Ignition System Test
Figure 501/TASK 74-00-00-991-300
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Ignition System Test Figure 502/TASK 74-00-00-991-301-A
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-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
(Ref. Fig. 502/TASK 74-00-00-991-
301-A)
3. On the panel 115VU:
- Make sure that the ENG/MODE selector switch is in the NORM position.
4. Set the ENG/MASTER 1 (2) control switch to ON.
5. Push the line key adjacent to the PUSH BUTTON TO START TEST indication. (Ref. Fig. 502/TASK 74-00-00-991-
301-A)
6. Set the ENG/MASTER 1 (2) control switch to OFF.
7. Push the line key adjacent to the RETURN indication.
8. Do the procedure again for the channel B of the FADEC 1 (2).
(Ref. Fig. 502/TASK 74-00-00-991-301-A)
- The CAUTION: IGNITERS WILL CYCLEDURING TEST IGNITER A TESTED THEN Bindication comes into view
(Ref. Fig. 502/TASK 74-00-00-991-301-A)
- IGNITER A THEN B WILL CYCLE FOR 10 SECS EACH. Make sure that igniter 1 of the engine 1(2) makes noise for 10 seconds and after about 2 seconds the igniter 2 of the engine 1(2) makes noise for 10 seconds.
- TEST COMPLETE comes into view. When the test is finished (Ref. Fig. 502/TASK 74-00-00-991-301-A)
- The ENGINE menu comes into view.
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-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
9. On the MCDU, push the line key
adjacent to the RETURN indication
until the CFDS menu page comes
into view.
10. Stop the MCDU.
R **ON A/C 151-154,
Subtask 74-00-00-710-050-A
A. Do this test :
WARNING : MAKE SURE THERE IS NO AIR PRESSURE SUPPLIED AT THE STARTER
_______
VALVE INLET.
NOTE : This test is for the system 1. For the other system(s), use the
____
indications between the parentheses.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:
- Push the line key adjacent to the FADEC 1A (2A) indication.
2. Push the line key adjacent to the IGN TEST indication. (Ref. Fig. 502/TASK 74-00-00-991-
301-A)
3. On the ENG PNL 115VU:
- Make sure that the ENG/MODE selector switch is in the NORM position.
- The ENGINE 1(2) MAIN MENU page comesinto view. (Ref. Fig. 502/TASK 74-00-00-991-301-A)
- The IGNITION TEST menu comes intoview.
(Ref. Fig. 502/TASK 74-00-00-991-301-A)
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4. Set the ENG/MASTER 1 (2) control switch to ON.
5. Push the line key adjacent to the PUSH BUTTON TO START TEST
indication.
(Ref. Fig. 502/TASK 74-00-00-991-301-A)
6. Set the ENG/MASTER 1 (2) control switch to OFF.
7. Push the line key adjacent to the RETURN indication.
8. Do the procedure again for the channel B of the FADEC 1 (2).
9. On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
10. Stop the MCDU.
- The WARNING TEST ACTIVE indicationcomes into view (Ref. Fig. 502/TASK 74-00-00-991-301-A)
- IGNITER 1 and 2 will cycle once for 10 seconds. Make sure that igniter 1 of the engine 1(2) makes noise for 10 seconds and after about 2 seconds the igniter 2 of the engine 1(2) makes noise for 10 seconds. 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM IGNITION 點(diǎn)火(5)
