M101

MYASISHCHEV M-101 Expedition

Aircraft
Name
M-101 Expedition
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, mid set
WTC
L
Type Code
L1T
Engine
Turboprop
Engine Count
Single
Position
Nose mounted
Landing gear
Tricycle retractable
Manufacturered as
MYASISHCHEV Gzhel
MYASISHCHEV M-101 Expedition
MYASISHCHEV Expedition
MYASISHCHEV M-101 Gzhel

M101

The Myasishchev M-101T is a Russian business class aircraft, designed by Myasishchev and built by Sokol.

Technical Data
Wing span (metric)
13.00 m
Length (metric)
9.98 m
Height (metric)
3.72 m
Powerplant

1 x Walter M601F turboprop, 567 kW

Engine Model(s)
Walter M601
Indicative Performance Data
Take-Off
V2
n/a
Distance
380 m
MTOW
3200 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
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
232 kts
MACH
n/a
Ceiling
260
Range
755 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
370 m

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