Dual Fuel Level – Cirrus Aircraft w/ CIES Inc. Senders

c. Disconnect the DB25 connector from the instrument. d. Check intensity control. e. Check the wiring installation and breaker or fuse. 12. Proceed to “Instrument Setup”. 1 2 3 SPRU1031S28 A200-DDC To harness connector Connection to Panel Rheostat RED BLACK BLUE 14V/28V Switched power Ground Panel rheostat (0V = min / Bus voltage = Max) BLUE BLACK (HARNESS) A200-DDC To harness connector RED BLACK BLUE 14V/28V Switched power Ground 0V = min / Bus voltage = Max BLUE BLACK (HARNESS) Connection to Independent Potentiometer Control 14V/28V Switched power Ground (Not Supplied) To Multiple Instruments BLUE Date: 3/15/2013 12:37:03 PM Sheet: 1/1 REV: TITLE: Document Number: Intensity Control Options - Rev 1.2a S200-DDC-INST B (c) 2009-2012 Aerospace Logic Inc. FL202G Wiring and Installation Schematic S200-FL202G-003 Rev 1.0 10/05/2012 DB25 CONNECTOR FL202G INSTRUMENT RED BLACK YELLOW ORANGE 6V - 36V SUPPLY GROUND EXTERNAL ALARM (MAX 100mA SINK) RS-232 DATA OUTPUT COLOR DESCRIPTION COLOR/TAG CONNECT TO (C) Aerospace Logic Inc. (2008-2012) ACCESSORY NOTES: 1. ** Remove for 14V operation Only to be used with CIES Inc. TSO'd fuel senders 1. INSTALLATION NOTES: Allow for current drain of 0.1A (100mA) Install using breaker or panel fuse Maximum 7 instruments per 1A of breaker capacity For multiple instrument installations install breakers to comply with redundancy requirements of AC 23.1309-1D Appendix 1 Connect all BLACK (GROUND) wires to the same ground point 1. 2. 3. 4. 5. LEFT SENDER SIGNAL RIGHT SENDER SIGNAL SENDER NOTES: 2. See Installation Instructions for sender wiring 3. WHITE / #1 WHITE / #2 BLUE RED TWISTED BUNDLE 14V/28V SUPPLY GROUND 0V-BUS VOLTAGE - VARIABLE INTENSITY INPUT A200-DDC Rev C BLACK ** REMOVE FOR 14V RED TWISTED BUNDLE 14V/28V SUPPLY GROUND A200-DDC Rev C BLACK BLACK GROUND WHITE LEFT SENDER POWER - (TAG LEFT PWR) RED TWISTED BUNDLE 14V/28V SUPPLY GROUND A200-DDC Rev C BLACK BLACK GROUND WHITE RIGHT SENDER POWER - (TAG RIGHT PWR) Only for installation on Cirrus Aircraft SR20, SR22 & SR22T 1 1 2 3 3 4 4 A A B B DWG NO. SH REV. CB2840570001 4 - TITLE SIZE SCALE DWG NO. REV. SHEET OF CAGE CODE 66YY1 WIRING MODIFICATION FUEL LEVEL SENDER CIRRUS SR-22 B CB2840570001 - 5 4 INC 791 NW TRENTON AVE BEND, OR 97701 1 1 2 3 3 4 4 A A B B DWG NO. SH REV. CB2840570002 3 - TITLE SIZE SCALE DWG NO. REV. SHEET OF CAGE CODE 66YY1 WIRING MODIFICATION FUEL LEVEL SENDER CIRRUS SR-20 B CB2840570002 - 6 3 INC 791 NW TRENTON AVE BEND, OR 97701 1 1 2 3 3 4 4 A A B B DWG NO. SH REV. CB2840570002 6 - TITLE SIZE SCALE DWG NO. REV. SHEET OF CAGE CODE 66YY1 WIRING MODIFICATION FUEL LEVEL SENDER CIRRUS SR-20 B CB2840570002 - 6 6 INC 791 NW TRENTON AVE BEND, OR 97701 200 Series Human Interface Definition – Rev 1.0 Aerospace Logic Inc. 180 James Street South, Suite 205, Hamilton, ON, L8P 4V1, CANADA Tel. 416-628-0725 | www.aerospacelogic.com | Fax. 416-352-5854 All 200 Series instruments have been designed around a standard Human Interface protocol. This allows identical operation of the two panel switches between all instruments while still allowing multiple functions. This document is a generic outline of the functionality of the switches, based on the various functional states of the instrument. Top Button The top button is the action button. It invokes different screen displays, allows selection of values and increments or decrements values. Examples of these actions are: 1. Moving between display screens 2. Selection of an action from a menu 3. Changing a value from within the setup menus 4. Entering a value during flight (clock instrument only) Bottom Button The bottom button is the navigation button. It will allow the cursor on the screen to move between allowable selections. Examples of these actions are: 1. Selection of different cylinders (EGT and CHT) in the Single Cylinder mode 2. Selection of different tanks (Fuel Level) 3. Selection of limits and functional items from within the setup menus 4. Time field selection (clock instrument only) There is one exception to the functionality of the bottom button. This is from the Primary Display (the screen that first comes on from power up). Pressing the button will display the instrument core status and support data. General 1. Each specific instrument contains detailed button options within the Operations Guide. 