Viking V-42

Piston twin engine • High Wing • Fixed gear

Range Visualization

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

Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lbs lbs / pax

Fuel on board

Extra 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.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

Endorsements & ratings:
  • Multi-Engine
139
KTAS
Cruise Speed
4
Occupants
869
nm
Max Range
620
lbs
Wet Payload
• Prototype
• Experimental Amateur-built, no type certificate

Estimated Ownership Costs

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About the Viking V-42

Overview

The Viking V-42 is a four-seat, high-wing experimental amateur-built twin from Viking Aircraft of Edgewater, Florida, the company behind the Honda-derived Viking auto-conversion engines. It pairs an all-aluminum, matched-hole, pull-rivet airframe with two 150-hp Viking 150 engines on fixed tricycle gear. Jan Eggenfellner unveiled the prototype at Sun ‘n Fun in April 2026.

As of mid-2026 the V-42 is a single prototype rather than a shipping product. Kits are planned but not yet for sale, and the first flight was targeted for AirVenture Oshkosh in July 2026. Every performance figure below is a manufacturer forecast rather than a flight-tested number, and should be read that way until the aircraft has flown and a kit is offered.

Key Features for GA Buyers

  • Light twin on automotive-derived power. Two liquid-cooled Viking 150 engines, each based on a 1.8-liter Honda HR-V, drive the design toward a forecast 160 mph (about 139 KTAS) cruise on 80 gallons of fuel.
  • All-aluminum, simple build. Matched-hole construction with pull-rivets is aimed at fast, repeatable assembly and straightforward inspection and repair.
  • Fixed gear, four seats. Fixed tricycle gear and a forecast 3,100-lb gross weight target an 1,100-lb useful load with 200 lb of baggage.
  • Multi-engine redundancy in the experimental class. A second engine is unusual at this weight and price in a homebuilt market where most kits are singles.

Trade-offs

  • Not yet flying, no kits for sale. This is a forecast aircraft. There is no flight data, no published price, and no delivered kit; the performance figures are manufacturer design targets the builder has still to demonstrate.
  • Multi-engine experimental ownership. Two engines mean two of everything to maintain, a multi-engine rating and currency to hold, and single-engine handling that a clean-sheet light twin has to prove before its safety case is settled.
  • Auto-conversion powerplant. The Viking 150 is an adapted automotive engine managed by its automotive engine-control unit, not a certified aircraft engine with a published TBO. It runs on auto fuel and carries the support and resale profile of the experimental world.
  • Forecast ground rolls. Viking forecasts an 800-ft takeoff roll and a 600-ft landing roll. These are unobstructed ground-roll targets, not over-50-ft obstacle distances, and remain unverified.

See Also

Technical Specifications

Figures below are manufacturer projections for an aircraft that has not yet completed flight testing.

Dimensions & Weights

Wingspan 38.125 ft
Height
Source: manufacturer figure 11.875 ft
Length
Source: manufacturer figure 30.0 ft
Parking area (ft2)
1684.38 ft2
Max Takeoff Weight
Source: manufacturer figure 3,100 lbs
Useful Load
Source: manufacturer figure 1,100 lbs
Fuel Capacity
Source: manufacturer figure 80 gal

Performance

Cruise Speed
Source: manufacturer figure 139 KTAS
Approach Speed
Source: manufacturer figure 65 KIAS
Stall, Clean (Vs1)
Source: manufacturer figure 50 KIAS
Range
Source: manufacturer figure 869 NM
Rate of Climb
1200 fpm

Engines

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