Elixir Aircraft Elixir

The Elixir is a side-by-side two-seat, low-wing, T-tailed composite trainer built by Elixir Aircraft in La Rochelle, France. It is the first clean-sheet airplane in decades designed from the outset around the economics of a flight school rather than around a private owner's shopping list, and its central idea is structural: the airframe is built with a one-shot carbon process — Elixir calls it Carbon OneShot — that reduces the entire structure to nine major parts and roughly 600 part numbers, against the tens of thousands of pieces in a riveted aluminum trainer. Fewer parts means fewer fasteners to inspect, no corrosion to chase, and, per Elixir, a 100-hour check one technician can complete in a single working session.

It is a genuinely certified airplane, not a light-sport one. EASA issued the CS-23 type certificate on 20 March 2020, initially at a 544 kg maximum takeoff mass, raised to 630 kg in 2022 and to 700 kg for the modification-2023-14 aircraft. The FAA issued its own Part 23 type certificate on 22 July 2025 at AirVenture, which is the fact that makes this page worth writing: an American buyer registers an Elixir in the standard category with a normal airworthiness certificate. There is no Experimental Exhibition workaround, no LSA acceptance question, no importation gymnastics.

The commercial story is a flight-training story. Elixir reports more than 300 orders and letters of intent, most of them American, and has stood up a North American hub at Sarasota Bradenton International (KSRQ) — a 12,500 sq ft hangar plus an adjacent 6,000 sq ft building — where La Rochelle-built airframes are reassembled, held as spares stock, and delivered. First US customer deliveries began in May 2026: two aircraft to Cirrus Aviation in Florida (against an order for 10) and one to Sierra Charlie Aviation in Scottsdale, Arizona (against a pre-order of 100). European operators already flying the type include Airbus Flight Academy Europe and Egnatia Aviation.

The two things a US buyer must understand before getting excited are on the type certificate itself. First, the airplane is approved for Day-VFR and Night-VFR only — there is no IFR approval, despite an IFR-grade Garmin panel. Second, at 100 horsepower and 700 kg it is a trainer and a tourer for two, not a family airplane, and the useful load rewards reading the Payload-Range section below before signing anything.

Two naming notes that matter when reading a logbook. "Elixir B" is the designation the approved documentation uses for a MOD-2023-14 aircraft; "Elixir+" is the marketing name for the same thing. And the TCDS spells out the serial number convention: MSNxxx-(B)-(N), where B means the 700 kg modification and N means the aircraft is eligible for a US standard airworthiness certificate. Read the data plate. A serial without the B is a 630 kg airplane with about 180 lb less useful load, and a serial without the N is not straightforwardly US-registrable.

The catalogue stores 125 KTAS and 610 NM from the factory's 85% table, but 4.9 gph rather than the factory's 3.9. That is a deliberate mismatch and it is the honest one. Elixir publishes three settings at 10,000 ft:

AOPA's coverage of the FAA certification gives 4.9 GPH for the 100 hp Rotax, a quarter above the factory's 85% figure, and Rotax's own published data for the 912 iS supports the higher number — 12.5 L/h is nearer a 55-60% setting than a genuine 75%. Because the stored burn feeds the cost-to-own model, storing the brochure figure would understate the headline ownership number by about 25% for every reader. The independent measurement wins. Plan on 4.5-5.0 GPH. Even at 5 GPH this is a two-seater burning less than a Cessna 152, and it is approved on unleaded E5 mogas as well as 100LL.

The ranges deserve a caveat. The TCDS gives 104 L total / 100 L usable (26.4 US gal), while Elixir's own specification page still describes a "single 94-liter tank". The published 610 NM appears to have been computed on the smaller figure and carries a substantial reserve either way, so treat it as conservative rather than optimistic — the right direction for the one number in this table that could strand you.

Climb is published as a 950-1,300 fpm band; 950 is the number stored, because it is the end you will see at 700 kg on a warm day. Service ceiling is 10,000 ft for the 100 hp aircraft, and that is a real ceiling, not a paper one — a normally aspirated 100 hp engine simply runs out of air. The TCDS separately permits operation to 16,000 ft, which is a certification limit rather than a capability, and the gap between the two is precisely the argument for the turbocharged 915iS variant. Glide ratio is published at 10:1; the best-glide speed is not published and is deliberately absent from the frontmatter.

