36-11 ENGINE BLEED AIR SUPPLY SYSTEM

36-11-00 ENGINE BLEED AIR SUPPLY SYSTEM

PB.201 ENGINE BLEED AIR SUPPLY SYSTEM - FAULT ISOLATION PROCEDURES
- 36-11-00-810-801-A [8]
  Loss of the BMC1
- 36-11-00-810-802-A [8]
  High Pressure Bleed Valve of the Engine 1 Blocked in the Open Position
- 36-11-00-810-803-A [8]
  Fan Air Valve of the Engine 1 Not in Fully Open Position
- 36-11-00-810-803-A-01 [8]
  Fan Air Valve of the Engine 1 Not in Fully Open Position
- 36-11-00-810-804-A [8]
  Loss of the BMC2
- 36-11-00-810-805-A [8]
  High Pressure Bleed Valve of the Engine 2 Blocked in the Open Position
- 36-11-00-810-806-A [8]
  Fan Air Valve of the Engine 2 Not in Fully Open Position
- 36-11-00-810-806-A-01 [8]
  Fan Air Valve of the Engine 2 Not in Fully Open Position
- 36-11-00-810-807-A [8]
  Bleed Pressure-Regulator Valve of the Engine 1 Blocked in the Open Position or Regulation Failure
- 36-11-00-810-808-A [8]
  Bleed Pressure-Regulator Valve of the Engine 2 Blocked in the Open Position or Regulation Failure
- 36-11-00-810-809-A [8]
  Bleed Pressure-Regulator Valve of the Engine 1 Blocked in the Closed Position or Regulation Too Low
- 36-11-00-810-810-A [8]
  Bleed Pressure-Regulator Valve of the Engine 2 Blocked in the Closed Position or Regulation Too Low
- 36-11-00-810-811-A [8]
  Overpressure Valve of the Engine 1 Blocked in the not Fully Open Position
- 36-11-00-810-812-A [8]
  Overpressure Valve of the Engine 2 Blocked in the not Fully Open Position
- 36-11-00-810-813-A [8]
  Loss of Automatic Electrical Closure for the Bleed Pressure Regulator Valve on Engine 1
- 36-11-00-810-814-A [8]
  Loss of Automatic Electrical Closure for the Bleed Pressure Regulator Valve on Engine 2
- 36-11-00-810-817-A [8]
  Loss of the Bleed Transferred-Pressure Transducer of the Engine 1
- 36-11-00-810-818-A [8]
  Loss of the Bleed Transferred-Pressure Transducer of the Engine 2
- 36-11-00-810-819-A [8]
  Loss of the Bleed Regulated-Pressure Transducer of the Engine 1
- 36-11-00-810-820-A [8]
  Loss of the Bleed Regulated-Pressure Transducer of the Engine 2
- 36-11-00-810-821-A [8]
  Shift of Calibration of the Bleed Regulated-Pressure Transducer of the Engine 1
- 36-11-00-810-822-A [8]
  Shift of Calibration of the Bleed Regulated-Pressure Transducer of the Engine 2
- 36-11-00-810-823-A [8]
  Bleed Pressure-Regulator Valve of the Engine 1 not Fully Closed
- 36-11-00-810-824-A [8]
  Bleed Pressure-Regulator Valve of the Engine 2 not Fully Closed
- 36-11-00-810-825-A [8]
  Loss of One Sensing Element of the Exchanger Outlet Temperature-Sensor of the Engine 1
- 36-11-00-810-826-A [8]
  Loss of One Sensing Element of the Exchanger Outlet Temperature-Sensor of the Engine 2
- 36-11-00-810-827-A [8]
  Loss of the Two Sensing Elements of the Exchanger Outlet Temperature-Sensor of the Engine 1
- 36-11-00-810-828-A [8]
  Loss of the Two Sensing Elements of the Exchanger Outlet Temperature-Sensor of the Engine 2
- 36-11-00-810-829-A [8]
  Loss of the Non-Return Function and Temperature Limitation Function of the Bleed Pressure-Regulator Valve of the Engine 1
