N808NW

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 96,290 hrs · 12,650 cycles

FWD EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY PER A330 AMM 33-51. OK FOR SERVICE. (7380450)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 95,799 hrs · 12,581 cycles

EMERGENCY PATH LIGHTS INOPERATIVE AT LOCATIONS 30A,49A,56A,56H & 43H. REPAIRED PER A330 AMM 33-51. OK FOR SERVICE. (8042139)

Part: DOOR — FOD (ZONE 800) · airframe 95,493 hrs · 12,542 cycles

SHIP 3308 CABIN DOOR 4R SHOWING OPEN WHEN CLOSED. CORRECTIVE ACTION: CYCLED DOOR AND REMOVED DEBRIS PER A330 AMM 52-10. INDICATION NORMAL. OK FOR SVC. (7833628)

Part: WIRE — DAMAGED (ZONE 200) · airframe 95,301 hrs · 12,518 cycles

SHIP 3308 EMERGENCY LIGHTS INOPERATIVE 46, 49, 56 JH. REPAIRED WIRING IAW AMM 33-51. (7922648)

Part: DOOR — OUT OF ADJUST (ZONE 800) · airframe 93,052 hrs · 12,236 cycles

SHIP 3308 1L DOOR OUT OF ADJUSTMENT. CORRECTIVE ACTION: ADJUSTED DOOR PER A330 AMM 52-11. OPS CHECK GOOD. THIS WAS A PRO-ACTIVE DOOR CHECK. (0954579)

Part: WIRE — DAMAGED (ZONE 200) · airframe 92,607 hrs · 12,180 cycles

SHIP 3308 SEAT MOUNTED EMERGENCY PATH LIGHTING INOP SEAT 56H. CORRECTIVE ACTION: REPLACED LIGHT ASSY AND REPAIRED WIRING PER A330 AMM 33-52. (6989147)

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 200) · airframe 91,353 hrs · 12,021 cycles

SHIP 3308 -ATO- AT 50KTS DUE TO THRUST LEVER NOT SET MESSAGE. CORRECTIVE ACTION: PERFORMED AFS AND AUTOLAND TEST WITH NO FAULTS FOUND. PERFORMED RESET OF FCMC 1/2, FMGEC 1/2, FWC 1/2 AND VERIFIED 1FD2 DISPLAYED ON BOTH PFDS WITH NO FAULTS FOUND. (6568218)

Part: BEAM — CRACKED (ZONE 800) · airframe 91,265 hrs · 12,010 cycles

SHIP 3308 FRAME FORK AREAS AT BEAM 4 IN THE AFT CARGO COMPARTMENT DOOR, FOUND A CRACK ON THE FR61 H-2. CORRECTIVE ACTION: INSTALLED NEW FRAME PER DELTA WORK CARD 5230-01164-10. (0726218)

Part: SUPPORT WEB — CRACKED (ZONE 400) · airframe 91,265 hrs · 12,010 cycles

SHIP 3308 RH PYLON LAPF NO.2 SUPPORT WEB. CORRECTIVE ACTION: STOP DRILL AT THE CRACK END AND APPLY DOUBLER REPAIR WITH MATERIAL 2024-0-0.063" AS PER PW CMM 54-56-11. (0726441)

Part: HEAT SHIELD — DAMAGED (ZONE 400) · airframe 91,265 hrs · 12,010 cycles

SHIP 3308 ELONGATED FASTENER HOLES COMMON TO AN EXISTING REPAIR WAS FOUND ON THE #2 ENGINE LAPF LOWER HEAT SHIELD. CORRECTIVE ACTION: REPAIRED PER ERA 623079-14. (0725383)

Part: SKIN — DENTED (ZONE 100) · airframe 91,265 hrs · 12,010 cycles

SHIP 3308 LOWER HALF FUSELAGE AT FR66 STRG55R FOUND DENT. CORRECTIVE ACTION: APPLIED DOUBLER REPAIR AS PER A330 SRM 53-41-11. (0724657)

Part: SKIN — CRACKED (ZONE 400) · airframe 91,265 hrs · 12,010 cycles

SHIP 3308 RH ENG LAPF LOWER SKIN CRACKED. CORRECTIVE ACTION: DOUBLER REPAIR AS PER PW MANUAL 51A702 CMM 54-56-11. (0724691)

Part: RIB — CRACKED (ZONE 400) · airframe 91,265 hrs · 12,010 cycles

SHIP 3308 LH PYLON LAPF LH SUPPORT NO.8 RIB CRACKED. CORRECTIVE ACTION: STOP-DRILLED AT THE END OF CRACK AT NO.8 LH RIB AND QPPLY DOUBLER REPAIR AS PER PW 51A702 CMM 54-56-11 REPAIR 13 REV 22. (0724726)

Part: WEB — CRACKED (ZONE 400) · airframe 91,265 hrs · 12,010 cycles

SHIP 3308 LH PYLON LAPF NO.1 SUPPORT WEB CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 541163-14. (0724567)

Part: PSU — OPEN (SEATS 32JH) · airframe 90,623 hrs · 11,927 cycles

SHIP 3308 PSU OPEN AT SEATS 32JH ON LANDING. CORRECTIVE ACTION: REPACKED MASKS AND RESECURED PANEL PER A330 AMM 35-23. (6396313)

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 89,969 hrs · 11,847 cycles

SHIP 3308 3L DOOR ASSIST BOTTLE LOW. CORRECTIVE ACTION: SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. OK FOR SERVICE. (4015040)

Part: OXYGEN PANEL — DETACHED (ZONE 200) · airframe 89,733 hrs · 11,817 cycles

SHIP 3308 OXYGEN PANEL FOR MASK IN 38AB DETACHED. CORRECTIVE ACTION: RE-SECURED PANEL AND RE-PACKED MASK PER A330 AMM 35-23. OK FOR SERVICE. (6052542)

Part: GIRT BAR — FOD (ZONE 200) · airframe 89,702 hrs · 11,813 cycles

SHIP 3308 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND FOD IN GIRT BAR TRACK. REMOVED PER A330 AMM 52-71. OK FOR SERVICE. (6052533)

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 6J) · airframe 89,493 hrs · 11,786 cycles

SHIP 3308 O2 MASK PANEL AT 6J OPENED ON LANDING. CORRECTIVE ACTION: RESECURED PER A330 AMM 35-23. OK FOR SERVICE. (6098944)

Part: VALVE — BINDING · airframe 89,493 hrs · 11,786 cycles

ATO - DUE TO ENG THRUST LOSS MESSAGE WHEN T/O POWER SELECTED. CORRECTIVE ACTION: DEFERRED PER MEL 36-11-02. THEN REPLACED LEFT ENGINE PRV PER A330 AMM 36-11. OPS AND LEAK TEST GOOD. MEL/PLAC REMOVED. (6098950)

Part: SKIN — DENTED (ZONE 800) · airframe 89,256 hrs · 11,756 cycles

SHIP 3308 DENT AND GOUGE AT L2 DOOR LOWER SKIN & DOOR ARM FITTING. CORRECTIVE ACTION: REPAIRED PER ER/A 615119-14. (0454547)

Part: GUST LOCK — FOD (PAX DOOR) · airframe 88,885 hrs · 11,709 cycles

ENTRY DOOR HARD TO OPEN OR CLOSE / LOCATION:606. CORRECTIVE ACTION: FOUND FOD STUCK IN BLACK PLASTIC CAP OF DOOR HOLD OPEN RELEASE PLUNGER. REMOVED FOD, OPS CK OK. REF A330 AMM 52-13. (0398872)

Part: DOOR — FOD (R1) · airframe 88,822 hrs · 11,701 cycles

SHIP 3308 DOOR 1R PIN WILL NOT STAY SECURE. CORRECTIVE ACTION: REMOVED FOD FROM DOOR PER A330 AMM 52-12. PIN NOW SECURE. (5956620)

Part: SIGN — BROKEN (EMERGENCY LGIHTS) · airframe 88,259 hrs · 11,631 cycles

SHIP 3308 LT SIDE EMERGENCY ROW EXIT SIGN BROKEN. CORRECTIVE ACTION: R/R EMERGENCY ROW EXIT SIGN PER A330 AMM 33-51. (4760690)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 88,209 hrs · 11,625 cycles

SHIP 3308 ESCAPE PATH (AFT) LIGHT INOP AT SEAT 3J. CORRECTIVE ACTION: FOUND CONNECTION LOOSE AT PLUG. RESECURED CK'S GOOD. (4760674)

Part: DOOR — HANDLER ERROR (L2) · airframe 87,140 hrs · 11,485 cycles

SHIP 3308 WHILE IN CVG, THE MID PASSENGER L2 DOOR (P/N F5217030002800) LOWER EDGE MADE CONTACT WITH THE JET BRIDGE. DAMAGE CONSISTS OF TWO AREAS, AREA A AND AREA B. DAMAGE AREA A IS A DENT TO THE LOWER EDGE OF THE DOOR OUTER SKIN AND UNDERLYING SEAL RETAINER ANGLE. DAMAGE AREA B INCLUDES A GOUGE TO THE DOOR SUPPORT HINGE ARM LOWER ATTACHMENT FITTING. DAMAGE AREA A DOOR DENT FORWARD EDGE BEGINS 14.5" FROM THE DOOR LEADING EDGE, MEASURING 8" WIDE (FWD/AFT) BY 1.4" TALL (FROM THE BOTTOM EDGE OF THE DOOR). THE MAXIMUM DEPTH AT THE DENT CENTER IS 0.455". THE DENT IMPACTS THE DOOR OUTER SKIN (P/N F5217003125000) MADE FROM 2.4-MM (0.094") THICK 2024 T351 ALUMINUM PER ABS5043A024 AND THE DOOR EDGE ANGLE (P/N F5217003625000) IS MADE FROM 2.5-MM (0.098") THICK 2024-T42 ALUMINUM PER ABS5044A025. THIS DAMAGE IS OUTSIDE OF ALLOWABLE LIMITS PER A330-300 SRM 52-10-00-283-001. DAMAGE AREA B IS ON THE DOOR SUPPORT HINGE ARM (P/N F5217031600400) AT THE LOWER LUG COMMON TO THE FUSELAGE ATTACHMENT LOCATION. THE LOWER LUG CONTAINS A GOUGE TO THE FORWARD FACE OF THE FITTING 0.3" BY 0.2" WITH A MAXIMUM DEPTH OF 0.005". AFTER BLENDING THE DAMAGED AREA MEASURED 1.0" WIDE X 3/16" INTO THE LUG WALL THICKNESS X 7/32" DOWN THE LUG FACE. CORRECTIVE ACTION: REPAIR REF ER/A 615119-14. (5400668)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,110 hrs · 11,348 cycles

