N213HA

Part: FIRE LOOP — FAULTED · airframe 22,126 hrs · 4,536 cycles

ETOPS - FIRE LOOP A CORE ECAM MESSAGE. REPLACED FIRELOOP A CORE PER AMM 26-12-17. OPS CHECK NOT GOOD. REPLACED LOOP A FIRE LOOP HARNESS PER AMM 26-12-61. OPS CHECK NOT GOOD. REMOVED AND REPLACED FIRE LOOP CORE LOOP B PER AMM 26-12-17. OPS CHECK IS GOOD. OKAY TO CONTINUE.

Part: PRESSURE SWITCH — FAULTED (APU OIL) · airframe 22,086 hrs · 4,528 cycles

ETOPS - APU AUTO SHUTDOWN. REMOVED & REPLACED. ECB & OIL PRESSURE SW PER AMM 49-61-34 & AMM 49-91-14. OPS + LEAK CK GOOD. OK FOR SVC

Part: SDU — LEAKING (NR 1 ENGINE) · airframe 21,036 hrs · 4,321 cycles

ETOPS - DIRTY SOCK SMELL DECSENDING THROUGH 6,000' - 3,000'. DURATION APPROXIMATELY 10 MIN. PUSHED DFDR EVENT BUTTON. FOUND OIL STREAKS COMING FROM #1 ENG INLET CONE WEEP HOLES AND OIL PUDDLING INSIDE OF #1 ENG INLET CONE. REPLACED THE FAN SHAFT COVER SEAL PE R AMM 72-15-00-960-801-A. LEAK CHK OK. ACCOMPLISHED #1 ENG WATER WASH PER T/C E1128-321-72-007. NO SOCK SMELL NOTED.

Part: SENSOR — FAULTED (ZONE 400) · airframe 21,031 hrs · 4,320 cycles

ETOPS - ON DECENT AS THRUST WENT TO IDLE "ENG 1 SENSOR FAULT". REMOVED BURNER PRESSURE SENSOR AND BURNER PRESSURE SENSOR TUBE IN REFERENCE TO AMM 73-21-23-000-801-A AND 73-21-23-000-802A K.H. 25197 06/15/2025. INSTALLED BURNER PRESSURE AND LINE PER AMM 73-21-23. OPS AND LEAK CHECK OK. OK FOR SVC.

Part: OIL FILTER — FAULTED (APU) · airframe 20,511 hrs · 4,219 cycles

ETOPS - APU AUTO SHUTDOWN AFTER 2 ATTEMPTS. PERFORMED TSM 49-00-81-810-849-A. REMOVED & REPLACED APU OIL FILTER ELEMENTS PER AMM 49-91--41-200-002-A. OPERATED APU PER AMM 49-00-00-860-009-A. NO DEFECTS NOTED. OK FOR SERVICE.

Part: FUEL FILTER — FAULTED (APU) · airframe 20,354 hrs · 4,189 cycles

ETOPS-APU AUTO SHUTDOWN TWICE ON STARTUP. FOUND CLOGGED OIL FILTER GEN SCAV + LUBE FILTERS MSG. REMOVED AND REPLACED OIL FILTERS APU. OPS AND LEAK CHK GOOD REF AMM49-91-41. REMOVED AND REPLACED APU FUEL FILTER PER AMM 49-32-41-920-001-A. OPS CHECK GOOD NO LEAKS FOUND. OK TO CONTINUE FOR SERVICE.

Part: WIRE HARNESS — DAMAGED · airframe 15,238 hrs · 3,387 cycles

ETOPS - FOUND 440VT2 TERMINAL BLOCK & WIRE 704001-000W24-22 DAMAGED WHILE TROUBLESHOOTING REPEAT GEN 2 FAULT. REMOVED AND REPLACED 440VT2 TERMINAL BLOCK AND WIRE 704001-000W24-22. PER AMM 24-21-61 AND AMM 24-92-00. OPS CHECK OKAY. OK FOR SVC. OSD: 1/24/2025

Part: BLEED VALVE — DAMAGED · airframe 19,323 hrs · 3,986 cycles

ETOPS - WHILE PERFORMING ASSIGNED BOROSCOPE TASK CARDS, FOUND BLEED PRESSURE REGULATING VALVE DAMAGED. REMOVED AND REPLACED BLEED PRESSURE REGULATING VALVE IAW A321 AMM 36-11-52. LEAK CHECK OK. ENGINE IDLE RUN PERFORMED. A/C OK FOR SERVICE.