Two published V-speeds are worth pausing on. VS0 is 47 KIAS and VS1 is 59 KIAS — high for a trainer, and a direct consequence of a small, efficient 8.24 m² wing. That is what buys the cruise efficiency, and it is also why the approach is flown faster than students trained on a 172 will expect. The airframe is spin-resistant by design (winglets, leading-edge treatment, and a certification basis that includes a special means of compliance for enhanced stall characteristics), not spin-approved: load factors are +4 / -2 flaps up, normal category.

Finally, an operating limitation that is easy to miss and matters enormously in the American Southwest: the composite structure is qualified only to 54°C (129°F), and the TCDS prohibits operation above that structure temperature. A dark-painted composite airframe sitting on a Phoenix ramp in July reaches that. Shade, covers and scheduling are not optional here.

On the 700 kg Elixir+ (Elixir B), useful load is about 595 lb (1,543 lb gross less 948 lb empty):

• Full usable fuel (26.4 gal / 158 lb) leaves 437 lb for people and baggage.
• Two 190 lb adults (380 lb) + full fuel: 538 lb of 595. There are 57 lb left over, and the baggage compartment is limited to 55 lb — so with two average American adults the airplane is full to its volume limit at almost exactly the same moment it fills to its weight limit. That is unusually well balanced design work.
• Two 220 lb adults (440 lb) + full fuel: 598 lb against 595 lb available — three pounds over gross, before a flight bag. Two large adults means leaving a gallon or two behind, which costs you nothing you will miss at 610 NM of range.
• Solo, 190 lb pilot, full fuel: 348 lb of 595. The remaining 247 lb is unusable — you cannot carry more than 26.4 gallons and you cannot put more than 55 lb behind the seats. This is a two-seat airplane whose useful load is genuinely matched to two seats, which is rarer than it sounds.

On the earlier 630 kg airframe (1,389 lb gross, ~921 lb empty) useful load falls to roughly 467 lb. Full fuel leaves 309 lb — two 155 lb people and nothing else. That configuration is a solo tourer and a lightweight-student trainer, and it is why the MOD-2023-14 uprating exists. Weigh the specific aircraft and read its actual weight-and-balance sheet; an equipped school airplane with air conditioning will not match the brochure empty weight.

Range at the factory's 85% setting is 610 NM; at its 75% setting it is 793 NM, and neither figure is affected by payload since the tank fills long before the airplane runs out of useful load. The binding constraint on a long day in an Elixir is the pilot, not the airplane.

• Flight training (9): This is the airplane's entire reason to exist and it is very good at it. Purpose-designed for ab-initio through commercial, spin-resistant, parachute-equipped, single-lever, a 100-hour check measured in hours rather than days, and fuel costs that undercut every legacy trainer in the fleet. The single point it loses is the one that costs a school money: it cannot currently be used for instrument training, because the type certificate is VFR-only. The Elixir+ Expert is meant to fix that and is not certified yet.
• Local fun flying (8): Light, modern, well-harmonised, cheap by the hour, with a parachute over your head and a glass panel in front of you.
• Cross-country (6): 125 knots on under 5 gallons an hour with 600+ NM of range is a genuinely capable touring number for two. Held down by VFR-only operation, a 10,000 ft ceiling that makes weather and terrain avoidance harder, 55 lb of baggage, and no de-ice of any kind.
• Surveying (4): Long endurance at low burn is exactly right; a low wing and modest downward visibility are exactly wrong.
• Business travel (3): Two seats, VFR only, no ice protection, and a ceiling that puts you under rather than over the weather. It will not get you somewhere on a schedule.
• Aerobatics (1): Normal category, +4/-2, no spin approval. No.
• Backcountry (1): Low wing, small wheels, composite belly, and a structure temperature limit. Pavement only.
• Cargo hauling (1): 55 lb behind the seats.

