S chwei z er 3 0 0 C T M H elicopter T echnical I nformation Schweizer 300CTM Helicopter Piston-Powered Multi-Mission Specifications Performance Standard day, sea level, maximum gross weight unless otherwise noted Maximum speed (VNE) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 95 Maximum cruise speed (VH) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86 Hover ceiling, In-Ground-Effect (1700 lb). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10,800 Hover ceiling, Out-of-Ground-Effect (1700 lb) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8,600 Range (long range cruise* speed @ 4,000 feet) (no reserve) - 32.5 gallon. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 191 - 64.0 gallon. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 375 kts . . kts . . ft. . . ft. . . . . . . . . . . . . . . . . . . . 176 . 159 3,292 2,621 km/hr km/hr m m nm . . . . . . . 354 km nm . . . . . . . 694 km Weights Maximum takeoff gross weight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2,050 lb . . . . . . . Empty weight, standard configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1100 lb . . . . . . . Useful load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 950 lb . . . . . . . 930 kg 499 kg 431 kg Dimensions Fuselage length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22.19 Fuselage width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.25 Fuselage height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7.17 Overall length (rotors turning). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30.83 Overall height (to top of tail rotor). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.72 Width (canopy) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.25 Main rotor diameter. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26.83 Tail rotor diameter. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.25 Main landing gear tread (fully compressed). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.54 ft. . ft. . ft. . ft. . ft. . ft. . ft. . ft. . ft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.76 1.30 2.18 9.40 2.65 1.30 8.18 1.30 1.99 m m m m m m m m m Accommodation Normal cabin seating (training) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Maximum certified cabin seating (utility). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 Cabin length. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.75 ft. . . . . . . Cabin width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.92 ft. . . . . . . 1.45 m 1.50 m Powerplants Type . . . . . . . . . . . . . . . Powerplant ratings (per engine, - Takeoff (5-minute) . . . . . . . - Maximum continuous . . . . . . . . . . standard . . . . . . . . . . . . . . . day, sea . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Textron Lycoming HIO-360-D1A level) . . . . . . . . . . . . . . . . . . . . . . . . . . 190 shp . . . . . . 141 kw . . . . . . . . . . . . . . . . . . . . . . . . . . 190 shp . . . . . . 141 kw Fuel Capacity Standard fuel capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32.5 US gal . . . 123.03 l Extended range capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 64.0 US gal . . . 242.27 I 1 Schweizer 300C Technical Information SZR-004 February 2008 1473 Aircraft Dimensions 8.72 ft (2.65 m) 6.54 ft (1.99 m) 4.25 ft (1.30 m) 15.29 ft (4.66 m) 30.83 ft (9.40 m) 13.42 ft (4.09 m) Anti-Submarine Warfare (ASW) Search and Rescue (SAR) 6.88 ft (2.10 m) 7.17 ft (2.18 m) 6.17 ft (1.88 m) 4.25 ft (1.30 m) 8.25 ft (2.51 m) 22.19 ft (6.76 m) Vertical Replenishment (VERTREPS) Anti-Surface Warfare (ASuW) 2 Schweizer 300C Technical Information SZR-004 February 2008 1473 Cockpit Layout The 300CTM helicopter’s cockpit offers two different configurations. The standard right-hand Pilot-In-Command (PIC) flight control configuration allows for comfortable seating of an instructor and student. With the optional left-hand PIC configuration, the right-hand controls can be removed making it possible to seat a pilot and two passengers. 3 Schweizer 300C Technical Information SZR-004 February 2008 1473 Cockpit Instrument Display Panel Standard Panel Intermediate Panel Full Panel (Police/Military) Small Profile Panel 4 Schweizer 300C Technical Information SZR-004 February 2008 1473 Standard Equipment Included in the aircraft basic certified empty weight. Based on 2007 data. Airframe and Control Systems • Three bladed fully articulated main rotor • Elasometric main rotor dampers • Dual flight controls, left hand pilot-in-command • Collective friction control • Cyclic friction control, two axis • Electric cyclic trim, two axis • Tubular skid-type landing gear • Conical tail rotor teetering bearings • Offset anti-torque pedals • Booted Oleo landing gear dampers • Heavy duty skid shoes • Ground handling wheel brackets • Fuselage jack/lift fittings • Tie down kit • White Glasurit Urethane paint • Three piece chin skin with integral side fairings Powerplant, Systems and Instruments • 32.5 gallon fuel tank • Airspeed indicator • Altimeter • Ammeter • Cylinder head temperature indicator • Dual engine/rotor tachometer • Dual large oil coolers • Engine oil pressure indicator • Engine oil temperature indicator • Exhaust collector • Fuel pressure indicator • Fuel quantity indicator • Fuel shut-off valve • Fuel flow oil filter, remotely mounted • Low fuel warning light • Lycoming HIO-360-D1A engine • M/R transmission oil temp/pressure warning light • Magnetic compass • Manifold pressure gauge • Oil cooling system with integral spin-off oil filter • Oil filler/dipstick • Outside air temperature gauge • Running time (Hobbs) meter, panel mounted • T/R transmission chip detector warning light Electrical System • 70 amp alternator • Cabin accessory plug • Circuit breaker protection • Cyclic mounted radio frequency scrolling switch*, ** • External APU plug • Lead acid battery • Light weight, high torque starter • Modular electric harness • Night lights with strobe beacons • Switchable hot mic intercom system *Requires purchase of communication transceiver **Not available w/cargo hook - optional grip available Electrical System • Adjustable ventilation system • Three-seat cushioned interior • Clear cabin door windows • Floor/cabin carpet • Circular air scoop vents on doors • Lap belts and shoulder harnesses • Tinted canopy windows • Single latch doors • Glove box Note: Manufacturer reserves the right to modify this configuration by substituting comparable or better equipment. 5 Schweizer 300C Technical Information SZR-004 February 2008 1473 Optional Equipment Utility and Convenience Options • Alternator, electrosystems 130 amp • Cabin cover • Cargo hook installation • Cargo rack • Cyclic grip, special • Door openers, pneumatic • Doors, triple latch • Elastomeric teeter bearings • Fire extinguisher, dry chemical • Fire extinguisher, halon • First aid kit • Float kit, fixed • Fuel system, auxiliary (64 gallon) • Grease fitting, short shaft • Ground handling wheels, flyable • Heater, muff • Heater, Paravion • High stance landing gear with extra heavy duty gear • Hobbs meter - landing gear contact switch • Landing lights - two or three position • Map case • Muffler • Skid shoes, extra heavy duty • STAR system (start-up overspeed limiter, automatic rotor engagement, low RPM warning device) • Up-stack exhaust installation • Up-stack exhaust with supertrap • Windows, with sliding glass Avionics Options • ADF receiver, KR87 with KI227-00 indicator • Attitude gyro • Audio panel, KMA24H-71 • Blind encoder, ACK A-30 • Clock, electrical • Clock, quartz (LC-2) • Clock, quartz (LC-2E) • Comm/GPS, Garmin GNC 420 • Comm/GPS, Garmin GNC 420A • Comm/GPS, moving map, Garmin 250XL • Comm transceiver, KY196A • Comm transceiver, KY96A • Compass-vertical card, overhead • Compass system, KCS55A with HSI and heading transmitter • Dimmer assembly, supplemental • Directional gyro • Emergency locater transmitter, EBC502 • Fan, avionics cooling • Intercom foot switch • Headset, David Clark H10-56 • Intercom, NATAA80 • Intercom, NATAA83 stereo • Intercom, NATAA85 • Marker beacon, KR21 • Master avionics switch • NAV/COMM, KX155-39 with 203 CDI • NAV/COMM/GS, KX155-43 with KI209 CDI • NAV/COMM/GS Garmin GPS, GNC 430 with Gi106A indicator • Transponder, Garmin GTX320A, 327 • Turn coordinator • Turn and slip indicator, Electric Gyro Corp. • Vertical speed indicator, United 7000 6 Schweizer 300C Technical Information SZR-004 February 2008 1473 Paint Options BASF Glasurit exterior paint is used on all Schweizer 300CTM helicopters. It is one of the most technically advanced paints available and is used by numerous premium automobile companies such as BMW and Mercedes. The Schweizer nine-step paint process assures superior corrosion protection and a durable, yet highly attractive appearance. The 300C helicopter is offered with an all white base coat as standard. Optional paint colors and trim schemes are available upon request. Factory Standard Trim Styles Type A Type B Type C Type D 7 Schweizer 300C Technical Information SZR-004 February 2008 1473 Safety and Crashworthiness The 300CTM helicopter’s extraordinary safety record is the result of its exceptional flight safety and crashworthiness characteristics. It is the beneficiary of more than thirty years and 20-million flight hours of commercial and military flight experience. Like its predecessors, the 300C aircraft retains high student margins that even seasoned pilots will appreciate. Crashworthiness Features • Energy absorption through plastic deformation • Seating configuration places occupants far from the rotor impingement zone • Unique geometry eliminating tailboom strikes Articulated rotor system Mast: rollover protection Proven dynamic system Rapid throttle response: reserve power Engine and fuel system Outside of Enclosed structure Low aft mounted engine Dual strobe lights – visible from all angles Rotor impingement outside crew envelope Energy absorption, 23 inches of strokes Safety Features • Rugged, reliable component design • Stable handling characteristics • Excellent safety record • Rapid throttle response 8 Schweizer 300C Technical Information SZR-004 February 2008 1473 Mission Performance Speed vs. Range 425.0 Maximum Range 400.0 Range (nautical miles) 375.0 1700 lb (771 kg) 350.0 325.0 VH 2050 lb (930 kg) 300.0 275.0 250.0 200.0 175.0 30 40 50 60 70 Airspeed (kts) 80 90 100 Speed vs. Endurance 8.00 Endurance (hourr – no reserves) Maximum Endurance 7.00 1700 lb (771 kg) 6.00 5.00 2050 lb (930 kg) 4.00 3.00 2.00 20 30 40 50 60 70 80 90 Airspeed (kts) Note: Performance charts vary with individual aircraft configuration. Consult Flight Manual for actual flight operations. 