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Check maintenance records, check general condition - leaks, discolorization dents, chafing, nicks, corrosion or cracks. Verify Telatemps show no unexplained temperature increases during prior flight. Cowl Door Master switch On Oil pressure, alternator, governor lights, low fuel On Warning light test switches Push to test Fuel quantity Rotor brake Actuation normal Master switch Off Aux fuel tank quantity Fuel filler cap Tight Aux fuel tank No leaks Aux fuel drain Sample Gearbox oil Full, no leaks Gearbox Telatemp Normal Flex coupling No cracks, nuts tight Yoke flanges No cracks Sprag clutch No leaks Static source Clear Control rod ends Free without looseness Steel tube frame No cracks All fasteners Tight Tail rotor control No interference Cowl door Latched Engine Right Side Carb air ducts Secure Carb heat scoop Secure Engine sheet metal No cracks Electrical terminals Tight Fuel line No leaks Oil cooler door Oil lines No leaks or chafing Exhaust system No cracks Engine general condition V-belt condition V-belt slack Sprag clutch No leaks Upper bearing No leaks Telatemp – upper bearing Normal Lower sheave groove wear Smooth & uniform Flex coupling No cracks, nuts tight Yoke flanges No cracks Steel tube frame No cracks Tail rotor control No interference

Engine - Rear Cooling fan nut Pin in line w/ marks Cooling fan No cracks Fan scroll No cracks Telatemps – lower bearing Normal Lower bearing No leaks Empennage Tail surfaces No cracks Fasteners Tight Position light Tail Rotor Gearbox Telatemp Normal Gearbox Oil full, no leaks Blades Clean & no damage/cracks Rod ends Free without looseness Pitch link jam nuts Tight Teeter bearings Teeter bearing bolt Does not rotate Control bellcrank Free without looseness Tailcone Rivets Tight Skins No cracks or dents Strobe light condition Antenna Attachment bolts Tight

Engine - Left Side Engine sheet metal No cracks Exhaust system No cracks Engine oil 4-6 qts Fuel lines No leaks Gascolator drain Sample Throttle linkage Operable Battery & relay Secure Alternator belt tension Steel tube frame No cracks Engine general condition Fuel Tank (Main) Leakage None Quantity Filler cap Tight Drain Sample Main Rotor CAUTION – Do not pull rotor blades down as damage may occur. To lower one blade, push opposite blade up. Blades Clean & no damage/cracks Pitch change boots No leakage Main hinge bolts Cotter pins installed All rod ends Free without looseness Pitch link jam nuts Tight Pitch link safety wire Secure All fasteners Tight Swashplate scissors No excessive looseness Turn rotors 90° and level

Fuselage Left Side Baggage compartment Removable controls Secure if installed Collective control Clear Seat Belt Check condition & fastened Door Unlocked & latched Door hinge safety pin Installed Landing gear Ground handling wheel Removed Position light Nose Section Pitot tube Clear Windshield condition & cleanliness Fresh air vent Clear Landing lights Fuselage Right Side Landing gear Ground handling wheel Removed Position light Door hinge safety pin Installed Baggage compartment Cabin Interior Loose articles Removed or stowed Seat belts Instruments, switches, & controls CAUTION – Removable controls should be removed if person in left seat is not a rated helicopter pilot. CAUTION – When flying solo, fill left baggage compartment to capacity before using right baggage compartment. Avoid placing objects in compartments that might injure occupants if seat collapses during hard landing.. CAUTION – Shorter pilots may require cushion to obtain full travel of all controls. When using cushion, verify aft cyclic travel is not restricted. Notes: STAND BACK AND LOOK AT ENTIRE AREA!