N506NK

Part: HEATER — OVERHEATED (SLIDING WINDOW) · airframe 59,397 hrs · 27,809 cycles

FO SLIDING WINDOW STARTED BUBBLING AND GOT ECAM A/I RT WINDOW KEPT BUBBLING SO WE CELETED TO PULL (W14 CB)RT WINDOW KEPT BUBBLING ACTUALLY MELTING EXTREMELY HOT W/IN ABOUT 2' OF WINDOW. WE ELECTED TO PULL CB W13 (WHC) THAT WORKED AS HEAT SLOWLY DECLINED AND BUBBLING / MELTING STOPPED. BUBBLING AREA AT LOWER FRONT NOT NEAR HEAT ELEMENT WHICH ARE AFT--

Part: A/C PACK — ODOR (NR 1) · airframe 58,393 hrs · 27,331 cycles

DIRTY SOCKS ODOR ON DECENT FUME REMOVALC CHECKLIST AVAILABLE ISOLATED TO PACK 1 ( PACKS A319 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )

Part: UNKNOWN — ODOR (CABIN) · airframe 57,903 hrs · 27,095 cycles

STRONG SOCK SMELL ON DESCENT IN COCKPIT PCK 1 TURND OFF SMELL WENT AWAY-REACTIVATED PACK & PERFORMED OPS TEST. NO FAULT OR SMELL NOTED, OPS TEST GOOD IAW AMM 21-51-00-040-002 HIS CLEARS DMI 3080182-1 PLACARD REMOVED MOC NOTIFIED

Part: NONE — NONE · airframe 56,275 hrs · 26,284 cycles

MILD VOMMIT SMELL IN COCKPIT DURING APPROACH. TURNED OFF PACK 1 NO HELP. COMPLETED FUME EVENT PROCEDURE AND TURNED OFF BOTH PACKS. MODERATE VOMMIT SMELL IN ENTIRE AIRCRAFT BY THE TIME WE PARKED.-PERFORMED TSM 05-50-00-810-831A & 71-00-00-810-801-A AND FOUND SOURCE OF SMELL TO BE COMING FROM ENG #1 PERFORMED INSPECTION ON THE ENGINE DE-OILER SEALS AND FOUND ENG 1 DE-OILER TO BE DEFECTIVE IAW TSM 71-00-00-810-087-A. PERFORMED ENG 1&2 RUN UP TEST IAW AMM 71-00-00. ISOLATED PACKS 1&2 AND FOUND #1 ENG TO BE SOURCE OF SMELL. A/C REQ NEW DE-OILER SEALS. REF L.P. 2958575-2 FOR CORRECTION.

Part: NONE — NONE · airframe 54,796 hrs · 25,642 cycles

MISCELLANEOUS COCKPIT F/O FLASHLIGHT INOP.-R&R MISCELLANEOUS COCKPIT F/O FLASHLIGHT IAW AMM 25-65-00. OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 54,550 hrs · 25,543 cycles

JUST AFTER TAKEOFF, RECEIVED F/CTRL FLAPS LOCKED ECAM RETURNED TO DFW. NO FLAP LANDING.-T/S IAW TSM 27-51-00-810-818-A AND PERFERMED DVI OF MECHANICAL PARTS OF LH/RH FLAP THRANSMISSION SYS IAW AMM 27-54-00-200-001, NO DEFECTS NOTED. CHECK OF FLAP DRIVE SYS OK PER AMM 27-54-00-220-007. ADJUSTMENT OF INTER-CONNECTING STRUTS OK PER AMM 27-51-44-820-001.A. INTER-CONNECTING STRUT SENSORS OK AT 0.5MM PER AMM 27-51-44-820-802-A...L/P (2871504-1) ACCOMPLISED OPS TEST OF FLAP DRIVE SYS IAW AMM 27-54-00-710-001-A . NO FAULTS NOTED. 67304. R/R SFCC #2 IAW AMM 27-51-34 AND PERFOMED LAND CAT III IAW AMM 22-97-00. NO FAULTS NOTED AT THIS TIME

Part: ACTUATOR — LEAKING (TE FLAP SYSTEM) · airframe 54,547 hrs · 25,541 cycles

F/CTL FLAPS LOCKED-PER TSM 27-51-00-810-818-A. PERFORMED VISUAL INSPECTION OF RH FLAP TRANSMISSION SYSTEM IAW AMM 27-54-00. FOUND RH FLAP #4 ACTUATOR TO BE LEAKING. PERFORMED LEAK CHECK OF RH FLAP DRIVE SYSTEM IAW AMM 27-54-00. NO DEFECTS NOTED. PERFORMED ADJUSTMEENT OF RH FLAP INTERCONNECT STRUT AND INTERCONNECT STRUT SENSOR IAW AMM 27-51-44. PERFORMED OPS CHECK OF FLAP DRIVE SYSTEM IAW AMM 27-54-00 NO DEFECTS

Part: MEGAPHONE — DAMAGED (CABIN) · airframe 54,517 hrs · 25,529 cycles

MEGAPHOME MOUTH PIECE CAME UNBONDED.-REPLACED MEGAPHONE FIN (7570MM) IAW AMM 25-61-51

Part: EPSU — INOPERATIVE (CABIN) · airframe 54,513 hrs · 25,528 cycles

BAT/ EPSU (11WL) EMER L FAILED OPS CHECK. REMOVED & REPLACED 11WL EPSU IAW AMM 33-51-38-000-001 & 33-51-38-400-001, SYSTEM OPS CHECKED GOOD IAW AMM 33-51-38-400-001 STEP 4D & 33-51-00-710-001 STEP 4A.

