Top
about
element
General Info

Daher-Socata
Socata TB 30 Epsilon


Socata TB 30 Epsilon
Role Light military trainer aircraft
Manufacturer SOCATA (Aérospatiale)
First flight 22 December 1979
Introduction 1983
Status Active service
Primary users French Air Force (historical)
Portuguese Air Force
Togolese Air Force
Senegalese Air Force
Produced 1979-1989
.
History SOCATA (later EADS Socata and DAHER-SOCATA)
Socata TB 30 Epsilon

In 1978, the French Air Force (Armée de l'Air) published a requirement for a new basic trainer aircraft to partially replace the Fouga Magister in the early parts of the syllabus for pilot training. The new aircraft was expected to have tandem seating, be powered by a 224 kW (300 hp) piston engine and have a three-hour endurance. Similar designs were proposed by the SOCATA subsidiary of Aérospatiale (based on their TB 10 Tobago light aircraft) and by GEPAL (the GEPAL Mk II). The SOCATA proposal, the TB 30B, was chosen in February 1979.

The Socata TB 30 Epsilon is a light military trainer aircraft produced by SOCATA (then part of Aérospatiale). It is a tandem two-seater with a metal airframe. The first prototype flew on 22 December 1979..

Variants

  • TB 30 Epsilon: Military trainer aircraft
  • TB 31 Oméga: Proposed turboprop powered version of the TB 30 Epsilon. Only one aircraft built

Operators

Current

A Portuguese Air Force TB 30
Portugal
Senegal
Togo

Former operators

France
Mystère IVN
TB 31 Oméga
.

0

Km

Ceiling

0

Km

MAX RANGE

0

Km/H

Aircraft Speed

0

Max Crew

element
element
Avions Marcel Dassault-Breguet Aviation

Dassault Aviation SA Avions
SOCATA (later EADS Socata and DAHER-SOCATA) Socata TB 30 Epsilon

1

General Info

    • Crew: 2
    • Length: 7.59 m (24 ft 11 in)
    • Wingspan: 7.92 m (26 ft 0 in)
    • Height: 2.66 m (8 ft 9 in)
    • Wing area: 9 m2 (97 sq ft)

Powerplant

  • Empty weight: 932 kg 
  • Max takeoff weight: 1,250 kg 
  • Powerplant: × Lycoming AEIO-540-L1B5D 6-cylinder air-cooled horizontally-opposed piston engine, 220 kW (300 hp)
  • Propellers: 2-bladed constant-speed propeller
plane
3

Specifications

  • Maximum speed: 378 km/h 
  • Cruise speed: 358 km/h 
  • Stall speed: 115 km/h (71 mph, 62 kn)
  • Never exceed speed: 520 km/h (320 mph, 280 kn)
  • Range: 1,300 km (810 mi, 700 nmi)
  • Service ceiling: 7,010 m (23,000 ft)
4

ArmanentUp to 480 kg (1,100 lbs) on four underwing hardpoints (export versions)

     
Special Links Avions Marcel Dassault-Breguet Aviation

Links to Youtube & Others

The Armée de l'Air placed an initial order for 30 Epsilons in 1981, with further contracts following with a total of 150 ordered.[7] First deliveries started in 1983, with the first training courses based on the Epsilon starting in September 1984.

 DAHER-SOCATA) Socata TB 30 Epsilon

Export orders were received from Togo for three armed Epsilons in 1984,

interior

Youtube Link

Export orders were received from Togo for three armed Epsilons in 1984,

interior
Aircrafttotal : EADS Socata and DAHER-SOCATA

Read more in Avions Marcel Dassault-Breguet Aviation

.
brand
brand
brand
brand
brand