Airbus - A321-211

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A-321-211 / Range 3,000 nm (3,500 mi) / Speed Mach .78 / Pax = 236
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Specifications

Cockpit Crew............................... 2
Passenger Capacity...................... 199 to 240
Length........................................ 146 feet
Wingspan................................... 117 feet
Height........................................ 39 feet
Typical Empty Weight.................. 106,900 lb (53.45 tons)
MTOW (Max Take-off Weight)...... 206,000 lb (93.5 tons)
Take-off Run at MTOW.............. 8,400 ft
Cruising Speed............................ Mach 0.78 at FL350
Service Ceiling............................ 41,100 ft
Range (Fully Loaded).................. 3,000 nm; 3,500 mi
Engines....................2 X CFM56-5B3 (30,000-33,000 lbs)
       
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ROLE

The Airbus A321 offers airline customers the best seat-mile costs of any single-aisle 
aircraft and seating capacities comparable to that of a widebody jetliner. This aircraft
 has a stretched fuselage with an overall length of 44.51 meters, along with
 an extended operating range of up to 3,000 nautical miles while carrying a 
maximum passenger payload. Like each member in Airbus’ A320 Family of jetliners,
 the A321 offers the lowest fuel burn, emissions and noise footprint in its class. 
With a range of up to 4,000 nm. /7,400km., the A321 is capable of flying longer 
routes, for example transatlantic flights from Europe to U.S East Coast. The A321 
typically accommodates 185 passengers in a two-class configuration (16 in business
 class and 169 in economy) – while offering unbeatable economics in high-density
 seating (with up to 220 passengers) for charter and low-cost operators. 

First Flight............................... 22 February 1987
Number Produced of Type........ Over 300
Unit Cost................................. A321: $114.9m