Part: SENSOR — FAULTED (NR 1 A/C PACK) · airframe 17,851 hrs · 3,694 cycles

ETOPS - CLASS 2 TEMP CONTROL MESSAGE FOUND ON STATUS PAGE. REMOVED AND REPLACED PACK 1 INLET SENSOR PER AMM 21-51-13-400-001-A. OPS CHECK GOOD, OK FOR SERVICE

Part: SHUTTLE VALVE — FAULTED (NR 1 ENG OIL) · airframe 16,740 hrs · 3,474 cycles

ETOPS - ENG1 OIL SYSTEM FAULT ON ECAM AFTER SHUTDOWN AT GATE. PERFROMED TSM 79-33-00810840A- NO DECTS NOTED REPLACED SHUTTLE VLV PER AMM 79-21-15-000-801A- REPLACED MAIN OIL PRESS OIL SENSOR PER AMM 79-33-21-400-801 SWAPPED #1 AND #2 PHMU TO ASSIT TROUBLESHOOTING FAULT DID NOT FOLLOW PER ENGINEERING WILL MONITOR MAINT MSG OK FOR SERVICE

Part: UNKNOWN — FAULTY (UNKNOWN) · airframe 14,982 hrs · 3,204 cycles

ETOPS - ON PDC FOUND ECAM MESSAGE ENG 1 FUEL VALVE FAULT FUEL VALVE NOT OPEN AND ENG 1 FADEC IDENT FAULT. PERFORMED TSM 77-31-00-810-801A FOUND #1 PHMU FAIL MESSAGE. REPLACED #1 PHMU PER AMM TASK 77-31-400-801A, RAN ENG NO FAULTS NOTED, OK TO CONTINUE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,898 hrs · 3,090 cycles

ETOPS - ON ENG START UP FOUND ENG 2 FADEC FAULT ON ECAM. N2 SPEED VIB INDICATION HAD AMBER X'S. REPLACED EEC PER AMM 73-21-01-400-801-A & AMM 73-21-01-400-801-A. OPS CHECK IS GOOD. OK TO CONTINUE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,893 hrs · 3,089 cycles

ETOPS - ENG2 FADEC SYS FAULT ECAM ILLUMIANTED FOR 5 SECONDS AND CLEARED. PERFORMED TSM 77-11-00-818-811-A TO (3) (D), CHECKED CONTINUITY AT WIRE HARNESS WO4, P63 AND P3. PINS Y-4,1,5. CONTINUITY CHECKED GOOD. SWAPPED PHMU 1+2 CONDITION SAME. RETURNED PHU 1+2 TO ORIGINAL POSITIONS. MOC NOTIFIED CONDITON REMAINS THE SAME FURTHER T/S REQUIRED. FOUND WO3 HARNESS WORN. REPLACED REF AMM 73-21-63. CHECK OK. RAN ENGINE. NO DEFECTS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,893 hrs · 3,089 cycles

ETOPS - ENG 2 FADEC SYS FAULT ON ENGINE START. ATTEMPTED ENGINE START BY MAINT DIRECTION. NORMAL ENGINE START. FAULT CLEARED WHEN AVAIL APPEARED. REMOVED & REPLACED #2 ENG EEC PER AMM 73-21-01. OPS CHECK GOOD. RAN #2 ENG IDLE. NO FAULTS NOTED OK TO CONTINUE

Part: UNKNOWN — FAULTY (UNKNOWN) · airframe 14,866 hrs · 3,084 cycles

ETOPS - ENG 2 FADEC SYS FAULT CODE 733101. REPLACED #2 PHMU PER AMM 77-31-01 NO FAULTS NOTED ENG RUN GOOD OK FOR SERVIC

Part: IGNITER — FAULTY (UNKNOWN) · airframe 14,674 hrs · 3,046 cycles

ETOPS - DURING BOROSCOPE INSPECTION FOUND #2 IGNITER WORN. REMOVED AND REPLACED IGNITER PER AMM 74-21-01. OPS CHK GOOD. A/C OK FOR SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,486 hrs · 3,008 cycles

ETOPS - APU AUTO SHUT DOWN ON ARRIVAL, ATEMPTED 3 STARTS UNSUCCESSFULLY. REMOVED AND REPLACED APU IGNITION EXCITER UNIT PER AMM 49-41-38. OPS CHECK GOOD NO FAULTS DETECTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,371 hrs · 2,985 cycles

