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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