BRM Aero · 2011+
BRM Aero Bristell Classic
Specifications
Cruise
117KTAS
Range
700nm
Seats
2
Useful Load
615lbs
Full-fuel payload
425lbs
Fuel Burn
5gph
Fuel Cap.
32gal
MPG
26.9mpg
Stall (Vs0)
31KIAS
T/O roll
500ft
Ldg roll
400ft
Power
100hp
Engine
piston single
Gear
Fixed
IFR
No
Category
light sport
Pricing
Typical
$270k
Range
$180k – $420k
Annual all-in
~$8k/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 gph)
- $3,250
- Engine reserve (toward overhaul)
- $625
- Fixed (insurance, hangar, annual, subscriptions)
- $4,125
- Total per year
- $8,000
- Per flight hour
- $80
- Miles flown / year (at cruise)
- 13,464 mi
- Cost per mile
- $0.59/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
- Widest cabin in LSA class (51 in); genuinely comfortable for two adults on long trips
- 117–141 KTAS cruise range depending on engine; one of fastest S-LSA options available
- Rotax 912/915/916 engines supported by broad North American shop network; strong parts availability
- Excellent cross-country platform: 700+ nm range, no medical, autopilot-capable avionics
Weaknesses
- 2-seat limit and tight useful load (310–410 lbs payload with full fuel) constrains real-world mission flexibility
- CG-sensitive stall behavior; aircraft not spin-tested or spin-approved—requires disciplined technique
- Bristell-specific airframe parts require 4–8 week lead times from Czech manufacturer; not stocked domestically
- 15 KIAS demonstrated crosswind limit; longer wing requires more precise crosswind management than shorter-wing LSAs
Overview
The BRM Aero Bristell is a Czech-designed two-seat light-sport aircraft that has earned a reputation as one of the fastest and most capable aircraft in the S-LSA category. Designed by aeronautical engineer Milan Bristela and manufactured by BRM Aero in Kunovice, Czech Republic, the aircraft first flew as a prototype on March 1, 2011, and entered US market at the AOPA Summit in September 2011. By December 2020 more than 600 examples had been delivered worldwide; by the time the B23 Part 23 type certificate was issued in September 2025, the company had delivered over 1,100 aircraft.
The Bristell occupies an unusual position in the LSA market: it is purpose-built as a touring and cross-country machine rather than a cheap trainer. Its 51-inch-wide cabin (the widest in the LSA class), all-metal low-wing construction, bubble canopy, and multi-engine-option powerplant lineup give it a character closer to a touring aircraft than a typical sport plane. When equipped with the Rotax 915iS turbocharged engine, it cruises well above 120 knots and climbs at rates that rival many Part 23 singles.
The original model (marketed as the Bristell Classic, formerly NG5) holds FAA S-LSA airworthiness certification under ASTM F2245 standards. In parallel, BRM Aero developed the Bristell B23, a dimensionally related but structurally distinct airframe that received EASA CS-23 certification and then FAA Part 23 Type Certification in September 2025 — a meaningful distinction for flight schools, since Part 23-certified aircraft can be used for formal instrument and commercial training without an E-LSA re-registration. Bristell has also designated much of its current lineup MOSAIC-ready (see mosaic), anticipating the expanded MOSAIC LSA category that took effect October 22, 2025.
BRM Aero produces roughly 120 aircraft per year. North American sales flow through Sport Flying USA (the primary importer) and a growing dealer network.