2. During setup, instructions are provided on screen and use of the buttons is as noted in this document. FL202G Instrument Setup Document # S200-FL202G-004 Rev 1.1 09/18/2012 Page 1 of 2 Aerospace Logic Inc. 180 James Street South, Suite 205, Hamilton, ON, L8P 4V1, CANADA Tel. 416-628-0725 | www.aerospacelogic.com | Fax. 416-352-5854 WARNING THIS INSTRUMENT MAY ONLY BE INSTALLED ON CIRRUS SR20 AND SR22 SERIES AIRCRAFT EQUIPPED WITH CIES INC. FUEL SENDERS. IT HAS BEEN PRE-CONFIGURED FOR THIS INSTALLATION CONFIGURATION AND WILL NOT WORK CORRECTLY WHEN INSTALLED IN ANY OTHER AIRCRAFT. 1. Color indications of the level indication bars have been preset based on Cirrus data for the specific aircraft. These values of usable fuel are automatically set when the instrument is calibrated: a. For SR20: i. Red line less than 0.1 USG ii. Yellow line 0.1 USG to 8.2 USG iii. Green line for all quantities above 8.2 USG b. For SR22: i. Red line less than 0.1 USG ii. Yellow line 0.1 USG to 14.0 USG iii. Green line for all quantities above 14.0 USG 2. The fuel imbalance warning values have been preset based on Cirrus data for the specific aircraft. These values are automatically set when the instrument is calibrated: a. SR20 - 7.5 USG b. SR22 - 10.0 USG 3. This instrument requires calibration before it will function. To calibrate each tank you will be required to add fuel at TWO gallon increments, starting with the unusable fuel in the tank (the legal, zero fuel point). a. Place the aircraft in a level flight attitude and support the aircraft wings, if necessary. b. Drain all tanks to be calibrated. c. Disable any cross feed between tanks. FL202G Instrument Setup Document # S200-FL202G-004 Rev 1.1 09/18/2012 Page 2 of 2 Aerospace Logic Inc. 180 James Street South, Suite 205, Hamilton, ON, L8P 4V1, CANADA Tel. 416-628-0725 | www.aerospacelogic.com | Fax. 416-352-5854 d. Place the unusable fuel in each tank to be calibrated. e. Complete the calibration process by following the interactive, instructions provided throughout the process on the instrument display (See 4). f. Calibration time is approximately one minute per two gallons of fuel. g. Note the calibration values on the provided calibration sheets. This value serves two purposes. i. It demonstrates a compliant installation, and ii. Provides a hard copy backup of all calibration data. h. It is not necessary to complete the full calibration at once. Calibration can be resumed at any point of the process by re-entering the setup. 4. To enter parameters and perform the calibration, proceed as follows: a. Turn off the power to the instrument b. Press and hold both top and bottom buttons and turn on the power to the instrument. c. When instructed, release both buttons. d. In the setup menus, use the bottom button to navigate and the top button to select an option. e. Follow the onscreen instructions to enter the correct operating parameters. NOTE: Depending on the installation orientation of the instrument the display may initially be upside down. The first prompt in the setup is to press the button at the top of the instrument. This will orientate it correctly. f. To perform the instrument calibration, follow the instructions provided on the instrument screen. 5. Once all calibration has been completed the instrument will be enabled and be ready for use. FL202G Operations Guide Document # S200-FL202G-005 Rev 1.0 15-SEP-2012 Page 1 of 2 Aerospace Logic Inc. 180 James Street South, Suite 205, Hamilton, ON, L8P 4V1, CANADA Tel. 416-628-0725 | www.aerospacelogic.com | Fax. 416-352-5854 This manual outlines the operating procedures for the FL202G product 1. Pre-Calibration Display – Default Screen FUEL INSTRUMENT NOT INSTALLED CORRECTLY FLIGHT PROHIBITED 2. Power Up / Default Screen Displays the fuel level in each tank. Colors are determined by the range values as set during installation. The quantity in each tank is permanently displayed beneath each indicator bar. A flashing yellow bar on either side indicates a fuel imbalance condition. The flashing tank indication will be that of the tank with the most fuel. Switch the fuel supply to that tank to begin burning fuel from the imbalanced tank. Once sufficient fuel has been burned to fall below the imbalance warning, the flashing yellow bar will return to its correct color indication for the specific fuel level. Imbalance limits are fixed values for the specific aircraft. Press the top button to move to the next display screen. FL202G Operations Guide Document # S200-FL202G-005 Rev 1.0 15-SEP-2012 Page 2 of 2 Aerospace Logic Inc. 180 James Street South, Suite 205, Hamilton, ON, L8P 4V1, CANADA Tel. 416-628-0725 | www.aerospacelogic.com | Fax. 416-352-5854 3. Trend Graph This screen provides a graphical display of fuel usage, since the most recent power on. The graph spans a time period of 192 minutes (3 hours 12 minutes). Once this graph area has been populated it will scroll to the left. The fuel value displayed at the bottom of the screen relates to the selected tank as indicated by the bracketed tank number at the top of the screen. Use the bottom button to scroll between tanks. Press the top button to return to the default screen. 