ETOPS - SKIN INLET FAULT. INITIALLY OVRD FOR BOTH INLET/EXHAUST EXTINGUISHED THE ECAM. DESCENDING THROUGH 13,000 FT, ECAM REOCCURED AND FORCED INTO MANUAL MODE TO DEPRESSURIZED TO SL. REMOVED AND REPLACED SKIN OUTLET VALVE PER AMM 21-26-53. REF DMI 207107 FOR FURTHER MAINTENANCE ACTION. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,346 hrs · 2,980 cycles

ETOPS - INFO TO MX INFLIGHT ENG2 FIRE LOOP A FAULT ECAM. THE ECAM WENT AWAY AFTER 2 MINUTES. REPLACED ENG2 FIRE LOOP A HARNESS FIN 4165KS PER AMM 26-11-61. OPS CHECK OK. NO FAULTS NOTED. SECURITY CHECK GOOD OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,311 hrs · 2,973 cycles

ETOPS - DURING #1 ENGINE CHANGE FOUND DAMAGED FIRE DETECTOR HARNESS. REMOVED AND REPLACED FIRE DETECTOR HARNESS PER AMM 26-12-16. CHECK IS GOOD NO DEFECTS NOTED OK TO CONTUNE SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,748 hrs · 2,861 cycles

MOMENTARY LAV SMOKE ECAM DURING CRUISE. PERFORMED SYS RESET AND INSPECTED IAW AMM 26-17-00. NO FAULTS FOUND, A/C GOOD FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 12,711 hrs · 2,654 cycles

SLIDE AT R1 DOOR ACCIDENTALLY DEPLOYED. R & R THE R1 DOOR DAMPER DIAPHRAM IAW AMM 52-11-14. NO LEAKS NOTED. R & R R1 DOOR ESCAPE SLIDE IAW AMM 25-62-44. INDICATIONS OK. OPS CHECKED OK. OK FOR SERVICE.

Part: RADAR — FAULTED (WX SYSTEM) · airframe 12,434 hrs · 2,597 cycles

ETOPS - WX RADAR GCS (GROUND CLUSTER SWITCH) IS BROKEN ( WEATHER RADAR SYSTEMS GROUND CLUTTER SUPPRESSION). REMOVED AND REPLACED WEATHER RADAR CTL UNIT AND BITE TEST OK IAW AMM 34-41-12 PB 401.

Part: NONE — NONE · airframe 12,085 hrs · 2,527 cycles

BTB - ENG 1 FIRE LOOP A FAULT, 5TH WRITE FROM 9-29-2022. FOUND WIRE 708003-20R26-12 SHORTED TO GROUND. REMOVED AND REPLACED HARNESS 4165KS PER AMM 71-51-75, OPS CHECK GOOD PER AMM 26-12-00. PLACARDS REMOVED & MIC SHEET CLEARED.

Part: NONE — NONE · airframe 11,055 hrs · 2,266 cycles

DESCENDING THOUGHT 5,000' - 3,000 ' ENGINE AT IDLE EXPERIENCE DIRTY SHOCK SMELL AGAIN // FOUND EVIDANCE OF OIL LEAK ON #1 ENG AT 9 O CHOCK POSITION IN THE FIC REPLACED SEAL FROM LP62 OIL PRESSURE TUBE REF AMM PW 10006-C-72-00-30-00A-702A-B LEAK CHECK GOOD 18439 6/14/22 NEED TO ACCOMPLISHED DECONTAMINATION PERFORM ECS WITH APU AND ENGINE #1 AND #2 ENGINE RUN WITH BLEED NO SIGNS AFTER 30 MIN CHECK GOOD LEVEL A PER TASK 21-00-00-615-802-A OK FOR SERVICE 6414

Part: SWITCH — INOPERATIVE · airframe 9,598 hrs · 1,941 cycles

ETOPS - RAT FAULT DURING RAT EXTENSION AND STOWAGE TEST // REMOVED AND REPLACED RAT ACTUATOR PRESSURE SWITCH REF AMM 29-22-53-400-013-A. OPS CHECK AND LEAK CHECK GOOD.

