*****AIRCRAFT
“Beech – 90 King Air”*****
REFERENCE
INFORMATION (by Aircraft performance database)
*****Aircraft Features*****
Wing
position: Low wing
Engine
position: (Front) Wing leading mounted
Tail
configuration: Regular tail, mid set
Landing gear:
Tricycle retractable
Wing
Span:
Length:
Height:
Power
plant2 x 500 SHP P&W PT6A -6 or 2 x 530 SHP
P&W PT6A -20 or
2 x 550 SHP P&W PT6A -21 or 2 x 560 SHP
P&W PT6A -34 turboprops
with 3 blade
propellers.
One or two pilots and 4 passengers
in main cabin.
Notes: Corporate and utility aircraft. In service since 1964.
Turboprop development of BEECH Queen
Air. Exists in some civil and
military versions,
E90 with more powerful engines and F90 (ICAO
designator: BE9T)
with the T-tail of the Beech 200 Super King Air.
Stretched development: Beech 100
King Air. This type has been taken
over and is
partly built by
Alternative names:
A90 to E90 King Air,
BEECH 90,A90 to E90 King Air (T-44,VC-6)
JETCRAFTERS Taurus 90, King Air (90), RAYTHEON 90
King Air
SWEARINGEN Taurus 90, T-44, Taurus 90, VC-6
BEECH 90,A90 to E90 King Air
*****Total Flight Simulator aircraft weight
with full fuel*****
VMO -
Maximum Operating Speed 220 KIAS
MMO -
Maximum Operating Speed Mach
nd Mach
Turbulent
Air Penetration Speed 000 KIAS/.00 Mach
VLO -
Maximum Gear Operating Speed 000 KIAS
VLE -
Maximum Landing Gear Extension Speed
000 KIAS/.00 Mach
*****Maximum Flap Placard Speeds*****
Flaps
degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: L
Distance: 700 mt
V2
(IAS): 100 kts
*****Climbing*****
-(to
IAS: 130 kt
ROC: 1500 ft/min
-(to
FL150)
IAS: 200 kt
ROC: 1000 ft/min
-(to
FL240)
IAS: 200 kt
ROC: 1000 ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 220 kt
MACh: 0.39
Ceiling: FL290
Range: 1150 NM
*****Descent *****
- (to
FL240)
mach: nd
ROD: nd ft/min
- (to
FL100)
IAS: 240 kt
ROD: 1000 ft/min
*****Approach*****
IAS: 130 kt
MCS: 90 kt
ROD: 1000 ft/min
*****Landing*****
Vht (IAS): 105 kt
APC: B
Distance: 380 mt