Part: MEGAPHONE — BROKEN (CABIN) · airframe 54,364 hrs · 25,469 cycles

FWD MEGAPHONE BROKEN -R&R MEGAPHONE IAW AMM 25-65-01. OPS CK GOOD.

Part: UNKNOWN — MALFUNCTIONED (LAVATORY) · airframe 54,249 hrs · 25,427 cycles

FWD & AFT LAVS INOP-RESET CIDS IAW AMM 23-73-00 OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 52,944 hrs · 24,888 cycles

HYD B ELEC PUMP OUT -PER TSM 29-12-00-810-806-A. R+R BLUE ELECTRIC PUMP IAW AMM 29-12-51. PERFORMED BLEEDING PROCEDURES IAW AMM 29-00-00. PERFORMED FUNCTIONAL CHECK OF BLUE ELECTRIC PUMP IAW 29-12-00. FUNCTIONAL AND LEAK CK OK. NO DEFECT NOTED AT THIS TIME. A/C OK FOR CONTINUED SERVICE

Part: SWITCH — FAULTY (AUTOBRAKE SYS) · airframe 51,827 hrs · 24,332 cycles

AUTO BRAKE MEDIUM INOP ( AUTO/BRK FUNCTION AUTO/BRK PANEL MODE LIGHTS (LO, MED, MAX) ON ). R/R AUTOBRAKE MED LIGHT PUSHSWITCH REF ESPM 20-45-22. OPS CHECK GOOD. DMI CLEARED. MOC NOTIFIED. PLACARD REMOVED.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 51,138 hrs · 24,030 cycles

CRACK FOUND ON WINDOW FRAME 4L, MAX DAMAGE LENGTH 8MM X MAX DAMAGE DEPTH 2MM, CAT B. RAF 2480133-2 OPENED. REF LTPR NRI 5000879765-0010.-REF LTPRNRI 5000879765-0010 ON LOG PAGE 2480136 01 AND HAS BEEN ACCOMPLISHED.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 50,481 hrs · 23,773 cycles

R2 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001. LEAK CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 50,198 hrs · 23,665 cycles

ODOR WAS DETECTED ON APPROACH BELOW 3000 CHEMICAL/ SWEET SMELL COCKPIT AND FWD CABIN ( PACKS )-PERFORMED TI 2100-1706 STAGE 1 CLEANING OF THE EFCS IAW AMM 21-00-00. FOUND NO EVIDENCE OF CONTAMINATION WITHIN OZONE FLITER R/R PRECAUTIONARY OZONE FILTER IAW AMM 21-51-41. R/R CONDENSER IAW AMM 21-52-32. PERFORMED ENGINE RUN IAW AMM 71-00-00. NO ODOR DETECTED. THIS CLEARS DMI# 2442277-1. PLACARD REMOVED MOC NOTIFIED

Part: ECS — CONTAMINATED · airframe 50,198 hrs · 23,661 cycles

"FUME EVENT CLIMBING 220-310 ISOLATED FUME EVENT DESCENT 180-GRND-ACCOMLISHED ECS DECONTAMINATION OF #1 & #2 PACKS WITH APU & ENG 1&2 NO FURHER AIR QUALITY EVENT NOTED IAW TSM 05-50-00-810-831A AND AEROTRACER FUME DETECTION TOOL"

Part: A/C PACK — ODOR (NR 1) · airframe 50,194 hrs · 23,664 cycles

AFTER TAKEOFF SWEET SMELL IN COCKPIT SMILIAR TO HYDRAULIC FLUID IN ECS. PACK 1 OFF & IMPROVED. SUSPECT CONTAMINATION OF DUCTING-FOLLOWED TSM 05-50-00-810-831-A ISOLATED TO TYPE 1 APU. FOLLOWED TSM 49-00-00-810-921-A. GVI PERFORMED REQUIRES MORE T/S DUE TO PREVIOUS HISTORY APU WILL BE PLACED ON DMI FOR ADDITIONAL T/S. PACK 1 SOURCE OF ODOR SEE FOLLOWING LP FOR CORRECTIVE ACTION. RASY OEUR AP 3628185

Part: UNKNOWN — FUMES · airframe 50,056 hrs · 23,598 cycles

ON FINAL APPROACH SUSPECTED FUME EVENT FWD OF AIRCRAFT ALTIDUDE 13000 ( PACKS WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )--

