N208HA

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 19,688 hrs · 4,311 cycles

DIV - AVIONICS DOOR OPEN IN FLIGHT MESSAGE A/C NOT PRESSURIZING NORMALLY. PERFORMED VISUAL INSPECTION OF AVIONICS DOOR. PERFORMED PRESSURIZATION TEST FOR AIR LEAKS PER AMM 05-53-00. NO DEFECTS NOTED. OK TO CONTINUE.

Part: FUEL SYS — LEAKING · airframe 19,494 hrs · 4,272 cycles

ETOPS - FUEL LEAK COMING OUT LH AND RH WING DRY BAY WEEP HOLES. REPAIRED BOTH LEFT & RIGHT WING DRY BAY FUEL LEAKS IN ACCORDANCE WITH SRM 51-76-12. PERFORMED LEAK TEST PER AMM 28-11-00. NO LEAKS NOTED.

Part: IGNITER — FAILED (NR 2 ENGINE) · airframe 18,944 hrs · 4,159 cycles

ETOPS - ENG 2 IGN A FAULT DURING START. REMOVED AND REPLACED IGN A IGNITER PLUG ON ENG 2 PER AMM 74-21-01. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE

Part: DISPLAY — FAULTED (ZONE 200) · airframe 18,854 hrs · 4,140 cycles

ETOPS - MCDU'S DON'T MATCH WHEN IT COMES TO FUEL PREDICTION, TIME PREDICTION, AND VERTICAL PATH ERROR. FO'S MCDU APPEARS TO SHOW TIME: 4 MINUTES EARLIER, FUEL BURN: 400 MORE POUNDS, ABOVE DESCENT PATH: 400 FEET. REMOVED AND REPLACED FQIC PER AMM 28-42-34-04. NO DEFECTS NOTED OK FOR SERVICE.

Part: VALVE — FAULTED (ZONE 400) · airframe 18,826 hrs · 4,134 cycles

ATB DUE TO ECAM ENG 2 BLEED FAULT. REMOVED AND REPLACED #2 ENGINE FAN AIR VALVE PER AMM 36-11-54. BITE TEST OF LEFT ENGINE BLEED SYSTEM GOOD. PERFORMED IDLE RUN OF #2 ENGINE. ALL CHECKS GOOD. OK TO CONTINUE

Part: IGNITER — FAILED (APU) · airframe 18,395 hrs · 4,046 cycles

ETOPS-BTB: APU FAIL. REPLACED APU IGNITOR PLUG AND LEAD REF AMM 49-41-41 AND 49-41-43, OPS TEST NORMAL. OK FOR SVC.

Part: SWITCH — FAULTED (APU OIL) · airframe 17,697 hrs · 3,911 cycles

ETOPS - BEFORE TOW OPERATIONS, ATTEMPTED TO START APU, "APU AUTO SHUT SHUTDOWN" MESSAGE SHOWN ON ECAM. APU GRANDSCAN CONFIRMS "OIL FILTER SWITCHES" FAULT. CLEAN CONNECTORS P5 & P9 IAW TSM 49-90-00-810-812-A. APU START NOT SUCCESSFUL. REMOVED & INSPECTED PRESSURE SWITCHES IAW AMM 49-91-14. NO DEFECTS NOTED. REINSTALLED- APU START NOT SUCCESSFUL. REMOVED & REPLACED OIL FILTERS IAW AMM 49-91-41. APU START NOT SUCCESSFUL. REMOVED & REPLACED IGNITION EXCITERIAW AMM 49-4-38-400-003-A. REMOVED & REPLACED BOTH OIL FILTER SWITCHES IAW AMM 49-91-14400-002-A. OPS CK GOOD. APU GROUNDSCAN-NO FAULT DETECTED. A/C OK FOR SVC

Part: OIL FILTER — CLOGGED (APU) · airframe 17,301 hrs · 3,833 cycles

ETOPS - FOUND APU OIL FILTERS CLOGGED. REMOVED AND REPLACED APU OIL FILTERS PER AMM 49-91-41-200-002-A. LEAK AND OPS CHECK GOOD. OK FOR SERVICE.

Part: CONTROL VALVE — FAULTED (NR 2 A/C PACK) · airframe 17,279 hrs · 3,829 cycles

ETOPS - PACK 2 FAULT PRIOR TO DEPARTURE. REMOVED AND REPLACED PACK 2 FLOW CONTROL VALVE PER AMM 21-51-51. OPS CHECK / LEAK CHECK OK.

