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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