Part: MEGAPHONE — MALFUNCTIONED (CABIN) · airframe 49,718 hrs · 23,463 cycles

ZONE M MEGAPHONE DOES NOT SQUEAL WHEN TEST PLUG PULLED OUT-R/R ZONE M MEGAPHONE IAW AC DRAWING NK319-132-EQ

Part: MEGAPHONE — NO TEST (AFT CABIN) · airframe 47,799 hrs · 22,637 cycles

AFT MEGAPHONE INOPERATIVE, DID NOT TEST. R & R THE AFT MEGAPHONE IAW DRAWING NK319-132-EQ, REV 4.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,136 hrs · 22,353 cycles

DURING APPROACH, AFT F/A'S REPORTED AN ODOR IN BACK, FUME PROCEDURE USED, ODOR WENT AWAY AFTER THE NR 2 PACK WAS TURNED OFF. PERFORMED TSM 05-50-00-810-831-A, RAN BOTH PACKS INDIVIDUALLY WITH EACH ENGINE AND BOTH PACK WITH ENGINE BLEED OFF WITH CROSSBLEED ON. NO ODOR NOTED. AND NO DEFECTS NOTED

Part: APU — CONTAMINATED · airframe 46,843 hrs · 22,235 cycles

PRIOR TO DEPARTURE TURNED ON APU AND ODOR FILLED CABIN AND FLIGHT DECK. PAX AND CREW COMPLAINED OF THE SMELL-IAW TSM 05-50-00 FOUND DE-ICING FLUID AROUND SEAL OF APU INTAKE PLENUM, SUSPECT OF ODOR EVENT. APU BLEED SOURCE OF ODOR ( APU BLEED AIR SUPPLY SYSTEM ). PERFORMED PACK BURN OUT VIA APU BLEED IAW 21-00-0. R/R RECERT FILTERS IAW AMM 21-63-17. OPC/ LEAK CHECK GOOD NO ODOR DETECTED AT THIS TIME THIS CLEARS DMI# 237819002 DMI LOG UPDATED PLACARDS REMOVED MOC NOTIFIED

Part: UNKNOWN — ODOR (CABIN) · airframe 46,596 hrs · 22,133 cycles

FA'S IN THE BACK REPORTED A STRONG ODOR DURING THE TAXI OUT, RETURN TO GATE. PERFORMED IDENTIFICATION OF ODOR IAW TSM 05-50-00-810-831-A. OPS CHECKED AND RAN APU. AFTER RUNS COULD NOT DUPLICATE ODOR. ODOR WAS EXTERNAL BASED ON CREW INFO. ACFT OK FOR RETURN TO SERVICE

Part: STRIP — UNSECURE (L4 DOOR) · airframe 44,617 hrs · 21,274 cycles

HISSING NOISE STILL COMING FROM L2 DOOR. INSPECTED THE L4 DOOR. FOUND UPPER DOOR TEFLON STRIP INTERFERING BETWEEN DOOR AND SEAL. REMOVED IAWAMM 52-13-18. UNABLE TO HEAR ANY NOISE WHEN PRESSURE APPLIED IAW 05-53-00.

Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 44,615 hrs · 21,273 cycles

LOUD HISSING NOISE CAME FROM L2 CABIN DOOR. INSPECTED THE L2 DOOR IAW AMM 52-11-00 AND FOUND LANYARD LOOSE. SECURED AND VERIFIED CLEARANCE OF GEAR BAR OPERATION GOOD , ACFT OK FOR SERVICE

Part: DOOR — DIRTY (EMERGENCY EXIT) · airframe 43,780 hrs · 20,896 cycles

F/A REPORTED LOUD WIND NOISE FROM THE RT WING EMERGENCY EXIT. PERFORMED OPS, CLEANING, AND LUBE OF THE RT EMERGENCY OVERWING EXIT DOOR IAW AMM 52-21-11. ACCOMPLISHED A PRESSURE CHECK IAW AMM 05-53-00. OPS CHECKED GOOD. NO NOISE NOTED, ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,778 hrs · 20,894 cycles

L2 DOOR EMERGENCY LIGHT IS INOPERATIVE.

Part: STRUT — OUT OF ADJUST (INTERCONNECT) · airframe 43,704 hrs · 20,859 cycles

FLIGHT CONTROL FLAP LOCKED ALIGNMENT FAULT. ACCOMPLISHED FAULT ISOLATION IAW TSM 27-51-08-810-818A, FOUND INTERCONNECT STRUT OUT OF ADJUSTMENT. ADJUSTED THE STRUT IAW AMM 27-51-44-820-001. PERFORMED BITE TEST OF SFCC 1 AND 2, NO FAULTS INDICATED AND OPS TESTED OK IAW AMM 27-54-00-710-001.

Part: DOOR SILL — CORRODED (FRAMES 16-20) · airframe 43,700 hrs · 20,856 cycles

FOUND CORROSION ON FWD RT DOOR SILL FRAMES 16 - 20 STRINGER 23L. REPAIRED IAW EO 53111738, REV 00, AND 7054901/017.

