Garmin RS-232 User Manual

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Microflo-L
Digital Fuel
Management System
with interface to LORAN-C and GPS receivers with
RS-232 output format
OPERATING MANUAL
Single and Twin Engine Indicators
For P/N: 91204XT-38-D
Shadin
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Summary of Contents

Page 1 - Microflo-L

Microflo-L™ Digital Fuel Management System with interface to LORAN-C and GPS receivers with RS-232 output format OPERATING MANUAL Single and Twi

Page 2 - TABLE OF CONTENTS

9 6. After reaching the correct total usable fuel figure, press the ENTER/TEST button and the computer will store that number as full fuel. The word

Page 3 - WWW.SHADIN.COM

10 Move the USED/REM toggle switch to the REM position. The system will display the fuel remaining on board. The pilot should confirm this figure wi

Page 4

11 2.5 PARTIAL FUEL ADDED There are two methods to enter partial fuel: Ramping MethodAdd the amount of fuel from the refueling meter to the amount o

Page 5

12 switch in the USED position and use the ENTER/TEST button to control the decrementing. Note: Adding or subtracting fuel by any method resets the f

Page 6

13 3.1.5 NAUTICAL MILES PER GALLON Nautical miles per gallon is selected by rotating the rotary switch to the NM/GAL position. The information is s

Page 7

14 3.2 WARNINGS 3.2.1 NOT ENOUGH FUEL When the rotary switch is in FUEL TO DEST. position, the information in the display window flashes if fuel on

Page 8

15 3.3 BRIGHTNESS CONTROL The display brightness is controlled by the BRIGHT/DIM toggle switch. Moving the BRIGHT/DIM toggle switch to BRIGHT repe

Page 9 - 2. PREFLIGHT PROCEDURES

16 5. ERROR MESSAGES ERROR 1: Dues to the necessity of Group 1 settings, if the Flow Meter is set to Operate Mode and the checksum of Group 1 is ba

Page 10

17 6. CONFIGURATION DATA ENTRY Manual Entry Mode Ordinarily, the fuel flow indicator has been set up by the factory to match the K-factor of the s

Page 11

18 Group 1: Generally, Group 1 is set up by the distributor and contains information defined by the part number. However, although functions are defi

Page 12

1 TABLE OF CONTENTS 1. GENERAL DESCRIPTION...3 1.1 THE SYSTEM PROVIDES...

Page 13 - 3. INFLIGHT OPERATIONS

Locations of the switches for the Microflo are as follows: F A C E 19 P L A T E SW4 SW3 SW2 SW1 Component side of board Board Edge Each switch has

Page 14

Manual Entry Mode There are two ways to access the Manual Entry Page. 1. Set Switches 1 and 2 to Entry Mode and power up. This allows access to bo

Page 15

21 The values displayed can be adjusted with the ADD/FULL toggle switch. ADD increments the value, and FULL decrements the value. As you hold ADD or

Page 16 - 4. EMERGENCY PROCEDURES

22 5. The K-factor values displayed can be adjusted with the ADD/FULL toggle switch located at the lower right corner. ADD increments the value, an

Page 17 - 5. ERROR MESSAGES

23 Display Description*L xxxxx = Left K-factor (where xxxxx is valid from 0 to 20,000. These are in 10s. A setting of 1234 would be a K-factor o

Page 18 - Manual Entry Mode

24 7. SPECIFICATIONS Certification: TSO-C44a Maximum usable fuel: 1,800 gallons 6,822 liters 9,999 lbs 5,484 Kg @ 0.805 Kg/lit Maximum

Page 19

25 COMPATIBLE RECEIVERS: ARNAV R15, R20, R21, R30, R40, R50, R50V, R50i, R5000, FMS5000, Star5000, FMS7000 BENDIX/KING KLN-35, KLN-89B, KLN-90, K

Page 20

8. WARRANTY INFORMATION 6831 Oxford Street St. Louis Park, MN 55426 Limited Warranty Shadin warrants this instrument and system components t

Page 21

27 No representative is authorized to assume any other liability for Shadin in connection with the sale or resale of Shadin’s products. If you do no

Page 22

28 Digital Fuel Management System Data (Microflo-L) Part Number: __________________________ Serial Number: __________________________ Left/Sin

Page 23

3.2.1 NOT ENOUGH FUEL...14 3.2.2 RESERVE FUEL WILL BE USED...

Page 24 - Display Description

P/N OP91204-38E 6831 Oxford Street St. Louis Park, MN 55426-4412 U.S.A. Sales Tel: (800) 328-0584 Tech Support Tel: (800) 388-2849

Page 25 - 7. SPECIFICATIONS

3 Microflo-L™ Although not required by the FAA, it is recommended that this manual be attached to the FAA-approved Flight Manual, or always kept on b

Page 26 - TRANSDUCER

4 1.1 THE SYSTEM PROVIDES 1.1.1 SPECIFIC RANGE Specific Range (NM/GAL) = Ground Speed (Kt.)/Fuel Flow per hour. This is an indication of how effici

Page 27 - 8. WARRANTY INFORMATION

5 1.1.5 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

Page 28

6 1.2 SYSTEM COMPONENTS The system consists of three (3) basic units: the fuel flow transducer, the navigation receiver (Loran-C or GPS) and the pan

Page 29

7 1.3 TEST FUNCTION Diagnostic software is built into the system. To activate it, press the ENTER/TEST button until all of the display digits fill

Page 30

8 2. PREFLIGHT PROCEDURES MICROFLO-L is a fuel flow measuring system and NOT a quantity-sensing device. A visual inspection and positive determinat

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