N806NW

Part: WIRE — DAMAGED (ZONE 200) · airframe 96,703 hrs · 12,687 cycles

EMERGENCY PATH LIGHTS AT 39ABC AND 40ABC INOP. REPAIRED WIRING PER A330 AMM 33-51. OK FOR SERVICE. (8508926)

Part: SEAL — FOD (ZONE 800) · airframe 96,382 hrs · 12,647 cycles

R4 DOOR SHOWING OPENED WHEN CLOSED. CLEARED DEBRIS FROM DOOR SEAL. CYCLED 4R DOOR OPEN & CLOSED SEVERAL TIMES. OPS CKS GOOD PER A330 AMM 52-13. (7205782)

Part: SIGN — DETACHED (ZONE 200) · airframe 96,252 hrs · 12,627 cycles

EMERGENCY EXIT SIGN FELL OFF. REPLACED MISSING LENS AT LOC 603. REF A330 AMM 33-51. OPS CKS GOOD. (LP 1323310)

Part: WIRE — DAMAGED (ZONE 200) · airframe 96,213 hrs · 12,622 cycles

30 JH FLOOR WHITE EMER LIGHT INOPERATIVE. REPAIRED WIRING PER A330 AMM 33-51. OK FOR SERVICE. (7205694)

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 95,519 hrs · 12,529 cycles

SEAT 58 AB EMER LIGHT INOP. REPLACED LAMP ASSY PER A330 AMM 33-52. OK FOR SERVICE. (6685002)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 95,519 hrs · 12,529 cycles

3R & 4R LAV RED EMER FLOOR LTS INOP. REPLACED EMER LIGHTS ON LAVS AT DOOR 3R & 4R PER A330 AMM 33-51. OK FOR SERVICE. (6685001)

Part: SKIN — DENTED (ZONE 500 SLAT) · airframe 91,408 hrs · 12,007 cycles

AIRCRAFT 3306, DENT AT LH WING #4 SLAT, PERFORM PERMANENT REPAIR AS PER ERA 620607-14. CORRECTIVE ACTION: TEMPORARY REPAIR REMOVED AND APPLY PERMENANT DOUBLER REPAIR AS PER PRI 620607-14 REV.0. COMPLIED AND COMPARED WITH ERA 620607-14 REV.A SECTION III. (LP 0693870)

Part: FASTENER — ELONGATED (LH ENG) · airframe 91,408 hrs · 12,007 cycles

SHIP 3306 LH ENG LAPF IB FASTENER HOLE ELONGATED. CORRECTIVE ACTION: REMOVED OLD DOUBLER AND REAMED THE WORN HOLE, APPLIED FREEZE PLUG AND DOUBLER REPAIR WITH MATERIAL: 2024-0-0.071" AS PER PRI 622696-14 REV.0. (0690405)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 90,431 hrs · 11,880 cycles

SHIP 3306 SEAT 42 AB EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REPLACED 42AB EMERGENCY FLOOR LIGHT ASSY. OK FOR SERVICE. (5123117)

Part: GIRT BAR — FOD (ZONE 200) · airframe 90,072 hrs · 11,836 cycles

SHIP 3306 DOOR 4R WOULD NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR PER A330 AMM 52-12. OK FOR SERVICE. (5631162)

Part: ENGINE — MAKING METAL (NR 1) · airframe 89,908 hrs · 11,816 cycles

SHIP 3306 -ATO- DISCONTINUED TAKEOFF AT 120 KNOTS DUE TO LEFT ENGINE FAILED. REPORTS OF FIRE INSIDE THE ENGINE. LEFT ENGINE FIRE BOTTLES DISCHARGED, NO COCKPIT FIRE INDICATION. CORRECTIVE ACTION: FOUND METAL IN THE 2.5 BLEED PORTS. REPLACED FIRE BOTTLES, INSPECTED PYLON, AND REPLACED #1 ENGINE PER DELTA WORK CARD 7100-9901-01. OK FOR SERVICE. (6076178)

Part: ENGINE — FAILED (LEFT) · airframe 89,900 hrs · 11,815 cycles

SHIP 3306 -ATO- DISCONTINUED TAKEOFF AT 120 KNOTS DUE TO LEFT ENGINE FAILED. REPORTS OF FIRE INSIDE THE ENGINE. LEFT ENGINE FIRE BOTTLES DISCHARGED, NO COCKPIT FIRE INDICATION. CORRECTIVE ACTION: FOUND METAL IN THE 2.5 BLEED PORTS. MAINTENANCE CURRENTLY IN PROGRESS REPLACING #1 ENGINE. (6076178)

Part: GIRT BAR — OBSTRUCTED (L4 DOOR) · airframe 89,781 hrs · 11,800 cycles

SHIP 3306 4L DOOR WILL NOT ARM. CORRECTIVE ACTION: CLEANED DEBRIS FROM DOOR, DOOR TRACK, AND GIRT BAR PER A330 AMM 52-12. OPS CHECK GOOD.

Part: LATCH — FAILED (LAV O2 MODULE) · airframe 88,921 hrs · 11,695 cycles

SHIP 3306 LT AFT LAV INOP DUE TO OXYGEN MODULE LATCH LOCATION "207". CORRECTIVE ACTION: R/R O2 MODULE PER A330 AMM 35-23. OK FOR SERVICE. (5616523)

Part: CANISTER — INOPERATIVE (LAV O2 MODULE) · airframe 88,921 hrs · 11,695 cycles

SHIP 3306 LAV OXYGEN MODULE LAV 207 AFT LEFT INOP. CORRECTIVE ACTION: REPLACED O2 CANISTER PER A330 AMM 35-23. OPS AND LEAK TEST GOOD. (5616522)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,292 hrs · 11,603 cycles

SHIP 3306 SEAT MOUNTED EMERGENCY ESCAPE PATH MARKING LIGHTS AT 38B 46B 54B ADN 55B INOP. CORRECTIVE ACTION: R/R EPL ASSY PER A330 AMM 33-51. (5831552)

Part: DOOR — FOD (L3) · airframe 87,745 hrs · 11,528 cycles

SHIP 3306 DOOR 3L VERY DIFFICULT TO DISARM. CORRECTIVE ACTION: CLEANED DEBRIS AND OPERATED 3L DOOR. ALL CHECKS GOOD. (5483558)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,141 hrs · 11,455 cycles

SHIP 3306 F/A'S REPORTED FUMES ON DESCENT INTO DTW. CORRECTIVE ACTION: WCONFIRMED FUMES COMING FROM APU DUE TO HYDRAULIC FLUID RUNNING BACK TO APU. CLEANED A/C EXTERIOR BELLY. PERFORMED LEVEL A ECS PACK BURN OUT DECONTAMINATION PROCEDURE. REPLACED FWD/AFT CARGO RECER FILTERS. RAN ENGINES ON ENGINE BLEED ONLY NO SMELL DETECTED. AFTER ENGINE SHUTDOWN ON APU BLEED NOTICED SMELL. WHILE ISOLATING PACKS WORKED WITH APU BLEED ONLY OIL SMELL IN CABIN & COCKPIT IS GONE. REPLACED ALL RECIRE FILTERS. RAN BOTH ENGS ON ENG BLEEDS ONLY NO NOTICEABLE ODOR IN COCKPIT OR CABIN. (4349671)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,137 hrs · 11,453 cycles

SHIP 3306 -ATB/HYD- DUE TO LEAK OF GREEN HYDRAULIC FLUID WITH ASSOCIATED ECAM MESSAGES. CORRECTIVE ACTION: REPLACED BLOWN SEAL ON BRAKE MANIFOLD ASSEMBLY AND RE-SECURED LOOSE RETURN LINE. (4349664)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,904 hrs · 11,424 cycles

SHIP 3306 LOCATION 605 SIGN ON FULL BRIGHT ENTIRE FLIGHT WHEN SHOULD BE ON ONLY WHEN GEAR DOWN. CORRECTIVE ACTION: COMPLETED OPERATIONAL TEST OF EMERGENCY LIGHTING SYS. ALL LIGHTS OPS CHK GOOD. (0064439)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,904 hrs · 11,424 cycles