Part: ARM — DAMAGED (RUDDER HINGE) · airframe 43,700 hrs · 20,856 cycles

RUDDER HINGE ARM BR4 AND BR5 HAS ELONGATED HOLE. PERMANENT RE OF RUDDER HINGE 4 AND 5 ELONGATED HOLES PERFORMED IAW EO 5536-1709 REV.00 DATED:MAY.16.2017 AND AIRBUS TO 80305432/005/2017 #A SEE LTPR D/O:5000651547-0010 AND M/O:1001938890-0010 THIS IS A CAT 'A' REPAIR!

Part: RIB — GOUGED (RT WING) · airframe 43,700 hrs · 20,856 cycles

FOUND A GOUGE ON THE RT WING WS 1228 RIB 23. REPAIRED IAW EO 5721-1720, REV 00, AND TD 80304436/005.

Part: DOOR SILL — CORRODED (L1 DOOR) · airframe 43,700 hrs · 20,856 cycles

FOUND CORROSION ON THE FWD LT DOOR SILL FRAME 16 - 20, STRINGER 23L REPAIRED IAW EO 5311-1739, REV 00, AND 70548978/023.

Part: WINDOW FRAME — CRACKED (FRAME 8) · airframe 43,700 hrs · 20,856 cycles

LEFT WINDSHIELD FRAME 8, Y 12292 FOUND CRACKED. PERFORMED A BLEND OUT REPAIR IAW EO 5311-1735.

Part: HINGE — GOUGED (LT ELEVATOR) · airframe 43,700 hrs · 20,856 cycles

FOUND A GOUGE ON THE LT ELEVATOR HINGE NR 4 FWD SPAR RIB 5-10. REPAIRED IAW EO 5526-1707, REV 00, AND TD 80302449/013/2017.

Part: WINDOW FRAME — GOUGED (COCKPIT) · airframe 43,700 hrs · 20,856 cycles

WINDOW FRAME FOUND GOUGED. REPAIRED THE RT WINDSHIELD FRAME IAW EO 5311-1740, REV 00, AND SRM 51-73-00, REV 118.

Part: RUDDER — DAMAGED · airframe 43,700 hrs · 20,856 cycles

FOUND WATER INGRESS ON RUDDER LT SIDE SHELL RIB HOIST POINT NR 2. AREA NR 1, 33 MM, AREA NR 2, 55 MM, AREA 1, 24 MM, AREAS 2, 78 MM WIDTH. PERFORMED DOUBLE REPAIR IAW EO 5541-1708

Part: DUCT — LOOSE (NR 2 ENGINE) · airframe 42,873 hrs · 20,943 cycles

F/A REPORT STRONG FUMES DURING DECENT (6000 FT) . FUMES NOTICED IN COCKPIT AS WELL. FOUND NR 2 ENG OIL BREATHER DUCT LOOSE, MISALIGNED WITH COWLING OUTLET. REALIGNED & SECURED IAW AMM 72-61-49 PB401. CLEANED ALL OIL RESIDUE IN FAN CASE IAW AMM 70-27-00. R&R DEOILER MATING RING ASSEMBLY IAW AMM 72-60-31- PB401 & 72-60-29 PB401. NO LEAKS NOTED IAW AMM 71-00-00.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 42,577 hrs · 20,365 cycles

FIRST OFFICER`S OXYGEN MASK LEAKING . R & R THE OXYGEN MASK IAW AMM 35-12-41. OPS CHECKED GOOD

Part: SEAL — UNKNOWN (DE OILER) · airframe 42,544 hrs · 20,350 cycles

F/A REPORTED A DIRTY SOCK ODOR AS ACFT CAME THROUGH 10,000FT. COCKPIT DIDN'T DETECTED ANY ODOR. R & R THE NR 1 AND 2 ENGINE DEOILER SEALS. TROUBLESHOT WITH TSM 05-50-00-810-831-A. PERFORMED RESIDUAL BURNING AND STAGE 2 CLEANING OF THE ECS IAW AMM 21-00-00-160-061. NO ODOR NOTED AT THIS TIME.

Part: UNKNOWN — ODOR · airframe 41,166 hrs · 19,716 cycles

DURING DESCENT AT APPROXIMATELY 5000 FT NOTICED A PECULIAR ODOR SIMILAR TO DIRTY SOCKS. PERFORMED ENGINE RUN OF NR 1 AND NR 2 ENGINE IAW TSM 71-10-00-810-801. ISOLATED BLEED AIR TO BOTH ENGINES AND APU AND COULD NOT DUPLICATE ODOR. CHECKED NR 1 AND NR 2 ENGINES AND APU FOR OIL LEAKS, NO LEAKS FOUND OR SIGNS OF LEAKAGE. NO ODORS NOTED AT THIS TIME. ACFT OK FOR SERVICE.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 38,333 hrs · 18,410 cycles

F/O O2 MASK AIRHOSE BROKE OFF. R & R F/O O2 MASK IAW AMM 35-12-41. OPS CHECK GOOD. NO LEAKS NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 35,568 hrs · 17,134 cycles

OXYGEN MASKS ABOVE L1 JUMPSEATS DEPLOYED IN FLIGHT. PERFORMED OXYGEN MASK DROP CHECK IAW AMM 35-23-00. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 35,552 hrs · 17,128 cycles

DURING TAXI OUT, O2 MASK DEPLOYED FROM FWD LAV. OPS CHECKED GOOD IAW AMM 35-23-00.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 32,161 hrs · 15,623 cycles

PRIMARY OBSERVER SEAT INOPERATIVE, OXYGEN MASK LEAKING. R & R OXYGEN MASK IAW AMM 35-12-41. OPS AND LEAK CHECKED GOOD.

