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 -replace the VALVE-BLEED PRESS REG (4001HA) (Ref. AMM TASK 36-11-52-000-040) and (Ref. AMM TASK 36-11-52-400-040).
 (a) If the fault continues:
 -replace the VALVE-OVERPRESSURE, ENG 1 (5HA1) (Ref. AMM TASK 36-11-53-000-001) and (Ref. AMM TASK 36-11-53-400-001).
 B. After the subsequent flight, make sure that the fault does not continue.
 1 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A234
 --Feb 01/05 ---CES - High Bleed Pressure of the Engine 1 in Cruise

 

 1. Possible Causes
_______________

 -VALVE-HP BLEED (4000HA)
 -XDCR-BLEED REGULATED PRESS, ENG 1 (8HA1)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 36-11-00-740-001 BITE Test of the BMC 1(2) AMM 36-11-16-000-001 Removal of the Bleed Regulated Pressure Transducer (8HA1,8HA2) AMM 36-11-16-400-001 Installation of the Bleed Regulated Pressure
 Transducer (8HA1,8HA2) 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) 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-HP BLEED (4000HA) (Ref. AMM TASK 36-11-51-000-040) and (Ref. AMM TASK 36-11-51-400-040).
 (a) If the fault continues:
 -replace the XDCR-BLEED REGULATED PRESS, ENG 1 (8HA1) (Ref. AMM TASK 36-11-16-000-001) and (Ref. AMM TASK 36-11-16-400-001).
 B. After the subsequent flight, make sure that the fault does not continue.
 1
 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A235
 --Feb 01/05R ---CES -

 

 Low Bleed Pressure of the Engine 1 in Climb
 1. Possible Causes
_______________

 -SOLENOID-BLEED PRESS REG V CTL, ENG 1 (10HA1)
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 36-11-00-740-001 BITE Test of the BMC 1(2) AMM 36-11-55-000-001 Removal of the Bleed-Pressure-Regulator Valve Control-Solenoid (10HA1,10HA2) AMM 36-11-55-400-001 Installation of the Bleed-Pressure-Regulator Valve Control-Solenoid (10HA1,10HA2) 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 SOLENOID-BLEED PRESS REG V CTL, ENG 1 (10HA1) (Ref. AMM TASK 36-11-55-000-001) and (Ref. AMM TASK 36-11-55-400-001).
 B. After the subsequent flight, make sure that the fault does not continue.
 1
 -EFF : ALL

-∞∞36-11-00∞∞∞∞∞∞∞∞∞∞Page A236
 --Feb 01/05R ---CES -

 

 Low Bleed Pressure of the Engine 1 in Cruise
 1. Possible Causes_______________
 -VALVE-BLEED PRESS REG (4001HA)
 -XDCR-BLEED REGULATED PRESS, ENG 1 (8HA1)
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
AMM 36-11-00-740-001  BITE Test of the BMC 1(2)
 AMM 36-11-16-000-001  Removal of the Bleed Regulated Pressure Transducer (8HA1,8HA2)
 AMM 36-11-16-400-001  Installation of the Bleed Regulated Pressure Transducer (8HA1,8HA2)
 AMM 36-11-52-000-040  Removal of the Bleed Pressure-Regulator Valve (4001HA)
 AMM 36-11-52-400-040  Installation of the Bleed Pressure-Regulator Valve (4001HA)
 TSM 36 PB 101
　
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