Part: CONNECTOR — DAMAGED (FIRE LOOP) · airframe 8,894 hrs · 1,803 cycles

ETOPS - ENG 1 FIRELOOP A FAULT CAME ON SHORTLY AFTER T/O. FOUND STUD C CONNECTOR OF ENG 1 LOOP A COMMON FWD DETECTOR CABLE BROKEN. REMOVED AND REPLACED (4181KS) PER AMM 26-12-61. ALSO PER MOC AS PRECAUTIONARY REMOVED & REPLACED #1 LOOP A AGB PER AMM 26-12-17. OK FOR SERVICE

Part: WIRE HARNESS — CHAFED (NR 2 FIRE LOOP) · airframe 8,827 hrs · 1,790 cycles

ETOPS - ENG 2 FIRE LOOP A FAULT. RESISTANCE CHECK AT PIN J - K AT FDU 2 (2WD2) CONNECTOR A. FOUND 1.49K OHMS. RESISTANCE GOOD WITH TAPPING DETECTORS. NO FAULT NOTED. NO SHORT TO GND. INSULATION TEST OK. DURING T/S FOUND CHAFED WIRE ON 4165KS HARNESS. REPLACED WIRE HARNESS 4165KS, ENG #2 FIRE LOOPS OPS CHECK OK PER AMM 26-12-00-710-001-A.

Part: GCU — FAULTED (NR 2) · airframe 7,577 hrs · 1,535 cycles

ETOPS - ATB - ELECT GEN 2 FAULT//REMOVED AND REPLACED GCU 2 IAW AMM 24-22-34. BITE TEST OK. PERFORMED ENGINE 2 RUN UP. OPS TEST GEN 2 NORMAL. NO FAULLTS NOTED.

Part: GCU — DEFECTIVE (NR 1) · airframe 6,457 hrs · 1,312 cycles

ETOPS ECAM MX STATUS "AC GEN". REMOVED & REPLACED NR 1 GCU, PER AMM 24-22-34. MX STATUS CLEARED, OK FOR SERVICE.

Part: BLADE — DAMAGED (ENGINE FAN) · airframe 6,181 hrs · 1,245 cycles

NR 4 FAN BLADE ON NR 2 ENGINE S/N JB1AEA4305 MISSING POLYURETHANE COAT. REMOVED AND REPLACED NR 4 FAN BLADE, PER AMM 72-11-03-400-801-A. FUNCTIONAL TEST FAN TRIM BALANCE AMM TASK 71-00-00-710-807-A PENDING. PERFORMED FUNCTION TEST (FAN TRIM BALANCE), PER AMM 71-00-00-710-807-A THRU STEP 4.A.(7) CONT. AT 80% N1 SPEED CU'S WAS 0.6 AND MAG WAS 0.2168. AT 91% (MAX N1 SPEED) CU'S WAS 1.0 AND MAG WAS 0.3242. NEED TO CONTINUE FROM STEP 4.A.(8) 9/13/20 17942. PER ENGINEERING, SWAPPED BLADES 3 (SN - JB1AEA4282) AND 14 (SN - JB1AEA1972). PERFORMED FAN TRIM BALANCE, PER AMM 71-00-00-710-807-A MAX MAG NOTED=0.0854. OK FOR SERVICE.

Part: PANEL — LEAKING (NR 2 NACELLE) · airframe 5,989 hrs · 1,183 cycles

ETOPS SIGNIFICANT SYSTEM - DURING CRUISE ECAM AIR ENG 2 BLEED LEAK. THIRD WRITE UP TODAY. FOUND GAP CLEARANCE OF OVER PRESSURE FLAP DOOR ON PANEL 423DT. REWORKED PRECOOLER PANEL 423DT #2 PYLON PER TASK CARD E105-213003-INI. REPLACED PANEL AND CLEARANCE CHECK OK.

Part: NONE — NONE (NONE) · airframe 4,577 hrs · 897 cycles

ATB - BIRD STRIKE ON DEPARTURE. RIGHT SIDE OF AIRCRAFT. // ACCOMPLISHED AMM TASK 05-51-14-200-803-A. FOUND EVIDENCE OF BIRD STRIKE ON INBOARD RH FLAP. WILDLIFE SVC COLLECTED EVIDENCE. CLEANED AREA. NO DEFECTS NOTED. A/C OK FOR SVC.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 3,855 hrs · 756 cycles

SMOKE AFT LAV ECAM WARNING ILLUMINATED MOMENTARILY NEAR TOP OF DESCENT. SUSPECTED VAPING NOTHING CONFIRMED. FLT ATTENDANT WITNESSED PASSENGER ENTER AFT LAV WITH VAPE PEN. OPS CHECKED DETECTOR - NO DEFECTS FOUND. OK FOR CONTINUED SVC.

