A/C	Manufacturer	Boeing		Boeing	Boeing	Boeing		Boeing	Boeing	Boeing	Boeing		Boeing		Boeing		Boeing		Boeing			Sources:
	Aircraft type	717-200		737-300	737-400	737-500		737-700	737-800	737-900	737-900ER		737-8		757-200		MD-80		MD-80		[1]	https://www.flightglobal.com/download?ac=73559
	Total number of operating A/C	145	[1]	214	141	161	[1]	979	4788	556*	556*	[1]	347	[1]	302	[1]	232	[1]	232	[1]	[2]	https://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/737_RevA.pdf
	Option/Variant	HGW	[5]	-	-	-		-	-	-	-		-		-		MD-82/-88	[15]	MD-87	[15]	[3]	https://www.easa.europa.eu/downloads/7297/en
Engine	No. of Engines	2	[6]	2	2	2	[2]	2	2	2	2	[2]	2	[4]	2	[12]	2	[15]	2	[15]	[4]	https://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/737MAX_RevF.pdf
	Model	BR700-715C1-30	[6]	CFM56-3B-2	CFM56-3C-1	CFM56-3B-1	[2]	CFM56-7B22	CFM56-7B22	CFM56-7B22	CFM56-7B22	[2]	LEAP-1B28	[4]	PW2040	[12]	JT8D-217	[15]	JT8D-217C	[15]	[5]	https://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/717.pdf
	Max. Rated Takeoff Thrust, T_TO [kN]	95,33	[9]	98,3	104,5	89,4	[11]	100,97	100,97	100,97	100,97	[11]	130,41	[11]	181,93	[14]	92,7	[16]	92,7	[16]	[6]	https://www.easa.europa.eu/downloads/8159/en
	Equivalent Power, P [kW]	-		-	-	-		-	-	-	-		-		-		-		-		[7]	https://www.boeing.com/commercial/aeromagazine/aero_19/717_characteristics.pdf
	Propeller	-		-	-	-	[2]	-	-	-	-	[2]	-		-		-		-		[8]	https://www.boeing.com/resources/boeingdotcom/company/about_bca/startup/pdf/historical/717_passenger.pdf
Cabin	Length, l_CABIN [m]	N/A		N/A	N/A	N/A		N/A	N/A	N/A	N/A		N/A		N/A		N/A		N/A		[9]	https://www.easa.europa.eu/downloads/7757/en
	Max. Height, h_CABIN [m]	2,2	[5]	2,2	2,2	2,2	[2]	2,2	2,2	2,2	2,2	[2]	2,2	[4]	2,13	[12]	2,04	[15]	2,04	[15]	[10]	https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/c1817d49c964876886256b1400759d25/%24FILE/A6WE.pdf
	Max. Width, d_F,I [m]	3,13	[5]	3,54	3,54	3,54	[2]	3,54	3,54	3,54	3,54	[2]	3,54	[4]	3,54	[12]	3,16	[15]	3,16	[15]	[11]	https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/179cdacd213801658625832a006b2e37/$FILE/A16WE_Rev_64.pdf
	Passenger Compartment Volume, V_CABIN [m³]	N/A		N/A	N/A	N/A		N/A	N/A	N/A	N/A		N/A		N/A		N/A		N/A		[12]	https://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/757_23.pdf
Fuselage	Height, h_F [m]	3,6	[5]	4,01	4,01	4,01	[2]	4,01	4,01	4,01	4,01	[2]	4,01	[4]	4,01	[12]	3,61	[15]	3,61	[15]	[13]	https://www.easa.europa.eu/downloads/7246/en
	Width, w_F [m]	3,34	[5]	3,76	3,76	3,76	[2]	3,76	3,76	3,76	3,76	[2]	3,76	[4]	3,76	[12]	3,35	[15]	3,35	[15]	[14]	https://man.fas.org/dod-101/sys/ac/docs/a2nm.pdf
