APU AUTO SHUTDOWN - INLET OVERHEAT, APU Inlet Temperature higher than Limit (131-9(A))
TASK 49-00-81-810-843-A
APU AUTO SHUTDOWN - INLET OVERHEAT, APU Inlet Temperature higher than Limit (131-9(A))
1. Possible Causes
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Fault Confirmation
Subtask 49-00-81-710-176-A ** ON A/C NOT FOR ALL
Subtask 49-00-81-810-124-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:40:39 UTC
APU AUTO SHUTDOWN - INLET OVERHEAT, APU Inlet Temperature higher than Limit (131-9(A))
1. Possible Causes
- NO LRU FAULT DETECTED
- blockage of the APU inlet
- fire of the APU inlet
damage/contamination of the electrical connector P6 - aircraft wiring
APU INLET TEMPERATURE SENSOR (P6) - ELECTRONIC CONTROL BOX [59KD]
- APU [4005KM]
APU INLET TEMPERATURE SENSOR (8010KM).
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | JUMPER-WIRE |
| No specific | AR | MULTIMETER - STANDARD |
| REFERENCE | DESIGNATION |
|---|---|
| AMM 49-00-00-860-008 | APU Start by External Power |
| AMM 49-11-11-000-004 | Removal of the Power Plant (APU) (131-9(A)) |
| AMM 49-11-11-400-004 | Installation of the Power Plant (APU) (131-9(A)) |
| AMM 49-23-14-000-001 | Removal of the Sensor-APU Inlet Temperature (131-9(A)) |
| AMM 49-23-14-400-001 | Installation of the Sensor-APU Inlet Temperature (131-9(A)) |
| AMM 49-61-34-000-003 | Removal of the Electronic Control Box (ECB) (131-9(A)) |
| AMM 49-61-34-400-003 | Installation of the Electronic Control Box (ECB) (131-9(A)) |
Subtask 49-00-81-710-176-A ** ON A/C NOT FOR ALL
A. Read-out of ECB Trouble-Shooting Data
(1) Put the APU MASTER SW to the ON position.
(2) Get access to the APU SHUTDOWN report.
(3) Push the '>' adjacent to LRU DATA:
4. Fault Isolation(1) Put the APU MASTER SW to the ON position.
(2) Get access to the APU SHUTDOWN report.
(3) Push the '>' adjacent to LRU DATA:
- the MCDU menu shows
NO LRU FAULT DETECTED
Subtask 49-00-81-810-124-A ** ON A/C NOT FOR ALL
A. If an APU auto shutdown occurs during the APU operation and the APU SHUTDOWN report gives the maintenance message:
INLET OVERHEAT
CHECK APU INLET
associated with Fault Code Numbers (FCN) 213
Subtask 49-00-81-810-124-B ** ON A/C NOT FOR ALL INLET OVERHEAT
CHECK APU INLET
associated with Fault Code Numbers (FCN) 213
- do a check for blockage of the APU inlet .
- do a check for a fire of the APU inlet :
- do a check of the inlet plenum for fire damage.
- do a check of the APU inlet duct through the inlet flap for fire damage.
- replace the APU (4005KM) AMM 49-11-11-000-004 and AMM 49-11-11-400-004.
- do a check for
damage/contamination of the electrical connector P6 of the APU INLET TEMPERATURE SENSOR (P6).
- do a repair/cleaning.
- disconnect the electrical connector P6
- put a JUMPER-WIRE across the sockets A and B of the electrical connector P6.
- use a MULTIMETER - STANDARD to do a resistance check of the aircraft wiring across the ECB (59KD) AB/H4 to ECB (59KD) AB/H3.
- replace the aircraft wiring.
- replace th
APU INLET TEMPERATURE SENSOR (P6) AMM 49-23-14-000-001 and AMM 49-23-14-400-001.
- replace the ELECTRONIC CONTROL BOX [59KD] of the APU [4005KM] AMM 49-61-34-000-003 and AMM 49-61-34-400-003.
A. If an APU auto shutdown occurs during the APU operation and the APU SHUTDOWN report gives the maintenance message:
INLET OVERHEAT
CHECK APU INLET
associated with Fault Code Numbers (FCN) 213
Subtask 49-00-81-710-177-A ** ON A/C NOT FOR ALL INLET OVERHEAT
CHECK APU INLET
associated with Fault Code Numbers (FCN) 213
- do a check for blockage of the APU inlet .
- do a check for a fire of the APU inlet :
- do a check of the inlet plenum for fire damage.
- do a check of the APU inlet duct through the inlet flap for fire damage.
- replace the APU (4005KM) AMM 49-11-11-000-004 and AMM 49-11-11-400-004.
- do a check for
damage/contamination of the electrical connector P6 of the APU INLET TEMPERATURE SENSOR (8010KM).
- do a repair/cleaning.
- disconnect the electrical connector P6
- put a JUMPER-WIRE across the sockets A and B of the electrical connector P6.
- use a MULTIMETER - STANDARD to do a resistance check of the aircraft wiring across the ECB (59KD) AB/H4 to ECB (59KD) AB/H3.
- replace the aircraft wiring.
- replace th
APU INLET TEMPERATURE SENSOR (8010KM). AMM 49-23-14-000-001 and AMM 49-23-14-400-001.
- replace the ELECTRONIC CONTROL BOX [59KD] of the APU [4005KM] AMM 49-61-34-000-003 and AMM 49-61-34-400-003.
B. Do the test given in Para. 3.