Variants & History
| Variant | Years | Engine | HP | MTOW (lbs) | Gear | Key Differences |
|---|---|---|---|---|---|---|
| NG5 UL | 2011–present | Rotax 912 ULS | 100 | 1,042 | Fixed tricycle | European ultralight gross weight; not US S-LSA |
| NG5 HD | 2011–present | Rotax 912 ULS | 100 | 1,323 | Fixed tricycle | Heavy-duty wing spars for higher gross weight |
| Classic (NG5 LSA) | 2011–present | Rotax 912 ULS / 912iS Sport / 915iS / 916iS | 100–162 | 1,320 | Fixed tricycle | Primary US S-LSA; long 29 ft 11 in wing |
| Classic TD | 2012–present | Rotax 912 ULS / 912iS | 100 | 1,320 | Fixed tailwheel | Taildragger variant; same airframe |
| Classic 915 | 2019–present | Rotax 915iS (turbo) | 135 | 1,320 | Fixed tricycle | Turbocharged; 23,000 ft ceiling; 141 KTAS at altitude |
| Classic 916 | 2022–present | Rotax 916iS (turbo) | 162 | 1,320 | Fixed tricycle | Highest-power LSA option; ~$340k new |
| RG | 2018–present | Rotax 912/915/916iS | 100–162 | 1,320 | Retractable | US experimental-only (FAA prohibits RG on S-LSA); 134 KTAS cruise |
| Speed Wing | ongoing | Various | Various | varies | Fixed | Homebuilt kit variant with shorter chord wing |
| B23-912 | 2025–present | Rotax 912S3 | 100 | 1,654 | Fixed tricycle | FAA Part 23 TC (Sept 2025); EASA CS-23; wider wing; BRS chute standard |
| B23-915 IFR | 2023–present | Rotax 915iS | 135 | 1,654 | Fixed tricycle | EASA IFR-certified variant; GTN 650 + G500TXi panel |
| B23-916 | Dec 2025–present | Rotax 916iS | 162 | 1,654 | Fixed tricycle | EASA CS-23 with 916 engine, Dec 2025 approval |
| M23 (MOSAIC) | 2025–present | Rotax 916iS | 162 | 1,653 | Fixed tricycle | MOSAIC-ready model; targets new MOSAIC LSA category |
Variant note: The Classic and B23 share design DNA but are distinct products. The Classic is the S-LSA for sport pilots without a medical certificate. The B23 is a Part 23 certified aircraft at 1,654 lb MTOW targeting flight schools and pilots wanting full FAA-certified training capability. Frontmatter data above applies to the Classic with Rotax 912 ULS — the most common US-market configuration.
Performance
Cruise speed context: The Classic with Rotax 912 ULS cruises at approximately 117 KTAS at 75% power and 3,000 ft MSL — fast for the LSA category, which historically tops out around 120 KIAS. Real-world pilots report 110–117 KTAS at economy cruise (5,000 rpm) on roughly 5 GPH. The 915iS-equipped variant reaches 125–141 KTAS depending on altitude, with fuel burn of 6–9 GPH; at FL100+ the turbo advantage compounds as TAS climbs toward 141 KTAS at only 8 GPH. The 916iS exceeds 145 KTAS in the Classic (still capped at 1,320 lb gross) or delivers the same speed with more useful load in the B23.
Stall characteristics: Published VS0 is 31 KIAS (full flaps, power off) and VS1 is 43 KIAS (clean). A 2020 Australian CASA safety notice flagged stall/spin incidents in Bristell aircraft attributed to CG positioning and cross-controlled stalls. BRM Aero subsequently corrected weight-and-balance datum documentation and provided spin-test data; CASA determined the corrected AOI data was adequate. Operators should treat aft-CG loading with care and avoid slipping into stalls — the aircraft is NOT spin-tested or spin-approved under ASTM standards.
Useful load reality: The Classic test aircraft (AOPA/Flying reviews) weighed 720–820 lbs empty depending on options, yielding 500–600 lbs useful load at 1,320 lb gross. With full fuel (190 lb at 31.7 gal) the pilot-and-passenger payload is 310–410 lbs depending on actual empty weight — competitive for LSA but tight with two heavy adults plus bags. The 43.2-gallon extended-range tanks cut payload further.
Density altitude: The naturally aspirated 912 ULS begins losing appreciable climb performance above 5,000 ft density altitude. The 915iS maintains rated power to approximately 15,000 ft MSL through its turbocharged intercooled architecture, making the turbo variant the preferred choice for western US high-altitude operations.
Long wing handling: The 30-ft wingspan generates high lift at slow speeds but can be lively in gusty crosswind conditions. Reviewers note the aircraft requires more precise crosswind management than shorter-wing LSAs. Demonstrated crosswind component is 15 KIAS (20 KIAS shown during testing).
Payload & Range
Reference aircraft: Classic with Rotax 912 ULS, 705 lb empty weight (per AOPA guide), 31.7 gal standard tanks.
