PNEUMATIC
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Internal Failure of the BMC1 A292 ALL Internal Failure of the BMC2 A295 ALL Loss of the BMC 1 and Overpressure A298 ALL or Overtemperature on the Engine 1 Bleed System Detected by the BMC 2 Loss of the BMC 2 and Overpressure B200 ALL or Overtemperature on the Engine 2 Bleed System Detected by the BMC 1 Loss of the 2nd BMC (the 1st is B202 ALL lost) Loss of the Bleed B204 ALL Regulated-Pressure Transducer of the Engine 1 (Detected by BMC2) Loss of the Bleed B207 ALL Regulator-Pressure Transducer of the Engine 2 (Detected by BMC1) Abnormal Bleed Temperature Shown B210 ALL Amber during BMC1 Test with the Engines Not in Operation Abnormal Bleed Temperature Shown B212 ALL Amber during BMC2 Test with the Engines Not in Operation BMC1 output failure for HP Bleed B214 151-199, 401-499 Override Solenoid of Engine 1 BMC2 output failure for HP Bleed B215 151-199, 401-499 Override Solenoid of Engine 2 HP Bleed Valve blocked in the B216 ALL closed position or regulation too low on Engine 1 without associated maintenance message HP Bleed Valve blocked in the B217 ALL closed position or regulation too low on Engine 2 without associated maintenance message High bleed pressure fluctuation on B218 ALL Engine 1 at take-off or climb phase High bleed pressure fluctuation on B219 ALL Engine 2 at take-off or climb phase Drift of the Pressure Transducer B220 ALL on the Engine 1 Drift of the Pressure Transducer B222 ALL on the Engine 2 Failure of the Bleed Pressure B224 ALL Regulator Valve Control Solenoid
 36-CONTENTS Page 7 Aug 01/05 R CES

 PNEUMATIC
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ or its Wiring Failure of the Overpressure Valve B227 ALL in Closed Position on the Engine 1 Failure of the Overpressure Valve B229 ALL in Closed Position on the Engine 2 Spurious APU leak indication on B231 106-149, 229-299 the Engine 1 303-399, 401-499 Spurious APU leak indication on B233 106-149, 229-299 the Engine 2 303-399, 401-499 Drift of the Engine 1 Bleed B234 106-149, 229-299 Regulated Pressure Transducer 303-399, 401-499 Drift of the Engine 2 Bleed B237 106-149, 229-299 Regulated Pressure Transducer 303-399, 401-499 Drift of the Engine 1 Bleed B240 106-149, 229-299 Transferred Pressure Transducer 303-399, 401-499 Drift of the Engine 2 Bleed B243 106-149, 229-299 Transferred Pressure Transducer 303-399, 401-499 Spurious ENG BLEED fault B246 106-149, 229-299 indication on the Engine 1 303-399, 401-499 Spurious ENG BLEED fault B248 106-149, 229-299 indication on the Engine 2 303-399, 401-499 Loss of Bleed Air from the Engine B250 ALL 1 because of Starter-Valve Opening Indication Loss of Bleed Air from the Engine B252 ALL 2 because of Starter-Valve Opening Indication
 ENGINE BLEED AIR SUPPLY SYSTEM 36-11-00
 TASK SUPPORTING DATA 301 ALL
 BMC output data bus (numerical 301 ALL
 word)

 APU BLEED AIR SUPPLY AND CROSSBLEED 36-12-00 SYSTEMS
 FAULT ISOLATION PROCEDURES 201 ALL
 Fault of the APU Bleed Supply 201 ALL
 Fault of the Crossbleed Valve 210 ALL
 Position Control
 Disagreement of the Position 215 ALL
 Switches of the Crossbleed Valve
 Low Air Pressure in the Right 218 ALL
 Crossbleed Duct
 To Slow Operation of the 219 ALL
 Crossbleed Valve

 36-CONTENTS Page 8 Aug 01/05 R CES

 PNEUMATIC
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________
 APU BLEED AIR SUPPLY AND CROSSBLEED 36-12-00
 SYSTEMS
 TASK SUPPORTING DATA 301 ALL

 LEAK DETECTION 36-22-00
 FAULT ISOLATION PROCEDURES 201 ALL Air Leak in the Left Wing 201 ALL Air Leak in the Right Wing 203 ALL Air Leak in the Engine 1 Pylon 205 ALL Air Leak in the Engine 2 Pylon 209 ALL Air Leak from the APU in the Aft 213 ALL Cargo Compartment Loss of the Leak Detection Loop A 214 ALL on the Right Wing Loss of the Leak Detection Loop A 217 ALL on the Left Wing Loss of the Leak Detection Loop B 220 ALL on the Right Wing Loss of the Leak Detection Loop B 223 ALL on the Left Wing Loss of the Leak Detection Loop on 226 ALL the Engine 1 Pylon Loss of the Leak Detection Loop on 228 ALL the Engine 2 Pylon Loss of the Leak Detection Loop of 230 ALL the APU Loss of the Left-Wing Leak 232 ALL Detection Loss of the Right-Wing Leak 233 ALL Detection Loss of the Left-Wing Leak 234 ALL Detection Loss of the Right-Wing Leak 235 ALL Detection Loss of the Left-Wing Leak 236 ALL Detection Loss of the Right-Wing Leak 237 ALL Detection Inadvertent Leak Detection by the 238 ALL left wing loops Inadvertent Leak Detection by the 239 ALL right wing loops Unwanted Engine 1 Leak Detection 240 ALL Unwanted Engine 2 Leak Detection 241 ALL
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) PNEUMATIC(6)