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SOCATA TB-31 Omega

From SKYbrary Wiki

Name TB-31 Omega
Manufacturer SOCATA
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Regular tail, low set
WTC Light
Type code L1T
Engine Turboprop
Engine count Single
Position Nose mounted
Landing gear Tricycle retractable
Mass group 1

Manufacturered as:

SOCATA TB-31 Omega

SOCATA TB-31 Omega

SOCATA TB-31 Omega SOCATA TB-31 Omega 3D


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 7.92 m25.984 ft
Length 7.59 m24.902 ft
Height 2.66 m8.727 ft
Powerplant 1 x Turboméca TP 319 1A2.
Engine model Turboméca Arrius

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 250 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 650 m ROC 2000 ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 600 m
MTOW 15001,500 kg
1.5 tonnes
Ceiling FL300 ROD ft/min APC A
WTC L Range 700700 nm
1,296,400 m
1,296.4 km
4,253,280.843 ft

Accidents & Serious Incidents involving TB31

None on SKYbrary