4. Other Options To display the instrument serial number and core information press and hold the bottom button when the instrument is first powered on. _____________________________________________________________ WARNINGS 1. NEVER RELY SOLELY ON ANY FUEL INDICATION INSTRUMENT FOR THE DETERMINATION OF AVAILABLE FUEL. 2. WHEN USED IN CONJUNCTION WITH A PHYSICAL INSPECTION, DETERMINATION OF AVAILABLE FUEL PLUS NECESSARY FLIGHT DURATION AND CONDITION CALCULATIONS, A FUEL LEVEL INSTRUMENT BECOMES A VALUABLE COCKPIT RESOURCE. 3. All operations are to be performed in accordance with the specific instructions pertaining to your aircraft, including those provided by the engine manufacturer. The FL202G instrument is only a parameter reporting device which can assist in engine and flight management when used in conjunction with these instructions. 4. The FL202G product is certified as a primary replacement ONLY, within the limits as described above. 5. IT MAY BE INSTALLED AS A PRIMARY OR SECONDARY INSTRUMENT ON CIRRUS AIRCRAFT WHICH HAVE “Cirrus Perspective Software Revision v0764.15 or later installed”. IT MAY BE INSTALLED AS A PRIMARY INSTRUMENT WHEN USED IN CONJUNCTION WITH CIES INC. TSO’d FUEL SENDERS, WHICH HAVE BEEN INSTALLED IN ACCORDANCE WITH CIRRUS AIRCRAFT CORPORATION INSTRUCTIONS AND CONNECTED AS PER THE FL202G INSTALLATION INSTRUCTIONS. FL202G Product Specifications Document # S200-FL202G-007 Rev 1.0 10/04/2012 Page 1 of 1 Aerospace Logic Inc. 180 James Street South, Suite 205, Hamilton, ON, L8P 4V1, CANADA Tel. 416-628-0725 | www.aerospacelogic.com | Fax. 416-352-5854 Certification / Compliance TSO C55a Environmental DO-160F A1CAASXXXXXXZBXXBBBCSBA1C11XXAX Software DO-178B DC Power Source Input voltage 6 to 36 VDC Power consumption 100mA Load dump tolerance +60V Direct spike tolerance +/- 60V Cable spike tolerance > +/- 1KV Operating Temperature Constant operating -15ºC to +55ºC Short term operating (1hr) -40ºC to +70ºC Storage -55ºC to +85ºC Signal Input 5.0V Pulse Width Modulated Sender Type CIES Inc. TSO C55A Qualified Senders Display Fuel Quantity US Gallons or Litres Accuracy Fuel Quantity AS405C +/- 1 USG Range 0 to 120 USG (defined by fuel sender/tank size) Display Sunlight readable LCD 176 X 192 display pixels, 65,535 colors Annunciator Output 100mA sink with reverse EMF protection RS-232 Data Output 1 second per full sequence at 57.6K bps (8/N/2/N) Interface Connector DB-25 Software Functionality Primary Fuel level in all tanks Fuel Imbalance Installer selectable SR20 or SR22 Trend Graph Graphic display of level vs time Dimensions 2.45” X 2.45” X 0.96” Weight (excluding harness) 4.05 oz Finish Black anodized 6061 aluminum FL202G Installation Compliance Document # S200-FL202G-007 Rev 1.0 10/07/2012 Page 1 of 1 Aerospace Logic Inc. 180 James Street South, Suite 205, Hamilton, ON, L8P 4V1, CANADA Tel. 416-628-0725 | www.aerospacelogic.com | Fax. 416-352-5854 1. Installation Procedures and Limitations Should your specific aircraft not be listed on our STC Approved Model List (AML), contact your local FSDO or flight authority for installation requirements BEFORE commencing any installation tasks. Installation must be in accordance with the following FL202G published documents: a. Installation Instructions, b. Wiring and Installation Schematic, and c. Instrument Setup. 2. Installation Location and Visibility The products are to be installed in existing panel holes and will replace existing instrumentation. As primary replacement products it is recommended and preferred that they be placed in the same panel location as the original equipment. Their visibility and placement relative to other instruments are the same or similar to the existing instruments. Where they are installed in a different location it is the responsibility of the installer to ensure that they are visible to the pilot under all conditions. 3. TSO COMPLIANCE NOTICE The conditions and tests required for TSO approval of this instrument are minimum performance standards. Those installing this instrument on or in a specific type or class of aircraft, must determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in an aircraft. The instrument may be installed only according to 14 CFR part 43 or the applicable airworthiness requirement.