Part: OXYGEN MASK — MALFUNCTIONED (COCKPIT) · airframe 32,161 hrs · 15,623 cycles

F/O OXYGEN MASK WILL NOT STOP RUNNING. R & R OXYGEN MASK AND STOWAGE BOX IAW AMM 35-12-41-400-001-A/35-12-41-000-001-A. PERFORMED LEAK CHECKS. NO LEAKS NOTED.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 32,157 hrs · 15,621 cycles

F/O OXYGEN MASK WILL NOT STOP RUNNING. R & R OXYGEN MASK AND STOWAGE BOX IAW AMM 35-12-41-400-001-A/35-12-41-000-001-A. PERFORMED LEAK CHECKS. NO LEAKS NOTED.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 30,986 hrs · 15,127 cycles

ROW 8L, OXYGEN MASK FELL DOWN. PERFORMED OPS CHECK OF MANUAL MASK RELEASE IAW AMM. OPS CHECKED GOOD.

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 30,947 hrs · 15,110 cycles

DURING TAKE OFF ROLL, DROPPED ONE OXYGEN MASK AT ROW 15, RT SIDE. REPACKED OXYGEN MASK AT SEAT ROW 15 RT IAW AMM 35-21-43-550-801-A.

Part: SEAL — MISALIGNED (EMERGENCY EXIT) · airframe 29,723 hrs · 14,575 cycles

LEFT OVERWING EXIT DOOR MAKING A HUMMING AND WHISTLING NOISE FROM UPPER PORTION OF WINDOW HATCH. REMOVED LT OVERWING DOOR. INSPECTED SEAL. FOUND SMALL SECTION UPPER SEAL DISPLACED. REINSTALLED SEAL. IAW MM.

Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 29,713 hrs · 14,572 cycles

1ST OBSERVERS OXYGEN MASK WILL NOT TRANSMIT SPEECH, IS VERY MUFFLED & DISTORTED. R & R OXYGEN MASK (10RN3 BOX) IAW AMM, CHECLED OK, NO LEAKS DETECTED.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 28,863 hrs · 14,171 cycles

RIGHT OVERWING DOOR EMERGENCY LIGHT COVER DAMAGED. R & R LIGHT COVER EMERGENCY RT OVERWING SECTION IAW ACFT MM, CHECKED OK.

Part: SLIDE — FAULTED (L1 DOOR) · airframe 28,766 hrs · 14,130 cycles

ERSU TEST SHOWS ESCAPE SLIDE LT/ EPSU (10WL) FWD FAULT IAW TSM. R & R L1 ESCAPE SLIDE ASSY IAW ACFT MM.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 28,657 hrs · 14,076 cycles

RIGHT OVERWING DOOR EMERGENCY LIGHT LENS COVER DAMAGED.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 28,440 hrs · 13,966 cycles

EMERGENCY LIGHTS NOT OPERATING PROPERLY, PERFORMED OPS TEST OF THE EPSU EMERGENCY LIGHTS IAW ACFT MM. ALL 4 BATTERIES FAULT AT LOCATION 10WL, 11WL, 12WL AND 13WL. R & R BATTERY PACK.

Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 28,230 hrs · 13,859 cycles

FA’S REPORT EMERGENCY EXIT WINDOW ACFT LT IS MAKE A LOUD "HISSING" NOISE AT FL 320. REMOVED & INSPECTED SEAL ON DOOR NO FAULTS FOUND INSTALLED DOOR IAW ACFT MM PRESSURISED CABIN FOUND NO LOUD HISSING.

Part: PANEL — DISLODGED (EMERGENCY EXIT) · airframe 27,596 hrs · 13,544 cycles

ACFT LEFT OVERWING EXIT SHOWED OPEN ON ECAM. FOUND LT OVERWING ACCESS HANDLE PANEL FELL OFF DOOR. INSTALLED ACCESS HANDLE PANEL IAW AMM. SYS OP OK.

Part: HANDLE — DISLODGED (EMERGENCY EXIT) · airframe 27,662 hrs · 13,579 cycles

EMERGENCY EXIT ECAM ON IN FLIGHT DUE TO HANDLE FELL OFF. REPLACED HANDLE, LIGHT OUT AND INSTALLED HANDLE IAW AMM.

Part: COVER — DISPLACED (EMERGENCY EXIT)

LEFT EMERGENCY EXIT ECAM CAME ON. COVER HAD FALLEN OFF. INSTALLED LT EMERGENCY EXIT DOOR COVER FLAP IAW AMM.