- 36-11-00-810-830-A [8]
  Loss of the Non-Return Function and Temperature Limitation Function of the Bleed Pressure-Regulator Valve of the Engine 2
- 36-11-00-810-831-A [8]
  Loss of the Manual Electrical Closure of the Bleed Pressure-Regulator Valve of the Engine 1
- 36-11-00-810-832-A [8]
  Loss of the Manual Electrical Closure of the Bleed Pressure-Regulator Valve of the Engine 2
- 36-11-00-810-833-A [8]
  Loss of the Coupling between the HP Bleed Valve and the Bleed Pressure-Regulator Valve of the Engine 1
- 36-11-00-810-834-A [8]
  Loss of the Coupling between the HP Bleed Valve and the Bleed Pressure-Regulator Valve of the Engine 2
- 36-11-00-810-835-A [8]
  HP Bleed Valve of the Engine 1 Blocked in the Open Position
- 36-11-00-810-836-A [8]
  HP Bleed Valve of the Engine 2 Blocked in the Open Position
- 36-11-00-810-837-A [8]
  Failure of the HP Bleed Valve of the Engine 1 Blocked in the Closed Position
- 36-11-00-810-838-A [8]
  Failure of the HP Bleed Valve of the Engine 2 Blocked in the Closed Position
- 36-11-00-810-839-A [8]
  HP Bleed Valve Locked in the Not Fully Open Position on the Engine 1
- 36-11-00-810-840-A [8]
  HP Bleed Valve Locked in the Not Fully Open Position on the Engine 2
- 36-11-00-810-841-A [8]
  Loss of the Coupling between the HP Bleed Valve of the Engine 1 and the Related Closure Control Solenoid
- 36-11-00-810-842-A [8]
  Loss of the Coupling between the HP Bleed Valve of the Engine 2 and the Related Closure Control Solenoid
- 36-11-00-810-843-A [8]
  Overpressure Valve of the Engine 1 Blocked in the Open Position
- 36-11-00-810-844-A [8]
  Overpressure Valve of the Engine 2 Blocked in the Open Position
- 36-11-00-810-845-A [8]
  Fan Air Valve of the Engine 1 Blocked in the Open Position
- 36-11-00-810-846-A [8]
  Fan Air Valve of the Engine 2 Blocked in the Open Position
- 36-11-00-810-847-A [8]
  Fan Air Valve of the Engine 1 Not in Fully Open Position
- 36-11-00-810-848-A [8]
  Fan Air Valve of the Engine 2 Not in Fully Open Position
- 36-11-00-810-849-A [8]
  Fan Air Valve of the Engine 1 Blocked in the Open Position
- 36-11-00-810-850-A [8]
  Fan Air Valve of the Engine 2 Blocked in the Open Position
- 36-11-00-810-851-A [8]
  Loss of the BMC1
- 36-11-00-810-852-A [8]
  Loss of the BMC2
- 36-11-00-810-853-A [8]
  Loss of the Power Supply of the Bleed Pressure-Regulator Valve of the Engine 1
- 36-11-00-810-854-A [8]
  Loss of the Power Supply of the Bleed Pressure-Regulator Valve of the Engine 2
- 36-11-00-810-855-A [8]
  Loss of the Bus from the EIU1
- 36-11-00-810-856-A [8]
  Loss of the Bus from the EIU2
- 36-11-00-810-857-A [8]
  Loss of the Bus from the CFDIU to the BMC1
- 36-11-00-810-858-A [8]
  Loss of the Bus from the CFDIU to the BMC2
- 36-11-00-810-859-A [8]
  Loss of the Engine Validity Signal between the EIU1 and the BMC1
- 36-11-00-810-860-A [8]
  Loss of the Engine Validity Signal between the EIU2 and the BMC2
- 36-11-00-810-861-A [8]
  Failure of the Bleed Air Precooler-Exchanger of the Engine 1
- 36-11-00-810-862-A [8]
  Failure of the Bleed Air Precooler-Exchanger of the Engine 2
