Midcontinent MD41-1817 Скачать руководство пользователя страница 14

Rev. D January 27, 2020 

14 

Manual Number 9018252   

SECTION 4

 

OPERATION 

 

4.1

 

FRONT PANEL CONTROLS AND ANNUNCIATIONS 

 

4.1.1

 

CONTROLS 

 

BATT/HEAT 

There are 2 different TB17 battery modes of operation that will determine 

actions when the BATT/HEAT momentary switch is depressed (see Manual 

Number 9018047, section 4.3 that describes Sleep and Active mode of 
TB17): 

 

When the TB17 battery is in 

sleep mode, pressing the BATT/HEAT 

momentary switch lights all annunciations as depicted in Figure 5, which 

includes MAIN BATTERY, TEMP, FAULT, BATT/HEAT button, CHARGING 

and HEATING for at least 3 seconds or until the button is released  

 

When the TB17 battery is in 

active mode, pressing the BATT/HEAT 

momentary switch lights all annunciations as depicted in Figure 5, which 

includes MAIN BATTERY, TEMP, FAULT, BATT/HEAT button, CHARGING 
and HEATING until the button is released   

 

BATT/HEAT button is white backlit. Refer to the installation manual 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 over temperature sensed on battery.  Land as 
soon as practical and present the battery for 
maintenance evaluation. 

FAULT 

(AMBER) 

Blinking - when battery has experienced a recoverable 
fault. Steady - when battery has experienced a non-
recoverable fault. For steady light, present battery for 
maintenance evaluation upon landing. 

CHARGING 

(WHITE) 

Lit when battery is charging.  If battery is used as an 
emergency power source, it is recommended flight not 
be initiated until CHARGING is no longer displayed, 
indicating a state of charge greater than 95%. 

BATT/HEAT 

(WHITE) 

Lit when panel lighting input is high (pin 17) and unit is 
connected to Battery 1 (pin 11), Battery 2 (pin 12), 
and/or aircraft power (pin 13).

 

HEATING 

(WHITE) 

Lit when battery heater is activated due to unit 
temperature below 10°C and battery is in active state.  It 
is recommended that an engine start not occur until the 
HEATING annunciation turns off.

 

 

FIGURE 7 

FRONT PANEL 

 

 

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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