Fiction livery made for myself to use but I thought some others may like to use it as whell.

The Epsilon is a low winged cantilever monoplane of all metal construction. It is powered by a Lycoming O-540 flat-six piston engine driving a two-blade propeller, and is fitted with a retractable nosewheel undercarriage. The pilot and instructor are sat in tandem under a sliding Plexiglas canopy, with cockpit layout designed to aid transition to the Dassault/Dornier Alpha Jet to which French students graduate after completing the Epsilon part of their training syllabus.

  
TB 31 Oméga
The first prototype was modified into a testbed for the Turbomeca TP 319 Arrius turboprop engine, flying in this form on 9 November 1985. The testbed was then modified into a dedicated turboprop trainer, the TB 31 Oméga, powered by a 360 kW (483 shp) Arrius 1A2 and fitted with ejection seats, returning to flight on 30 April 1989. While it was offered for the United States Air Force/United States Navy Joint Primary Aircraft Training System competition to replace the Beechcraft T-34 Mentor and Cessna T-37 Tweet, it was rejected, with no sales resulting.

General characteristics

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)
Aspect ratio: 7
Airfoil: root: RA 1643 (16%) ; tip: RA 1243 (12%)[14]
Empty weight: 932 kg (2,055 lb)
Max takeoff weight: 1,250 kg (2,756 lb)
Powerplant: × Lycoming AEIO-540-L1B5D 6-cylinder air-cooled horizontally-opposed piston engine, 220 kW (300 hp)
Propellers: 2-bladed constant-speed propeller
Performance

Maximum speed: 378 km/h (235 mph, 204 kn)
Cruise speed: 358 km/h (222 mph, 193 kn)
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)
Rate of climb: 9.4 m/s (1,850 ft/min)