Total	Length, l_A/C [m]	37,81	[6]	33,4	36,45	31,01	[3]	32,18	39,5	42,1	42,1	[3]	39,47	[4]	47,32	[13]	45,02	[15]	39,75	[15]	[15]	https://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/md80.pdf
	Span, b_W [m]	28,45	[6]	28,88	28,88	28,88	[3]	35,79	35,79	35,79	35,79	⁸[3]	35,92	[4]	38,02	[13]	32,85	[15]	32,85	[15]	[16]	https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/e902a54c589cfaca862586b800631b4f/$FILE/E9NE%20Rev%2012.pdf
	Height, h_A/C [m]	8,88	[6]	11,13	11,13	11,13	[3]	12,57	12,57	12,57	12,57	[3]	12,29	[4]	13,75	[13]	9	[15]	9,2	[15]		Comments:
Landing Gear	Track, l_T [m]	4,9	[5]	5,23	5,23	5,23	[2]	5,72	5,72	5,72	5,72	[2]	5,72	[4]	7,32	[12]	5,08	[15]	5,08	[15]		*Number of operating aircrafts includes all variants of the aircraft type
	Wheelbase, l_WB [m]	17,6	[5]	12,45	14,27	11,07	[2]	12,6	15,6	17,17	17,17	[2]	15,6	[4]	18,29	[12]	22,05	[15]	19,18	[15]		¹ Standard day, zero wind, reserves based on 200 nm alternate
Wing	Area, S_W [m²]	92,97	[6]	N/A	N/A	N/A		N/A	N/A	N/A	N/A		N/A		N/A		N/A		N/A			² Standard day, zero wind, domestic reserves
	Taper ratio, λ_W	0,27	[5]	0,25	0,25	0,25	[2]	0,22	0,22	0,22	0,22	[2]	0,24	[4]	0,23	[12]	0,24	[15]	0,24	[15]		³ Standard day, zero wind, no winglets, typical mission rules
	1/4 Chord Sweep, φ_25,W [°]	24	[5]	26	26	26	[2]	26	26	26	26	[2]	26,5	[4]	23,5	[12]	24	[15]	24	[15]		⁴ Standard day, zero wind, typical mission rules
Vertical Tail	Area, S_V [m²]	N/A		N/A	N/A	N/A		N/A	N/A	N/A	N/A		N/A		N/A		N/A		N/A			⁵ Standard day, nominal performance, ATA domestic reserves
	Height, b_V [m]	4,75	[5]	6,38	6,38	6,38	[2]	7,73	7,72	7,66	7,66	[2]	7,73	[4]	8,01	[12]	4,59	[15]	4,59	[15]		⁶ FAR 121.639, 200 nm distance to alternate, standard day, no wind
	Taper ratio, λ_V	0,74	[5]	0,42	0,42	0,42	[2]	0,22	0,23	0,22	0,22	[2]	0,27	[4]	0,37	[12]	0,71	[15]	0,71	[15]		⁷ Domestic reserves at 200 nm alternate plus 45 min at LRC, standard day, no wind, no aux tank
	1/4 Chord Sweep, φ_25,V [°]	43	[5]	35	35	35	[2]	30	30	30	30	[2]	33,5	[4]	39	[12]	40	[15]	40	[15]		⁸ without winglets: 34,32
Horizontal Tail	Area, S_H [m²]	N/A		N/A	N/A	N/A		N/A	N/A	N/A	N/A		N/A		N/A		N/A		N/A
	Span, b_H [m]	11,2	[5]	12,7	12,7	12,7	[2]	14,35	14,35	14,35	14,35	[2]	14,35	[4]	15,21	[12]	12,25	[15]	12,25	[15]
	Taper Ratio, λ_H	0,37	[5]	0,52	0,52	0,52	[2]	0,33	0,33	0,33	0,33	[2]	0,2	[4]	0,36	[12]	0,37	[15]	0,37	[15]
	1/4 Chord Sweep, φ_25,H [°]	31	[5]	29	29	29	[2]	32	32	32	32	[2]	30	[4]	31	[12]	31	[15]	31	[15]
