N204HA

Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 18,464 hrs · 3,847 cycles

ATB - DUE TO #1 - L DOOR SLIDE MALFUNCTION OVER WEIGHT LANDING CHECKLIST APPLIED. NEED OVERWEIGHT INSPECTION. OVER WEIGHT LANDING CHECKLIST COMPLIED WITH. IAW AMM 05-52-00. #1-L DOOR RAFT DISLODGED FROM DOOR. 1L DOOR SLIDE REMOVED IAW 25-62-44-000-012. INSTALLED 1L DOOR SLIDE PER AMM 25-62-44-400-007-A. O.K. TO CONTINUE.

Part: FILTER — UNKNOWN (LT IDG) · airframe 18,060 hrs · 3,765 cycles

ETOPS - LH IDG DRAIN, REMOVE AND DISCARD THE SCAVENGE AND CHARGE FILTER ELEMENTS AND REPLENISH IDG OIL. DICARED FILTERS DRAINED OIL AND REPLENISHED IN REF TO AMM 24-21-00-920-802-A. OPS CHECK GOOD OKAY TO CONTUINE SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 16,604 hrs · 3,473 cycles

ETOPS - ENG 2 COMPRESSOR VANE FAULT ON ECAM. REMOVED AND REPLACED HIGH PRESSURE COMPRESSOR STATOR VANE ACTUATOR PRIMARY PER AMM 75-31-02 EXERSIZED PRIMARY AND SECONDARY STATOR VANE LINKAGE VERIFIED MOVING SMOOTH, OPS CHCK GOOD OK TO CONTINUE SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 16,261 hrs · 3,402 cycles

ETOPS - DURING BOROSCOPE INSPECTION FOUND #1 ENG IGNITER PLUG B WORN. REMOVED AND REPLACED #1 ENG IGNITER PLUG B IAW A321 AMM 74-21-01-400-801-A. PERFORMED OPS TEST IAW A321 AMM 74-00-00-710-802. OPS TEST GOOD. NO DEFECTS NOTED. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 16,074 hrs · 3,364 cycles

ETOPS - FADEC SYS 2 FAULT. EEC INTERNAL FAIL. REMOVED AND REPLACE #2 ENG EEC PER AMM 73-21-01. OPS CHECK GOOD. OK FOR SVC.

Part: BLADE — DAMAGED (NR 2 ENG FAN) · airframe 14,634 hrs · 3,080 cycles

ETOPS - DMI 206748 - #2 ENG FAN BLADE POLY COAT PEELING. 0.25"X0.25" AREA - A. DEFERED PER AMM 72-11-03-220-805-A. REPAIR OR REPLACE IN 2600FC. TRANSCRIBED TO E1128-321-72-065 CLEARED MIC SHEET. ORIGINAL SUBMISSION DATE: 4/5/2023.

Part: UNKNOWN — UNKNOWN · airframe 14,438 hrs · 3,042 cycles

SUPPLEMENTAL TO HALA2023031400041 - DMI# 206653 AIR BLEED MAINTENANCE MESSAGE. (CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY). RESET FWC # 1 & 2 AND BMC # 1 & # 2. PERFORMED TEST OF THE EBAS PER TSM 36-00-00-810-804-A. TEST OK. NO FAULTS DETECTED. AIR BLEED MESSAGE CLEARED ON ECAM. A/C OK TO CONTINUE PLACARD REMOVED. MIC SHEET UPDATED.

Part: UNKNOWN — UNKNOWN · airframe 14,417 hrs · 3,038 cycles

ETOPS - DMI# 206653 AIR BLEED MAINTENANCE MESSAGE. (CLASS II MAINTENANCE MESSAGES DISPLAYED ON ECAM STATUS PAGE OF ECAM SYSTEM DISPLAY). AWAITING RESOLUTION.

Part: NONE — NONE · airframe 14,358 hrs · 3,023 cycles

ETOPS- ENG 1 FIRE LOOP B FAULT. AVIONICS FOUND ENG 1 PYLON FIRE DETECTOR LOOP B BAD. REMOVED AND REPLACED ENG 1 PYLON FIRE DETECTOR RAMP ASSY PER AMM 26-12-16. REPLACED ENG 1 LOOP B PYLON FIRE DETECTOR REF 26-12-16. REPLACED 45VC-A HARNESS ENG REF AMM 71-51-75. OPS TEST GOOD. BITE GOOD OK FOR SVC.

