PILATUS PC-21

Aircraft
Name: 
PC-21
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing
Tail: 
Regular tail, mid set
WTC
L
Type Code: 
L1T
Engine: 
Turboprop
Engine Count: 
Single
Position: 
In fuselage
Landing gear: 
Tricycle retractable
Manufacturered as
PILATUS PC-21

PC21

Turboprop trainer aircraft with tandem cockpit. Manufactured by Pilatus Aircraft of Switzerland. First flight in 2002, type certification in 2004. Can be used for various purposes, including simulation, basic, advanced and fighter lead-in training.

Technical Data
Wing span: 
9.11 m
Length: 
11.22 m
Height: 
3.75 m
Powerplant: 

1 x PT6A-68B turboprop (1600 shp)

Engine Model: 
Pratt & Whitney Canada PT6
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
490 m
MTOW: 
4250 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
4250 ft/min
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
3325
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
2125 ft/min
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
370 kts
MACH: 
0.72
Ceiling: 
380
Range: 
700 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
600 m

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