• As delivered (current standard): Garmin G3X Touch glass, with the full-glass configuration EASA-certified in late 2023 comprising dual G3X touchscreens, a GTN 750Xi and a GNC 355a, plus a Garmin autopilot. That is a panel most $400,000 four-seaters would be pleased with, and it is standard equipment rather than an option sheet.
• The trap: that hardware is IFR-capable; the airplane is not IFR-approved. A GTN 750Xi does not confer an approval the type certificate withholds. You can legally train an instrument student in an Elixir only in the way you can in any VFR airplane — under the hood in VMC, which is how European operators describe using it. Actual IMC is prohibited.
• Coming: the Elixir+ Expert pairs the 700 kg airframe with Garmin AXIS flight displays and is specifically intended to carry an IFR approval. Elixir has not disclosed a certification date. Treat it as a roadmap item.
• What you will not need to budget for: a US ADS-B retrofit. Unlike gray-market European light aircraft, US-delivered Elixirs are assembled and configured for the US market in Sarasota under the "N" regional configuration.

This is the airplane's strongest technical argument and its weakest practical one, at the same time.

• The design case is real. Nine major airframe parts, roughly 600 part numbers, no corrosion, no rivets, no life-limited structure. Elixir reports a 100-hour inspection completed by one technician in a single session (four to seven hours, depending on which account you read), against the day-plus a legacy trainer takes. Over a 500-hour training year that is a meaningful difference in downtime, and downtime is what a school actually pays for.
• Parts availability: fair. Everything is single-source from La Rochelle, and there is no aftermarket, no salvage yard, and no PMA alternative for anything. Against that, Elixir now holds spares inventory at Sarasota (KSRQ) with a local technical support team, and plans roughly 200 staff there by 2027 — which is a far better position than any comparable European import has ever offered a US buyer. A structural item will still come from France.
• Mechanic familiarity: specialist. The Rotax half is easy; Rotax-capable shops are widespread. The airframe half is factory-supported and effectively factory-only today. Confirm you have a shop willing and trained to sign for it before you buy, and understand that outside Florida and Arizona that shop may be Elixir itself.
• Annual/100-hour inspection: budget $1,500-2,500 on the strength of the published labor hours. This should be the cheapest recurring line on the airplane.
• Typical annual operating cost: roughly $15,000 at 100 hours — about $2,900 fuel (100 hr at ~4.9 GPH, mogas or 100LL), $5,000 insurance, $3,600 hangar, $1,500-2,500 inspection, $700 engine reserve, and a few hundred toward the parachute and propeller sinking funds. Insurance is the largest single line, at nearly twice the fuel bill — the direct consequence of a $430,000 hull on a two-seat airplane. Elixir's own "$50 per flight hour" claim covers fuel and maintenance only, and on those two lines the arithmetic supports it.
• Reserves: $7/hr engine (a $14,000 Rotax 912 overhaul over 2,000 hours — and note that a new or exchange 912 at $17,600-19,600 less core makes replacement, not overhaul, the usual choice at TBO). The MT propeller carries a calendar/hours overhaul interval; confirm the current figure with MT-Propeller and fund it separately. The ballistic parachute has a finite rocket and canopy life and is a four-figure sinking fund, not a free feature.
• The honest summary: the maintenance design is excellent and the maintenance ecosystem is one company with one US facility. If you are within reach of Sarasota, or you are a fleet operator Elixir wants to keep flying, the support will be very good. If you are a single private owner in Montana, ask hard questions about turnaround before you sign.

Two things dominate here, and both are unusual.

