2 If no damage is found:
_
- do a cleaning of the connector and receptacle using a bristle brush with stoddard solvent (Material No. CP2011) (Ref. AMM TASK 73-21-50-210-002).
(b) If the failure continues during the subsequent flights:
- replace the SENSOR-N1 ROTATIONAL SPD (4000EV) (Ref. AMM TASK 77-11-10-000-002) and (Ref. AMM TASK 77-11-10-400-002).
(c) If the failure continues during the subsequent flights:
- replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
(d) If the failure continues during the subsequent flights:
- replace the HJ10 harness (Ref. AMM TASK 73-21-50-000-043) and (Ref. AMM TASK 73-21-50-400-043).
(3) If the failure message N1 SNSR, J10, ECU is confirmed: R - disconnect the HJ10 harness from the N1 sensor (N1-B connector).
R (a) Visually examine the receptacle and the connector for damaged R pins or contamination (Ref. AMM TASK 73-21-50-210-002).
1 If damage is found:
_ - repair or replace as required.
2 If no damage is found:
_ R - do the electrical resistance test through the N1 sensor R (4000EV) (channel B) between:
. pins 1 and 2 (40 to 80 ohms)
for S/N different than 25451 and up:
F 『 EEFF : ALL E ∞∞77-10-00∞∞∞∞∞∞∞∞∞∞Page 229
E E Aug 01/99 E E ECES
E
F 『
E C F M E
E E
E 56 E
E E
. pins 1 and 3 (>5 kiloohms)
R . pin 1 and the ground (>10 megohms)
for S/N 25451 and up: . pins 1 and 3 (>10 megohms)
R . pin 1 and the ground (>10 megohms).
a If the resistance values are out of the specified limits:
_
- replace the N1 sensor (4000EV) (Ref. AMM TASK 77-11-10-000-002) and (Ref. AMM TASK 77-11-10-400-002).
b If the resistance values are in the specified limits:
_ R - connect the HJ10 harness to the N1 sensor.
R (b) Disconnect the HJ10 harness from the ECU (4000KS) and visually R examine the receptacle and the connector for damaged pins or R contamination (Ref. AMM TASK 73-21-50-210-002).
1 If damage is found:
_ - repair or replace as required.
2 If no damage is found:
_ R - do the electrical resistance test through the HJ10 harness R between:
. pins 16 and 17 (40 to 80 ohms)
for S/N different than 25451 and up: . pins 16 and 6 (>5 kiloohms)
R . pin 16 and the ground (>10 megohms)
for S/N 25451 and up: . pins 16 and 6 (>10 megohms)
R . pin 16 and the ground (>10 megohms).
a If the resistance values are in the specified limits:
_
- replace the ECU (4000KS) (Ref. AMM TASK 73-21-60-000-001) and (Ref. AMM TASK 73-21-60-400-001).
b If the resistance values are out of the specified limits:
_
- replace the HJ10 harness (Ref. AMM TASK 73-21-50-000-043) and (Ref. AMM TASK 73-21-50-400-043).
B. Do the test given in Para. 3.A.
(1) No additional maintenance action is required if the fault is not confirmed.
(2) Repeat the fault isolation procedure if the fault continues.
F 『 EEFF : ALL E ∞∞77-10-00∞∞∞∞∞∞∞∞∞∞Page 230
E E Aug 01/99 E E ECES
E
F 『
E C F M E
E E
E 56 E
E E
TASK 77-10-00-810-819
Loss of N2 Feedback Signal - Engine 1 - Channel A and Channel B
1. Possible Causes
_______________
- SENSOR-N2 ROTATIONAL SPD (4001EV)
- ECU (4000KS)
- HJ7 harness
- HJ8 harness
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific bristle brush
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP2011 *
stoddard solvent (Ref. 70-30-00)
C. Referenced Information 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 發(fā)動(dòng)機(jī)指示(126)
