N924VA

Part: PRECOOLER — RUPTURED (HYD SYSTEM) · airframe 8,439 hrs · 2,261 cycles

HYDRAULIC G SYSTEM LO PR. GROUNDED-YES. G HYDRAULIC PRESSURE LINE IN PYLON FWD OF PRE-COOLER RUPTURED. R & R G SYSTEM PRESSURE LINE, PER REF 29-11-49-00-813-A PRESSURE LINE ROBBED FROM N925VA LP 60031954. G SYSTEM PRESSURE OPERATIONS CHECK GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (ENGINE OIL PRESS) · airframe 5,968 hrs · 1,614 cycles

DURING T/O POWER FLEX #1 ENGINE OIL PSI 126 AND FLASHING GREEN STOPPED WHEN CLIMB POWER SELECTED GROUNDED - YES. SEE STATEMENT FROM GE PSE FOR A/C DISPOSITION. REFERENCE GE CASE NUMBER 01171838. CFM HAS NO OTHER RECOMMENDATION TO RELEASE THE ENGINE REGARDING THE HIGH OIL PRESSURE SEEN. NO FAULT IS PRESENT IN THE PFR (TIME TO SET A HIGH OIL PRESSURE IS 30S) AND NOTHING PARTICULAR WAS FOUND DURING THE TSM. THE LAST STEP CONCERNING THE OIL FLOW CHECK FOR ANY OBSTRUCTION IS NOT APPLICABLE IN THIS SITUATION REGARDING THAT THERE IS NO IMPACT ON THE OIL PRESSURE IN CRUISE AND THE OIL PRESSURE TRENDS IN T/O OR CR IN MYCFM PORTAL ARE STABLE WITHOUT ANY DEVIATION. THE OIL PRESSURE SNAPSHOT SENT FROM THE SISTER ENGINE HAS THE SAME BEHAVIOR DURING THE SAME FLIGHT. IT WAS THE FIRST FLIGHT OF THE DAY AFTER SPENDING THE NIGHT NEAR 0Ï¿½C IN WASHINGTON WHICH MAY EXPLAIN THE HIGH OIL PRESSURE SEEN IF THE ENTIRE OIL CIRCUIT WAS NOT HEATED ENOUGH. TECH SERVICES RECOMMENDS CLOSING THIS ITEM AT THIS TIME.

Part: FLOOR PANEL — PUNCTURED (FWD CARGO) · airframe 5,625 hrs · 1,537 cycles

FWD CARGO COMPARTMENT, 2ND FLOOR BOARD BACK FROM THE FWD BULKHEAD, R/H SIDE IS PUNCTURED  GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR TO FWD CARGO COMPARTMENT, 2ND FLOOR BOARD BACK FROM THE FWD BULKHEAD, R/H SIDE IAW A321 SRM 53-02-00-300-005

Part: FLOOR PANEL — PUNCTURED (FWD CARGO BAY) · airframe 5,625 hrs · 1,537 cycles

FWD CARGO COMPARTMENT, AFT FLOOR BOARD, AFT L/H CORNER IS PUNCTURED  GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR TO FWD CARGO COMPARTMENT, AFT FLOOR BOARD, AFT L/H CORNER IAW A321 SRM 53-02-00-300-005

Part: FLOOR PANEL — PUNCTURED (FWD CARGO) · airframe 5,625 hrs · 1,537 cycles

FWD CARGO COMPARTMENT BETWEEN FRAMES 34 AND 35.1 L/H SIDE WALL LOWER GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR TO FWD CARGO COMPARTMENT BETWEEN FRAMES 34 AND 35.1 L/H SIDE WALL LOWER SLANT PANEL IAW A321 SRM 53-02-00-300-005

Part: SENSE LINE — LEAKING (NR 2 ENGINE) · airframe 5,293 hrs · 1,466 cycles

AIR BLEED CLASS II MSG DURING ACCOMPLISHING RMA 3276, FOUND TUBE AIR SENSE LINE PN ER9691P01 LEAKING @ BRAIDED PORTION. ON #2 ENGINE GROUNDED - YES. REMOVED AND REPLACED SENSE LINE PN: ER9691P01 ACCOMPLISHED OPERATIONAL TEST IAW AMM 36-11-49 OPS CHECK GOOD. AIRCRAFT RELEASED FROM MEL 36-11-01-02B MAINT PROCEDURES REVERSED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,265 hrs · 1,459 cycles

CLASS II MESSAGE "AIR BLEED" GROUNDED - YES. PERFORMED BITE TEST OF THE ENGINE BLEED AIR SYSTEM REF AMM 36-11-00-740-804-A. OPS TEST OK. MSG CLEARED. OK FOR SERVICE.

