N216HA

Part: FUEL FILTER — CLOGGED (NR 2 ENGINE) · airframe 17,547 hrs · 3,814 cycles

ETOPS - INFO TO MX ON DEPARTURE CLIMB ENG 2 AMBER CLOG ANNUNCIATOR ILLUMINATED ON ENG SD PAGE. MESSAGE CLEARED AFTER A FEW MINS. PERFORMED TSM 73-11-00-810-822-A. REMOVED AND REPLAACED FUEL FILTER. FADEC SYSTEM IDLE TEST OK. NO LEAKS NOTED. OK FOR SVC.

Part: SMOKE DETECTOR — NO DISCREPANCY (ZONE 200) · airframe 17,324 hrs · 3,770 cycles

LAV SMOKE ECAM IN FLIGHT. ECAM CLEARED ITSELF AFTER 3 SECONDS, FA'S INVESTIGATED AND FOUND NO SOURCE OF FIRE. SUSPECT PAX VAPING. PERFORMED TSM 36-17-00-810-804-A NO DETECTORS FAULTING. NO FAULTS ON POST FLIGHT REPORT CLEANED DUST FROM ALL 4 LAVS. OK FOR SERVICE.

Part: CONNECTOR — INOPERATIVE (HYD PUMP) · airframe 17,238 hrs · 3,753 cycles

ETOPS - BTB. HYD G ENG 1 PUMP LO PR INDICATION 8X ON TAXI OUT. HYD PAGE PUMP LOW PRESSURE PTU OPERATING SHOWING AMBER AND GREEN INDICATIONS ENG 1 PUMP FAULT LIGHT ON OFF THROUGH INDICATIONS. REMOVED AND REPLACED PRESSURE SWITCH PART #450-1-3100-00 AND ELECTRICAL CONNECTOR P/N EN299E61203BN ON ENG#1 GREEN HYD SYS IAW AMM 29-11-17-400-802. PERFORMED ENGINE RUN ON #1 ENGINE, IDLE TO 25-30% NO FAULTS NOTED G HYDRAULIC PUMP INDICATES PRESSURE NORMAL RAN ENGINE FOR 20 MINS OPS CHECK GOOD.

Part: LATCH — FOD (R4 DOOR SLIDE) · airframe 17,150 hrs · 3,737 cycles

4R DOOR DISARMED DURING FLIGHT. WOULD NOT REARM. PERFORMED PRESSURIZATION CHECK WITH 4R DOOR ARMED. FOUND ARM/DISARM LEVER NOT FLUSH. FOUND SLIDE LOCK/LATCH BLOCKED WITH DEBRIS. RMEOVED DEBRIS. OPS CHECK OK. OK FOR SVC.

Part: PRESSURE SWITCH — LOOSE (HYD PUMP) · airframe 49,805 hrs · 3,684 cycles

ETOPS-ECAM HYD G ENG 1 PUMP LO PR TURNED OFF ENG 1 PUMP AS INSTRUCTED BY ECAM. PERFORMED TSM 29-11-00-810-804-A, FOUND PRESSURE SWITCH LOOSE. REMOVED AND REPLACED ENG 1 PUMP PRESSURE SWITCH (1047GK) PER AMM 29-11-17. OPS CHECK AND LEAK CHECK GOOD, NO FAULT NOTED. OK FOR SVC.

Part: SEAL — LEAKING (FAN SHAFT) · airframe 15,411 hrs · 3,387 cycles

ETOPS - DURING WALK AROUND, FOUND OIL SEEPING FROM EN1 S/N: P770687 INLET CONE. UPON INSPECTION, FOUND OIL INSIDE INLET CONE. REMOVED & REPLACED FAN SHAFT COVER SEAL PER AMM 72-15-00-960-801-A. NO LEAKS NOTED POST IDLE RUN. OK FOR SERVICE.

