Canadair CL-215 / CL-415 Super Scooper

The Canadair CL-215 and its turbine successors (CL-215T, CL-415, CL-415EAF, and the forthcoming DHC-515 Firefighter) are the only purpose-built amphibious water bombers in production or recent production anywhere in the world. Designed by Canadair in the late 1960s in response to Quebec's demand for a dedicated forest-fire aircraft, the CL-215 first flew on 23 October 1967 and entered service in 1969. Its defining capability is the ability to scoop roughly 1,620 US gallons (6,137 L on CL-415) of water from a lake, river, or ocean in about 12 seconds while skimming the surface, then drop that load on a fire and return to repeat the cycle — often within 10-minute turn times when the water source is near the fire.

The original CL-215 was powered by two Pratt & Whitney R-2800-83AM 18-cylinder radials producing 2,100 hp each. 125 CL-215s were built by Canadair/Bombardier between 1969 and 1990. The piston-radial variant was rugged but labor-intensive to maintain, with increasingly scarce R-2800 overhaul capacity driving the turbine conversion program.

The CL-215T replaced the R-2800s with two Pratt & Whitney Canada PW123AF turboprops (2,380 shp each), added winglets, finlets, power-assisted flight controls, and upgraded systems. Many CL-215Ts were factory conversions of existing CL-215 airframes.

The CL-415 (later rebadged Bombardier 415) was a new-build all-turbine aircraft sharing the CL-215T powerplant and aerodynamic refinements, but incorporating a modernized cockpit, redesigned systems, and improved water-drop capacity (6,137 L vs. 5,455 L). 95 CL-415s were built between 1993 and 2015 under Canadair and later Bombardier, before the type was sold to Viking Air / Longview Aviation Capital in 2016.

The CL-415EAF (Enhanced Aerial Firefighter) is a Viking/Longview program that takes used CL-215 airframes and converts them with PW123AF turbines, Collins Pro Line Fusion avionics, new winglets/finlets, rewiring, and 75 service bulletins to effectively bring them to near-415 standard. Bridger Aerospace is the launch customer, with six aircraft ordered under a $204M contract (approximately $34M per conversion).

The DHC-515 Firefighter is the restarted new-production program under De Havilland Canada (which acquired the type certificate as part of Viking/Longview's DHC brand consolidation). As of 2026, firm orders stand at 20+ aircraft from Croatia, Greece, France, Italy, Portugal, Spain, plus Canadian provinces of Manitoba, Ontario, and Alberta (the latter a C$400M commitment announced February 2026). First assembly began in Calgary in March 2026 with first deliveries targeted for 2028, and later orders slotted to 2031.

Total global fleet across all variants is roughly 160-170 airframes in active service, the vast majority government-operated. This is a commercial/government fleet aircraft, not a general aviation type.

The CL-series is a slow, draggy, high-lift airplane optimized for exactly one envelope: low-altitude scooping and drop runs. Book cruise of 180 KTAS is realistic in the clean configuration, but most ferry legs are flown lower and slower. The aircraft is not pressurized; service ceiling around 14,700 ft is academic because firefighting ops rarely exceed 3,000 ft AGL.

Scooping runs are flown at 70-80 kt just above stall, with the aircraft dragging its hull probes through the water for about 10-12 seconds to fill the 1,620-gallon tanks. The margin between scoop speed and stall is razor-thin and demands constant training — this is one of the most physically demanding airplanes in civil aviation to operate. Pilots fly in crews of two with heavy control forces even with hydraulic assist.

Fuel burn is substantial: roughly 240 US gph total in cruise, higher in scoop/drop cycles. Per-hour direct operating cost is estimated at $3,000-$5,000 depending on fuel and cycle intensity, and annual cost-to-operate per aircraft (including crew, maintenance, hangar, insurance) is cited by RAND at approximately $1.5 million — not counting the $1.5M/yr annualized acquisition cost on a 30-year life.

