
May 1955 to March 1964
Trans-Canada Air Lines (TCA)
CF-TGO - c/n 52 - a V.724 series Viscount
Canada registered
November 1952
An order was placed by Trans-Canada Air Lines (TCA) for fifteen Type 724 aircraft at a total cost of Can$11,500,000. This was the seventh one built.
Production Aircraft No. 53 - the 53rd production Type 700 series Viscount built,
was the 22nd Viscount fuselage assembled at Hurn, Bournemouth, Hampshire, England,
and the 25th Viscount assembled at Hurn, Bournemouth, Hampshire, England.
Production Order No. F07/724. Sales Order No. F07/51B. Stock Order No. F01/22B.
10 September 1954
Fuselage assembly commenced at Hurn Airport, Bournemouth, Hampshire, England.
1 November 1954
Fuselage to Erecting Shop 'E' at Hurn Airport, Bournemouth, Hampshire, England.
21 March 1955
TCA issued technical instruction V-05.04-1/1 to apply the word 'Viscount' to the tail section in 8.5 inch high red letters edged in white at the first opportunity.
20 April 1955
First flight from Hurn Airport, Bournemouth, Hampshire, England.
It was fitted with Rolls-Royce Dart RDa3 Mark 506 engines.
1 May 1955
Aircraft passed off by TCA inspectors as completed and ready for delivery.
It then departed from Hurn Airport, Bournemouth, Hampshire, England on delivery to Trans-Canada Air Lines (TCA) with fleet number '607'.
It was flown to Canada by Vickers test pilot Gabriel (Gabe) Robb 'Jock' Bryce accompanied by his wife Nancy.
She was born at Ocean Falls, British Columbia, Canada and became the first female to fly across the North Atlantic in a turboprop aircraft.
After refuelling at Prestwick Airport, Ayrshire, Scotland it then flew on to Keflavik Airport, Iceland (743 nautical miles) where it stopped for six hours.
2 May 1955
Departed from Keflavik Airport, Iceland to Bluie West One (BW1) Airfield, Southern Greenland (804 nautical miles), Goose Bay Airport, Newfoundland & Labrador, Canada (672 nautical miles), Dorval International Airport, Montreal, Province of Quebec, Canada (810 nautical miles).
BW1 was built during WWII to assist the transfer of military aircraft from North America to Europe and was opened in January 1942.
2 June 1955
TCA issued technical instruction V-31.02-2/5 to apply the word 'Viscount' to the inside of the passenger loading door in 4 inch high red letters edged in white at the first opportunity.
The cabin seating was installed in Canada, as the seats used by TCA were of American manufacture.
The cabin was fitted out with 40 seats which was a reduction from the original 48 seat specification and provided more leg room.
This was heavily marketed and resulted in a high load factor compared to the 18 seat Douglas DC-3 that it replaced on some routes.
1 November 1955
First Viscount to operate on the Montreal to Vancouver route.
July 1956
Cabin interior changed to a two class 44 seat arrangement.
10 July 1957
TCA issued instructions that all Viscounts would be repainted in a 'White Top' livery when a suitable maintenance period became available.
31 July 1958
Scheduled to enter the Winnipeg Airport, Manitoba, Canada TCA maintenance facility for the replacement of the life expired wing lower inner spar boom at approximately 6100 landings for this component. This usually took 28 days to complete.
31 August 1960
Total time 13,847 hours and 10,714 total landings.
6 January 1963
Withdrawn from service and stored at Winnipeg Airport, Manitoba, Canada.
Total time 17,994 hours and 14,743 total landings.
2 March 1964
Sold to William C Wold & Associates.
|