*****AIRCRAFT
“Cessna – C525 Citation”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: (Both sides
of rear fuselage
Tail configuration: T-tail
Landing gear: Tricycle retractable
Wing Span: 14.3 m
Length: 13.0 m
Height: 4.2 m
Power plant: 2 x 8.45 kN Williams R-R FJ44-1A turbofans.
Accommodation: One or two pilots and 5 passengers.
Notes: Small corporate jet. In service since 1993 (CJ1 since 2000).
Developed as replacement of the CESSNA 500 Citation 1 with shorter fuselage,
super critical wings and T-tail. Combines jet speed with very good field
performance. To be replaced by CJ1 after 2000.
Alternative names:
CESSNA 525
CitationJet, Citation CJ1, Citation CJ1,
CitationJet, CJ1
CESSNA 525 CitationJet.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 4.717 kg
VMO - Maximum Operating Speed 370 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: 939
mt
V2 (IAS): 115
kts
*****Climbing*****
-(to 5000 ft)
IAS: 145
kt
ROC: 3000
ft/min
-(to FL150)
IAS: 230
kt
ROC: 2500
ft/min
-(to FL240)
IAS: 230
kt
ROC: 1800
ft/min
-(mach)
mach: 0.62
ROC: 1500
ft/min
*****Cruise*****
TAS: 370
kt
MACh: 0.63
Ceiling: FL410
Range: 1485
NM
*****Descent
*****
- (to FL240)
mach: 0.66
ROD: 1000
ft/min
- (to FL100)
IAS: 250
kt
ROD: 2000
ft/min
*****Approach*****
IAS: 220
kt
MCS: 130
kt
ROD: 1500 ft/min
*****Landing*****
Vht
(IAS): 110 kt
APC: B
Distance: 838
mt