| Scenario | Fuel (gal) | Fuel Weight (lbs) | People + Bags (lbs) | Total Payload (lbs) | Range (nm) | Notes |
|---|---|---|---|---|---|---|
| Full fuel, 2 pax economy | 31.7 | 190 | 425 | 615 | ~640 | 2×170 lb + 85 lb bags; near max useful load |
| Full fuel, 2 light pax | 31.7 | 190 | 340 | 530 | ~700 | 2×155 lb + 15 lb bags; comfortable margin |
| Extended tanks full, 2 pax | 43.2 | 259 | 356 | 615 | ~870 | With 43.2-gal option; payload reduced to ~356 lbs |
| Short hop, reduced fuel | 15 | 90 | 525 | 615 | ~320 | Full 2-person payload flexibility |
| 915iS typical cruise | 31.7 | 190 | ~310 | ~500 | ~540 | 820 lb empty typical for 915 build; tighter margins |
Key takeaway: The Classic with 912 is genuinely comfortable for two average adults on trips up to 3 hours. The extended tank option transforms it into an 800+ nm aircraft but requires lighter occupants or less baggage — typical for a 1,320 lb gross LSA. The turbo 915/916 variants weigh 100+ lbs more empty (820–900 lbs typical), compressing useful load to ~420–500 lbs at LSA gross; full fuel with two adults is tight but workable for the typical 150–160 lb pilot demographic. The B23's 1,654 lb MTOW is a meaningful improvement — 662 lbs useful load allows two average adults plus gear plus most fuel scenarios without compromise.
Mission Suitability
| Mission | Score | Rationale |
|---|---|---|
| flight-training | 7 | Excellent trainer ergonomics, wide cockpit, docile handling. 912 economy supports high cycles. Not spin-approved; S-LSA category limits formal IFR/CPL training use (B23 Part 23 addresses this). |
| backcountry-bush | 2 | Fixed tricycle gear, low wing, and 10 in propeller ground clearance make backcountry strips marginal to unsuitable. No tundra or rough-field options exist. Tailwheel version slightly better but still limited. |
| business-travel | 6 | 700 nm range, 117–141 KTAS cruise, and 51-in wide cabin make it genuinely useful for short trips. No medical required is a major plus. Limited by 2-seat capacity and LSA speed cap; 915/916 models meaningfully close the gap with faster certified aircraft. |
| aerobatics | 1 | +4/-2 G limit, no spin approval, not aerobatic. Unsuitable. |
| cross-country | 8 | One of the best cross-country LSAs available. 700+ nm range (extended tanks), 117 KTAS economy, 51-in cabin, Garmin G3X with autopilot, and no medical requirement make it a compelling touring platform. Turbo variants push this to 9. |
| cargo-hauling | 2 | Two-seat aircraft; 33 lbs fuselage bay plus 44 lbs per wing locker. No meaningful cargo capacity. |
| local-fun-flying | 8 | Responsive controls, excellent visibility, easy handling, and high performance make it genuinely fun. Comfortable for longer recreational flights. |
| surveying | 5 | Low wing partially limits downward visibility. Side-by-side seating limits sensor configurations. Adequate for basic aerial observation work; not ideal. |
Avionics Ecosystem
The Bristell is designed around the Garmin G3X Touch ecosystem. BRM Aero and Sport Flying USA offer a tiered option structure:
Base / VFR (Package A):
- Single 10.6-inch Garmin G3X Touch (GDU 460)
- Garmin GEA 24 engine data module (EMS, fuel, flaps, trim displayed)
- ADS-B In and Out integrated
- Heated pitot-static probe
- 10-watt COM radio
- XM traffic and weather capability
- Electronic Stability and Protection (ESP) — automatic unusual attitude prevention
Mid / Cross-Country (Package B–C):
- Dual 10.6-inch G3X Touch screens + dual ADAHRS (independent backup)
- Garmin GNX 375 GPS/NAV/COM with LPV approach capability (IFR vertical guidance on RNAV approaches — requires ELSA re-registration for US IFR flight)
- Garmin GMC507 autopilot module: 3-axis with altitude hold, NAV tracking, heading hold, vertical speed
- G5 backup EFIS with independent battery (~20–30 min)
- TOSTEN CS-8 stick-mounted grip with PTT, trim, and frequency controls
Full IFR / Premium (Packages D–E / B23 IFR config):
- Garmin GTN 650Xi GPS/NAV/COM or GTN 750Xi
- Garmin G500 TXi or G3X with G5 backup EFIS
- GI 275 standby EFIS
- DME and stormscope (B23-915 IFR model)
- GMA 345 digital audio panel
- Heated angle-of-attack probe with custom alerting thresholds
Key notes on IFR: An S-LSA cannot be flown IFR under FAR 91 in the US. Some owners convert to E-LSA status, which permits IFR panel modifications and IFR flight if the aircraft is appropriately equipped — but E-LSA conversion is one-way (cannot revert). The Bristell B23 Part 23 resolves this: as a certified aircraft it can legally be equipped and operated IFR, and BRM Aero has already type-approved an IFR variant through EASA, with FAA IFR certification planned as a follow-on to the 912 type certificate.
Autopilot pricing: basic 2-axis autopilot (heading hold, GPS steering, altitude hold, ESP) adds approximately $5,900. Full GMC507 3-axis package runs higher. See avionics-pricing for Garmin G3X stack cost benchmarks.