Part: SELECTOR — FAILED (CABIN TEMP) · airframe 15,165 hrs · 3,337 cycles

ETOPS-FORWARD TRIM AIR VALVE NOT RESPONDING APPROPIATELY TO SWITCH POSITION. TEMP IN CABIN HOT WITH FULL COLD SET. PREVIOUSLY WRITTEN UP, NO CHANGE. REMOVED AND REPLACED TEMPERATURE SELECTOR PER AMM 21-63-11-000-001-A (21315 3/8/24. PENDING OPS CHECK. PERFORMED OPS CHECK OF CAB TEMP CONTROL PER AMM 21-63-00-710-004-A, TEST OK. OK FOR SVC

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 15,149 hrs · 3,334 cycles

AFT EXIT SIGN BURNT OUT AIRCRAFT LEFT SIDE. CLEANED AFT EXIT SIGN CONNECTORS. OPS CHECKED PER AMM 33-51-00 CHECK GOOD OK FOR SERVICE.

Part: PUMP — FAULTY (HYD SYS) · airframe 13,376 hrs · 2,945 cycles

ETOPS - ENG #2 HYDRAULIC DRIPPING, 1 DRIP PER SECOND. REMOVED AND REPLACED ENG#2 HYD PUMP IAW AMM 29-13-51-000-806-A. ACCOMPLISHED ENG #2 IDLE RUN, NO LEAKS NOTED. AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 12,767 hrs · 2,818 cycles

ETOPS - INFO TO MTX: ON CLIMB OUT MOMENTARY ECAM OF: ENG 1 FIRE LOOP A FAULT. CLEARED ITSELF UP AS WE BEGAN ECAM ACTIONS. INSTALLED NEW #1 ENG FIRE ELEC HARNESS ASSY. PER AMM TASK 26-12-61, OPS TEST OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 12,671 hrs · 2,799 cycles

INFO TO MX: DURING CRUISE BRIEF ECAM (2X) ENG.1 FIRE LOOP A FAULT. ECAMS CLEARED AFTER APPROX 3 SECS. NOTED BY MAINTENANCE. PERFORMED OPERATIONAL TEST OF THE ENG. FIRE AND OVERHEAT DETECTION TEST I.A.W. AMM 26-12-00-710-002-B. TEST O.K.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 12,418 hrs · 2,748 cycles

ATB - RIGHT WING FUEL AND TEMP INDICATIONS AMBER XX'S, FOB AMBER XX'S. ATTEMPTED QRH RESET WITH MX VIA SATCOM - UNSUCCESSFUL. REMOVED & REPLACED R WING TANK FUEL PROBES 30QT2 & 59QT2 PER AMM 28-42-15 R TANK INDICATION & FOB INDICATION & TEMP INDICATION SHOW NORMALLY.

Part: WIRE HARNESS — OUT OF LIMITS (FIRE LOOP B) · airframe 11,777 hrs · 2,621 cycles

ETOPS-ENG B FIRE LOOP ON ECAM. CHECKED RESISTANCE BETWEEN PINS J-K AT FDU 2 LOOP B. FOUND RESISTANCE FLUCTUATING FRANTICALLY OUT OF LIMITS WHILE TAPPING HARNESS 4166KS. REMOVED & REPLACED HARNESS 4166KS PER AMM 26-12-62. RESISTANCE STAYED SOLID AT 1.5K OHMS. ECAM MSG CLEARED OK FOR SERVICE.

Part: DEU — FAULTED (LAVATORIES) · airframe 11,632 hrs · 2,590 cycles

ETOPS - ALL LAVATORIES NOT WORKING IN FLIGHT, HEADING BACK TO LAX. PERFORMED CIDS POWER UPTEST AND FAULTED 300RH8. REMOVED AND REPLACED DEU-B 300RH8 IAW AMM 23-73-47 PB 401, OPS CHECK OF ALL LAV AS OKAY. AC OK TO CONTINUE. ORIG SUB DATE: 1/3/2023

Part: HPC — USED · airframe 11,248 hrs · 2,509 cycles

ETOPS-DURING PDC FOUND #2 ENG LEAKING FUEL AT HPC PRIMARY STATOR VANE ACTUATOR. REMOVED AND REPLACED #2 ENG HPC PRIMARY STATOR VANE PER AMM 75-31-02-400-801-A. MECH 16488 / 21800. PENDING IDLE RUN / LEAK CHECK. COMPLETED IDLE RUN & LEAK CHECK PER AMM 71-00-00-720-811. NO LEAKS NOTED. A/C OK FOR SVC.

