SCHWEIZER MODEL 300C MULTI

Transcription

SCHWEIZER MODEL 300C MULTI
SCHWEIZER MODEL 300C
MULTI-ROLE PISTON HELICOPTER
SCHWEIZER 300C
MULTIPURPOSE HELICOPTER
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TH-55/TH-300C WORLDS
STANDARD MILITARY TRAINERS
TH-55 OSAGE - U.S. ARMY EXPERIENCE
PRIMARY U.S. ARMY TRAINER 1965-1988
OVER 60,000 PILOTS TRAINED
OVER 4,000,000 FLIGHT TRAINING HOURS
OVER 12,000,000 TOUCHDOWN AUTOROTATIONS
ONLY 1 CATEGORY “A” ACCIDENT SINCE TRAINING
BEGAN AT FT. RUCKER (1972)
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MODEL 269 SERIES HELICOPTERS
OVER 3750 AIRCRAFT PRODUCED
PRIMARY TRAINER FOR MILITARY IN 24 COUNTRIES
OVER 20 MILLION HOURS ON FLEET
MILESTONES-1964-First TH-55A to U.S. Army
1970-Hughes developed Model 300C
1983-Program Transitioned to Schweizer
2005-1000TH Schweizer helicopter produced
300C DESIGN PHILOSOPHY
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COST EFFECTIVE
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MAXIMUM SAFETY
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LOW MAINTENANCE
– LONG LIFE COMPONENTS
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HIGH PERFORMANCE
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STABLE, VIBRATION-FREE FLIGHT
CHARACTERISTICS
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300C HELICOPTER
THREE-VIEW DRAWING & WEIGHT STATEMENT
TH-300C PAYLOAD-WEIGHTS
30 MINUTE FUEL
GROSS WEIGHT
EMPTY WEIGHT
PILOT
FUEL
PAYLOAD
5
FULL
FUEL
EXTERNAL
LOAD
INTERNAL
LOAD
2050
1100
170
180
600
2150
1100
170
30
850
2050
1100
170
30
750
CHRONOLOGY OF MAJOR MILESTONES
FOR MODEL 269 SERIES HELICOPTERS
1983 TRANSITIONED PROGRAM TO
SCHWEIZER AIRCRAFT
1958 U.S. ARMY PURCHASED 5
PRE-PRODUCTION MODELS
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1984 FACTORY PRODUCED
INSTRUMENT TRAINER
1961 FIRST PRODUCTION
HELICOPTER CAME OFF THE
LINE
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1988 330 PROTOTYPE FIRST FLIGHT
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1992 MODEL 330 FAA CERTIFICATION
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1995 MODEL 300CB FAA CERTIFICATION
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1997 MODEL 330SP CERTIFIED
1955 WORK BEGUN ON 269 CONCEPT
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1956 269 PROTOTYPE
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1964 U.S. ARMY ORDERED TWENTY
TH-55A’S
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1967 EIGHT HUNDRED TH-55A’S IN U.S.
ARMY INVENTORY
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1999 DELIVERED 750th SCHWEIZER
PRODUCED 300C
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1970 DEVELOPED MODEL 300C
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1980 DELIVERED 1000th MODEL 300C
2000 DELIVERED 3500TH 269 SERIES
HELICOPTER
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1981 DEVELOPED THROTTLE
GOVERNOR SYSTEM FOR 300C
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2000 CERTIFICATION OF MODEL 333
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1981 ELASTOMERIC MAIN ROTOR
DAMPERS INCORPORATED
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2005 1000TH SCHWEIZER PRODUCED
HELICOPTER
300C WORLD’S BEST
PISTON-POWERED TRAINER
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TO DATE, OVER THREE THOUSAND SEVEN HUNDRED
AIRCRAFT PRODUCED
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U.S. ARMY’S STANDARD TRAINER AT FT. RUCKER
AVIATION CENTER - 1964 THRU 1988
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TRAINER USED BY 24 GOVERNMENTS THROUGHOUT
THE WORLD
U.S. ARMY EXPERIENCE
30 DAY PERIOD - 1980
FT. RUCKER EXPERIENCE
• 137 A/C USED
• 4 MILLION TOTAL HOURS ON U.S.
ARMY FLEET
• 8,621 TOTAL FLIGHT HOURS
• 55,000 PILOTS TRAINED
• 57,880 LANDINGS
• 27,759 AUTOROTATIONS
• 1,800 STUDENTS AND 110,000
FLIGHT HOURS IN 1987
• OVER 12,000,000 TOUCHDOWN
AUTOROTATIONS
• ONLY 1 CATEGORY “A” ACCIDENT
SINCE TRAINING BEGAN AT FT.
