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FFA AS-202 Bravo

From SKYbrary Wiki

Name AS-202 Bravo
Manufacturer FFA
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Regular tail, low set
WTC Light
Type code L1P
Engine Piston
Engine count Single
Position Nose mounted
Landing gear Tricycle retractable
Mass group 1

Manufacturered as:

FFA Wren
FFA AS-202-18 Wren
FFA Bravo
FFA AS-202-15 Bravo
FFA AS-202-18 Bravo
FFA AS-202-26 Bravo

FFA AS-202 Bravo

FFA AS-202 Bravo FFA AS-202 Bravo 3D


The AS/SA 202 Bravo is a two to three-seat civil light aircraft jointly designed and manufactured by the Swiss company Flug- und Fahrzeugwerke Altenrhein (FFA) and the Italian company Savoia-Marchetti. The aircraft was designated the AS 202 in Switzerland, and the SA 202 in Italy.

Technical Data

Wing span 9.75 m31.988 ft <br />
Length 7.50 m24.606 ft <br />
Height 2.81 m9.219 ft <br />
Powerplant 1 x Lycoming O-235-C2A 4-cylinder air-cooled horizontally-opposed piston engine, 86 kW (115 hp)
Engine model Lycoming O-235

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 138 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 235 m ROC 1000 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 210 m
MTOW 12001,200 kg <br />1.2 tonnes <br /> kg Ceiling FL170 ROD ft/min APC
WTC L Range 480480 nm <br />888,960 m <br />888.96 km <br />2,916,535.435 ft <br /> NM

Accidents & Serious Incidents involving AS02

None on SKYbrary