***AIRCRAFT
“Cessna - 560 XL Citation ”***
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing (winglets)
Engine position: Both sides of rear fuselage
Tail configuration: Regular tail, high set
Landing gear: Tricycle retractable
Wing Span: 17.0 m
Length: 15.8 m
Height: 5.2 m
Power plant: 2 x 16,2 kN P&W PW545A turbofans.
Accommodation: Flightcrew of two and various seat
configurations for up to 8 passengers
Notes: Small to mid-size, short range corporate jet. In service since
1998.
CESSNAs new
business development of Citation family with shorter Citation X
fuselage,
unswept supercritical wings of the Ultra and new PW 545A engines.
Alternative names:
CESSNA 560XL
Citation Excel, Citation Excel, Excel
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 8.709 kg
VMO - Maximum Operating Speed 430 KIAS
MMO - Maximum Operating Speed Mach 0.73 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: 1055
mt
V2 (IAS): 115
kts
*****Climbing*****
-(to 5000 ft)
IAS: 145
kt
ROC: 2500
ft/min
-(to FL150)
IAS: 270
kt
ROC: 3000
ft/min
-(to FL240)
IAS: 270
kt
ROC: 2200
ft/min
-(mach)
mach: 0.65
ROC: 1000
ft/min
*****Cruise*****
TAS: 430
kt
MACh: 0.73
data
Ceiling: FL450
Range: 2000
NM
*****Descent
*****
- (to FL240)
mach: 0.70
ROD: 1000
ft/min
- (to FL100)
IAS: 270
kt
ROD: 3000
ft/min
*****Approach*****
IAS: 210
kt
MCS: 180
kt
ROD: 1000
ft/min
*****Landing*****
Vht (IAS): 125
kt
APC: B
Distance: 890
mt