- 36-11-00-810-863-A [8]
  Loss of or Accidental Automatic Closure of the Bleed Pressure-Regulator Valve of the Engine 1
- 36-11-00-810-864-A [8]
  Loss of or Accidental Electrical Closure of the Bleed Pressure-Regulator Valve of the Engine 2
- 36-11-00-810-870-A [8]
  Fan Air Valves of the Engine 1 and Engine 2 Blocked in the Open Position
- 36-11-00-810-871-A [8]
  High Bleed Pressure of the Engine 1 in Climb
- 36-11-00-810-872-A [8]
  High Bleed Pressure of the Engine 1 in Cruise
- 36-11-00-810-873-A [8]
  Low Bleed Pressure of the Engine 1 in Climb
- 36-11-00-810-874-A [8]
  Low Bleed Pressure of the Engine 1 in Cruise
- 36-11-00-810-875-A [8]
  Low Bleed Pressure of the Engine 1 in Descent/Taxi
- 36-11-00-810-876-A [8]
  Loss of the Bleed Pressure Monitoring of the Engine 1
- 36-11-00-810-877-A [8]
  High Bleed Pressure of the Engine 2 in Climb
- 36-11-00-810-878-A [8]
  High Bleed Pressure of the Engine 2 in Cruise
- 36-11-00-810-879-A [8]
  Low Bleed Pressure of the Engine 2 in Climb
- 36-11-00-810-880-A [8]
  Low Bleed Pressure of the Engine 2 in Cruise
- 36-11-00-810-881-A [8]
  Low Bleed Pressure of the Engine 2 in Descent/Taxi
- 36-11-00-810-882-A [8]
  Loss of the Bleed Pressure Monitoring of the Engine 2
- 36-11-00-810-883-A [8]
  High Bleed Temperature of the Engine 1 in Climb
- 36-11-00-810-884-A [8]
  High Bleed Temperature of the Engine 1 in Cruise
- 36-11-00-810-885-A [8]
  High Bleed Temperature of the Engine 1 in Descent
- 36-11-00-810-886-A [8]
  Low Bleed Temperature of the Engine 1 in Climb
- 36-11-00-810-887-A [8]
  Low Bleed Temperature of the Engine 1 in Cruise
- 36-11-00-810-888-A [8]
  Low Bleed Temperature of the Engine 1 in Descent
- 36-11-00-810-889-A [8]
  Loss of the Bleed Temperature Monitoring of the Engine 1
- 36-11-00-810-890-A [8]
  High Bleed Temperature of the Engine 2 in Climb
- 36-11-00-810-891-A [8]
  High Bleed Temperature of the Engine 2 in Cruise
- 36-11-00-810-892-A [8]
  High Bleed Temperature of the Engine 2 in Descent
- 36-11-00-810-893-A [8]
  Low Bleed Temperature of the Engine 2 in Climb
- 36-11-00-810-894-A [8]
  Low Bleed Temperature of the Engine 2 in Cruise
- 36-11-00-810-895-A [8]
  Low Bleed Temperature of the Engine 2 in Descent
- 36-11-00-810-896-A [8]
  Loss of the Bleed Temperature Monitoring of the Engine 2
- 36-11-00-810-897-A [8]
  Small Variation of the Bleed Pressure Indication
- 36-11-00-810-898-A [8]
  Variation of the Bleed Pressure Indication for the Engine 1
- 36-11-00-810-899-A [8]
  Variation of the Bleed Pressure Indication for the Engine 2
- 36-11-00-810-900-A [8]
  High Variation of the Bleed Pressure Indication for the Engine 1
- 36-11-00-810-901-A [8]
  High Variation of the Bleed Pressure Indication for the Engine 2
- 36-11-00-810-902-A [8]
  The Bleed Pressure-Regulator Valve of the Engine 1 is Shown Open Amber on the Lower ECAM DU
- 36-11-00-810-903-A [8]
  The Bleed Pressure-Regulator Valve of the Engine 1 is Shown Closed Amber on the Lower ECAM DU
- 36-11-00-810-904-A [8]
  The HP Bleed Valve of the Engine 1 is Shown Closed Amber on the Lower ECAM DU
