Midcontinent MD41-1817 Скачать руководство пользователя страница 13

Rev. D January 27, 2020 

13 

Manual Number 9018252   

3.4

 

MOUNTING 

 

Refer to Section 2: Pre-Installation Considerations in regards to equipment location. 
 

The MD41 ACU is designed for rear panel mounting only. A cutout should be made in the panel in 

accordance with Figure 4 for the unit bezel and two mounting holes. A cutout template is available from 

Mid-Continent Instruments and Avionics (reference p/n 8014474) upon request. 

 

Prior to completing the mounting of the unit in the aircraft, make sure to set the Annunciator Dim 
Adjustment if automatic dimming is configured for the annunciations. Ideally this procedure is best 

performed in a dark cockpit to simulate low-light/night time conditions. Connect the unit to the cable 

harness and turn on master power to the instrument panel and lighting bus. Use a small flat-bladed 

screwdriver to access the adjustment screw inside the hole on the bottom of the unit (see Figure 4). 

Adjust the screw to increase or decrease the annunciator lighting brightness to a level appropriate with 

the rest of the panel instrument lighting.  
  

Secure the indicator to the panel with two #4-40 x 3/8 flat head phillips screws. 

 

2.75

2.25

0.80

R0.16 typ.

2.50

3.00

0.13

Text Direction

2X 4-40 UNC-2B

3/8" max thread depth

Momentary Switch

 

FIGURE 6 

OUTLINE DRAWING MD41-1817 

 

 

Содержание MD41-1817

Страница 1: ...17 Annunciation Control Unit For Lithium Ion Battery Systems MD41 1817 28vdc Horizontal Mount Mid Continent Instruments and Avionics Manual Number 9018252 9400 E 34th Street N Wichita KS 67226 USA Rev...

Страница 2: ...USA Phone 316 630 0101 Fax 316 630 0723 We welcome your comments concerning this manual Although every effort has been made to keep it free of errors some may occur When reporting a specific problem p...

Страница 3: ...07 29 15 Added Environmental Qualification Form C 04 25 16 Revised graphics and text to change annunciation text from STANDBY to CHARGING and FAIL to TEMP Minor modifications to Sections 3 and 4 Adde...

Страница 4: ...ING CONTROLS 11 3 3 2 POWER AND SIGNALS 12 3 3 3 HARNESS VERIFICATION 12 3 4 MOUNTING 13 SECTION 4 OPERATION 14 4 1 FRONT PANEL CONTROLS AND ANNUNCIATIONS 14 4 1 1 CONTROLS 14 4 1 2 ANNUNCIATIONS 14 S...

Страница 5: ...switch dead front inactive annunciations and the installation option for manual or automatic dimming An external annunciation dimming adjustment is provided for balancing low level light conditions 1...

Страница 6: ...ignal lines with any high energy sources Examples of these sources include 400 Hz AC Comm DME HF and transponder transmitter coaxial cables Always use shielded wire when shown on the installation prin...

Страница 7: ...inspection for evidence of any damage that may have incurred during shipment 3 2 1 INCLUDED PARTS A Main Battery ACU MCIA P N MD41 1817 series B Installation Manual MCIA P N 9018252 3 2 2 AVAILABLE PA...

Страница 8: ...C Battery 1 24 GROUND 12 28 VDC Battery 2 25 GROUND 13 28 VDC Aircraft Power TABLE 4 SCHEMATIC PINOUT CHARGING ANNUN BATT 1 USE 2A CIRCUIT BREAKER FROM LIGHTING BUS HEATING ANNUN BATT 2 OUTPUT TO RTD1...

Страница 9: ...N1 BATT 1 OUTPUT TO RTD1 PIN1 BATT 1 CHARGING ANNUN BATT 1 FAIL FAULT ANNUN BATT 1 BATTERY 1 GROUND BATTERY 1 28 VDC 2A 28VDC BATTERY 1 RESERVED NOTES 1 ALL WIRING SHALL BE 24 AWG UNLESS OTHERWISE NOT...

Страница 10: ...ING ANNUN BATT 1 RTD1 PIN1 BATT 1 OUTPUT TO RTD1 PIN1 BATT 1 CHARGING ANNUN BATT 1 FAIL FAULT ANNUN BATT 1 BATTERY 1 GROUND BATTERY 1 28 VDC 2A 28VDC BATTERY 1 RESERVED BATTERY 2 GROUND NOTES 1 ALL WI...

Страница 11: ...WGUNLESSOTHERWISENOTED 5 18 21 16 15 19 6 4 12 25 14 22 23 G F A C D B RESERVED RESERVED RESERVED RESERVED RESERVED RTD1 PIN2 BATT1 INPUTFROMRTD2 PIN1 BATT1 RTD2 PIN1 BATT1 E FIGURE 5 WIRING DIAGRAM O...

Страница 12: ...xists pins 22 and 23 will be tied together with a 100 series resistance This output signal can be utilized as a battery over temperature indicator to other systems in the aircraft The TEMP annunciatio...

Страница 13: ...ming is configured for the annunciations Ideally this procedure is best performed in a dark cockpit to simulate low light night time conditions Connect the unit to the cable harness and turn on master...

Страница 14: ...al and operating instructions of the TB17 for additional operational and functional interface details 4 1 2 ANNUNCIATIONS MAIN BATTERY WHITE Lit when any of the annunciations are ON TEMP RED Lit when...

Страница 15: ...RTHINESS STATEMENT No periodic scheduled maintenance or calibration is necessary for continued airworthiness of the MD41 series ACU If the unit fails to perform to specifications the unit must be remo...

Страница 16: ...p 55C Survival High Temp 85C Short and Normal Operating High Temp 70C Altitude 55 000 ft Temperature Variation 5 Category S2 Humidity 6 Category B Operational Shock and Crash Safety 7 Category B Vibra...

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