SHIP 3306 LOCATIONS 603 EXIT SIGN ON ENTIRE FLIGHT. CORRECTIVE ACTION: COMPLETED OPERATIONAL TEST OF EMERGENCY LIGHTING SYS. ALL LIGHTS OPS CHK GOOD. (0064441)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,452 hrs · 11,369 cycles

SHIP 3306 4R IDICATING DOOR OPEN. CORRECTIVE ACTION: CYCLED DOOR INDICATION GOOD. (4618464)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,841 hrs · 11,294 cycles

SHIP 3306 DURING PDC WALK AROUND- #1 ENGINE LAPF FOUND MISSING FILLER PANEL ON OUTBOARD SIDE. CORRECTIVE ACTION: REMOVED, FABRICATED AND REPLACED STRIP PER A330 SRM 51-44 AND 51-31. (4405912)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,305 hrs · 11,230 cycles

SHIP 3306 OVEN SMOKING AT LOCATION 404. CORRECTIVE ACTION: R&R OVEN AT LOC 404. (2880270)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,172 hrs · 11,214 cycles

SHIP 3306 4R DOOR SHOWED OPEN AFTER SLIDE ARMED. CORRECTIVE ACTION: DOOR 4 RT OPEN AND CLOSED OK. OPS TEST PERFORMED. NO FAULT CONFIRMED. TEST OK. (4866834)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,203 hrs · 11,218 cycles

SHIP 3306 SEAT 34BA, 38BA, 40BA, 58BA, 34JH WHITE EMER FLOOR PATH LIGHTS INOP. CORRECTIVE ACTION: FOUND 34AB, 34JH, 58BA UNPLUGGED AT WALL. PLUGGED CONNECTOR BACK IN. REF A330 AMM 33-51. FOUND 38BA, 40 BA PINS IN PLUGS DAMAGED. RETERMINATED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,897 hrs · 11,179 cycles

SHIP 3306 - ATB - DURING CLIMBOUT, EXPERIENCED HYDRAULIC GREEN RESERVOIR OVERHEAT ON ECAM. COMPLIED WITH QRH PROCEDURE HOWEVER PRESSURE AT 3000PSI AFT GREEN PUMPS TURNED OFF. AFTER 40 MINUTES GREEN HYDRAULIC PRESSURE DECREASED TO ZERO. RETURNED TO ATB. CORRECTIVE ACTION: REPLACED #2 ENGINE DRIVEN PUMP, GREEN SYSTEM CASE AND FILTER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,742 hrs · 11,157 cycles

SHIP 3306 AFTER PARKING AT GATE, THE PARKING BRAKE HANDLE WAS MOVED TO THE ON POSITION. PARKING BRAKE WOULD NOT SET. BRAKES HELD MANUALLY UNTIL AIRCRAFT CHOKED. CORRECTIVE ACTION: TESTED BOTH BSCU. NO FAULTS. BOTH TEST GOOD. PARKING BRAKE CYCLED SEVERAL TIMES CKS GOOD. (4940600)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,059 hrs · 11,071 cycles

SHIP 3306 ACFT CONDITIONED AIR HAS MUSTY DIRTY SOCK SMELL IN COCKPIT AND CABIN ON GROUND AND IN FLIGHT. CORECTIVE ACTION: T/S. A VISUAL INSPECT OF ENG 1 AND 2 INLET FOR OIL, NONE FOUND. INSOECTED APU BLEED DUCT FOR OIL, NONE FOUND. ACCOMPLISHED DECONTAMINATION OF APU BLEED AIR SYSTEM. COMPLETE LEVEL A DECONTAMINATION OF ECS WITH ENG'S. ODOR STILL PRESENT. FOUND EVIDENCE OF OIL COMING OUT OF APU DRAIN FOUND LUBE PUMP LEAKING, FOUND EVIDENCE OIL IN APU AIR SUPPLY LINE. R/R APU OIL PUMP. OPS CHECK GOOD NO LEAKS NOTED. REPLACED FWD CARGO RECIRCULATION FILTER. AFT CARGO RECIRCFILTER REPLACED. COMPLETED LEVEL A DECONTAMINATION OF ECS. COMPLETED DECONTAMINATION OF ECS. RAN APU AND ENGINES. NO ODOR PRESENT. (4627284)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,885 hrs · 11,051 cycles

SHIP 3306 DAMAGE ON JOINT ASSY PANEL P/N F55182525001A02. CORRECTIVE ACTION: REMOVED DAMAGE. PERFORMED ULTRASONIC INSPECTION ON ALL AFFECTED AREAS, BOTH SIDES, NO DELAMINATION FOUND. INSTALLED PERMANENT REPAIR PER PRI 607707-14. C/W ERA 607707-14. (2707324)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,785 hrs · 11,038 cycles

SHIP 3306 EMER FLOOR LIGHT UNDER SEAT 40 J/H INOP. CORRECTIVE ACTION: R&R FLOOR LIGHT. NO HELP. FOUND WALL CONNECTOR LOOSE. RE-SECURED CONNECTOR. (9526932)

Part: NONE — NONE · airframe 83,508 hrs · 11,005 cycles

SHIP 3306 DURING SAFA INSPECTION FOUND OVERHEAD EMERGENCY LIGHTING DOOR 1 LH DOESN T WORK PROPERLY. CORRECTIVE ACTION: CIDS RESET AND EMERGENCY OPS TEST OK. (4126505)

Part: NONE — NONE · airframe 83,250 hrs · 10,971 cycles

SHIP 3306 EEPLS @ 4L RED/WHITE DAMAGED. CORRECTIVE ACTION: R&R 4L LAV RED & WHITE LIGHT ASSY. (4088900)

Part: NONE — NONE · airframe 83,242 hrs · 10,970 cycles

SHIP 3306 FO FIXED WINDOW HAS A BLACK MARK ON THE BOTTOM LEFT - DISCOLORATION. CORRECTIVE ACTION: INSPECTED WINDOW AND FOUND DISCOLORATION TO BE A BURNT SPOT ON THE BUS BAR. SIZE OF BURNT SPOT (1" X 0.5") IS WITHIN LIMITS. R/R FO FIXED WINDOW REF A330 AMM 56-11 IN ATL. (4051135)

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LGIHTS) · airframe 83,040 hrs · 10,947 cycles

R2 DOOR FWD RED EMERGENCY ESCAPE LIGHT INOPERATIVE. LOCATED FWD OF FLT ATTND. SEAT ON BULKHEAD. FOUND WIRE HARNESS 9101WL19 DISCONNECTED. RECONNECTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 82,965 hrs · 10,938 cycles

ON FINAL DECENT, LIGHT ACRID ODOR AFTER BLOCK-IN. STATUS MSG SMOKE, CAB TEMP & EPGS. CHECKED OVERHEAD LIGHTS & BALLASTS, PASSENGER READING LIGHTS & PSU LIGHTS, IFE EQUIPMENT & POWER OUTLETS, GALLEY OVENS & COFFEEMAKERS, WIRING VISIBLE IN THE AREA REPORTED. NO DISCREPENCIES NOTED. RAN BOTH ENGINES WITH PACKS RUNNING CABIN FANS ON & OFF, NO SMOKE OR ODOR. ALSO CHECKED E/E COMPARTMENT, NTF. SMOKE, CAB TEMP, EPGS, CLASS II MESSAGES, UNRELATED, REVIEWED OIL CONSUMPTION TRENDS, NORMAL. NO FAULTS NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 82,806 hrs · 10,919 cycles

SHIP 3306 DURING DESCENT A NOTICABLE SMELL SIMILAR TO HOT AIR CONDITIONING PACKS COULD BE SMELLED IN THE FLIGHT DECK. ALL PACK TEMPERCRES , BLEED TEMPS AND AIR COND ZONE TEMPS WERE NORMAL. SMELL WAS SIMILAR TO HOT OIL AND INTENSITY WAS LIGHT. SMELL WAS NOT NOTICABLE IN CABIN. CORRECTIVE ACTION: DETERMINED CAUSE OF FUMES #2 ENGINE PER TABLE IN A330 TSM 05-50. FOUND NO EVIDENCE OF OIL IN BLEED AIR DUCTS. COMPLETED LEVEL A DECONTAMINATION. NO SMELLS NOTED. REPLACED RECIRC FILTERS. ACCOMPLISHED HIGH POWER RUN IN ADDITION TO AMM PROCEDURES. NO SMELLS NOTED. (8170226)