Part: SEAL — DISLODGED (EMERGENCY EXIT) · airframe 27,580 hrs · 13,533 cycles

LEFT OVERWING EMERGENCY EXIT WINDOW MAKING LOUD HISSING NOISE. REMOVED OVERWING EXIT HATCH FOUND SEAL DISLODGES, SECURED SEAL IAW AMM, . NO LEAKS NOTED, NO AUDIBLE SOUNDS.

Part: CYLINDER — LOW PRESSURE (R1 DOOR ASSIST) · airframe 26,588 hrs · 13,036 cycles

R1 DOOR PSI (PASSENGER-ASSIST CYLINDER) APPROX 1100 PSI REQ'S SERVICING. SERVICED R1 DOOR ASSIST CYLINDER W/ NITROGEN TO REQ'D LEVEL IAW AMM 52-10-00-614-001-A. LEAK CK OK AT THIS TIME.

Part: CYLINDER — LOW PRESSURE (L1 DOOR ASSIST) · airframe 26,588 hrs · 13,036 cycles

L-1 DOOR ASSIST ACTUATOR PRESSURE LOW. CORRECTIVE ACTION: REMOVED AND REPLACED L-1 DOOR CYLINDER DAMPER IAW AMM 52-11-14-000-001-B/52-11-14-400-001-B OPERATIONAL CHECK NORMAL

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,900 hrs · 12,671 cycles

ON TAKEOFF, CABIN EMERGENCY LIGHTS FLASHED. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-001-A TEST NORMAL.

Part: ACCUMULATOR — LOW PRESSURE (PAX DOOR) · airframe 25,387 hrs · 12,418 cycles

R1 DOOR ACCUMULATOR PRESSURE LOW. SERVICED R1 DOOR ACCUMULATOR PRESSURE AS REQ IAW AMM 52-10-00-614-001.

Part: ACM — FAILED (NR 1) · airframe 25,266 hrs · 12,355 cycles

AFTER LIFT OFF SMOKE DETECTED FROM ACFT DUCTS IN FLIGHT DECK. CABIN CREW ALSO DETECTED AND SAW SMOKE FROM ACFT OUTLETS. NO ECAM FAULTS OR SMOKE WARNINGS WERE TRIGGERED. AFTER SELECTING PACK 1 TO OFF SMOKE DISSIPATED IN FLIGHT DECK AND CABIN. PACK 2 REMAINED ON FOR THE ENTIRE FLIGHT. RETURNED TO LANDED AT APPROX 1340 ACCOMPLISHED OPS TEST OF PACK 1 IAW AMM 21-61-00-710-001-A PACK FAILED IN 2 MIN AIR PACK 1 OVERHEAT MESSAGE ACCOMPLISHED TROUBLESHOOTING IAW TSM 21-61-00-810-801-A FAULT MESSAGE P1 DISCHARGE.

Part: ACCUMULATOR — LOW PRESSURE (R1 DOOR) · airframe 25,266 hrs · 12,355 cycles

R1 DOOR EMERGENCY ACCUMULATOR PRESSURE IS BELOW MINIMUM. SERVICED ACCUMULATOR IAW AMM 52-10-00-614-001. NO LEAKS NOTED.

Part: CYLINDER — LOW PRESSURE (DOOR ASSIST) · airframe 25,113 hrs · 12,269 cycles

R1 ASSIST. DOOR CYLINDER LOW PRESSURE. SERVICED R1 DOOR ASSIST CYLINDER PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 24,612 hrs · 12,017 cycles

R1 DOOR ACCUMULATOR PRESSURE LOW. SERVICED R1 DOOR ACCUMULATOR PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 24,520 hrs · 11,969 cycles

R1 DOOR ASSIST ACCUMULATOR REQUIRES SERVICE. SERVICED IAW 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 24,294 hrs · 11,855 cycles

L2 OPEN ASSIST BOTTLE LOW. SERVICED DOOR ASSIST BOTTLE AT L-2 IAW AMM 52-10-00-614-001-A.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 24,294 hrs · 11,855 cycles

R1 DOOR OPEN ASSIST BOTTLE LOW. SERVICED R1 DOOR OPEN ASSIST BOTTLE IAW AMM 52-10-00-614-001-A.

Part: DOOR — LEAKING (EMERGENCY EXIT) · airframe 23,926 hrs · 11,679 cycles

ACFT LEFT OVERWING EXIT, LOUD HUMMING NOISE. R & R DOOR IAW AMM 52-62-00-040-006-A. CLEANED SEAL, INSPECTED AREA AND ADJUSTED LOWER PANEL ON SIDEWALL. NO FAULTS NOTED.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 23,858 hrs · 11,645 cycles

R-1 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED R-1 DOOR IAW 52-10-00-614-001A.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 23,517 hrs · 11,475 cycles

R1 DOOR EMER CYLINDER/ACCUMULATOR PRESSURE LOW. SERVICED WITH NITROGEN CYLINDER/ACCUMULATOR TO NORMAL RANGE IAW AMM 52-10-00-614-001. OK FOR SERVICE.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 23,039 hrs · 11,247 cycles