• There is no published US list price. Elixir has not released one. The figures in the frontmatter are the European prices reported in trade coverage — AOPA cites approximately €400,000, Flying describes the trainer as "north of €300,000" — converted at roughly $1.15/€ to give a $345,000-$460,000 bracket. Get a written quote from the Sarasota office before treating any of this as a price. Specification, avionics, and whether the aircraft is a 700 kg B airframe will move it materially.
• There is essentially no US used market. First US deliveries were May 2026. Every American Elixir is a new or near-new airplane, most of them in flight-school fleets that ordered in tens and hundreds. There are no comparable sales, no Bluebook history, and no basis for an appraisal. That cuts both ways: you will not find a bargain, and you will not find a buyer quickly either.
• 630 kg vs 700 kg is the biggest single value lever. About 180 lb of useful load separates a two-adults-and-full-fuel airplane from one that makes you choose. Price them as different aircraft, because they are.
• VFR-only caps the buyer pool. Until the Elixir+ Expert is certified, this airplane cannot serve the instrument-training market or an owner who wants to file. That is a real, permanent-until-it-isn't discount against a DA20 or a 172 in the same money.
• Depreciation is genuinely unknown. A five-year-old type with a 300-aircraft order book and a manufacturer that raised $50M is a reasonable bet, but nobody has yet sold a used Elixir into the American market and discovered what it fetches. Treat resale as the largest uncosted risk in the purchase, and size the deposit accordingly.
• Where value should hold up: no airframe life limit, no corrosion, a maintenance profile that stays cheap as hours accumulate, and Rotax economics. High-time is far less punishing on this airframe than on an aluminum trainer, which should compress the usual high-hours discount over time.

The type is five years old with a small global fleet, and the honest position is that there is not yet an accumulated defect history to report — which is information, not reassurance.

• No EASA or FAA airworthiness directive against the airframe was located in this research. Absence of a finding at this fleet age and size is weak evidence; check the EASA AD tool and FAA DRS for the specific serial as part of any pre-buy rather than relying on this line.
• Rotax 912 service documents apply regardless of airframe — the 1,000-hour gearbox rubber-coupling and slipper-clutch inspection above all. Any Rotax-capable shop knows this; make sure yours has done it.
• Ballistic parachute currency. The rocket and canopy have finite lives and a repack/replacement cost. A time-expired system on an otherwise clean airplane is a four-figure surprise and is routinely missed in pre-buys of parachute-equipped types.
• Structure temperature limit (54°C / 129°F). Ask directly how a candidate aircraft has been stored. A school airplane that has lived on an unshaded Arizona or Florida ramp for three summers is a different proposition from a hangared one, and there is no simple inspection that quantifies the difference.
• Trainer duty cycle. Most airframes in existence are in schools. Expect high cycles relative to hours, and inspect the gear, brakes and nose leg accordingly — landing count, not tach time, is what wears a trainer.
• Composite repair history. Any structural repair on a one-shot carbon airframe should have been done under factory supervision. The nine-part construction that makes the airplane cheap to maintain also makes a damaged major component a large, single-source item.

Pre-buy red flags: a serial without the B suffix sold at B money; a serial without the N suffix offered for US registration; a time-expired parachute; unshaded hot-climate storage with no covers; any composite repair without factory paperwork; and European avionics configuration on an aircraft that did not come through Sarasota.

• Hull: roughly $4,300-$6,000/year on a ~$430,000 hull, working from the published hull rate band of 0.8-2.5% and the fixed-gear-single class. $5,000 is the planning figure. The airframe is simple — fixed gear, 100 hp, a parachute, benign certified handling — which is everything an underwriter likes; what they do not like is a type with no US claims history and no adjuster who has seen one.
• Liability: $1,000-1,500/year for $1M smooth.
• The hull value, not the aircraft, drives the premium. This is a $430,000 two-seater. Insuring it costs several times what insuring a $85,000 DA20 costs even though the risk profile is similar, and owners coming from legacy trainers are routinely surprised by that. It is arithmetic, not underwriting prejudice.
• Commercial flight-school use is a different policy class entirely — higher premium, named-insured CFIs, student solo coverage. Do not price a school operation from an owner-flown quote.
• Underwriting quirks: expect a factory or factory-approved checkout requirement and, for low-time owners, dual instruction minimums. Confirm before purchase that a carrier will write the type at all — a brand-new import can take a broker several weeks to place even when the airplane itself is uncontroversial.
• Rare-type penalty: with a handful of US airframes, minor composite damage is likely to be settled generously or as a total loss rather than repaired locally. That is fine for you and is priced into the premium.