Part: SENSOR — FAULTY (NR 2 ENGINE) · airframe 4,561 hrs · 1,276 cycles

ENGINE 2 MINOR FAULT ECAM GROUNDED - YES. R/R SENSOR- N2 SPEED REF AMM 77-11-10 PB 401. PERFORMED IDLE TEST REF AMM 73-29-00-740-803. OPS TEST OK. THIS CLEARS MDDR 68228. PLACARD REMOVED MEL LIST UPDATED.

Part: PRESSURE SENSOR — FAILED (NR 1 ENGINE) · airframe 3,575 hrs · 1,033 cycles

ENGINE 1 FUEL STRAINER SENSOR FAULT. GROUNDED - YES. ENGINE NR 1 FUEL STRAINER DIFFERENTIAL PRESSURE SENSOR REMOVED AND REPLACED PER AMM 73-34-10. OPERATION TEST PER AMM 73-34-10-700-050A COMPLETED. NO FAULTS. AIRCRAFT OK FOR SERVICE.

Part: LOCK — MALFUNCTIONED (THRUST REVERSER) · airframe 3,565 hrs · 1,025 cycles

ENGINE 1 REVERSER MINOR FAULT GROUNDED - YES. T/S PER TSM 78-37-00-810-840-A. PERFORMED MANUAL RESET OF TERTIARY LOCK SYS REF AMM 78-37-00. OPS TESTED T/R PER AMM 73-29-00. NO FAULTS NOTED PLACERD REMOVED. MEL LIST UPDATED MCC CORY NOTIFIED. THIS CLEARS MDDR 64314.

Part: PACKING — LEAKING (APU) · airframe 3,001 hrs · 869 cycles

APU LOW OIL LEVEL (ADV MSG) GROUNDED - YES. ON INSPECTION FOUND APU LUBE FILTER HOUSING WITH LEAK. REMOVED AND REPLACED LUBE FILTER PACKING IAW AMM 49-91-41. OPS CHECK GOOD. THIS CLOSES MDDR 62722 AND MDDR 62723. MEL LIST UPDATED. PLACARD REMOVED. MCC NOTIFIED

Part: DISC — DAMAGED (FUEL OVER PRESS) · airframe 2,831 hrs · 824 cycles

FUEL VENTILATION OVERPRESSURE DISC ON INBOARD SIDE OF RIGFHT WING HAS NO CROSS ONIT GROUNDED - YES. DEFERRED. AIRCRAFT IS ETOPS RESTRICTED

Part: CVR — MALFUNCTIONED · airframe 2,539 hrs · 729 cycles

NO AUDIO TONE ON CVR TEST.***CVR ETA TO SFO, 11-20 0800 LOCAL.*** GROUNDED - YES. REF A321 TSM 23-71-00-810-801-A. ACCOMPLISHED OPS TEST OF CVR, NO AUDIO IN CAPT AND F/O LOUD SPEAKER. PERFORMED ALTERNATIVE CVR TEST THROUGHOUT PANEL 50VU HEADSET JACK 22RK. OPS TEST GOOD.

Part: HOSE — FAILED (NR 2 ENGINE) · airframe 2,386 hrs · 679 cycles

ENG NR 2 PRSOV NR 1 UPPER TUBE HOSE DAMAGED. ITEM 17 ON FIGURE 30-21-51-991-90500-03-A. GROUNDED - YES. R/R ENG NR 2 PRSOV NR 1 UPPER TUBE HOSE. IAW AMM 30-21-51 PB401. SEE LOG PAGE 8029622 ITEM 2 FOR LEAK CHECK.

