Rutan · 1980–1985
Rutan Long-EZ (Model 61)

Specifications
Cruise
144KTAS
Range
1400nm
Seats
2
Useful Load
575lbs
Full-fuel payload
263lbs
Fuel Burn
5.2gph
Fuel Cap.
52gal
MPG
31.9mpg
Stall (Vs0)
52KIAS
T/O roll
750ft
Ldg roll
900ft
Power
118hp
Engine
piston single
Gear
Fixed
IFR
No
Category
experimental
Pricing
Typical
$45k
Range
$25k – $85k
Annual all-in
~$7k/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 (5.2 gph)
- $3,380
- Engine reserve (toward overhaul)
- $917
- Fixed (insurance, hangar, annual, subscriptions)
- $2,203
- Total per year
- $6,500
- Per flight hour
- $65
- Miles flown / year (at cruise)
- 16,571 mi
- Cost per mile
- $0.39/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
- Exceptional fuel efficiency (5–6 GPH) and 1,400+ nm range for cross-country touring
- Low acquisition cost ($35–55K typical) with reasonable operating expenses ($6–9K annual)
- Distinctive tandem seating, high visibility, and genuine 144 KTAS cruise on modest horsepower
- Active owner community (Canard Aviators, Canard Zone) provides peer support where factory support ended in 1985
Weaknesses
- Builder-quality variance is extreme; each airframe is unique and requires knowledgeable pre-buy inspection
- Requires canard-savvy A&P for condition inspections and composite work; generic mechanics insufficient
- High approach speed (85–90 KIAS) and long landing roll demand smooth, longer runways; grass/rough fields discouraged
- No IFR certification, known-ice, or single-engine reliability redundancy; not suitable for business or instrument flying
Overview
The Rutan Long-EZ is Burt Rutan's Model 61, a tandem two-seat, canard-configured, pusher-propeller composite homebuilt designed at the Rutan Aircraft Factory (RAF) in Mojave and first flown on June 12, 1979. An evolution of the earlier rutan-varieze, it used a longer wingspan, larger main wings, and a bigger strake fuel tank system to produce one of the most fuel-efficient piston singles ever built. Plans were sold by RAF from 1980 to 1985; roughly 700-800 airframes are registered with the FAA, making it the most-built Rutan canard. The Long-EZ became famous for holding the Burt Rutan/Dick Rutan distance record of over 4,800 miles in class and for its distinctive ramp appeal. Owners tend to be engineers, efficiency enthusiasts, and cross-country pilots — the same demographic that gravitated to the later cozy-mk-iv and berkut-360.
RAF ceased supporting Long-EZ plans after 1985 following the fatal accident of John Denver in a modified Long-EZ, but the design lives on through an active owner community centered on Canard Aviators, Canard Zone, and the Canard Owners and Builders Association.
Variants & History
| Variant | Years | Engine | HP | Gross | Notes |
|---|---|---|---|---|---|
| Long-EZ (plans, RAF) | 1980-1985 | Lyc O-235 | 108-118 | 1325 lb | Design baseline; most built |
| Long-EZ O-320 | — | Lyc O-320 | 150-160 | ~1425 lb (builder) | Popular owner mod; better climb, more useful load |
| Long-EZ O-360 | — | Lyc O-360 | 180 | varies | Aggressive repower; W&B critical |
| Long-EZ turbo/auto-conv | — | various | varies | varies | Subaru, Mazda rotary and turbo experiments; mixed reliability |
| N-numbered derivatives | — | varies | varies | varies | Individual builders; each airframe unique |
Major design descendants (separate pages): rutan-varieze (smaller predecessor), cozy-mk-iv (four-seat Nat Puffer derivative), berkut-360 (faster moldless-to-mold Long-EZ evolution).
Performance
Book cruise of 144 KTAS at 75% is achievable and sometimes exceeded — the Long-EZ is genuinely efficient, burning roughly 5-6 GPH at long-range cruise settings and delivering 25+ mpg. The 52-gallon strake fuel capacity combined with low burn produces a legitimate 1,400+ nm still-air range, the basis of its long-distance reputation.
The airplane is fast for its horsepower because of low parasite drag, laminar flow on the canard and main wing, and the pusher configuration that keeps the fuselage in clean air. Service ceiling of 27,000 ft is real (normally aspirated, oxygen required) because the canard stall-limited design maintains control authority at very low indicated airspeeds at altitude.
