*****AIRCRAFT
“Beech – PD 373”*****
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:
Length:
Height:
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.
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
In
by RAYTHEON,
US Navy (700 aircraft). Export
customers of T-6A are
(24 aircraft designated CT-156 Harvard II) and
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*****
VMO -
Maximum Operating Speed 300 KIAS
MMO -
Maximum Operating Speed Mach
nd 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: 250 mt
V2
(IAS): 90 kts
*****Climbing*****
-(to
IAS: 145 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: nd
ROC: nd ft/min
*****Cruise*****
TAS: 300 kt
MACh: nd
Ceiling: FL380
Range: 860 NM
*****Descent *****
- (to
FL240)
mach: nd
ROD: nd 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