Boeing 737 (100/200) Original

Family

Original's

Series

100

200 Adv

Production:

First flight

9 Apr 1967

8 Aug 1967

First delivery

28 Dec 1967

29 Dec 1967

Launch customer

Lufthansa

United

2 Nov 1969

2 Aug 1988

Powerplant:

Model

JT8D

JT8D

Type

-7

-15A

Static Thrust (kN)

64.4

71.2

Static Thrust (Lb)

14,000

16,000

Bypass Ratio

1.1

0.99

EGT Margin (C)

Fan tip diameter (in)

54

54

Max Nacelle Width (m)

1.50

1.50

Dimensions:

Fuselage:

Aircraft length (m)

28.65

30.53

Fuselage length (m)

27.66

29.54

Height (m)

4.01

4.01

Width (m)

3.76

3.76

Cabin width (m)

3.53

3.53

Finess Ratio

7.42

7.92

Wing:

Span (m)

28.35

28.35

Gross Area (m²)

102.0

102.0

Aspect Ratio

8.83

8.83

Taper Ratio

0.266

0.266

Root Chord %

4.71

4.71

Tip Chord %

1.60

1.60

M.A.C.(m)

3.80

3.80

Dihedral (º)

6

6

¼ Chord Sweep (º)

25.00

25.00

Wing High Lift Devices:

Flap Span/Wing Span

0.740

0.740

Flap Area/Wing Area

0.290

0.290

Fin:

Aircraft Height (m)

11.23

11.23

Fin Height (m)

6.15

6.15

Fin Area (m²)

20.81

20.81

Rudder Area (m²)

5.22

5.22

Aspect Ratio

1.64

1.64

Taper Ratio

0.288

0.288

¼ Chord Sweep (º)

35

35

Horiz Stabilizer:

Span (m)

10.97

10.97

Tailplane Area (m²)

28.99

28.99

Elevators Area (m²)

6.55

6.55

Aspect Ratio

4.15

4.15

Taper Ratio

0.260

0.260

Dihedral (º)

7

7

¼ Chord Sweep (º)

30

30

Undercarriage:

Track (m)

5.23

5.23

Wheelbase (m)

10.46

11.38

Turning radius (m)

17.20

17.58

No. of Nose Wheels

2

2

Nose Wheel Diameter (Inches)

24

24

Nose Wheel Tread Width (Inches)

7.75

7.75

Nose Tyre Pressure (psi)

No. of Main Wheels

4

4

Main Wheel Diameter (Inches)

40

40

Main Wheel Tread Width (Inches)

14.5

14.5

Main Tyre Pressure (psi)

133

183

Operational Items:

Accomodation:

Max certified seating

124

136

Typical seating

113

119

No. abreast

6

6

Cabin Width

3.53

3.53

Hold volume (m³)

18.40

24.78

Volume per Passenger

0.22

0.19

Std Weights (kg):

Max. ramp

44361

52615

Max. take-off

44225

52390

Max. landing

40687

46720

Max. zero-fuel

38555

43091

IGW Weights:

Max. ramp

44361

58332

Max. take-off

44225

58105

Max. landing

40687

48534

Max. zero-fuel

38555

44906

Fuel capacity (ltrs)

17865

19532

Fuel capacity (kg)

14292

15750

Typical DOW

25941

27646

Design payload

10925

12350

Max payload

15710

Weight Ratios:

Ops Empty/Max T/O

0.622

0.528

Payload/Max T/O

0.247

0.236

Max Fuel/Max T/O

0.354

0.298

Fuel (litres):

Standard

17865

19532

Optional

22600

Performance:

Loadings:

Thrust Loading (kg/kN)

343.17

367.91

Wing Loading (kg/m²)

433.33

513.63

Thrust/Weight Ratio

0.297

0.2771

Long range cruise:

IAS / Mach

0.73

0.73

TAS (kt)

420

420

Ceiling (ft)

35000

37000

L.R. Fuel flow (kg/h)

?

2827

Range with max payload (nm)

1590

2645

Design Parameters:

Fuel/pax/nm (kg)

0.0264

0.0632

Seat x Range (seats.nm)

218500

247000