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Boeing 737-700
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The 737-600
and -700 are the smaller members of Boeing's
successful Next Generation 737-600/700/800/900
family.
The 737's new
wing has greater chord, span and wing area,
while the tail surfaces are also larger. The 2,4
meter high winglets first developed for the
Boeing Business Jet development are now offered
as an option on the 737-700. Among the many
changes, the Next Generation 737s feature more
efficient CFM56-7B turbofans. The CFM56-7
combines the core of the CFM56-5 with the
CFM56-3's low pressure compressor and a 1,55 m
fan. And the 777 style EFIS flight deck with six
flat panel LCDs which can present information as
on the 777 or as on the 737-300/400/500 series,
the latter allowing a common pilot type rating
for the two 737 families. A HUD is optional.
Boeing
Business Jet
Boeing 737 BBJ
- This 737-700 model airplane is equipped with a
737-800 landing gear configuration. This model
is also equipped with auxiliary fuel tanks in
the cargo compartment for additional range
capability. Main cabin interiors to customer
preference. Typical configuration includes a
crew rest area, forward lounge, private suite
with double bed and private bathroom facilities
including shower, 12 first class sleeper seats
at four abreast and 152 cm pitch, and rear
galley and bathroom facilities. Alternatively
rear cabin can seat 24 passengers at two abreast
and feature a conference area or exercise gym,
or up to 63 passengers at six abreast.
Boeing C-40A
Clipper
The BBJ's
airframe also forms the basis for the
convertible passenger/freighter variant of the
700, the 737-700QC, which has been ordered by
the US Navy as the C-40A Clipper (to replace the
DC-9 based C-9B). The C-40 first flew on April
17, 2000. The naval aircraft can be converted to
carry 121 passengers, or 3 pallets of cargo plus
70 passengers, or 8 pallets of cargo only. The
737-700C variant features a 3,35 x 2,13 m cargo
door on the right side of the aircraft and cargo
handling systems in the cabin and a strengthened
floor. These aircraft are currently (2002) based
at Naval Air Station Fort Worth, Texas (VR-59)
and Naval Air Station Jacksonville, Florida
(VR-58).
Project Wedge
tail
The AEW&C
system combines the new high-performance Boeing
737-700 increased gross weight (IGW) aircraft
with the Northrop Grumman Multi-role
Electronically Scanned Array (MESA) radar.
Included in the platform are an advanced
identification friend or foe (IFF) system; an
expanded, passive surveillance system; a
flexible, open-system architecture and a highly
effective self-defense capability.
Using the latest sensor
technology, Northrop Grumman’s 360-degree steer
able beam MESA radar is able to track air and
sea targets simultaneously and can help the
operator track high-performance aircraft while
continuously scanning the operational area. More
than 1500 hours of wind tunnel testing have
demonstrated the compatibility of the aircraft
and the radar.
The Boeing team was awarded an
Initial Design Activity contract by the
Australian Defence Force in December 1997. As
part of that contract, the team worked on a
design solution to meet the Royal Australian Air
Force (RAAF) requirements for an AEW&C system.
In July 1999, the Boeing team was selected as
the preferred contender for Project Wedge tail.
A development and acquisition contract was
signed in December 2000. It provides for four
737 AEW&C systems with options for up to three
additional systems. The contract also provides
for ground-based support segments for flight and
mission crew training, a mission support segment
and other system support facilities and spare
parts. The first two aircraft are expected to be
delivered to the Commonwealth of Australia in
2006. |
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Developing nation: |
United States of
America. |
|
Manufacturer/designer: |
Boeing
Commercial Airplane Company. |
| Production line: |
Renton Municipal
Airport, WA. |
| Type aircraft: |
Short to medium
range airliner. |
|
First flight: |
- 737-100 April 9, 1967, N73700.
- 737-200 August 8, 1967, N9001U.
- 737-200C September 18, 1968.
- 737-200Adv April 15, 1971.
- 737-300 February 24, 1984, N350AU.
- 737-400 February 19, 1988, N73700.
- 737-500 June 30, 1989, N73700.
- 737-600 January 22, 1998, N7376.
- 737-700 February 9, 1997,
N737X.
- 737-800 July 31, 1997, N737BX.
- 737-900 September 2000, N737X. |
| First delivery: |
- 737-100 December 28, 1967 to Lufthansa.
- 737-200 December 29, 1967 to United
Airlines.
- 737-200C October 30, 1968 to Wien
Consolidated.
- 737-200Adv May 20, 1971 to All Nippon
Airways.
- 737-300 November 28, 1984 to USAir.
- 737-400 September 15, 1988 to Piedmont.
- 737-500 February 28, 1990 to Southwest.
- 737-600 August, 1998 to SAS.
- 737-700 December 17, 1997
to Southwest.
- 737-800 April 22, 1998 to Hapag Lloyd.
- 737-900 May 16, 2001 to Alaska Airlines. |
| Last delivery: |
- 737-100 July 26, 1973 to NASA.
- 737-200 April 5, 71 to Indian Airlines.
- 737-200C July 5, 1985 to Markair.
- 737-200Adv August 8, 1988 to Xiamen
Airlines.
- 737-300 December 17, 1999 to Air New
Zealand.
- 737-400 February 25, 2000 to CSA Czech
Airlines.
- 737-500 July 26, 1999 to Air Nippon. |
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Boeing 737-700 |
|
Cockpit crew: |
two pilots. |
| Passengers
single class: |
148. |
| Passengers two
class: |
- 8 first class.
