-EFF : ALL --
-CES
APU AUTO SHUT DOWN - IGV FAILURE, Inlet Guide Vanes
Fault (GTCP36-300)
Differential Pressure-Sensor Fault (GTCP 36-300)
Total Pressure-Sensor Fault (GTCP 36-300)
Load Control-Valve Fault (GTCP 36-300)
Surge Control-Valve Fault (GTCP 36-300)
No APU Bleed-Air Pressure, Low or Fluctuating APU
Bleed-Air Pressure (GTCP 36-300)
No APU Bleed-Air Pressure, Low or Fluctuating APU
Bleed-Air Pressure (with AIDS Support) (GTCP 36-300)
Bleed Flow-Transducer Fault (APS 3200)
APU AUTO SHUT DOWN - SURGE /REVERSE FLOW, Bleed
 Control Valve Fault (APS3200)
APU AUTO SHUT DOWN - OVERTEMPERATURE, Inlet Guide
 Vane Actuator Fault (APS 3200)
Load-Compressor Discharge Temperature-Sensor Fault
 (APS 3200)
Inlet Pressure/Temperature Sensor Fault (APS 3200)
No APU Bleed-Air Pressure, Low or Fluctuating APU
 Bleed-Air Pressure (APS 3200)
Inlet-Guide Vane-Actuator (P21) Fault (131-9(A))
Differential-Pressure Transducer (P24) Fault
 (131-9(A))
Total-Pressure Transducer (P23) Fault (131-9(A))
Load-Control Valve (P12) Fault (131-9(A))
Bleed Shutoff due to Reverse Flow Condition
 (131-9(A))
Surge Control Valve (P18) Fault (131-9(A))
Bleed Load-Valve Position-Switch Fault (GTCP 36-300)

 1

-∞∞36-12-00∞∞∞∞∞∞∞∞∞∞Page 201
-May 01/05--

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM  24-41-00-861-002  Energize the Aircraft Electrical Circuits from the External Power
 AMM  24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied from the External Power
 AMM  31-60-00-860-001  EIS Start Procedure
R R R R R R R  AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM ASM  36-11-34-000-001 36-11-34-400-001 49-00-00-710-001 49-00-00-710-005 49-00-00-710-009 49-00-00-860-003 49-00-00-860-004 49-00-00-860-005 49-00-00-860-006 49-00-00-860-008 49-00-00-860-009 49-61-34-000-001 49-61-34-000-002 49-61-34-000-003 49-61-34-400-001 49-61-34-400-002 49-61-34-400-003 36-12/00 Removal of the BMC (1HA1, 1HA2)Installation of the BMC (1HA1, 1HA2) Self-Test of the ECB (59KD) (GTCP 36-300)Self-Test of the ECB (APS 3200)Self-Test of the ECB (131-9(A)) APU Start by External Power (GTCP 36-300) APU Shutdown by External Power (GTCP 36-300)APU Start by External Power (APS 3200)APU Shutdown by External Power (APS 3200)APU Start by External Power (131-9(A))APU Shutdown by External Power (131-9(A)) Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300)Removal of the Electronic Control Box (ECB) (59KD) (APS 3200)Removal of the Electronic Control Box (ECB) (131-9(A)) Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300)Installation of the Electronic Control Box (ECB) (59KD) (APS 3200)Installation of the Electronic Control Box (ECB) (131-9(A))
 3. Fault Confirmation__________________
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------
PANEL  DESIGNATION  IDENT. LOCATION
 -------------------------------------------------------------------------------
49VU AIR BLEED/X FEED/VALVE/BAT 49VU AIR BLEED/ENG 1/CTL 49VU AIR BLEED/ENG 1/MONG 121VU APU/APU/CTL 121VU APU/ECB/SPLY 122VU AIR BLEED/ENG 2/CTL 122VU AIR BLEED/ENG 2/MONG 122VU AIR BLEED/X FEED VALVE/NORM  2HV 3HA1 2HA1 2KD 1KD 3HA2 2HA2 1HV  D13D12D11L42L41Z23Z22Z20

 1 -EFF : ALL

-∞∞36-12-00∞∞∞∞∞∞∞∞∞∞Page 202
 --May 01/05 ---CES - B. Aircraft Maintenance Configuration

 (1)
 Energize the aircraft electrical circuits
 (Ref. AMM TASK 24-41-00-861-002)

 (2)
 Do the EIS start procedure (Ref. AMM TASK 31-60-00-860-001).

 (3)
 On panel 30VU, make sure that the OFF legends on the PACK 1 and PACK 2 pushbutton switches are on.

R **ON A/C 001-049, 101-105, 151-199, 201-210,
 C. Test

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 Do the self test of the ECB (Ref. AMM TASK 49-00-00-710-009).

 2.
 Start the APU (Ref. AMM TASK 49-00-00-860-008).
　
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