Part: WARNING MESSAGE — FALSE INDICATION (NR 2 ENGINE) · airframe 2,414 hrs · 471 cycles

ETOPS SIGNIFICANT SYSTEM - ENG 2 AIR SYSTEM FAULT ON APPROACH. // PERFORMED BITE TEST ON EEC 1 & 2, NO FAULTS NOTED. DID A HISTORY SEARCH ON THIS FAULT AND NONE WERE FOUND PREVIOUS OF THIS ONE. WILL CONTINUE MONITORING AS REQUIRED PER TSM 75-26-00-810-819-A. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,390 hrs · 274 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER 30S ON IGN/START, NR 2 ENG OIL CHIP DETECTION ON ECAM. CLEARED AFTER 5 SECONDS, NO FURTHER INDICATIONS. INSPECTED MAGNETIC CHIP DETECTORS PER AMM 75-00-00-281-802-A NO CHIP DETECTED. OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,390 hrs · 274 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER 30S ON IGN/START,#2ENG OIL CHIP DETECTION ON ECAM. CLEARED AFTER 5 SECONDS, NO FURTHER INDICATIONS.//INSPECTED MAGNETIC CHIP DETECTORS PER AMM 75-00-00-281-802-A NO CHIP DETECTED. OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,380 hrs · 272 cycles

SUP - ETOPS SIGNIFICANT SYSTEM - NR 2 ENG OIL CHIP DETECTION ECAM WHEN IGN/START SELECTED. EXTINGUISHED AFTER 30 SECONDS. NO FURTHER INDICATIONS. CHECKED MAGNETIC CHIP DETECTORS PER AMM 79-00-00-281-802-A - NO CHIPS DETECTED - OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 1,354 hrs · 267 cycles

ETOPS SIGNIFICANT SYSTEM - NR 2 ENG OIL CHIP DETECTOR ECAM WHEN IGN/START SELECTED. EXTINGUISHED AFTER 1 MINUTE. NO FURTHER INDICATIONS. PERFORMED AMM TASK 79-00-00-281-802-A. CHECKED CHIP DETECTOR-NO CONTAMINANTS FOUND. RAN NR 2 ENG- NO ECAM MESSAGE ASSOCIATED. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CHIP DETECTOR) · airframe 1,301 hrs · 257 cycles

ETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED WHILE ATTEMPTING TO START ENGINE #2.// PERFORMED CHIP DETECTOR INSP PER TSM 79-00-00-281-802A. NO FAULTS FOUND. CLOSED COWLS. RAN ENGINE, NO ECAM MESSAGE NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 2 CHIP DETECT) · airframe 977 hrs · 195 cycles

ETOPS SIGNIFICANT SYSTEM - UPON PLACING ENGINE MODE SELECTOR TO IGN/START, ENG 2 OIL CHIP DETECTED ECAM DISPLAYED. MAINTENANCE ADVISED TO START ENG 2, ENG HAD A NORMAL START AND CAM DISAPPEARED WHEN ENG 2 MASTER SWITCH WAS PLACED TO ON.// PERFORMED AMM 79-00-00-281-802-A ON #2 ENG. NO DEFECTS NOTED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (CHIP DETECTOR) · airframe 977 hrs · 195 cycles

ETOPS SIGNIFICANT SYSTEM - UPON PLACING ENGINE MODE SELECTOR TO IGN/START, ENG 2 OIL CHIP DETECTED ECAM DISPLAYED. MAINTENANCE ADVISED TO START ENG 2, ENG HAD A NORMAL START AND CAM DISAPPEARED WHEN ENG 2 MASTER SWITCH WAS PLACED TO ON.// PERFORMED AMM 79-00-00-281-802-A ON #2 ENG. NO DEFECTS NOTED. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 ENGINE) · airframe 899 hrs · 180 cycles

ETOPS SIGNIFICANT SYSTEM - DURING PREFLIGHT - ECAM ENG 2 BOWED ROTOR PROTECTION FAULT DISPLAYED. // PERFORMED EEC SYSTEM TEST PER AMM 73-21-00. TEST OK. PERFORMED EEC RESET TO CONFIRM IF ACTUAL FAULT. MESSAGE CLEARED. CONTACT PRATT & WHITNEY REP. PERFORMED IDLE ENGINE RUN FOR 5 MUNITES PER AMM 71-00-00-860-823-A & 71-00-00-720-811-A. NO ECAM FOR ENG 2 BOWED ROTOR PROTECTION FAULT. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 747 hrs · 151 cycles