- 120 economy class. |
| Cabin length: |
24,13 m.
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| Cabin diameter: |
3,54 m.
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| Cabin height: |
2,20 m.
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| Cabin floor: |
75 m².
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| Cargo volume: |
- under floor 27,3 m³. |
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Wing span: |
34,31 m. |
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Wing area: |
125 m². |
| Wing sweep: |
25 degrees. |
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Fuselage length: |
33,63 m. |
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Fuselage diameter: |
3,76 m. |
| Height: |
12,57 m. |
| Horizontal tail
unit: |
10,97 m. |
| Wheelbase: |
12,60 m. |
| Track: |
5,72 m. |
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Engines: |
- two CFM International CFM56-7B each rated
108 kN. |
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Weight: |
- empty: 37.648 Kg.
- max. zero-fuel weight: 55.202 Kg.
- fuel: 26.035 liters.
- max. payload: 17.544 Kg. |
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Max. take off weight: |
70.080 Kg. |
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Max. landing weight: |
58.604 Kg. |
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Cruise speed: |
938 km/h. |
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Max. speed: |
974 km/h.
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Service ceiling: |
11.582 m. |
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Max. ceiling: |
12.500 m. |
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Range: |
6.038 km. |
| |
Boeing 737-700C /
C-40A*
|
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Passengers: |
- 121 single
class.
- 70 in combi configuration with
3 pallets. |
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Cabin floor: |
75,1
m². |
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Cargo volume: |
- under floor 27,3 m³.
- total cargo volume 107,6 m³. |
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Standard 2.24m x 3.17m pallets: |
- main cargo deck of freighter 8. |
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Weight: |
-
empty: 38.000 Kg.
- max. zero-fuel weight: 57.153
Kg.
- fuel: 26.033 liters.
- max. payload: 18.655 Kg. |
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Max. take off weight: |
77.565 Kg. |
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Max. landing weight: |
60.782 Kg. |
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Range: |
- with 121
passengers 5.555 km.
- with 9.072 kg cargo 5.324 km. |
*
Generally similar to the Boeing 737-700 except
in the following particulars. |
|
| |
Boeing 737-700
with winglets*
|
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Wing span: |
35,79 m. |
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Wing area: |
125 m². |
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Winglet height: |
2,44
m. |
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Weight: |
-
empty: 37.648 Kg.
- max. zero-fuel weight: 55.202
Kg.
- fuel: 46.063 liters.
- max. payload: 17.554 Kg. |
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Max. take off weight: |
70.080 Kg. |
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Max. landing weight: |
58.604 Kg. |
*
Generally similar to the Boeing 737-700 except
in the following particulars.
| |
Boeing
BBJ*
|
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Wing
span: |
35,79 m. |
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Wing
area: |
125 m². |
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Winglet height: |
2,44 m. |
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Engines: |
- two CFM International
CFM56-7B each rated 117.4 kN.
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Weight: |
- max. zero-fuel weight:
57.152 Kg. |
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Max.
take off weight: |
77.564 Kg. |
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Max.
landing weight: |
60.781 Kg. |
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With 3 auxiliary fuel
tanks: |
-
empty: 41.887 Kg.
- max. payload: 15.300
Kg.
- cargo volume lower
deck: 17,3 m³.
- fuel: 31.646 liters. |
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With 4 auxiliary fuel
tanks: |
-
empty: 42.058 Kg.
- max. payload: 15.126
Kg.
- cargo volume lower
deck: 14,6 m³.
- fuel: 33.611 liters. |
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With 5 auxiliary fuel
tanks: |
-
empty: 42.362 Kg.
- max. payload: 14.821
Kg.
- cargo volume lower
deck: 11,7 m³.
- fuel: 35.579 liters. |
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With 6 auxiliary fuel
tanks: |
-
empty: 42.540 Kg.
- max. payload: 14.609
Kg.
- cargo volume lower
deck: 9 m³.
- fuel: 37.540 liters. |
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With 7 auxiliary fuel
tanks: |
-
empty: 42.633 Kg.
- max. payload: 14.520
Kg.
- cargo volume lower
deck: 7,6 m³.
- fuel: 38.660 liters. |
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With 8 auxiliary fuel
tanks: |
-
empty: 42.797 Kg.
- max. payload: 14.385
Kg.
- cargo volume lower
deck: 6,1 m³.
- fuel: 39.584 liters. |
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With 9 auxiliary fuel
tanks: |
-
empty: 42.896 Kg.
- max. payload: 14.286
Kg.
- cargo volume lower
deck: 4.6 m³.
- fuel: 40.485 liters. |
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Range:
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- 8
passengers: 11.480 km.
- 25 passengers: 11.075
km.
- 50 passengers: 10.205
km. |
*
Generally similar to the Boeing 737-700
except in the following particulars.
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Boeing 737-700 production:
built
704, active 703,
approximately on order 274, stored 1 at April 2005.
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Boeing 737 built
of each type: |
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- 30 Boeing 737-100 |
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- 1095 Boeing 737-200 |
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- 19 Boeing T-43A |
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- 1113 Boeing 737-300 |
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- 486 Boeing 737-400 |
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- 389 Boeing 737-500 |
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- 57 Boeing 737-600 |
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- 704 Boeing 737-700 |
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- 855 Boeing 737-800 |
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- 46 Boeing 737-900 |
No Boeing 737-700 written-off by accidents: |
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