Part: SUPPORT BRACKET — BROKEN · airframe 82,767 hrs · 10,913 cycles

BROKEN SWITCH PRESSURE SUPPORT BRACKET (40MJ) IN FWD AVIONIC COMPARTMENT. REMOVED AND REPLACED PRESSURE SWITCH 40MJ IAW AMM 52-71. PERFORMED LEAK TEST OF THE PRESSURE LINE AND PERFORMED OPERATIONAL TEST OF THE CABIN PRESSURE SWITCH. ALL TESTS ARE GOOD. NO FOUND LEAK.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 82,767 hrs · 10,913 cycles

POWER SUPPLY DID NOT PASS TEST, 14WL, DOOR 2R, DURING EPSU TEST PUSH BUTTON, LIGHT UNIT FAULT IS ON. REMOVED AND REPLACED EPSU 14WL DOOR 2R, PERFORMED ELECTRICAL BONDING TEST. (2554549)

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 82,767 hrs · 10,913 cycles

EPSU 16WL DID NOT PASS TEST. DOOR 3R DURING EPSU TEST PUSHBUTTON, LIGHT UNIT FAULT IS ON. REMOVED AND REPLACED EPSU 16WL DOOR 3R, PERFORMED ELECTRICALBONDING TEST.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 82,767 hrs · 10,913 cycles

POWER SUPPLY DID NOT PASS TEST 15WL, DOOR 3L DURING EPSU TEST PUSH BUTTON, LIGHT UNIT FAULT IS ON. REMOVED AND REPLACED EPSU 15WL DOOR 3L. PERFORMED ELECTRICAL BONDING TEST.

Part: FRAME — CRACKED (FRM 40) · airframe 82,767 hrs · 10,913 cycles

CRACK FRAME 40 LH SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE 260, CRACK DIRECTION IS 6 OCLOCK. COMPLIED WITH PRI 604048-14AD. VALIDATED ER/A 604048-14AD MATCHES PRI 604048-14AD. PERFORMED REPAIR INSTRUCTIONS ON FRAME 40 LH SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE 260 AS PER ER/A 604048-14AD.

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FLOOR BEAM WEB AROUND TH E COLLAR OF THE REINFORCEMENT STRAP ATTACHMENT FASTENERS BTW FR 75 TO FR79 IN PASSENGER CABIN. COMPLIED WITH PRI 603703-14, VALIDATED ER/A #603703-14 MATCHES PRI 603703-14. EXISTING ALTERATION INSTALLED PER 5320-01135. INSTALLATION IS APPROVED BY STC ST02455LA. STC IS APPROVED FOR DAMAGE TOLERANCE IN ACCORDANCE WITH FAR25.47 AND 25.571.

Part: WEB — CRACKED (FRM 40) · airframe 82,767 hrs · 10,913 cycles

CRACK FRAME 40 RH SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE 260, CRACK DIRECTION IS 9 OCLOCK. COMPLIED WITH PRI 604048-14AD. VALIDATED ER/A 604048 -14ADMATCHES PRI 604048-14AD. PERFORMED REPAIR INSTRUCTIONS ON FRAME 40 RH SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE 260 AS PER ER/A 604048-14AD.

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SLAT 5. COMPLIED WITH PRI 603703-14, VALIDATED ER/A #603703-14 MATCHES PRI 603703-14. EXISTING REPAIR INSTALLED PER A330 SRM 57-40-00-300-008 APPROVED AS A CAT A.

Part: PLATE — CRACKED (GIRT BAR) · airframe 82,767 hrs · 10,913 cycles

CRACK GIRT BAR PLATE LOCATED FRAME 73A RH SIDE IN. INSTALLED NEW GIRT BAR PLATE AND GIRT BAR LOCATED FRAME 73A RH SIDE IN PASSENGER CABIN.

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR R4 E XTERNAL SKIN AFT LOWER CORNER IN PASSENGER CABIN. COMPLIED WITH PRI 603703-14 REV. 0, VALIDATED ER/A #603703-14 REV. ORIGINAL MATCHES PRI 603703-14 REV. 0. EXISTING REPAIR INSTALLED PER ER/A 594953-14 AND SRM 52-13-00-300-013 AS PER A330 SRM 52-13-00-300-013.

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK LOCATED RIB 6 AFT ON LH WING COMPLIED WITH PRI 603703-14, VALIDATED ER/A #603703-14 MATCHES PRI 603703-14. EXISTING REPAIR INSTALLED PER EM 5720-01066-03A AND AIRBUS REPAIR DRAWING R57257026. REPAIR IS APPROVED PER AIRBUS REPAIR DRAWING R57257026 ACCORDING TO FAA AD 2006-22-14, PARA. (K) GUIDELINES. EM 5720-01066-06A. (2552300)

Part: FLOOR SUPPORT — CORRODED (FRMS 72-74) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

CORROSION FLOOR BEAM -Y450 BETWEEN FR72 TO FR74 IN PASSENGER CABIN. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM -Y450 BETWEEN FR72 TO FR75 IN PASSENGER CABIN.

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED AT FR94, STR3L TO STR4L ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 603703-14, VALIDATED ER/A# 603703-14 MATCHES PRI 603703-14. EXISTING REPAIR INSTALLED PER NWA EA 33-207461. (2549659)

Part: SKIN — DEFORMED (FRM 66 S41-42R) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 ERA 585481-14 AFT CARGO ON ARRIVAL NOTED DENT BETWEEN AFT AND BULK CARGO DOOR. LOC. EXTERNAL SKIN FR66 AND STR41R TO STR42R DENT AND DEFORMATION. CORRECTIVE ACTION: COMPLIED WITH PRI 585481-14, VALIDATED ER/A 585481-14, MATCHES PRI 585481-14. ACCOMPLISHED PERMANENT REPAIR ON EXTERNAL FUSELAGE SKIN LOCATED AT FR 66 BETWEEN STR41R AND STR42R AT LOWER FUSELAGE AS PER ER/A 585481-14. (2549999)

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK LOCATED RIB6 A FT ON RH WING. CORRECTIVE ACTION: COMPLIED WITH PRI 603703-14 REV 0, VALIDATED ER/A 603703-14 REV. ORIGINAL MATCHES PRI 603703-14 REV. 0. EXISTING REPAIR INSTALLED PER EM 5720-01066-03B AND AIRBUS REPAIR DRAWING. REPAIR IS APPROVED PER AIRBUS REPAIR DRAWING ACCORDING TO FAA AD. (2550045)

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR L4 E XTERNAL SKIN AFT LOWER CORNER IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH PRI 603703-14, VALIDATED ER/A# 603703-14 MATCHES PRI 603703-14. EXISTING REPAIR WAS REMOVED SINCE IT WAS FOUND DAMAGED AND DISCREPANT. INSPECTIONS WERE EXECUTED WITH NIL FINDING AND A NEW REPAIR WAS INSTALLED AS PER A330 SRM 52-13-00-300-013 WITHOUT DESVIATIONS. AS PER A330 SRM 52-13-00-300-013, REPAIR IS CONSIDERED AS CATEGORY B WITHSUPLEMENTAL INSPECTIONS REQUIRED AS PER A330 SRM 52-13-00-205-013. (2549637)

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR EXTERNAL FWD LOWER CORNER IN BULK CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 603703-14, VALIDATED ER/A# 603703-14 MATCHES PRI 603703-14. EXISTING REPAIR INSTALLED PER ER/A 519806-14. (2550015)

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 14R AT FR53.8 I N PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH PRI 603703-14, VALIDATED ER/A #603703-14 MATCHES PRI 603703-14. EXISTING REPAIR INSTALLED PER ER/A 582356-14. (2550049)

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN AND STRING ER FROM FR67 TO FR68, STR47R TO STR52R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 603703-14, VALIDATED ER/A# 603703-14 MATCHES PRI 603703-14. EXISTING REPAIR INSTALLED PER ER/A 581387-14. (2549652)

