N926VA

Part: LINE — LEAKING (#1 ENGINE) · airframe 13,445 hrs · 3,480 cycles

HYD G RSVR LO LVL, G LO PR GROUNDED - YES. REMOVED ENG 1 PANEL 413AL. FOUND PRESSURE ASSY LINE LEAKING REF IPC 29-11-86-51B ITEM 240. REMOVED AND REPLACED PRESSURE ASSY LINE (P/N=D2902083800000) AND PRESS ASSY LINE (P/N=D2902083900000) OER REF AMM 29-11-49-400-813-A UP TO SUBTASK 29-11-49-420-132-A F(3). OPS CHECK GOOD. NO LEAKS NOTED. SEE LOGPAGE 60478098 FOR FURTHER REFERENCE FOR PANEL 413AL AND CLOSEUP.

Part: CONTROL VALVE — FAILED (AC BAY) · airframe 6,035 hrs · 591 cycles

DURING #2 ENG. START BLEED PRESS DROPPED TO 18 PSI AND R/H PACK FAULT ILLUMINATES ON R/H PACK PACK FLOW CONTROL VALVE STICKING OPEN. GROUNDED - YES. MANUALLY OPERATE R/H PACK WITH APU BLEED. WITH PACK 2 SELECTED OFF R/H PACK FLOW CONT VALVE DOES NOT CLOSE AND 2 AIR PACK REG FAULT ILLUM. ON ECAM. R&R #2 PACK FLOW CONTROL VALVE (24HB) REF. AMM 21-51-51. OPS CHECK GOOD. THIS CLEARS MDDR 77162 & MEL 21-52-01-02. MX PROCEDURE REVERSED. PLACARD REMOVED. MEL LIST UPDATED. SEAMC NOTIFIED

Part: FAULT MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 5,745 hrs · 1,526 cycles

ENGINE 2 REVERSER MINOR FAULT ON ECAM. GROUNDED - YES. FAULT WAS NOT REPORTED IAW TSM 78-37-00-810-843-A. NO MAINTENANCE ACTION IS REQUIRED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 5,696 hrs · 1,512 cycles

ENG 1 ANTI-ICE CLASS II MX MESSAGE GROUNDED - YES. PERFORMED OPS CHECK ON NR 1 ENG. ANTI-ICE PER AMM 30-21-00-710-002-A. OPS CHECK GOOD, NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 ENG) · airframe 5,259 hrs · 1,409 cycles

AIR ENGINE 1 BLEED LOW TEMP ECAM GROUNDED - YES. RESET BMC #1 AND BITE TEST, TEST GOOD AND FAULT CLEARED PER AMM 36-11-00-740-001-A

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 1 BLEED TEMP) · airframe 5,173 hrs · 1,390 cycles

AIR ENGINE #1 BLEED LOW TEMP GROUNDED - YES. PERFORMED TSM 36-11-00-810-A98 UP TO STEPS 4A(2). NO FAULTS NOTED. NO MAINTENANCE ACTION NECESSARY

Part: IDG — FAILED (NR 2) · airframe 5,047 hrs · 1,362 cycles

DURING DECENT THRUST IS AT IDLE APU : #2 IDG OIL TEMP FLASHES AMBER AT 190 C WHEN TRUST ADVANCE TEMP BACK TO GREEN RANGE GROUNDED - YES. R & R #2 IDG IAW AMM 24-21-51 PB 401 OPS CHK GOOD - NO LEAKS NOTED A/C RELEASED FROM MEL 24-20-01 - MDDR 73029 REMOVED MAINT PROC REVERSED , LOG UPDATED , PLACAR REMOVED, MCC NOTIFIED

Part: VALVE — MISINSTALLED (NR 1 ANTI-ICE) · airframe 4,852 hrs · 1,315 cycles

ON CLIMB W/ WING ANTI-ICE ON ECAM AIR ENG 1 BLEED WING ANTI ICE OFF BUT BLEED TEMP ENG 1 AT CRUISE STILL 65C ( OPPOSITE SIDE 200C) GROUNDED - YES. UPON INSPECTION OF FAN AIR VALVES, FOUND THE FLUSH ROD BOLT NOT CONNECTED & ROD HANGING. REINSTALLED ROD TO THE FAN AIR AIR VALVE IAW AMM 36-11-54. PEROFMRED ENG#1 IDDLE- FUN WILL BLEED, OPS CHECK GOOD OK FOR SVC.

