Beechcraft King Air

First flight year — 1963

Beechcraft King Air Specifications


	B100	B200	King Air 350

Dimensions
Length (m)	12.2	13.3	14.2
Wingspan (m)	14.0	16.6	17.6
Height (m)	4.7	4.5	4.4
Wing area (m2)	26.0	28.2	28.8
Weight
Maximum take-off weight (kg)	5 350	5 670	6 800
Maximum landing weight (kg)			6 800
Operating empty weight (kg)	3 210	3 520	4 340
Maximum zero fuel weight (kg)			5 670
Maximum payload (kg)		1 820	2 440
Standard fuel capacity (litres)			2 040
Performance
Maximum range (km)	2 450	3 300	3 300
Maximum speed (km/h)	490	540	580
Maximum operating altitude (m)	7 570	10 670	10 600
Take-off field length (m)			1 000
Landing field length (m)			820
Engines	Garrett TPE-331, 2 x 840 hp	P&WC PT6A-42, 2 x 850 hp	P&WC PT6A-60A, 2 x 1050 hp
Cabin Data
Passengers (1-class)	13	13	15
Cabin length (m)		5.08	5.94
Cabin width (m)		1.37	1.37
Cabin height (m)		1.45	1.45