Shadin Avionics Product Families Fuel Flow Systems n

Shadin Avionics Product Families Fuel Flow Systems n Air Data Computers n Altitude Management n ETM n Converters n

Fuel Flow Systems n Digital systems designed to provide complete fuel management information under real flight conditions ¨ ¨ ¨ Miniflo-L Microflo-L Digiflo-L WARNING These products are fuel flow measuring systems and NOT a quantity-sensing device. Therefore, it cannot determine the amount of usable fuel in the fuel tanks. It is imperative that an accurate figure of usable fuel on board be entered into the system to ensure accurate readings.

Fuel Flow Systems n n Connected to the engine fuel flow transducer for fuel flow information with option to interface with GPS for navigational data via RS-232 or (RS-422 Digiflo-L only) serial port. Designed to measure the flow of fuel in either gallons, liters, pounds, or kilos, and it can be installed on virtually any reciprocating or turbine engine by selecting the proper size fuel flow transducer.

Fuel Flow Systems n Provides: ¨ Fuel flow ¨ Fuel used ¨ Fuel remaining ¨ Endurance ¨ Nautical miles per unit of fuel ¨ Fuel to destination ¨ Fuel reserve

Fuel Flow Systems n Provides: ¨ Specific Range – (NM/GAL) = Ground Speed (KTS/Fuel Flow) per hour. This is an indication of how efficient the cruise is and the optimum cruise speed can be determined by selecting the power setting, which yields the highest nautical miles per gallon/liters/pounds. ¨ Fuel to Destination - Calculates (under real wind conditions) the fuel necessary to reach the destination as selected on the Loran-C or GPS receiver by multiplying the fuel flow by the estimated time en route to the destination. (If an intermediate waypoint is selected for navigation purposes, the displayed fuel to destination represents the fuel needed to reach the intermediate waypoint unless the distance to the destination is in the serial message. ) ¨ Fuel Reserve - Calculates the amount of fuel which will be available on board when the aircraft reaches the destination or waypoint indicated on the Loran-C or GPS receiver. This feature provides the pilot with accurate information so that the reserve fuel situation can be evaluated and action can be taken if necessary. (If an intermediate waypoint is selected for navigation purposes, the displayed fuel reserve represents the fuel reserve at the intermediate waypoint unless the distance to the destination is in the serial message. ) Fuel Reserve = Fuel Remaining – Fuel to Reach Destination.

Fuel Flow Systems n Provides: ¨ ENDURANCE - Calculates the time left to fly in hours and minutes based on the fuel remaining and the present fuel flow. ¨ FUEL FLOW - The system provides a digital readout of the fuel per hour to a tenth of a gallon up to 100 gallons and to the nearest gallon above 100 gallons. For the pounds version, the readout is to the nearest pound up to 999 lbs. /hour and to the nearest 10 lbs. above 999 lbs. /hour. FUEL USED - The system keeps track of the fuel used since the last fuel entry or reset. ¨ FUEL REMAINING - The system keeps track of the fuel remaining on board. Fuel Remaining is equal ¨ to Initial Starting Fuel minus Fuel Used.

Fuel Flow Systems n System Components: ¨ Fuel Flow Transducer - The fuel flow transducer mounted in the fuel line measures the flow of fuel and generates electrical pulses directly proportional to the fuel flow. The transducer is fail-safe designed, and stopped rotor will not interrupt fuel flow to the engine. ¨ GPS Receiver - GPS receiver provides ground speed, distance, and estimated time en route through the serial port. ¨ Indicator/Controller - Panel Mounted Miniflo-L, Microflo-L, Digiflo-L Fuel Management indicator. Dislpays syetem information and allows page selection for requested data.

Fuel Flow Systems n Warnings provided by system: ¨ Not enough fuel - When the rotary switch is in FUEL TO DEST. position, the information in the ¨ Reserve Fuel will be used - With the rotary switch is in F. AT DEST. position, the information in ¨ Low Endurance - The Microflo-L can be configured to display a warning based on the time remaining ¨ Low Fuel Remaining - The system displays “Lo FUEL” when the fuel remaining reaches the pre- display window flashes if fuel on board is insufficient to reach either the destination selected as the active waypoint or the final destination (if that total distance record is provided in the serial message). Display window shows amount of fuel short to reach destination preceded by a negative sign. the display window flashes if the aircraft will arrive at the destination with less than the pre-programmed Endurance Warning Time minutes of fuel - calculated at the present cruise power setting. This warning is intended to alert the pilot that the prevailing condition will require the use of some of the selected reserve fuel to reach the destination. to fly. When the rotary switch is in the ENDURANCE position, and the actual endurance is less than the preprogrammed Endurance Warning Time, the data in the right half of the display flashes. Press the TEST/ENTER button to acknowledge the warning. (Note: Resetting the Microflo-L or adding fuel resets this condition and the warning is enabled again). programmed Low Fuel Level configured in setup. Fuel flow information will not be displayed again until the pilot acknowledges this word by pressing the ENTER/TEST button. Fuel calculations are not interrupted by this message. (Note: Resetting the Microflo-L or adding fuel resets this condition and the warning is enabled again).