Part: SENSOR — FAULTED (ENGINE) · airframe 4,463 hrs · 1,232 cycles

SMR FAULTS FOUND ON ENG 2 CHANNEL A. DISPLAYED SMR FAULT IS 0343-N2 SENSOR. ATA 771120. DATE 1507. WHEN THIS/THESE SMR FAULTS ARE REPAIRED, TASK 730000-L1-1 IS REQUIRED TO BE ASSIGNED AND ACCOMPLISHED BEFORE THE WATCH ITEM IS CLEARED.SMR FAULTS FOUND ON ENG 1 CHANNEL B. DISPLAYED SMR FAULTS IS 2427-TLS SNSR. ATA 783000. DATE 2207. WHEN THIS/THESE SMR FAULTS ARE REPAIRED, TASK 730000-L1-1 IS REQUIRED TO BE ASSIGNED AND ACCOMPLISHED BEFORE THE WATCH ITEM IS CLEARED. GROUNDED - YES. ON DEFERRAL

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,449 hrs · 1,228 cycles

FUEL CTR R XFR FAULT ON ECAM. GROUNDED - YES. PERFORMED TROUBLESHOOTING IAW TSM 28-26-00-810-807-A AND OPERATIONAL TEST IAW AMM 28-26-00-710-001-A. CENTER TANK R XFR VALVE OPERATES NORMALLY WITH NO FAULTS DETECTED MEL REF 28-21-02-03A.

Part: UNKNOWN — MALFUNCTIONED (BLEED AIR SYS) · airframe 3,946 hrs · 1,080 cycles

AIR ENG 2 BLEED LO TEMP, ECAM WITH WING A/ICE ON. NOTE: LOW PRE-COOLER TEMPS OBSERVED DURING ENTIRE CRUISE (65). PRESSURE NORMAL. GROUNDED - YES. VERIFIED AIR ENG 2 BLLED LO TEMP INOP, RELEASED PER MEL 36-11-04-03 , MEL LOG UPDATED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 3,784 hrs · 1,043 cycles

ENG 2 BLEED LOW TEMP W/ WING A/I SELECTED. GROUNDED - YES. PERFORMED BITE TEST OF THE EBAS OPS TEST GOOD REF. AMM 36-11-00-740-804. DEFECT HISTORY REF. RMA-3031

Part: LINE — LEAKING (NR 1 SENSING) · airframe 3,784 hrs · 1,043 cycles

FOUND LEAK ON ENG #1 SENSELINE ON THE ECS DUCT TO PYLON. GROUNDED - YES. R/R ENG #1 INDICATING TUBE ON THE ECS IAW AMM 36-11-49-400-831-A. OPS / LEAK CHECK GOOD. OK FOR SERVICE.

Part: ENGINE — STALLED (NR 2) · airframe 3,778 hrs · 1,041 cycles

NR 2 ENGINE STALL ON ECAM ON POWER REDUCTION IN INITIAL DESCENT. AIRCREW FELT A YAW AND QUICK DROP AND RETURN OF ENGINE PARAMETERS, NO EXCEEDANCES NOTED. GROUNDED - YES. REMOVED AND REPLACED THE NR 2 ENGINE IAW AMM 71-00-51.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 BLEED AIR) · airframe 3,713 hrs · 1,025 cycles

WHILE FLYING IN ICING CONDITIONS WE RECEIVED ECAM AIR ENG 2 BLEED LO TEMP ECAM ACTION UNSUCCESSFUL GROUNDED - YES. RESET BMC 2 REF AMM 36-11-00 BITE CHECK GOOD RAN ENGINES NO FAULTS FOUND A/C OK FOR SERVICE

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 2,775 hrs · 792 cycles

ENGINE 1 FADEC MESSAGE AT GATE GROUNDED - YES. RESET FADEC 1 AMM 73-29-00-710-040=01 CLASS 2 MSG CLEARED.