Part: CONNECTOR — DAMAGED (ZONE 100) · airframe 17,019 hrs · 3,779 cycles

ETOPS - APU FAULT ON TAXI OUT BTB. ITEM ALREADY ON DMI, REPLACED AND RESECURED PINS/ JUMP CONNECTORS PER AMM 49-16-00-003-A OPS CHK OF APU GOOD OK TO REMAIN ON DMI.

Part: STICK SHAKER — WARNING MESSAGE (ZONE 200) · airframe 31,726 hrs · 34,527 cycles

ABORTED TO @ 30-40 KTS PSEU AND STICK PUSHER FAIL MSG. PERFORMED SLAT DISAGREE BITE PER FIM 27-80 TASK 803. COULD NOT DUPLICATE FAULT. OK TO CONTINUE

Part: PACKING — LEAKING (NR 1 ENGINE) · airframe 16,653 hrs · 3,697 cycles

ETOPS - #1 ENG OIL NEAR FAN BLADES (OIL BLADES). REMOVED AND REPLACED #1 ENG FAN SHAFT COVER PACKING IDLE POWER TEST GOOD. LK CK GOOD. OK FOR SERVICE IAW AMM 72-15-00-960-801-A

Part: FILTER — FAULTED (ZONE 100) · airframe 15,744 hrs · 3,517 cycles

ETOPS - APU AUTO SHUTDOWN TWICE DURING PREFLIGHT. PERFORMED BITE TEST, FAULTED GEN SCAV AND LUBE FILTERS. REMOVED AND REPLACED BOTH FILTERS IN REF W/ AMM 49-91-41-200-002-A. APU OPS CHECK GOOD. LEAK CHECK GOOD. NO LEAK NOTED. OK FOR SVC.

Part: APU — SHUTDOWN (ZONE 100) · airframe 15,525 hrs · 3,472 cycles

ETOPS - APU: AUTO SHUT DOWN ON TAXI IN 3X ATTEMPTS FAILED. REMOVED & REPLACED WIRING FROM APU STARTER MOTOR + TERMINAL LUG TO 7120VC PIN 1. WIRES X011A20, X011B14, X011C14 PER ESPM 20-33-11. REMOVED & REPLACED APU STARTER MOTOR CLUTCH PER AMM 49-42-52. PERFORMED OPS TEST OF APU PER AMM 49-00-00, OPS TEST GOOD. OK FOR SERVICE.

Part: PACKING — LEAKING (HYD PRESS SWCH) · airframe 14,519 hrs · 3,273 cycles

ETOPS - HYD LEAK COMING FROM LH AFT DRAIN MAST. REMOVED AND REPLACED PACKING ON # 1 ENG HYD PUMP PRESSURE SWITCH PER AMM 29-11-17, OPS AND LEAK CHECK OKAY.

Part: PLUG — MISSING (OIL MANIFOLD DRN) · airframe 14,350 hrs · 3,238 cycles

ETOPS - SAW A FEW DROPS OF OIL UNDER #1 ENGINE FAN COWL. FOUND LP05 OIL MANIFOLD DRAIN PLUG MISSING SCREW REF PIPC 79-21-49-01 ITEM 320 & 140 & 150. INSTALLED MISSING BOLT P/N: ST2601-06. NO LEAKS NOTED OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,288 hrs · 3,224 cycles

FOUND EMER LT/EPSU (12WL) INOP DURING SERVICE CHECK. REMOVED AND REPLACED EPSU BATTERYPER AMM 33-51-38. BITE TEST GOOD. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,940 hrs · 3,139 cycles

ETOPS - HYDRAULIC OIL LEAKING FROM RH ENGINE. REMOVED AND REPLACED O RING SEAL IN COUPLING HALFT FROM YELLOW HYDRAULIC SYSTEM PER AMM 29-13-39. LEAK CHECK WITH DRY MOTOR OF ENGINE PER AMM 71-00-00-860-817A GOOD. NO FAULTS. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 13,717 hrs · 3,063 cycles

ETOPS - 1L DOOR HANDSET UNREADABLE ON INTERCOMAND PA. REMOVED AND REPLACED 1L DOOR HANDSET. OPS CHECK GOOD. OK FOR SERVICE PER AMM 23-73-44.

