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Boeing 737-600 vs. McDonnell Douglas DC-9-30

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737-600

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DC-9-30

Price (USD)
$57 Million$10 Million
First Flight
19981966
Body Type
Narrow-bodyNarrow-body
Length
31 m102 ft
36 m119 ft
Wingspan
34 m112 ft
28 m93 ft
Wing Area
124 m²1,341 ft²
93 m²1,001 ft²
Fuselage Width
3 m12 ft
3 m11 ft
Height
12 m41 ft
8 m27 ft
Max Takeoff Weight
66,000 kg145,505 lbs
48,988 kg108,000 lbs
Number of Engines
22
Engine Options
CFMI CFM56Pratt & Whitney JT8D
Max Thrust Per Engine
101 kN22,700 lbf
67 kN15,000 lbf
Max Total Thrust
202 kN45,400 lbf
134 kN30,000 lbf
Fuel Capacity
26,000 l6,868 gal
13,900 l3,672 gal
Range
5,650 km3,051 nm
2,800 km1,512 nm
Cruise Speed
850 km/h528 mph
897 km/h557 mph
Typical Seating
123 pax115 pax
Max Seating
149 pax127 pax

What Are the Differences Between the Boeing 737-600 and McDonnell Douglas DC-9-30

Boeing 737-600 vs McDonnell Douglas DC-9-30 Size Comparison

  • At 36.40 meters, the McDonnell Douglas DC-9-30 is 5.20 meters longer than the Boeing 737-600.
  • With a wingspan of 34.30 meters, the Boeing 737-600 is 5.90 meters wider from wingtip to wingtip.
  • The Boeing 737-600 and McDonnell Douglas DC-9-30 have heights of 12.60 meters and 8.50 meters respectively - making the Boeing 737-600 4.10 meters taller.

Boeing 737-600 vs McDonnell Douglas DC-9-30 Range

  • Boeing 737-600’s range of 5,650 kilometers is greater than McDonnell Douglas DC-9-30’s range of 2,800 kilometers. Therefore, the Boeing 737-600 can fly nonstop approximately 2,850 kilometers further.
  • The Boeing 737-600 can hold 6,868 gallons of fuel, which is 3,196 gallons more than the McDonnell Douglas DC-9-30’s tank capacity of 3,672 gallons.

Boeing 737-600 vs McDonnell Douglas DC-9-30 Seating

  • In a typical seating configuration, the Boeing 737-600 can accommodate 123 passengers, which is about 8 passengers more than McDonnell Douglas DC-9-30’s seating capacity.
  • The Boeing 737-600’s max seating capacity is 149 passengers, compared to 127 passengers of the McDonnell Douglas DC-9-30.

About the Boeing 737-600

Launched in 1998, the Boeing 737-600 is the smallest aircraft in the 737 Next Generation (NG) series. It succeeded the 737-500, and was a significant evolution in Boeing's narrow-body offerings. It featured many upgraded features from the previous 737s, including aerodynamics, engines, and avionics. As the smallest NG variant, the 737-600 was designed for efficiency and adaptability, catering to airlines requiring a compact jet for short to medium-haul routes.

This aircraft extends 102.4 feet (31.2 meters) in length with a wingspan of 112.6 feet (34.3 meters). The 737-600, with a typical seating capacity for 123 passengers, offers an ideal balance between passenger comfort and efficiency, making it a fitting choice for airlines serving routes with moderate passenger demand. Equipped with two CFM International CFM56-7B20 engines, the 737-600 has a total thrust of 45,400 lbf (202.0 kN). This engine power, coupled with a fuel capacity of 6,868 US gallons (26,000 liters), gives the -600 a range of 3,051 nautical miles (5,650 kilometers). The 737-600 has a cruise speed of 528 mph (850 km/h) enabling airlines to maintain efficient and swift operations, particularly beneficial for regional network connections.

In the late 1990s and early 2000s, the Boeing 737-600 competed with aircraft such as the Airbus A318 and Bombardier CRJ series, offering airlines a modern alternative in the narrow-body market. Airlines including Scandinavian Airlines (SAS), Westjet, and Air Algerie operated the Boeing 737-600. Ultimately, the -600 variant was not a popular model of the 737 due to its economics. The -700, only slightly heavier, had a much greater payload. Additionally, the larger market was moving more towards higher capacity narrow-bodies with lower unit costs and greater revenue opportunities.

About the McDonnell Douglas DC-9-30

The McDonnel Douglas DC-9-30, a narrow-body jet airliner first introduced in 1966, stands as a significant aircraft in the evolution of commercial aviation. Designed during an era of rapid growth in air travel, the DC-9-30 was developed to meet the demands of short to medium-haul routes, offering airlines a more efficient and practical alternative to the larger jetliners of the time. The Series 30 of the DC-9 included four main sub-variants, -31, -32, -33, and -34. During its production, the -30 was by far the most popular model of the DC-9 with 585 units delivered.

This aircraft was initially developed as the Douglas DC-9, prior to August 1967 merger with McDonnell Aircraft. The DC-9-30 measures in at 36.4 meters (119.3 feet) in length. This size enabled it to operate efficiently in smaller airports and on shorter runways - a niche that was underserved at the time of its introduction. Powered by a pair of Pratt & Whitney PWJTD engines, the DC-9-30 has a total thrust output of 134.0 kN (30,000 lbf). Its fuel capacity of 13,900 liters (3,672 US gallons) gives the DC-9-30 a range of approximately 2,800 kilometers (1,512 nautical miles). This range was particularly advantageous for airlines looking to serve regional networks with an efficient and reliable jet.

The DC-9-30's typical five abreast seating layout can fit around 115 passengers, with a maximum of 127 in a high-density layout.

In its market segment, the McDonnel Douglas DC-9-30 was a key competitor to other short-haul aircraft of the era. Its introduction provided airlines with a jetliner that was not only smaller and more versatile than the larger, long-haul aircraft but also more efficient and economical for short to medium-range routes.

Airlines such as Delta Air Lines, Eastern Air Lines, and TWA were prominent operators of the DC-9-30, utilizing its capabilities to enhance their regional route networks. The aircraft's role in these fleets demonstrated its effectiveness in bridging the gap between propeller-driven airliners and larger jets, contributing significantly to the growth of regional air travel.

The McDonnel Douglas DC-9-30's production and service history highlight its importance as a practical and versatile aircraft in commercial aviation. The last DC-9 to ever be built was delivered in 1982. After its retirement, McDonnell Douglas went on to produce the MD-80 and the MD-95.

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Values shown may not be 100% accurate, as some metrics are averages or only represent certain production years and configurations. Engine specs are based on the best options available.

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