Velocity Aircraft · 1996+
Velocity XL
Specifications
Cruise
200KTAS
Range
1000nm
Seats
4
Useful Load
1100lbs
Full-fuel payload
680lbs
Fuel Burn
15gph
Fuel Cap.
70gal
MPG
15.3mpg
Stall (Vs0)
65KIAS
T/O roll
1400ft
Ldg roll
1500ft
Power
300hp
Engine
piston single
Gear
Retractable
IFR
Yes
Category
experimental
Pricing
Typical
$185k
Range
$120k – $310k
Annual all-in
~$10k/yr
All-in estimate at ~100 flying hours a year — fuel, annual inspection, engine reserve, insurance, and hangar. It scales with your actual hours, and insurance and hangar vary most by region and pilot.
Cost to own — estimate
Set your yearly hours and local fuel price. Fixed costs (insurance, hangar, annual inspection) don't change with hours; fuel and the engine reserve do.
- Fuel (15 gph)
- $9,750
- Engine reserve (toward overhaul)
- $2,750
- Fixed (insurance, hangar, annual, subscriptions)
- $0
- Total per year
- $12,500
- Per flight hour
- $125
- Miles flown / year (at cruise)
- 23,016 mi
- Cost per mile
- $0.54/mi
Estimate, not a quote — insurance and hangar (the fixed bucket) vary most by region and pilot. Anchored to our model figure at 100 hrs and $6.50/gal.
Strengths
- 200 KTAS cruise on 15 gph with 1,000+ nm range; best dollar-per-mile four-seater in experimental aviation
- Canard spin resistance; forward surface stalls first, providing genuine stall-safe handling
- Strong factory support and VOBA community; parts availability and transition training unusually robust for a kit aircraft
- 47.5-inch cabin width exceeds Bonanza; suitable for cross-country and business travel
Weaknesses
- Experimental-only; no dual controls on many builds, single-pilot operation, insurance and perception challenges for business use
- Builder quality variance is the dominant risk; poorly-built examples can have hidden structural, wiring, or fuel-system flaws
- Slow-speed handling poor; requires specialist transition training and 30–50 nm descent planning due to energy bleed
- Not a short-field airplane; 2,000–2,500 ft realistic takeoff distance, considerably more at high density altitude
Overview
The Velocity XL is a four-to-five seat composite canard pusher kit aircraft manufactured by Velocity Aircraft LLC of Sebastian, Florida. Designed by Dan Maher and first flown in the 1990s as an enlarged development of the earlier Velocity SE (itself derived from Rutan's Long-EZ/rutan-long-ez family lineage), the XL scaled up the cabin, fuel, and gross weight to accept the Lycoming IO-540 and true four-place, full-fuel cross-country capability. Velocity is the most prolific canard kit company still in business, with well over 500 airframes flying worldwide. The factory in Sebastian (200 W. Airport Drive, KX26) offers builder assist, transition training, and the Velocity Owners and Builders Association (VOBA) provides an unusually well-organized support community for a kit airplane.
The XL is marketed as the "high-speed, long-range cabin-class" canard: a 47.5-inch-wide cabin (wider than a Bonanza), 200 KTAS cruise on 15 gph, and no-spin handling inherited from the canard configuration. Kits ship approximately 80% complete when ordered with the full fast-build option, making the XL one of the quicker paths to a 200-knot four-seater. It competes conceptually with the cozy-mk-iv (larger, faster, factory-supported) and against certified high-performance singles on a dollars-per-knot basis.
Variants & History
| Variant | Years | Engine | HP | Gross | Key Differences |
|---|---|---|---|---|---|
| XL-FG | 1996-present | Lycoming IO-540 | 260-300 | 2700 lb | Fixed gear, 4-seat; simplest XL |
| XL-FG-5 | 2005-present | Lycoming IO-540 | 300 | 2800 lb | Fixed gear, 5-seat (rear bench for 3) |
| XL-RG | 1996-present | Lycoming IO-540 / Cont. IO-550 | 300-350 | 2700-2800 lb | Retractable tricycle gear; ~15 kt faster |
| TXL-RG-5 | 2005-present | Continental IO-550 | 310-350 | 3000 lb | Twin-XL stretched, 5-seat, RG; range king |
| V-Twin | 2012-present (limited) | 2x Lycoming IO-320 | 2x160 | 3200 lb | Experimental twin pusher prototype; "no-spin twin" |
| SE (legacy) | 1987-1996 | Lycoming IO-360 | 180-200 | 2250 lb | Earlier/smaller predecessor, now out of production as new-kit |
Earlier SE kits (180-200 HP IO-360) remain on the used market but the XL platform has been the factory's primary product since the late 1990s. The "standard" XL referenced here is the XL-RG with the Lycoming IO-540, which is the most common configuration.
