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VISUAL VIEW OF AIRCRAFT BOEING 737-400

GENERAL CHARACTERISTICS BOEING 737-400

  Dimensions  
Length (m) 36.5
Wingspan(m) 28.9
Height (m) 11.1
Wing Area(sq m) 105.4
  Weight  
Max. take-off weight(kg) 62 900 - 68 100
Max. landing weight (kg) 54 900 - 56 240
Empty weight(kg) 34 820
Max. Weightwithout fuel(kg) 53 070
Max. payload (kg) 18 260
Fuel tank capacity(litre) 23 830
  Flight data  
Range with max. payload (km) 2 500 - 3 500
Max. cruising speed(km / h)
Ceiling(max. Altitude) (m) 11 300
Takeoff(m) 2 540
Length (m) 1 540
Engines CFMI CFM56-3B2/3C1, 2 x 9990-10670 êãñ
Specific fuel consumption(g / passenger km) 20.9
Fuel consumption per hour(kg) 2 600
  The passenger compartment  
Number ofseats (economy)
Number ofseats (economy / business)
Cabin width (m) 3.53
     

 

 

VISUAL VIEW OF AIRCRAFT BOEING 737-400

 

 

 

 

FUEL SYSTEM BRIEF INFORMATION

 

In the wingandcenter sectionhas threefuel tanks: the wingand center. Firstproducedcentral, then-the wing.Eachtankhastwofuel pumps. The total maximumcapacity of the tanks737aircraftfamilyOriginalfrom12700to15600kg,depending on the modification.
Airplanesfamily737Classic,containertanksincreased to16200kg,also have the optionto install an additionalfuel tankin the reartrunk.
In general, similar to the737NG,tankcapacityincreased to20,800kg, modified fuel tanks: the central tankcoversnot only thecenter section, but also part ofthe wing fromthe root to theengine strut. Alsochangedthe locationof pumps andadded to the systemto remove waterfrom the tanks.
OnBBJaircrafthave the abilityto install up to9additional fuel tanksin the cargo areas, increasing the capacityto37,712kg.


Date: 2015-01-11; view: 2244


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