Fuel Flow Systems n Compatible n n n n n Receivers ARNAV - R 15, R 20, R 21, R 30, R 40, R 50 V, R 50 i, R 5000, FMS 5000, Star 5000, FMS 7000 BENDIX/KING - KLN-35, KLN-89 B, KLN-90 A, KLN-90 B, KLN-94, KLX-135, KLN-900 BFGOODRICH/FOSTER - F 4, F 14, 500, 501, 616, LNS-6000 GARMIN - 100, 150 XL, 155 XL, 165, 250 XL, 300 XL, 430, 480, 530 MAGELLAN - 5000 NORTHSTAR -M 1 (above S/N 14800), M 1 A, M 2, M 3, 600 SKYFORCE -(*AIM) KMD-150, Skymap IIIC TRIMBLE - 1000 DC, 2000, 3000, 2100, 3100 IIMorrow/UPS Aviation Technologies. Apollo - 612 B, 618 TCA, 820 GX 50/55/60/65, 360, CNX 80 NMS 2001, NMC 2001 *Avionics Installation Module

Miniflo-L n n Shadin’s most popular fuel flow indicator Large, easy to read, red 7 segment LED display with adjustable brightness 3¼” x 1 ¼” x 7½” allows for the conservation of panel space Provides accuracy of ± 2%

Microflo-L n n n Offers easy readings with a red dot matrix LED display with adjustable brightness Provides accuracy of ± 2% 2¼” display allows for easy installation with limited panel space

Digiflo-L n n Allows added feature of constant left and right fuel flow rate Easy to read, red 7 segment LED display Certified to replace original gauge in many twin engine aircraft Provides accuracy of ± 2%

Product Selling Points n n n Fuel Flow Products Accuracy better than published 2% because each system is fine tuned and matched with the fuel flow transducer Digital readout vs. bar graph or analog dial Allows the pilot to fine tune the aircraft for best fuel economy Provides important fuel management information for in flight planning and GPS compatible.

Air Data Computers Digidata n ADC 2000 n ADC 6000 n ¨ Designed to interface with GPS ¨ panel or remote mounted systems available

Digidata Panel-mounted, Fuel/Airdata system for your GPS receiver n Automatically calculates and displays fuel, airdata and navigation information n

Digidata Functions n Navigation ¨ n Fuel Flow ¨ n Heading, ground track, magnetic variation Left/Right fuel flow, fuel used, fuel remaining, endurance, fuel used/remaining at destination E-6 B Data ¨ Pressure Altitude, Density Altitude, OAT, Wind Aloft, Wind Component, Indicated and True Air Speed, Ground Speed, Mach and Instantaneous Vertical Speed WARNING ¨ Digi. Data is a fuel flow measuring system and NOT a quantitysensing device. Therefore, it cannot determine the amount of usable fuel in the fuel tanks. It is imperative that an accurate figure of usable fuel on board be entered into the system to ensure accurate readings.

Digidata System n Components -The system consists of the fuel flow transducers, a navigational receiver (Loran. C or GPS), the panel mounted unit, heading input, OAT probe, and a Pitot/Static connection. n Fuel Flow Transducer - mounted in the fuel line measures the flow of fuel and generates electrical pulses directly proportional to the amount of fuel flow. The transducer is fail safe designed; rotor locking will not interrupt fuel flow to the engine. n GPS Receiver - Provides ground speed, distance, and estimated time enroute through the serial port. n n Indicator/Controller - All system electronics, functions, controls, and digital displays are contained in a single instrument that mounts in a standard 3 1/8” hole and requires no periodic maintenance, adjustments or calibration once properly installed. - The heading input, Pitot/Static connection and OAT probe allow the Digi. Data to perform its Airdata functions. Note

Digidata System n n n Fuel Management Functions - Identical as Minflo-L, Microflo-L and Digiflo-L Air. Data Functions - Airdata Pages: Several Airdata functions have been incorporated into the Digi. Data. These functions include Pressure Altitude, Density Altitude, Baro Corrected Altitude, Instantaneous Vertical Speed, Indicated Airspeed, True Airspeed, Mach, Outside Air Temperature, True Air Temperature, Heading, Rate of Turn, Wind Component and Wind Direction/Speed. All of these functions can be accessed when the rotary switch is in the AIRDATA position provided that all of the pages are enabled. The ADD/FULL switch is used to page through the functions. Navigational Functions - In addition to Airdata functions, the AIRDATA position allows access to navigational data as it is received from a Loran-C or GPS receiver. These include Ground Speed, Distance to Destination (or waypoint), Track (Magnetic or True depending on the GPS) and Magnetic Variation. These pages are included for your convenience, as well as providing a way to view the data that is used in many of the Digi. Data’s calculations.