Part: IGNITER — FAILED (APU) · airframe 2,457 hrs · 10,987 cycles

ETOPS - APU AUTOSHUTDOWN - TRIED A SECOND TIME WITH ANOTHER AUTOSHUTDOWN. REMOVED AND REPLACED IGNITER AS PER AMM 49-41-41-400-0041-A, ALSO REMOVED AND REPLACED EXITER BOX AS PER AMM 49-41-38-400-003-A, PERFORMED OPS CHECK NORMAL. APU VERIFICATION FLIGHT FOR N216HA (FLT#79) COMPLETED "SATISFACTORILY." INFLIGHT START ON 1ST ATTEMPT @ FL340 (-46)

Part: SENSOR — FAULTED (INLET) · airframe 10,966 hrs · 2,453 cycles

AIR ENG 1 HP VALVE FAULT. REPLACED PACK INLET PRESS SENSOR (LH) FIN (23HB1) PER AMM 21-51-13. LEAK CHECK OK. OPS PENDING 10-19-22 16801... REMOVED AND REPLACED #1 ENG HPV PER AMM 36-11-51. OPS AND LEAK CHECK PENDING 7880 10/18/22.. CONT ON LOG #895086 ITEM 1. HP VALVE OPS AND LEAK CHECK OK PER AMM 36-11-51. LH PACK INLET PRESS SENSOR OPS AND LEAK CHECK OK PER AMM 21-51-13. PERFORMED HIGH POWER RUN ON BOTH ENGINES, ALL PARAMETERS NORMAL. NO FAULTS NOTED. A/C OK FOR SVC.

Part: NONE — NONE · airframe 10,341 hrs · 2,313 cycles

ETOPS - ENG 2 FIRE LOOP B FAULT DURING CLIMB @ 16000' PRIOR TO ETOPS ENTRY // REMOVED & REPLACED ENG 2 FIRE LOOP B AGB PER AMM 26-12-17. OPS TEST OF ENG FIRE & OVERHEAT DETECTION GOOD PER AMM 26-12-00. OK FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT\CABIN) · airframe 8,559 hrs · 1,846 cycles

ON APPROACH STRONG SOCK SMELL LEVELING OFF @ 4000 IN COCKPIT AND FWD CABIN. PERSISTING THROUGH ENG SHUTDOWN // PERFORMED #1 & #2 ENG IDLE RUN PER AMM 71-00-00-860-823-A.OPERATIONAL CHECK OF #1 & #2 PACK PER AMM 21-51-00-710-002-A. NO SMELL NOTED. OK FOR SVC.

Part: OIL SYSTEM — OVERSERVICED (NR 1 ENGINE) · airframe 8,383 hrs · 1,812 cycles

INFO TO MX ON DESCENT PASSING 5000' FAINT WET SOCK SMELL THROUGH AIR GASPRES. WENT AWAY AFTER A FEW MIN. FOUND ENG 1 OVER SERVICED BY APPROX 3 QTS. REMOVED EXCESS OIL FROM TANK. OPERATED ENG @ IDLE FOR FOR APPROX 5 MIN. NO SMELL. OK FOR SVC.

Part: NONE — NONE · airframe 7,880 hrs · 1,714 cycles

ETOPS - APU SHUTDOWN PRIOR TO A/C REPOSITIONING // PERFORMED TSM 49-00-81-810-825-A NEED TO REPLACE IGNITION EXCITER PER PARAGRAGH 4A2A REMOVED AND REPLACED IGNITION EXCITER PER AMM 49-41-38. ALL CHECKS GOOD.