RUCKER (1972)
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TYPICAL 269C HELICOPTER
360-DEGREE VISIBILITY
WINDSHIELD
THREE PLACE
INTERIOR
32.5 GALLON
FUEL CAPACITY
FULLY ARTICULATED THREE
BLADED MAIN ROTOR SYSTEM
INTERCHANGEABLE BLADES
TAIL ROTOR
TRANSMISSION WITH
BEVEL GEARING AND
INTEGRAL OIL SUPPLY
ONE-PIECE TAIL ROTOR
DRIVE SHAFT - NO
INTERMEDIATE BEARINGS
CONSOLEINSTRUMENTSINTREGAL LIGHTING
TAIL ROTOR
FIBERGLASS
BONDED TO
STEEL SPAR
LIGHTWEIGHT TUBULAR
STEEL FRAME
SPIRAL BEVEL GEAR MAIN
TRANSMISSION WITH
INTEGRAL OIL SUPPLY
VERTICAL STABILIZER
FOR ENHANCED
DIRECTIONAL STABILITY
WIDE-ACCESS DOORS
HYDRAULIC
SHOCK-MOUNTED
SKID GEAR
LYCOMING FUEL-INJECTED
ENGINE; ELECTRIC FUEL
BOOST PUMP;
THERMOSTATIC OIL BYPASS;
TWO STARTING VIBRATORS
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BELT DRIVE SYSTEM-POSITIVE
ENGAGEMENT AND DISENGAGEMENT;
ALLOWS ENGINE OPERATION WITHOUT
ROTORS TURNING
TAIL SKID FOR
TAIL ROTOR PROTECTION
HIGH PERFORMANCE
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95 MPH CRUISE SPEED
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1,000 LB USEFUL LOAD
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SMOOTH, COMFORTABLE RIDE
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3 PLACE, PLUS CARGO
“DESIGNED-IN” SAFETY FEATURES
• FIXED STATIC MAST FOR ROLL-OVER PROTECTION
360 DEGREE
VISIBILITY
• FAIL SAFE ROTOR DESIGN
• SEPARATE DRIVE SHAFT
ROTOR
IMPINGEMENT
OUTSIDE
CREW ENVELOPE
BREAKAWAY
FUEL TANK
DIRECT FLIGHT
CONTROLS
• NO HYDRAULICS
STRUCTURALLY ENHANCED
SADDLE FITTING
ENERGY ABSORBING
CRUSHABLE STRUCTURE
LOW, AFT MOUNTED
ENGINE
SHOCK ABSORBING,
LANDING GEAR
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LOW MAINTENANCE
ALL METAL 3-BLADED
MAIN ROTOR WITH
ARTICULATED HUB
FOAM AND OILED FILLED SPLIINED M/R DRIVE
SHAFT
HIGH TIME-LIFE COMPONENTS
THROUGHOUT
ELASTOMERIC M/R BEARINGS
ELASTOMERIC T/R
BEARINGS (OPTIONAL)
INSTRUMENT PANEL
EASILY REMOVABLE
ONE PIECE UPPER PULLEY
HUB; IMPROVED COATINGS
EXTENDED
TAILBOOM LIFE
ONE-PIECE
TAIL ROTOR DRIVESHAFT
CHADWICK PLUG ON
INSTRUMENT PANEL
SINGLE TRANSMISSION
2 GEARS
WIDE, EASY ACCESS:
EASILY REMOVABLE
DOORS
IMPROVED ABRASION
STRIPS
LIGHTWEIGHT, RUGGED
TUBULAR STEEL FRAME
NEW CHIN SKINIMPROVED
MAINTENANCE
ACCESS
OIL FILLER - EASILY ACCESSIBLE
225 HP ENGINE
190 HP FLAT RATED
MOUNTED HORIZONTALLY
BRONZE-CARBIDE
SKID SHOES
IMPROVED DAMPER SEALS
LIGHT WEIGHT STARTER
50 HOUR OIL CHANGE
Easy Access for Inspection and Servicing of ALL Dynamic System Components
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SCHWEIZER MODEL 300C
HELICOPTER & INSTALLED COMPONENTS
BASIC ACCESSORIES
Upstack With Noise Diffuser
Muffler
Paravion Heater System
Auxiliary 64 Gallon Fuel System
Ground Handling Wheels
Map Case
Safety Kit
Triple Latch Locking Doors
AVIONICS
King-Complete Line
Emergency Locator Transmitter
IFR Avionics Suite
Garmin GPS
David Clark Headset & Boom Mike
Blind Encoder
Intercom Floor Switch
INSTRUMENT PANEL OPTIONS
Small Profile Panel
Intermediate Panel
Full Panel
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LAW ENFORCEMENT OPTIONS
Search Lights
P.A./Siren System
FLIR/TV Sensor & Controls
Radio/Intercom/P.A. Mixer
130 Amp Alternator
UTILITY & CONVENIENCE OPTIONS
Utility Float Kit
ENG Configuration
High Stance Landing Gear
Columbia Cargo Rack (1)
Protective Cover, Waterproof
Mesh Seat Kit (2 Seats)
Heavy Duty Skid Shoes
Hartzell Overspeed Governor
Cargo Hook
Agricultural Spray Equipment
Start-Up Overspeed Control Unit
OPTIONS
POLICE RADIOS & SEARCHLIGHTS
CARGO HOOK
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FLOATS
HIGH STANCE LANDING GEAR
SPARE PARTS AND PRODUCT SUPPORT
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WARRANTY - 1000 HOURS OR ONE YEAR
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SPARES SUPPORT
AOG - 24 HOUR SERVICE - 99.9% OF PARTS SHIPPED SAME DAY
ROUTINE ORDERS - 3-4 DAYS IN 92% OF CASES
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FACTORY TRAINING
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SPARES INVENTORY AT SERVICE CENTERS & FACTORY
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TECH REPs - PERIODIC VISITS
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TECHNICAL SUPPORT AT FACTORY
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PUBLICATIONS
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EXCHANGE PROGRAM