SOCATA TB-30 Epsilon

Basic Trainer Aircraft

France | 1983

"Produced from 1979 until 1989, the TB-30 was eventually taken on by the air services of France, Portugal, Togo, and Senegal."

Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the SOCATA TB-30 Basic Trainer Aircraft.

1 x Lycoming AEIO-540-L 1B5D 6-cylinder, air-cooled piston engine developing 300 horsepower driving two-bladed propeller unit at the nose.
Propulsion

236 mph
380 kph | 205 kts
Max Speed

22,999 ft
7,010 m | 4 miles
Service Ceiling

808 miles
1,300 km | 702 nm
Operational Range

1,850 ft/min
564 m/min
Rate-of-Climb

Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the SOCATA TB-30 Basic Trainer Aircraft.

2
(MANNED)
Crew

24.9 ft
7.60 m
O/A Length

26.0 ft
(7.92 m)
O/A Width

8.7 ft
(2.65 m)
O/A Height

2,061 lb
(935 kg)
Empty Weight

2,756 lb
(1,250 kg)
MTOW

Variants
Notable series variants as part of the SOCATA TB-30 Epsilon family line.

TB-30 "Epsilon" - Base series designation.

TB-31 "Omega" - Proposed variant featuring turboprop powerplant; based in the TB-30 platform; single example completed.

Operators
Global customers who have evaluated and/or operated the SOCATA TB-30 Epsilon. Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 56 Units
Contractor(s): SOCATA (Aerospatiale) - France

[ France; Portugal; Senegal; Togo ]

Going Further...
The SOCATA TB-30 Epsilon Basic Trainer Aircraft appears in the following collections:

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