*****AIRCRAFT
“Gulfstream - G150”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing (winglets)
Engine position: Both sides of rear fuselage
Tail configuration: Regular tail, low set
Landing gear: Tricycle retractable
Wing Span: 16.94 m
Length: 17.3 m
Height: 5.82 m
Power plant: 2x Honeywell TFE731-40AR (19.7kN).
Accommodation: 2 crew and between 6 and 8 passengers.
Notes: The G150 is a
development from the G100. The G150 had it's first
flight
on the 3rd May
2005. The aircraft has received steep approach certification.
Notes: Long range corporate jet. In service since 1980. Improved
development of G-1159 Gulfstream 2 with a revised wing, larger wing span,
stretched fuselage and winglets. Production changed to G-1159C Gulfsream 4 in 1986. Mil. types: C-20A to E.
Alternative names:
Gulfstream 3,
GULFSTREAM G-1159A Gulfstream 3, GULFSTREAM SRA-1, SRA-1.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 11.839 kg
VMO - Maximum Operating Speed 460 KIAS
MMO - Maximum Operating Speed Mach 0.80 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: M
Distance: 1524
mt
V2 (IAS): 115
kts
*****Climbing*****
-(to 5000 ft)
IAS: 220
kt
ROC: 3300
ft/min
-(to FL150)
IAS: 300
kt
ROC: 2800
ft/min
-(to FL240)
IAS: 300
kt
ROC: 2500
ft/min
-(mach)
mach: 0.79
ROC: 2000
ft/min
*****Cruise*****
TAS: 460
kt
MACh: 0.80 data
Ceiling: FL450
Range: 3000
NM
*****Descent
*****
- (to FL240)
mach: 0.80
ROD: 2600
ft/min
- (to FL100)
IAS: 240
kt
ROD: 2400
ft/min
*****Approach*****
IAS: 200
kt
MCS: 180
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 130 kt
APC: C
Distance: 878
mt