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ROBIN R-1180 Aiglon

From SKYbrary Wiki

Name R-1180 Aiglon
Manufacturer ROBIN
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Regular tail, mid set
WTC Light
Type code L1P
Engine Piston
Engine count Single
Position Nose mounted
Landing gear Tricycle fixed
Mass group 1

Manufacturered as:

ROBIN R-1180 Aiglon
ROBIN Aiglon

ROBIN R-1180 Aiglon

ROBIN R-1180 Aiglon ROBIN R-1180 Aiglon 3D


The Robin R.1180 Aiglon is a French four-seat touring and training monoplane designed and built by Avions Robin.

Technical Data

Wing span 9.08 m29.79 ft
Length 7.26 m23.819 ft
Height 2.38 m7.808 ft
Powerplant 1 x Lycoming O-360-A3AD flat-four piston engine, 134 kW (180 hp)
Engine model Lycoming O-360

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 165 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 470 m ROC 850 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 460 m
MTOW 11001,100 kg
1.1 tonnes
Ceiling FL135 ROD ft/min APC A
WTC L Range NM

Accidents & Serious Incidents involving R100

None on SKYbrary