Boeing 737NG - Revision history

Alasizon: Protected "Boeing 737NG" [edit=autoconfirmed:move=autoconfirmed]

2009-12-24T18:26:08Z

Protected "Boeing 737NG" [edit=autoconfirmed:move=autoconfirmed]

← Older revision		Revision as of 18:26, 24 December 2009
Line 4:		Line 4:
	\|manufacturer= Boeing		\|manufacturer= Boeing
	\|status= In Production		\|status= In Production
	\|number built= ~~1825~~		\|number built= 2265
	\|unit cost= 36.000.000v$-70.000.000v$		\|unit cost= 36.000.000v$-70.000.000v$
	\|updateday=3		\|updateday=3
Line 14:		Line 14:

	==Boeing 737-600==		==Boeing 737-600==
			The 737-600 is the direct replacement of the 737-500 and competes with the [[Airbus A320 Family\|Airbus A318]]. It is the only Boeing 737 still in production that does not include winglets as an option. WestJet was to be the Boeing launch customer for the 737-600 winglets, but announced in their Q2 2006 results that they were not going to move ahead with those plans. The 737-600 was launched by Scandinavian Airlines System in 1995 with the first aircraft delivered on 18 September 1998. A total of 69 -600s have been delivered with no further announced unfilled orders as of 2009.

	==Boeing 737-700==		==Boeing 737-700==
			The 737-700 was the first of the Next Generation series launched when launch customer Southwest Airlines ordered the variant in November 1993. The variant was based on the 737-300 and entered service in 1998. It replaced the 737-300 in Boeing's lineup, and its direct competitor is the [[Airbus A320 Family\|Airbus A319]]. It typically seats 137 passengers in a two class cabin or 149 in all economy configuration.

			A total of 1522 -700s have been ordered with 999 of those having been delivered as of September 4th, 2009.

			==Boeing 737-700ER==
			Boeing launched the 737-700ER on January 31, 2006. All Nippon Airways is the launch customer, with the first one of five 737-700ER’s delivered on February 16, 2007. The 737-700ER is a mainline passenger version of the BBJ1 and 737-700IGW. It combines the 737-700 fuselage with the wings and landing gear of a 737-800. It will offer a range of 5,510 nautical miles (10,200 kilometers), with seating for 126 passengers in a traditional 2-class configuration.[16] A competitor to this model would be the A319LR. The 737-700ER has the second longest range for a 737 after the BBJ2. The 737-700ER is inspired by the Boeing Business Jet and is designed for long-range commercial applications. It is able to fly transatlantic services such as Flyglobespan services from Glasgow to Boston.

			All Nippon Airways, Japan’s second-biggest carrier, is to pioneer the model in Asia with a daily service between Tokyo and Mumbai. ANA’s service, believed to be the first all-business class route connecting to a developing country, was to start in September 2007 and use a Boeing 737-700ERs outfitted with 38 (38 Club ANA) and 48 (24 Club ANA/24 Economy) in four-across seats configuration and an extra fuel tank.

			==Boeing 737-700C==
			The 737-700C is a convertible version where the seats can be removed from the plane to carry cargo. There is a large door on the left side of the aircraft. The US Navy was the launch customer for the 737-700C under the military designation C-40 Clipper. A total of 12 -700C's have been ordered and delivered with no further orders as of September, 2009

	==Boeing 737-800==		==Boeing 737-800==
			The 737-800 is a stretched version of the 737-700, and replaces the 737-400 in Boeing's lineup. It also filled the gap left by Boeing's discontinuation of the McDonnell Douglas MD-80 and MD-90 after Boeing's merger with McDonnell Douglas. The -800 was launched by Hapag-Lloyd Flug (now TUIfly) in 1994 and entered service in 1998. The 737-800 seats 162 passengers in a two class layout, or 189 in one class, and competes with the [[Airbus A320 Family\|Airbus A320]]. For many airlines in the U.S., the 737-800 replaced aging Boeing 727-200 trijets.

			The 737-800 is also among the models replacing the McDonnell Douglas MD-80 and MD-90 series aircraft in airline service; it burns 850 gallons of jet fuel per hour, or about 80% of the fuel needed by an MD-80 on a comparable flight, even while carrying more passengers than the latter. According to the Airline Monitor, an industry publication, a 737-800 burns 4.88 gallons of fuel per seat per hour. Alaska Airlines replaced the MD-80 with the 737-800, saving $2,000 per flight, assuming jet fuel prices of $4 per gallon. The fuel cost of each such flight (2008 prices) on a 737-800 is about $8,500.00. For example, on 14 August 2008, American Airlines announced 26 orders for the 737-800 (20 are exercised options from previously signed contracts and six are new incremental orders) as well as accelerated deliveries.

