Specifications (415)
Data from Bombardier Aerospace Website
General characteristics
- Crew: 2 pilots
- Additional Seating: one on jump seat, eight on bench seats
- Payload: 6,400lb (2,900 kg)
- Length: 65 ft (19.82 m)
- Wingspan: 93 ft 11 in (28.6 m)
- Height: 29 ft 3 in (8.9 m)
- Wing area: 1,080 sq ft (100 sq m)
- Airfoil: NACA 4417
- Empty weight: 28,400 lb (12,880 kg)
- Maximum fuel weight: 10,250 lb (4650 kg)
- Maximum takeoff weight (from land, disposable load): 43,850 lb (19,890 kg)
- Maximum takeoff weight (from land, non-disposable load): 41,000 lb (18,600 kg)
- Maximum takeoff weight (from water): 37,850 lb (17,170 kg)
- Max Capacity (Water or Retardant): 13,536 lb (6,140 kg)
- Maximum weight after scooping: 47,000 lb (21,360 kg)
- Maximum landing weight: 37,000 lb (16,780 kg)
- Powerplant: 2 × Pratt & Whitney Canada PW123AF turboprop, takeoff power: 2,380 shp (1,775 kW) each
Performance
- Maximum speed: 223 mph (359 km/h (194 kt))
- Cruise speed: 207 mph (333 km/h (180 kt))
- Stall speed: 78 mph (126 km/h (68 kt))
- Range: 1,518 miles (2,443 km)
- Service ceiling: 14,700 ft (4,500 m)
- Rate of climb: 1,600 ft/min (8.1 m/s)
- Takeoff distance (ISA, land): 2,750 ft (840 m)
- Takeoff distance (ISA, water): 2,670 ft (815 m)
- Landing distance (ISA, land): 2,210 ft (675 m)
- Landing distance (ISA, water): 2,180 ft (665 m)
- Minimum water depth: 6 ft (1.8 m)
Avionics
- Honeywell Primus 2 Radio Navigation
- RNZ-850 with ADF, VOR/ILS/Marker Beacon and DME
- Litef/Honeywell LCR93, Attitude and Heading Reference System
- Honeywell EDZ-605 EFIS with Dual EADI and EHSI
- Radio Altimeter (Honeywell AA-300)
- Parker-Gull Three-tube Active Matrix LCD Integrated Instrument Display System
- Dual CIC/Aerosonics Air Data Computers
- Dorne & Margolin ELT-8 Emergency Beacon
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