240 first flew on March 16, 1947.[5]

The Model 240 was followed by the Model 340 that had a longer fuselage, longer-span wings and more powerful engines. The 340 first flew on October 5, 1951.[6] In 1954, in an attempt to compete with turboprop-powered airliners like the Vickers Viscount, Convair produced the Model 440 Metropolitan, with more streamlined cowlings, new engine exhausts and better soundproofing for the cabin.[7] As the "Super 240" evolved into the CV-340 and CV-440, the limit of piston-engine performance was reached, and future development centered on conversion to turboprop power.[1]

Operational history[edit]

The first delivery of a production Convairliner was to American on February 29, 1948.[5] A total of 75 were delivered to American, with another 50 going to Western Airlines, Continental Airlines, Pan American Airways, KLM, Swissair, Sabena and Trans Australia Airlines.[8]

Two Convair 580s of the Aspen, Colorado-based Aspen Airways at Stapleton International Airport in Denver, USA in 1986

A CV-240 was the first private aircraft used in a United States presidential campaign. In 1960, John F. Kennedy used a CV-240 named Caroline (after his daughter) during his campaign. This aircraft is now preserved in the National Air and Space Museum.

After aborted negotiations with TWA and Eastern for "Super 240" orders, the production of the 240 series was temporarily halted. In response to a United inquiry, however, Convair redesigned the Super 240, calling it the CV-340. United ordered 55, and more US orders came from Braniff, Continental, Delta, Northeast and National. Other orders came from abroad, and the CV-340 proved popular in South America. The CV-340 earned an enviable reputation for reliability and profitability, and was developed into the CV-440 Metropolitan, the final piston-engined variant of the "Convairliners."[1]

Kelowna Flightcraft Air Charter, the major remaining operator of this model, currently holds the type certificate for this aircraft.

Used price for a Convair 240 in 1960 was around £40,000.[9]

Variants[edit]

Data from:General Dynamics Aircraft and their Predecessors[1]

Civil variants[edit]

Convair 340 of KLM landing at Manchester (Ringway) Airport in 1954
Convair 440 Metropolitan of Lufthansa at Copenhagen (Kastrup) Airport in 1968
Convair 580 operated by the Australian arm of New Zealand airline Pionair. This example was converted from a CV-340
Convair 640F freighter of Kitty Hawk Aircargo converted with Rolls-Royce Dart turboprop engines
Convair Model 110
Unpressurized prototype with seats for 30 passengers. 89 ft (27.13 m) wingspan, 71 ft (21.64 m) length, powered by two 2,100 hp (1,567 kW) Pratt & Whitney R-2800-SC13G engines. One built.[2]
Convair CV-240
Initial production version. Powered by two Pratt & Whitney R-2800 engines.
Convair CV-240-21 Turboliner
turboprop-powered conversion fitted with Allison T38 engines. It became the first turboprop airliner to fly in the United States (on December 29, 1950), but problems with the engines resulted in development being terminated and the prototype being converted back to piston power.
Convair CV-300
a conversion from a Convair CV-240 with two R-2800 CB-17 engines and nacelles as used on the CV-340.[10] A CV-300 was involved in an accident that killed three members and the manager of the rock group Lynyrd Skynyrd.[11]
Convair CV-340
Built for United Airlines and other operators including KLM, was basically a CV-240 lengthened to hold an additional four seats. The wingspan was also extended for better performance at higher altitudes. The CV-340 replaced the DC-3 in United service. The airline flew 52 340s for 16 years without a fatality. KLM operated the type from spring 1953 until mid-1963. Many CV-340 aircraft were converted to CV-440 standard.[12]
Convair CV-440 Metropolitan
CV-340 with improved soundproofing and an option for weather radar. Maximum weight rose to 49,700 lbs. An optional increase from 44 to 52 passengers was facilitated by the replacement of the carry-on luggage area with two more rows of seats, marked by the addition of an extra cabin window. This option was taken up by several airlines including Swissair, Lufthansa and SAS.[12] Finnair operated the type from 1953 until 1980 without a single accident.
Convair CV-540
Conversion from a Convair CV-340 aircraft with two Napier Eland turboprop engines in place of the piston engines. Six aircraft were converted by Napier for Allegheny Airlines.[13] Cost for the conversions was £160,000 per-aircraft. 12 built as new-builds by Canadair for RCAF as CC-109 in 1960 for £436,000 per-aircraft. First flight February 9, 1955.[14]
Convair CV-580
conversion from Convair CV-340 (Allison Prop-Jet Convair 340) or CV-440 aircraft with two Allison 501 D13D/H turboprop engines with four-blade propellers, in place of piston engines with three-blade propellers, an enlarged vertical fin and modified horizontal stabilizers. The conversions were performed by Pacific Airmotive on behalf of the Allison Engine Company.[13] Cost of the conversions was around £175,000 per aircraft and took 60 days.[9]
Convair CV-600
Conversion from a Convair 240 aircraft with Rolls-Royce Dart turboprop engines with four-blade propellers, in place of piston engines with three-blade propellers. CV-600 conversions were performed by Convair.[13] The CV-600 first flew with Central Airlines on 30 November 1965. The CV-600 aircraft that flew with Air Metro Airways was configured as a 40-passenger airliner. In 2012 the last Convair CV-600 (Rhoades Aviation) went out of service.[15]
Convair CV-640
Conversion from a Convair CV-340 or -440 with Rolls-Royce Dart turboprop engines with four-blade propellers, in place of piston engines with three-blade propellers. The conversions were performed by Convair.[13] In 2012, a total of seven Convair CV-640 aircraft remain in airline service, with Rhoades Aviation (one) and C&M Airways (six).[15]
Convair CV5800
Conversion from a C-131 Samaritan by Kelowna Flightcraft Ltd. in Canada. The CV5800 is a C-131 Samaritan stretched by 14 ft 3 in with the Samaritan's original tail unit rather than the enlarged tail of the CV-580. These conversions also have a new freight door, digital avionics with EFIS and Allison 501-D22 engines in place of the original R-2800 engines.