			A total of 1689 -800s have been delivered as of September, 2009 with a further 1416 on order.

	==Boeing 737-900==		==Boeing 737-900==
			Boeing later introduced the 737-900, the longest variant to date. Because the -900 retains the same exit configuration of the -800, seating capacity is limited to 177 seats in two classes, or 189 in a single-class layout. Alaska Airlines launched the 737-900 in 1997 and accepted delivery on May 15, 2001. The 737-900 also retains the MTOW and fuel capacity of the -800, trading range for payload. These shortcomings until recently prevented the 737-900 from effectively competing with the Airbus A321.

			Only 52 -900s have been ordered and delivered with no current orders for the variant.

			==Boeing 737-900ER==
			The 737-900ER, which was called the 737-900X prior to launch, is the newest addition and the largest variant of the Boeing 737 line and was introduced to meet the range and passenger capacity of the discontinued [[Boeing 757\|757-200]] and to directly compete with the [[Airbus A320 Family\| Airbus A321]].

			An additional pair of exit doors and a flat rear pressure bulkhead increase seating capacity to 180 passengers in a 2-class configuration or 215 passengers in a single-class layout. Additional fuel capacity and standard winglets improve range to that of other 737NG variants.

			The first 737-900ER was rolled out of the Renton, Washington factory on August 8, 2006 for its launch customer, Lion Air. Lion Air received this aircraft on April 27, 2007 in a special dual paint scheme combining the Lion Air lion on the vertical stabilizer and the Boeing livery colors on the fuselage.

			A total of 59 -900ERs have been delivered with 181 unfilled orders as of September 2009.

	==Specifications==		==Specifications==
	{\| style="text-align: center; font-size:95%;" class="wikitable"		{\| style="text-align: center; font-size:95%;" class="wikitable"

Alasizon at 15:47, 3 May 2009

2009-05-03T15:47:11Z

← Older revision		Revision as of 15:47, 3 May 2009
Line 88:		Line 88:
	\|Engine ground clearance \|\| colspan=3 \| 18 in (46 cm) \|\| colspan=2 \| 19 in (48 cm)		\|Engine ground clearance \|\| colspan=3 \| 18 in (46 cm) \|\| colspan=2 \| 19 in (48 cm)
	\|}		\|}

			[[Category:Narrowbody Jetliners]]

Alasizon: New page: {{Infobox Aircraft Type |type= Narrowbody Jetliner |country= USA |manufacturer= Boeing |status= In Production |number built= 1825 |unit cost= 36.000.000v...

2009-05-03T15:41:10Z

New page: {{Infobox Aircraft Type |type= Narrowbody Jetliner |country= USA |manufacturer= Boeing |status= In Production |number built= 1825 |unit cost= 36.000.000v...

New page

{{Infobox Aircraft Type
|type= [[:Category:Narrowbody Jetliners|Narrowbody Jetliner]]
|country= USA
|manufacturer= Boeing
|status= In Production
|number built= 1825
|unit cost= 36.000.000v$-70.000.000v$
|updateday=3
|updatemonth=5
|updateyear=2009
|picture= yes
}}
The Boeing 737NG (Next Generation) series is a group of narrowbody jetliners produced by Boeing.