SHIP 3308 43B AND H EMER LIGHTS RED INOP 44H INOP. CORRECTIVE ACTION: REPINNED 43B/H AND 44H AS NEEDED. (8945926)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,691 hrs · 11,298 cycles

SHIP 3308 EMERGENCY EXIT SIGNS INOPERATIVE. LOCATIONS:600. CORRECTIVE ACTION: RECYCLED EMER EXIT LT SWITCH.WORKS NML NOW. (2997114)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,949 hrs · 11,207 cycles

SHIP 3308 GUST LOCK STUCK IN HOUSING. DOOR 4R. CORRECTIVE ACTION: INSPECTED GUST LOCK AND OPERATIONAL CHECKED MULTIPLE TIMES. NO FAULTS NOTED. (2915838)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,581 hrs · 11,163 cycles

SHIP 3308 EMERGENCY LIGHTS ON SEATS43,44JH 43AB AND 56JH ARE INOP. CORRECTIVE ACTION: RECONECTED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT 44 JH, 43 AB AND 56JH. REMOVED AND REPLACED SEAT EMERGENCY LIGHT AT 43 JH. (4672479)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 84,370 hrs · 11,137 cycles

AIRCRAFT 3308, EMER EXIT ROW LIGHTS INOP R/H ROW 31, 44, 57, 53. CORRECTIVE ACTION: FOUND LIGHT ASSY'S DISCONNECTED @ 31H, 44H, 57H, 53H, LIGHTS RECONNECTED IAW A330 AMM 33-52. (LP 4854922)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,920 hrs · 11,080 cycles

SHIP 3308 CREW REPORT POSSIBLE BIRD STRIKE ON TAKEOFF. CORRECTIVE ACTION: FOUND BIRD STRIKE ON RH SIDE OF RADOME, DAMAGE INSPECTED AND FOUND OUT OF LIMITS AS PER A330 AMM 53-15-11-200-801-A. REMOVED AND REPLACED. (4803642)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,862 hrs · 11,073 cycles

SHIP 3308 - DIV - INTO JFK DUE TO G SYS LEAK ECAM MSG AND HYD QTY INDICATING BELOW AMBER MARK. ALTERNATE GEAR EXTENSION EXECUTED. CORRECTIVE ACTION: GREEN BRAKING MANIFOLD FOUND LEAKING FROM PLUG DUE TO DAMAGED PACKING. REPLACED PACKING AND PERFORMED LEAK CHECKS. AS PRECAUTION, RAN MOTORS TO VERIFY NOT FURTHER LEAKS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,877 hrs · 11,075 cycles

SHIP 3308 SEAT 3A & 6A SEAT BELT/AIRBAGS FAILED OPS CHK. REPLACED SEAT 3A AND 6A EMA.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,561 hrs · 11,036 cycles

SHIP 3308 1L DOOR PRESSURE CHECK ON FAP. CORRECTIVE ACTION: DEU B R/R. (4159824)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 83,324 hrs · 11,009 cycles

SHIP 3308 SEAT 39B SEAT EMERGENCY EXIT LIGHT INOP. CORRECTIVE ACTION: R/R LIGHT ASSY PER A330 AMM 33-51. OK FOR SERVICE. (9959022)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 INOP EPSU-EMERGENCY POWER SUPPLY UNIT 18WL ON PASSENGER CABIN. CORRECTIVE ACTION: REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 18WL ON PASSENGER CABIN, PERFORMED BONDING CHECK. PERFORMED BITE OF THE SMOKE DETECTION SYSTEM AND PERFORMED CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE CHECK. ALL TEST AND BONDING CHECK ARE GOOD. (2616437)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DENT ON EXTERNAL SKIN LOC BTW FR 66 TO FR 67 AT LEVEL OF STRG 56R TO 57R. CORRECTIVE ACTION: COMPLIED WITH ER/A 605293-14 PRI REV-0, REV-1 AND PRI REV-2 AND VALIDATED WITH ER/A 605293-14 REV-ORIGINAL MATCHES PRI 605293-14REV-0, REV-1 AND REV-2, PERFORMED PERMANENT REPAIR ON DENT AREA LOC. BTW FR66 TO FR67 AND BTW STR56R TO STR57R ON EXTERNAL SKIN LOWER FUSELAGE AS PER ER/A 605293-14 REV-ORIGINAL. TIME CONTROLLED ITEMS SECTION DTE ASSOCIATED ER/A 00-605293 ADDED FOR AC 3308. (2615235)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DENT EXTERNAL SKIN FR68 TO FR69 AND STR52R TO STR56R LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 605293-14 PRI REV-0, VALIDATED WITH ER/A 605293-14 REV-ORIGINAL MATCHES HAS BEEN WITH PRI REV-0, PERFORMED PERMANENT REPAIR ON DENT AREA LOC. BTW FR68 TO FR69 AND BTW STR52R TO STR56R ON EXTERNAL SKIN LOWER FUSELAGE AS PER ER/A605293-14 REV-ORIGINAL, AND REPETITIVE INSPECTION IS REQUIRED. (2615249)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER P ANEL AT HOLE H263 RH SIDE. AA 5716-01017. SB A330-57- 3115 REV 02. AD 2019-16-07. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE H263 RH LOC. ON FR40 VERTICAL WEB ABOVE CENTER WING BOX LOWER PANEL RH SIDE AS PER ER/A604913-14AD. RE-INSPECTION IS REQUIRED. (2615921)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER P ANEL AT HOLE H263 LH SIDE. AA 5716-01017. SB A330-57- 3115. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE H263 LH LOC. ON FR40 VERTICAL WEB ABOVE CENTER WING BOX LOWER PANEL LH SIDE AS PER ER/A604913-14AD REV-ORIGINAL, COMPLIED WITH ER/A 604913-14 AD REV-ORIGINAL MATCH HAS BEEN VALIDATED WITH ALL STEP ON PRI REV-0, PRIREV-1 AND PRI REV-2, RE-INSPECTION IS REQUIRED. JOB COMPLETE. (2615911)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER P ANEL AT HOLE H260 RH SIDE. AA 5716-01017. SB A330-57- 3115. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE H260 LOC. ON FR40 VERTICAL WEB ABOVE CENTER WING BOX LOWER PANEL RH SIDE AS PER ER/A604913-14AD REV-ORIGINAL, COMPLIED WITH ER/A 604913-14 AD REV-ORIGINAL MATCH HAS BEEN VALIDATED WITH ALL STEP ON PRI REV-0, PRIREV-1 AND PRI REV-2, RE-INSPECTION IS REQUIRED. JOB COMPLETE ASSOCIATED ER/A 14-604913 ADDED FOR AC 3308. (2615933)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE H260 LH SIDE. AA 5716-01017. SB A330-57-3115 REV 02. AD 2019-16-07. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE H260 LOC. ON FR40 VERTICAL WEB ABOVE CENTER WING BOX LOWER PANEL LH SIDE AS PER ER/A604913-14AD REV-ORIGINAL, COMPLIED WITH ER/A 604913-14 AD REV-ORIGINAL MATCH HAS BEEN VALIDATED WITH ALL STEP ON PRI REV-0 , PRIREV-1 AND PRI REV-2, RE-INSPECTION IS REQUIRED AT HOLE H260 LH WITHIN 21,279 FC/ 152,554 FH (WHICHEVER OCCURS FIRST) FROM AIRCRAFT FIRST FLIGHT AND THEREAFTER WITHIN EVERY 9.110 FC/ 61,600 FH (WHICHEVER OCCURS FIRST) AFTER INITIAL INSPECTION AS PER ER/A 604913-14AD REV-ORIGINAL, TIME CONTROL ITEMS, SECTION V RII INSPECTION COMPLETE. (2615899)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DENT EXTERNAL SKIN FR58 TO FR59 AND STR55L TO STR56L LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 605293-14 PRI REV-0, VALIDATED ER/A 605293-14 REV-ORIGINAL HAS BEEN MATCHES WITH PRI-REV-0, PERMANENT REPAIR ON DENT AREA LOC. BTW FR58 TO FR59 AND BTW STR55L TO STR56L ON EXTERNAL SKIN LOWER FUSELAGE AS PER ER/A 605293-14 REV-ORIGINAL, AND REPETITIVE INSPECTION IS REQUIRED FROM FIRST FLIGHT AT INTERVALS OF 35,400 FC/FH NOT RELEVANT AND REPETITIVE INSPECTION ATINTERVALS OF 2,250 FC/FH NOT RELEVANT ASPER ER/A 605293-14 REV- ORIGINAL, SECTION III. JOB COMPLETE. (2615726)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DONT PAST TEST EMERGENCY POWER SUPPLY UNIT (18WL). CORRECTIVE ACTION: REPLACED EMERGENCY POWER SUPPLY UNIT (18WL), PERFORMED OPERATIONAL CHECK OF THE POWER SUPPLY UNIT BITE CHECK, PERFORMED BONDING CHECK, AND PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT VIA THE EPSU TEST PUSH BUTTON, AND REPLACED SLIDE RAFT AFT DOOR 4 RH DUE TO TSM. ALL OPERATIONAL TEST ARE GOOD. (2616400)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DURING HCK AT AEROMAN (SAL) AND DURING INSPECTION PER EM 5716-01 017, HOLE 260 LH AND RH WERE FOUND CRACKED. REPAIRS WERE ACCOMPL ISHED PER SECT I AND III OF ERA 604913-14AD. CORRECTIVE ACTION: ACCOMPLISH THE SECT IV OF ERA 604913-14 AT HOLE 260 LH AND RH AT A THRESHOLD OF 21,279 TOTAL FC OR 152,554 TOTAL FH AND REPEAT A T AN INTERVAL OF 9,110 FC OR 61,600 FH THEREAFTER. (2614008)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DURING HCK AT AEROMAN (SAL) AND INSPECTION PER EM 5716-01017, HO LE 263 RH WAS FOUND CRACKED. A REPAIR WAS ACCOMPLISHED PER SECT IV OF ERA 604913-14AD. CORRECTIVE ACTION: ACCOMPLISH THE SECT VII INSPECION OF HOLE 263 RH AT A THRESHOLD OF 26,579 TOTAL FC OR 188,454 TOTAL FH AND REPEAT AT AN INTERVAL OF 3,860 FC OR 26,100 FH THEREAFTER. (2614019)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DURING HCK AT AEROMAN (SAL) AND INSPECTION PER EM 5716-01017, CRACK WAS FOUND AT HOLE 263 LH. A REPAIR WAS ACCOMPLISHED PER SECT II OF ERA 604913-14AD. CORRECTIVE ACTION: ACCOMPLISH THE SECT VI INSPECTION OF HOLE 263 LH AT A THRESHOLD OF 21,409 TOTAL FC OR 153,454 TOTAL FH AND REPEAT AT AN INTERVAL OF 3,410 FC OR 23,000 FH THEREAFTER. (2614017)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR29 TO FR31 BTW STR51L TO STR51R AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 486923-14. ISSUE C, WITHSUPPLEMENTAL INSPECTIONS ALREADY TRACKED AS PER DAL LP 0437802. ALSO, DUE THE DISCREPANT FASTENER LOCATION ENCOUNTERED AS PERINSPECTION OF THIS ER/A, SECTION IV OF ER/A 486923-14 REV F WAS ACCOMPLISHED WITHOUT DEVIATIONS. COMPLIED WITH ER/A 604660-14. (2612812)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DURING HCK, A DENT ON THE FUSELAGE SKIN WAS FOUN D AT FR 66 TO 67, STR 56R TO 57R. THE DENT WAS REWORKED AND INSP ECTED PER SECT II OF ERA 605293-14. CORRECTIVE ACTION: THE DENT REORKED AND INSPECTED PER SECTION II IS APPROVED. (2613663)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN DOOR INNER LOCATED FR.62 TO FR.62 A IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER A330 SRM 52-32-00. COMPLIED WITH ER/A 604660-14. (2612807)

