FSI LOGO Revision 1.0
HELICOPTER OPERATIONS
MODERN HELICOPTERS
MODERN HELICOPTERS
MODERN HELICOPTERS
MODERN HELICOPTERS
HUMS Ground Station Overview Health and Usage Monitoring System Ground Station Help System Pre-Flight Procedures Initializing a DTMU Card Post-Flight Procedures Downloading a DTMU Card Downloading from Other Sources Maintenance Debrief Rotor Tuning Procedures Vibration Diagnostics Mechanical Diagnostics Strip Chart Data Analysis Operation Explorer Generic Trending Reports Data Export Administration User Security Configure Tasks Configure Menu Aircraft Configuration Data Management.
Operators Off Shore Air Taxi Corporate Military State Government State Police Air Ambulance Fire Fighting SAR
Specialty Helicopter S-92 Rescue Hoist
Specialty Helicopters
Specialty Helicopters
Specialty Helicopters
Specialty Helicopters
Specialty Helicopters
HELICOPTER STRUCTURES S-76 C++
Aircraft Zones
Cockpit / Cabin Zone 1
Tailboom / Landing Gear Zone 2 Tailboom Fire Bottles AC Junction Box RCCB s DC Junction Box Landing Gear
Tail Rotor Pylon Zone 3 Tail Rotor Horizontal Stabilizer Tail Rotor Gearboxes Tail Rotor Driveshafts
Powerplant Zone 4 Allison 250-C30 TurboMeca Arriel 1S1 / 2S1 Pratt & Whitney PT6B-36B
Main Rotor / Flight Controls Zone 5 Flight Controls M/R Hub & Blades Main Transmission Hydraulics
Aircraft Systems Electrical Power Fuel Hydraulics Landing g Gear Flight Controls Powertrain Rotors Powerplant Floats Autopilot
TYPES of HELICOPTER ROTOR SYSTEMS Conventional, Tandem and Counter, Rotating Rotor Systems
Conventional Helicopter
Rotorhead Components Control Horn Pitch link MRB Swashplate Mast
Rotorhead Components
Drive system (Conventional)
Engine Inlet
BARRIER FILTER
ENGINE INSTALLATION
ENGINE INSTALLATION
MAIN GEAR BOX AND ROTOR HEAD ASSEMBLY
Accessory Gearbox
Tail Rotor Drive Shaft
INTERMEDIATE GEAR BOX
Tail Rotor Assembly
ROTOR BRAKE
TORQUE COMPENSATION
LATERAL LEAD
STABILATOR AIRFLOW - HOVER
STABILATOR AIRFLOW - INFLIGHT
TAIL PYLON AERODYNAMICS
NOTAR NOTAR
NOTAR
Helicopter Controls Cyclic
PITCH FLIGHT CONTROLS BLOCK DIAGRAM
ROLL FLIGHT CONTROLS BLOCK DIAGRAM
Helicopter Controls Collective
COLLECTIVE FLIGHT CONTROLS BLOCK
Yaw Pedals Helicopter Controls
YAW FLIGHT CONTROLS BLOCK DIAGRAM
FLIGHT CONTROLS SYSTEM COMPONENTS
TAIL ROTOR CONTROL CABLES
HYDRAULIC SYSTEM COMPONENTS
Tandem Helicopter
TANDEM ROTORS
Drive system (Tandem)
Combining Transmission Transmission i
Accessory Module Accessory Modules
Tandem Helicopters Hover Turn Sideward
COUNTER ROTATING
TYPES OF ROTOR SYSTEMS
ROTOR SYSTEMS Lynx A Star A Star
Fully Rigid BK-117
Semi-Rigid Bell Jet Ranger
Fully Articulated S-76
Fully Articulated MRB Damper Reservoir Bifilar Vibration Absorber Elastomeric Bearing Control Horn Damper
Elastomeric Bearings Droop Stop
Spindles ¾ Steel Bolt Outer Race Plastic Collar Inner Race
INSPECTION OWL
FLOATS
Floats
Floats
Float Bottle
Float Bottle
Inflated Floats
Floats
FlightSafety International MAIN ROTOR BLADE CONSTRUCTION
FlightSafety International BLADE INSPECTION METHOD (BIM)
FlightSafety International Blade Construction
FlightSafety International Blade Construction
FlightSafety International Blade Construction
FlightSafety International Blade Construction
FlightSafety International Blade Construction
FlightSafety International MEASURED STATION STA STA STA STA STA STA 30.0 60.0 140.0 200.0 260.0 300.0 (SEE NOTE 4) ZONE 1 ZONE 2 ZONE 3 ZONE 4 15" 12" 9" 6" 0" D C B A D C B A 15" 12" 9" 6" 0" D C B A D C B A 10" BLADE STA 235.0 NOTES 1. REINFORCED PLASTIC (0.090) INCORPORATES 6. ALL SHEET METAL CALLOUTS DEICING BLANKET. ARE 6061-T6 ALUMINUM ALLOY, QQ-A-250-11. 2. COMPOSITE MADE FROM GLASS FABRIC AND A -BASIC SKIN (0.063) REDUCED GRAPHIC PLIES, BONDED WITH ADHESIVE TO 0.033-0.043 INCH THICKNESS. RESIN. B EXAMPLE -BASIC SKIN (0.063) REDUCED TO 3. INCORPORATES BIM BLANKET. 0.018-0.023 INCH THICKNESS. DAMAGE 10 INCHES TO FRONT 4. REPAIRS INBOARD OF ZONE 1 (STATION 60.0) 7. ON TIP CAP 70150-09107-049. OF TRAILING EDGE AT BLADE DO NOT NEED TO BE RECORDED. REPAIRS STA 235.0 IS IN ZONE 3C. IN THIS AREA WILL NOT AFFECT CHORDWISE 8. CRACKS ARE USUALLY FOUND AT OR SPANWISE BALANCE. HOLES 4 AND 5; 1/2 INCH OUTBOARD OF HOLE 6; BETWEEN HOLES 6 AND 7, 1 5. HELICOPTERS WITH BLADES SERIAL NOS INCH AFT OF HOLE 6. A007-02550 TO A007-02900 WILL HAVE A NOTCH IN TRIM TAB.
FlightSafety International ERROSION
FlightSafety International ERROSION
MRB Skin Disbond
Trailing Edge Delamination
Tail Rotor
TRB Spar Delamination
TRB Spar Delamination
Tail Rotor Failure
Blade Damage
Completed Repair
Sikorsky k X-2 THE FUTURE
PROTOTYPE HELICOPTER Sikorsky k X-2 287 MPH Fly by Wire Twin Rotors Pusher Propeller
THE FUTURE AUTO PILOT Oil Rig Landings SAR Grids FLY BY WIRE Flight Controls
TRAINING TOPICS Rotorcraft Aerodynamics Rotor Systems Structures Rotor Blades Flight Controls Hydraulics Floats Hoists
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THE END Fred Banke FlightSafety International