==Boeing 737-600==

==Boeing 737-700==

==Boeing 737-800==

==Boeing 737-900==

==Specifications==
{| style="text-align: center; font-size:95%;" class="wikitable"
|- bgcolor="#DDDD"
!Measurement
!737-600
!737-700/ 737-700ER
!737-800
!737-900ER
|- bgcolor="#EEEEEE"
|Cockpit crew || colspan=4 | Two
|- bgcolor="#EEEEEE"
|Seating capacity || colspan=1 | 132 (1-class, dense), 123 (1-class, standard)) || colspan=1 | 149 (1-class, dense), 140 (1-class, standard) || | 189 (1-class, dense), 175 (1-class, standard)|| | 215 (1-class, high-density), 204 (1-class, dense), 177 (1-class, standard)
|- bgcolor="#EEEEEE"
|Seat pitch || colspan=3 | 30 in (1-class, dense), 32 in (1-class, standard) || 28 in (1-class, high-density), 30 in (1-class, dense), 32 in(1-class, standard)
|- bgcolor="#EEEEEE"
|Seat width || colspan=4 | 17.2 in (1-class, 6 abreast seating)
|- bgcolor="#EEEEEE"
|Length || colspan=1 | 102 ft 6 in (31.2 m) || colspan=1 | 110 ft 4 in (33.6 m) || 129 ft 6 in (39.5 m) || 138 ft 2 in (42.1 m)
|- bgcolor="#EEEEEE"
|Wingspan || colspan=4 | 117 ft 5 in (35.7 m)
|- bgcolor="#EEEEEE"
|Height || 41 ft 3 in (12.6 m) || colspan=3 | 41 ft 2 in (12.5 m)
|- bgcolor="#EEEEEE"
|Wing sweepback || colspan=4 | 25.02° (437 mrad)
|- bgcolor="#EEEEEE"
|Aspect ratio || colspan=4 | 9.45
|- bgcolor="#EEEEEE"
|Fuselage width || colspan=4 | 12 ft 4 in (3.76 m)
|- bgcolor="#EEEEEE"
|Fuselage Height || colspan=4 | 13 ft 2 in (4.01 m)
|- bgcolor="#EEEEEE"
|Cabin width || colspan=4 | 11 ft 7 in (3.54 m)
|- bgcolor="#EEEEEE"
|Cabin height || colspan=4 | 7 ft 3 in (2.20 m)
|- bgcolor="#EEEEEE"
|Empty weight || 80,031 lb (36,378 kg) || 84,100 lb (38,147 kg) || 91,108 lb (41,413 kg) || 98,495 lb (44,676 kg)
|- bgcolor="#EEEEEE"
|Maximum take-off weight || 145,500 lb (66,000 kg) || '''Basic:''' 154,500 lb (70,080 kg) '''ER:''' 171,000 lb (77,565 kg) || 174,200 lb (79,010 kg) || 187,700 lb (85,130 kg)
|- bgcolor="#EEEEEE"
|Maximum landing weight || 121,500 lb (55,112 kg) || 128,928 lb (58,604 kg) || colspan=2 | 146,300 lb (66,361 kg)
|- bgcolor="#EEEEEE"
|Cargo capacity || 756 ft³ (21.4 m³) || 966 ft³ (27.3 m³) || 1,591 ft³ (45.1 m³) || 1,852 ft³ (52.5 m³)
|- bgcolor="#EEEEEE"
|Takeoff run at MTOW || 8,016 ft (2,400 m) || 8,283 ft (2,480 m) || colspan=2 | 8,181 ft (2,450 m)
|- bgcolor="#EEEEEE"
|Service ceiling || colspan=4 | 41,000 ft (12,500 m)
|- bgcolor="#EEEEEE"
|Cruising speed || colspan=3 | 0.785 (514 mph, 828 km/h) || 0.78 (511 mph, 823 km/h)
|- bgcolor="#EEEEEE"
|Maximum speed || colspan=4 | 0.82 (544 mph, 876 km/h, 473 kt)
|- bgcolor="#EEEEEE"
|Range fully loaded || 3,050 NM (5,648 km) || '''Basic:''' 3,365 NM (6,230 km) '''WL:''' 3,900 NM (7,220 km) '''ER:''' 5,375 NM (9,955 km) || 3,060 NM (5,665 km) || 2,700 NM (4,996 km) in 1 class layout, 3,200 NM (5,925 km) in 2 class layout with 2 aux. tanks
|- bgcolor="#EEEEEE"
|Max. fuel capacity || colspan=3 | 6,875 US gal (26,020 L) || 7,837 US gal (29,660 L)
|- bgcolor="#EEEEEE"
|Engine (x 2)|| CFM 56-7B20 || CFM 56-7B26 || CFM 56-7B27 || CFM 56-7
|- bgcolor="#EEEEEE"
|Max. thrust (x 2)|| 20,600 lbf (91.6 kN)|| 26,300 lbf (116.0 kN)|| colspan=2 | 27,300 lbf (121.4 kN)
|- bgcolor="#EEEEEE"
|Cruising thrust (x 2)|| 5,210 lbf (23.18 kN)|| colspan=3 |5,480 lbf (24.38 kN)
|- bgcolor="#EEEEEE"
|Fan tip diameter || colspan=4 | 61 in (1.55 m)
|- bgcolor="#EEEEEE"
|Engine length || colspan=4 | 98.7 in (2.51 m)
|- bgcolor="#EEEEEE"
|Engine ground clearance || colspan=3 | 18 in (46 cm) || colspan=2 | 19 in (48 cm)
|}