Boeing 737 (600/700/800/900) NG

Boeing 737 Next Generation - 737-600 / 737-700 / 737-800 / 737-900

 

Family

NG's

Series

600

700

800

900

Production:

       

First flight

22 Jan 1998

9 Feb 1997

31 Jul 1997

3 Aug 2000

First delivery

18 Sep 1998

17 Dec 1997

22 Apr 1998

15 May 2001

Launch customer

SAS

Southwest

HapagLloyd

Alaska

Powerplant:

       

Model

CFM56-7

CFM56-7

CFM56-7

CFM56-7

Type

7B18

7B20

7B24

7B26

Static Thrust (kN)

82.0

89.0

107.0

117.3

Static Thrust (Lb)

18,500

20,600

24,200

26,300

Bypass Ratio

5.5

5.4

5.3

5.1

EGT Margin (C)

145

148

125

85

Fan tip diameter (in)

61

61

61

61

Max Nacelle Width (m)

2.06

2.06

2.06

2.06

Dimensions:

       

Fuselage:

   

 

 

Aircraft length (m)

31.20

33.60

39.50

42.10

Fuselage length (m)

29.88

32.18

38.08

40.68

Height (m)

4.01

4.01

4.01

4.01

Width (m)

3.76

3.76

3.76

3.76

Cabin width (m)

3.53

3.53

3.53

3.53

Finess Ratio

8.01

8.63

10.21

10.91

Wing:

       

Span (m)

34.32

34.32

34.32

34.32

Gross Area (m²)

124.58

124.58

124.58

124.58

Aspect Ratio

9.45

9.45

9.45

9.45

Taper Ratio

0.159

0.159

0.159

0.159

Root Chord %

7.88

7.88

7.88

7.88

Tip Chord %

1.25

1.25

1.25

1.25

M.A.C.(m)

3.96

3.96

3.96

3.96

Dihedral (º)

6

6

6

6

¼ Chord Sweep (º)

25.02

25.02

25.02

25.02

Wing High Lift Devices:

       

Flap Span/Wing Span

0.599

0.599

0.599

0.599

Flap Area/Wing Area

0.300

0.300

0.300

0.300

Fin:

       

Aircraft Height (m)

12.6

12.6

12.6

12.6

Fin Height (m)

7.16

7.16

7.16

7.16

Fin Area (m²)

26.44

26.44

26.44

26.44

Rudder Area (m²)

5.22

5.22

5.22

5.22

Aspect Ratio

1.91

1.91

1.91

1.91

Taper Ratio

0.271

0.271

0.271

0.271

¼ Chord Sweep (º)

35

35

35

35

Horiz Stabilizer:

 

     

Span (m)

14.35

14.35

14.35

14.35

Tailplane Area (m²)

32.78

32.78

32.78

32.78

Elevators Area (m²)

6.55

6.55

6.55

6.55

Aspect Ratio

6.16

6.16

6.16

6.16

Taper Ratio

0.203

0.203

0.203

0.203

Dihedral (º)

7

7

7

7

¼ Chord Sweep (º)

30

30

30

30

Undercarriage:

       

Track (m)

5.76

5.76

5.76

5.76

Wheelbase (m)

 

12.60

15.60

 

Turning radius (m)

 

19.50

   

No. of Nose Wheels

2

2

2

2

Nose Wheel Diameter (Inches)

27

27

27

27

Nose Wheel Tread Width (Inches)

7.75

7.75

7.75

7.75

Nose Tyre Pressure (psi)

146-208

142-208

123-208

?-208

No. of Main Wheels

4

4

4

4

Main Wheel Diameter (Inches)

43.5 or 44.5

43.5 or 44.5

44.5

44.5

Main Wheel Tread Width (Inches)

14.5

14.5

14.5

14.5

Main Tyre Pressure (psi)

117-205

117-205

120-205

?-205

Operational Items:

       

Accomodation:

 

     

Max certified seating

149

149

189

189

Typical seating

145

145

180

180

No. abreast

6

6

6

6

Cabin Width

3.53

3.53

3.53

3.53

Hold volume (m³)

23.30

30.20

47.10

52.40

Volume per Passenger

0.18

0.20

0.25

0.28

Std Weights (kg):

       

Max. ramp

65317

70295

79229

79229

Max. take-off

65090

70068

79002

79002

Max. landing

54657

58594

66349

66349

Max. zero-fuel

51482

55193

62721

63628

IGW Weights:

       

Max. ramp

65317

77791

79229

79229

Max. take-off

65090

77564

79002

79002

Max. landing

54657

60781

66349

66349

Max. zero-fuel

51482

57153

62721

63628

Fuel capacity (ltrs)

26025

26025

26025

26025

Fuel capacity (kg)

21000

21000

21000

21000

Typical DOW

36440

37585

41480

42460

Design payload

12540

14155

17955

17955

Max payload

14380

16505

20540

20240

Weight Ratios:

     

 

Ops Empty/Max T/O

0.560

0.542

0.530

0.537

Payload/Max T/O

0.193

0.204

0.230

0.227

Max Fuel/Max T/O

0.320

0.300

0.266

0.264

Fuel (litres):

 

 

 

 

Standard

26035

26035

26035

26035

Optional

 

37712 (BBJ)

37712 (BBJ2)

 

Performance:

       

Loadings:

       

Thrust Loading (kg/kN)

396.89

389.89

365.51

336.79

Wing Loading (kg/m²)

522.39

556.98

627.77

634.11

Thrust/Weight Ratio

0.2568

0.2615

0.2789

0.3027

Long range cruise:

       

IAS / Mach

230/0.785

230/0.785

230/0.785

230/0.785

TAS (kt)

450

450

450

450

Ceiling (ft)

41000

41000

41000

41000

L.R. Fuel flow (kg/h)

1932

2070

2187

<2300

Range with max payload (nm)

3153

3299

2926

2726

Design Parameters:

       

Fuel/pax/nm (kg)

0.0534

0.0480

0.0465

0.0409

Seat x Range (seats.nm)

421212

476353

547533

515592


B737NG
 
 
B737NG Seating
 
 
B737NG Cross sections

 

 


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