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| Historical Fleet |
| Mc Donnell Douglas DC-9-32 (D9S) |
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The Canadian transcontinental and Montreal-New York routes were enhanced with the introduction of the DC-9's in April 1966. Since that time there have been modifications to existing aircraft, and the introduction of new technologically updated DC-9 models, so that they are still valuable contributors to the North American and Southern routes of Air Canada.
The most distinctive feature of the DC-9 is the high-level horizontal stabilizer mounted at the top of the rudder assembly to accommodate the installation of the Pratt & Whitney turbofan engines on either side of the aft fuselage.
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| Technical characteristics |
| Timetable code |
D9S |
| Period of use |
1966 - 2002 |
| Manufacturer |
McDonnell Douglas |
| Engines |
JT8D-7B |
| Seats (typical) |
91 |
| Cargo capacity |
3,410 lbs (1 547 kilos) |
| Fuel capacity |
4,260 usg (16 126 l.) |
| Overall length |
119.3 feet (36,3 m.) |
| Wing span |
93.3 feet (28,4 m.) |
| Top of fin from ground |
27.5 feet (8,4 m.) |
| Cruise speed |
490 mph (789 km/h) |
| Range (full passengers) |
1,265 miles (2 036 km) |
| Cruise altitude (typical) |
33,000 feet (10 058 m.) |
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