Boeing 737 differences

Family	Original's		Classic's			NG's
Series	100	200 Adv	300	400	500	600	700	800	900
First flight	9-Apr-67	8-Aug-67	24-Feb-84	19-Feb-88	30-Jun-89	22-Jan-98	9-Feb-97	31-Jul-97	3-Aug-00
First delivery	28-Dec-67	29-Dec-67	28-Nov-84	15-Sep-88	28-Feb-90	18-Sep-98	17-Dec-97	22-Apr-98	15-May-01
Units produced	30	1114	1113	489	388	66	760	1026	52
Still in service	0	595	1002	460	367	66	759	1025	52
Powerplant:
Model	JT8D	JT8D	CFM56-3	CFM56-3	CFM56-3	CFM56-7	CFM56-7	CFM56-7	CFM56-7
Type	-7	-15A	-100	C-1	#VALUE!	7B18	7B20	7B24	7B26
Static Thrust (kN)	64.4	71.2	88.9	104.5	82.3	82.0	89.0	107.0	117.3
Static Thrust (Lb)	14,000	16,000	20,000	23,500	18,500	18,500	20,600	24,200	26,300
Bypass Ratio	1.1	0.99	5	4.9	5	5.5	5.4	5.3	5.1
EGT Margin (C)			50	45	90	145	148	125	85
Fan tip diameter (in)	54	54	60	60	60	61	61	61	61
Max Nacelle Width (m)	1.5	1.5	2	2	2	2.06	2.06	2.06	2.06
Dimensions:
Fuselage:
Aircraft length (m)	28.65	30.53	33.4	36.45	31.01	31.2	33.6	39.5	42.1
Fuselage length (m)	27.66	29.54	32.30	35.23	29.80	29.88	32.18	38.08	40.68
Height (m)	4.01	4.01	4.01	4.01	4.01	4.01	4.01	4.01	4.01
Width (m)	3.76	3.76	3.76	3.76	3.76	3.76	3.76	3.76	3.76
Cabin width (m)	3.53	3.53	3.53	3.53	3.53	3.53	3.53	3.53	3.53
Finess Ratio	7.42	7.92	8.66	9.46	8.02	8.01	8.63	10.21	10.91
Wing:
Span (m)	28.35	28.35	28.88	28.88	28.88	34.32	34.32	34.32	34.32
Gross Area (m²)	102.00	102.00	105.40	105.40	105.40	124.58	124.58	124.58	124.58
Aspect Ratio	8.83	8.83	9.16	9.16	9.16	9.45	9.45	9.45	9.45
Taper Ratio	0.266	0.266	0.240	0.240	0.240	0.159	0.159	0.159	0.159
Root Chord (m)	7.32	7.32	7.32	7.32	7.32	7.88	7.88	7.88	7.88
Tip Chord (m)	1.60	1.60	1.62	1.62	1.62	1.25	1.25	1.25	1.25
M.A.C.(m)	3.8	3.8	3.41	3.41	3.41	3.96	3.96	3.96	3.96
Dihedral (º)	6.00	6.00	6.00	6.00	6.00	6.00	6.00	6.00	6.00
¼ Chord Sweep (º)	25.00	25.00	25.00	25.00	25.00	25.02	25.02	25.02	25.02
Wing High Lift Devices:
Flap Span/Wing Span	0.740	0.740	0.720	0.720	0.720	0.599	0.599	0.599	0.599
Flap Area/Wing Area	0.290	0.290	0.290	0.290	0.290	0.300	0.300	0.300	0.300
Fin:
Aircraft Height (m)	11.23	11.23	11.13	11.13	11.13	12.6	12.6	12.6	12.6
Fin Height (m)	6.15	6.15	6.15	6.15	6.15	7.16	7.16	7.16	7.16
Fin Area (m²)	20.81	20.81	23.13	23.13	23.13	26.44	26.44	26.44	26.44
Rudder Area (m²)	5.22	5.22	5.22	5.22	5.22	5.22	5.22	5.22	5.22
Aspect Ratio	1.64	1.64	1.81	1.81	1.81	1.91	1.91	1.91	1.91
Taper Ratio	0.288	0.288	0.310	0.310	0.310	0.271	0.271	0.271	0.271
¼ Chord Sweep (º)	35.00	35.00	35.00	35.00	35.00	35.00	35.00	35.00	35.00
Horiz Stabilizer:
Span (m)	10.97	10.97	12.7	12.7	12.7	14.35	14.35	14.35	14.35
Tailplane Area (m²)	28.99	28.99	31.4	31.4	31.4	32.78	32.78	32.78	32.78
Elevators Area (m²)	6.55	6.55	6.55	6.55	6.55	6.55	6.55	6.55	6.55
Aspect Ratio	4.15	4.15	4.04	4.04	4.04	6.16	6.16	6.16	6.16
Taper Ratio	0.260	0.260	0.260	0.260	0.260	0.203	0.203	0.203	0.203
Dihedral (º)	7	7	7	7	7	7	7	7	7
¼ Chord Sweep (º)	30.00	30.00	30.00	30.00	30.00	30.00	30.00	30.00	30.00
Undercarriage:
Track (m)	5.23	5.23	5.25	5.25	5.25	5.76	5.76	5.76	5.76
Wheelbase (m)	10.46	11.38	12.40	14.27	11.07		12.60	15.60
Turning radius (m)	17.20	17.58	19.51	20.73	18.30		19.50
No. of Nose Wheels	2	2	2	2	2	2	2	2	2
Nose Wheel Diameter (Inches)	24.000	24.000	27.000	27.000	27.000	27.000	27.000	27.000	27.000
Nose Wheel Tread Width (Inches)	7.750	7.750	7.750	7.750	7.750	7.750	7.750	7.750	7.750
