Sonerai II

Piston • single engine • Mid Wing • Fixed gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

MOSAIC Eligibile Sport Pilot-flyable
122
KTAS
Cruise Speed
2
Occupants
300
nm
Max Range
370
lbs
Wet Payload

Estimated Ownership Costs

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About the Sonerai II

Overview

The Monnett Sonerai II is a high-performance, mid-wing, tandem two-seat experimental aircraft originally derived from a Formula V racer. Designed by John Monnett, it is famous for its use of modified Volkswagen automotive engines, offering a high-speed, sporty flying experience on a budget. Its wings are designed to fold back against the fuselage, allowing for easy towing and storage in a standard garage.

Key Features for GA Buyers

  • Folding Wings: Significantly reduces ownership costs by allowing garage storage and eliminating hangar fees.
  • Operational Economy: Consumes only 4-5 gallons of fuel per hour using a VW-based engine, making it one of the most affordable cross-country cruisers.
  • Sporty Handling: Exceptional roll rates and responsiveness; stressed for limited aerobatics when flown solo.
  • Versatility: Available in mid-wing or low-wing (II-L) configurations, and as a taildragger or tricycle gear (II-LT).

Trade-offs

  • Payload Constraints: With two adults and fuel, the aircraft often nears its gross weight limits; baggage space is very limited.
  • Cockpit Comfort: The tandem cockpit is narrow (approx. 23 inches), which may be cramped for larger pilots or long trips.
  • Maintenance: As a plans-built experimental aircraft, build quality varies significantly between units, requiring thorough pre-buy inspections of the 4130 steel frame and fabric covering.

Technical Specifications

Dimensions

Wingspan
18.67 ft
Length
18.83 ft
Height
5.0 ft
Parking area (ft2)
683.21 ft2

Weights

Max Takeoff Weight
1,150 lbs
Max Landing Weight
1,150 lbs
Useful Load
430 lbs
Fuel Capacity
10 gal

Performance

Cruise Speed
122 KTAS
Never-Exceed (Vne)
174 KIAS
Max Structural Cruise (Vno)
122 KIAS
Approach Speed
50 KIAS
Stall, Clean (Vs1)
38 KIAS
Range
300 NM
Service Ceiling
13,000 ft
Rate of Climb
500 fpm
Takeoff over 50 ft obstacle
900 ft
Landing ground roll
500 ft

Engine

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