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*****AIRCRAFT “Pilatus – PC9”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position: Low wing

Engine position: Nose mounted

Tail configuration: Regular tail, mid set

Landing gear: Tricycle retractable

Wing Span: 10.1 m

Length: 10.7 m

Height: 3.3 m

Power plant: PC-9: 1 x 1.150 SHP P&W PT6A-62 turbo-prop with 4 blade propeller.

T-6A: 1 x 1.708 SHP P&W PT6A-68 turbo-prop with 4 blade propeller.

PC-9: 1 x 1.150 SHP P&W PT6A-62 turbo-prop with 4 blade propeller.

T-6A: 1 x 1.708 SHP P&W PT6A-68 turbo-prop with 4 blade propeller.

Accommodation: Pilot and trainee in tandem position.

Notes: Advanced trainer. In service since 1985 (T-6A since 2000). More powerful development of PILATUS PC-7 turbo trainer with new cockpit and tail.

Major operators in Europe, Asia and Africa. In Germany operating 10 PC-8Bs as target towings. Further development by RAYTHEON, United States, T-6A Texan II for US Air Force and US Navy (700 aircraft). Export customers of T-6A are Canada (24 aircraft designated CT-156 Harvard II) and Greece (45 aircraft).
Alternative names:
CT-156 Harvard 2, Harvard 2, PC-9, PD-373 Beech, PILATUS PC-9, RAYTHEON PC-9, 3000, RAYTHEON T-6, CT-156, Texan 2, Harvard 2, T-6 Texan 2, Texan 2, PC-9/T-6A

 

*****Total Flight Simulator aircraft weight with full fuel*****  

Max weight: 3270 kg,  0000 lbs

VMO - Maximum Operating Speed 300 KIAS

Max speed:556 km/h, Mach 0,  0 knots

Range:0 km, 0 miles

Max. endurance, ISA at 0 KIAS, Including 0 nm reserve

 

*****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:         250 mt

V2 (IAS):         90 kts

 

*****Climbing*****

-(to 5000 ft)

 

IAS:                 140 kt

ROC:               4100 ft/min

-(to FL150)

IAS:                 150 kt

ROC:               2500 ft/min

-(to FL240)

IAS:                 150 kt

ROC:               1700 ft/min

-(mach)

mach:              0.00

ROC:               0000 ft/min

 

*****Cruise*****

 

TAS:                300 kt

MACh:             no data

Ceiling:            FL380

Range:            860 NM

 

*****Descent *****

- (to FL240)

mach:              0.00

ROD:               0000 ft/min

- (to FL100)

IAS:                 250 kt

ROD:               3000 ft/min

 

*****Approach*****

IAS:                 200 kt

MCS:               90 kt

ROD:               1500 ft/min

 

*****Landing*****

Vht (IAS):        80 kt

APC:                A

Distance:         350 mt