*****AIRCRAFT
“Cessna – C650 Citation”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: In wing
mounted
Tail configuration: Cruciform tail
Landing gear: Tricycle retractable
Wing Span: 11.7 m
Length: 9.8 m
Height: 2.8 m
Power plant: 2 x 4,56 kN Continental J69-T-25 turbojets.
Accommodation: Trainee pilot and instructor side by side.
Notes: Basic and advanced trainer. In service since 1957. Basic
trainer development for the US Air Force. Built in a few versions: T-37A
initial version (534 aircraft were built) replaced by more powerful T-37B in
1959 (449 aircraft were built) optional with wing-tip tanks. Final version
T-37C Tweet or Tweeti Bird for export (269 aircraft were
built). The US Air Force T-37 will be replaced by the PC-9 based T-6A Texan 2.
The T-37 is the standard trainer of several Air Forces. Germany Air Force in
USA, NATO, Greece, Turkey, Pakistan and Korea beeing
the major users.
Alternative names: , CESSNA 318A/B/C, CESSNA
T-37, T-37, T-37
Tweet.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 2.980 kg
VMO - Maximum Operating Speed 400 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: 650
mt
V2 (IAS): 90
kts
*****Climbing*****
-(to 5000 ft)
IAS: 120
kt
ROC: 3300
ft/min
-(to FL150)
IAS: 280
kt
ROC: 2000
ft/min
-(to FL240)
IAS: 280
kt
ROC: 2000
ft/min
-(mach)
mach: 0.60
ROC: 1000
ft/min
*****Cruise*****
TAS: 400
kt
MACh: 0.65
Ceiling: FL390
Range: 800
NM
*****Descent
*****
- (to FL240)
mach: 0.65
ROD: 5000
ft/min
- (to FL100)
IAS: 300
kt
ROD: 5000
ft/min
*****Approach*****
IAS: 250
kt
MCS: nd kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 95 kt
APC: B
Distance: 700
mt