GarminメーカーRS-232の使用説明書/サービス説明書
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Microflo-L ™ Digital Fuel Management System with interface to LORAN-C and G PS receivers with RS-232 output format OPERATING MANUAL Single and Twin Engine Indicators For P/N: 91204XT-38-D Shadin.
1 TABLE OF CONTENTS 1. GENERA L DESCRIPTION .......................................................................... 3 1.1 THE SYS TEM PROVIDES ......................................................................... 4 1.1.1 SPECIF IC RANGE .......
3.2.1 NOT ENOUGH FUEL..................................................................... 14 3.2.2 RESERVE FUEL WILL BE USED................................................. 14 3.2.3 LO W ENDURANCE ....................................................
3 Microflo-L ™ Although not required by the FAA, it is recommended that this manual be attached to th e FAA-a pproved Flight Manual, or always kept on board for reference.
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 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.
5 1.1.5 FUEL FLOW The system provides a digital re adout 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.
6 1.2 SYSTEM COMPONENTS The system consists of three (3) basic units: the fuel flow transducer, the navigatio n receiver (Loran-C or GPS) and the panel mounted unit. 1.2.1 FUEL FLOW TRANSDUCER The fuel flow transducer mounted in the fuel line measures the flow of fuel and genera tes electrical pulses directly proportional to the fuel flow.
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 with a checkerboard pattern, and then release it.
8 2. PREFLIGHT PROCEDURES MICROFLO-L is a fuel flow measuring system and NOT a quantity-sensing device. A visual inspec tion and positive determination of the usable f uel in the fuel tanks is a ne cessity. Therefore, it is imperative tha t the determ ined available usable fu el be manually entered into the system .
9 6. After reaching the correct total usable fuel figure, press the ENTER/TEST button and the comput er will store that number as full fuel. The word “ FUL” disappears and the com puter will return to the opera ting mode. Release the ADD/FULL toggle switch.
10 Move the USED/REM toggle swit ch to the REM position. The system will display the fuel rem a ining on board. The pilot should confirm this figure with the actual fuel on board. 2.3 NO FUEL ADDED This automatically stores inform ation concerning previous fu el levels, even in the case of a pow er down.
11 2.5 PARTIAL FUEL ADDED There are two methods to enter partial fuel: Ramping Method Add the amount of fuel from the refueling m eter to the amount of fuel remaining. Enter the total using the following steps: 1. Move USED/REM toggle switch to REM position and hold.
12 switch in the USED position and u se the ENTER/TEST button to control the decrem enting. Note: Adding or subtracting fuel by any method resets the fuel used value to zero. 3. INFLIGHT OPERATIONS 3.1 INSTRUMENT OPERATION 3.1.1 FUEL FLOW For Single Engine Aircraft: FUEL FLOW is displayed continuously on the left display window.
13 3.1.5 NAUTICAL MILES PER GALLON Nautical miles per gallo n is selected by rotating the rotary switch to the NM/GAL position. The inf ormation is shown on the right display window. 3.1.6 FUEL TO DESTINATION Fuel to destination is selected by rotating the ro tary switch to the FUEL TO DEST.
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 board is insufficient to reach either th e destination se lected as the active waypoint or the final dest ination (if that total distance record is provided in the seri al message).
15 3.3 BRIGHTNESS CONTROL The display brightness is cont rolled by the BRIGHT/DIM toggle switch. Moving the BRIGHT/DIM toggle switch to BRIGHT repeatedly will make the disp lay brighter; moving it to DIM repeatedly will dim the display. Th e default brightness after power up is full brightness.
16 5. ERROR MESSAGES ERROR 1: Dues to the necessity of Group 1 settings, if the F low Meter is set to Operate Mode and the checksum of Group 1 is b ad, the display will flash: E1 .
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 supplied transducers and other set-up information. However, there are built-in provisions to change the set-up.
18 Group 1: Generally, Group 1 is set up by the distributor and contains information defined by the part number. However, although functions are defined here , do not change them without proper knowledge or they will affect perform ance of the indicator.