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 15,054 hrs · 3,378 cycles

ETOPS - ENG 2 FIRE LOOP A FAULT ON ECAM PAGE. REMOVED AND REPLACED FIRE DETECTOR ELECTRICAL LOOP A PER AMM 26-12-61-000-807-A. OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,643 hrs · 2,639 cycles

SUPPLEMENTAL SUBMISSION TO HALA2023041300086. CORRECTION FROM REGISTRATION # 217HA TO 208HA. ATB - AFTER REACHING CRUISE ALT FL340 ENG 1 START VALVE FAULT ECAM. VERIFIED START VALVE POS CLOSED, MOVED FREELY (REF TSM 80-11-00-810-828-A) REMOVED AND REPLACED #1 STARTER PER AMM 80-AA-01. LEAK CHECK AND OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,483 hrs · 2,608 cycles

ETOPS - DUIRNG T/C 321-72-HWI-03 LEAK CHECK FOUND PRV MUSCLE TUBE CRACKED AND LEAKING BLEED AIR. REMOVED AND REPLACED PRV MUSCLE TUBE IAW AMM 36-11-52-000-802-A. AND 36-11-52-400-802-A. OPS CK GOOD. LEAK TEST GOOD. OK TO CONTINUE.

Part: FAN — FAULTY · airframe 11,427 hrs · 2,597 cycles

SUPPLEMENTAL TO HALA2023032000051. UPDATED WITH RESOLUTION. ETOPS - DMI# 206665 VENT EXTRACT FAULT. (CREW PLACARD). REMOVED AND INSTALLED VENT EXTRACT FAN PER AMM 21-26-51-00. PERFORMED OPERATIONAL TEST OF VENTILATION SYSTEM PER AMM 21-26-00-710-001-A. OPS CHECK GOOD. PLACARD REMOVED MIC SHEET UPDATED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 11,386 hrs · 2,589 cycles

ETOPS - DMI# 206665 VENT EXTRACT FAULT. (CREW PLACARD). AWAITING RESOLUTION.

Part: UNKNOWN — UNKNOWN · airframe 11,359 hrs · 2,583 cycles

ETOPS - DMI# 206657 ENG 1 FIRE LOOP B FAULT IN CRUISE ( ENGINE FIRE DETECTION SYSTEMS LOOP B (EXCEPT FOR ER OPERATIONS BEYOND 120 MINUTES, ONE MAY BE PROVIDED: ASSOCIATED LOOP A IS OPERATIVE / THE ENGINE FIRE TEST IS PERFORMED BEFORE EACH DEPARTURE) ) TROUBLESHOT PER TSM 26-12-00-810-804-A. FOUND PYLON LP "B" DETECTOR (4WD1) INTERNAL SHORTING TO GROUND. NEED TO REPLACE #1 ENGINE PYLON DETECTOR LP "B". REMOVED AND REPLACED, #1 ENGINE PYLON DETECTOR LOOP "B", PER AMM 26-12-16. OPS CHECK GOOD. MIC SHEET CLEARED, PLACARD REMOVED.

Part: COMPUTER — FAULTED · airframe 11,254 hrs · 2,561 cycles

ETOPS - AVNCS SYS FAULT DURING PREFLIGHT. FOUND INLET BYPASS V (16HQ) FAULT. DEFERRED PER MEL 21-26-03. REF TSM 21-26-00-810-806-A, CHSNGED INLET BYPASS VALVE (16HQ), CONDITION SAME. REMOVED & REPLACED AEVC COMPUTER. BITE CHECK GOOD, NO FAULTS NOTED. PLACARD RMVD, MIC SHEET UPDATED.

Part: NONE — NONE · airframe 9,448 hrs · 2,178 cycles

ETOPS - APU LEAK DETECT FAULT ON ECAM. PERFORMED TSM 36-22-00-810-876-A. FOUND ELEMENT SESOR (15HF) SHORTED TO GRN. REMOVED AND REPLACED OVHT SENS ELEMENT (15HF) PER AMM 36-22-17-400-001 BITE TESET GOOD. OK FOR SVC.

Part: NONE — NONE · airframe 9,192 hrs · 2,111 cycles

ETOPS - AT 8000' "ENG 2 FADEC SYS FAULT THRUST LEVER 2 NOT ABOVE IDLE" THRUST LEVERS WERE IN CL DETENT // PERFORMED INSPECTION OF ENG #2 EEC AND N2 SPEED TRANSDUCER HARNESS & CONNECTIONS PER TSM 77-11-00. CHECKS OK. REMOVED & REPLACED ENG #2 N2 SPEED TRANSDUCER PER AMM 77-11-23. NO FAULTS NOTED. OK FOR SVC.

