*****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