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ROBIN R-1180 Aiglon

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R100
Aircraft
Name R-1180 Aiglon
Manufacturer ROBIN
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Regular tail, mid set
WTC Light
APC A
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

Description

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)
Descent
(to FL100)
Descent (FL100
& below)
Approach
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
kg
Ceiling FL135 ROD ft/min APC A
WTC L Range NM

Accidents & Serious Incidents involving R100

None on SKYbrary