Lancair 235 project
🇨🇭 Schweiz
🟡 7 Tage

Lancair 235 project

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KI-Preisbewertung (gem. EU AI Act, Art. 13): Diese Preisbewertung ist eine automatisierte, nicht-verbindliche Schätzung auf Basis vergleichbarer Marktdaten — sie stellt weder eine Kaufpreisempfehlung noch eine gutachterliche Wertermittlung dar. Für eine verbindliche Bewertung empfehlen wir, einen anerkannten Luftfahrt-Sachverständigen hinzuzuziehen.

Lancair 235, SN 198, year 1987, no instrumentation.Not airworthy, kit is 100% complete, no parts missing, progress ca. 80%, 800h on workload already invested (roughly value 40- 50tsd), needs rest of workload according Lancair manual, all composite works are finished.Built under EAS environment & supervision, means seamless EAS proof on progress.This beauty has been built by a EASA licensed mechanic. Weighing data available. Timeline :1987 Kit ordered.1989 First owner (Composite Tecnica) began work.1998 Second owner purchased the kit.o All structural composite work contracted to Composite Tecnica. o Structural load test of the wings completed and certified by EAS.o All related company invoices and EAS work reports available.Early 2000s Project paused.2012 Project taken over by sussessoro At takeover, all major composite shell bonding was completed.o Carry out of the extensive trimming and surface finishingwork on the composite structures.o Detailed current progress is available in the document Lancair 235(Experimental) Current Build Status . Key ParticularitiesAll structural and composite work has been carried out exclusively by professionals:o Composite Tecnica (specialized composite company) for the initial build and structural tasks.o EASA B1 licensed aircraft engineer, for subsequent work.This is not a typical amateur/hobbyist setting the aircraft has been professionally managed from the start.Details : Fuselage, canopy with front opening, wings with extended range fuel tank, complete new hydraulic kit, upgraded landing gear, all the original lancair kit hardware perts, pushrods and rudder wires, flight controls, cockpit panel in aluminium, front tank, brakes and lines, reinforced engine mount (for 235 or 320 engine), firewall, el. variable pitch 3 blades MT propeller (for lycoming 235 or 320), el. flap actuator, mechanical trim, upgraded rudder pedals.This Lancair has been built by a EASA B1 certified aircraft maintenance engineer, stop

Baujahr
1998
Standort
Switzerland
Quelle
planecheck.com
Online seit
2026-08-18 🟡 7 Tage
Daten täglich aktualisiert
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