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 29 TO FR30 BTW STR26L TO STR27L AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 603703-14, VALIDATED ER/A# 603703-14 MATCHES PRI 603703-14. EXISTING REPAIR INSTALLED PER A330 SRM 53-21-11-300-015. (2549669)

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN AT FR60A B TW STR46R TO STR47R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 603703-14, VALIDATED ER/A# 603703-14 MATCHES PRI 603703-14. EXISTING REPAIR INSTALLED PER ER/A 529525-14 AND A330 SRM 53-41-11-300-016. AS PER A330 SRM 53-41-11-300-016, SUPPLEMENTAL INSPECTIONSPER A330 SRI 53-41-11-205-028. (2549665)

Part: SKIN — NOT REPORTED (FRM 66 S39-42R) · airframe 82,767 hrs · 10,913 cycles

PERMANENT REPAIR WAS ACCOMPLISHED PER SECT III O F ER/A 585481-14, REV C AT FR 66, STR 39R TO STR 42R. PERMANENT REPAIR WAS ACCOMPLISHED PER SECT III O F ER/A 585481-14, REV C AT FR66, STR 39R TO STR 42R. CORRECTIVE ACTION: DTE TRACKING - THE REPAIR PER SECT III OF ERA 585481-14, REV C I S APPROVED FOR 6 MONTHS FROM 16DEC22. OBTAIN STAGE 2 AND 3 DAMAG E TOLERANCE APPROVAL OF THE SECT III REPAIR BY 16JUN23. ON 13JUN23, STAGE 2 AND 3 DTE HAS BEEN COMPLETED. (2548156)

Part: CROSSBEAM — CRACKED (FRM 74 S26R) · airframe 82,767 hrs · 10,913 cycles

CRACKED CROSSBEAM, FRAME 74, STRINGER 26R. COMPLIED WITH PRI 603922-14 REV 0 REV 1. VALIDATED ER/A 603922-14 MATCHES PRI 603922-14. PERFORMED REPAIR INSTRUCTIONS ON CROSS BEAM -YB FRAME 74 AT LEVEL OF STRINGER 26R IN PASSENGER CABIN IAW ERA 603922-14.

Part: STRUCTURE — CRACKED (NOT REPORTED) · airframe 82,767 hrs · 10,913 cycles

DURING AN H CHECK, AND DURING ACCOMPLISHMENT OF EM 5716-01017, HOLE 260LH AND 260RH WERE FOUND CRACKED. THE HOLES WERE REPAIRED P ER SECT I AND SECT II ER/A 604048-14.

Part: CROSSBEAM — CRACKED (FRM 74 S26L) · airframe 82,767 hrs · 10,913 cycles

CRACKED CROSSBEAM, FRAME 74, STRINGER 26L. PERFORMED REPAIR INSTRUCTIONS ON CROSS BEAM YB FRAME 74 AT LEVEL OF STRINGER 26L IN PASSENGER CABIN ASPER ERA 603922-14.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,546 hrs · 11,382 cycles

SHIP 3306 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR L4 EXTERNAL SKIN AFT LOWER CORNER IN PASSENGER CABIN. CORRECTIVE ACTION: ACCOMPLISHED GENERAL VISUAL INSPECTION ON AREA OF INSTALLED REPAIR AND NOT FOUND DAMAGE. ACCOMPLISHED DETAILED VISUAL INSPECTION ON REPAIR AREA AND FOUND THAT REPAIR MATCHES AND MEET ALL REQUIREMENTS AS PER A330 SRM 52-13-00-300-013. (2540180)

Part: STRINGER — CRACKED (FRM 79-80 S26L) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CRACK STRINGER 26L BTW FRAME 79 AND FRAME 80 AT AFT GALLEY AREA. CORRECTIVE ACTION: REMOVED AND REPLACED STRINGER COUPLING LOCATED ON STRINGER 26 L BTW FRAME 79 AND FRAME 80 AS PER A330 SRM 51-42-11-801. (2536223)

Part: STRINGER — CRACKED (FRMS 79-80 S26R) · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CRACK STRINGER 26R BTW FRAME 79 AND FRAME 80 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED STRINGER COUPLING LOCATED ON STRINGER 26R BTW FRAME 79 AND FRAME 80 AS PER A330 SRM 51-72-11-911-001. (2536225)

Part: FLOOR SUPPORT — CORRODED (FRMS 67-69) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CORROSION FLOOR STRUCTURE BEAM LOCATED LH SIDE FR67 TO FR69 AT LEVEL FLOOR STRUCTURE IN BULK CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE BEAM LOCATED LH SIDE FR67 TO FR69 AT LEVEL FLOOR STRUCTURE IN BULK CARGO COMPARTMENT AS PER A330 SRM 51-72-11-911-001. (2533484)

Part: NONE — NONE (NONE) · airframe 82,767 hrs · 10,913 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN AT FR60A BTW STR46R TO STR47R AT LOWER FUSELAGE. ACCOMPLISHED DETAILED VISUAL INSPECTION ON REPAIR DOUBLER LOC. ON FUSELAGE SKIN AT FR60A AND BTW. STR46R TO STR47R AND NOT FOUND SIGN OF DAMAGE, CORROSION, PULLED FASTENERS OR DENTS AS PER NTM 51-90-00 AND ER/A# 603703-14. (ITEM 14) AND ACCOMPLISHED GENERAL VISUAL INSPECTION OF THE INSTALLED REPAIR AND ENSURED THE REPAIR FOUND ON THE AIRCRAFT MATCHES THE DESCRIPTION IN THE COMMENTS SECTION FOR THIS ITEM AND MEET ALL REQUIREMENTS AS PER A330 SRM 53-41-11-300-016 AND ERA#529525-14. (2533465)

Part: FLOOR SUPPORT — CORRODED (FRMS 33-37) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CORROSION FLOOR BEAM Y1456 BETWEEN FR33 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: EVALUATED REWORKED AREAS ON FLOOR BEAM Y1456 LOC BTW FR33 TO FR37 IN PASSENGER CABIN AND FOUND WITHIN LIMITS AS PER A330 SRM53-00-15-283-002. (2531656)

Part: SEAT TRACK — CORRODED (FRM 73-74) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

CORROSION SEAT TRACK LOCATED BTW FRAME 73 AND FRAME 74 LH SIDE IN PAS SENGER CABIN. REPLACED SEAT TRACK YB1 LOC. BTW FRAME 73 AND FRAME 74 LH SIDE IN PASSENGER CABIN.

Part: SEAT TRACK — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CORROSION SEAT TRACK LOCATED BTW FRAME 73 AND FRAME 74 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM YB LOCATED BTW FRAME 73 AND FRAME 74 LH SIDE IN PASSENGER CABIN AS PER A330 SRM 51-72-11. (2527710)

Part: SEAT TRACK — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

CORROSION SEAT TRACK BTW FRAME 73 AND FRAME 74 LH SIDE IN PASSENGER CABIN. REPLACED SEAT TRACK YC1 BTW FRAME 73 AND FRAME 74 LH SIDE IN PASSENGER CABIN IAW SRM 51-42-11 AND APPLIED CORROSION PREVENTION COMPOUND IAW SRM 51-22-00-801.

Part: SEAT TRACK — CORRODED (FRMS 71-75) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

CORROSION SEAT TRACK Y450 BTW FRAME 71 AND FRAME 75 IN PASSENGER CABIN. REPLACED SEAT TRACK Y450 LOC. BTW FRAME 71 AND FRAME 75 IN PASSENGER CABIN ASPER A330 SRM 51-42-11 AND APPLIED CORROSION PREVENTION COMPOUND. (2518668)

Part: SEAT TRACK — CORRODED (FRM 73A) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

CORROSION ON THE SEAT TRACK -Y2462. PERFORMED DVI ON THE SEAT TRACK AT FRAME 73A, NO DAMAGE FOUND. CORROSION WAS FOUND ON THE SEAT TRACK. REPLACED THE SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRMS 33-36) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

SHIP 3306 CORROSION FLOOR SUPPORT Y2462 BETWEEN FRAMES 33 AND 36. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-801.