Part: NONE — NONE · airframe 82,358 hrs · 10,891 cycles

SHIP 3308 DURING HCK, MULTIPLE DENTS WERE FOUND ON THE REAR FUSELAGE LOWER SKIN PANEL. THE DENTS WERE REWORKED AND INSPEC TED PER SECT I OF ERA 605293-14. CORRECTIVE ACTION: ACCOMPLISH THE SECT III DVI INSPECTION OF THE SECTION I REWORKED DENTS PER DELTA ERA 605293-14. (2613661)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK RIB 6 AFT ON LH WING. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER EM 5720- 01066-03A AND AIRBUS REPAIR DRAWING R57257026. REPAIR IS APPROVED PER AIRBUS REPAIRDRAWING R57257026 ACCORDING TO FAA AD 2006-22-14, PARAGRAPH (K) GUIDELINES. EM 5720-01066-06A(FORECAST:33-0557-8-0083) IS TRACKING INSPECTIONS BASED ON SRI 57-21-36 INSPECTION INSTRUCTION. AS PER ER/A 604660-14 PRI REV-0, HAS BEEN COMPLIED WITH ER/A604660-14 REV-ORIGINAL MATCHES JOB COMPLETE. (2611790)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.27 TO FR.28 BTW STR 50L TO STR 51L AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 486923-14, DUE THE DISCREPANT FASTENER LOCATION ENCOUNTERED AS PER INSPECTION OF THIS ER/A, SECTION IV OF ER/A 486923-14 WAS ACCOMPLISHED WITHOUT DEVIATIONS, AS PER ER/A 604660-14 HAS BEEN COMPLIED WITH. ER/A 604660-14 MATCHES JOB COMPLETE. (2611837)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK RIB 6 AFT ON RH WING. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER EM 5720-01066-03B AND AIRBUS REPAIR DRAWING R57257026. REPAIR IS APPROVED PER AIRBUS REPAIR DRAWING R57257026 ACCORDING TO FAA AD 2006-22-14, PARAGRAPH (K) GUIDELINES. EM 5720-01066-06B(FORECAST:33-0557 -8-0082) IS TRACKING INSPECTIONS BASED ON SRI 57-21-36 INSPECTION INSTRUCTION. ASPER ER/A 604660-14 PRI REV-0, HAS BEEN COMPLIED WITH ER/A 604660-14 REV-ORIGINAL MATCHES JOB COMPLETE. (2611899)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CORROSION STRINGER 55R AT LEVEL OF FRAME 65 IN BULK CARGO COMPARTMENT. CORRRECTIVE ACTION: PERFORMED PERMANENT REPAIR INSTRUCTIONS ON INTERNAL AREA LOC. ON FR65 AT LEVEL OF STR55R ON LOWER REAR FUSELAGE AS PER ER/A #605292-14. (2611615)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.83 TO FR.84 BTW STR33R TO 36R AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER NWA EA 33-201684, REV B. ALSO INSPECTIONS AND INSTALLATION OF MISSING FASTENERS WAS ACCOMPLISHED WITH NIL DEVIATIONS. ASPER ER/A 604660-14 PRI REV 0. HAS BEEN COMPLIED WITH ER/A 604660-14 REV-ORIGINAL MATCHES JOB COMPLETE. (2611850)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN DOOR INNER AT FR61 TO FR61A IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER A330 SRM 52-32-00. AS PER ER/A604660-14 PRI REV-0 HAS BEEN COMPLIED WITH ER/A 604660-14 REV-ORIGINAL MATCHES. (2611636)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FLOOR BEAM WEB AROUND THE COLLAR OF THE REINFORCEMENT STRAP ATTACHMENT FASTENERS BTW FR75 TO FR79 IN PASSENGER CABIN. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER EO 5320-01135. STC IS APPROVED FOR DAMAGE TOLERANCEIN ACCORDANCE WITH FAR25.47 AND 25.571. AS PER ER/A 604660-14, HAS BEEN COMPLIED WITH ER/A 604660-14 MATCHES JOB COMPLETE. (2611885)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED DOOR L4 AFT CORNER AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTEN REPAIR INSTALLED PER A330 SRM 52-13-00, FIGURE 213, WHICH IS SUPERSEDED BY A330 SRM 52-13-00-300-013. AS PER ER/A 604660-14 PRI REV-0 HAS BEEN COMPLIED WITH ER/A604660-14 REV-ORIGINAL MATCHES. (2611652)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.27 TO FR.28 BTW STR50L TO STR51L AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 486923-14, INSPECTIONS ALREADY TRACKED AS PER DAL LP 0437802. ALSO, DUE THE DISCREPANT FASTENER LOCATION ENCOUNTERED AS PER INSPECTION OF THIS ER/A, SECTION IV OF ER/A 486923-14 WAS ACCOMPLISHED WITHOUT DEVIATIONS, AS PER ER/A 604660-14. HAS BEEN COMPLIED WITH ER/A 604660-14 MATCHES JOB COMPLETE. (2611731)

Part: EXTINGUISHER — OUT OF LIMITS (AFT CARGO) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 OUT LIMIT FIRE EXTINGUISHER BOTTLE WEIGTH (AFT BOTTLE) IN FWD CARGO COMPARTMENT (1 EA). CORRECTIVE ACTION: REMOVED AND REPLACED FIRE EXTINGUISHER BOTTLE (AFT BOTTLE) IN FWD CARGO COMPARTMENT (1 EA). PERORMED OPERATIONAL CHECK OF FIRE EXTINGUISHING BOTTLE LOW PRESSURE INDICATION CIRCUIT BY PTT. OPERATIONAL TEST LDCC VENTILATION SYSTEM. TEST ARE OK. (2600126)

Part: EXTINGUISHER — OUT OF LIMITS (FWD CARGO) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 OUT LIMIT FIRE EXTINGUISHER BOTTLE WEIGTH (FWD BOTTLE) IN FWD CARGO COMPARTMENT (1 EA). CORRECTIVE ACTION: REMOVED AND REPLACED FIRE EXTINGUISHER BOTTLE (FWD BOTTLE) IN FWD CARGO COMPARTMENT (1 EA). PERORMED OPERATIONAL CHECK OF FIRE EXTINGUISHING BOTTLE LOW PRESSURE INDICATION CIRCUIT BY PTT AND OPERATIONAL TEST LDCC VENTILATION SYSTEM. TEST ARE OK. (2600114)

Part: SKIN — DENTED (CARGO DOOR) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 DENT DOOR INNER SKIN BTW BEAM 4 AND BEAM 5 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC. BTW FR63 TO FR63A AND BTW BEAM 4 AND BEAM 5 ON DOOR INNER SKIN OF AFT CARGO COMPARTMENT DOOR AS PER A330 SRM 52-32-00-300-008. (2599551)

Part: PINTLE PIN — CORRODED (RT MLG) · airframe 82,354 hrs · 10,889 cycles

CORRODED REAR PINTLE PIN ON RT MAIN LANDING GEAR. REMOVED UNSERVICEABLE REAR PINTLE PIN AND INSTALLED A NEW SERVICEABLE REAR PINTLE.

Part: STRINGER SPLICE — CRACKED (FRMS 79-80 S26R) · airframe 82,354 hrs · 10,889 cycles

CRACKED SPLICE BETWEEN FRAMES 79 - 80, S26R. REPLACED SPLICE AND FASTENERS IAW SRM.

Part: STRINGER FITTING — CRACKED (FRMS 79-80 S26L) · airframe 82,354 hrs · 10,889 cycles

CRACK SPLICE, FRAMES 79 - 80, STRINGER 26L. REPLACED THE STRINGER SPLICE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FRMS 74-75) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROED FLOOR SUPPORT -Y 450, FRAMES 74 - 75 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR SUPPORT Y2462, FRAMES 73 - 74 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM.

Part: SKIN — DENTED (NR 1 SLAT) · airframe 82,354 hrs · 10,889 cycles

THE NR 1 SLAT, WAS FOUNDED DENTED A AND SCRATCHED ON THE TOP SKIN. REPAIRED IAW ERA 602677-14.

Part: FLOOR SUPPORT — CORRODED (FRM 75) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORRODED FLOOR SUPPORT +Y450 LOCATED BTW FR.75. REPLACED FLOOR SUPPORT Y450 LOC BTW FR75 TO FR80 AT AFT GALLEY AREA IAW SRM 51-72-11-911, SRM 51-42-11-801.

Part: FLOOR SUPPORT — CORRODED (FRMS 75-76) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR SUPPORT -Y1447.8 BTW FR75 TO FR76 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT -Y1447.8 LOC. BTW FR74 TO FR78 AT AFT GALLEY AREA AS PER A330 SRM 51-72-11-911-001.

Part: SEAT TRACK — CORRODED (FRMS 71-75) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION SEAT TRACK Y450 LOCATED BTW FR.71 TO FR.75 AT AFT GALLEY AREA. REPLACED FLOOR BEAM Y450 LOC. BTW FR.71 TO FR.75 AT AFT GALLEY AREA AS PER A330 SRM 51-72.