Part: NONE — NONE · airframe 7,831 hrs · 1,739 cycles

ETOPS - STATUS MSG , ENG # 1 FIRE LOOP A FAULT // RESET FDU 1 C/B'S PER AMM 26-12-34, AS PRECAUTIONARY REMOVED AND REPLACED FDU 1 CAS6465, RAN # 1 ENG AT IDLE FOR FIVE MINUTES NO FAULTS NOTED, OPS CHECK GOOD , OK FOR SERVICE

Part: COMPUTER — FAULTED (SLAT\FLAPS) · airframe 7,597 hrs · 1,656 cycles

BTB 2 - SELECTING FLAPS 1 ECAM F/CTL FLAPS FAULT // PERFORMED BITE OF SFCC PER AMM 27-54-00. FAULTING SFCC2 22CV. REMOVED AND REPLACED SFCC2 PER AMM 27-51-34, OPS CHECK GOOD. OK FOR SVC

Part: NONE — NONE · airframe 7,597 hrs · 1,656 cycles

BTB 1 - SPEED LIMIT DISPLAYED ON BOTH PFD’S FD+SPD LIM RED INDICATIONS // RE-SET A/C TO NORMAL CONDITIONS. BOTH PFD FD AND SPD LIM INDICATIONS ARE ABSENT. INDICATIONS READING NORMAL.

Part: SKIN — DAMAGED · airframe 7,332 hrs · 1,602 cycles

DURING PDC FOUND BOTTOM TAIL AREA FUSELAGE SKIN DAMAGE AND AFT GALLEY DRAIN MAST DAMAGE. DAMAGE AREA: FRAME 61-70, STRINGER 42LH - 40 RH. 176" LONG 22" WIDE // REPAIRED DAMAGE TO BOTTOM TAIL AREA AT FRAME 61-70 STRINGER 42LH-40RH AS PER AIRBUS WOTD: M-308924-EMBOD 12/30/21 MECH 2590 INSP 12559

Part: CLAMP — LOOSE (FIRE LOOP) · airframe 7,174 hrs · 1,571 cycles

ETOPS - ENG 1 FIRE LOOP A FAULT DURING TOW UP, FAULTING ENG 1 LOOP A CORE AND AGB LOOPS FOUND LOOSE CLAMP AND WIRE ON LOOP A HI TEMP WIRE HARNESS. SECURED CLAMP AND ADJUSTED SLACK ON HARNESS REPLACED ENG 1 LOOP A CORE DETECTOR PER AMM 26-12-17. ALL OPS CHECK GOOD

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE) · airframe 6,763 hrs · 1,476 cycles

ETOPS - ENG2 FIRE LOOP A. PERFORMED TSM26-12-00-810-825-A & TSM 26-12-00-810-914-A. REPLACED ENG2 FIRE LOOP A PER AMM26-12-16-400-803-A AND INSTALLED PYLON FIRE DETECTOR IAW AMM 26-12-16-400-802-A. SECURITY CHECKED GOOD. RAMP ASSY.AMM26-12-00-710-001.SECURITY CK,OPS TEST OK. BIE FDU & BMC2 NO FAULTS, OPS CHECKED GOOD. P/N OFF/ON:8891-48. S/N OFF:D0069794,P/N ON 8891-48 S/N ON:D0042882

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 6,415 hrs · 1,407 cycles

ETOPS - PASSING FLI 80 "ENG 2 FIRE LOOP B FAULT" MSG. MSG CLEARED AFTER APPROX 5 MINS. REPEAT WRITE UP. FOUND ENG 2 LOOP B INTERMITTENT. PERFORMED CONTINUITY CHECK PER TSM 26-12-00. NO FAULT NOTED. PRECAUTIONARY ACTION, REMOVED AND REPLACED FWD FIRE LOOP ASSY PER AMM 26-12-17, STEPS 1 THRU 4.B. OPERATIONAL CHECK OK PER AMM 26-12-00-710-801-A.

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 6,348 hrs · 1,394 cycles

ETOPS - ECAM ENG2 FIRE LOOP A FAULT, REMOVED AND REPLACED FIRE DETECTOR ENG 2 LOOP A PYLON IAW AMM 26-12-16 OPS CHECK OK NO FAULTS NOTED.

Part: FIRE LOOP — BROKEN (NR 2 NACELLE) · airframe 5,897 hrs · 1,305 cycles

ETOPS - #2 FIRE LOOP A FAULT // FOUND ENGINE 2 PYLON DETECTOR LOOP A (3WD2) BROKEN. REMOVED PYLON FIRE-DETECTOR RAMP ASSY PER A321 AMM 26-12-16-000-802-A. 21402. 3/29/21.