Nose Tyre Pressure (psi)			160-165	173-184	186-194	146-208	142-208	123-208	?-208
No. of Main Wheels	4	4	4	4	4	4	4	4	4
Main Wheel Diameter (Inches)	40	40	40 or 42	40 or 42	40 or 42	43.5 or 44.5	43.5 or 44.5	44.500	44.500
Main Wheel Tread Width (Inches)	14.5	14.5	14.5	14.5	14.5	14.5	14.5	14.5	14.5
Main Tyre Pressure (psi)	133.000	183.000	195-203	211-217	193-202	117-205	117-205	120-205	?-205
Operational Items:
Accomodation:
Max certified seating	124	136	149	188	140	149	149	189	189
Typical seating	113	119	149	179	140	145	145	180	180
No. abreast	6	6	6	6	6	6	6	6	6
Cabin Width	3.53	3.53	3.53	3.53	3.53	3.53	3.53	3.53	3.53
Hold volume (m³)	18.40	24.78	30.20	38.90	23.30	23.30	30.20	47.10	52.40
Volume per Passenger	0.22	0.19	0.20	0.22	0.18	0.18	0.20	0.25	0.28
Std Weights (kg):
Max. ramp	44361	52615	56700	63049	63049	65317	70307	79229	79229
Max. take-off	44225	52390	56472	62822	62823	65090	70080	79002	79002
Max. landing	40687	46720	51710	54885	49895	54657	58604	66349	66349
Max. zero-fuel	38555	43091	47625	51256	46720	51709	55202	62721	63628
IGW Weights:
Max. ramp	44361	58332	63502	68266	63049	66224	77791	79229	85366
Max. take-off	44225	58105	63276	68039	62823	65997	77564	79002	85139
Max. landing	40687	48534	52889	56245	49895	54657	60781	66349	71350
Max. zero-fuel	38555	44906	49668	53070	46720	51709	57153	62721	67721
Fuel capacity (ltrs)	17865	19532	20103	20103	20103	26025	26025	26025	26025
Fuel capacity (kg)	14292	15750	16200	16200	16200	21000	21000	21000	21000
Typical DOW	25941	27646	32900	35100	31900	36440	37585	41480	42460
Design payload	10925	12350	14250	16530	12540	12540	14155	17955	17955
Max payload		15710	14805	18260	14770	14380	16505	20540	20240
Weight Ratios:
Ops Empty/Max T/O	0.622	0.528	0.523	0.516	0.609	0.560	0.542	0.530	0.537
Payload/Max T/O	0.247	0.236	0.225	0.243	0.239	0.193	0.204	0.230	0.227
Max Fuel/Max T/O	0.354	0.298	0.256	0.237	0.307	0.320	0.300	0.266	0.264
Fuel (litres):
Standard	17865	19532	20105	20105	20105	26035	26035	26035	26035
Optional		22600	23829	23829	23829		37712 (BBJ)	37712 (BBJ2)
Performance:
Loadings:
Thrust Loading (kg/kN)	343.17	367.91	353.48	325.35	318.28	396.89	389.89	365.51	336.79
Wing Loading (kg/m²)	433.33	513.63	596.29	645.15	497.05	522.39	556.98	627.77	634.11
Thrust/Weight Ratio	0.297	0.2771	0.2884	0.3133	0.3203	0.2568	0.2615	0.2789	0.3027
Take-off (m):
ISA s.l.	1829?	1990	1939	2540	1832
ISA +20ºC s.l.	1859?	2030	2109	2665	2003	1878	2042	2652
ISA 5,000ft	2886?	3332	2432	2932	2316
ISA +20ºC 5,000ft	3292?	3749	2637	4005	2649
Landing (m):
ISA s.l.	?	1350	1396	1540	1357	1340	1415	1634	1704
Speeds (kt/Mach):
V2 F5 at MTOW	?	147	155	167	145
Vref F40 at MLW	?	131	132	139	128
Vmo/Mmo	350/0.84	350/0.84	340/0.82	340/0.82	340/0.82	340/0.82	340/0.82	340/0.82	340/0.82
CLmax (T/O @ MTOW)	1.75	2.07	2.16	2.02	2.06
CLmax (Land @ MLW)	2.73	2.73	2.88	2.76	2.96
Long range cruise:
IAS / Mach	0.73	0.73	250/0.745	250/0.745	250/0.745	230/0.785	230/0.785	230/0.785	230/0.785
TAS (kt)	420	420	430	430	430	450	450	450	450
Ceiling (ft)	35000	37000	37000	37000	37000	41000	41000	41000	41000
L.R. Fuel flow (kg/h)	?	2827	2250	2377	2100	1932	2070	2187	<2300
Range with max payload (nm)	1720	2645	2950	2800	2950	4500	4400	4000	3200
Design Parameters:
(W/S)/CLmax	1557	1845	2031	2296	1650
W/SCLtoST	1997	2538	2683	2792	1962
Seat x Range (seats.nm)	218500	247000	427500	469800	224400	421212	476353	547533	515592