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SOCATA TB-31 Omega

From SKYbrary Wiki

TB31
Aircraft
Name TB-31 Omega
Manufacturer SOCATA
Body Narrow
Wing Fixed Wing
Position Low wing
Tail Regular tail, low set
WTC Light
APC A
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 Omega


SOCATA TB-31 Omega

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

Description

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)
Descent
(to FL100)
Descent (FL100
& below)
Approach
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
kg
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
NM

Accidents & Serious Incidents involving TB31

None on SKYbrary