Part: WIRE HARNESS — FAULTED (NR 1 FIRE DETECT) · airframe 14,085 hrs · 2,970 cycles

ETOPS-DURING INTIAL TAXI ECAM ENG 1 FIRE LOOP A FAULT. INDICATED BTD. FOUND FWD AGB FIRE DETECTOR SHORT TO GROUND. REMOVED AND REPLACED FWD AGB FIRE DETECTOR PER AMM 26-12-17. NO FAULTS NOTED OK FOR SERVICE. REMOVED AND REPLACED FIRE HARNESS ASSY ( 4165KS) PER AMM26-12-61, OPS CHECK GOOD OK FOR SERVICE

Part: NONE — NONE · airframe 11,012 hrs · 2,202 cycles

BTB FRONT LEFT NOSE WHEEL TIRE WORN TO CHORD.// REMOVED AND REPLACED LEFT SIDE NOSE TIRE AS PER AMM 32-41-12. SPIN/SECURITY CHECK GOOD. OK TO CONTINUE.

Part: FIRE LOOP — OUT OF LIMITS (APU LOOP B) · airframe 10,091 hrs · 2,011 cycles

ETOPS - ECAM: APU FIRE LOOP B FAULT // FOUND LOOP B FIRE DETECTOR OUT OF LIMITS. REMOVED AND REPLACED APU FIRE DETECTOR LOOP B. PER AMM 26-13-00. OPS CHECK GOOD.

Part: NONE — NONE · airframe 10,003 hrs · 1,993 cycles

ETOPS - ENG 1 OIL CHIP DETECTED // PERFORMED TSM 79-35-00-810-808-A REMOVED AND REPLACED OIL FILTER ELEMENT PER AMM 79-21-06-960-801-A ENG RUN AND LEAK CHECK GOOD NO FAULTS NOTED OK FOR SERVICE

Part: WARNING MESSAGE — FALSE ACTIVATION (TURBINE COOLING) · airframe 9,150 hrs · 1,824 cycles

ETOPS - ENG 1 TURB COOL FAULT // PER AIRBUS RECOMENDATION - ACCOMPLISH TSM 75-24-00-810-803-A, 7907. ACCOMPLISHED TSM 75-24-00-810-803 UP TO AND INCLUDING STEPS 4A(4). PERFORMED TSM 75-24-00-810-803-A STEPS 4A(6) THRU 4A(8)(B)3. NO DEFECTS NOTED, ALL WIRES RESISTANCE CHECKS AT .45 OHM AND NO SHORTS AND OPEN TO GND. PRECAUTIONARY REPLACED #1 ENG ACC VALVE PER AMM 75-24-00 6414. OPERATIONAL CHECK GOOD PER AMM 75-24-60

Part: STRAP — BROKEN (EMERGENCY EXIT) · airframe 7,336 hrs · 1,458 cycles

EMERGENCY EQUIPMENT, EMERGENCY EXIT DOORS SAFETY STRAP FOR PIN BROKE AT POSITION 2. RESECURED SAFETY STRAP. OPERATIONS CHECK, OK FOR SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (RADIOR) · airframe 7,166 hrs · 1,417 cycles

ATB, BOTH HF RADIOS ARE INOP, NO TRANSMISSION ON TRANSMIT OR RECEIVING. PERFORMED RESET AND BITE TEST OF BOTH HF SYS, IAW AMM 23-13-00. OPS TEST GOOD. PRECAUTIONALLY REMOVED AND REPLACED NR 3 RMP, PER AMM 23-13-13. OPS GOOD. NO FAULTS NOTED. OK FOR SVC.

Part: AUTOTHRUST SYS — MALFUNCTIONED · airframe 6,621 hrs · 1,295 cycles

ETOPS SIGNIFICANT SYSTEM - BLOCK TURN BACK - AUTO THRUST AND CAT 3 SYSTEM INOP. SHUTDOWN ENGINE AND RESET AUTO/THRUST AND DISCONNECT. // PERFORMED AFS TEST PER AMM 22-96-00, OPS TEST PASSED. OK FOR SERVICE. LAND TEST PASSED PER AMM 22-97-00.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 5,218 hrs · 1,017 cycles

ON REMOVAL OF THE R1 DOOR SLIDE, IT DEPLOYED. REPAIR IN WORK.