Part: NOT REPORTED — MALFUNCTIONED (APU) · airframe 2,670 hrs · 757 cycles

APU AVAIL NO ECAM AT CAUTIONS AND AT ENGINE SHUT DOWN THE ELECTRIC DID NOT TRANSFER TO THE APU. GROUNDED - YES. DEFERRED.

Part: HARNESS — FAILED (NR 2 ENGINE) · airframe 2,658 hrs · 753 cycles

ENGINE NR 2 IGNITER SYSTEM B FAULT NO ENGINE LIGHT UP ONLY SYSTEM A GROUNDED - YES. SWAPPED EIU 1&2, NO HELP FAULT REMAINS. SWAPPED CONNECTORS AT IGNITION EXCITERS FROM A TO B AND FAULT FOLLOWED RETURNED TO ORIGINAL POSITION . FURTHER T/S REQUIRED. PER TSM 74-21-00-810-805-A REMOVED AND REPLACED NR 2 ENGINE CHANNEL B IGNITION HARNESS HJ2B (4178KS) REF 71-51-43. ENGINE START SUCCESSFUL ON CHANNEL B AND A MULTIPLE TIMES. INSTALLED IGNITION CHANNEL B HARNESS FIN 4178KS P/N # 515167-3 SN S17450333 ON ENGINE S/N 598226 PER AMM 71-51-43. OPS CHECK GOOD OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,449 hrs · 598 cycles

CLASS II MAINTENANCE MESSAGE TEMP CTL 2 GROUNDED - YES. RESET C/BS & PERFORMED CABIN TEMP CONTROL BITE TEST IAW AMM 21-63-00 OPS CHECK GOOD OK FOR SERVICE.

Part: SENSOR — FAILED (FUEL STRAINER) · airframe 2,327 hrs · 663 cycles

DURING W/O 384707, T/C 730000-L1-1 SMR CORRECT FADEC FAULTS SHOWS FUEL STRAINER SNSR FAULT ON ENG 2 CH B. REF TSM 73-34-00-810-102-A SUBTASK B. REF MDDR 62199 FOR WI. GROUNDED - YES. R&R ENG 2 FUEL STRAINER DIFFERENTIAL PRESSURE SENSOR PER AMM 73-34-10 PB 401. AND TSM 73-34-00-810-825-A PARA 4B(2)(B)2. TEST OK. NO FAULTS AND NO LEAKS NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 1,813 hrs · 515 cycles

CLASS II APU MSG ON ECAM GROUNDED - YES. DEFERRED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,538 hrs · 436 cycles

AFTER LANDING ENG 1 REV MINOR FAULT. GROUNDED - YES. PERFORMED ENG 1 OPERATIONAL T/R CYLING TEST. TEST OK REF TSM 78-37-00-810-839-A THIS CLEARS MDDR 60170 MEL LIST UPDATED PLACARD REMOVED MCC GEORGE NOTIFIED

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,357 hrs · 386 cycles

APU MAINT MESSAGE. GROUNDED - YES. ACCOMPLISHED APU RESET AND OPS CHECK PER AMM 49-00-00-710-010 NO STATUS MESSAGE PRESENT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 1,262 hrs · 352 cycles

ENG 2 MINOR FAULT MSG DISPLAYED AFTER LANDING GROUNDED - YES. *DEFERRED*

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 976 hrs · 265 cycles

AFTER SHUTDOWN, ECAM CLASS II MESSAGE FOR APU. ACFT GROUNDED. APU TEST COMPLETED IAW AMM 49-70-00, TEST PASSED. MESSAGE CLEARED.

Part: VALVE — MALFUNCTIONED (AC BAY) · airframe 250 hrs · 60 cycles

HOT AIR A/C VALVE STUCK IN CLOSED POSITION GROUNDED - YES. PERFORMED BITE TEST OF ACSC SYSTEM OPS CK GOOD, HOT AIR VALVE CLOSED AND OPEN OK, REF AMM 21-61-00-00,