Part: SEAT TRACK — CORRODED (FRM 73A) · corrosion level 2 · airframe 82,767 hrs · 10,913 cycles

CORROSION FOUND ON SEAT TRACK Y2462, FRAME 73A. PERFORMED DVI ON THE SEAT TRACK, NO DAMAGE. CORROSION WAS FOUND ONTHE SEAT TRACK YA. REPLACED THE SEAT TRACK YA IAW SRM 51-42-11. (2517231)

Part: NONE — NONE · airframe 82,729 hrs · 10,908 cycles

SHIP 3306 DOOR 2L HARD TO ARM. CORRECTIVE ACTION: OPENED DOOR FOUND VELCRO LOOSE ON GIRT BAR SECURED VELCRO. (9443956)

Part: NONE — NONE · airframe 82,578 hrs · 10,888 cycles

SHIP 3306 -ATB- AFTER TAKEOFF AIRCRAFT SHUTTERED WITH LEFT ENGINE STALL MESSAGE, ALL ENGINE PARAMETERS NORMAL. QRH NOTE SAYS NOT TO INITIATE OVER WATER CROSSING, AIRCRAFT RETURNED TO SEA. CORRECTIVE ACTION: SEA MAINTENANCE TROUBLESHOT LEFT ENGINE STALL MESSAGE PRE A330 TSM. COMPLETED BOROSCOPE INSP. NO DEFECTS NOTED. INSTALLED NEW EEC AND FMU. TESTED AT HIGH POWER. (9390177)

Part: NONE — NONE · airframe 82,471 hrs · 10,874 cycles

SHIP 3306 DURING IDLE POWER DECESNT, STALE ODOR COMING FROM AIR CONDITIONING. CORRECTIVE ACTION: RUN APU WITH BLEED VALVE OPEN NO ODOR. RUN BOTH ENG ISOLATED APU AND ENG BLEED NO SMELL NOTED ON EITHER ENG. R/R FWD AFT REC FILTER PER A330 A,, 21-21. FOUND FWD FILTER DIRTY. CK PFR NO MSG FOUND. R/R BOTH LEFT AND RIGHT OZONE COVERTER PER A330 AMM 21-51. RUN APU AND ENG ISOLATED EACH SYSTEM. NO SMELL NOTED. INSPECTED APU FOR ANY SIGN OF OIL NOTHING NOTED. (9390115)

Part: NONE — NONE · airframe 82,479 hrs · 10,875 cycles

SHIP 3306 3R DOOR BOTTLE LOW (YELLOW BAND). CORRECTIVE ACTION: SERVICED BOTTLE PER A330 AMM 52-22. (9618680)

Part: NONE — NONE · airframe 81,660 hrs · 10,772 cycles

SHIP 3306 FAP DOOR PAGE WARNING: DOOR 3RH PRESSURE CHK. CORRECTIVE ACTION: PAX/CREW EMERG DOOR LOC#3RH ACTUATOR CYLINDER PRESSURE CHK AND ADJUSTMENT PFMD IAW A330 AMM 52-10. (8020391)

Part: LIGHT — INOPERATIVE · airframe 80,634 hrs · 10,646 cycles

SHIP 3306 FOUND SEAT 31JH EMERGENCY LIGHT INOP. CORRECTIVE ACTION: RECONNECTED SEAT 31JH HARNESS 9104WL15 TO SEAT IAW A330 AWM 33-51-23. (9264410)

Part: NONE — NONE · airframe 80,469 hrs · 10,626 cycles

SHIP 3306 EMERGENCY LIGHTS AT ROW 34 DO NOT ILLUMINATE DURING TEST OF EMERGENCY LIGHTS. CORRECTIVE ACTION: FOUND BROKEN WIRES AT SEAT ROW 34. REPINNED WIRES. (8678529)

Part: UNKNOWN — UNKNOWN · airframe 79,724 hrs · 10,522 cycles

SHIP 3306 DURING SVC CK SEATS 38JH, 36JH EMER LIGHT INOP. CORRECTIVE ACTION: FOUND CONNECTORS DISCONNECTED. RECONNECTED. (8519783)

Part: NONE — NONE · airframe 79,351 hrs · 10,469 cycles

SHIP 3306 ENTRY DOOR HARD TO OPERATE. CORRECTIVE ACTION: CLEANED GIRT BAR FITTINGS. (8770313)

Part: NONE — NONE · airframe 79,099 hrs · 10,428 cycles

SHIP 3306 -ATB- DUE TO ECAM MESSAGE ENG 2 AIR BLEED LEAK. CORRECTIVE ACTION: LEAK CHECKED. FOUND NO LEAKS. REPLACED NO. 2 BMC & PYLON OVERHEAT SENSING ELEMENT. TESTED OK. (8560508)

Part: NONE — NONE · airframe 78,861 hrs · 10,392 cycles

SHIP 3306 EXIT SIGN 2 RIGHT BROKEN. CORRECTIVE ACTION: EXIT SIGN COVER RESECURED. (8209312)

Part: NONE — NONE · airframe 78,873 hrs · 10,394 cycles

SHIP 3306 ELEVATOR SCHEDULED FOR MOISTURE INGRESS INSPECTION. AD RELATED. CORRECTIVE ACTION: ACCOMPLISHED THERMOGRAPHIC SKIN PANEL INSPECTION PER AA 5520-01035-02A-SHOP. REPAIRED AREAS OF MOISTURE INGRESSION AND DELAMINATION WITH REFERENCE TO A330 SRM 55-21-11. RESTORED TRAILING EDGE MATERIAL AND PROTECTIVE FINISH WITH REFERENCE TO OEM CMM 55-21-17. NEW ELEVATOR WEIGHT IS 308.6LBS/139.97KGS. ACCOMPLISHED THERMOGRAPHIC SKIN PANEL INSPECTION PER AA 5520-01035-02A-SHOP. REPAIRED AREAS OF MOISTURE INGRESSION AND DELAMINATION WITH REFERENCE TO A330 SRM 55-21-11. RESTORED TRAILING EDGE MATERIAL AND PROTECTIVE FINISH WITH REFERENCE TO OEM CMM 55-21-17. NEW ELEVATOR WEIGHT IS 308.6LBS/139.97KGS. (7372385)

Part: NONE — NONE · airframe 78,217 hrs · 10,294 cycles

SUPPLEMENTAL INFORMATION SHIP 3306 DOOR 4R AFT LOWER CORNER DENT. CORRECTIVE ACTION: REFERENCE ER/A 594953-14. REMOVED FASTENERS IN AFT LOWER & LOWER SEAL RETAINER. REMOVED FASTENERS COMMON TO REPAIR AREA. ACCOMPLISHED HFEC INSPECTION OF CUT OUT AREA. FOUND ADDITIONAL DAMAGE, REMOVED DAMAGE PER SRM 52-13-00. INSTALLED REPAIR PER A330 52-13. (7873399)

Part: NONE — NONE · airframe 78,197 hrs · 10,291 cycles

SHIP 3306 SEVERAL DENTS WERE FOUND ON LH PYLON FORWARD FAIRING DOOR ASSY. 451CR & 451CL. DENTS WERE EVALUATED AND SOME OF THEM WERE FOUND OUT OF LIMITS DUE TO SHORT DISTANCE BETWEEN DENT EDGE AND MEMBER SUPPORT. CORRECTIVE ACTION: REF ER/A 594533-14. (1979434)

Part: NONE — NONE · airframe 78,197 hrs · 10,291 cycles

SHIP 3306 TWO DENTS WERE FOUND IN THE UPPER SURFACE OF THE FWD SIDE IN THE LH PYLON. DAMAGE HAS BEEN EVALUATED, RESULTING IN AN OUT OF LIMITS DUE TO SHORT DISTANCE BETWEEN DENT EDGE AND MEMBER SUPPORT. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 594473-14. (1978608)

Part: NONE — NONE · airframe 78,197 hrs · 10,291 cycles

SHIP 3306 DONT PASS TEST DOOR EMERGENCY CHECK THE ESCAPE-SLIDE LOCKING MECHANINSM ICE PROTECTION AT CONTROL UNIT 15DH. CORRECTIVE ACTION: REPLACED HEATED SLIDE FITTING 19DH. (1976844)