Part: CHIP DETECTOR — FALSE INDICATION (NR 1 ENGINE) · airframe 4,706 hrs · 930 cycles

ETOPS SIGNIFICANT SYSTEM- AFTER LANDING: ECAM ENG 1 OIL CHIP DETECTED. // PERFORMED TSM 79-35-00-810-808-A "CHIP DETECTED ALERT BY ODM" NO METAL DEBRI FOUND. OK TO CONTINUE. REMOVED AND REPLACED OIL FILTER PER AMM 79-21-06-960-801-A. PERFORMED IDLE RUN LEAK CHECK. LEAK CHECK GOOD. OK TO CONTINUE.

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 4,415 hrs · 866 cycles

SUP - ECAM: ENG. 2 FIRE LOOP A FAULT ON CLIMB. // REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECK OK. OK FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (FIRE LOOP A) · airframe 4,415 hrs · 866 cycles

ETOPS: ECAM - ENG 2 FIRE LOOP A FAULT ON CLIMB. REPLACED FIRE LOOP A DETECTOR PER AMM 26-12-16, FUNCTIONAL CHECKED OK.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 4,210 hrs · 825 cycles

ETOPS SIGNIFICANT SYSTEM - AFTER GO AROUND ECAM "ENG 1 START VALVE FAULT. START VALVE NOT CLOSED" COMPLIED WITH ECAM ACTIONS. // PERF EEC OPS TEST NO.6 PER AMM 73-21-00-710-807-A. NO DEFECTS NOTED.

Part: START VALVE — OPEN (NR 2 ENGINE) · airframe 3,218 hrs · 628 cycles

ETOPS SIGNIFICANT SYSTEM - ENGINE 2 START VALVE FAULT, VALVE NOT CLOSED. REMOVED AND REPLACED STARTER ON ENGINE 2, PER AMM 80-11-01. OPS CHECK GOOD. OK TO CONTINUE.

Part: FAULT MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 2,887 hrs · 563 cycles

ATO - BRAKE SYSTEM 2 FAULT CAME ON @ TAKEOFF POWER. ABORTED TAKEOFF RESET A/SKID AND N/W STEG. RESET SUCCESSFUL. NO INBOUND FAULTS. PREFORMED TROUBLESHOOTING IN REF. WITH TSM 32-51-00-810-514-A. NO DEFECTS NOTED. OKAY FOR SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 2,362 hrs · 460 cycles

LAVATORY SMOKE ECAM IN-FLIGHT, PAX SUSPECTED OF SMOKING IN LAV D. CHECKED LAV D SMOKE DETECTOR & WASTE BIN FIRE EX, NO FAULTS FOUND. PERFORMED CIDS SDF1 LAV SMOKE WARN TEST NO FAULTS. OK FOR SVC. REF AMM 26-17-00

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 1,770 hrs · 345 cycles

LAV C SMOKE WARNING WENT OFF FOR SEVERAL SECONDS AND FA'S VERIFIED OPS NORMAL WITH NO SMELL. T/S PER TSM 26-16-17-00-810-812-A. OPS CKS GOOD, OK TO CONTINUE.

Part: OUTFLOW VALVE — FAULTED (CABIN PRESSURE) · airframe 1,698 hrs · 331 cycles

ATB - VENT SKIN VALVE FAULT. // FOUND MAIN SKIN AIR OUTLET VALVE IN PARTIALLY OPEN POSITION, MANUALLY OPENED VALVE TO FULL OPEN. ACCOMPLISHED AEVC TEST TWICE, BOTH PASSED. VALVE OPS OK.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 870 hrs · 172 cycles

DURING FLIGHT LAV SMOKE WARNING, FA PANEL INDICATED LAV 1, NO SMOKE FOUND.// NO SMOKE DETECTED, NO SMOKE INDICATED. OK FOR SERVICE PER AMM26-17-01.

Part: IGNITER — MALFUNCTIONED (NR 2 ENGINE) · airframe 341 hrs · 71 cycles

ETOPS SIGNIFICANT SYSTEM - BTB ENG 2 IGN A INOP. PERFORMED OPERATIONAL CHECK OF #2 ENGINE IGNITER "A" OPS CK NORMAL ON GROUND. OK TO CONTINUE. REF AMM 74-00-00 PB 501.

Part: FIRE LOOP — FAULTED (NR 2 ENGINE) · airframe 30 hrs · 10 cycles

ETOPS SIGNIFICANT SYSTEM - ATB - DUE TO ENG. 2 LOOP "A" FAULT. // REMOVED AND REPLACED PYLON FIRE - DETECTOR RAMP ASSEMBLY PER AMM 26-12-16. EMPLOYEE# 3752 (11/14/18). OPERATIONAL CHECK PENDING. OPS CHECK GOOD PER AMM 26-12-00-710-002, FAULT WENT AWAY AND NO DEFECTS NOTED.