Digidata System Warnings n n n Not Enough Fuel - When the rotary switch knob is in the FUEL TO DESTINATION position, the information in the display window flashes if the fuel on board is not enough to reach the destination selected as the active waypoint. The display window shows the amount of fuel short to reach the destination preceded by a negative sign. A search for a more suitable destination (in the same direction) can be done by selecting different destinations on your GPS receiver. Monitor the Fuel To Destination figure until a reachable destination is found. Low Endurance - The Digi. Data can be configured to display a warning based on the time remaining to fly. For example, if the “Low Endurance Warning” is configured to 45 minutes, a warning will flash if the time remaining to fly at the present power setting is less than 45 minutes. The warning “Endur. Low” will flash on the lower window. This warning occurs regardless of the currently selected function on the rotary switch knob. Press the TEST/ENTER button to acknowledge the warning. Once the warning is acknowledged it will not be displayed in the future (Note: Resetting the Digi. Data or adding fuel resets this condition and the warning is enabled again). Low Fuel Remaining - The Digi. Data can be configured to display a warning based on the fuel remaining. For example, if the “Low Fuel Warning” is configured to 20 gallons, a warning will flash if the fuel remaining is less than 20 gallons. The warning “Fuel Rem Low” will flash on the lower window. This warning occurs regardless of the currently selected function on the rotary switch knob. Press the TEST/ENTER button to acknowledge the warning. Once the warning is acknowledged it will not be displayed in the future (Note: Resetting the Digi. Data or adding fuel resets this condition and the warning is enabled again).

ADC 200 n Remote mounted computer requiring NO panel space n Versatile Fuel/Airdata computer that generates real time information and displays that information on a GPS through a standard RS 232/422 format

ADC 200 Functions n n n n IAS IVS TAS Mach P. ALT D. ALT OAT Left/Right Fuel Used n n n n TAT Winds Aloft Wind Component Rate of Turn Fuel Flow Fuel Used Fuel Remaining Endurance

ADC 2000 Remote mounted computer requiring NO panel space as all functions are viewed via the GPS n All of the functions of the ADC 200 including: n ¨ ARINC 429 ¨ Automatic Baro-Correction

ADC 6000 RVSM Solution for the Cessna Citation 500 (Post 275), 501, 550, S 550, 551, and 560

ADC 6000 Current STC’s STC# MODEL PART ST 02115 CH SA 02098 CH Cessna 500 Citation I Cessna 501 Citation I SP 25 23 ST 02115 CH SA 02098 CH ST 02115 CH Cessna 550 Citation II Cessna S 550 Citation II Cessna 551 Citation II SP Cessna 560 Citation IV 25 25 23 25

ADC 6000 n n The ADC 6000 replaces the AZ-241 Air Data Computer and interfaces with the existing aircraft equipment and flight director Brings the airframe to RVSM compliance while retaining all possible original factory equipment and wiring

ADC 6000 n The ADC 6000 has reserved internal space for future product enhancements planned at a later date, to include ¨ ETM ¨ Fuel Management ¨ Maximum Computed N 1 n The operation STC was acquired through AEROMECH and is part of the ADC-6000 RVSM Install Kit

Product Selling Points n Air Data and Altitude Management n ADC-200/2000 – An economical solution for providing Air Data and fuel flow information to your GPS and TAWS computers. The ADC 2000 offers baro corrected altitude and a 429 data bus. This product can also be used with HUMS products for the Rotor market. ADC 6000 – The most affordable RVSM system for the 500 series Citation Aircraft. This product is also a direct replacement for the Honeywell AZ-241 air data computer AMS 2000 – An economical solution for the pilot who wants an altitude warning system to prevent altitude violations. This product also provides gear warning alerts. When coupled with the Shadin Avionics 8800 T high resolution serializer, the AMS 2000 provides a time based warning as the aircraft approaches target altitude instead of a fixed altitude buffer to help the pilot start the level off in the proper time regardless of the aircraft’s rate of clime or descent. Additionally, the AMS 2000 calculates instantaneous vertical speed and allows the pilot to select resolution in 10 ft increments, rather than 100 feet. n n

Altitude Management n AMS 2000 ¨ Time based Altitude alerting ¨ Density Altitude display ¨ Real-Time IVS display

Altitude Management n AMS 2000 ¨ AMS 2000 is an Altitude Management and Alert System. Its purpose is to alert you when you are approaching or deviating from your target altitude. Other features include alerts when you reach your Decision Height or Minimum Descent Altitude, and a landing gear reminder when you approach your destination altitude. The AMS 2000 also will calculate density altitude and engine performance. These alerts and calculations help you fly safer and easier. ¨ AMS 2000 does not act as an auto pilot, or control the aircraft in any way. Think of it as an assistant to you, the pilot, which keeps track of minor details and frees you to fly the aircraft. No longer do you have to keep both eyes on the sky and one on the altimeter. ¨ AMS 2000 receives its altitude information from your encoder, and displays it in 100 -foot increments. When connected to a Falcon Altitude Encoder or Converter, AMS 2000 displays altitude in 10 foot increments, and also offers a page displaying Instantaneous Vertical Speed (IVS). IVS display does not have the lag inherent in static system VSI displays.

