Cessna 172s full training pilot course step by step,

 WELCOME ADVANCE FLYING ACADEMY 

ROBINSON R22 FULL PILOT TRAINING COURSE STEP BY STEP 

FUEL SYSTEM

The fuel system is gravity-flow (no fuel pumps) and includes a main tank, an optional auxiliary tank, a shutoff valve control located behind the left seat, and a strainer (gascolator). Fuel tanks on later aircraft have flexible bladders in aluminum enclosures while earlier aircraft use all-aluminum tanks. Fuel tank air vents are located inside the mast fairing. Plunger-style drain valves are provided for the gascolator and for each fuel tank sump. The gascolator is located on the lower left side of the firewall. The drain valves for the auxiliary tank and bladder-style main tank are located inside the cowl door below the auxiliary tank. Plastic tubes attached to the valves allow fuel to be drained overboard. 

Fuel samples are taken by pushing on the plunger(s). For all-aluminum main tanks, the drain is located on the left side of the fuselage and is opened by pushing in on the plastic tube. Fuel should be sampled from all three locations prior to the first flight of the day and after refueling to verify no contamination and correct grade.

The fuel gages are electrically operated by float-type transmitters in the tanks. When the gages read E the tanks are empty except for a small quantity of unusable fuel. The low fuel caution light is actuated by a separate electric sender located on the bottom of the main tank.

The auxiliary tank is interconnected with the main tank and is located somewhat higher so it will become empty first while fuel still remains in the main tank. The fuel shutoff valve controls flow from both tanks to the engine.

CLICK 👉 ROBINSON R22 HANDBOOK  

CLICK 👉 PREFLIGHT INSPECTION 

CLICK 👉 BEFORE STARTING ENGINE

CLICK 👉 STARTING ENGINE AND RUN-UP

CLICK 👉 SHUTDOWN PROCEDURE

CLICK 👉 FLIGHT AND MANEUVER LIMITATIONS

CLICK 👉 KINDS OF OPERATION LIMITATIONS

CLICK 👉 FUEL LIMITATIONS

CLICK 👉 POWER FAILURE - GENERAL

CLICK 👉 POWER FAILURE ABOVE 500 FEET AGL

CLICK 👉 POWER FAILURE BETWEEN 8 FEET AND 500 FEET AGL

CLICK 👉 EMERGENCY WATER LANDING – POWER OFF

CLICK 👉 EMERGENCY WATER LANDING – POWER ON

CLICK 👉 ROTOR SYSTEMS

CLICK 👉 DRIVE SYSTEM

CLICK 👉 POWERPLANT

CLICK 👉 FLIGHT CONTROLS

CLICK 👉 REMOVABLE FLIGHT CONTROLS

CLICK 👉 RPM GOVERNOR

CLICK 👉 CONTROL TRIM AND FRICTION

CLICK 👉 ENGINE CONTROLS

CLICK 👉 CLUTCH ACTUATOR

CLICK 👉 FUEL SYSTEM

CLICK 👉 ELECTRICAL SYSTEM

CLICK 👉 LIGHTING SYSTEM

CLICK 👉 AUDIO SYSTEM

CLICK 👉 OPTIONAL AVIONICS

CLICK 👉 PITOT-STATIC SYSTEM

CLICK 👉 DUAL TACHOMETER

CLICK 👉 WARNING AND CAUTION LIGHTS

CLICK 👉 CABIN HEATING AND VENTILATION

CLICK 👉 SEATS, BELTS, AND BAGGAGE

CLICK 👉 LANDING GEAR

CLICK 👉 ROTOR BRAKE

CLICK 👉 ENGINE PRIMER SYSTEM

CLICK 👉 CARBON MONOXIDE DETECTOR

CLICK 👉 EMERGENCY LOCATOR TRANSMITTER

CLICK 👉 OPTIONAL ACCESSORY MOUNTS

CLICK 👉 REQUIRED DOCUMENTS

CLICK 👉 REQUIRED INSPECTIONS

CLICK 👉 GROUND HANDLING

CLICK 👉 PARKING

CLICK 👉 CABIN DOORS

CLICK 👉 TAIL ROTOR GEARBOX OIL

CLICK 👉 BATTERY

CLICK 👉 CLEANING HELICOPTER

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