Part: UNKNOWN — ODOR · airframe 7,598 hrs · 1,658 cycles

IMMEDIATELY AFTER ENGINE START (LIGHT) AND AFTER INITIATING DESCENT (STRONG) DIRTY SOCK SMELL IN COCKPIT. PERFORMED TROUBLESHOOTING OF ENGINES AFTER SMOKE/OIL FUMES IN THE CABIN PER TSM 71-00-00-810-847-A. RAN BOTH ENGINES 1&2 AND OPERATED ALL PAX SYSTEMS. NO ODORS DETECTED. LEAK CHECK GOOD. OK TO CONTINUE

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 5,734 hrs · 1,285 cycles

EMER EQ - EPSU BATTERIES 11WL AND 13WL FAULTING // REMOVED AND REPLACED EPSU BATTERIES AT 11WL AND 13WL PER AMM 33-51-38-400-002-A. OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,526 hrs · 498 cycles

ETOPS SIGNIFICANT SYSTEM - ENG 2 IGN B ECAM WENT THRU THE ALT START PROCEDURES. THE ECAM WENT AWAY (STATUS) AFTER ENGINE SHUTDOWN AT DESTINATION. PERFORMED OPS TEST OF THE ENG 2 IGN A+B PER AMM 74-00-00-710-802-A, OPS NORMAL. NO CURRENT FAULT DISPLAYED, OK FOR SVC.

Part: TRANSDUCER — DEFECTIVE (RT ELEVATOR) · airframe 1,513 hrs · 299 cycles

ATB - "F/CTL ELEV SERVO FAULT" ILLUMINATED ON CLIMB OUT. PERFORMED OPS TEST OF SIDE STICK ASSY PER AMM 27-96-00-710-020-A. PERFORMED WIRING CHK OF POS RVDT MON SIGNAL FROM ELAC 1 MON PART TO FIRST TERMINAL BLOCK REF 27-93-07. SWAP ELAC 1 AND ELAC 2 NO HELP SWAP TO ORIGINAL. AMM 27-93-34. FLT CTL PITCH FAULT + FCDC 1 REMAINS (ELAC 1 OR WIRING FROM R ELEV POS MON XDCR). ELAC 1 (2CE1) CONNECTOR AE TO ELEV POS R XDCR UNIT (49CE2) CONNECTOR B WIRING CK OK, 2E-G, 2F-H, 2G-D, 2H-E. ALSO SEC 1 (1CE1) CONNECTOR AD TO ELEV POS R XDCR UNIT (49CE2) CONNECTOR B WIRING CK OK, 14G-G, 14H-H, 14J-D, 14K-E. ALL WIRES CONTINUITY CK GOOD, NO SHORT TO GND PER WDM 27-93-31. DURING CHECKING TRANSDUCER RESISTANCE CK, FOUND PIN D AND E PUSHED BACK ON CONNECTOR B. REMOVED & REPLACED SYS PRESSURE SWITCH(2151GN) PER TSM 27-933-00-810-947A & PRESSURE TRANSDUCER(2065GN) AMM 29-32-11, CONDITION SAME. REMOVED & REPLACED RH ELEVATOR POSITION TRANSDUCER UNIT PER TSM 27-9-00-810-872A & AMM 27-92-13. DUE TO 2 PINS PUSHED IN ON TRANSDUCER OPS CHECK OF TRANSDUCER GOOD. REMOVED AND REPLACED 1837VT TERMINAL BLOCK PER ESPM 20-44-51. PERFORMED OPS TEST OF ELAC 1 + SEC 1 PER AMM 27-93-00-710-001-A + AMM 27-94-00-710-002-A, OK FOR SVC. AIRCRAFT RETURNED TO DEPARTED STATION, WHERE A UNEVENTFUL LANDING WAS MADE.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR) · airframe 550 hrs · 112 cycles

ETOPS SIGNIFICANT SYSTEM - CAPTAIN'S SIDE ND FLICKERS BETWEEN WX + TERRAIN WHEN TERRAIN SELECTED. // DURING T/S FOUND FLICKERING ONLY OCCURS WHILE WXR 2 IS ON. REMOVED AND REPLACED #2 WXR TRANSCEIVER IAW AMM 34-41-33 PB 401 CONF 01 OPS TEST GOOD, FLICKERING BETWEEN WX AND TERR HAS STOPPED.

