Aerospool Club

The Aerospool WT9 Dynamic Club is a model in the WT9 Dynamic family. It is described here as a Two-seat composite low-wing piston single. EASA type-certificate reference: EASA.A.644.

The WT9 Dynamic Club is the fixed-gear member of the EASA-certified WT9 Dynamic LSA family. EASA.A.644 identifies the Rotax 912 ULS2 certification configuration, while Aerospool production material documents fixed-gear Club and related WT9 versions with different engine and tank options. Current-generation WT9 data support a 600 kg class maximum takeoff mass. Fuel capacity varies with tank installation, so the page preserves the large-capacity 119 L usable figure as configuration-specific rather than universal.

Standard usable fuel: 31.4 U.S. gallons. Current WT9 LSA operating data show up to 119 L usable in the applicable large-capacity fuel configuration; tank capacity is configuration-dependent.

WT9 production spans several generations and multiple engine, propeller and tank options. Confirm whether the aircraft is the EASA-certified Club/LSA configuration represented here and use its approved POH for exact fuel and loading values.

Maximum takeoff weight: 1,323 lb. Use the POH applicable to the specific WT9 Club configuration. Use 600 kg (1,323 lb) only for the approved configuration that carries that maximum mass. The 119 L usable figure belongs to the applicable large-capacity system and must not be assigned to every historical WT9. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Aerospool WT9 Dynamic Club calculator.