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 FEATURESComplete 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.

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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.

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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

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BD-Micro.com

Wing Span 17.0 ft

Length 13.33/14.25 ft

Height 6.0 ft

Wing Area 37.8 sq ft

Width w/o Wings 4.0 ft

Horiz. Stab. Span 7.3 ft

Cabin Length 64 in

Cabin Width 23.5 in

Cabin Height 36 in

Empty Weight 416 lbs

Gross Weight 860 lbs

Useful Load 444 lbs

Fuel Capacity 30/46* U.S. Gal

* with Aux Fuel Tank

DIMENSIONAL SPECIFICATIONS

Max Thrust 265 lbs

Min SFC 1.10 lbs/lbt/hr

Start Time < 35 sec

Acceleration 75% To 95% < 6 sec

Oil Consumption 150 ml/hr max

Turbine Oil Type MIL-L-23699

Jet Fuel Type Jet A, JP4

Initial Cycle Life 600 starts

Power Output To Battery 720w (25a)

Max Re-light Altitude 26,000 ft

POWERPLANT SYSTEM SPECIFICATIONS

PERFORMANCE SPECIFICATIONS

6.0 (@ 720 lbs)

T.O. Distance 1,500 ft

Landing Distance 1,000 ft

Rate of Climb @ Sea Level 2,750 ft/m

Rate of Climb @ 12,500 ft 1,400 ft/m

Stall Speed (flaps @ gross wt) 65 KIAS

Endurance (no reserve) 1.5 to 2.5* hrs

Top Speed Vne 250 KIAS**

Cruise Speed (N1 @ 85%) 159 KIAS

270° /sec

+/ -

Max Roll

+/ - 9.0

Limit "G"

Ultimate "G"* with Aux Fuel Tank** Prelim Spec- Higher Speeds Capable

The Quantum Turbine Powerplant System for the FLS Microjet was designed around the PBS TJ100 turbojet engine. This high-tech engine features a compact and lightweight design, a modern FADEC control, and a high thrust to weight ratio. BD-Micro worked directly with PBS to further develop several engine safety features for this application.

In developing the Quantum Turbine Powerplant System for the FLS Microjet, primary goals were safety and reliability. To that end, extensive resources were dedicated to design and testing. Several rounds of revision were completed before we were satisfied with the results.

POWERPLANT SYSTEM

1260 Wade RdSiletz, OR 97380 USATel/Fax 541-444-1343Email: Sales@BD-Micro.com

BD-Micro Technologies, Inc.

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FADEC (Full Authority Digital Engine Control).

Fuel & Lubrication Systems Fully Self-Contained.

Brushless Induction Starter/Generator.

Fully Automatic Start-Up/Shut-Down Operation.

No Outside Power Source Required For Startup.

High Thrust To Weight Ratio.

Dual Fuel Pumps (Dual Feed @ >96% RPM).

Manual Emergency Fuel Shutoff.

Inverted Fuel System.

Microcontrolled Throttle Unit- Emer Backup Control.

Dedicated Electrical Bus.

More Features Too Numerous To List.

POWERPLANT SYSTEM FEATURES