Performance
Real-world XLs flown at 8,500-11,500 ft routinely see 195-205 KTAS at 65-75% power on a 300 HP IO-540, burning 14-16 gph. The aircraft is notably clean aerodynamically (canard+pusher with no cowl flaps, no exhaust drag on the wing), so pitch/power management on descent is critical — XL pilots learn early to start down 30-50 nm from destination. Unlike conventional low-wing aircraft, canards bleed energy slowly and speed brakes (optional) are a welcome addition.
The canard configuration provides genuine spin resistance: the forward canard stalls before the main wing, producing a nose-drop that unloads the wing before a full stall develops. The FAA allows the XL to display placarded minimum speeds rather than true Vs0/Vs1 because the main wing is not permitted to stall. The "stall" numbers in frontmatter represent minimum controllable airspeeds at gross weight.
Density altitude affects takeoff notably due to the loaded pusher prop behind a relatively blunt fuselage — published 1,300 ft book numbers require perfect technique; plan on 2,000-2,500 ft for realistic operation, and considerably more at high density altitude. The XL is not a short-field airplane.
Payload & Range
With 1,100 lb useful load and 70 gal (420 lb) standard fuel:
- Full fuel + 2 people + bags: 1,100 - 420 = 680 lb for people/bags. Two 200 lb adults = 280 lb available for baggage, which is ample; the XL handles this mission effortlessly with 1,000 nm range.
- Four adults (800 lb) + bags (100 lb) = 900 lb payload: Leaves 200 lb (33 gal) of fuel, ~2.0 hours endurance and ~400 nm range with VFR reserves. True four-place loadings force a fuel stop on any long trip.
- XL-5 with five aboard (1,000 lb) + minimal bags: Needs the 2,800-3,000 lb gross variants and ~35 gal of fuel for a ~420 nm leg — realistic as a shorter regional hop, not a true transcontinental 5-seater.
- Optional 93-100 gal tanks: Restore full-fuel range to 1,400+ nm but don't solve the full-seats payload-range problem — the airframe is useful-load limited, not tank limited.
Compared to a Cozy Mk-IV (cozy-mk-iv), the XL carries more and cruises faster but burns noticeably more fuel. Compared to a Long-EZ (rutan-long-ez), the XL is a generation more capable in cabin, payload, and IFR panel fit but costs 3-5x as much to acquire and operate.
Mission Suitability
Cross-country (9): This is the XL's sweet spot. 200 KTAS, 1,000+ nm range with 70 gal (1,300+ nm with the optional 93-100 gal tanks), 20,000 ft ceiling, and a quiet cabin (engine is behind you) make it one of the best dollar-per-mile four-seaters in experimental aviation. See cross-country.
Business travel (8): Wide cabin, air-conditioning STC options, and speed comparable to a Bonanza A36 or Cirrus SR22 at a fraction of the acquisition cost. The experimental status and canard novelty are the main drawbacks for business use (insurance, customer perception, rental/charter prohibition). See business-travel.
Local fun (6): Enjoyable to fly but overkill for $100-burger runs; fuel burn and hangar footprint work against it.
Flight training (2): Single-pilot experimental with no dual controls on many builds, high performance, and specialist transition training required. Not a primary trainer.
Backcountry (1) / Aerobatics (1): Retractable gear, low prop clearance (pusher), high approach speed, and composite structure disqualify it from rough-field and acro work. The G-limits on the Wikipedia spec (+9/-7) reflect structural capability but the airframe is not certified or intended for aerobatics.
Cargo hauling (4): 1,100 lb useful load is respectable but the baggage area is modest and the cabin shape doesn't accommodate bulky items.
Surveying (3): Too fast, canard visibility is compromised by the forward surface, and low-and-slow loitering is not its strength.
Avionics Ecosystem
As an experimental, the XL can use the full range of non-TSO avionics, which is a major cost advantage. Common panel tiers:
- Budget (~$15-25k): Single Garmin G3X Touch 10.6", GTR 200 comm, GTX 45R transponder, G5 backup. VFR/light IFR capable.
- Mid (~$35-55k): Dual G3X Touch, GTN 650Xi, GFC 500 autopilot (experimental version), GMC 507 controller, engine monitoring via G3X EIS. Full IFR with approach capability.
- High-end (~$70-120k): Garmin G3X + GTN 750Xi + GFC 500 + ADS-B in/out + synthetic vision + datalink weather + AoA + electronic ignition + dual alternator. Comparable to a new Cirrus G6 panel at half the price.
Because the XL cruises in the high teens, oxygen and/or a pressurization-adjacent flight profile matter — most XL owners install a built-in oxygen system. See avionics-pricing for detail on experimental pricing tiers.
2016 Van's RV-10
Dual G3X Touch · IFR · Beautiful Owner Build
STCs & Modifications
Experimentals do not use STCs in the certified sense, but Velocity Aircraft and third parties offer factory-approved modifications:
- Extended range tanks (70 → 93 or 100 gal): +$3,500-6,000; extends range to 1,300+ nm.