2011 CubCrafters Carbon Cub
Carbon Cub SS · STOL Legend · Tundra Tires
STCs & Modifications
S-LSAs operate under ASTM consensus standards rather than FAA STC authority. Modifications are governed by the manufacturer's approval process and ASTM F2295 (continued airworthiness). Notable modifications:
Engine upgrades (manufacturer-approved):
- Rotax 912 ULS → 912iS Sport (fuel injection, same 100 HP, lower fuel burn at ~4 GPH)
- Rotax 915iS upgrade kit (~$10,000–$15,000 installed over 912): adds 35 HP and turbocharging; transforms climb and altitude performance; requires new cowl and engine mounts
- Rotax 916iS (162 HP): highest-power option; further reduces fuel burn per knot of cruise speed
Propeller options:
- DUC Flash 4-blade carbon composite: smoother, better ground clearance than 3-blade options
- Sensenich 3-blade composite: lighter, simpler
- MT Propeller: available for turbo variants
Fuel system:
- Extended-range tanks (43.2 gal total vs. 31.7 gal standard): adds 11+ gallons (~70 lbs), cuts useful load proportionally; extends range to 800+ nm at economy cruise
BRS parachute system:
- Available as factory option; standard on B23
- Ballistic Recovery Systems unit mounted in fuselage spine
- Adds approximately 45–55 lbs to empty weight
Tailwheel conversion (TD model):
- Factory-option tailwheel configuration available from new; not a field STC
E-LSA re-registration:
- Owners may re-register as Experimental LSA (one-time, irreversible); enables owner maintenance, IFR avionics, and more extensive modifications per FAR 21.190
No traditional FAA STCs exist for the S-LSA platform — all performance modifications flow through BRM Aero's ASTM-governed modification approval process.
Maintenance & Support
Maintenance framework: S-LSA aircraft follow manufacturer-specified maintenance per ASTM F2295 (continued airworthiness). Annual condition inspections replace FAA annuals; they must be performed by an appropriately rated person (A&P, repairman certificate, or LSA repairman with inspection rating). Interval is 12 calendar months. The Bristell maintenance manual specifies 100-hour periodic inspections for airframe and propeller in addition to the condition inspection.
E-LSA owner maintenance: Owners who convert to E-LSA status and complete an approved Sport Pilot Repairman course may perform their own condition inspections and maintenance — a significant cost advantage.
Rotax engine maintenance specifics:
- 912 ULS / 912iS: 2,000-hour TBO; 5-year rubber replacement ($2,500–$4,000); gearbox overhaul at 1,000 hrs ($450–$850); complete overhaul ~$12,500
- 915iS: 1,200-hour TBO (shorter, more intensive); overhaul cost approximately $15,000–$20,000
- Rotax engines are supported by a broad network of Rotax-certified shops in North America; not limited to factory-trained Bristell mechanics
Airframe support:
- Sport Flying USA (primary US importer) stocks Bristell-specific parts and is described as the only factory-trained Bristell mechanic operation in the US
- All-metal construction (primarily aluminum) means most airframe repairs are within A&P competence for standard skin and structural repairs
- Composite components (canopy frame, fairings) require composite repair skills
- Manufacturer warranty: 18 months / 200 hours from new
Annual ownership cost estimate: $6,000–$10,000/year for a typical privately owned example with moderate hours, including condition inspection ($800–$1,500), engine reserves, consumables, and routine maintenance. Does not include hangar, fuel, or insurance. Condition inspections on the Bristell are generally straightforward; the main cost drivers are prop and engine reserve accrual. See maintenance-ecosystem for LSA maintenance cost benchmarks.
Parts availability: Good for Rotax engine components (wide supply chain). Bristell-specific airframe parts (control surfaces, canopy, structural) require ordering from the manufacturer or Sport Flying USA; lead times can be 4–8 weeks from Czech Republic. Rated good overall but not excellent — a significant damage event requiring unique Czech-sourced parts may ground the aircraft for weeks.
Valuation Factors
The Bristell market is heavily configuration-driven. Engine type and avionics tier drive more price variance than airframe hours, particularly given Rotax's well-documented longevity and the fact that LSA condition inspections replace traditional annuals.
