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*****AIRCRAFT “Pilatus – PC6T”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

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

Wing position: High wing (wing struts)

Engine position: Nose mounted

Tail configuration: Regular tail, high set

Landing gear: Tricycle fixed

Wing Span: 15.9 m

Length: 10.9 m

Height: 3.2 m

Power plant: 1 x 550 SHP P&W PT6A-27 turboprop with 3 blade propeller.

Accommodation: One pilot and up to11 passengers.

Notes: STOL utility transport aircraft. In service since 1965. Turboprop development of PC-6 Porter (ICA Designator: PC6P).First flight in 1959. Replaced by PC-6/B2-H2 in 1970. Current version PC-6/B2-H4 with increased max. take-off weight, revised wingtips, strengthened airframe structure and improved gear. Also used by military as troop-transporter and ambulance aircraft. US Army type UV-20 Chiricahuas. Licence production by FAIRCHILD, United States, as PC-6 Heli-Porter and UA-23 Peacemaker.
Alternative names:
FAIRCHILD (1) PC-6 Heli-Porter, Heli-Porter, PC-6 Heli-Porter, PC-6A/B/C Turbo-Porter
PILATUS PC-6A/B/C Turbo-Porter, PILATUS UV-20 Chiricahua, Turbo-Porter
UV-20 Chiricahua
.

 

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

Max weight: 2770 kg,  0000 lbs

VMO - Maximum Operating Speed 130 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:         100 mt

V2 (IAS):         60 kts

 

*****Climbing*****

-(to 5000 ft)

 

IAS:                 90 kt

ROC:               1200 ft/min

-(to FL150)

IAS:                 100 kt

ROC:               800 ft/min

-(to FL240)

IAS:                 100 kt

ROC:               700 ft/min

-(mach)

mach:              0.00

ROC:               0000 ft/min

 

*****Cruise*****

 

TAS:                130 kt

MACh:             no data

Ceiling:            FL250

Range:            850 NM

 

*****Descent *****

- (to FL240)

mach:              0.00

ROD:               0000 ft/min

- (to FL100)

IAS:                 120 kt

ROD:               700 ft/min

 

*****Approach*****

IAS:                 110 kt

MCS:               65 kt

ROD:               500 ft/min

 

*****Landing*****

Vht (IAS):        60 kt

APC:                A

Distance:         100 mt