T411
KHRUNICHEV T-411 Aist
KHRUNICHEV T-411 Aist
Aircraft
Name
T-411 Aist
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High wing
Tail
Regular tail, mid set
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Position
Nose mounted
Landing gear
Tricycle fixed
Manufactured as
KHRUNICHEV Wolverine
KHRUNICHEV Aist
KHRUNICHEV T-411 Aist
KHRUNICHEV T-411 Wolverine
AEROPROGRESS T-411 Aist-2
AEROPROGRESS Aist-2
T411
The Khrunichev T-411 Aist is a Russian light utility monoplane designed by the Khrunichev design bureau. Marketed in the United States as the Aeroprogress T-411 Wolverine powered by a Continental TSIO-550-B.
Technical Data
Wing span (metric)
13.02 m
Length (metric)
9.50 m
Height (metric)
2.60 m
Powerplant
1 x 360HP Vedeneyev M14P radial piston engine.
Engine Model(s)
Vedeneyev M14P
Indicative Performance Data
Take-Off
V2
n/a
Distance
210 m
MTOW
1600 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
1500 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
110 kts
MACH
n/a
Ceiling
100
Range
650 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
330 m