Part: NONE — NONE · corrosion level 2 · airframe 78,197 hrs · 10,291 cycles

SHIP 3306 CORROSION LOC. BTW FR35 TO FR 37.1 ON FLOOR BEAM Y1959 PAX CABIN. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR OF SEAT TRACK SECTION LOC. BTW FR35 TO FR 37.1 ON FLOOR BEAM Y1959 PAX CABIN AS PER A330 SRM 53-00. (1973172)

Part: NONE — NONE · airframe 78,197 hrs · 10,291 cycles

SHIP 3306 DENT EXTERNAL SKIN EXISTING REPAIR FR29 TO FR30 AND STR26L TO STR27L LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC. ON EXTERNAL SKIN ON BTW FR29 TO FR30 AND BTW STR26L TO STR27L LOWER FUSELAGE AS PER A330 SRM 53-21-11-300-015 AND RESTORED SURFACE PROTECTION ON REPAIR AREA AS PER SRM A330 51-75-12-911. (1968899)

Part: NONE — NONE · airframe 78,197 hrs · 10,291 cycles

SHIP 3306 DENT EXTERNAL SKIN EXISTING REPAIR BULK CARGO DOOR FWD LOWER CORNER IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED DOUBLER REPAIR ASPER ER/A #519806-14. (1963737)

Part: NONE — NONE · airframe 78,197 hrs · 10,291 cycles

SHIP 3306 ACCOMPLISH VA 99564MA REV IR IN CONJUNCTION WITH AA 3351-01053. CORRECTIVE ACTION: ACCOMPLISHED VA99564MA REV. IR IN CONJUNCTION WITH AA3351-01053. (1949507)

Part: FAULT MESSAGE — FALSE ACTIVATION · airframe 77,839 hrs · 10,242 cycles

SHIP 3306 -DIV- TO DUB DUE TO AIR ENG 2 BLEED FAULT AND CABIN ALTITUDE CLIMBING. CORRECTIVE ACTION: REPLACED RIGHT ENGINE PRV. RAN LEFT ENGINE AND PRESSURIZED CABIN WITH BOTH PACKS. INSPECTED PACK BAYS AND FOUND NO LEAKS IN THE SYSTEM. (7871635)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,794 hrs · 10,059 cycles

SHIP 3306 EMER EXIT PATH LIGHTS INOP AT PAX SEAT ROW 21AB & 29AB. CORRECTIVE ACTION: REMOVED & REPLACED LIGHT ASSY AT 21AB PER A330 AMM 33-51. RE-TERMINATED ELECTRICAL CONNECTOR ON OUTBD SEAT ROW 29AB. (7649529)

Part: LIGHT — INTERMITTENT (CABIN) · airframe 76,347 hrs · 10,002 cycles

SHIP 3306 EMERGENCY EXIT SIGNS INOPERATIVE LOC 603. CORRECTIVE ACTION: PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST PER AMM A330-300 TASK 33-51, ALL EMERGENCY LIGHTS WORKING OK. (1775265)

Part: INLET — CONTAMINATED (APU) · airframe 75,668 hrs · 9,885 cycles

ON GROUND AFTER APU START AND ON DESCENT THROUGH FL180 DIRTY SOCKS ODOR FROM PACKS IN COCKPIT NO ODOR DETECTED IN CABIN. CORRECTIVE ACTION: T/S PER A330 TSM TASK 21-00-00-810-801-A. FOUND EXCESS DE-ICING FLUID AROUND APU INLET AREA. ISOLATED SMELL W/ APU ON AND LT PACK RUNNING. T/S PER A330 TSM TASK 49-00-00-810-831-A. CLEANED EXCESS FLUID AROUND APU EXTERNAL AREA. C/W DECONTAMINATION OF ECS, PER A330 AMM 21-00. R & R FCV LT + RT, PER A330 AMM 21-51. ALL CHECKS OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (AFT PAX DOOR) · airframe 75,617 hrs · 9,878 cycles

DOOR L AFT CABIN GOT MESSAGE AT CRUISE. CORRECTIVE ACTION: PRESSURIZED A/C INSPECTED DOOR. NTF. RAN PSCU TEST. NO FAULTS, CHECKS OK.

Part: FAULT MESSAGE — ILLUMINATED (LT AFT DOOR) · airframe 75,603 hrs · 9,874 cycles

ECAM MESSAGE/CAUTION DOOR L AFT CABIN ANNUNCIATED AT FL 410 PRESSURE NORMAL DIF 8.6. PERFORMED ECAM + QRH TO LIGHTS OUT NO PRESSURE PROBLEMS. CORRECTIVE ACTION: POST FLIGHT REPORT FAULTS PROX SENSOR (23MJ)/PROX SENSOR(25MJ)/PSCU(5MJ). T/S REF A330 TSM 52-13-00-810-803-A. FAULT CLEARED. NO FAULT DETECTED DURING GND SCANNING AND PSCU TEST OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 75,301 hrs · 9,822 cycles

ONE EMERGENCY ESCAPE PATH AT DOOR 3L INOPERABLE. CORRECTIVE ACTION: FOUND LOOSE CONNECTION. SECURED CONNECTION. OPERATIONS CHECK NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 74,673 hrs · 9,727 cycles

ROW 11JH UNDERSEAT FLOOR EMERGENCY LIGHT INOPERABLE. CORRECTIVE ACTION: SECURED LIGHT ASSEMBLY CONNECTOR AT SEAT HARNESS. OPERATIONS CHECK GOOD, PER A330 AMM 33-51.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 74,543 hrs · 9,704 cycles

AFT LT CABIN DOOR INDICATION. CORRECTIVE ACTION: CHECKED CLEARANCE OF PROX SENSORS 23MJ AND 25MJ, AS PER AMM 52-71. ALL CLEARANCES WITHIN LIMITS. CLEANED PROX SENSORS AND TARGETS, PER A330 AMM 52-71. NO CURRENT FAULTS.

Part: WARNING MESSAGE — FALSE ACTIVATION (AFT PAX DOOR) · airframe 74,543 hrs · 9,704 cycles

GOT DOOR LT AFT CABIN ILLUMINATION ON E/W DISPLAY AND AMBER CABIN WITH SLIDE DISAGREEMENT LIGHT AT 39,000 FT 1 1/2 HOURS AFTER T/O. DOOR HANDLE VISUALLY DOWN. CORRECTIVE ACTION: PERFORMED TSM 52-13-00-810-813-A A330-200. NO FAULTS CONFIRMED. ALL INDICATIONS FUNCTION CORRECTLY AT THIS TIME.

Part: COVER — MISSING (TE FLAP) · airframe 71,623 hrs · 9,303 cycles

LEFT WING NBR 3 FLAP TRACK FAIRING FORWARD COVER MISSING. INSTALL SPEED TAPE AND DEFERRED PER CDL 57-00-07 UNTIL FIXED FAIRING CAP AVAILABLE TO REPLACE. LP 6378791

Part: THRESHOLD — CORRODED (R2 DOORWAY) · corrosion level 2 · airframe 71,552 hrs · 9,295 cycles

DURING C CHECK, DOOR 2R THRESHOLD PLATE HAS CORROSION. REPLACED DOOR SILL. LP 1334138

Part: THRESHOLD — CORRODED (R4 DOORWAY) · corrosion level 2 · airframe 71,552 hrs · 9,295 cycles

DURING C CHECK, DOOR 4R THRESHOLD PLATE HAS CORROSION ON THE UPPER SURFACE AT THE 2 AFT INBOARD FASTENER HOLES. CLEANED CORROSION. LP 1332526

Part: TORSION BOX — CRACKED (FRAME 53) · airframe 71,552 hrs · 9,295 cycles

DURING C CHECK, DURING ACCOMPLISHMENT OF WC 5332-2003, CRACK INDICATIONS WERE FOUND ON DOOR 3R TORSION BOX STRINGER S-14R AT FR 53.8, S-15L AT FR 53.5 AND S-15R AT 53.5 DURING SURFACE HFEC INSPECTIONS PER NTM 53-32-07-250-801. REPLACED STRINGER S-15L F53370179000 AND S-15R F53370179001 PER DRAWING F533700200. LP 1331473