Part: FLOOR SUPPORT — CORRODED (FRM 80) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR STRUCTURE PLATE AT LEVEL Y-450 AND FR80 IN PASSENGER CABIN. REPLACED FLOOR STRUCTURE PLATE AT LEVEL Y-450 AND FR80 IN PASSENGER CABIN. (2582268)

Part: FLOOR SUPPORT — CORRODED (FRMS 75-80) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR SUPPORT -Y450 LOCATED BTW FR.75 TO FR.80 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y450 LOCATED BTW FR.75 TO FR.80 AT AFT GALLEY AREA ASPER A330 SRM-51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CORROSION FLOOR BEAM -Y2462 LOCATED BTW FR.73 TO FR. 74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y2462 LOCATED BTW FR.73 TO FR.74 AT AFT GALLEY AREA A330 SRM 51-42-11-801 AND A330 SRM 51-72-11-901-001. (2579192)

Part: NONE — NONE (NONE) · airframe 82,354 hrs · 10,889 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN 48 INCHES FWD OF DOOR L2 1 FOOT BLOW ENGINE SCAN LIGHT AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED DETAIL VISUAL INSPECTION OF THE INSTALLED DOUBLER LOC.EXTERNAL FUSELAGE SKIN 48 INCHES FWD OF DOOR 2L, 1 FOOT BELOW ENGINE SCAN LIGHT BTW FR30 TO FR31 AND BTW STRG 26 TO 28. AND NOT FOUND SIGN OF DEGRADATION (E.G. REPAIRS WITH EVIDENCE OF CRACKS, CORROSION, PULLED FASTENERS OR DENTS). PERFORMED GVI ON INSTALLED DOUBLER CONFIRMED INSTALLEDDOUBLER MATCHES A330 SRM 53-21-11-300-015 AS PER NTM 51-90-00.

Part: SEAT TRACK — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CORROSION SEAT TRACK YB1 LOCATED BTW FR.73 TO FR.74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM YB1 LOC. BTW FR73 TO FR74 AT AFT GALLEY AREA AS PER A330 SRM 51-72-11. (2575588)

Part: SEAT TRACK — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CORROSION SEAT TRACK YC1 LOCATED BTW FR.73 TO FR.74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED NEW FLOOR BEAM YC1 LOC. BTW FR73 TO FR74 AT AFT GALLEY AREA ASPER SRM A330 51-72-11-911-001 AND A330 SRM 51-42-11-801. (2575689)

Part: FLOOR SUPPORT — CORRODED (FRM 75-78) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR BEAM -Y381 BTW FR 75 TO FR 78 RH SIDE AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y381 LOC BTW FR75 TO FR78 IN AFT GALLEY AREA AS PER A330 SRM 51-72-11, A330 SRM 51-42-11 AND DWG F53478040.

Part: FLOOR SUPPORT — CORRODED (FRMS 75-78) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR SUPPORT Y381 FR75 TO FR78 LT SIDE IN PASSENGER CABIN. REPLACED FLOOR BEAM Y381 LOC. BTW FR75 TO FR78 IN PASSENGER CABIN ASPER A330 SRM 51-72-11, A330 SRM 51-42-11 AND DWG F53478040.

Part: SEAT TRACK — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 CORROSION SEAT TRACK YB LOCATED BTW FR.73 TO FR.74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM YB LOC. BTW FR73 TO FR74 AT AFT GALLEY AREA ASPER SRM A330 51-72-11-911-001 AND DRAWINGS F53478009 AND F53478040. (2573667)

Part: FLOOR SUPPORT — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR BEAM -YB LOCATED FR73 TO FR74 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -YB LOC. BTW FR73 TO FR74 AT AFT GALLEY AREA IAW SRM 51-72-11-911-001 AND DRAWINGS F53478009.

Part: FLOOR SUPPORT — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR BEAM -YB1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -YB1 LOC. BTW FR73 TO FR74 AT AFT GALLEY AREA ASPER SRM A330 51-72-11-911-001 AND DRAWINGS F53478101 AND F53478008.

Part: FLOOR SUPPORT — CORRODED (FRMS 73-74) · corrosion level 2 · airframe 82,354 hrs · 10,889 cycles

CORROSION FLOOR BEAM -YC1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -YC1 LOC. BTW FR73 TO FR74 IN PASSENGER CABIN AS PER A330 SRM 51-42-11, A330 SRM 51-72-11.

Part: SKIN — DENTED (LT NR 1 SLAT) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 SLAT #1 L/H DENT WITH SCRATCH DAMAGE LOCATED BELOW STR1 BETWEEN WFX4506 AND WFX4770. CORRECTIVE ACTION: PERMANENT REPAIR ACCOMPLISHED IAW ERA 602677-14. (2557631)

Part: UNKNOWN — UNKNOWN (R1 DOOR) · airframe 82,215 hrs · 10,872 cycles

1R DOOR DIFFICULT TO DISARM. PERFORMED INSP & CK OF DOOR 1R SLIDER MECHANISM & ACTUATED SEVERAL TIMES.

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 IN PREPARATION FOR ACCOMPLISHMENT OF 5310-01461-01, IT WAS IDENTIFIED THAT THE CAPITAL TOOL KIT CALLED OUT IN THE WORK INSTRUCTIONS, P/N FTIA330533273-1, FOR COLD WORKING DOES NOT ALIGN WITH THE DAL ATICTS TOOLING P/N. THE CAPITAL KIT CONTAINS STANDARD TOOLING THAT IS REUSABLE AND OWNED BY DAL / READILY AVAILABLE TO BE PULLED VIA ATICTS FOR DAL MTC. VA 99359MA ADDRESSES THIS DIFFERENCE IN WHAT S OBTAINABLE VIA ATICTS VS. WHAT IS CALLED OUT IN THE SECTION 01 WORK CARD BY SPECIFICALLY CALLING OUT USE OF DAL P/N S LB-20 (PULLER) AND FT-20 (POWER PACK) IN ADDITION TO THE OVERALL KIT PART NUMBER THESE PULLER AND POWER PACK PART NUMBERS MAKE UP THE NECESSARY PIECES OF CAPITAL KIT, P/N FTIA330533273-1, FOR ACCOMPLISHMENT OF 5310-01461-01. CORRECTIVE ACTION: ACCOMPLISHED VA NUMBER 99359MA IN CONJUNCTION WITH EM 5310-01461-01. (2509090)

Part: NONE — NONE (NONE) · airframe 82,354 hrs · 10,889 cycles

SHIP 3308 DURING ACCOMPLISHMENT OF THE MODIFICATION REQUIRED PER FAA AD 2019-19-09 AND SB A330-53-3273 REV. 2 VIA WORK CARD 5310-01461- 01, MTC HAS REPORTED AN ERROR REFERENCING AN INCORRECT FIGURE VIEW WITHIN THE WORK STEPS. CORRECTIVE ACTION: ACCOMPLISHED VA NUMBER 99370MA WITH EM 5310-01461. (2500635)

Part: NONE — NONE (NONE) · airframe 82,354 hrs · 10,889 cycles

EM 5716-01017 WAS WRITTEN TO PERFORM THE ACTIONS REQUIRED BY AD 2019-16-07. DURING ACCOMPLISHMENT OF EM -01 AND -02 WORK CARDS, WHICH INCLUDE SB A330-57-3115 AND SB A330-57-3131 INSTRUCTIONS, CERTAIN STEPS FROM THE MODIFICATION SB WERE FOUND TO HAVE AN IMPROPER "NA" SIGN OFF STEP. REFERENCE STEP 32 OF THE WORK CARDS. ACCOMPLISHED VA NUMBER 99350MA IN CONJUNCTION WITH EM 5716-01017 WORK SECTION01 AND 02.

Part: NONE — NONE · airframe 81,676 hrs · 10,803 cycles

SHIP 3308 DOOR 3L DOOR DAMPER REQUIRES SERVICING, CORRECTIVE ACTION: CHARED 3L DOOR DAMPER IAW A330 AMM 52-10 (9387742)

Part: NONE — NONE · airframe 81,676 hrs · 10,803 cycles

SHIP 3308 EMERG LIGHTS INOP 51BA & 57JH, CORRECTIVE ACTION: RESEATED CONNECTORS FOR EMERG. LIGHTS AT SEATS 51BA/ 57JH IAW A330 AMM 33-51 (9387741)

Part: NONE — NONE · airframe 81,229 hrs · 10,744 cycles

SHIP 3308 AFTER TAKEOFF GEAR RETRACTED. EXIT SIGNS ABOVE CABIN DOORS AND IN CREW REST MODULE REMAINED ILLUMINATED AND NO SMOKING LIGHT EXTINGUISHED WHEN IN AUTO POSITION. CORRECTIVE ACTION: PERFORMED TEST. NO TROUBLE FOUND. PERFORMED POWER UP TEST ON CIDS PER A330 AMM 23-73. TEST OK. PER PRECAUTION RESET CIDS PER A330 AMM 23-73. (9071026)

Part: NONE — NONE · airframe 81,212 hrs · 10,742 cycles

SHIP 3308 4R DOOR WOULD NOT DISARM. CORRECTIVE ACTION: CLEARED FLOOR ATTACHMENT POINTS AND CYCLED ARMING MECHANISM. (9071012)

Part: NONE — NONE · airframe 80,700 hrs · 10,680 cycles

SUPPLEMENTAL INFORMATION SHIP 3308 SEAT 57JH ESCAPE PATH LIGHT IS INOP. CORRECTIVE ACTION: FOUND WIRE PLUG DISCONNECTED. RECONNECTED. (9227470)

Part: NONE — NONE · airframe 81,580 hrs · 10,790 cycles

SUPPLEMENTAL INFORMATION SHIP 3308 UPON ARRIVAL IN ATL, MTC FOUND A V-SHAPED GOUGE ON THE NOSE FWD FUSELAGE RH SKIN. JUST FWD OF FR13 AND ABOVE STR 30. ONE LEG OF THE GOUGED AREA MEASURES 2.50 INCHES IN LENGTH WHILE THE OTHER IS 5.00 INCHES IN LENGTH WITH MAXIMUM DEPTH OF 0.15 INCHES. THE DAMAGE IS IN EXCLUDED AREA. CORRECTIVE ACTION: CW ALL STEPS ON PRI 600479-14. ALSO REF ER/A 600479-14. (2298850)

Part: FIRE BOTTLE — WARNING LIGHT · airframe 79,876 hrs · 10,578 cycles

SHIP 3308 VERIFIED APU FIRE BOTTLE DISCH LIGHT ILLUMINATED ON OVERHEAD. CORRECTIVE ACTION: REPLACED APU FIRE BOTTLE IAW A330 AMM 26-22. (8637629)

