TB31

SOCATA TB-31 Omega

Aircraft
Name
TB-31 Omega
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, low set
WTC
L
APC
A
Type Code
L1T
Engine
Turboprop
Engine Count
Single
Position
Nose mounted
Landing gear
Tricycle retractable
Manufacturered as
SOCATA Omega
SOCATA TB-31 Omega

TB31

Sole prototype of this plane, an improved variant of the Socata TB-30 Epsilon with a new avionics and engineering. First flown in 1985, but no further production.

Technical Data
Wing span (metric)
7.92 m
Length (metric)
7.59 m
Height (metric)
2.66 m
Powerplant

1 x Turboméca TP 319 1A2.

Engine Model(s)
Turboméca Arrius
Indicative Performance Data
Take-Off
V2
n/a
Distance
650 m
MTOW
1500 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
2000 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
250 kts
MACH
n/a
Ceiling
300
Range
700 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
600 m

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