- 36-11-00-810-905-A [8]
  Amber XX on the Lower ECAM DU Replace the Position Indication of the Bleed Pressure-Regulator Valve of the Engine 1
- 36-11-00-810-906-A [8]
  Amber XX on the Lower ECAM DU Replace the Position Indication of the HP Bleed Valve of the Engine 1
- 36-11-00-810-907-A [8]
  The Bleed Pressure-Regulator Valve of the Engine 2 is Shown Open Amber on the Lower ECAM DU
- 36-11-00-810-908-A [8]
  The Bleed Pressure-Regulator Valve of the Engine 2 is Shown Closed Amber on the Lower ECAM DU
- 36-11-00-810-909-A [8]
  The HP Bleed Valve of the Engine 2 is Shown Closed Amber on the Lower ECAM DU
- 36-11-00-810-910-A [8]
  Amber XX on the Lower ECAM DU Replace the Position Indication of the Bleed Pressure-Regulator Valve of the Engine 2
- 36-11-00-810-911-A [8]
  Amber XX on the Lower ECAM DU Replace the Position Indication of the HP Bleed Valve of the Engine 2
- 36-11-00-810-912-A [8]
  Internal Failure of the BMC1
- 36-11-00-810-913-A [8]
  Internal Failure of the BMC2
- 36-11-00-810-919-A [8]
  Loss of the 2nd BMC (the 1st is lost)
- 36-11-00-810-926-A [8]
  Loss of the Bleed Regulated-Pressure Transducer of the Engine 1 (Detected by BMC2)
- 36-11-00-810-927-A [8]
  Loss of the Bleed Regulator-Pressure Transducer of the Engine 2 (Detected by BMC1)
- 36-11-00-810-928-A [8]
  Abnormal Bleed Temperature Shown Amber during BMC1 Test with the Engines Not in Operation
- 36-11-00-810-929-A [8]
  Abnormal Bleed Temperature Shown Amber during BMC2 Test with the Engines Not in Operation
- 36-11-00-810-930-A [8]
  BMC1 output failure for HP Bleed Override Solenoid of Engine 1
- 36-11-00-810-931-A [8]
  BMC2 output failure for HP Bleed Override Solenoid of Engine 2
- 36-11-00-810-936-A [8]
  HP Bleed Valve blocked in the closed position or regulation too low on Engine 1 without associated maintenance message
- 36-11-00-810-937-A [8]
  HP Bleed Valve blocked in the closed position or regulation too low on Engine 2 without associated maintenance message
- 36-11-00-810-938-A [8]
  High bleed pressure fluctuation on Engine 1 at take-off or climb phase
- 36-11-00-810-939-A [8]
  High bleed pressure fluctuation on Engine 2 at take-off or climb phase
- 36-11-00-810-944-A [8]
  Failure of the Bleed Pressure Regulator Valve Control Solenoid or its Wiring
- 36-11-00-810-945-A [8]
  Failure of the Overpressure Valve in Closed Position on the Engine 1
- 36-11-00-810-946-A [8]
  Failure of the Overpressure Valve in Closed Position on the Engine 2
- 36-11-00-810-951-A [8]
  Spurious APU leak indication on the Engine 1
- 36-11-00-810-952-A [8]
  Spurious APU leak indication on the Engine 2
- 36-11-00-810-953-A [8]
  Drift of the Engine 1 Bleed Regulated Pressure Transducer
- 36-11-00-810-954-A [8]
  Drift of the Engine 2 Bleed Regulated Pressure Transducer
- 36-11-00-810-955-A [8]
  Drift of the Engine 1 Bleed Transferred Pressure Transducer
- 36-11-00-810-956-A [8]
  Drift of the Engine 2 Bleed Transferred Pressure Transducer
- 36-11-00-810-957-A [8]
  Spurious ENG BLEED fault indication on the Engine 1
- 36-11-00-810-958-A [8]