The canard will not stall in the conventional sense — it reaches a limiting angle of attack and begins gentle pitch bobbing before the main wing ever stalls. This is a safety feature but produces unusually high approach speeds (85-90 KIAS) and long landing rolls that surprise pilots trained on Cessnas. Crosswind handling is limited; the low-slung wingtip rudders and narrow gear track reduce directional authority. Takeoff rotation requires the canard to fly first and runway must be smooth — rough fields and grass are generally discouraged.
Payload & Range
Useful load of ~575 lb on a typical O-235 Long-EZ (heavier on an O-320 build with reduced useful load) produces the classic canard payload-range profile:
- Full fuel (312 lb) + pilot (200 lb): Leaves ~63 lb for passenger and baggage — solo or very light passenger only. This is the efficient long-range configuration: 1,400+ nm still-air.
- Two adults (400 lb) + 30 lb strake baggage: Leaves ~145 lb of fuel = ~24 gallons, giving ~650 nm range at 5.2 GPH — still a strong cross-country number for two people.
- Typical mission (two adults, 40 gal fuel, light bags): ~900-1,000 nm range with reserves — genuinely usable coast-to-coast with one fuel stop.
- Limiting factor: Not fuel or power but CG. The canard configuration has a narrow CG envelope and a light passenger or baggage change can push the airplane out of limits. Pilots routinely carry ballast in the nose for solo flight. Pre-flight W&B is mandatory every flight with different loading.
The Long-EZ, more than almost any other two-seat piston, delivers on the promise of efficient two-person transportation — the right pilot with the right mission gets a $45K airplane that rivals a Mooney on fuel burn per nautical mile. See cross-country for comparison against certified alternatives.
Mission Suitability
- Cross-country (9): The Long-EZ's reason for existing. Low burn, high cruise, massive range, high service ceiling, and excellent comfort for two with baggage in the strakes make it arguably the best efficiency-per-dollar touring platform in experimental GA. See cross-country.
- Local fun flying (8): Head-turning ramp appeal, unique flying qualities, and excellent visibility from the tandem canopies. It is a joy to fly once you adapt to canard pattern work.
- Business travel (5): Fast and efficient two-place travel, but no IFR certification on most examples, no known-ice capability, and runway limitations keep it from being a serious business tool.
- Surveying (2): Poor — single engine, no hardpoints, difficult to mount sensors, and the pusher prop rules out nose-mounted gear.
- Flight training (1), Backcountry (1), Aerobatics (1), Cargo (1): Disqualified. Experimental amateur-built aircraft may not be used for primary instruction for compensation. The long landing roll, fragile composite belly, and short-coupled nose gear make backcountry strips inadvisable. The airframe is not aerobatic (Rutan explicitly prohibited it). Baggage volume is limited to the strakes.
Avionics Ecosystem
- Traditional builder panels ($2-5K): Steam gauges, handheld GPS, basic comm — common on older examples.
- Mid-tier experimental ($8-15K): Dynon D10/D100, Garmin GTR 200, uAvionix tailBeacon X for ADS-B Out, basic autopilot servo.
- Modern glass ($20-40K): Dual Dynon SkyView HDX or Garmin G3X Touch, GTN 650Xi, TruTrak or Dynon autopilot, ADS-B In/Out. Experimental category permits these installations at a fraction of certified cost; see avionics-pricing.
- IFR equipped: Rare but possible with GTN 650Xi + WAAS; limited by lack of known-ice and airframe certification basis. Most owners fly VFR.
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STCs & Modifications
Experimental amateur-built aircraft do not use STCs; modifications are at builder/owner discretion. Common mods:
- O-320 repower: +30-40 HP, significantly improved climb and hot/high performance. Requires W&B rework and often a heavier prop.
- Klaus Savier LightSpeed ignition: Electronic ignition replacing one or both magnetos; ~5-8% fuel burn reduction.
- Vance Atkinson carb heat / fuel flow mods: Address known carb ice and fuel starvation issues.
- Wheel pants and NACA inlet tuning: Small speed gains; most builders fit these from the start.
- Roncz canard: Later airfoil redesign that addresses the original GU canard's rain-trim issue (severe pitch-down in rain); strongly recommended for any Long-EZ still flying the original GU canard.
