36-11 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
-
36-11-00-810-801-A
[8]
- 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
-
36-11-00-810-968-A
[8]
- PB.301 ENGINE BLEED AIR SUPPLY SYSTEM - TASK SUPPORTING DATA