Part: SEAT TRACK — CORRODED (FRAME 75) · corrosion level 2 · airframe 71,552 hrs · 9,295 cycles

DURING C2 CHECK, SEAT TRACK BETWEEN FR 75, -YC FOUND CORRODED. REPLACED SEAT TRACK/FLOORBEAM PER SRM 51-42-11. LP 1331075

Part: STRUCTURE — GOUGED (L4 DOOR LOWER) · airframe 71,552 hrs · 9,295 cycles

DURING C2 CHECK, DOOR 4L LOWER AFT CORNER FOUND GOUGED. BLENDED OUT WITH MARGINAL FASTENER EDGE DISTANCE. INSTALLED REPAIR PRE SRM 52-13-00-300-005. LP 1329794

Part: AXLE — DAMAGED (LT MLG) · airframe 71,552 hrs · 9,295 cycles

DURING INSPECTION, LEFT MAIN GEAR BOGIE AXLE SLEEVE NBR 5 CHROME PLATING MISSING AND PEELING. REPLACED AXLE SLEEVE PER AMM 32-41-14. LP 1328860

Part: AXLE — DAMAGED (LT MLG) · airframe 71,552 hrs · 9,295 cycles

DURING INSPECTION, LEFT MAIN GEAR BOGIE AXLE SLEEVE NBR 2 CHROME PLATING MISSING AND PEELING. REPLACED AXLE SLEEVE PER AMM 32-41-14. LP 1328862

Part: COVER — MISSING (TE FLAP) · airframe 70,988 hrs · 9,231 cycles

ON WALK AROUND, FOUND LEFT WING NR 5 MOVEABLE FLAP TRACK FAIRING INBOUND AFT COVER MISSING. REPLACED COVER. LP 6155626

Part: FAIRING — DETACHED (NR 3) · airframe 70,503 hrs · 9,174 cycles

ATB - AFTER TAKE-OFF AND FLAP RETRACTION A CUSTOMER NOTIFIED THE F/A THAT A FLAP CANOE FAIRING ON THE LEFT WING WAS HANGING DOWN. MAINTENANCE FOUND LEFT #3 FAIRING LOOSE WITH DAMAGE TO FAIRING AND THE ACTUATOR ROD HANGING. REMOVED FLAP TRACK FAIRING AND DEFERRED PER CDL 27-00-04A-ATL REPAIRED LEFT OUTBOARD FLAP ATTACH BRACKET PER ER/A 580098-14 AND RE-INSTALLED FLAP TRACK FAIRING.

Part: ENGINE — FIRE (RIGHT) · airframe 64,597 hrs · 8,434 cycles

CREW PERFORMED AN AIR TURNBACK DUE TO RIGHT ENGINE FIRE INDICATION. ENGINE WAS SHUT DOWN AND EMERGENCY DECLARED. ENGINE FIRE CONFIRMED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,855 hrs · 8,335 cycles

EMERGENCY ESCAPE PATH MARKING LIGHT AT SEAT 28B INOP. DEFERRED FOR REPLACEMENT OF THE EMERGENCY SEAT LIGHT ASSEMBLY.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK WAS FOUND CORRODED AT AFT CABIN FR73, -YB. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK WAS FOUND CORRODED AT AFT CABIN FRAME 74. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT AFT CABIN FRAME 74, YC. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT AFT CABIN FR 74. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK WAS FOUND CORRODED AT AFT CABIN FR 73. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 45) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK WAS FOUND CORRODED AT AFT CABIN FR 45. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT MID CABIN FRAME 37, 1959. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT MID CABIN FRAME 33, 1552.5. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 35) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT MID CABIN FRAME-35, 953. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK WAS FOUND CORRODED AT AFT CABIN FRAME 73. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT AFT CABIN FRAME 74, YB. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK CORRODED AT MID CABIN FRAME 33, 953. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT AFT CABIN, FRAME 73-74, YB. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, FOUND SEAT TRACK CORRODED AT AFT CABIN FRAME 74 OTBD. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT AFT CABIN FRAME 74 YB OTBD. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 17-18) · airframe 53,582 hrs · 7,015 cycles

DURING M-CHECK, SEAT TRACK FOUND CORRODED AT FORWARD CABIN FRAME 17-18, 953. REPLACED SEAT TRACK.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 49,327 hrs · 6,490 cycles

EMERGENCY SEAT MOUNTED LIGHTING INOPERATIVE. RECONNECTED SEAT HARNESS AT SIDEWALL AT SEATS 14, 15 AB.

Part: LEVER — MALFUNCTIONED (L3 DOOR) · airframe 49,032 hrs · 6,454 cycles

L3 DOOR SHOWS SLIDE ARMED. CYCLED ARMING LEVER. INDICATION CAME BACK TO NORMAL. INDICATION FOLLOWS ARMING/DISARMING LEVER POSITION.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 48,910 hrs · 6,439 cycles

EMERGENCY EXIT LIGHT SWITCH IN COCKPIT, WHEN PLACED TO ARM, TURNS ON EMERGENCY LIGHTS IN THE BACK. REPLACED THE SWITCH.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 47,469 hrs · 6,255 cycles

FOUND 34 A & B AND 11 A & B EMERGENEY ESCAPE PATH LIGHT INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 45,766 hrs · 6,045 cycles

EMERGENCY LIGHT INOPERAIVE AT SEATS 30-32 AB. RECONNECTED CONNECTOR AT SEAT 32.

Part: LINKAGE — BROKEN (LT MLG) · airframe 43,653 hrs · 5,772 cycles

FLIGHT RETURNED TO DEPARTURE DUE TO THE INABLITY TO RAISE THE LANDING GEAR DURING CLIMB TO 6000 FT. NO APPLICABLE QRH PROCEDURES, NO EMERGENCY DECLARED. MAINTENANCE FOUND THE LEFT GEAR SHORTENING MECHANISM LINKAGE BROKEN. COMPLIED WITH ERA 520918-14, REPLACED BELLCRANK, PERFORMED GEARSWING, OPS CHECKED GOOD. 32-31-00-740-801.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,643 hrs · 5,770 cycles

SEAT TRACK -Y794.3 FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-41-14 FIG 103. SEAT TRACK REMOVED AND REPLACED IAW PRI ER/A 519797-14 REV O.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 57 - 57.4. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 69 - 71. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 59 - 61. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 53.8 - 54. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED FRAMES 59 - 61. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

-Y450 SEAT TRACK FOUND CORRODED AT FRAMES 37.1-37.3. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND RE PLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 60 - 61. CORROSION REMOVED IAW SRM 51-74-00. SEAT TRACK REMOVED IAW SRM 51-42-11. NEW SEAT TRACK REWORKED IAW DWG F53477233 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 53.3 - 53.8. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 38 - 39. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED IAW SRM 51-42-11. NEW SEAT TRACK REWORKED IAW DWG F53310898 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 57.4 - 58. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORROSION FRAMES 57.2 - 58. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y1456 SEAT TRACK FOUND CORRODED AT FRAMES 33 - 35. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 61 - 63. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 31 - 35. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y450 SEAT TRACK FOUND CORRODED AT FRAMES 59 - 62. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y450 SEAT TRACK FOUND CORRODED AT FRAMES 69 - 70. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORROSION FRAMES 61 - 62 Y1959. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

-Y450 SEAT TRACK FOUND CORRODED AT FRAMES 57.1 - 57.3. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 012. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 57.1 - 57.4. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORROSION AT FRAMES 53.8 - 53.9 . CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED IAW SRM 51-42-11. NEW SEAT TRACK REWORKED IAW DWG F53329024 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 53.3 - 54. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y2462 SEAT TRACK FOUND CORRODED FRAMES 65 - 70. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAME 74. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-41-14 FIG 103. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 61 - 62. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED IAW SRM 51-42-11. NEW SEAT TRACK REWORKED IAW DWG F53477233 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED FRAMES 63-68. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-1 1.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

-Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 19 - 20. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 101. SEAT TRACK REMOVED IAW SRM 51-42-11. NEW SEAT TRACK REWORKED IAW DWG F 53272112 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 40.2 - 42. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 42 - 46. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEED LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

