A/C	Manufacturer	Fokker		Fokker			Sources:
	Aircraft type	Fokker 50		Fokker 100		[1]	https://www.flightglobal.com/download?ac=73559
	Total number of operating A/C	86	[1]	109	[1]	[2]	https://www.fokkerservices.com/media/53peaal2/fokker100_informationbooklet.pdf
	Option/Variant	F27 Mark 050	[6]	F28 Mark 0100	[3]	[3]	https://www.easa.europa.eu/downloads/7450/en
Engine	No. of Engines	2	[6]	2	[2]	[4]	https://web.archive.org/web/20091127210225/http:/www.flyfokker.com/downloads/FlyFokker/Leaflet%20Fokker%20100.pdf
	Model	PW125B	[6]	Tay 650-15	[2]	[5]	https://web.archive.org/web/20120321232627/http:/www.aer.ita.br/~bmattos/mundo/airliner/fo100.htm
	Max. Rated Takeoff Thrust, T_TO [kN]	-	[6]	67,17	[3]	[6]	https://www.easa.europa.eu/downloads/8335/en
	Equivalent Power, P [kW]	1864	[8]	-		[7]	https://www.fokkerservices.com/media/z05j5mhx/fokker50_informationbooklet.pdf
	Propeller	R352/6-123-F/1	[6]	-		[8]	https://www.easa.europa.eu/downloads/7725/en
Cabin	Length, l_CABIN [m]	N/A		21,19	[5]	[9]	https://www.allianceairlines.com.au/docs/default-source/Fleet/fokker-50_c.pdf?sfvrsn=6e0f1e9e_2
	Max. Height, h_CABIN [m]	N/A		2,01	[5]	[10]	https://en.wikipedia.org/wiki/Fokker_50
	Max. Width, d_F,I [m]	2,5	[10]	3,1	[5]		Comments:
	Passenger Compartment Volume, V_CABIN [m³]	N/A		N/A			¹ ISA, zero wind, LRC, EU-OPS1.225 reserves: 100 nm alternate
Fuselage	Height, h_F [m]	2,8	[7]	3,3	[2]
	Width, w_F [m]	2,7	[10]	3,3	[2]
Total	Length, l_A/C [m]	25,25	[7]	35,53	[2]
	Span, b_W [m]	29	[7]	28,08	[2]
	Height, h_A/C [m]	8,32	[7]	8,42	[2]
Landing Gear	Track, l_T [m]	7,2	[7]	5,04	[2]
	Wheelbase, l_WB [m]	8,1	[7]	14,01	[2]
Wing	Area, S_W [m²]	70	[10]	N/A
	Taper ratio, λ_W	0,40	[7]	0,29	[2]
	1/4 Chord Sweep, φ_25,W [°]	1,5	[7]	17,5	[2]
Vertical Tail	Area, S_V [m²]	N/A		N/A
	Height, b_V [m]	4,6	[7]	4,08	[2]
	Taper ratio, λ_V	0,385	[7]	0,705	[2]
	1/4 Chord Sweep, φ_25,V [°]	17	[7]	37,5	[2]
Horizontal Tail	Area, S_H [m²]	N/A		N/A
	Span, b_H [m]	9,75	[7]	10,04	[2]
	Taper Ratio, λ_H	0,36	[7]	0,41	[2]
	1/4 Chord Sweep, φ_25,H [°]	6	[7]	25,5	[2]
Cruise	V_MO [kt]	305	[10]	462	[5]
	M_MO [Mach]	0,507	[10]	0,77	[5]
	Cruise Speed, M_CR [Mach]	0,45	[9]	N/A
	Max. Certified Flight Level, h_MCR [FL]	250	[6]	350	[3]
	Cruise Altitude, h_CR [FL]	N/A		N/A
Fuel	Unusable Fuel [l]	N/A		94	[3]
	Optional Fuel [l]	-		-
	Max usable fuel [l]	5136	[6]	13365	[3]
Range	Max. Payload, R_MPL [nm]	600	¹[7]	1370	¹[2]
	Max. Pax, R_M,pax [nm]	920	¹[7]	1590	¹[2]
	Max. Range, R_PLMR [nm]	1720	¹[7]	1720	¹[2]
Mass	Max. Ramp, m_MR (MRM) [kg]	20865	[6]	46040	[3]
	Max. Take-Off, m_MTO (MTOM) [kg]	20820	[6]	45810	[2]
	Max. Landing, m_ML (MLM) [kg]	20030	[6]	39915	[2]
	Max. Zero Fuel, m_MZF (MZFM) [kg]	18900	[6]	36740	[2]
	Operating Empty, m_OE (OEM) (MZFM-MPL) [kg]	13400	[7]	24747	[5]
	Max. Payload, m_MPL (MPL) [kg]	5500	[7]	11993	[5]
	Payload at Max. Range, m_PLMR [kg]	3300	[7]	9200	[2]
Cargo	Volume, V_CARGO [m³]	5,51	[9]	18,02	[5]
	Cargo Capacity	-		-
	Max. Pallet Underfloor	-		-
Seats	Max. Seats, n_M,SEAT	62	[6]	109	[2]
	Std. Layout, n_SEAT	50	[6]	100	[2]