RALL – Commodore


Name: RALL – Commodore

Manufacturer: SOCATA

WTC: L

APC: A

Type: L1P


Technical Information

Wing Span: 9.7 m

Length: 7.2 m

Height: 2.8 m

Engine: 880B: 1 x 100 HP Continental O-220-A piston engine with 2 blade propeller. 890: 1 x 150 HP Lycoming O-320 piston engine with 2 blade propeller. 894: 1 x 235 HP Lycoming O-540-B4BT piston engine with 3 blade propeller.


Performance Data

Take-Off

Maximum Take Off Weight (MTOW): 1050 kg

Distance to Take Off: 300 m

V2 Speed: 65 kt

Climb

Climb Speed IAS: 95 kt

Rate Of Climb (ROC): 100 ft/min

Cruise

Cruise Speed TAS: 120 kts

MACH: no data

Max Operating Ceiling: FL 110

Range: 700 NM

Descent

Descent Speed IAS: 110 kt

Rate of Descent (ROD): 500 ft/min

Landing

Landing Speed VAT IAS: 60 kt

Landing APC: A

Distance To Land: 200 m