Military variants[edit]

Convair C-131 Samaritan
The CV-240/340/440 series was used by the United States Air Force for medical evacuation and VIP under this designation
Convair T-29 trainer
A trainer model of the C-131 was used to instruct navigators and radio operators
Convair R4Y Samaritan
The United States Navy used the Samaritan under this designation
Canadair CC-109 Cosmopolitan
Conversion from CV-440, with Napier Eland turboprops in place of the piston engines. The conversions were performed in Canada by Canadair. In Royal Canadian Air Force and later in Canadian Armed Forces (Canada) service they were known as the CC-109 Cosmopolitan. All were re-engined in 1966 with Allison 501-D13 engines.
Canadair CL-66
Company designation for the CC-109 Eland powered variant

Operators[edit]

Civil operators[edit]

KLM Convair CV-240
A Convair 580 freighter operated by the IFL Group
A Nolinor Convair 580 landing at Vancouver International Airport
An Air Chathams Convair 580 at Tuuta Airport, Chatham Islands in September 2003
Two North Central CV-580 at Chicago Airport in 1973.

Military operators[edit]

 Australia
 Bolivia
 Canada
 Colombia
CV-580
 Germany
CV-440
 Italy
 Paraguay
  • Paraguayan Air Force: CV-440/C-131D
 Sri Lanka
 Mexico

Other operators[edit]

 United States
 Canada

Accidents and incidents[edit]

Specifications (CV-240)[edit]

Data from General Dynamics Aircraft and their Predecessors[26]

General characteristics

  • Crew: 2 or 3 flight deck crew
  • Capacity: 40
  • Length: 74 ft 8 in (22.76 m)
  • Wingspan: 91 ft 9 in (27.97 m)
  • Height: 26 ft 11 in (8.20 m)
  • Wing area: 817 sq ft (75.9 m2)
  • Empty weight: 25,445 lb (11,542 kg) (revised 29,500 lb (13,381 kg))
  • Gross weight: 40,500 lb (18,370 kg) (revised 42,500 lb (19,278 kg))
  • Fuel capacity: 1,000 US gal (3,785.41 l) - 1,550 US gal (5,867.39 l)
  • Powerplant: 2 × Pratt & Whitney R-2800-CA3 Double Wasp / CA15 / CA18 / CB3 or CB16 18-cyl aircooled radial engines, 2,400 hp (1,800 kW) each
  • Propellers: 3-bladed Hamilton Standard or Curtiss

