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***AIRCRAFT
“Diamond – DA40 ultralight”***
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Nose mounted
Tail configuration: T-tail
Landing gear: Tricycle fixed
Wing Span: 11.94 m
Length: 8.01 m
Height: 1.97 m
Power plant: 1x Fixed
pitch Textron Lycoming O-360-A4M (180HP) F or 1x constants speed propellor Textron Lycoming IO-360 M1A or 1x constant speed
FADEC controlled Thielert "Centurion" 135
hp (101 kW) diesel engine.
Accommodation: 1 pilot
and 3 passengers.
Notes: The prototype first flew on the 5th November 1997.
It received
certification in October 2000.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 1.150 kg
VMO - Maximum Operating Speed 150 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: 345
mt
V2 (IAS): 73
kts
*****Climbing*****
-(to 5000 ft)
IAS: 130
kt
ROC: 1100
ft/min
-(to FL150)
IAS: nd kt
ROC: nd ft/min
-(to FL240)
IAS: nd kt
ROC: nd ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 150
kt
MACh: no data
Ceiling: FL140
Range: 720
NM
*****Descent
*****
- (to FL240)
mach: 0.00
ROD: 0000
ft/min
- (to FL100)
IAS: 150
kt
ROD: 800
ft/min
*****Approach*****
IAS: 120
kt
MCS: 65
kt
ROD: 550
ft/min
*****Landing*****
Vht
(IAS): 80 kt
APC: A
Distance: 700
mt