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Light Wing Lightwing AC4

AircraftLight WingLightwing AC4 › Lightwing AC4

The Lightwing AC4 is a model in the Lightwing AC4 family. It is described here as a Two-seat high-wing piston single. EASA type-certificate reference: EASA.A.588.

Light Wing Lightwing AC4 specifications

ManufacturerLight Wing
ModelLightwing AC4
Aircraft typeTwo-seat high-wing piston single
Seats2
Landing gearFixed tricycle
CertificationEASA EASA.A.588

Light Wing Lightwing AC4 weights and capacities

Maximum takeoff weight1,389 lb
Maximum baggage110 lb combined

Light Wing Lightwing AC4 engine and configuration

EngineBRP-Rotax · 915 iSc · 141 hp

Fuel capacity and configuration

FuelThe current AC4 GT configuration lists 90 L flyable fuel.

Light Wing Lightwing AC4 history and development

The Lightwing AC4 is a two-seat high-wing light aircraft certified under EASA.A.588. The current AC4 GT glider-tow configuration uses a Rotax 915 iSc turbo engine rated at 141 hp and a constant-speed propeller. EASA and current manufacturer data identify a 630 kg maximum takeoff mass and 90 L usable/flyable fuel. The AC4 type includes configuration evolution, so this page identifies the current GT/tow figures as configuration-specific.

Light Wing Lightwing AC4 fuel capacity

Standard usable fuel: 23.8 U.S. gallons. The current AC4 GT configuration lists 90 L flyable fuel.

Light Wing Lightwing AC4 model applicability and configuration

Engine and towing equipment vary across AC4 configurations. Verify the exact model/variant and AFM before applying the current 915 iSc/630 kg figures to an earlier AC4.

Light Wing Lightwing AC4 weight and balance

Maximum takeoff weight: 1,389 lb. Maximum combined baggage: 110 lb. The current AC4 GT configuration uses 630 kg (1,389 lb) MTOW, 90 L (23.8 U.S. gal) usable fuel and two 25 kg baggage zones. Aircraft-specific loading data remain controlling. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Lightwing AC4 calculator.

Always verify aircraft applicability. Check the current POH or AFM, equipment list and weight and balance records for the individual aircraft.

Light Wing Lightwing AC4 frequently asked questions

What engine does the Lightwing AC4 use?

The engine listed for this model is BRP-Rotax 915 iSc.

What is the maximum takeoff weight of the Lightwing AC4?

The represented maximum takeoff weight is 1,389 lb.

How much usable fuel does the Lightwing AC4 carry?

The represented standard usable fuel capacity is 23.8 U.S. gallons.

Reference sources

EASA: Type Certificate Data Sheet EASA.A.588 - Lightwing AC4

Light Wing: AC4 GT technical data

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