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 |



BOEING 737 - PHOTOS
Boeing 737-8AS - Ryanair |
Boeing 737-8AS - Ryanair |
Boeing 737-86J - Air Berlin |
Boeing 737-31S - Air One |