- Winglet rudder upgrades and brake upgrades: Improve ground handling.
Maintenance & Support
Per maintenance-ecosystem:
- Parts availability (fair): The Lycoming O-235/O-320 is universally supported. Airframe-specific parts (canopy, wheel pants, nose gear hardware) are builder-sourced or fabricated. Aircraft Spruce stocks many Long-EZ materials. No factory parts pipeline — Rutan Aircraft Factory closed in 1985.
- Mechanic familiarity (specialist): Generic A&Ps can handle the Lycoming but the composite airframe, canard rigging, and pusher installation require someone who has touched a Long-EZ. Most owners maintain their own aircraft under experimental rules with a repairman certificate for the original builder; subsequent owners need an A&P willing to sign the condition inspection.
- Annual condition inspection: $500-$1,500 if self-done, $1,500-$3,500 with a canard-savvy A&P.
- Typical annual operating cost: $6,000-$9,000 including fuel (~80 hrs), insurance, hangar, reserves, and inspection.
- Expensive items: Composite repair after damage ($2-10K), canopy replacement ($3-5K), O-235 overhaul ($20-25K), O-320 overhaul ($25-30K), full repaint in structural white ($8-15K).
- Community: Canard Aviators mailing list, Canard Zone forums, Canard Owners and Builders Association, and annual Rough River fly-in are essential resources. This community is the effective "factory support" for the Long-EZ fleet.
Valuation Factors
Per valuation-methodology, experimental canard valuation weights build quality and airworthiness history over hours and year. Current market (2025-2026):
- Project / needs work: $15,000-$25,000 — incomplete builds, old panels, needs canard or fuel system rework.
- Typical flyer: $35,000-$55,000 — good O-235, mid-era panel, Roncz canard, clean logs. Median asking around $45K.
- Premium example: $60,000-$85,000 — O-320 upgrade, modern Dynon/Garmin panel, recent paint, excellent build reputation, builder-documented history.
- Outliers: Show-quality or famous-provenance examples occasionally exceed $90K but the market is thin.
Value drivers: Roncz canard retrofit (+$5-10K), O-320 vs O-235 (+$8-15K), modern glass panel (+$10-20K), documented builder pedigree (+$5-15K), fresh engine (+$10-15K). Value killers: GU canard, original carbureted O-235 with high time, unknown builder, soft/damaged foam, water intrusion in strakes.
ADs & Common Problems
Experimental aircraft do not receive ADs, but RAF-issued Canard Pusher newsletters and community advisories function similarly:
- GU canard rain trim: Original canard airfoil loses significant lift in heavy rain, causing uncommanded pitch-down. Roncz canard retrofit is the accepted fix.
- Fuel system vapor lock and starvation: Long sump lines in hot weather can vapor lock; numerous fatal and non-fatal accidents traced to fuel delivery. Careful plumbing, return lines, and electric boost pumps are community best practice.
- Composite delamination and UV damage: Uncovered or poorly painted airframes suffer epoxy UV degradation. White paint is mandatory structurally (not cosmetic) to keep the foam core below its glass transition temperature.
- Nose gear actuator wear: Manual crank retract system is simple but bushings and gears wear; mis-rigged nose gear is a common pre-buy finding.
- Prop strike from rotation mishandling: Tailstrike-equivalent on a pusher — over-rotation on takeoff or touchdown can strike the prop.
- Builder quality variance: Each Long-EZ is unique. Layup quality, resin ratios, and rigging vary dramatically. A knowledgeable canard pre-buy inspector is essential.
Insurance Profile
Per insurance-underwriting: the Long-EZ is one of the most insurable experimentals because of the large fleet, solid safety record (when flown within limits), and low hull values. Representative quotes:
- Liability only: $1,200-$1,500/yr for 500-hour pilot with 50 in type.
- Full coverage, $40K hull: $2,500-$3,000/yr for experienced pilot; $1,700 hull-only quoted on $38K hull in community data.
- Low-time pilot transition: Underwriters typically require 10-25 hours dual or supervised solo in type. A canard checkout with an experienced Long-EZ pilot is standard.
- No-hull liability-only is common given the $35-50K hull range — many owners self-insure the hull.
Insurance is cheaper than a comparable cozy-mk-iv because of the lower hull value and single-pilot tandem config.
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