Locations of the switches for the Microflo are as follows: F A C E 19 P L A T E SW4 SW3 SW2 SW1 Compone nt side of board Board Edge Each switch ha s 16 posit ions, 0- 9, A, B, C , D, E, F. Operation Mode vs. Entry Mode FE: If Switch 1 is set to F and Switch 2 is set to E, the unit is in Entry Mode .
Manual Entry Mode There are two ways to access the Manual Entry Page. 1. Set Switches 1 and 2 to Entry Mo de and power up. This allows access to both groups. 2. If the Switches are not set to Entry Mode , while running under normal conditions, press the TEST/ENTER button to start the test mode.
21 The values displayed can be ad justed with the ADD/FULL toggle switch. ADD increments the value, and FULL decrem ents the value. As you hold ADD or FULL, th e scrolling rate will increase up to a maximum speed.
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, and FULL decrements the value. 6. Move the REM/USED switch at the upper right corner to the USED position to move to page “r” for the right engine in twin engine aircraft and repeat Step 5.
23 Display Description *L xxxxx = Left K-factor (wher e xxxxx is valid from 0 to 20,000. These are in 10s. A setting of 1234 would be a K-factor of 12,340) *R xxxxx = Right K-factor (as above).
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 Altitude: 40,000 ft Operating temperature: -30° to 50°C Humidit.
25 COMPATIBLE RECEIVERS: ARNAV R15, R20, R21, R3 0, R40, R 50, R50V, R50i, R5000, FMS5000, Star5000, FMS7000 BENDIX/KING KLN-35 , KLN -8 9B, KL N-90, KLN-90A, KLN-90B, KL N- 94 , KL X-135, KLN-900 BFG.
8. WARRANTY INFORMATION 6831 Oxford Street St. Louis Park, MN 55426 Limited Warranty Shadin warrants this instrument and system components to be free from defects in materials and workmanship for a period of one year from the user invo ice date.
27 No representative is authorized to assum e any other liability for Shadin in connection with the sale or resale of Shadin’s products. If you do not agree an d accept the terms of this Warran ty, you may return the product in new condition, with receipt, within thirty (30) days for a refund.
28 Digital Fuel Management System Data (Micro flo-L) Part Number: _________________ _________ Serial Number: _________ ___ ______________ Left/Single Tran sdu cer Part or Kit Number: _______________ _.
P/N OP91204-38 E 6831 Oxford Street St. Louis Park, MN 55426-4412 U.S.A. Sales Tel: (800) 328-0584 Tech Support Tel: (800) 388-2849 International Tel: (952) 927-6500 Main/Sales Fax: (952) 924-1111 Tech Support Fax: (952) 924-1122 Sales E-Mail: sales@shadin.
デバイスGarmin RS-232の購入後に（又は購入する前であっても）重要なポイントは、説明書をよく読むことです。その単純な理由はいくつかあります：
Garmin RS-232をまだ購入していないなら、この製品の基本情報を理解する良い機会です。まずは上にある説明書の最初のページをご覧ください。そこにはGarmin RS-232の技術情報の概要が記載されているはずです。デバイスがあなたのニーズを満たすかどうかは、ここで確認しましょう。Garmin RS-232の取扱説明書の次のページをよく読むことにより、製品の全機能やその取り扱いに関する情報を知ることができます。Garmin RS-232で得られた情報は、きっとあなたの購入の決断を手助けしてくれることでしょう。
Garmin RS-232を既にお持ちだが、まだ読んでいない場合は、上記の理由によりそれを行うべきです。そうすることにより機能を適切に使用しているか、又はGarmin RS-232の不適切な取り扱いによりその寿命を短くする危険を犯していないかどうかを知ることができます。
ですが、ユーザガイドが果たす重要な役割の一つは、Garmin RS-232に関する問題の解決を支援することです。そこにはほとんどの場合、トラブルシューティング、すなわちGarmin RS-232デバイスで最もよく起こりうる故障・不良とそれらの対処法についてのアドバイスを見つけることができるはずです。たとえ問題を解決できなかった場合でも、説明書にはカスタマー・サービスセンター又は最寄りのサービスセンターへの問い合わせ先等、次の対処法についての指示があるはずです。