Part: TRANSCEIVER — MALFUNCTIONED (WX RADAR) · airframe 529 hrs · 108 cycles

ETOPS SIGNIFICANT SYSTEM - WX + T + H AND TERR FLASH CONTINUOUSLY WHEN TERR ON ND IS SELECTED ON CA'S SIDE ND.// FOUND DEFECT ASSOCIATED WITH #2 RADAR SYS. RE-RACKED #2 WEATHER RADAR TRANSCEIVER "15Q2" DEFECT CLEARED. OPS CHECK GOOD. OK TO SERVICE

Part: CARBON SEAL — MISSING (NR 1 ENGINE) · airframe 216 hrs · 48 cycles

ETOPS SIGNIFICANT SYSTEM - DURING BOROSCOPE INSPECTION OF #1 ENG FOUND AFT #3 BRG DRY FACE CARBON SEAL MISSING.// REPLACED #1 ENGINE PER TASK CARD J321-72-HWI -02. ALL REQUIRED TESTS CHECK OK. OK FOR SERVICE. ENGINE: IAE, PW1133G-JM.

Part: CONTROL VALVE — UNKNOWN (AC BAY) · airframe 216 hrs · 48 cycles

ATB AT 8,000 ECAM, AIR FAULT PACK 2. REMOVED AND REPLACED PACK FLOW CONTROL VALVE PER AMM 21-51-51-400-001-A AND PERFORMED OPS TEST OF FLOW CONTROL AND INDICATING SYSTEM PER AMM 21-51-00-710-002-A. OPS CHECK GOOD OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 180 hrs · 40 cycles

ATB - AFT CARGO DOOR OPEN IN FLIGHT. INSPECTED DOOR, VERIFIED AFT CARGO DOOR CLOSED AND LOCKED PER AMM 52-70-00. PRESSURE CHECK OF AFT CARGO DOOR OK PER AMM 05-53-00-780-001-A. PERFORMED OVERWEIGHT LANDING INSPECTION PER AMM 05-51-11-200-004-B. NO DAMAGE NOTED.

Part: PRESSURE SENSOR — FAULTY (NR 1 ENGINE) · airframe 72 hrs · 18 cycles

ETOPS SIGNIFICANT SYSTEM - ENGINE 1 OIL FILTER DEGRADE. (OIL FILTER DEGRADE CAUTION ON ECAM. REMOVED & REPLACED NR 1 OIL FILTER & NR 1 OIL FILTER DIFFERENTIAL PRESS SENSOR. ENG NR 1 OIL FILTER DEGRADE MESSAGE DID NOT RETURN. A/C IS OK FOR CONTINUE SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (CARGO DOOR) · airframe 51 hrs · 13 cycles

OPEN - ATB - AFT CARGO OPEN WARNING IN CLIMB OUT 2500FT. ECAM DOOR PAGE INDICATIONS CARGO DOOR, (INDICATIONS MAY BE INOPERATIVE PROVIDED A VISUAL CHECK IS MADE BEFORE EACH DEPARTURE TO CONFIRM THAT DOORS ARE CLOSED AND LOCKED). SUP - ATB - PERFORMED ALTERNATIVE TEST OF PROXIMITY SWITCH PER AMM 52-35-00 TEST GOOD AMM 52-35-00 TEST GOOD PRESSURIZED TO 4.5 PSI DEFERENTIAL NO ECAM WARNING NOTED MIC SHEET CLEARED PLACARD REMOVED.

Part: RECEIVER — BURNED (COCKPIT NAV)

AIRCRAFT DEPARTED RIC. EN ROUTE, CREW NOTED BURNED ODOR AND THE NAV UNIT EMITTED SMOKE (A WHISP). CREW PULLED THE CIRCUIT BREAKER OF THE AFFECTED UNIT AND RETURNED TO RIC.

Part: RECEIVER — FAILED (NR 1 NAV)

NAVIGATION RECEIVER CONVERTER FAILED CAUSING UNIT TO EMIT A BURNED ODOR IN THE AIRCRAFT COCKPIT AND UNIT DID SMOKE AT FAILURE. CREW PULLED THE CIRCUIT BREAKER AND RETURNED. NO PASSENGERS ON BOARD.