Schweizer 300C Helicopter - WFH Florida

1 Schweizer 300 CTM HelicopterPiston-Powered Multi-Mission Schweizer 300 CTM HELICOPTERTECHNICAL INFORMATION1 Schweizer 300c Technical InformationSZR-004 February 2008 1473 Performance Standard day, sea level, maximum gross weight unless otherwise notedMaximum speed (VNE) 95 kts 176 km/hrMaximum cruise speed (VH) 86 kts 159 km/hrHover ceiling, In-Ground-Effect (1700 lb) 10,800 ft 3,292 mHover ceiling, Out-of-Ground-Effect (1700 lb)

2 8,600 ft 2,621 mRange (long range cruise* speed @ 4,000 feet) (no reserve)- 32 5 gallon 191 nm 354 km- 64 0 gallon 375 nm 694 kmWeights Maximum takeoff gross weight

3 2,050 lb 930 kgEmpty weight, standard configuration 1100 lb 499 kgUseful load 950 lb 431 kgDimensionsFuselage length

4 22 19 ft 6 76 mFuselage width 4 25 ft 1 30 mFuselage height 7 17 ft 2 18 mOverall length (rotors turning) 30 83 ft 9 40 mOverall height (to top of tail rotor)

5 8 72 ft 2 65 mWidth (canopy) 4 25 ft 1 30 mMain rotor diameter 26 83 ft 8 18 mTail rotor diameter

6 4 25 ft 1 30 mMain landing gear tread (fully compressed) 6 54 ft 1 99 mAccommodationNormal cabin seating (training) 2 Maximum certified cabin seating (utility)

7 3 Cabin length 4 75 ft 1 45 mCabin width 4 92 ft 1 50 mPowerplantsType Textron Lycoming HIO-360-D1 APowerplant ratings (per engine, standard day, sea level)- Takeoff (5-minute)

8 190 shp 141 kw- Maximum continuous 190 shp 141 kwFuel CapacityStandard fuel capacity 32 5 US gal 123 03 lExtended range capacity 64 0 US gal 242 27 ISpecificationsAnti-Submarine Warfare (ASW)Anti-Surface Warfare (ASuW)Search and Rescue (SAR)Vertical Replenishment (VERTREPS)

9 2 Schweizer 300c Technical InformationSZR-004 February 2008 1473 ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m) ft( m)Aircraft Dimensions3 Schweizer 300c Technical InformationSZR-004 February 2008 1473 The 300 CTM 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 Layout4 Schweizer 300c Technical InformationSZR-004 February 2008 1473 Full Panel (Police/Military)

10 Small Profile PanelStandard PanelIntermediate PanelCockpit Instrument Display Panel5 Schweizer 300c Technical InformationSZR-004 February 2008 1473 Standard EquipmentAirframe 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