Cruise	V_MO [kt]	492	[10]	492	492	492	[11]	492	492	492	492	[11]	492	[11]	513	[14]	500	[10]	492	[10]
	M_MO [Mach]	0,82	[10]	0,82	0,82	0,82	[11]	0,82	0,82	0,82	0,82	[11]	0,82	[11]	0,86	[14]	0,84	[10]	0,82	[10]
	Cruise Speed, M_CR [Mach]	N/A		N/A	N/A	N/A		N/A	N/A	N/A	N/A		N/A		0,8	[12]	N/A		N/A
	Max. Certified Flight Level, h_MCR [FL]	370	[10]	370	370	370	[11]	410	410	410	410	[11]	410	[3]	420	[13]	370	[10]	370	[10]
	Cruise Altitude, h_CR [FL]	N/A		350	350	350	[2]	N/A	N/A	N/A	N/A	[2]	N/A		390	[12]	350	[15]	350	[15]
Fuel	Unusable Fuel [l]	154	[10]	N/A	N/A	N/A	[2]	N/A	N/A	N/A	N/A	[2]	N/A		N/A		138	[10]	137	[10]
	Optional Fuel [l]	-		3785	3785	3785	[2]	-	-	-	3641	[2]	-		-		4278	[10]	4339	[10]
	Max usable fuel [l]	14758	[10]	23827	23827	23827	[2]	26022	26022	26022	29666	[2]	25817	[4]	42680	[12]	22129	[10]	22126	[10]
Range	Max. Payload, R_MPL [nm]	1200	¹[5]	1900	1700	1800	²[2]	2150	2000	2000	1700	³[2]	2650	⁴[4]	2450	⁵[12]	1170	⁶[15]	1400	⁷[15]
	Max. Pax, R_M,pax [nm]	2050	¹[5]	2800	2650	2950	²[2]	3700	3400	2850	3800	³[2]	3700	⁴[4]	4150	⁵[12]	2050	⁶[15]	2400	⁷[15]
	Max. Range, R_PLMR [nm]	2000	¹[5]	2750	2500	2900	²[2]	3350	4050	2800	4250	³[2]	3450	⁴[4]	3800	⁵[12]	2040	⁶[15]	2380	⁷[15]
Mass	Max. Ramp, m_MR (MRM) [kg]	55338	[5]	63503	68266	61915	[2]	70307	79333	79243	85366	[2]	82871	[3]	116119	[13]	68266	[15]	63957	[15]
	Max. Take-Off, m_MTO (MTOM) [kg]	54884	[5]	63276	68039	61689	[2]	70080	79016	79016	85139	[2]	82645	[3]	115893	[13]	67812	[15]	63503	[15]
	Max. Landing, m_ML (MLM) [kg]	49898	[5]	52889	56245	49895	[2]	58604	66361	66814	71350	[2]	69308	[3]	95254	[13]	58567	[15]	58060	[15]
	Max. Zero Fuel, m_MZF (MZFM) [kg]	45586	[5]	49714	53070	46720	[2]	55202	62732	63639	67721	[2]	65952	[3]	90718	[13]	55338	[15]	50802	[15]
	Operating Empty, m_OE (OEM) (MZFM-MPL) [kg]	31071	[5]	32904	33643	31311	[2]	37648	41413	42901	44677	[2]	40823	[4]	54431	[12]	35369	[15]	33236	[15]
	Max. Payload, m_MPL (MPL) [kg]	14515	[5]	16148	19881	15182	[2]	17554	21319	20738	23045	[2]	25129	[4]	36287	[12]	19969	[15]	17566	[15]
	Payload at Max. Range, m_PLMR [kg]	10500	[5]	11000	15000	10000	[2]	11500	10500	15000	10500	[2]	21000	[4]	26500	[12]	14500	[15]	13000	[15]
Cargo	Volume, V_CARGO [m³]	20,7	[5]	30,2	38,9	23,3	[2]	27,4	44,1	52	51,7	[2]	43,6	[4]	51	[12]	35,5	[15]	26,6	[15]
	Cargo Capacity	-		-	-	-		-	-	-	-		-		-		-		-
	Max. Pallet Underfloor	-		-	-	-		-	-	-	-		-		-		-		-
Seats	Max. Seats, n_M,SEAT	134	[6]	149	189	149	[2]	148	184	189	215	[2]	189	[3]	239	[14]	172	[15]	139	[15]
	Std. Layout, n_SEAT	106	[5]	134	159	122	[2]	128	160	177	186	[2]	180	[3]	186	[12]	155	[15]	130	[15]