Engine Trend Monitoring n Functions: ¨ Air Data Computer ¨ Fuel Management System ¨ Secondary Engine Instrument Display ¨ Navigation

ETM Components Remote Display Mounted in Aircraft Control Panel Remote Processor Unit Mounted in Avionics Bay or Under the Floor Key Recorder Panels Mounted in Aircraft Cockpit

ETM Helicopter STC’s n Bell ¨ 212, n 412, 412 EP, 206 Series Eurocopter France ¨ AS 355 F 2 n Eurocopter Deutschland ¨ BO 105, n BK 117 Messerschmitt-Volkow-Blohm ¨ MBB-BK 117

ETM Fixed Wing STC’s n Beechcraft King. Air ¨ 200, n Cessna Caravan ¨ 208, n C 90, E 90, F 90, 1900 C, 1900 D 208 A, 208 B Socata ¨ TBM 700 ¨ TBM 850

ETM System n The ETM is designed to monitor, display, and record all engine and airframe parameters and, if desired, to alarm the pilot when those parameters exceed established limits. The system provides the pilot with a centralized location for engine monitoring, fuel management, navigation, and airdata. It provides the maintenance personnel with a detailed record of engine and airframe use. Most importantly however, the ETM automatically collects and records data for use with the Pratt & Whitney ECTM program.

ETM Capabilities n n Monitor and display primary airdata, including pressure altitude, indicated air speed, and outside air temperature. Interface with a long range navigational receiver and display latitude, longitude, course (track), ground speed, ETE, waypoint ID and distance to destination data. Calculate and display secondary data, including density altitude, true airspeed, mach, drift, wind speed/direction, ETA, shaft horsepower, and specific fuel consumption. Monitor engine and airframe parameters.

ETM Capabilities n n Monitor and display engine data, including engine temperature, and torque; fuel flow, and turbine speeds Detect and record all exceedances for the engines and airframe. Priority display the exceedances of any parameter, regardless of any other display function. Display on demand any of the monitored parameters.

ETM Capabilities n n n Automatically Log engine total time and number of starts, as well as airframe total time, and total cycles. Sample and record data which is required as an input for subsequent power check calculations. Provide the pilot with complete fuel management data, including full fuel, added fuel, fuel remaining, fuel used, fuel at destination, and fuel to destination. Record events such as engine starts, takeoff, landing, and engine shutdowns; as well as power check calculation inputs and user requested data in the form of printouts and key reports. Provide a multifunction clock including GMT, local time, stopwatch, and calendar.

ETM Benefits n Engine ¨ Engine fuel control unit n Documents whether the aircraft is performing as intended (flight plan, book performance) ¨ Automatically isolate segments and fuel for analysis ¨ Reduces unexpected problems and/or in-flight shutdowns through monitoring abnormal performance by engine data trending

Product Selling Points n Engine Trend Monitoring n Constant Engine critical health monitoring with and visual alerts to exceedances. Provides pilots critical information prior to a catastrophic failure in most cases. Trend Monitoring for total life of the engine that helps asses engine maintenance costs and requirements. Capable to automatically interface with the Pratt and Whitney ECTM IV and HECTM engine monitoring programs. First year of Trend monitoring offered at no charge to the customer through the Trend Group in Clovis California. Maintenance count down timer to prevent over flying mandatory FAA inspection items Recorded information can be used to monitor and record engine use for aircraft leased by the flight hour Provides Navigational and Air Data information in addition to Engine Data n n n n

Product Selling Points n Engine Trend Monitoring n Numerous offerings of converters offered by Shadin Avionics. Some of the converters offered: Synchro to ARINC, AC fuel Flow to ARINC 429, ARINC 419 to Map Serial Converter, ARINC 429 to Serial and many more. One of the top selling converters is the 933612 -02 ARINC 429 HS/LS to Serial Converter primarily used in Electronic Flight Bag installations integrating with an onboard GPS system. Call your Shadin Avionics representative for more details on any converter requests n n

Converters n Shadin offers a variety of converters in 3 families: ¨ ARINC to Serial ¨ Serial to ARINC ¨ ARINC to ARINC