-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A245
 --Feb 01/05R ---CES -

 High Bleed Temperature of the Engine 1 in Climb
 1. Possible Causes_______________
 -THERMOSTAT-FAN AIR VALVE CTL (7170HM1)
 -EXCHANGER-BLEED AIR PRECOOL (7150HM1)
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM 36-11-00-740-001  BITE Test of the BMC 1(2)
 AMM 36-11-42-000-001  Removal of the Bleed-Air Precooler Exchanger (7150HM1,7150HM2)
 AMM 36-11-42-400-001  Installation of the Bleed-Air Precooler Exchanger (7150HM1,7150HM2)
 AMM 36-11-43-000-001  Removal of the Fan Air Valve Control Thermostat (7170HM1, 7170HM2)
 AMM 36-11-43-400-001  Installation of the Fan Air Valve Control Thermostat (7170HM1, 7170HM2)
 TSM 36 PB 101
 3. Fault Confirmation__________________
 A. Test
 (1) Do the BITE test of the BMC1 (Ref. AMM TASK 36-11-00-740-001).
 4. Fault Isolation_______________
 A. If the test gives a maintenance message, you can find the related trouble shooting procedure in the (Ref. TSM 36 PB 101).
 (1) If there is no maintenance message:
 -replace the THERMOSTAT-FAN AIR VALVE CTL (7170HM1) (Ref. AMM TASK 36-11-43-000-001) and (Ref. AMM TASK 36-11-43-400-001).
 (a) If the fault continues:
 -replace the EXCHANGER-BLEED AIR PRECOOL (7150HM1) (Ref. AMM TASK 36-11-42-000-001) and (Ref. AMM TASK 36-11-42-400-001).
 B. After the subsequent flight, make sure that the fault does not continue.
 1
 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A246
 --Feb 01/05R ---CES -

 High Bleed Temperature of the Engine 1 in Cruise
 1. Possible Causes
_______________

 -VALVE-FAN AIR, ENG1 (9HA1)
 -VALVE-HP BLEED (4000HA)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 36-11-00-740-001 BITE Test of the BMC 1(2)
 AMM 36-11-51-000-040 Removal of the High Pressure Bleed Valve (4000HA)
 AMM 36-11-51-400-040 Installation of the High Pressure Bleed Valve

 (4000HA) AMM 36-11-54-000-001 Removal of the Fan Air Valve (9HA1,9HA2) AMM 36-11-54-400-001 Installation of the Fan Air Valve (9HA1,9HA2) TSM 36 PB 101
 3. Fault Confirmation
__________________
 A. Test

 (1) Do the BITE test of the BMC1 (Ref. AMM TASK 36-11-00-740-001).
 4. Fault Isolation
_______________

 A. If the test gives a maintenance message, you can find the related trouble shooting procedure in the (Ref. TSM 36 PB 101).
 (1) If there is no maintenance message:
 -replace the VALVE-FAN AIR, ENG1 (9HA1) (Ref. AMM TASK 36-11-54-000-001) and (Ref. AMM TASK 36-11-54-400-001).
 (a) If the fault continues:
 -replace the VALVE-HP BLEED (4000HA) (Ref. AMM TASK 36-11-51-000-040) and (Ref. AMM TASK 36-11-51-400-040).
 B. After the subsequent flight, make sure that the fault does not continue.
 1
 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A247
 --Feb 01/05R ---CES -

 High Bleed Temperature of the Engine 1 in Descent
 1. Possible Causes
_______________

 -SENSOR-EXCHANGER OUT TEMP, ENG 1 (6HA1)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 36-11-00-740-001 BITE Test of the BMC 1(2) AMM 36-11-17-000-001 Removal of the Heat-Exchanger Outlet-Temperature Sensor 6HA1(6HA2) AMM 36-11-17-400-001 Installation of the Heat-Exchanger Outlet-Temperature Sensor 6HA1(6HA2) TSM 36 PB 101
 3. Fault Confirmation
__________________
 A. Test

 (1) Do the BITE test of the BMC1 (Ref. AMM TASK 36-11-00-740-001).
　
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