R2 DOOR REQUIRES SERVICE. FOUND THE AFT RT PASS/CREW DOOR EMER OPERATION CYLINDER CHARGED TO THE PROPER PRESSUERE IAW AMM 52-11-14-200-001.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 23,039 hrs · 11,247 cycles

FWD RT PAX / CREW DOOR OPERATION CYLINDER REQUIRES SERVICE. CHARGED THE FORWARD RT PASS/CREW DOOR EMER OPERATION CYLINDER TO THE PROPER PRESSURE IAW AMM 52-10-00-614-001. NO LEAKS NOTED.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 22,526 hrs · 10,971 cycles

R1 DOOR PASSENGER DOOR ASSIST CYLINDER INADEQUATE PRESSURE ON GAUGE. SERVICED R1 DOOR PASSENGER ASSIST CYLINDER W/ NITROGEN IAW AMM 52-10-00-614-001. NO LEAKS DETECTED AT THIS TIME.

Part: CYLINDER — LOW PRESSURE (R1 DOOR ASSIST) · airframe 22,339 hrs · 10,866 cycles

R1 DOOR ASSIST CYLINDER HAS LOW PRESSURE. SERVICED R1 DOOR TO PROPER AIR PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 22,168 hrs · 10,781 cycles

R1 DOOR ASSIST BOTTLE REQUIRES SERVICE. SERVICED R1 DOOR ASSIST BOTTLE AS REQUIRED IAW AMM 52-10-00-614-001.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 22,015 hrs · 10,711 cycles

R-1 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED R-1 DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 21,967 hrs · 10,690 cycles

R 1 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED THE R1 DOOR ASSIST BOTTLE TO PROPER PRESSURE. IAW AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 21,815 hrs · 10,619 cycles

PAX R1 DOOR ACCUMULATOR ASSIST BOTTLE PRESSURE LOW. SERVICED PAX R1 DOOR ACCUMLATOR ASSIST BOTTLE PRESSURE IAM AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 21,752 hrs · 10,585 cycles

R1 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED DOOR ASSIST BOTTLE AS REQUIRED IAW 52-10-000-614-001.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 21,422 hrs · 10,418 cycles

LOWER FUSELAGE, STA 7087 BETWEEN STRINGER 30LT AND STRINGER 32LT, LT E&E COMPARTMENT VACUUM WATER PIPE CLAMP SUPPORT ANGLE CRACKED. NOTE: THE SUPPORT ANGLE CRACK REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.

Part: STRAP — WORN (FAN COWL) · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 2, FAN COWL, AIR INTAKE COWL, CAPPING STRAP UPPER AREA LT AND RT CORNERS WITH WEAR. NOTE: THE CAPPING STRAP WEAR REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.

Part: PAD — WORN (FAN COWL) · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 2, FAN COWL, FWD UPPER CORNERS PADS WITH WEAR. THE CORNER-PADS WEAR REQUIRE A MAJOR REPAIR IAW SRM GUIDELINES.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 2, PLYLON PRECOOLER PANEL (423DL) SKIN VENT GRILL WITH CRACK. NOTE: THE SKIN PANEL CRACKS REQUIRE A MAJOR REPAIR IAW SRM GUIDELINES.

Part: ANCHOR FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

RIGHT WING, INNER SPAR BETWEEN RIB 2 AND RIB 2, MLG RETRACTION JACK ANCHORAGE FITTING'S BORE AND LOWER FACE WITH CORROSION. NOTE: THE FITTING'S CORROSION/REWORK REQUIRES A MAJOR REPAIR IAW ENGINEERING GUIDELINES.

Part: SKIN — CRACKED (RT WING) · airframe 21,422 hrs · 10,418 cycles

RIGHT WING, L/E AREA, BETWEEN RIB 15-STA 8268 AND RIB 16-STA 8744 SKIN (SEAL, UP STOP) WITH CRACK. MAJOR REPAIR IAW SRM.

Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 21,422 hrs · 10,418 cycles

LOWER FUSELAGE, FR28-STA 1163 BETWEEN STRINGER 38LT AND STRINGER 38RT, FWD CARGO COMPARTMENT FLOOR SUPPORT PLATE WITH CRACK. NOTE: THE PLATE CRACK REQUIRES A MAJOR REPAIR IAW ENGINEERING GUIDELINES.

Part: FITTING — CRACKED (NR 1 NACELLE) · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 1, PYLON AFT FIXED FAIRING, LOWER FWD SUPPORT FITTING WITH CRACK. MAJOR REPAIR IAW SRM.

Part: ANCHOR FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

LEFT WING, INNER SPAR BETWEEN RIB 2 AND RIB 2, MLG RETRACTION JACK ANCHORAGE FITTING'S BORE AND LOWER FACE WITH CORROSION. NOTE: THE FITTING'S CORROSION/REWORKS REQUIRES A MAJOR REPAIR IAW ENGINEERING GUIDELINES.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 21,422 hrs · 10,418 cycles

LEFT WING, RIB 17-STA 9235 OTBD FLAP UPPER SKIN, RUB STRAP CRACKED. NOTE: THE RUB STRAP CRACKED REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.

