PURPOSE-BUILT FLIGHT TRAINER

AIRCRAFT ARCHITECTURE & SPECS

Engineered from the ground up for high-utilization flight training, rapid student progression, and industry-leading hourly operating economics.

01

CONSTRUCTION & SYSTEMS

Heavy-duty structural components designed to withstand daily student training operations.

AIRFRAME

High-strength aluminum alloy main structure combined with carbon-reinforced composite control surfaces. Built to withstand high-cycle landings, taxi abuse, and flight school wear.

AVIONICS

Modern integrated dual-screen glass cockpit with touchscreen PFD/MFD displays, ADS-B In/Out, synthetic vision, and dual student/instructor radio controls.

ENGINE

Liquid-cooled, fuel-injected 100 HP aircraft engine with dual digital FADEC control. Optimized for Unleaded Auto Fuel (Mogas) or Avgas to dramatically reduce fuel costs.

PROPELLER

3-blade composite fixed-pitch propeller fitted with nickel leading-edge protection against field debris, optimized for climb efficiency and quick solo departures.

02

AIRCRAFT SPECIFICATIONS

Seating Capacity
2 Place (Side-by-Side Dual Control)
Wingspan
28 ft 6 in (8.68 m)
Overall Length
21 ft 4 in (6.50 m)
Height
7 ft 8 in (2.33 m)
Empty Weight
820 lbs (372 kg)
Max Takeoff Weight (MTOW)
1,320 lbs (600 kg)
Useful Load
500 lbs (228 kg)
Usable Fuel
26 US gal (98 L)
03

FLIGHT PERFORMANCE

Max Cruise Speed
120 kts (138 mph)
Stall Speed (Flaps Landing)
40 kts (46 mph)
Rate of Climb
950 ft/min (Sea Level)
Service Ceiling
14,000 ft
Takeoff Roll
580 ft (177 m)
Landing Roll
490 ft (149 m)
Max Range (75% Power)
550 NM (1,018 km)
Fuel Burn Rate
4.8 gal/hr (18.1 L/hr

READY TO EVALUATE THE MOSAIC TRAINER FOR YOUR FLEET?

Speak with our team to arrange a flight demonstration or request detailed dispatch economics.