DR40 – Cadet


Name: DR40 – Cadet

Manufacturer: ROBIN

WTC: L

APC: A

Type: L1P


Technical Information

Wing Span: 8.7 m

Length: 7 m

Height: 2.2 m

Engine: 1 x 112 HP Lycoming O-235-L2A or 1 x 160 HP Lycoming O-320 or 1 x 180 HP Lycoming O-320-A or 1 x 200 HP Lycoming O-360 piston engine with 2 blade propeller. DR-400/125: 1 x 112 HP Lycoming O-240 piston engine with 3 blade propeller.


Performance Data

Take-Off

Maximum Take Off Weight (MTOW): 1100 kg

Distance to Take Off: 350 m

V2 Speed: no data kt

Climb

Climb Speed IAS: 110 kt

Rate Of Climb (ROC): 500 ft/min

Cruise

Cruise Speed TAS: 140 kts

MACH: no data

Max Operating Ceiling: FL 150

Range: 450 NM

Descent

Descent Speed IAS: 140 kt

Rate of Descent (ROD): 500 ft/min

Landing

Landing Speed VAT IAS: 65 kt

Landing APC: A

Distance To Land: 250 m