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时间:2011-03-29 09:20来源:蓝天飞行翻译 作者:航空
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 (131-9(A))
 ASM 49-61/02

 3. Fault Confirmation
__________________
 A. Read-out of ECB Trouble-Shooting Data
 (1) Put the APU MASTER SW to the ON position.

 (2) Get access to the APU LAST LEG/PREVIOUS LEG report.

 (3) Push the '>' adjacent to the related CFDS failure message:


 - the MCDU menu shows:
 OIL TEMP SENSOR SHOWS OUT OF RANGE LOW
 or
 OIL TEMP SENSOR SHOWS OUT OF RANGE HIGH

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page B218
 201-210, Config-1 Aug 01/05 CES


 (4) Get access to the APU GND SCANNING menu.

 4. Fault Isolation
_______________ R **ON A/C 001-049, 101-105, 107-107, 151-154, 201-207,
 A. If the APU GND SCANNING menu gives the maintenance message:
 OIL TEMP SENSOR P11
 associated with Fault Code Number (FCN) 54 or 55

 - do a check for damage/contamination of electrical connector P11 of the OIL TEMPERATURE SENSOR (P11)
 (1) If the electrical connector P11 is damaged/contaminated:

 - do a repair/cleaning.

 (2) If the electrical connector is OK:


 - use a multimeter to do a resistance check across pin A and pin B of the OIL TEMPERATURE SENSOR (P11).
 (a) If the resistance value is not between 60 Ohms to 200 Ohms:

 - replace the OIL TEMPERATURE SENSOR (P11) (Ref. AMM TASK 49-94-15-000-001) and (Ref. AMM TASK 49-94-15-400-001).

 (b) If the resistance value is between 60 Ohms and 200 Ohms:


 - do a check and repair of the aircraft wiring from the ECB (59KD) AB/J5,B8 to the OIL TEMPERATURE SENSOR (P11) P11/A,B (Ref. ASM 49-61/02).
 1 If the fault continues:
_
 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-003) and (Ref. AMM TASK 49-61-34-400-003).
 **ON A/C 001-049, 101-105, 151-199, 201-210,
 Post SB 49-1062 For A/C 001-049,101-105,151-154,201-207,

 A. If the APU GND SCANNING menu gives the maintenance message: NOTE : With introduction of the ECB Software V2 the wording of the fault
____ message Oil Sump Temp Sensor (8084KM) is not correct. The functional item number of the Oil Temperature Sensor is (8092KM).
 OIL SUMP TEMP SENSOR (8084KM)
 associated with Fault Code Number (FCN) 54 or 55
 - do a check for damage/contamination of electrical connector P11 of the OIL TEMP SENSOR (8092KM)
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page B219
 201-210, Config-1 Aug 01/05 CES


 (1) If the electrical connector P11 is damaged/contaminated:

 - do a repair/cleaning.

 (2) If the electrical connector is OK:


 - use a multimeter to do a resistance check across pin A and pin B of the OIL SUMP TEMP SENSOR (8084KM).
 (a) If the resistance value is not between 60 Ohms to 200 Ohms:
 - replace the OIL TEMP SENSOR (8092KM)
 (Ref. AMM TASK 49-94-15-000-001) (Ref. AMM TASK 49-94-15-400-001).
 (b) If the resistance value is between 60 Ohms and 200 Ohms:
 - do a check and repair of the aircraft wiring from the ECB (59KD) AB/J5,B8 to the OIL TEMP SENSOR (8092KM) P11/A,B (Ref. ASM 49-61/02).
 1 If the fault continues:
_
 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-003) (Ref. AMM TASK 49-61-34-400-003).
R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
 B. Do a check of the APU GND SCANNING menu to verify the fault is not present.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page B220
 201-210, Config-1 Aug 01/05 CES

 TASK 49-00-81-810-870


 APU Oil-Heater (P28) Fault (131-9(A))
 1. Possible Causes
_______________
 - OIL HEATER FAILURE

 - damage/contamination of electrical connector P28

 - APU OIL HEATER (P28)

 - APU AUX CTL RELAY (32KD)

 - aircraft wiring

 - SERVICE BUS 2 (214XP-B)

 - APU OIL HEATER (8093KM)


 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
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