| S | U | N/A | Item | Notes | |||||||
| Regulatory Prerequisites and Placards: | |||||||||||
| x | Has construction manual | None Provided, Replacement available | |||||||||
| x | ID plate is fireproof, and completed | Quicksilver Serial Number Plate present | |||||||||
| x | ID plate installed in proper location | ||||||||||
| x | N-number installed in 3" block letters in proper location | USUA Registration number on aircraft | |||||||||
| x | Weight and Balance done, and shows within designer limits | None provided, current W&B will be provided with sale. | |||||||||
| All controls, both flight and engine, marked as to use | |||||||||||
| x | Throttle, open/close | Not marked | |||||||||
| x | Fuel, on/off | ||||||||||
| x | Fuel quantity and type marked at each cap | Visual fuel quantity | |||||||||
| Cockpit and Interior: | |||||||||||
| x | Seat belts function | ||||||||||
| x | Seat belt anchor points firm, no interference | ||||||||||
| x | Seat and seat tracks OK, stops on aft rails | ||||||||||
| Instruments and Required Equipment: | |||||||||||
| x | Fuel Gauge, each tank, functions correctly | Visual | |||||||||
| x | Altimeter | ||||||||||
| x | Airspeed | ||||||||||
| x | Tach. Tach time: | ||||||||||
| x | Compass | None | |||||||||
| x | EGT | Dual | |||||||||
| x | CHT | Dual | |||||||||
| Hobbs | None. Reported 108 airframe, 30 engine (since rebuild, see note) | ||||||||||
| x | Anti-collision lights/rotating beacon | Single, Kingpost | |||||||||
| Electrical: | |||||||||||
| x | Electrical system wiring adequate size, and secure | ||||||||||
| x | Switches marked for operation and wired properly | ||||||||||
| Fuel System: | |||||||||||
| x | Caps fit, and vented on all tanks | ||||||||||
| x | Fuel drain installed at lowest portion of tank | Loop, as specified | |||||||||
| x | Fuel drain installed at lowest point in system | Loop, as specified | |||||||||
| x | Fuel vent system vented properly | Vented cap | |||||||||
| x | Shutoff valve/selector switch operates easily and is clearly marked | ||||||||||
| x | Fuel line routing is of proper material and diameter | ||||||||||
| x | Fuel filter installed | ||||||||||
| x | Fuel lines protected from chafing and secure | Some additional standoffs recommended. Easily accomplished. | |||||||||
| x | Fuel line routing avoids areas of heat | ||||||||||
| Gear, Wheels, Brake Systems: | |||||||||||
| x | Brake system lines routed correctly | ||||||||||
| General Condition, Fuselage, Wing, Tail Assembly: | |||||||||||
| x | Skin condition, wrinkles, rivets, tape | 2 small patches on wing skin (applied by U-FLY-IT) | |||||||||
| x | Vertical fin, movement and condition | ||||||||||
| x | Ailerons, movement and condition | Smooth. Tension could be relaxed slightly with minor adjustment to friction bolt | |||||||||
| x | Elevator assembly, movement and condition | ||||||||||
| x | Control travel stops | Rudder pedals have been trimmed slightly on corners to accommodate fairing. | |||||||||
| x | Control cables safety wired correctly | ||||||||||
| x | Windshield overall condition | Windscreen and fiberglass fairing in good condition | |||||||||
| x | Wing attach brackets and hardware | Some new hardware installed by U-FLY-IT | |||||||||
| x | Tail group attach brackets and hardware | Some new hardware installed by U-FLY-IT | |||||||||
| Flight Controls: | |||||||||||
| x | Proper tension of cables | ||||||||||
| x | Clearance on controls, no hitting panel, sides, floorboards | Rudder pedals do contact fairing at full deflection, but do not hinder rudder travel | |||||||||
| x | Freedom of movement | ||||||||||
| x | Proper direction | ||||||||||
| x | Rudder hinges, horns, and attachments | ||||||||||
| x | Aileron hinges, horns and attachments | ||||||||||
| x | Elevator hinges, horns and attachments | ||||||||||
| Engine Compartment: | |||||||||||
| x | Throttle cables anchored and functional | Routing of cable could be changed slightly. Carb end needs new rubber boot at cable ($3.50) | |||||||||
| x | Throttle defaults to open position | Rotax design, defaults to closed | |||||||||
| x | Choke cable anchored and functional | Primer system installed, functions correctly. | |||||||||
| x | Clearances in engine compartment | ||||||||||
| x | Fuel line routing to avoid heat and bends | ||||||||||
| x | Sufficient fuel line diameter | ||||||||||
| x | Fuel and oil hoses proper material | ||||||||||
| x | Engine mount secure, no cracks | ||||||||||
| x | Signs of oil leaks | ||||||||||
| x | Muffler/exhaust condition | Has Rotax intake silencer, Rotax intake filter and after muffler. All with good mounts and in good condition | |||||||||
| Propeller: | |||||||||||
| x | Prop nicks and/or cracks | Has adhesive leading edge tape. Very small knicks in L/E, easily dressed on carbon fiber props. | |||||||||
| x | Safety wired bolts of sufficient size | Self locking nuts, new prop bolts installed by U-FLY-IT | |||||||||
| x | Bolts clear engine | ||||||||||
| x | Prop is correct length to clear airframe | ||||||||||
| x | Hub has no cracks or corrosion | ||||||||||
| Notes: | |||||||||||
| Both landing gear down tubes are new, and so are both tensions struts. | |||||||||||
| Much hardware was replaced during our inspection. UV protection was | |||||||||||
| applied to the wings. The 2 small fabric tears were patched by U-FLY-IT. | |||||||||||
| Overall, a nice single place sprint with low time motor. As equipped, the | |||||||||||
| current replacement cost of this aircraft would be approximately $14,000 | |||||||||||