AS02
FFA AS-202 Bravo
FFA AS-202 Bravo
Aircraft
Name
AS-202 Bravo
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, low set
WTC
L
Type Code
L1P
Engine
Piston
Engine Count
Single
Position
Nose mounted
Landing gear
Tricycle retractable
Manufactured as
FFA AS-202-15 Bravo
FFA AS-202-18 Bravo
FFA AS-202-26 Bravo
FFA Wren
FFA AS-202-18 Wren
FFA Bravo
AS02
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 (metric)
9.75 m
Length (metric)
7.50 m
Height (metric)
2.81 m
Powerplant
1 x Lycoming O-235-C2A 4-cylinder air-cooled horizontally-opposed piston engine, 86 kW (115 hp)
Engine Model(s)
Lycoming O-235
Indicative Performance Data
Take-Off
V2
n/a
Distance
235 m
MTOW
1200 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
1000 ft/min
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
138 kts
MACH
n/a
Ceiling
170
Range
480 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
210 m