Part: NONE — NONE · airframe 79,232 hrs · 10,495 cycles

SHIP 3308 ALL FA CREW BUNK 02 MASKS DEPLOYED. CORRECTIVE ACTION: RE-STOWED CREW 02 MASKS IN LDMCR. CONFIRMED NO 02 GENERATORS USED. (8652554)

Part: NONE — NONE · airframe 79,232 hrs · 10,495 cycles

SHIP 3308 O2 MASKS HANGING IN CREW REST.CORRECTIVE ACTION: REPOSITIONED AND SECURED CREW REST MASK. (8652550)

Part: NONE — NONE · airframe 78,541 hrs · 10,400 cycles

SHIP 3308 RED EMERGENCY PATHWAY LIGHT ASSY AT RT FWD COAT CLOSET MISSING. CORRECTIVE ACTION: FOUND MISSING LIGHT ASSY AND REINSTALLED PER A 330 AMM 33-51. (8723574)

Part: NONE — NONE · airframe 78,153 hrs · 10,346 cycles

SHIP 3308 UNABLE TO DISARM SLIDE AT 1LEFT. CORRECTIVE ACTION: PERFORMED OP CHECK PER A330 AMM 52-10. FAULT COULD NOT BE DUPLICATED. LUBED GIRT BAR. CHKS NML. (8560916)

Part: NONE — NONE · airframe 78,298 hrs · 10,367 cycles

SHIP 3308 1L AND 4R DOORS WONT DISARM. CORRECTIVE ACTION: R/R DOOR 1L FWD SLIDE FITTING REF A330 AMM 30-46.OPS CKS GOOD. AFT DOOE SLIDE FITTING CKS GOOD. DOOR 4R PASSES ALL CKS. (2099138)

Part: NONE — NONE · airframe 78,135 hrs · 10,344 cycles

SHIP 3308 ON ENG SHUTDOWN DOORS 1L AND 4R WOULD NOT DISARM, FROZEN. CORRECTIVE ACTION: THAWED DOORS 1L AND 4R GIRT BARS. LUBED GIRT BAR. (8560908)

Part: NONE — NONE · airframe 78,114 hrs · 10,340 cycles

SHIP 3308 REPETITIVE WRITE UPS OF 1L DOOR WONT DISARM UPON ARRIVING TO GATE. CORRECTIVE ACTION: T/S. TESTED "OK" ON HEAT CONTROL UNIT 30H. HOWEVER REMOVED AND REPLACED 3DH DUE TO LOOSE LATCH TO CONNECTOR. R/R 3MJ PROX SWITCH CTL UNIT PER A330 AMM 52-71. BITE TEST PASSED. NO FAULTS DETECTED. (2092101)

Part: NONE — NONE · airframe 78,055 hrs · 10,332 cycles

SHIP 3308 ON ARRIVAL 1L SLIDE WOULD NOT DISARM. CORRECTIVE ACTION: APPLIED HEAT, EXERCISED HANDLE. 1L SLIDE DISARMED NORMALLY. OPS CHECK GOOD. (8272271)

Part: NONE — NONE · airframe 78,044 hrs · 10,328 cycles

SHIP 3308 1LEFT DOOR SLIDE WILL NOT DISARM. CORRECTIVE ACTION: FOUND GIRT BAR MECHANISM NOT SET CORRECTLY.RECTIFIED SAME PER A330 AMM 52-10. SLIDE DISARMED AS REQUIRED. (8272252)

Part: NONE — NONE · airframe 77,869 hrs · 10,304 cycles

SHIP 3308 1L DOOR ARMING LEVER DIFFICULT TO MOVE TO DISARM POSITION. CORRECTIVE ACTION: CHK'D DOOR FRAME AREA FOR DEBRIS, NONE FOUND. OPERATED DOOR ARMING MULTIPLE TIMES NO DISCREPANCIES. (8258090)

Part: NONE — NONE · airframe 78,044 hrs · 10,328 cycles

SHIP 3308 4R DOOR HARD TO DISARM. CORRECTIVE ACTION: HEATING CONTROL UNIT 22DH TEST OK. LUBRICATED BOTTOM SLIDER MECHANISM & GIRT. DEBRIEFED CREW. NO DEFECTS NOTED. T/S. ALL CHECKS GOOD. NO DEFECTS NOTED. ARM/DISARM CONTROL HANDLE OPS SMOOTHLY. (2074333)

Part: NONE — NONE · airframe 77,839 hrs · 10,299 cycles

SHIP 3308 4R DOOR SLIDE WOULD NOT DISARM AFTER ARRIVAL AT THE GATE. CORRECTIVE ACTION: FOUND TRASH UNDERNEATH THE ESCAPE SLIDE AND AROUND GIRT BAR, TRASH REMOVED. OPS CHECK OF 4R DOOR SLIDE PERF AND SATISFACTORY. (8258078)

Part: NONE — NONE · airframe 77,736 hrs · 10,283 cycles

SHIP 3308 FLIGHT ATTENDANT AT DOOR 4R HAD A HARD TIME DISARMING THE SLIDE. CORRECTIVE ACTION: OPERATED ARM/DISARM LATCH MULTIPLE TIMES. COULD NOT REPLICATE ISSUE. (8258042)

Part: NONE — NONE · airframe 77,736 hrs · 10,283 cycles

SHIP 3308 DOOR 4R DIFFICULT TO DISARM. CORRECTIVE ACTION: PERFORMED PAX DOOR 4R OPERATION CK PER A330 AMM 52-12. DISARM FUNCTION CKS GOOD. (8258036)

Part: NONE — NONE · airframe 77,685 hrs · 10,271 cycles

SHIP 3308 DONT PASS TEST EPSU-EMERGENCY POWER SUPPLY UNIT. CORRECTIVE ACTION: REPLACED EPSU 14WL. PERFORMED SYSTEM TEST OF EPSU 14WL. (2056226)

Part: NONE — NONE · airframe 77,682 hrs · 10,270 cycles

SHIP 3308 DONT PASS TEST GREEN LIGHT UNIT 22DH UNDER FLOOR IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SLIDE FITTING HEATED 24DH. (2043110)

Part: NONE — NONE · airframe 77,682 hrs · 10,270 cycles

SHIP 3308 MISSING DOOR L2 AND R2 SAFETY PIN AT SLIDE RAFT IN PASSENGER CABIN. CORRECTIVE ACTION: INSTALLED DOOR L2 AND R2 SAFETY PIN AT SLIDE RAFT IN PASSENGER CABIN. INSPECTION COMPLETE. (2034371)

Part: NONE — NONE · airframe 77,661 hrs · 10,267 cycles

SHIP 3308 32AB EMER SEAT ESCAPE PATH LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED LIGHT ASSY. (8352974)

Part: NONE — NONE · airframe 77,678 hrs · 10,269 cycles

SHIP 3308 11JF SEAT EMER PATH LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED LIGHT ASSY. (8352975)

Part: NOT REPORTED — NOT REPORTED · airframe 77,379 hrs · 10,217 cycles

SHIP 3308 DOOR 4R HAS INCORRECT HINGE PANEL INSTALLED. CORRECTIVE ACTION: FOUND HINGE PANEL INSTALLED AND NOT EFFECTIVE FOR A/C. REMOVED HINGE PANEL. COMPLETED REQUIRED MODIFICATION AND REPAIR PER ERA 594961-14. (8098157)

Part: NONE — NONE · airframe 77,682 hrs · 10,270 cycles

SHIP 3308 WAS DISCOVERED TO HAVE INCORRECT DOOR 4R INTERIOR PANEL ASSEMBLY P/N G2527645802100 INSTALLED WHERE P/N F2527041007900 SHOULD BE. CORRECTIVE ACTION: REF ER/A 594961-14. (1989307)

Part: NONE — NONE · airframe 77,379 hrs · 10,217 cycles

SUPPLEMENTAL INFORMATION SHIP 3308 ON WALK FOUND PUNCTURE ON PANEL 191AB. CORRECTIVE ACTION: REFERENCE ER/A 594915-14 FOR REPAIR. REPLACED ACCESS PANEL 191AB. (8098146)

Part: NONE — NONE · airframe 77,682 hrs · 10,270 cycles

SHIP 3308 PYLON 1 AFT INBD T/E. SEVEN SCREWS PULLED THROUGH SKIN AFT LOWER EDGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC LOWER AFT PYLON FAIRING #1 AS PER ER/A #595848-14. (8092309)

Part: CIDS — FAULTED (EMERGENCY LIGHTS) · airframe 76,728 hrs · 10,115 cycles

SHIP 3308 LEFT SIDE EXIT LIGHTS STAY ON EVEN WHEN LANDING GEAR RETRACTED. CORRECTIVE ACTION: CIDS 1+2 RESET PERFORMED. CABIN LIGHTS CHECK PASSED PER A330 AMM 33-20. (7327646)

Part: OXYGEN GEN — INOPERATIVE (FA OXYGEN) · airframe 76,746 hrs · 10,117 cycles

SHIP 3308 F/A #1 BUNK OXYGEN GEN INOP. CORRECTIVE ACTION: REMOVED AND REPLACED #1 FA LDMCR OXYGEN GENERATOR PER A330 AMM 35-21. (7906991)

Part: OXYGEN MASK — MISINSTALLED (CREW REST) · airframe 76,668 hrs · 10,104 cycles

SHIP 3308 ALL MASKS DEPLOYED IN LDMCR. CORRECTIVE ACTION: INSPECTED PILOT AND BUNK #2 FOR ISSUES. BOTH LOCATION HAD IMPROPER OXYGEN MASK STOWED. PERFORMED ANOTHER DEPLOY. ALL LOC DEPLOYED AS INTENDED. (1917678)

Part: ENGINE — MAKING METAL (NR 2) · airframe 76,610 hrs · 10,096 cycles

SHIP 3308 - ATB- DUE TO RIGHT ENGINE HIGH EGT AND VIBRATION AFTER TAKEOFF. MAINTENANCE FOUND METAL IN TAIL PIPE, WILL REQUIRE ENGINE CHANGE. REPLACED #2 ENGINE.

