*********10********20********30********40********50********60
*****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