Performance

  • Maximum speed: 315 mph (507 km/h; 274 kn)
  • Cruise speed: 280 mph (243 kn; 451 km/h) (maximum)
  • Range: 1,200 mi (1,043 nmi; 1,931 km)
  • Service ceiling: 16,000 ft (4,877 m)
  • Rate of climb: 1,520 ft/min (7.7 m/s)

See also[edit]

Related development
Aircraft of comparable role, configuration and era

References[edit]

Notes[edit]

  1. ^ a b c d e f g h i Wegg 1990, pp. 187–199.
  2. ^ a b c Wegg 1990, p. 183.
  3. ^ Gradidge 1997, p. 10.
  4. ^ Wegg 1990, pp. 187–188.
  5. ^ a b Wegg 1990, p. 188.
  6. ^ Wegg 1990, pp. 188–189.
  7. ^ Wegg 1990, p. 192.
  8. ^ Gradidge 1997, pp. 10–11.
  9. ^ a b http://www.flightglobal.com/pdfarchive/view/1960/1960%20-%202680.html
  10. ^ "Convair-Liner History." The American Museum of Aviation. Retrieved: October 21, 2011.
  11. ^ "ASN Aircraft accident: Convair CV-300 N55VM Gillsburg, MS." Aviation Safety Network. Retrieved: October 21, 2011.'
  12. ^ a b Gradidge 1997, p. 13
  13. ^ a b c d Frawley 1997, p. 86.
  14. ^ http://www.flightglobal.com/pdfarchive/view/1960/1960%20-%202679.html
  15. ^ a b Flight International, October 3–9, 2006.
  16. ^ Hagby 1998, p. 34.
  17. ^ http://en.wikipedia.org/wiki/1977_Convair_CV-300_crash
  18. ^ "N39 (FAA Convair 580) KBFI 3/8." NYCAviation.com. Retrieved: September 1, 2010.
  19. ^ Smithson, Peter. "Convair C-131B (340-70) aircraft." airliners.net, October 26, 2010. Retrieved: June 7, 2011.
  20. ^ Groenendijk, Bob. "Convair 580." airliners.net, 1981. Retrieved: June 7, 2011.
  21. ^ Kempf, Steve. "Convair 580." airliners.net, December 2, 2004. Retrieved: June 7, 2011.
  22. ^ King, Royal S. "Convair 580." airliners.net, August 5, 2012 Retrieved: November 14, 2012.
  23. ^ Lockett, Brian. "Convair 580." airliners.net, February 25, 2008. Retrieved: June 7, 2011.
  24. ^ Rodriguez, Javier. "Convair 580." airliners.net, 1999. Retrieved: June 7, 2011.
  25. ^ Derden, Jonathan. "Convair 580." airliners.net, April 19, 2008. Retrieved: June 7, 2011.
  26. ^ Wegg 1990, pp. 188, 199.

Bibliography[edit]

  • Frawley, Gerald. "Convair CV-540, 580, 600, 640 & CV5800". The International Directory of Civil Aircraft 1997/98. Fyshwick ACT, Aerospace Publications, 199, p. 86 ISBN 1-875671-26-9.
  • Gradidge, Jennifer. The Convairliners Story. Tonbridge, Kent, UK: Air-Britain (Historians) Ltd., First edition, 1997, pp. 10–13. ISBN 0-85130-243-2.
  • Hagby, Kay . Fra Nielsen & Winther til Boeing 747. Drammen, Norway. Hagby, 1998. ISBN 8-2-9947-520-1.
  • Wegg, John. General Dynamics Aircraft and their Predecessors. London: Putnam & Company Ltd., 1990, pp. 187–199 ISBN 0-87021-233-8.

External links[edit]