9 Schweizer 300C Technical Information SZR-004 February 2008 1473 100 Mission Performance Hover Ceiling In-Ground-Effect Pressure altitude (feet in thousands) 14 12 1700 lb (771 kg) 10 8 1900 lb (862 kg) 6 2050 lb (930 kg) 4 2 ISA + 20° ISA 0 0 10 20 30 40 50 60 70 Ambient temperature (°F) 80 90 100 90 100 Hover Ceiling Out-of-Ground-Effect Pressure altitude (feet in thousands) 14 12 10 1700 lb (771 kg) 8 6 1900 lb (862 kg) 4 2050 lb (930 kg) ISA + 20° 2 ISA 0 0 10 20 30 40 50 60 70 Ambient temperature (°F) 10 Schweizer 300C Technical Information SZR-004 February 2008 1473 80 Mission Performance Vne vs. Density Altitude Density altitude (feet in thousands) 16 Note: Maximum cruise speed is limited by Vne at higher altitudes 1700 lb (771 kg) 14 1900 lb (862 kg) 12 10 8 2050 lb (930 kg) 6 4 ISA 2 0 30 40 50 60 70 80 (Kias) 90 100 110 120 Rate of Climb Pressure altitude (feet in thousands) 16 14 12 10 8 1900 lb (862 kg) 2050 lb (930 kg) 1700 lb (771 kg) 6 4 Engine Critical Altitude 2 0 0 200 400 600 800 1000 Rate of climb (feet per minute) 11 Schweizer 300C Technical Information SZR-004 February 2008 1473 1200 1400 Mission Performance Height-Velocity Diagram 500 Height abovesurface (feet) 450 Smooth hard surface avoid operation in crosshatched areas 350 300 Recommended takeoff profile 250 200 150 30 40 50 60 70 80 90 100 110 120 (Kias) Autorotation Rate of Descent 2200 Height abovesurface (feet) 2000 1800 1600 1400 1200 20 30 40 50 (Kias) 12 Schweizer 300C Technical Information SZR-004 February 2008 1473 60 70 Overhaul and Retirement Schedule Components with Scheduled Overhaul Times Main rotor transmission. . . . . . . . . . . . . . . Tail rotor transmission. . . . . . . . . . . . . . . . Engine. . . . . . . . . . . . . . . . . . . . . . . . Belt drive system overhaul - Upper ball bearings, belt drive frame assembly. . - Lower ball bearings, belt drive frame assembly. . - Idler pulley bearings, belt drive assembly. . . . . Hours . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,500 * . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,800 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,000 *Aircraft must be operated in accordance with Lycoming Service Instruction SI-1009 Components with Mandatory Retirement Times Main transmission ring gear carrier/coupling. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6,000 Main transmission pinion assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6,000 Main rotor drive shaft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,200 Main rotor hub. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8,000 Main rotor mast . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13,590 Main rotor thrust bearing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,000 Main rotor pitch bearing shaft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,600 Main rotor blade assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5,500 Tailboom assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4,200 Horizontal stabilizer assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4,200 Vertical stabilizer assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20,540 Tail rotor drive shaft assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6,000 Tail rotor gearbox input shaft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8,600 Elastomeric main rotor damper. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6,000 Tail rotor blade assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9,000 Tail rotor blade retention straps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5,100 Lower pulley coupling shaft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6,000 Tailboom attaching strut assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10,700 13 Schweizer 300C Technical Information SZR-004 February 2008 1473 Estimated Direct Operating Costs The following represents estimated average operating costs over a period of 5,000 hours (1,000 hours per year over five years) in US dollars, assuming US costs predicted for fuel, shop labor rates, and parts costs. Fuel and lubricants Average fuel consumption (gallons per hour). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel cost per gallon (dollars/gal) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cost of fuel (dollars/fh). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Cost of lubricants, 3% of fuel (dollars/fh). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.80 5.31 62.66 1.88 Total costs for fuel and lubricants (dollars/fh). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 64.54 Maintenance Labor Shop labor rate (dollars/fh). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Direct maintenance (m/fh). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Indirect maintenance (m/fh). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Total maintenance (m/fh). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55.00 0.38 0.12 0.50 Total cost for maintenance labor (dollars/fh) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27.50 Reserves Engine overhaul. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16.80 Unscheduled replacement and on-condition parts. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.70 Scheduled maintenance/inspection materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.80 Major component overhaul @ TBO and replacement of retirement items . . . . . . . . . . . . . . . . . . . . . . . . . . 14.62 Total cost of reserves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36.92 Total direct operating cost (dollars/fh). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 128.96 Note: The operating data provided herein are estimates only. Schweizer Aircraft endeavors to ensure that this data is current and meaningful for operating cost evaluations. Schweizer Aircraft, however, does not warrant, and you should not rely upon, this data as defining the operating costs or overhaul/retirement times for any particular 300C helicopter or its components 14 Schweizer 300C Technical Information SZR-004 February 2008 1473 Notes Notes Elmira, NY 14845, USA +1 (607) 739-3821 www.sacusa.com SXR-004 1473 5C February 2008