  Spurious ENG BLEED fault indication on the Engine 2
- 36-11-00-810-959-A [8]
  Loss of Bleed Air from the Engine 1 because of Starter-Valve Opening Indication
- 36-11-00-810-960-A [8]
  Loss of Bleed Air from the Engine 2 because of Starter-Valve Opening Indication
- 36-11-00-810-961-A [8]
  Discrete Signal Failure of the BMC1
- 36-11-00-810-962-A [8]
  Discrete Signal Failure of the BMC2
- 36-11-00-810-963-A [8]
  Loss of the communication between BMC and CFDIU
- 36-11-00-810-964-A [8]
  PRV Closed in Green in ECAM Bleed Page in Engine 1
- 36-11-00-810-966-A [8]
  PRV Closed in Green in ECAM Bleed Page in Engine 2
- 36-11-00-810-972-A [8]
  Failure of Regulation of the Bleed-Pressure Regulating Valve during Take-Off on Engine 1
- 36-11-00-810-977-A [8]
  Fault Fuselage Loop Pin Programming
- 36-11-00-810-B39-A [8]
  Failure of Regulation of the Bleed-Pressure Regulating Valve during Take-Off on Engine 2
PB.201 CONF:[21] ENGINE BLEED AIR SUPPLY SYSTEM - FAULT ISOLATION PROCEDURES
- 36-11-00-810-968-A [8]
  Cold Flow Path (1) Monitoring Failure
- 36-11-00-810-969-A [8]
  Cold Flow Path (2) Monitoring Failure
- 36-11-00-810-973-A [8]
  High Pressure Valve of Engine 1 Failed in Close Position
- 36-11-00-810-974-A [8]
  High Pressure Valve of Engine 2 Failed in Close Position
- 36-11-00-810-975-A [8]
  Failure of the HPV of Engine 1 in the Open Position
- 36-11-00-810-976-A [8]
  Failure of the HPV of Engine 2 in the Open Position
- 36-11-00-810-978-A [8]
  Over Pressure Valve of Engine 1 Failed in Open or Close Position
- 36-11-00-810-979-A [8]
  Over Pressure Valve of Engine 2 Failed in Open or Close Position
- 36-11-00-810-980-A [8]
  Bleed Valve of Engine 1 Failed in Open or Close Position
- 36-11-00-810-981-A [8]
  Bleed Valve of Engine 2 Failed in Open or Close Position
- 36-11-00-810-982-A [8]
  Failure of the Bleed Pressure Sensor of Engine 1
- 36-11-00-810-983-A [8]
  Failure of the Bleed Pressure Sensor of Engine 2
- 36-11-00-810-984-A [8]
  Bleed Pressure Sensor of Engine 2 Failed
- 36-11-00-810-985-A [8]
  BMC1 Failure
- 36-11-00-810-986-A [8]
  Fan Air Valve of the Engine 1 Failed
- 36-11-00-810-987-A [8]
  Fan Air Valve of the Engine 2 Failed
- 36-11-00-810-988-A [8]
  Over Temperature of the EBAS of Engine 1
- 36-11-00-810-989-A [8]
  Over Temperature of the EBAS of Engine 2
- 36-11-00-810-990-A [8]
  BMC2 Failure
- 36-11-00-810-991-A [8]
  CrossBleed Valve Failed
- 36-11-00-810-992-A [8]
  APU By-pass Relay 1 Failed
- 36-11-00-810-993-A [8]
  APU By-pass Relay 2 Failed
- 36-11-00-810-999-A [8]
  Bleed Pressure Sensor of Engine 1 Failed
- 36-11-00-810-A00-A [8]
  Engine 1 Bleed-Manifold Pressure Sensor Measurement Failure
- 36-11-00-810-A01-A [8]
  Engine 2 Bleed-Manifold Pressure Sensor Measurement Failure
- 36-11-00-810-A03-A [8]
  Engine 2 Pylon Loop B Inoperative
- 36-11-00-810-A04-A [8]
  Engine 1 Bleed Temperature Sensor Channel A Measurement Failure
- 36-11-00-810-A05-A [8]
  Engine 1 Bleed Temperature Sensor Measurement Failure
- 36-11-00-810-A06-A [8]
  Engine 2 Bleed Temperature Sensor Channel A Measurement Failure
