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*****AIRCRAFT “AFG - Pilatus PC12”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

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

Wing position: Low wing (winglets)

Engine position: Nose mounted

Tail configuration: T-tail

Landing gear: Tricycle retractable

Wing Span: 16.2 m

Length: 14.4 m

Height: 4.3 m

Power plant: 1 x 1.200 SHP P&W PT6A-67B turboprop with

4 blade propeller.

Accommodation: One or two pilots and typical 9 passengers (6 in executive- , 4 in combi version).

Notes: Light utility and business transport. In service since 1994. Latest single engined powered Pilatus product. PC-12 has a King air sized cabin with EFIS cockpit. Also used as combi passenger / freighter. New smaller winglets since 1998.
Alternative names:
PC-12,Eagle
PILATUS PC-12,Eagle
.

 

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

000,000 lbs - 4.500 kg

VMO - Maximum Operating Speed 270 KIAS

MMO - Maximum Operating Speed Mach   .00 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:         600 mt

V2 (IAS):         110 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 130 kt

ROC:               1700 ft/min

-(to FL150)

IAS:                 130 kt

ROC:               1000 ft/min

-(to FL240)

IAS:                 130 kt

ROC:               700 ft/min

-(mach)

mach:              N.D.

ROC:               N.D. ft/min

 

*****Cruise*****

TAS:                260 kt

MACh:             no data

Ceiling:            FL300

Range:            2000 NM

 

*****Descent *****

- (to FL240)

mach:              N.D.

ROD:               N.D. ft/min

- (to FL100)

IAS:                 210 kt

ROD:               1500 ft/min

 

*****Approach*****

IAS:                 180 kt

MCS:               140 kt

ROD:               1500 ft/min

 

*****Landing*****

Vht (IAS):        85 kt

APC:                A

Distance:         550 mt