Part: PIN — MIGRATED (ANTI-ICE VALVE) · airframe 2,321 hrs · 657 cycles

ECAM AIR ANTI ICE ENG 2 VALVE INFLIGHT W/ENG 2 ANTI/ICE SELECTED ON. GROUNDED - YES. FOUND DEATIVATION PIN MIGRATED OUT OF THE NAI VALVE. CAUSING THE VALVE TO RETURN TO THE CLOSED POSITION. CORRECTED THE DEFECT. PER THE MEL.30-21-01-04. MCC NOTIFIED. THIS MEL MEL REMAINS OPEN.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,321 hrs · 657 cycles

ENG 2 REV MINOR FAULT ECAM MESSAGE. GROUNDED - YES. DEFERRED

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 2,311 hrs · 653 cycles

ITEM 2: AMBER ECAM MESSAGE IN FLIGHT ANTI-ICE ENG 2 VALVE CLOSED AVOID ICING CONDITIONS. GROUNDED - YES. DEFERRED.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 2,307 hrs · 651 cycles

ECAM AMBER MESSAGE IN FLIGHT:ANTI ICE ENG 2 VALVE CLOSED MESSAGE DURRING ICING CONDITIONS. GROUNDED - YES. ACCOMPLISHED ENG RUN. RESET ENG A/I VALVE DURING RUN. A/I SYSTEMS OPERATED NORMAL IAW AMM 73-29-00-740-803-A. A/C IS GOOD FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (ANTI-ICE SYS) · airframe 2,158 hrs · 599 cycles

AFTER SHUTDOWN IN GATE MAINT STATUS ENG 2 ANTI ICE ON LOWER ECAM. GROUNDED - YES. DEFERRED

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,075 hrs · 571 cycles

ENG 2 ANIT-ICE STATUS MSG. DISPLAYED AFTER ENG. SHUTDOWN. GROUNDED - YES. COULD NOT DUPLICATE FAULT - ANTI-ICE SYS OK PER AMM 30-21-00.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 1,937 hrs · 523 cycles

NR 2 ENGINE THRUST REVERSER MINOR FAULT. ACFT GROUNDED.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 1,905 hrs · 514 cycles

NR 2 ENGINE THRUST REVERSER MONOR FAULT MESSAGE RECEIVED AFTER LANDING. ACFT GROUNDED. PERFORMED FAULT CONFIRMATION IAW TSM 78-31-01-810-805-A, EEC TESTED GOOD. NO FAULTS NOTED, NO MAINTENANCE ACTION REQUIRED. ENG 2 T/R OPS CHECKED GOOD.

Part: WARNING MESSAGE — ILLUMINATED (NR 1 ENGINE) · airframe 1,798 hrs · 485 cycles

NR 1 ENGINE HAD A MINOR FAULT AMBER MESSAGE. ACFT GROUNDED.

Part: OIL FILTER — DIRTY (NR 2 ENGINE) · airframe 1,788 hrs · 483 cycles

CAPTAIN REPORTED DURING 2 LEGS, THE NR 2 ENGINE OIL FILTER, APPROACH BYPASS MESSAGE ON ECAM. ACFT GROUNDED. R & R THE OIL FILTER CARTRIDGE IAW AMM 79-21-05, AND PERFORMED A VISUAL INSPECTION AND CLEANED THE OIL DEBRIS MONITORING SYSTEM (ODMS) IAW AMM 79-36-00. LEAK CHECKED GOOD, ACFT OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER) · airframe 1,770 hrs · 478 cycles

NR 1 ENGINE REVERSER MINOR FAULT ECAM ON START. ACFT GROUNDED. TROUBLESHOT IAW TSM 78-37-00-810-843-A, NO FAULTS 3 FLT LEGS. ACCOMPLISHED A THRUST REVERSER TEST AND INSPECTION, NO FAULTS AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,713 hrs · 460 cycles

ENGINE NR 2 REVERSER MINOR FAULT AFTER LANDING ECAM APPEARED. GROUNDED - YES. AS PER TSM 78-31-01-810-805-A SYSTEM CHECKED AND FOUND OK NO FAULTS SEEN BY FADEC 2A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,596 hrs · 423 cycles

ENGINE NR 1 MINOR FAULT GROUNDED - YES. UPON ARRIVAL FAULT MESSAGE EXTINUISHED. MX PERF EIU 1 SYS TEST. GRD SCAN, FADEC 1A AND 1B TEST. ALL TESTS PASSED, AMM REF 73-29-00-710-802-A, A/C OK TO CONTNUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,458 hrs · 381 cycles

ENGINE NR 1 MINOR FAULT GROUNDED - YES. IF INITIAL FAULT OCCURRED IN PHASE 9 AND DID NOT OCCUR WITHIN THE NEXT 2 FLIGHT, THEN NO MAINTENANCE ACTION IS NECESSARY PER TSM 77-11-00.

