ONE-BCnF Build Certify n’ FLY!

1. ONE-BCnFBuild Certify n’ FLY! Systems Team Preliminary Design Review

2. Updated Schedule Aug Nov Sep Oct May-Jun Sep 2010 2011 2012 • Select Teams Train Teams • Purchase Kit • Kit Delivery Build Tail Build Wings Build Fuselage Final Assembly Systems Installation Flight Test • Certification NOW BOEING PROPRIETARY

3. Fuel System Fuel Quantity Indication Indicates Electrical Connection F ------ E Fuel Quantity Indication F ------ E Filler cap Filler cap Tank Vent Tank Vent Wing Tank Fuel Sender EI Fuel Sender EI Filler cap Header Tank Tank Vent Fuel Sender Princeton Fuel Selector Andair Fuel Pump Switch Boost/Auxiliary Pump Andair Fuel Flow Indication Throttle Mixture Fuel Filter Andair Gascolator Andair Firewall Engine Pump Fuel Injection Engine Nozzles BOEING PROPRIETARY

4. Fuel System System Components choice • Fuel Sender/Level Probe • Header Tank: Princeton Capacitive Probe • Compatible with Dynon Skyview • Wing Tank: Electronics International Capacitive Probe • Two probes, running from each wingtip to the center of the tank • Sum the readings from each to get accurate tank quantity at all flight attitudes • Boost/Auxiliary pump, fuel filter, gascolator, selector valve • Andair Fuel Pump Kit • Designed for IO-360 engines • Comes with bracketry and bulkhead fittings • Vents • Using Glasair float valves in wing • Using custom routing for header tank vent BOEING PROPRIETARY

5. Electrical System • Aux Fuel Pump • Interior Lights • Exterior Lights • Autopilot • Flap Motor • Power Outlet BATT BUS Essentials Switch Avionics Switch ESSENTIALS BUS Standby Alt MAIN BUS AVIONICS BUS • Pitot Heat Starter / Magneto Switch Main Alt BOEING PROPRIETARY

6. Electrical System • Fault Tolerance: • System was designed to protect all components • All components will have a circuit breaker • Essentials Bus architecture • Provides redundant power to critical flight systems • Avionics Bus architecture • Provides redundant power to avionics • Backup batteries • Individual critical systems provided with a backup battery • Split Master Battery/Alternator Switch • Traditional switch to isolate alternator from system • Traditional switch to isolate most electrical items from battery • Augmented by essentials switch BOEING PROPRIETARY

7. Avionics System • Overview (cont’d) • Garmin SL-30 • COMM /NAV radio • Heated pitot / AOA probe • Whiskey Compass • 406 MHz ELT • Roll Axis Autopilot • Pitch-axis budget-permitting • Standby Instruments • Round-dial • Attitude, airspeed, altitude • NavWorx ADS600 • ADS-B In capability • FIS-B & TIS-B capability • Overview • Dynon Skyview • Primary Flight Instruments • Engine Instruments • CDI / Moving Map • Mode-S transponder (ADS-B Out) • Garmin GMA240 • Intercom functionality • COMM Panel • Aux audio input • Garmin GTN650 • COMM/NAV Radio • WAAS-certified GPS signal • Touch-screen interface BOEING PROPRIETARY

8. Avionics System • Dynon Skyview BOEING PROPRIETARY

9. Avionics System • Other Systems Integrated into Skyview • Synthetic Vision • Flap setting display • Fuel tank quantity indication • Fuel flow / fuel totalizer • Electrical system monitoring • Alternator & battery voltage & current • Canopy secure indication • AOA / stall warning • G-meter • Sky-view is an expanding system • Additional inputs available for other aircraft indications • Working on integrated COMM / NAV radios • Working on XM weather & ADS-B In FIS-B weather • Fuel Leaning Assist • Flight time meters (hobbs/tach) • Warning indications • Traffic display (TIS-B) BOEING PROPRIETARY

10. Avionics System • Instrument Panel Preview BOEING PROPRIETARY

11. Avionics System • Fault Tolerance: • Designed for redundancy in critical systems • Attitude/airspeed/altitude information • Skyview ADAHRS primary / round-dial backup • NAV information • GTN650 primary (GPS & NAV radio) / Skyview GPS backup / SL-30 backup (NAV radio) • COMM radio • GTN650 primary / SL-30 backup • Avionics Power • Powered through Main Bus & Essentials bus • Skyview system & standby attitude indicator equipped with backup batteries • Standby alternator BOEING PROPRIETARY

12. Other Systems • Exterior Lights • LED powered for NAV • HID for Landing • Alternate Air • Cabin Heat • Brakes: • Looking into replacing Glasair brakes • Will have a parking brake • Engine • 180hp IO-360 • Purchase next year for budgeting • Lean-of-peak operations equipped • Wingtip Extensions • Electric Flap • Working on Boeing-style flap detent system • Interior Lights • LED powered • White for boarding, red for in-flight BOEING PROPRIETARY

13. Cabin System • Current Status: • Completing interior Mock-up • Includes panel, center console, and seats • Next Steps: • Spatial Integration • Interior Mock-up and cardboard models will be used to ensure the Panel/Center Console, Seat/Side Walls, and Overhead areas are usable and sensibly located. • Test Spatial Integration • Get feedback from pilot(s) who use the Interior Mock-up to run through scenarios/procedures • Industrial Design and Manufacturing Methods • Decide on types of materials, such as carpet, fabric and paint that will be used in the interior. Decide on manufacturing methods needed to install materials. • Choose the color scheme and general aesthetics, such as how accent colors will be used. • Detail Part Definition • Design the usable interior and mock up with foam or other prototyping materials. Come up with final part sizing and definition. • Model anything that will be needed for the manufacturing methods selected in Interior Design. BOEING PROPRIETARY

14. Questions and comments ? BOEING PROPRIETARY