- Air conditioning: ~$8,000-12,000 kit; significant for Florida/desert operators given the large canopy.
- Electronic ignition (dual LightSpeed or SureFly): ~$2,500-4,500 installed; 5-10% fuel savings.
- Speed brakes: Factory option; essential for high-altitude descents.
- Winglets / wing cuffs: Most XLs come with winglets standard (part of the canard aerodynamic design).
- IO-550 upgrade (from IO-540): +$20-30k at overhaul; adds ~15 KTAS and climb.
- Whelen LED lighting, MT composite prop upgrade, Garmin autopilot retrofit: Common incremental upgrades on older airframes.
Maintenance & Support
Per maintenance-ecosystem:
- Parts availability: Good. Velocity Aircraft is operational and stocks most kit components; VOBA member forums trade used parts. Third-party canard parts (canard hinges, elevator control arms) are harder to source.
- Mechanic familiarity: Specialist. Most general-aviation A&Ps have never touched a composite canard pusher; the airplane is owner-maintained under experimental rules, but condition inspections (annual equivalent) require an A&P or the owner if they hold a repairman certificate for that specific airframe.
- Annual condition inspection: $1,200-2,500 if done by a Velocity-experienced shop; more if troubleshooting discovers build issues.
- Typical annual operating cost (100 hours/year): $9,000-12,000 including fuel (15 gph at $6.50), oil, inspections, insurance, and a reserve for overhaul.
- Expensive items: Pusher prop overhauls (3-blade MT composite) $4-7k; IO-540 overhaul $50-65k; composite repair after ramp damage is labor-intensive.
- Support ecosystem: The VOBA website, annual Velocity fly-in at Sebastian, and factory-run builder assist program are unusually strong for a kit aircraft — far better than most orphaned canard designs.
Valuation Factors
The XL's used-market range is wide because builder quality drives price more than on certified aircraft. Key factors per valuation-methodology:
- Base price range (used): $120,000 (older SE/low-time build, dated panel) to $310,000 (late-model TXL-5 RG with full glass and AC).
- Typical well-equipped XL-RG: $170,000-220,000.
- Engine time: TBO matters less than on certified engines since experimental engines can be run on condition, but 1,500+ SMOH airframes discount $15-30k.
- Avionics premium: Dual G3X + GTN 750 panel adds $40-60k over a steam-gauge XL.
- Factory vs. home build: Factory-assist builds (Velocity offers a "builder assistance center" where owners complete the airframe at the factory in 3-6 weeks) command a 15-25% premium due to known quality.
- Kit cost (new 2024): Base kit ~$54,000; fully fast-build kit ~$75-85k; plus $50-70k for engine, $15-60k for avionics, $10-20k for paint/interior, 800-1,800 build hours. All-in completed cost: $180-280k.
ADs & Common Problems
Experimentals are not subject to FAA ADs, but Velocity Aircraft issues Service Bulletins through VOBA that operators should treat as mandatory:
- Canard elevator trim tab bonding: Several older SBs on trim tab delamination; inspect at annual.
- Main gear strut corrosion (RG variants): Aluminum strut can pit; requires disassembly inspection every 500 hours.
- Fuel tank sealant (older strake tanks): Pre-2005 kits used a sealant formulation that can degrade; some airframes have required tank reseal ($8-15k).
- Pusher prop extension bolts: Torque checks every 100 hours; several fatigue failures historically.
- Nose gear retraction mechanism: The free-castering nose can develop shimmy; rebuild is straightforward but needs attention.
- Builder quality variance: The single biggest risk with any used XL. A well-built XL is a beautiful airplane; a poorly-built one can have hidden structural, wiring, or fuel-system problems. Pre-buy inspection by a Velocity-experienced builder or factory visit is essentially mandatory.
Accident history is dominated by pilot transition issues (high-speed approach, pusher CG effects on landing) rather than structural or systems failures.
Insurance Profile
Insurance is the Velocity XL's single biggest operating-cost surprise for buyers coming from certified aircraft. Per insurance-underwriting:
- Hull insurance (typical $180k agreed value): $3,500-5,500/year for an experienced pilot; $6,000-9,000/year for a transitioning pilot.
- Liability: $1M smooth is often unavailable; most policies cap at $1M/$100k sublimit.
- Underwriter requirements: Typically 500+ TT, 100+ retractable gear time, 25+ hours make-and-model dual (factory transition training at Sebastian satisfies this), and instrument rating. Low-time pilots can expect 50+ hours dual before solo.
- Market: Only a handful of carriers (Avemco, Starr, USAIG's experimental book) write Velocity hull coverage; shop aggressively.
- Claims history: Canard pushers have historically higher loss ratios than conventional experimentals due to transition accidents, which keeps premiums elevated.
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