Commercial Aircraft Directory - Aircraft Specification

Boeing - 737-600

The Boeing 737-600 is the smallest current production version of the Next Generation 737 family. The program was launched on March 15 1995 with an order for 35 from SAS, and was the third of the family to fly. The 737-600 is essentially a 737-700 with two sections of fuselage removed which results in an overall length of 31.2m (a reduction of 2.38m compared with the -700). As a result of this change in length the fuselage contour at the wing trailing edge is changed and the -600 features an aft fairing between the wing and fuselage. There are also aerodynamic changes to the outer fuselage skins. The 737-600 is powered by the CFM56-7B18/20/22 the 7B22 offering a 9.25% increase in take off thrust compared with the -7B20 and 14% more compared with the 7B18. The 737-600 is also the only Next Generation 737 which does not offer winglets; their fitment not delivering a positive cost/benefit outcome over the sectors the -600 is employed on. This situation however may change given increases in oil prices. The 737-600 is a replacement for the 737-500 in the Boeing product line but has a significantly better range/payload performance.
A 737-600 with a take-off weight of 54,431 kg can carry a 9247 kg payload some 2547 km. By comparison a 737-500 under the same conditions can carry the same payload 1907 km (a 25% range /payload performance improvement). SAS took delivery of its first aircraft on 18 September 1998 and eventually accepted a total of 28 aircraft. Other operators who ordered the 737-600 were Continental Airlines (who ordered 30 but changed the order to larger variants), Westjet who ordered 17 and Tunis Air who ordered and accepted 7. The advent of larger capacity regional jets such as the E-195 which offer lower empty weights and growth in capacity demand has impacted on 737-600 orders which have only attained 72 having been subject to 134 cancellations from an original total of 206 ordered up to August 2006. At that time only 8 aircraft remained to be delivered with the last due to be delivered in July 2008 to Westjet

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: 22 Jan 1998  
Certification date:  
Launch customer(s): SAS Cargo
 

PRINCIPAL DIMENSIONS

Fuselage width: 3.76 m 
Fuselage height: 4.01 m 
Fuselage length: 29.79 m 
Cabin length: 21.79 m 
Cabin width: 3.54 m 
Cabin height: 2.2 m 
Cabin volume:  
Hold volume: 20 m3 

WEIGHTS

Empty operating: 36,378 kg 
Max zero fuel: 51,936 kg 
MTOW: 65,544 kg 
MLW: 55,112 kg 
Standard fuel capacity: 26,020 kg 
Max fuel capacity: 26,020 kg 

SPEEDS

Normal cruise: 833 km/h 
Max cruise: 871 km/h 

PERFORMANCE

Long Range Cruise alt: 11,887 m 
Max ceiling: 12,497 m 
Take off field length: 1,795 m 
Landing field length: 1,342 m 
Max Payload Range: 5,634 m 
Range notes: Payload option 5650km with 110 pax  
Max passengers: 132  
Typical passengers: 110  

POWERPLANT

Category: Turbofan  
Manufacturer: CFM International  
Model/Submodel: CFM56 7B20  
Thrust: 92 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: CFM International  
Model/Submodel: CFM56 7B22  
Thrust: 101 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: CFM International  
Model/Submodel: CFM56 7B18  
Thrust: 87 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: CFM International  
Model/Submodel: CFM56 7B22/3  
Thrust: 101 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: CFM International  
Model/Submodel: CFM56 7B20/3  
Thrust: 92 kN  

POWERPLANT

Category: Turbofan  
Manufacturer: CFM International  
Model/Submodel: CFM56 7B18/3  
Thrust: 87 kN  

MAINTENANCE PROVIDERS

Abu Dhabi Aircraft Technologies
Aerostar Maintenance International Limited (AMIL)
Air Berlin Technik Berlin GmbH
Air China Technology Company
ATC Lasham
China Aircraft Services (CASL)
Digex Aero Maintenance
Korean Air
Omega Industries
Revima
Scandinavian Airlines System (SAS) Denmark
Scandinavian Airlines System (SAS) Norway
Servisair Line Maintenance
SR Technics Ireland
SR Technics UK
Tarom Technical Division
Tunisair