Part: CHIP DETECTOR — CONTAMINATED (NR 1 ENGINE) · airframe 4,890 hrs · 952 cycles

ETOPS / AFTER LANDING ENG 1 OIL CHIP DETECTOR FAULT. PERFORMED TSM 79-00-00281-802-A. FOR INSP OF MAGNETIC CHIP COLLECTORS FOR OIL CONTAMINATION. FOUND DEBRIS NOT MORE THAN 25% OF PROBE TIP PERIMETER. PER TSM CLEAN CHIP COLLECTORS AND RETURNED A/C FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,765 hrs · 733 cycles

R1 DOOR EMERGENCY WALL LIGHT (90WL2) INOP. // REPLACED EMERGENCY LIGHT AS REQUIRED. OPS CHECKS GOOD. OK FOR SVC

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,765 hrs · 733 cycles

R1 DOOR EMERGENCY WALL LIGHT (90WL2) INOP. REPLACED EMERGENCY LIGHT AS REQUIRED. OPS CHECKS GOOD. OK FOR SVC.

Part: STARTER — FAULTY (NR 1 ENGINE) · airframe 3,333 hrs · 651 cycles

ATB / AFTER TAKEOFF ECAM ENG 1 START VALVE FAULT. START VALVE NOT CLOSED PERFORMED ECAM ACTIONS. REPLACED STARTER.

Part: START VALVE — FAILED (NR 1 ENGINE) · airframe 3,312 hrs · 646 cycles

AIR TURN BACK ECAM FOR ENGINE NR 1 START VALVE FAULT. SAV (STUCK) FAILED OPEN. REMOVED AND REPLACED STARTER AIR CONTROL VALVE.

Part: WARNING MESSAGE — FALSE ACTIVATION (NR 2 IGNITION) · airframe 2,615 hrs · 512 cycles

ETOPS SIGNIFICANT SYSTEM - ENG 2 IGN A FAULT ON LANDING. // PERFORMED OPS TEST ENG 2 IGN SYS A AND B PER AMM 74-00-00-710-802-A. OPS NORMAL. PERFORMED ENG RUN SWITCHING TO IGN B. NO CURRENT FAULTS DISPLAYED. OK FOR SVC.

Part: START VALVE — FAULTED (NR 1 ENGINE) · airframe 2,473 hrs · 485 cycles

ATB - ETOPS SIGNIFICANT SYSTEM - AFTER TAKEOFF "ENG 1 START VALVE FAULT - START VALVE NOT CLOSED" ECAM. ATTEMPTED 1(ONE) ENG 1 BLEED SWITCH IS SET BUT FAILED.// REMOVED AND REPLACED #1 ENGINE START VALVE IAW AMM 80-11-03 PB 401 CONF 21 OPS AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: FIRE LOOP — FAULTY (NR 2 ENGINE) · airframe 2,214 hrs · 433 cycles

ETOPS SIGNIFICANT SYSTEM, ENG 2 FIRE LOOP A FAULT. REMOVED & REPLACED PYLON A LOOP PER AMM 26-12-16-000-802 & AMM 26-12-16-400-802. FAULT CLEARED OPERATIONAL TEST OF ENGINE FIRE & OVERHEAT DETECTION OK PER AMM 26-12-00-710-002-A. OK FOR SERVICE.

Part: AUTOTHROTTLE SYS — MALFUNCTIONED (COCKPIT) · airframe 2,024 hrs · 396 cycles

ETOPS SIGNIFICANT SYSTEM, ECAM AUTO FLT A/THR OFF AFTER ENG START. RETURNED TO GATE. PERFORMED AFS TEST, TEST PASSED.

Part: NOT REPORTED — MALFUNCTIONED (WEATHER RADAR) · airframe 1,982 hrs · 388 cycles

ETOPS SIGNIFICANT SYSTEM - WX RADAR SYS 2 IN AUTO HAS ERRONEOUS READINGS. NEEDS TO BE CALIBRATED. SYS 1 OPS OK. PERFORMED BITE TEST AND SYSTEM TEST OF WEATHER RADAR SYSTEM 2 PER AMM 34-41-00. NO DEFECTS NOTED. OPS TEST GOOD. OK FOR SVC

Part: TIE DOWN — CONTAMINATED (CARGO BAY) · airframe 1,982 hrs · 388 cycles

AT GATE, FA'S AND PILOTS NOTICED STRONG CHEMICAL SMELL CONCENTRATED TOWARDS AFT/LAST 10 ROWS OF AIRCRAFT. FA'S COMPLAINED OF LIGHT HEADINESS. REMOVED EXCESS SEALANT AROUND BARRIER TIE DOWNS. VENTED AFT CARGO COMPARTMENT. NO CHEMICAL ODOR NOTED.

