****AIRCRAFT “Raytheon - BAe125-1000”****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Both sides of rear fuselage
Tail configuration: Cruciform tail
Landing gear: Tricycle retractable
Wing Span: 15.7 m
Length: 16.4 m
Height: 5.2 m
Power plant: 2 x 23.13kN PWC PW 305 turbofans.
Accommodation: Flightcrew of two and typical 8 passengers in corporate, up to 15 in
high density configuration.
Notes: Long range corporate jet. In service since 1991. Largest member
of HS/BAe-125 family. Stretched fuselage development of Hawker 800 with seven
cabin windows per side, optimized for long range intercontinental operation.
The BAe 125-1000 aircraft has been taken over and is
partly built by RAYTHEON, USA. Production ceased in 1997 after 52 aircraft were
built. Will be replaced by Hawker 4000 Horizon.
Alternative names:
British Aerospace BAe-125-1000, RAYTHEON Hawker 1000, Hawker 1000.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 14.060 kg
VMO - Maximum Operating Speed 450 KIAS
MMO - Maximum Operating Speed Mach 0.76 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: 1900
mt
V2 (IAS): 125
kts
*****Climbing*****
-(to 5000 ft)
IAS: 155
kt
ROC: 3500
ft/min
-(to FL150)
IAS: 290
kt
ROC: 2500
ft/min
-(to FL240)
IAS: 290
kt
ROC: 2000
ft/min
-(mach)
mach: 0.72
ROC: 1500
ft/min
*****Cruise*****
TAS: 450
kt
MACh: 0.76 data
Ceiling: FL430
Range: 3100
NM
*****Descent
*****
- (to FL240)
mach: 0.72
ROD: 1000
ft/min
- (to FL100)
IAS: 290
kt
ROD: 4000
ft/min
*****Approach*****
IAS: 250
kt
MCS: 220
kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 132 kt
APC: C
Distance: 889
mt