FLS MICROJET FEATURES BD-Micro Technologies, Inc. ▪ 541-444-1343 ▪ www.BD-Micro.com Following a multi-year development and modernization program, we are proud to introduce our next generation FLS Microjet. In this development effort, objectives focused on providing a high level of quality, with an emphasis on safety and reliability. This newest version of the FLS Microjet has come a long way, as evidenced by a comprehensive high-end features list. Highlights include a modern turbine powerplant system, all glass panel, solid state electrical system, HOTAS controls, GPS navigation, systems redundancy, and more. The following lists highlight many of the features included with the all new FLS Microjet. FLS MICROJET FEATURES Complete Advanced Kit Including Powerplant System, Avionics and Builder Assist Program. Technology Integration With Focus On Systems Reliability and Reduced Pilot Workload. Compound Curved Aluminum Monocoque Construction. Removable Wings With Indexed Flap & Aileron Controls. Improved Wing Design Dramatically Improves Stall Characteristics. Strengthened Wing Spar to Reduce Airframe Fatigue and Maintain Airfoil Integrity. Inverted Fuel System for Aerobatic Maneuvers. Fuselage Stretch Enhances CG And Isolates Main Gear Retract Mechanism From Cockpit for Safety. Detachable Horizontal Stabilators (All Flying Tail). NACA Style Jet Engine Intake Scoops With Back Flow Doors. Attenuator (Thrust Reverser) With Throttle Lever Lockout. Wrist Action Side Stick Control (As In Modern Day Fighters). Retractable Landing Gear (One Second Cycle Time). Oleo Nose Strut. 1 1 1 1 1 1 1 1 1 1 1 1 1 1 Automatic Flap Positioning System With EFIS Position Display. Electrically Actuated Two Speed Anti-Servo Tab (Trim Tab) With EFIS Position Display. Capacitance Fuel Level Indication System (3 Channel With EFIS Display). Audio Gear Up Warning System. Low Drag Self-Contained Led Synchronized Strobe and Position Lights. Angle-Of-Attack Vane Mounted On Extended Pitot Tube. 3 Position Hartwell Canopy Latch System. Fuel No-Drip Quick Connects Aid Wing Removal. Several Items for Ease of Maintainance and Enhanced Serviceability. Professional Grade Features in a Clean and Tightly Integrated Package. Optional Smoke System for Airshow Performances. Optional Extended Range Internal Fuselage Fuel Tank. Optional Integrated 2 Axis Autopilot. 1 1 1 1 1 1 1 1 1 1 1 1 1 AVIONICS & ELECTRICAL A key feature of the FLS Microjet is its avionics package and solid state electrical system. Our effort in integration design and component selection has paid off by providing extensive capabilities in a clean format, thus enhancing cockpit resource management. The various avionic components were selected for size, reliability, operating features, and systems integration along strict design and performance criteria. The result rivals capabilities found in commercial airliners. Grand Rapid Technologies Horizon System Features: Primary Flight Data, Moving Map, and Graphical Engine Data. Sunlight-Readable, Wide-Temperature Range Display. XM Satellite Weather option. HSI, Arc View, and Weather Maps. Highway-in-the-Sky Integrated Navigation/Attitude Display. Multiple Display Units provide Redundancy and Functionality. Dual AHRS and Dual Magnetometers. Convenient USB Memory Stick for Software Loading. Database Updates and Data Logging. Split Screens, customizable to pilot preferance. Operating Temperature -15° to +160° F. Attitude Sensor Package (AHRS) Features: Attitude Solution Independent of GPS or Pitot/Static. Suitable for IFR Primary Attitude Reference. Dedicated Processor for Reliability. Fully Functional During Aerobatics. Continuous Self-Test. Gyro-Stabilized Slaved Magnetic Heading. All axis 200°/sec; Pitch and Roll Range Unlimited. Airspeed Range 50 to 580 mph. IFR Accuracy -1,000 to +35,000 ft. Trig Mode S Transponder (Built-In Encoder). Garmin SL-30 Nav/Com. GPS, ILS, VOR Navigation. 10 Channel Audio Mixer. Tone Annunciator. Dimmable LED Indicator, Warning, and Annunciator Lights. AOA Featuring Military Style Chevron Display. Solid-State Triple Bus Redundant Electrical System (No Mechanical Circuit Breakers). HOTAS (Hands On Throttle And Stick) Controls. Complete 24 vdc Electrical System. Ability to Save Flight and Engine Performance Data to USB. Memory Sticks. Xfer to Spreadsheet For Trend Analysis. Microcontrolled Throttle Unit With Independant Graphical Display for Engine Prestart Systems Check, Engine Operating Mode and Status. Secondary Throttle Control Capability In Case Of Primary Throttle Failure. Alternate Stand Alone Engine Display for % RPM and EGT. All Digital Dual EFIS Display Instrument Panel Integrated Equipment/Features 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1