Part: FITTING — CORRODED (PAX DOOR SILL) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

LT-FWD PASSENGER DOOR, STA 808 Z-520 Y+1780, LOWER SILL BOX FITTING WITH CORROSION. MAJOR REPAIR.

Part: FITTING — CORRODED (PAX DOOR SILL) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

LT FWD PASSENGER DOOR, STA 709 Z-520 Y+1780, LOWER SILL BOX FITTING WITH CORROSION. MAJOR REPAIR.

Part: FITTING — CORRODED (PAX DOOR SILL) · airframe 21,422 hrs · 10,418 cycles

RT-FWD PASSENGER DOOR, STA 709 Z-520 Y-1780, LOWER SILL BOX FITTING WITH CORROSION. MAJOR REPAIR.

Part: FITTING — CORRODED (PAX DOOR SILL) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

RT-FWD PASSENGER DOOR, STA 808 Z-520 Y-1780, LOWER SILL BOX FITTING WITH CORROSION. MAJOR REPAIR.

Part: PANEL — WORN (THRUST REVERSER) · airframe 21,422 hrs · 10,418 cycles

ENGINE NR2, OTBD/RT THRUST REVERSE C-DUCT, PAN-DOWN PANEL WITH WEAR. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

PAX CABIN, UPPER REAR FUSELAGE BEWTEEN STA 2870 AND STA 2946, +Y1160 FLOOR SUPPORT WITH CORROSION. NOTE: THE FLOOR SUPPORT REQUIRES A MAJOR REPAIR SRM GUIDELINES.

Part: PANEL — WORN (THRUST REVERSER) · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 1, OTBD/ LT THRUST REVERSER C-DUCT, PAN-DOWN PANEL WITH WEAR. MAJOR REPAIR.

Part: PANEL — WORN (THRUST REVERSER) · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 2, INBD/LT THRUST REVERSE C-DUCT, PAN-DOWN PANEL WITH WEAR. MAJOR REPAIR.

Part: SKIN PANEL — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 2, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. MAJOR REPAIR.

Part: SKIN PANEL — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 1, PYLON AFT FIXED FAIRING, OTBD AND INBD LATERAL SKIN PANEL WITH CORROSION. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

PAX CABIN, UPPER REAR FUSELAGE AT STA 2992, +Y450 FLOOR SUPPORT WITH CORROSION. NOTE: THE FLOOR SUPPORT REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.

Part: PANEL — WORN (THRUST REVERSER) · airframe 21,422 hrs · 10,418 cycles

ENGINE NR 1, INBD/ RT THRUST REVERSE C-DUCT, PAN-DOWN PANEL WITH WEAR. MAJOR REPAIR.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

PAX CABIN, UPPER REAR FUSELAGE BEWTEEN STA 2800 AND STA 2870, +Y129 FLOOR SUPPORT WITH CORROSION. NOTE: THE FLOOR SUPPORT REQUIRES A MAJOR REPAIR SRM GUIDELINES.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,422 hrs · 10,418 cycles

PAX CABIN, UPPER REAR FUSELAGE BEWTEEN FR69 AND FR70, +Y1160 FLOOR SUPPORT WITH CORROSION. NOTE: THE FLOOR SUPPORT REQUIRES A MAJOR REPAIR IAW SRM GUIDELINES.

Part: STRIP — WORN (LT WING) · airframe 21,422 hrs · 10,418 cycles

LT WING, T/E, STA 5512 BETWEEN SPOILER NR 1 AND SPOILER NR 2 FIXED FAIRING LOWER SECTION, STRIP RUBBING WITH WEAR. MAJOR REPAIR .

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,888 hrs · 7,787 cycles

CORROSION DAMAGE TO FLOORBEAM 140 BETWEEN FR66 AND FR68. R & R FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,888 hrs · 7,787 cycles

CORROSION ON TOP SURFACE OF FLOORBEAM FR68 - FR70 Y62.5. R & R FLOORBEAM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,888 hrs · 7,787 cycles

CORROSION DAMAGE ON TOP SURFACE OF FLOORBEAM 170 BETWEEN FR66 AND FR68. REMOVED AND REPLACED FLOORBEAM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,404 hrs · 4,668 cycles

RT FLOORBEAM - Y1292 FRAME 68-69 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,404 hrs · 4,668 cycles

MINOR CORROSION ON FLOOR SUPPORT Y254, FRAME 67-68. REMOVED AND REPLACED FLOOR SUPPORT. (K)

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 9,404 hrs · 4,668 cycles

CORNER SHEAR WEB CORRODED - Y1732 FRAME 69-70. REMOVED AND REPLACED SHEAR WEB. (K)

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE)

FLOOR SUPPORT Y254, FRAME 68-70 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT. (K)

Part: HOOK — DIRTY (L1 DOOR) · airframe 5,583 hrs · 2,819 cycles

L1 DOOR WILL NOT LOCK OPEN. REMOVED DOOR STAY MECHANISM , CLEANED DEBRIS FROM MECHANISM, REINSTALLED STAY MECHANISM.