New aircraft pricing (2025–2026):
- Classic 912 ULS base: ~$159,700 AOPA guide list; real-world equipped pricing starts around $210,000–$250,000
- Classic 912iS Sport equipped: ~$230,000–$270,000
- Classic 915iS Turbo equipped: ~$280,000–$350,000
- Classic 916iS Turbo equipped: ~$310,000–$370,000
- B23-912 Part 23: ~$267,000 listed; pricing still being established in US market
- High-spec 916 RG or M23 MOSAIC: $400,000–$434,000
Used market pricing (2022–2024 vintage):
- 2022 model, 600 hrs, 912 ULS: ~$250,000–$270,000
- 2023 model, low time, 915iS: ~$370,000–$410,000
- Depreciation is modest for well-equipped low-time examples; heavily optioned aircraft may lose 10–20% in the first 1–2 years
Key value drivers (see valuation-methodology):
- Engine hours vs. TBO: Mid-TBO 912 (1,000–1,500 hrs) trades at slight discount vs. low-time; near-TBO aircraft discount more steeply unless price already reflects overhaul
- Avionics tier: Full IFR panel with GTN 650 and 3-axis autopilot can add $30,000–$50,000 of value over base VFR glass
- BRS parachute: Adds ~$12,000–$15,000 to value; some buyers strongly prefer it
- Extended fuel tanks: Modest premium ($3,000–$5,000) for the added range
- Hours on airframe: Less important than certified aircraft given ASTM-based maintenance; low hours still command premium
- Turbo vs. NA: 915iS-equipped aircraft command the largest premium in the used market; 916iS used examples are scarce
ADs & Common Problems
No FAA Airworthiness Directives apply to the Bristell S-LSA. Under ASTM standards, manufacturer safety directives are mandatory for S-LSAs; owners must monitor BRM Aero's service bulletin (SB) and mandatory service letter (MSL) issuances.
Known Issues / Pre-Buy Red Flags:
Stall/spin characteristics (CG-sensitive): In 2020, Australia's CASA issued a safety notice after stall-related incidents. Investigation revealed incorrect weight-and-balance datum in some Aircraft Operating Instructions (AOI), placing the CG outside its envelope without the pilot's knowledge. BRM Aero corrected the datum from wing leading edge to engine firewall and reissued AOI documentation. Pre-buy: verify the aircraft's AOI version is current and W&B documentation reflects the corrected datum.
Engine mount inspection: Rotax 912/912iS/915iS engine mounts should be inspected per Rotax overhaul schedule. Rubber isolator mounts harden with age regardless of hours; 5-year rubber replacement is mandatory per Rotax SI-912-016 and SI-915-003.
Fuel system compatibility: Rotax engines are approved for 100LL and mogas (unleaded auto fuel meeting Rotax specification). If mogas has been used, verify fuel system hoses, O-rings, and gaskets are ethanol-compatible (Rotax requires certification of compatibility for E10+ fuels). Hose degradation from unapproved ethanol blends is a known issue across the Rotax fleet.
Canopy latching mechanism: The single-latch front-hinge canopy has been noted in forum discussions for requiring positive confirmation of closure before flight. Verify latch action and canopy seal condition during pre-buy.
Avionics integration (older units): Earlier aircraft used non-Garmin glass panels (Dynon, Kanardia). Verify panel configuration matches maintenance documentation and that ADS-B Out compliance has been addressed on older aircraft.
Crosswind weathervaning (tailwheel TD): The taildragger variant requires tailwheel endorsement and more deliberate crosswind technique than the tricycle model; used TD models should be pre-flown with an instructor before purchase.
Insurance Profile
The Bristell falls into the light sport aircraft insurance category, treated similarly to other high-value S-LSA in the $200,000–$400,000 hull range. See insurance-underwriting for LSA-category underwriting norms.
Hull insurance: At typical hull values of $230,000–$350,000, annual hull premiums run approximately 1.0–1.5% of hull value for experienced pilots — roughly $2,500–$5,000/year. For new certificates or low-time sport pilots the rate may climb to 2–3%.
Liability coverage: $1,000,000 smooth (per occurrence) is standard; $100,000 per passenger is commonly selected. Annual liability-only premium: $400–$800.
Total annual premium estimate: $3,000–$5,500 for an experienced pilot with a well-equipped $280,000 example.
Underwriting factors:
- Sport Pilot certificate holders generally get favorable rates on S-LSA due to the specific-aircraft focus of the rating
- High-time private pilots flying S-LSA are viewed very favorably (lower-risk profile)
- Flight school use on an S-LSA commands a surcharge; B23 Part 23 aircraft used in formal training programs are underwritten differently
- BRS parachute installation is viewed positively by some underwriters and may yield a small premium discount
- Turbocharged variants may carry slightly higher rates due to higher hull values and more complex systems
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