Part: LIGHT — INOPERATIVE (SEAT 16HJ) · airframe 76,436 hrs · 10,055 cycles

SHIP 3308 PAX SEAT 16HJ EMERGENCY PATH LIGHT INOP. CORRECTIVE ACTION: REMOVED & REPLACED EMERGENCY LIGHT ASSY AT 16HJ. (7908626)

Part: FASTENER — MISSING (PYLON FAIRING) · airframe 76,986 hrs · 10,153 cycles

SHIP 3308 A SINGLE MISSING FASTENER COMMON TO #2 ENG PYLON LOWER AFT FAIRING. THE FASTENER HOLE IS ENLARGED. CORRECTIVE ACTION: REFER TO ER/A 592642-14. (7380726)

Part: A/C PACK — ODOR (NR 1) · airframe 75,927 hrs · 9,977 cycles

SHIP 3308 ODOR ON APU START AND DESCENT THRU 10K FT. CORRECTIVE ACTION: METALLIC SMELL NOTED AFTER PACK 1 IS STARTED THEN QUICKLY DISSIPATES. OPENED DUCT BETWEEN ACM AND REHEATER AND NOTED STRONG SMELL AT ACM TURBINE INLET. NO SMELL AT HEATED FLOOR PANELS OR APU START COMPONENTS IN BULK CARGO. REPLACED PACK 1 ACM. (7338562)

Part: FAN — FAILED (RECIRCULATION) · airframe 75,910 hrs · 9,973 cycles

SHIP 3308 ELECTRIC ODOR ON DESCENT. CORRECTIVE ACTION: INSPECTED GLARESHIELD LIGHTS. PERFORMED GVI OF APU COMPARTMENT, APU BATTERY AND APU BCL. REPLACED FWD AND AFT RECIRC FAN FILTERS. REPLACED LEFT RECIRC FAN. FOUND CIRCUIT BREAKER TRIP EXTERNAL HORN MESSAGE ON ECAM. HORNS SMOKED THE TRIPS BEAKER. REPLACED MECHANIC CALL HORN. CANNOT DUPLICATE SMELL. (7338537)

Part: FAN — FAILED (EXTRACT) · airframe 75,800 hrs · 9,958 cycles

SHIP 3308 NUMEROUS VENT EXTRACT OVBD CAUTION MESSAGES WITH ASSOCIATED ELECTRICAL SMELL DURING DESCENT. CORRECTIVE ACTION: POST FLIGHT REPORTS EXTRACT FAN(7HQ)/AEVC(2HQ). FOUND BAD FAN (7HQ). R&R EXTRACT FAN PER A330 AMM 21-26. OPS CHECKS GOOD. NO ODOR NOTED. AVEC SYSTEM TEST PASS. (7338508)

Part: GUST LOCK — STUCK (L2 DOOR) · airframe 75,542 hrs · 9,917 cycles

SHIP 3308 DOOR 2L GUST LOCK BUTTON STUCK IN THE DOWN MANNER. CORRECTIVE ACTION: GUST LOCK BUTTON RELEASED AND TESTED FOUND TO BE OPS NORMAL. (1790409)

Part: GUST LOCK — BINDING (R2 DOOR) · airframe 75,032 hrs · 9,843 cycles

SHIP 3308 DOOR 2R GUST LOCK JAMMED IN HOUSING. CORRECTIVE ACTION: RE-POSITIONED GUST LOCK. (1747314)

Part: HANDLE — MALFUNCTIONED (L1 DOOR) · airframe 74,829 hrs · 9,815 cycles

SHIP 3308 DURING BLOCK IN 1L DOOR HANDLE WOULD NOT DISARM THE SLIDE. HANDLE WOULDN'T MOVE FAR ENOUGH TO INSERT PIN. CORRECTIVE ACTION: CYCLED DISARM/ARM HANDLE DOOR OPS CHECK GOOD.

Part: COVER — MISSING (TE FLAP) · airframe 72,529 hrs · 9,449 cycles

DURING WALK AROUND PDC FOUND COVER ON FLAP FAIRING NBR 3 RIGHT SIDE INBOARD MISSING. INSTALLED MISSING CAP ON RIGHT WING NBR 3 FLAP FAIRING, LP 6549126

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 72,014 hrs · 9,377 cycles

DOOR 2R SLIDE WILL NOT ENGAGE PROPERLY. DOOR SLIDE INDICATION SHOWS ARMED WHEN DISENGAGED AT GIRT BAR. FOUND GIRT BAR LOOSE. RE-INSTALLED GIRT BAR.

Part: COVER — MISSING (TE FLAP) · airframe 71,943 hrs · 9,366 cycles

DURING WALK AROUND FOUND A FLAP TRACK FAIRING COVER MISSING FROM MOVEABLE FAIRING NBR 5 ON RIGHT HAND, ZONE 634 COVER FIN 634CR. DEFERRED PER CDL 57-00-07-REPLACED CAP ON NBR 5 RIGHT FLAP TRACK FAIRING. LP 6678931

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 71,648 hrs · 9,327 cycles

DURING HFA CHECK, EPSU SYSTEM TEST, EPSU 15WL AND 16WL AT DOOR 3 FAILED. REPLACED EMERGENCY EXIT SIGN ABOVE DOOR 3L. LP 6698126

Part: CLAMP — BROKEN (PRECOOLER) · airframe 71,459 hrs · 9,302 cycles

SHIP 3308 -ATB- RETURNED TO MSP DUE TO RIGHT ENGINE BLEED LEAK MESSAGE AFTER TAKEOFF. HOT SMELL NOTICED IN CABIN. CORRECTIVE ACTION: FOUND CLAMP FROM FLEX DUCT TO PRECOOLER BROKEN. REPLACED CLAMP ON FORWARD FLANGE OF PRE-COOLER AND DAMAGED PANELS. LP 6546106

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 71,440 hrs · 9,298 cycles

DURING C CHECK, EPSU A DOOR 4L FIN 17WL SELF TEST RESULTED WITH UNIT FAULTY. REPLACED EPSU. LP 1374520

Part: SEAT TRACK — CORRODED (FRAME 36) · corrosion level 2 · airframe 71,440 hrs · 9,298 cycles

DURING C CHECK, SEAT TRACK AT FR 36, -Y1959 AT G2AR RIGHT GALLEY FORWARD MOUNT FOUND CORRODED. SPLICED NEW SECTION OF SEAT TRACK FOR SRM 53-00-15. LP 1372160

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 71,440 hrs · 9,298 cycles

DURING C CHECK, OUTBOARD SEAT TRACK AT DOOR 2R CORRODE AT BOTH GIRT BAR ATTACH POINTS. REPLACED SEAT TRACK PER AIRBUS DRAWING 14F532176401 AND ER/A 583260-14. LP 1372110

Part: SEAT TRACK — CORRODED (FRAME 34) · corrosion level 2 · airframe 71,440 hrs · 9,298 cycles

DURING C CHECK, SEAT TRACK AT FR 34, -Y1959 IN G2 GALLEY FOUND CORRODED. CONTAINED DAMAGED AND EVALUATED PER SRM 53-00-15-283-001. LP 1371961

Part: THRESHOLD — CORRODED (L4 DOOR) · corrosion level 2 · airframe 71,440 hrs · 9,298 cycles

DURING CHECK, DOOR 4L THRESHOLD PLATE HAS LIGHT SURFACE CORROSION VISIBLE. REPLACED DOOR SILL PER SRM 51-42-00. LP 1369389

Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,750 hrs · 9,214 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 15AB. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT SEAT 15AB. LP 6205182

Part: LIGHT — DAMAGED (CABIN) · airframe 68,005 hrs · 8,884 cycles

EMERGENCY FLOOR LIGHTNING DAMAGED AT GALLEY 1A. REPLACED EMERGENCY FLIGHT LIGHT. LP 0991317

Part: PANEL — CRACKED (R3 DOOR) · airframe 62,327 hrs · 8,165 cycles

DOOR 3R INTERIOR TOP PANEL PREVENTS THE DOOR FROM OPENING AND IS CRACKED. REPAIRED PANEL AND RE-INSTALLED PANEL AND CHECKED DOOR RIGGING.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,072 hrs · 8,124 cycles

EMERGENCY LIGHTS SEAT 16JH TO 29JH ARE INOPERATIVE. REPLACED EPSU 16WL AND BATTERY PACK.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 62,072 hrs · 8,124 cycles

DURING INSPECTION, FOUND SEAT 10JH EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR LOOSE BELOW SEAT PAN, RECONNECTED THE CONNECTOR.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 60,777 hrs · 7,957 cycles

L3 DOOR EMERGENCY EXIT SIGN COVER LOOSE. REPLACED EXIT LENS COVER.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 59,194 hrs · 7,762 cycles

ROW 10A EMERGENCY LIGHT INOPERATIVE. FOUND WIRE PULLED OUT OF PIN. PINNED THE CONNECTOR.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 59,104 hrs · 7,750 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHT BATTERIES FAILED CAP CHECK IAW WC 0591-0204. REPLACED THE BATTERY PACKS IAW AMM 33-512.

Part: ACCUMULATOR — LEAKING (HYD SYSTEM) · airframe 58,576 hrs · 7,683 cycles

THE FLIGHT CREW PERFORMED A REJECTED TAKE OFF AT 60 KNOTS DUE TO A GREEN HYDRAULIC SYSTEM PRESSURE LOSS. WHILE TAXING BACK TO GATE LOST STEERING AND BRAKES, USED ALT BRAKES TO STOP. MAINTENANCE REPLACED THE GREEN HYD SYSTEM ACCUMULATOR, BLED GREEN HYD SYSTEM. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,088 hrs · 7,609 cycles

DURING SERVICE CHECK, FOUND MONUMENT MOUNTED EMERGENCY ESCAPE PART MARKER ON THE RIGHT SIDE OF GALLEY A4 INOPERATIVE. REPLACED EMERGENCY LIGHT.

Part: WARNING MESSAGE — ILLUMINATED (L3 DOOR SLIDE) · airframe 53,288 hrs · 6,995 cycles

DURING M-CHECK, ESCAPE SLIDE LT SWITCH, EPSU DOOR 3L CLASS 1 CMC MESSAGE APPEARED. REPLACED DOOR 3L SLIDE.

Part: PANEL — CRACKED · airframe 53,288 hrs · 6,995 cycles

DURING M-CHECK, A CRACK WAS FOUND ON HOLE B, THE CWB LOWER LT PANEL WHILE PERFORMING EM 5716-01015, SB A330-57-3081. REMOVED THE DAMAGE BY REAMING THE HOLE .4MM AND INSTALLED STRAIGHT BUSHING AND WASHER IAW ER/A 539595-14AD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · airframe 53,288 hrs · 6,995 cycles

DURING M CHECK, AFT CABIN FR 73-74, -YB1 FLOOR STRUCTURE FOUND CORRODED. REPLACED FLOOR STRUCTURE IAW SRM 51-42-11, REV 88.