Takeoff and landing performance is respectable for a 44,000-lb twin: around 2,670 ft ground roll off dry pavement, and water takeoff distances roughly 2,670 ft on glassy water. The amphibious gear allows land operation from paved strips down to about 4,000 ft.

The CL family has a unique payload-range curve because it operates in three distinct loadouts:

• Ferry / repositioning (no water, full fuel): 1,310 nm still-air range at 180 KTAS, useful for cross-continent repositioning between fire seasons (e.g., hemispheric transfers from Europe to South America).
• Fire-attack loadout (partial fuel, water drops): Typical mission is 30-60 minutes out to a fire, then continuous scoop/drop cycles from a nearby water source. Fuel is carried to cover transit plus 1-2 hours of drop cycling plus reserves. Water mass (6,137 kg / 13,500 lb) displaces fuel on each drop but is re-loaded with each scoop, so effective payload-per-hour exceeds any conventional tanker.
• Maritime patrol / transport (rare): Up to ~7,000 lb of cabin payload across a range of 1,000+ nm, but this role is almost never flown because the fire mission dominates the global fleet.

Cycle-limited rather than range-limited: the wing and hull fatigue life per scoop/drop evolution is the binding constraint on long-term economics, not range or fuel.

Related pages: cargo-hauling · dehavilland-dhc6-twin-otter · maintenance-ecosystem · insurance-underwriting · valuation-methodology

• Firefighting / cargo hauling (6): The aircraft is purpose-built for aerial firefighting, which is essentially a specialized cargo-drop mission. Score reflects mass-delivery-per-hour capability for the one payload it carries (water/retardant). For conventional freight hauling the hull geometry is wrong.
• Cross-country (3): Can reach 1,310 nm on full internal fuel, but slow, loud, and expensive. Ferry flights are a means to an end, not a mission.
• Backcountry (2): Not a bush plane. The hull requires water or long paved runways; it cannot operate from unimproved strips like a dehavilland-dhc6-twin-otter.
• Local fun / flight training / aerobatics / business travel (1): Categorically not applicable. Two-pilot crew required, Part 25 airplane, commercial/government operation only.
• Surveying (2): Poor altitude performance and sensor integration make it a non-starter vs. dedicated survey platforms.

• CL-215 (piston): Original analog steam gauge cockpit with legacy VOR/ILS, HF radios, and weather radar. Most surviving airframes have been upgraded with GPS and collision avoidance as airspace rules demand.
• CL-215T / early CL-415: Part-glass cockpit with EFIS primary flight displays, dual FMS, weather radar, TCAS I/II, and military-style mission gear on government aircraft.
• CL-415EAF / DHC-515: Collins Aerospace Pro Line Fusion integrated avionics suite — full glass cockpit with synthetic vision, electronic charts, integrated FMS, ADS-B, EVS, and fire-mission-specific overlay software for drop coordination. This matches the avionics profile of current-generation regional turboprops.

There is no "panel upgrade market" in the GA sense — avionics work is done at OEM-authorized MROs (Cascade Aerospace, De Havilland Calgary, operator in-house shops) on a fleet-management basis.

Modifications to the CL family are almost exclusively driven by the type certificate holder (Canadair → Bombardier → Viking → De Havilland) and major MROs. Notable:

• PW123AF turbine conversion (CL-215 → CL-215T/EAF): The defining STC. Factory program under Canadair/Bombardier, then continued by Viking/Longview with Cascade Aerospace of Abbotsford, BC as prime conversion facility. Adds winglets, finlets, power-assist controls, rewiring, 75 service bulletins. Converted-aircraft value is roughly 3-4x unconverted piston CL-215 value.
• Pro Line Fusion retrofit (CL-415EAF): Bundled into the EAF conversion.
• Foam Injection System (FIS): Optional additive tank for mixing Class A foam into scooped water.
• Maritime patrol / SAR / utility fit: Limited conversions for Spanish and Italian forces with surveillance radar, FLIR, observer stations.

There is no aftermarket STC ecosystem comparable to GA aircraft — see valuation-methodology on why mod premiums here are driven by OEM/MRO programs rather than owner-installed STCs.

