Removal of the Inlet Guide Vane - Actuator (8014KM)
 (131-9(A))

Installation of the Inlet Guide Vane - Actuator
 (8014KM) (131-9(A))
Removal of the Electronic Control Box (ECB)
 (131-9(A))
Installation of the Electronic Control Box (ECB)
 (131-9(A))

 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.

 「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 A262
 201-210, Config-1 Aug 01/05 CES

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

 - the MCDU menu shows
 IGV TORQUE MOTOR SHOWS OPEN CIRCUIT
 or
 IGV TORQUE MOTOR SHOWS SHORT CIRCUIT

 (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:
 IGV ACTUATOR P21
 associated with Fault Code Number (FCN) 109

 - do a check for damage/contamination of electrical connector P21 of the IGV ACTUATOR (P21).
 (1) If the electriacl connector P21 is damaged/contaminated:

 - do a repair/cleaning.

 (2) If the electrical connector is OK:

 - use a multimeter to do a resistance check across pin 4 and pin 7 of the IGV ACTUATOR (P21).
 (a) If the resistance is > 100 Ohms:

 - replace the IGV ACTUATOR (P21) (Ref. AMM TASK 49-23-51-000-004) and (Ref. AMM TASK 49-23-51-400-004).

 (b) If the resistance is > 15 Ohms and < 100 Ohms:

 - do a check and repair of the aircraft wiring between ECB (59KD) AB/G8,G9 and IGV ACTUATOR (P21) P21/4,7 (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).
 B. If the APU GND SCANNING menu gives the maintenance message:
 IGV ACTUATOR P21
 associated with Fault Code Number (FCN) 110

 - do a check for damage/contamination of electrical connector P21 of the IGV ACTUATOR (P21).
 (1) If the electriacl connector P21 is damaged/contaminated:
 - do a repair/cleaning.
 「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 A263
 201-210, Config-1 Aug 01/05 CES (2) If the electrical connector is OK:

 - use a multimeter to do a resistance check across pin 4 and pin 7 of the IGV ACTUATOR (P21), pin 4 and pin 10 of the IGV ACTUATOR (P21).
 (a) If the resistance is
 < 15 Ohms (pin 4-7)
 or
 < 100K Ohms (pin 4-10):

R - replace the IGV ACTUATOR (P21) (Ref. AMM TASK 49-23-51-000-004) R and (Ref. AMM TASK 49-23-51-400-004).
 (b) If the resistance is
 > 15 Ohms and < 100 Ohms (pin 4-7)
 and
 > 100K Ohms (pin 4-10):

 - do a check and repair of the aircraft wiring between ECB (59KD) AB/G8,G9 and IGV ACTUATOR (P21) P21/4,7 and/or IGV ACTUATOR (P21) P21/10 and aircraft GND (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:
 IGV ACTUATOR (8014KM)
 associated with Fault Code Number (FCN) 109
 - do a check for damage/contamination of electrical connector P21 of the IGV ACTUATOR (8014KM)
 (1) If the electriacl connector P21 is damaged/contaminated:

 - do a repair/cleaning.

 (2) If the electrical connector is OK:

 - use a multimeter to do a resistance check across pin 4 and pin 7 of the IGV ACTUATOR (8014KM)
 (a) If the resistance is > 100 Ohms:

 - replace the IGV ACTUATOR (8014KM) (Ref. AMM TASK 49-23-51-000-004) and (Ref. AMM TASK 49-23-51-400-004).

 (b) If the resistance is > 15 Ohms and < 100 Ohms:
　
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