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General Info

Conroy Skymonster
(CL-44-0) Guppy

Role Large outsize-cargo transport aircraft
Manufacturer Conroy Aircraft
First flight 1969
Status Retired
Primary users Heavylift Cargo
Transmeridian Air Cargo
Number built 1
Developed from Canadair CL-44
Career
Registration N447T, EI-BND, 4K-GUP, 9G-LCA, RP-C8023, N447FT
In service 1970-1999, 2013-2022
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History Conroy Skymonster
(CL-44-0) Guppy



The Conroy Skymonster (CL-44-0) is a 1960s United States specialized cargo aircraft based on the Canadair CL-44 freighter, with an outsize fuselage.

The aircraft was designed by John M. Conroy as a transport aircraft that could be used to ferry three Rolls-Royce RB.211 jet engines from Belfast, Northern Ireland, to Palmdale, California, United States. The engines were to be installed on the Lockheed L-1011 TriStar airliner. The Skymonster was derived from a Canadair CL-44 freighter, in turn a derivative of the Bristol Britannia. It features an enlarged fuselage, like the Aero Spacelines Mini Guppy, which was produced by Jack Conroy's previous company, Aero Spacelines. The conversion was performed outdoors, under covered scaffolding, at the Santa Barbara California airport. The nose section was built using foam covered with fiberglass, while the larger fuselage was constructed using conventional aluminum structure.


Operational history

The Skymonster at Bournemouth when it was registered as 9G-LCA
N447FT at Bournemouth in 2014.

After a long period of storage, activity was again seen around the Skymonster during the summer of 2013. In July 2013 it was registered N447FT in the United States to a Jordan Harlan Wayne, but has since been deregistered.

As of 21 May 2021 the Skymonster remains at Bournemouth International Airport, moved from its original parking spot to make way for airport development.

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Aeromacchi Leonardo

Canadair / Bombardier
Conroy Skymonster (CL-44-0) Guppy

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General Info

      • Crew: 2 pilots, 1 flight engineer plus loadmasters as required.
      • Capacity: 160 passengers and 66,048 lb (29,959 kg) useful load
      • Length: 136 ft 11 in (41.73 m)
      • Wingspan: 142 ft 4 in (43.37 m)
      • Height: 36 ft 8 in (11.18 m)
      • Wing area: 2,075 sq ft 
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Powerplant


      • Empty weight: (40,348 kg)
      • Max takeoff weight:  (95,000 kg)
      • Powerplant: 4 × Rolls-Royce Tyne 515/50 turboprops, 5,730 shp each
      • Propellers: 4-bladed variable pitch propellers
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Performance

  • Maximum speed:  (670 km/h
  • Cruise speed: 401 mph (646 km/h
  • Range: 5,588 mi (8,993 km
  • Service ceiling:(9,100 m)
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Special Links Canadair / Bombardier

Links to Youtube & Others

The rollout of the Yukon was a near-disaster because the prototype could not be pushed out of the hangar since the vertical fin could not clear the hangar doors

Canadair
 Canadair CT-114 Tutor

The RCAF specified the CL-44 to be equipped with Bristol Orion engines

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Youtube Link

The CC-106 Yukons retired in March 1971 and were replaced by the CC-137 (Boeing 707)

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