STRONG ODOR CIRCULATED THROUGHOUT ENTIRE AIRCRAFT DURING DESCENT FROM FL200 DOWN TO THE SURFACE, SMELLED LIKE DIRTY SOCKS & CHEMICALS. NOTICED SMELL IN CABIN UPON ENTRY TO AIRCRAFT. ISOLATED EACH BLEED SYSTEM AND OPERATED PACKS ON FULL HOT/ FULL COLD. SMELL DISSIPATED WHEN OPERATING PACKS WITH NR 1 ENGINE BLEED. MONITORED OIL QTYS OF ENGINES AND APU BEFORE DURING AND AFTER ENG RUN. QTYS NORMAL. OPENED NR 1 ENGINE TR COWL AND VISUALLY INSPECTED #1 ENG EXTERNALLY, NO LEAKS NOTED. SUSPECT SMELL WAS FROM RESIDUAL OIL PRIOR TO NR 1 ENG CHANGE. REFERENCE TSM 05-50-00, AMM 71-00-00 & AMM 21-51-00. OK FOR SERVICE.

Part: BEARING — FAILED (NR 1 ENGINE) · airframe 742 hrs · 148 cycles

ETOPS SIGNIFICANT SYSTEM - IN CRUISE, ECAM MASTER WARNING AIR-BLEED LEAK. FOLLOWED ECAM PROCEDURE AND ECAM CLEARED. REMAINING ECAM: AIR ENG 1 AND 2 BLEED FAULT RIGHT COND HOT AIR FAULT, ENG 1 OIL CHP DETECTED. SMOKE SMELL DETECTED AFTER ENGINE NR 1 START// BORESCOPED NR 3 FWD AND AFT BEARING FAILED. REMOVED AND REPLACED NR 1 ENGINE PER TASK CARD J321-72-HWI-02. OPS CHECK & LEAK CHECK GOOD. OK FOR SERVICE.

Part: DUCT — CONTAMINATED (BLEED AIR SYS) · airframe 714 hrs · 147 cycles

BTB SMOKE SMELL DETECTED AFTER ENGINE NR 1 START. FOUND OIL INTERMEDIATE PRESSURE DUCTING ON ENG NR 1.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 714 hrs · 147 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER LANDING ENG 1 OIL CHIP DETECTED. PERFORMED ENG 1 OIL CHIP DETECTORS INSPECTION PER AMM 79-00-00 281-802-A. NO DEBRIS FOUND INSPECTED AND REPLACED ENG 1 OIL FILTER PER 79-21-06-960-801-A. ENG 1 RUN OK.

Part: IGNITER — FAULTED (NR 2 ENGINE) · airframe 701 hrs · 139 cycles

ETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A FAULT. REMOVED AND REPLACED ENG 2 IGN A PER AMM 74-21-01, IGNITER TEST GOOD ON CH A+B. OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 695 hrs · 138 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER ENG 1 START, ECAM MSG APPEARED " ENG 1 HEAT SYS FAULT" AFTER CONFERRING W/MOC. RESTARTED ENG 1, MESSAGE CLEARED. PERFORMED TSM 73-11-00-810-849-A. EXAMINED HARNESSES AND ELECTRICAL CONNECTOR AT IFPC. NO DEFECT FOUND. IDLE RUN ENG NR 1 A AND B CHANEL. NO MAINTENANCE MSG OCCUR. OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 536 hrs · 107 cycles

ETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A FAULT. PERFORMED TASK 74-00-00-810-830-A. NO FAULTS NOTED ON GROUND. OK FOR SERVICE. ENG RUN ON GROUND FOUR TIMES ALL START SUCCESSFUL.

Part: EXCITER — FAILED (NR 2 ENGINE) · airframe 116 hrs · 25 cycles

NR 2 ENGINE IGNITER A, FAULTED ON START. REPLACED THE NR 2 ENGINE IGNITER A IAW AMM 74-21-01-000-801-A. PERFORMED AN OPS TEST IAW 74-00-00-710-802-A, OPS OK FOR AUDIBLE TEST. RAN THE NR 2 ENGINE AND IGNITER FAULT RETURNED. REPLACED THE NR 2 ENGINE EXCITER IAW AMM 74-11-01. AUDIBLE TEST PASSED, RAN THE NR 2 ENG AND FAULT DID NOT REAPPEAR. OK FOR SERVICE.