- 36-11-00-810-A07-A [8]
  Engine 2 Bleed Temperature Sensor Measurement Failure
- 36-11-00-810-A08-A [8]
  Loss of the Bus from the EIU1
- 36-11-00-810-A09-A [8]
  Loss of the Bus from the EIU2
- 36-11-00-810-A10-A [8]
  Loss of the Data Reception from the ACSC1
- 36-11-00-810-A11-A [8]
  Loss of the Data Reception from the ACSC2
- 36-11-00-810-A12-A [8]
  Loss of the Communication from CFDIU
- 36-11-00-810-A13-A [8]
  Loss of the Comunication from DLRB
- 36-11-00-810-A14-A [8]
  Engine 1 Bleed Pressure Sensor Drift Measurement
- 36-11-00-810-A15-A [8]
  Engine 2 Bleed Pressure Sensor Drift Measurement
- 36-11-00-810-A16-A [8]
  Engine 1 Bleed Manifold Pressure Sensor Drift Measurement
- 36-11-00-810-A17-A [8]
  Engine 2 Bleed Manifold Pressure Sensor Drift Measurement
- 36-11-00-810-A18-A [8]
  Engine 2 Differential Pressure Transducer Drift Measurement
- 36-11-00-810-A19-A [8]
  Engine 1 Differental Pressure Transducer Drift Measurement
- 36-11-00-810-A20-A [8]
  Engine 1 Differential Pressure Transducer Measurement Failure
- 36-11-00-810-A21-A [8]
  Engine 2 Differential Pressure Transducer Measurement Failure
- 36-11-00-810-A22-A [8]
  Loss of Bleed Air from the Engine 1 because of Starter-Valve Opening Indication
- 36-11-00-810-A23-A [8]
  High Bleed Pressure of the Engine 1 in Cruise
- 36-11-00-810-A24-A [8]
  High Bleed Pressure of the Engine 2 in Cruise
- 36-11-00-810-A25-A [8]
  High Bleed Temperature of the Engine 1 in Descent
- 36-11-00-810-A26-A [8]
  High Bleed Temperature of the Engine 1 in Cruise
- 36-11-00-810-A27-A [8]
  High Bleed Temperature of the Engine 2 in Descent
- 36-11-00-810-A28-A [8]
  High Bleed Temperature of the Engine 2 in Cruise
- 36-11-00-810-A29-A [8]
  Low Bleed Pressure of the Engine 1 in Descent/Taxi
- 36-11-00-810-A30-A [8]
  Low Bleed Pressure of the Engine 2 in Descent/Taxi
- 36-11-00-810-A31-A [8]
  Low Bleed Pressure of the Engine 2 in Climb
- 36-11-00-810-A32-A [8]
  Low Bleed Pressure of the Engine 2 in Cruise
- 36-11-00-810-A33-A [8]
  Small Variation of the Bleed Pressure Indication
- 36-11-00-810-A34-A [8]
  Loss of Bleed Air from Engine 2 because of Starter-Valve Opening Indication
- 36-11-00-810-A35-A [8]
  High Bleed Pressure of Engine 1 in Climb
- 36-11-00-810-A36-A [8]
  High Bleed Pressure of Engine 2 in Climb
- 36-11-00-810-A37-A [8]
  High Bleed Temperature of Engine 1 in Climb
- 36-11-00-810-A38-A [8]
  High Bleed Temperature of Engine 2 in Climb
- 36-11-00-810-A39-A [8]
  Low Bleed Pressure of Engine 1 in Climb
- 36-11-00-810-A40-A [8]
  Low Bleed Pressure of Engine 1 in Cruise
- 36-11-00-810-A41-A [8]
  Low Bleed Temperature of Engine 1 in Climb
- 36-11-00-810-A42-A [8]
  Low Bleed Temperature of Engine 1 in Cruise
- 36-11-00-810-A43-A [8]
  Low Bleed Temperature of Engine 1 in Descent
- 36-11-00-810-A44-A [8]
  Low Bleed Temperature of ENG 2 in Climb
- 36-11-00-810-A45-A [8]
  Low Bleed Temperature of ENG 2 in Cruise
- 36-11-00-810-A46-A [8]
  Low Bleed Temperature of ENG 2 in Descent
PB.301 ENGINE BLEED AIR SUPPLY SYSTEM - TASK SUPPORTING DATA