| SUBJECT |
HOURS |
| AIRCRAFT |
1.0 |
| General Description |
|
| Airframe and Engines |
|
| ENGINES |
3.0 |
| Engine Description |
|
| Temperature Limitations |
|
| Thrust Limitations |
|
| Fuel Control |
|
| Power and Compressors |
|
| Free Turbine Principal |
|
| Accessory Section |
|
| Engine Controls |
|
| Power Levers |
|
| Reverse Levers |
|
| Fuel Levers |
|
| Engine Instuments |
|
| Fan N1% |
|
| ITT Gauges |
|
| Turbine N2% |
|
| Fuel Flow Gauge |
|
| Oil Pressure Gauge |
|
| Oil Temperature Gauge |
|
| Starting Procedures and Limits |
|
| Hot Starts |
|
| Hung Starts |
|
| Starter Limitations |
|
| Engine Clearing Procedures |
|
| Bypass Ratio |
|
| Ignition System |
|
| Auto Igniters System |
|
| ITT Probes |
|
| Fuel Nozzles |
|
| Air Induction System |
|
| Ice Protection System |
|
| Air Flow |
|
| Engine Fuel System |
|
| Oil-to-Fuel Heater |
|
| Engine Oil System |
|
| Quantity |
|
| Tank and Location |
|
| Oil Reading |Hot-Cold |
|
| Fire Detection and Extinguishing |
|
| Auto Ignition System |
|
| Arming System |
|
| Recommended Uses |
|
| PREFLIGHT & NORMAL PROCEDURES |
3.0 |
| Aircraft Preflight |
|
| Before Starting Engine |
|
| Starting Engine |
|
| Before Taxiing |
|
| Taxiing |
|
| Engine Run-up Testing |
|
| Before Take Off |
|
| Line Up and Take Off |
|
| After Take Off |
|
| Climb Power Set Limitations |
|
| Cruise Power Set |
|
| Descent Checklist |
|
| Before Landing Checklist |
|
| After Landing |
|
| Shutdown Checklist |
|
| LANDING GEAR & BRAKES |
1.5 |
| Hydraulic Landing Gear |
|
| Electrical Landing Gear |
|
| Components |
|
| Normal Operation and Safety |
|
| Emergency Systems | Operations |
|
| Brake System |
|
| Componenets |
|
| Parking Brake |
|
| Limitations |
|
| FUEL SYSTEM |
1.5 |
| Tanks |
|
| Location and Type |
|
| Vent System |
|
| Indicating System |
|
| Pumps |
|
| High Pressure Pump Orientation |
|
| Boost Pumps Orientation |
|
| Standby Pumps Orientation |
|
| Normal | Crossfeed Operations |
|
| Fuel Additives |
|
| Cold Weather Operations |
|
| ELECTRICAL SYSTEM |
1.5 |
| Battery |
|
| Lead Acid | Nicad Description |
|
| Power Distribution & Control |
|
| Cross Generator |
|
| Start Assist Procedures |
|
| Normal Operations |
|
| Emergency Operations |
|
| External Power Procedures |
|
| Monitoring System |
|
| Annunicator Lights |
|
| Volt | Ammeter |
|
| Avionics Emergency Busses |
|
| Lighting |
|
| Internal | External |
|
| Annunciator Panel Lighting |
|
| ENVIRONMENTAL SYSTEMS |
1.0 |
| Air Distribution; Heating | Ventilation |
|
| Heating Electrical |
|
| Heating Bleed Air |
|
| Heating Combustion Heaters |
|
| Heating Operations & Limits |
|
| Pressurization System |
|
| Safety Valve Control |
|
| Outflow Valve Operation|Test |
|
| High Altitude Physiology |
|
| Air Conditioning System |
|
| Oxygen System & Operation |
|
| EMERGENCY PROCEDURES |
2.0 |
| Loss of Power Procedures |
|
| Electrical System Maintenance |
|
| Fuel System Control | Crossfeed |
|
| Avionics Bus Failure |
|
| Instrument Failure & Procedure |
|
| Landing Gear System Failure |
|
| Pressurization Emergency Procedure |
|
| Split Flap System & Checks |
|
| Spins |
|
| Alternate Static System |
|
| FLIGHT CONTROLS |
1.0 |
| Ailerons |
|
| Aileron Trim |
|
| Elevator & Trim (Emergency) |
|
| Rudder & Rudder Trim |
|
| Flap System and Limitations |
|
| Nose Wheel Steering |
|
| Stall Warning System |
|
| Limitations |
|
| FLIGHT INSTRUMENTS |
1.0 |
| Pilot Static System |
|
| Vacuum | Pressure System |
|
| Engine Instruments |
|
| Flight |
|
| ANTI-ICE | DE-ICE SYSTEMS |
1.0 |
| Anti-Ice |
|
| Pilot Heat |
|
| Stall | Vent Heat |
|
| Ice Vanes | Lip-Ice Boots |
|
| Windshield Heat |
|
| De-Ice |
|
| Surface De-Ice System |
|
| WEIGHT & BALANCE |
2.0 |
| Efects of Weight & Balance on C.G |
|
| Aircraft Forms |
|
| Determining Weight & Balance |
|
| Sample Problems |
|
| Performance |
|
| Explanation of Tables |
|
| Interpreting Charts |
|
| Practical Exercise |
|
| Single Engine Performance Charts |
|
| Review FAR 23.149 |
|
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|
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