Part: STRUCTURE — BENT (LOWER FUSELAGE)

TAIL STRIKE ON FUSELAGE BELLY AT FRAMES 62 TO 68, FOUND ON GROUND DURING WALK AROUND. SECTION 18 FRAMES 65-70 AND PARTIAL REPLACEMENT OF SECTION 17 FRAMES 61-64 STRINGER 32 LT TO 32 RT. ON AUGUST 13 2018 THE SUBJECT ACFT OPERATED BY HAWAIIAN AIRLINES. SUSTAINED TAIL STRIKE DAMAGE DURING LANDING AT LAX ON FLIGHT NR HA56. NO LOAD 15 REPORT WAS TRIGGERED AND NO PILOT WRITE UPS FOR HARD LANDING WERE GENERATED. DFDR ANALYSIS WAS COMPLETED BY AIRBUS AND IT SHOWED THAT NONE OF THE HARD LANDING CRITERIA HAS BEEN EXCEEDED. THE INSPECTION ARE COMPLETED IAW ECRA5341-01131 AND REVEALED THAT RESULTANT DAMAGE SPANS FROM APPROX FRAME 62 TO FRAME 68 AND STRINGER 42R TO STRINGER 42L AND INCLUDES FUSELAGE SKINS IDENTIFIED IN SRM 53-41-11 FIGURE 005, ITEM 5 AS PN E5347441020600 AND SRM 53-41-11 FIGURE 012 ITEM 1 AS PN D5348001620000 AS WELL ADJACENT UNDERLYING FRAME CLIPS, SHEAR WEBS, FRAMES, CROSSBEAM MEMBERS, STRINGERS, AND OTHER UNDERLYING STRUCTURES. REFERENCE 3 DAMAGE ASSESSMENT REPORT SHOWS THE DAMAGE DETAILS. THIS ECRA PROVIDES ZERO STRESS JACKING AND SHORING AS WELL AS REPAIR PROCEDURES FOR THE NOTED DAMAGE.

Part: WARNING MESSAGE — FALSE ACTIVATION (IGNITER) · airframe 1,904 hrs · 373 cycles

NR 1 ENG IGNITER A FAULTED ON START. PERFORMED TSM 74-00-00-810-834A, & AMM 74-00-80-710-802. IGNITERS A & B CHECKED OK. AUDIBLE SOUND HEARD. OK FOR SERVICE. NO 30 DAYS HISTORY.

Part: SOLENOID — FAILED (NR 1 ENGINE) · airframe 1,359 hrs · 268 cycles

NR 1 ENGINE SYS FAULT ILLUMINATED. PERFORMED TSM 75-32-00-810-844-A. REPLACED THE LT ENGINE ACTIVE HPC BLEED VALVE CONTROL SOLENOID IAW AMM 75-32-03-400-801-A. TEST 3 IDLE & LEAK CHECKED GOOD. OK FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (AIR SYSTEM NR 2) · airframe 136 hrs · 29 cycles

AIR SYS 2 FAULT ECAMS DURING DESCENT. PERFORMED ECAMS ACTION WITH ENG 2 BLEED OFF AND PACK 2 OFF. PERFORMED TSM 75-26-00-810-818-A. NO FAULTS NOTED. PERFORMED ALTERNATE METHOD PARA 4. NO FAULTS NOTED. OK TO CONTINUE.

Part: WARNING LIGHT — FALSE ACTIVATION (AIR SYS 2) · airframe 110 hrs · 24 cycles

AIR SYS 2 FAULT DURING DESCENT. PERFORMED TSM 75-26-00-810-818A, OPERATED THE RT ENGINE AT 80% N1 IAW AMM 71-00-00-720-816-A. NO FAULTS DURING ENGINE RUN. EIU2 AND FADEC2 SHOW NO FAULTS ON LAST LEG REPORT. COULD NOT DUPLICATE ISSUE, ACFT OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 95 hrs · 21 cycles

ECAM WARNING FOR LAVATORY SMOKE DURING CRUISE ALTITUDE. F/A REPORTED IN LAVATORY D. PERFORMED TSM 26-17-00-810-804-A, LAVATORY SMOKE WARNING WITHOUT FIRE FOR LAV 'D'. ALL TEST PASSED, NO FAULTS NOTED, OK TO CONTINUE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 55 hrs · 13 cycles

AFTER THE NR 2 ENGINE START, STATUS A/THR APPEARED 'BTB'. RESET FMGC 1& 2, PERFORMED AFS TEST IAW AMM 22-96-00 NO FAULTS NOTED. ALL TEST PASSED OK TO CONTINUE.