Part: SENSE LINE — FAILED (NR 2 ENGINE) · airframe 1,305 hrs · 341 cycles

AIR BLEED STATUS MESSAGE GROUNDED - YES. PER TSM 36-11-00 PB201 SUBTASK 36-11-00-810-562-A. R&R BRAIDED AIR SENSE LINE ON THE ECS DUCTS ENG NR 2 IAW AMM 36-11-49. OPS CHECK GOOD AT THIS TIME.

Part: WIRE HARNESS — FAILED (NR 1 ENGINE) · airframe 1,250 hrs · 329 cycles

PILOT REPORTED THE NR 1 ENGINE WITH A MINOR FAULT. ACFT GROUNDED. R & R THE NR 1 ENGINE HJ5A WIRE HARNESS, OPS CHECKED NORMAL IAW AMM 77-11-00-810-839-A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,201 hrs · 315 cycles

ENGINE NR 1 REVERSER MINOR FAULT. GROUNDED - YES. OPS CK OF REVERSER THRU MCDU W/ NO FAULTS REF AMM 78-30-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 979 hrs · 258 cycles

ENGINE 1 MINOR FAULT. CEOD DOWNLOADED 5-20, WAITING ON RESPONSE. GROUNDED - YES. PERFORMED ENG 1 IDLE TEST, REF AMM 73-29-00-740-803-A, TESK OK, NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (FADEC) · airframe 773 hrs · 204 cycles

NR 1 ENGINE FADEC ECAM AFTER LANDING. ACFT GROUNDED. PERFORMED THE NR 1 ENGINE FADEC TEST IAW AMM 73-29-00. NO FAULTS NOTED.

Part: SENSOR — FAULTY (NR 1 ENGINE) · airframe 699 hrs · 183 cycles

ENG 1 MINOR FAULT ON ECAM GROUNDED - YES. R&R N2 SPEED SENSOR PER AMM 77-11-20. IDLE TEST PER 73-29-00-740-803-A. NO ISSUES NOTED. MDDR CLOSED. MEL LIST UPDATED. MCC NOTIFIED.

Part: FAULT LIGHT — FALSE ACTIVATION (NR 1 ENGINE) · airframe 687 hrs · 179 cycles

NR 1 ENGINE MINOR FAULT ON UPPER ECAM AFTER TOUCHDOWN. ACFT GROUNDED. PERFORMED AN OPERATIONAL CHECK OF THE NR 1 ENGINE IAW TSM 77-11-00-810-840-A. OPS CHECKED GOOD, NO DEFECTS OR FAULT MESSAGES NOTED. ACFT OK FOR SERVICE.

Part: FADEC — MALFUNCTIONED (NR 1) · airframe 628 hrs · 163 cycles

NR 1 ENGINE FADEC SYS FAULTED AFTER LANDING. ACFT GROUNDED. RESET THE CIRCUTI BREAKER FOR THE NR 1 FADEC SYS IAW TSM 24-00-00-810-818. OPS CHECKED GOOD IAW AMM 73-29-00-710-040. NO FURTHER DEFECTS NOTED.

Part: FAULT MESSAGE — FALSE ACTIVATION (NR 1 ENGINE) · airframe 618 hrs · 159 cycles

NR 1 ENGINE MINOR FAULT, ACFT GROUNDED. PERFORMED A BITE TEST OF THE NR 1 ENGINE EIU SYSTEM 1 & 2 AND FADEC 1 CHANNEL A & B. ALL TESTED NORMAL IAW AMM 77-00-00. UNABLE TO DUPLICATE FAULT. ACFT OK FOR SERVICE.

Part: RECORDER — MALFUNCTIONED · airframe 445 hrs · 117 cycles

FDIMU NOT TRANSMITTING DATA. ACFT GROUNDED. IAW ENGINEERING, FDIMU IS TRANSMITTING PROPERLY. THIS CLEARS MDDR 54033. MEL LIST UPDATED. PLACARD REMOVED. MCC GEORGE NOTIFIED.

Part: BOLT — LOOSE (FUEL OIL/COOLER) · airframe 121 hrs · 29 cycles

NR 1 ENG LEAKING UPON SHUTDOWN GROUNDED - YES. FOUND LOOSE BOLTS ON FUEL OIL COOLER AFT LINE SECURED BOLTS PER AMM 73-11-50-400-802A ACP IDLE RUN & NO LEAKS NOTED PER AMM 71-00-00-710-815A.