-Y2462 SEAT TRACK FOUND CORRODED AT FRAMES 37.2 - 37.3. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED IAW SRM 51-42-11 . NEW SEAT TRACK REWORKED IAW DWG F53278804 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y450 SEAT TRACK FOUND CORRODED AT FRAMES 37.1 - 37.2. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

-Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 33 - 34. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED FRAMES 38 - 39.2. CORROSION REMOVED IAW SRM 51-74-00 . FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED IAW SRM 51-42-11 . NEW SEAT TRACK REWORKED IAW DWG F53310898 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 75 - 76. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-41-14 FIG 103. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y400 SEAT TRACK FOUND CORRODED AT FRAMES 75 - 76. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-41-14 FIG 103. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y450 SEAT TRACK FOUND CORRODED AT FRAMES 35 - 37. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORROED AT FRAMES 42 - 43. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMIT IAW SRM 53-31-15 FIG 101. SEAT TARCK REMOVED IAW SRM 51-42-11. NEW SEAT TRACK REWORKED IAW DWG F57112439 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 39 - 39.1. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED IAW SRM 51-42-11 AND NEW SEAT TRACK REWORKED IAW DWG F53310898 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

-Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 37.2 - 37.4. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED IAW SRM 51-42-11. NEW SEAT TRACK REWORKED IAW DWG F532788022 AND INSTALLED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-41-14 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

-Y1456 SEAT TRACK FOUND CORRODED AT FRAMES 33 - 35. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 5 3-41-14 FIG 103. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-41-14 FIG 103 . SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED FRAMES 51 - 53.1. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED FRAMES 50 - 51. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT LIMITS IAW SRM 53-31-15 FIG 101.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED FRAMES 53 - 53.1. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 51 - 53.1. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 43,630 hrs · 5,768 cycles

SEAT TRACK FOUND CORRODED AT FRAMES 52 - 53.1. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS SRM 53-31-15 FIG 101 . SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,722 hrs · 5,540 cycles

DURING CABIN EMERGENCY LIGHTNING TEST BOTH POWER SUPPLY BATTERY PACKS 11WL AND 12WL FAULTED. R & R BATTERIES AT 11WL AND 12WL TEST OK, OK FOR SERVICE.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 29,440 hrs · 3,934 cycles

BATTERY EPSU (13WL) DOOR 2 FAILED SYSTEM CHECK, REPLACED BATTERY AND TESTS OK.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 29,440 hrs · 3,934 cycles

BATTERY EPSU (16WL) DOOR 3 FAILED SYSTEM CHECK, REPLACED BATTERY AND TESTS OK.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 29,440 hrs · 3,934 cycles

BATTERY EPSU (19WL) FAILED SYS CHECK, REPLACED BATTERY AND TESTS OK.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 29,440 hrs · 3,934 cycles

BATTERY EPSU (11WL) DOOR 1 FAILED SYSTEM CHECK, REPLACED BATTERY AND TESTS OK.

Part: OVEN — SMOKE (GALLEY) · airframe 27,194 hrs · 3,661 cycles

DURING CRUISE, OVEN NR 2 POSITION 1-6 OVERHEATED, THE FOOD BEGAN TO SMOKE AND LAVATORY SMOKE DETECTOR WENT OFF. THE OVEN CIRCUIT BREAKER WAS PULLED AND 2 HALON BOTTLES WERE DISCHARGED INTO OVEN AND THE SMOKE QUICKLY DISIPATED. FLIGHT CONTINUED TO DESTINATION AND LANDING WAS UNEVENTFUL. OVEN WAS REPLACED AND OK FOR SERVICE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR48-FR51. REPAIRED IAW SRM 51-52-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 40. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK Y450 FR39. REPAIRED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 47. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 39-FR 47. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 46. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR53. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT FR 38-FR 39 . REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR38-FR39. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR40-FR47. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,459 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 37. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 52-FR 53. REPAIRED IAW SRM 51-42-11 AND SRM 51-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR53- FR54. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR50. REPAIRED IAW SRM 53-31-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-1959 CORRODED AT FR53 TO 54. REPAIRED IAW SRM 53-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR 37 TO 38. REPAIRED IAW SRM 51-42-11, AND SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR37 TO 38. REPAIRED IAW SRM 53-31-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 62-FR 70. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR55 TO 58. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR37. REPAIRED IAW SRM 51-42-11, AND SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK CORRODED AT FR52 TO 53. REPAIRED IAW SRM 53-31-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR67 TO 71. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR39 TO 47. REPAIRED IAW SRM 53-31-13.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-1959 CORRODED AT FR54 TO 58. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-1959 CORRODED AT FR53 TO 54. REPAIRED IAW SRM 53-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-2462 CORRODED AT FR40 TO 41. REPAIRED IAW SRM 53-31-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-1959 CORRODED AT FR52. REPAIRED IAW SRM 53-31-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR53 TO 54. REPAIRED IAW SRM 53-31-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-450 CORRODED AT FR68 TO 71. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK CORRODED AT FR59 TO 66. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y-2462 WAS CORRODED AT FR50 TO 58. REPAIRED IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y1959 CORRODED AT FR 39-2. REPAIRED IAW SRM 53-31-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON FLOOR SUPPORT UNDER PANEL 272KF. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK Y450 FR 58-67. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 62-70. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 55-57. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 59-60. REPAIRED IAW SRM 51-42-11.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 87,479 hrs · 77,093 cycles

DURING "L" CHECK FOUND CRACK IN FLOOR PANEL NR66. REPAIRED IAW SRM 51-30-2 AND SRM 53-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1456 FR 19. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,673 hrs · 3,585 cycles

DURING "H" CHECK FOUND SEAT TRACK Y953 AT FR37-2 HAS CORROSION. REPAIRED IAW SRM 53-00-15.

Part: WARNING LIGHT — FALSE ACTIVATION (EPSU) · airframe 23,960 hrs · 3,228 cycles

BATTERY EPSU (14WL) MESSAGE DURING TEST, REPLACED BATTERY AND TESTS OK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 23,487 hrs · 3,162 cycles

BATTERY EPSU (15WL) DOOR 3 FAILED SYSTEM CHECK, REPLACED BATTERY AND TESTS OK.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS)

BATTERY EPSU (17WL) FAILED SYS CHECK, REPLACED BATTERY AND TESTS, OK. (K)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,263 hrs · 2,866 cycles

BATTERY EPSU 12WL DOOR 1 FAILED CAPACITY CHECK, REPLACED BATTERY AND TESTS OK.

Part: RIB — CRACKED (RT WING) · airframe 17,453 hrs · 2,309 cycles

DURING INSPECTION PER AD 2006-22-14 FOUND CRACKS IN RT WING RIB NR 6. REPAIRED PER EA 33-208520.

Part: RIB — CRACKED (LT WING) · airframe 17,453 hrs · 2,309 cycles

DURING INSPECTION PER AD 2006-22-14, FOUND CRACKS IN LT WING RIB NR 6. REPAIRED PER EA 33-208520.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 12,895 hrs · 1,699 cycles

AT CRUISE RECEIVED "HYD G ENG 1 LO PR", FOLLOWED COM AND TURNED OFF NR 1 ENGINE PUMP. THEN RECEIVED "HYD G ENG 2 LO P", FOLLOWED COM AND TURNED OFF NR 2 ENGINE PUMP. THEN RECEIVED "HYD G RES LO LVL", FOLLOWED COM AND TURNED OFF GREEN ELECTRIC PUMP. DECLARED A YELLOW EMERGENCY, LANDING WAS UNEVENTFUL, PINNED GEAR AND WAS TOWED TO GATE. FOUND NR 2 ENGINE DRIVEN PUMP LEAKING, REPLACED BOTH EDP AND BLED THE SYSTEM AND CHECK OK.

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 260 hrs · 43 cycles

DURING CRUISE, RECEIVED MASTER CAUTION AND MOMENTARY ECAM WARNINGS FOR SMOKE IN THE IN-FLIGHT ENTERTAINMENT BAY, AFT CARGO COMPARTMENT, AND AVIONICS VENT. WARNINGS CLEARED WITHOUT CREW ACTION AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. RESET THE PASSENGER SYSTEM PUSH BUTTON. BITE TEST OF SDCU GOOD.