Part: SEAT TRACK — CORRODED (FRAMES 72-75) · airframe 53,288 hrs · 6,995 cycles

DURING M-CHECK, AFT CABIN FR 72-75, -Y450 SEAT TRACK FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-42-11, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · airframe 53,288 hrs · 6,995 cycles

DURING M-CHECK, AFT CABIN FRAME 73-74, -YB 1. FLOOR STRUCTURE FOUND CORRODED. SSI 534159-01-01. REPLACED FLOOR STRUCTURE IAW SRM 51-42-11, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · airframe 53,288 hrs · 6,995 cycles

DURING M-CHECK, AFT CABIN, FRAME 73-74, YB 1, FLOOR STRUCTURE FOUND CORRODED, SSI 534159-01-1. REPLACED FLOOR STRUCTURE IAW SRM 51-42-01, REV 88.

Part: SKIN — DAMAGED (FRAME 1) · airframe 53,288 hrs · 6,995 cycles

DURING M-CHECK, LIGHTNING STRIKE DAMAGE, FRAME 1, STR 33-34 LT. REPAIRED IAW SRM 53-21-11 AND 53-00-11, FIG 219.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 53,286 hrs · 6,994 cycles

DURING M CHECK, AFT CABIN FR 73-74, -YB SEAT TRACK FOUND CORRODED. REPLACED SEAT TRACK IAW SRM51-42-11, REV 88.

Part: TRACK — CORRODED (RT WING TE FLAP) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, FOUND DDS OF RT WING NR 3 TRACK CORRODED. REPLACED DDS OF RT WING NR 3 TRACK IAW AMM 27-54-56-401.

Part: TRACK — CORRODED (RT WING TE FLAP) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, FOUND DDS OF RT WING NR 4 TRACK CORRODED. REPLACED DDS OF RT WING NR 4 TRACK IAW AMM 27-54-56-401.

Part: CROSSBEAM — CORRODED (FRAME 76) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, BULK CARGO FRAME 76, Y-240 CROSS BEAM FOUND CORRODED. REPLACED BULK CARGO CROSS BEAM IAW SRM51-42-01, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAME 76) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, AFT CABIN FRAME 76, DOOR 4R AFT FLOOR STRUCTURE FOUND CORRODED. REPLACED FLOOR STRUCTURE IAW SRM 51-42-11, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, BULK CARGO FRAME 67-69 FLOOR STRUCTURE FOUND CORRODED. REPLACED FLOOR STRUCTURE IAW SRM 51-42-00, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAME 76) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, AFT CABIN FRAME 76, DOOR 4L AFT FLOOR STRUCTURE FOUND CORRODED. REPLACED FLOOR STRUCTURE IAW SRM 51-42-11, REV 88, LP 2289565.

Part: FLOOR SUPPORT — CORRODED (FRAMES 75-78) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, AFT CABIN FRAME 75-78, Y450 INBD FLOOR STRUCTURE FOUND CORRODED. REPLACED FLOOR STRUCTURE IAW SRM 51-42-11, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · airframe 53,286 hrs · 6,994 cycles

DURING M CHECK, AFT CABIN FRAMES 73-74 -YC1 FLOOR STRUCTURE FOUND CORRODED. REPLACED FLOOR STRUCTURE SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, AFT CABIN FRAME 73, -YB TO -YC SEAT TRACK FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-42-11, REV 88.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, MID CABIN FRAME 37-37.4 SEAT TRACK FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-42-11, REV 88.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, MID CABIN FRAME 37-37.4, -Y450 SEAT TRACK FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-42-11, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAMES 73-74) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, AFT CABIN FRAME 73-74, YC 1 FLOOR STRUCTURE FOUND CORRODED. REPLACED FLOOR STRUCTURE IAW SRM 51-42-11, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, BULK CARGO FRAME 66-67, Y480 FLOOR STRUCTURE FOUND CORRODED. REPLACED FLOOR STRUCTURE IAW SRM 51-42-00, REV 88.

Part: FLOOR SUPPORT — CORRODED (FRAMES 72-73) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, AFT CABIN FR 72-73 YC FLOOR STRUCTURE FOUND CORRODED.

Part: SEAT TRACK — CORRODED (FRAMES 31-37) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, MID CABIN FRAME 31-37, Y-1456 SEAT TRACK WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-42-11, REV 88.

Part: SEAT TRACK — CORRODED (FRAMES 31-37) · airframe 53,286 hrs · 6,994 cycles

DURING M-CHECK, MID CABIN FRAME 31-37, Y1959 SEAT TRACK FOUND CORRODED. REPLACED SEAT TRACK SRM 51-42-11, REV 88.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 52,074 hrs · 6,847 cycles

EPSU 19WL FAULT MESSAGE ON MCDU. REPLACED EPSU 14WL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 50,231 hrs · 6,627 cycles

LOWER DECK CABIN CREW REST COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. ROW 16-29 FLOOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY 16WL AND REPAIRED CONNECTOR AT SEAT 16JH.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,885 hrs · 6,585 cycles

DURING PASSENGER COMPARTMENT CHECK FOUND EPSU AT DOOR 3R INOPERATIVE. REPLACED EPSU AT DOOR 3R.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 47,408 hrs · 6,268 cycles

FOUND EMERGENCY LIGHTS INOPERATIVE AT SEATS 20H, 27B, 39H, AND 10A. CONNECTED CONNECTOR TO SEAT 20H.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 47,479 hrs · 6,277 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEATS 10A, 37B, AND 39H INOPERATIVE. FOUND LOOSE CONNECTORS AT CABIN SIDEWALL FOR EACH SEAT.

Part: STRUCTURE — DAMAGED (L4 DOOR) · airframe 43,416 hrs · 5,779 cycles

DURING CHECK, L4 DOOR AFT LOWER CORNER DAMAGED. REPAIRED IAW SRM 52-13-00, FIG 213.

Part: SEAT TRACK — CORRODED (FRAME 19) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y1959, FRAME 19 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. NEW SEAT TRACK REWORKED IAW DWG F53272112, ISSUE B. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 65-70) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y2462 FRAMES 65, 68 AND 70 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 56-58) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y2462, FRAMES 56, 57.2, 57.4 AND 58 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 35) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y2462, FRAME 35 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 53.3) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK AT +Y2462, FRAME 53.3. FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FR 53.3, FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101, NEW SEAT TRACK REWORKED IAW DWG F53326701, ISSUE F, SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-68) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y1959, FRAMES 64 AND 68 FOUND CORRODED. CORROSION REMOVED SRM 51-74-00, FOUND EXCEEDED LIMIT IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11 .

Part: SEAT TRACK — CORRODED (FRAMES 42-46) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y1959 FRAMES 42, 45 AND 46 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED OUT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 39) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y2462, FRAMES 39, AND 39.1 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT RACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 19) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y1456 FRAME 19 FOUND CORRODED. CORROSION REMOVED SRM 51-74-00, FOUND EXCEED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 62-63) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK - Y953 FRAMES 62 AND 63 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102, NEW SEAT TRACK REWORKED IAW DWG F53477233, ISSUE A, SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y450 FRAMES 53.9 AND 54 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 59-62) · airframe 43,277 hrs · 5,759 cycles

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

Part: SEAT TRACK — CORRODED (FRAME 57) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y1959, FRAMES 57.1, 57.3 AND 57.4 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y450 FRAMES 37.1, 37.3 AND 37.4 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 56-58) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y450, FRAMES 56, 57, 57.2 AND 58 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEED LIMITS IAW SRM 353-00- 15, FIG 101. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-68) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y1959 FRAMES 64 AND 68 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMIT IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 54-58) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK + Y1959, FRAMES 57.1, 57.3 AND 58 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. NEW SEAT TRACK REWORKED IAW DWG F53326711, ISSUE A. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 69-70) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y450, FRAMES 69 AND 70 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMIT IAW SRM 53-00-15 FIG 102. SEAT TRACK REPLACED IAW SRM 51-42- 11.

Part: SEAT TRACK — CORRODED (FRAMES 59-60) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +450 FRAMES 59 AND 60 AND FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42- 11.

Part: SEAT TRACK — CORRODED (FRAMES 48-53) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y450, FRAMES 48, 50, 51 53 AND 53.1 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACEMENT CARRIED OUT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 53) · airframe 43,277 hrs · 5,759 cycles

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

Part: FLOOR SUPPORT — CORRODED (FRAME 73) · airframe 43,277 hrs · 5,759 cycles

FLOOR SUPPORT FRAME 73 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. FLOOR SUPPORT REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 75) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y1447.8 FRAME 75 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 38-39) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK Y450, FRAMES 38, 39, AND 39.2 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. NEW SEAT TRACK REWORKED DWG F53310898. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 73) · airframe 43,277 hrs · 5,759 cycles

FLOOR SUPPORT -Y1137.1, FRAME 73 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. FLOOR SUPPORT REPLACED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 75) · airframe 43,277 hrs · 5,759 cycles

FLOOR SUPPORT -Y1447.8, FRAME 75 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMIT IAW SRM 53-41-14, FIG 103. FLOOR SUPPORT REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 51-53) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK AT -Y1959, FRAMES 51, 52 AND 53.1 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101, SEAT TRACK REPLACEMENT CARRIED OUT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 80) · airframe 43,277 hrs · 5,759 cycles

FLOOR SUPPORT -Y450, FRAME 80 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103. FLOOR SUPPORT REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 40-45) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y450, FRAMES 40.2, 41, 42 AND 45 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 32-33) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y953 FRAME 32 AND 33 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102, SEAT TRACK REPLACED IAW SRM 51-42- 11.

Part: SEAT TRACK — CORRODED (FRAMES 59-60) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y1959, FRAMES 59 AND 60 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y450 FRAMES 37.1, 37.3 AND 37.4 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEED LIMITS SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 41-45) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y1959 FRAMES 41, 42 AND 45 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 73) · airframe 43,277 hrs · 5,759 cycles

FLOOR SUPPORT -YA FRAME 73 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-41-14, FIG 103. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 35-37) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y1959 FRAMES 35 AND 37 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00, -15 FIG, 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 73) · airframe 43,277 hrs · 5,759 cycles

FLOORBEAM FROM +YA TO +YB AT FRAME 73, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-41-14, FIG 103. REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 76) · airframe 43,277 hrs · 5,759 cycles

FLOOR SUPPORT -Y450, FRAME 76 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-41-14, FIG103. FLOOR SUPPORT REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 43-45) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK Y-953 FRAMES 43 AND 45 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 72) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK CORRODED FRAME 72. REMOVED CORROSION IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 57-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 69-70) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y450, FRAME 69 AND 70 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 32-33) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y1959, FRAMES 32 AND 33 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51- 42-11.