Reference maintenance-ecosystem. Support structure is entirely commercial-fleet oriented:

• OEM support: De Havilland Canada (Calgary) holds the type certificate and provides parts, technical publications, and fleet engineering support.
• Primary MROs: Cascade Aerospace (Abbotsford, BC) for heavy maintenance, mods, and CL-415EAF conversions. Aeroplex / Aerocraft in Spain for European fleet support. Operator in-house shops for large fleets (Securite Civile, SOPFEU, Bridger).
• Parts availability: Fair for turbine variants (new-production pipeline reopened with DHC-515), poor for original CL-215 R-2800 radials and many piston-era systems.
• A&P familiarity: Rare globally. Type-specific training and experience are required; there is no "find a local A&P" option. Qualified mechanics are concentrated at the ten or so facilities that regularly support the fleet.
• Expensive items: PW123AF hot-section inspections ($400K-$600K per engine), heavy checks tied to cycle count ($1M-$3M per event), hull/float corrosion repairs, and avionics lifecycle replacements. Annual cost per aircraft including everything is approximately $1.5M (RAND estimate, consistent with operator public disclosures).

Reference valuation-methodology. The CL family sits entirely outside GA comp pricing and must be valued on a commercial-asset basis (discounted cash flow of contract revenue, residual value on remaining cycles, conversion status).

Approximate ranges (2026 market):

Key value drivers:

• Turbine vs. piston: Converted airframes trade at 3-4x unconverted equivalents because R-2800 overhaul cost and parts pipeline are unsustainable.
• Remaining cycles: Each scoop/drop counts as a landing cycle on wing and hull structure. Low-cycle airframes command large premiums.
• Saltwater history: Freshwater-only airframes trade higher than Mediterranean-operated fleet returns.
• Avionics generation: Pro Line Fusion-equipped aircraft trade meaningfully above legacy-cockpit examples.
• Contract attachment: Aircraft with active government standing contracts (CAL FIRE, Quebec SOPFEU, Securite Civile) trade as cash-flow assets, not just airframes.

The CL-series has an active AD history from both Transport Canada (primary certification authority) and FAA. Recurring themes:

• Corrosion: Saltwater scooping operations (Mediterranean, Pacific, Atlantic) accelerate hull and structural corrosion. Several ADs address lower fuselage, bilge, step, and float structure inspections at reduced intervals.
• Water rudder and nose gear door integrity.
• Flight control cable and pulley wear on manually-boosted CL-215s.
• Engine mount and nacelle cracking on CL-215 R-2800 installations.
• Wing attach fitting inspections on high-time airframes (the cycle count from scoop/drop missions is brutal on the wing).
• PW123AF hot-section inspection intervals on turbine variants.
• Flight manual supplements and AFM revisions as late as the 1997 FAA AD 97-10-XX series on CL-415.

Common pre-acquisition red flags on used CL-215/215T airframes: saltwater operational history, corrosion in the planing bottom, incomplete service bulletin compliance, R-2800 parts pedigree (for unconverted 215s), and airframe fatigue life remaining relative to scoop/drop cycle count.

Reference insurance-underwriting. The CL family falls into the specialized commercial firefighting category — there is no retail GA market.

• Hull insurance: Typical annual hull premium $350K-$600K per aircraft depending on hull value, cycle exposure, and claims history. Hulls are insured at current-market values of $20M-$40M.
• Liability: $50M-$100M limits standard, with specialized fire-mission endorsements for third-party property damage and wildland firefighter ground liability.
• Crew requirements: Underwriters require two ATP-rated pilots with significant multi-engine turbine time, type-specific training (often done at De Havilland Calgary or operator in-house), recurrent training at 6-month or annual intervals, and documented scoop/drop currency.
• Underwriters: Global Aerospace, Starr Aviation, Allianz, and Lloyd's syndicates are primary markets. Only a handful of underwriting teams in the world actively quote the type.

This is not an insurable aircraft for a private individual under any realistic circumstance.