*****AIRCRAFT
“Gulfstream – G280”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing (winglets)
Engine position: Both sides of rear fuselage
Tail configuration: T-tail
Landing gear: Tricycle retractable
Wing Span: 19.2 m
Length: 20.37 m
Height: 6.5 m
Power plant: 2x 2x Honeywell HTF7250G (7445lb /33kN).
Accommodation: 2 pilots and between 8-10 passengers.
Notes: Initially know as the
G250, but was renamed to the G280, as it is a more
"amenable
number sequence in certain cultures" according to Gulfstream senior VP
marketing & sales Larry Flynn.
The aircraft
had it's first flight on 11. December 2009 and
received full certification
from Israel
and United States on 4. September 2012.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 17.962 kg
VMO - Maximum Operating Speed 472 KIAS
MMO - Maximum Operating Speed Mach 0.83 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: 1448
mt
V2 (IAS): 135
kts
*****Climbing*****
-(to 5000 ft)
IAS: 230
kt
ROC: 5500
ft/min
-(to FL150)
IAS: 280
kt
ROC: 3500
ft/min
-(to FL240)
IAS: 280
kt
ROC: 2500
ft/min
-(mach)
mach: 0.83
ROC: 3000
ft/min
*****Cruise*****
TAS: 472
kt
MACh: 0.83 data
Ceiling: FL450
Range: 3600
NM
*****Descent
*****
- (to FL240)
mach: 0.83
ROD: 2800
ft/min
- (to FL100)
IAS: 250
kt
ROD: 2100
ft/min
*****Approach*****
IAS: 230
kt
MCS: 190
kt
ROD: 1800
ft/min
*****Landing*****
Vht
(IAS): 134 kt
APC: C
Distance: 950
mt