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KHRUNICHEV T-411 Aist

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T411
Aircraft
Name T-411 Aist
Manufacturer KHRUNICHEV
Body Narrow
Wing Fixed Wing
Position High 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:

AEROPROGRESS T-411 Aist-2
AEROPROGRESS Aist-2
KHRUNICHEV Wolverine
KHRUNICHEV Aist
KHRUNICHEV T-411 Aist
KHRUNICHEV T-411 Wolverine


KHRUNICHEV T-411 Aist

KHRUNICHEV T-411 Aist KHRUNICHEV T-411 Aist 3D

Description

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 13.02 m42.717 ft
Length 9.50 m31.168 ft
Height 2.60 m8.53 ft
Powerplant 1 x 360HP Vedeneyev M14P radial piston engine.
Engine model Vedeneyev M14P

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 110 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 210 m ROC 1500 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 330 m
MTOW 16001,600 kg
1.6 tonnes
kg
Ceiling FL100 ROD ft/min APC A
WTC L Range 650650 nm
1,203,800 m
1,203.8 km
3,949,475.069 ft
NM

Accidents & Serious Incidents involving T411

None on SKYbrary