Part: SEAT TRACK — CORRODED (FRAMES 56-58) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y450 FRAMES 56, 57, 57.2 AND 58 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 80) · airframe 43,277 hrs · 5,759 cycles

FLOOR SUPPORT +Y450, FRAME 80 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-41-14, FIG 103. FLOOR SUPPORT REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y1552.5, FRAME 33 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEED LIMITS IAW AMM SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 64-65) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y2462, FRAMES 64 AND 65 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK FRAME 74 FOUND CORRODED. CORROSION REMOVED AS IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 38-39.2) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y450 FRAMES 38 AND 39.2 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101 NEW SEAT TRACK REWORKED IAW DWG F53310898 ISSUED. SEAT TRACK REPLACED IAW SRM 51-42 -11.

Part: SEAT TRACK — CORRODED (FRAME 54) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK Y1959, FRAME 54 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. NEW SEAT TRACK REWORKED IAW DWG F53326702, ISSUE F. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 18-19) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK + Y1456, FRAMES 18 AND 19 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102, NEW SEAT TRACK REWORKED IAW DWG F53272108, ISSUE G, SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 32-33) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK AT -Y1456, FRAMES 32 AND 33 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102, NEW SEAT TRACK REWORKED IAW DWG 53276406, ISSUE A, SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 52-53) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK, -Y953, FRAMES 52 AND 53.1 FOUND CORRODED. CORROSION REMOVED IAW 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACEMENT CARRIED OUT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 51-53) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y2462 FRAMES 51 AND 53.1 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15 FIG 101, SEAT TRACK REPLACEMENT CARRIED OUT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 50-53) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y1959, FRAMES 50, 51 AND 53 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEED LIMITS IAW SRM 53-31-15, FIG 101, SEAT TRACK REPLACEMENT CARRIED OUT IAW SRM 51- 42-11.

Part: SEAT TRACK — CORRODED (FRAMES 48-53) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK AT STA +Y450 FRAMES 48, 50, 51,52, 53 AND 53.1 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEED LIMITS IAW SRM 53- 31-15, FIG 101. SEAT TRACK REPLACEMENT CARRIED OUT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 53.9-54) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK Y450 FRAMES 53.9 AND 54 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 59-61) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y1959 FRAMES 59 AND 61 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 39-40) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y450 FRAMES 39.2 AND 40 FOUND CORRODED. CORROSIONS REMOVED, AND FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 40-46) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK -Y450, FRAMES 40.3, 41, 42, 45 AND 46 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y1959 FRAME 37.2 AND 37.3. FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102 NEW SEAT REWORKED IAW SWG F53278802, ISSUE A. SEAT TRACK REPLACED IAW SRM 52-42-11.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK +Y450, FRAME 73 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 73) · airframe 43,277 hrs · 5,759 cycles

FLOOR SUPPORT -Y794.3, FRAME 73 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 103 FLOOR SUPPORT REPLACED SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 35) · airframe 43,277 hrs · 5,759 cycles

SEAT TRACK + Y2462, FRAME 35 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEEDED LIMITS IAW SRM 53-00-15, FIG102. NEW SEAT TRACK REWORKED IAW DWG F53276408, ISSUE A, SEAT TRACK REPLACED IAW SRM 53-42-11.

Part: POWER SUPPLY — UNKNOWN (EMERGENCY LIGHTS) · airframe 42,533 hrs · 5,666 cycles

EPSU TEST FAILED, AFTER EPSU TEST, MESSAGE 335100 BAT/EPSU, 17WL, DOOR 4. PERFORMED LOCALIZED SYS TEST ON EPCU 17WL IAW AMM 33-51-00-740- 801, EPCU GIVES BATTERY FAILED. RECONNECTED PLU ON EPCU. PERFORMED LOCALIZED TEST AFTER 1 MIN, TEST OK. PERFORMED TEST EMERGENCY LIGHTS USING MCDU ACC AMM 33-51. NO FAULTS ACTIVE

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,188 hrs · 5,382 cycles

DURING CARD 2125-9402, ITEM H FOUND FAULT ON CIDS 1 EPSU OCR 119 WL/DEU 300RH14. TROUBLESHOT IAW TSM 33-51 NO POWER AT EPSU CEILING PANEL AT 19WL LT DOWN 393164. REPLACED FSPU IAW MM 33-51, CHECKED OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,376 hrs · 5,281 cycles

FOUND CEILING EMERGENCY LIGHT INOPERATIVE ON RT SIDE ROW 24. REPLACED EMERGENCY LIGHT ASSY IAW AMM 33-51-11, OP CHECKED OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 7,930 hrs · 1,033 cycles

EMERGENCY FLOOR PATH LIGHT FOUND INOPERATIVE AT SEAT 44H. RE-SECURED CONNECTOR AT 44H, OPS CHECK GOOD. ATL JAN 23 393148.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,458 hrs · 967 cycles

REMOVED DAMAGED SKIN INSTALLED REPAIR DOUBLER AND FILLER IAW A330 SRM 53-00-11, FIG 224.

Part: EPSU — FAULTED (EMERGENCY LIGHT) · airframe 31,521 hrs · 4,248 cycles

WHILE PERFORMING EMERGENCY LIGHT TEST FAULTED EPSU (12WL). REPLACED EPSU AND TESTS OK.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHT) · airframe 31,521 hrs · 4,248 cycles

WHILE PERFORMING EMERGENCY LIGHT TEST FAULTED BATTERY PACK EPSU (16WL), REPLACED BATTERY AND TESTS OK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,202 hrs · 3,927 cycles

DURING GROUND OPERATIONS FUSELAGE SKIN DAMAGED BETWEEN FR 27 & FR 28 AT S50L- S51R AND FR 31 AT S54L. TEMPORARY REPAIR ACCOMPLISHED PER ERA 486923-14 SECTION I, SECTION II REQUIRES FOLLOW UP NOT TO EXCEED 50 CYCLES FROM AIRCRAFT RETURN TO SERVICE.

Part: FAN — FAILED (RECIRCULATION) · airframe 27,519 hrs · 3,722 cycles

ENROUTE, CREW REPORTED A VERY STRONG ELECTRICAL ODOR IN CABIN AND STRONGEST AROUND ROWS 18-22 RT SIDE OF GALLEY. ALL PASSENGER SYS WAS TURNED OFF AND THE SMELL SUBSIDED. CREW FOLLOWED COM PROCEDURE AND CONTINUED FLIGHT TO WHERE LANDING WAS UNEVENTFUL. INSP REVEALED LT RECIRCULATION FAN CIRCUIT BREAKER POPPED. REPLACED LT RECIRCULATION FAN AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,334 hrs · 3,699 cycles

DURING DOOR 2L SLIDE CHANGE, FOUND EPSU 13WL FAULTED. REPLACED EPSU AT DOOR 2L AND FUNCTIONAL CHECK WAS NORMAL.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT -Y2462 FR30-FR37. REPLACED SEAT TRACK IAW ERA 479534-14 & 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y953 FR11-FR18. REPAIRED IAW ERA 479529-14 REV O.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR47 TO FR 53. REPLACED SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT -Y1959 FR40-FR47. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT -Y1959 FR37. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND SEAT TRACK -Y1959 AT FR47 TO 53 CORRODED. REPAIRED IAW SRM 53-31-15, & 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND SEAT TRACK -Y1959 AT FR55-58, WAS CORRODED. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND SEAT TRACK -Y2462, FR58 TO 62, WAS CORRODED. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK, FOUND SEAT TRACK -Y2462, AT FR47-53, WAS CORRODED. REPAIRED IAW SRM 51-42-11, AND SRM 53-31-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND SEAT TRACK -Y1959, AT FR18 TO 26, CORRODED. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — UNKNOWN (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND SEAT TRACK -Y1552, AT FR31 TO 34. REPAIRED IAW SRM 53-00-15, AND SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND SEAT TRACK -Y1959, AT FR58 TO 72, WAS CORRODED. REPAIRED IAW SRM 53-00-15.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT -Y450 FR 37-47. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

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

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 58-FR 72 . SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT -Y450 FR 55-FR 68. SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT -Y450 FR 68-FR 72 . SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 53-FR 55 . SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 40-FR 53 . SEAT TRACK REPLACED IAW SRM 51-42-11.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND Z-PROFILE CRACKED AT FR80 S26R. REPLACED IAW Z-PROFILE IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,138 hrs · 3,542 cycles

DURING "H" CHECK FOUND CRACKED FLOOR SUPPORT AT FR80 S26L. REPLACED Z-PROFILE IAW SRM 51-542-11.

Part: LIGHT — FAULTED (EVAC SLIDE) · airframe 25,499 hrs · 3,450 cycles

DOOR 4R SLIDE LIGHT FAULTED ON EMERGENCY LIGHT TEST. THE EVACUATION SLIDE WAS REPLACED AND CHECKS OK.

Part: BRAKE ASSY — FIRE (MLG) · airframe 17,997 hrs · 2,370 cycles

DURING AIRCRAFT ARRIVAL AT GATE, SMALL FLAMES WERE COMING FROM BRAKE POSITION NR 8. NO "ECAM" WARNING OR MESSAGES, NO EXCESSIVE BRAKE TEMPERATURE "(415 DEG C.)", FLIGHT CREW DID NOT REPORT ANY DISCREPANCIES. CARGO LOADERS CALLED CFR, FLAMES EXTINGUISHED BY ITSELF. WHEEL AND BRAKE INSPECTED AND FOUND FREE ROTATION AND NO HYDRAULIC LEAKS, CHECKED AXLE SLEEVE TO HAVE NO DAMAGE. FOUND A LOT OF GREASE ON THE OUTSIDE OF INNER WHEEL BEARING AND INNER WHEEL RIM HALF. CLEANED AND REMOVED EXCESSIVE GREASE AND CHECKED BEARINGS AND REINSTALLED WHEEL AND AIRCRAFT RETURNED TO SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 17,453 hrs · 2,219 cycles

DURING INSPECTION PER AD 2006-22-14, FOUND CRACKS IN LT WING RIB NR 6. REPAIRED PER EA 33-208521.

Part: RIB — CRACKED (RT WING) · airframe 17,453 hrs · 2,219 cycles

DURING INSPECTION PER AD 2006-22-14, FOUND CRACKS IN RT WING RIB NR 6. REPAIRED PER EA 33-208521.

Part: SLIDE — FAULTED (R2 DOOR) · airframe 13,266 hrs · 1,734 cycles

DURING TEST OF THE EMERGENCY LIGHT SYSTEM THE ESCAPE SLIDE LIGHT DOOR NR 4 RIGHT FAULTED. TROUBLE SHOT DOWN TO THE ESCAPE SLIDE. REMOVED AND REPLACED ESCAPE SLIDE AND TESTED OK.