N857NW

Part: SENSOR — FAULTED (ZONE 800) · airframe 84,718 hrs · 10,840 cycles

DIV- TO AMS DUE TO (DOOR R AFT CABIN) ECAM MESSAGE. CONFIRMED FAULT WITH DOOR INDICATING OPEN. REPLACED DOOR SENSORS 22MJ AND 24MJ. OK FOR SERVICE (8028253)

Part: WIRE — DAMAGED (ZONE 200) · airframe 84,311 hrs · 10,779 cycles

SEAT 34B EMERGENCY LIGHT INOP. REPLACED ASSY AND REPAIRED WIRING PER A330 AMM 33-51. (7982148)

Part: GIRT BAR — FOD (ZONE) · airframe 83,769 hrs · 10,716 cycles

2R DOOR WILL NOT ARM. CLEARED DIRT AND FOD FROM GIRT BAR AND LINKAGES. OPS CHECK GOOD. (7929210)

Part: OVEN — SPARKS (ZONE 900) · airframe 83,703 hrs · 10,707 cycles

DIVERTED INTO ACC DUE TO SPARKS AND SMOKE FROM MID GALLEY OVEN. INSTALLED A NEW OVEN. OPS CHECKED OK.

Part: GIRT BAR — FOD (ZONE 800) · airframe 83,093 hrs · 10,637 cycles

SHIP 3357 CREW REPORTS L2 DOOR WILL NOT ARM. CORRECTIVE ACTION: CLEANED DEBRIS OFF GIRT BAR. OPS CHECK GOOD. (7572978)

Part: FAIRING — DAMAGED (ZONE 500 FLAP) · airframe 82,873 hrs · 10,613 cycles

SHIP 3357 FOUND MULTIPLE PUNCTURE HOLES ON LEFT WING OUTBOARD FLAP BELOW WING LEFT OF #3 FLAP TRACK FAIRING. COMPLIED WITH ER/A 627962-14. (7582900).

Part: PROXIMITY SWITCH — OUT OF ADJUST (ZONE 800) · airframe 82,649 hrs · 10,587 cycles

SHIP 3357 DOOR L AFT CABIN ECAM MSG IN FLT. CORRECTIVE ACTION: ADJUSTED PROX SWITCHES PER A330 AMM 52-71. (1056802)

Part: SENSOR — OUT OF ADJUST (ZONE 800) · airframe 82,606 hrs · 10,582 cycles

SHIP 3357 4L DOOR SHOWS OPEN WITH DOOR CLOSED, CYCLE DOOR NO HELP. CORRECTIVE ACTION: FOUND SENSOR 23MJ OUT OF ADJUSTMENT. ADJUSTED 23MJ CKS OK, REF A330 AMM 52-71-11. OK FOR SERVICE. (7304990)

Part: SWITCH — FAULTED (ZONE 800) · airframe 82,577 hrs · 10,578 cycles

DIV - INTO BOS DUE TO (L) AFT DOOR OPEN INDICATION AT CRUISE. DEACTIVATED DOOR INDICATION AND FWD TO MEL. CONTINUE IN SERVICE. THEN R/R PSCU PER A330 AMM 52-71. OK FOR SERVICE.

Part: OXYGEN MASK — DISLODGED (ZONE 200) · airframe 82,104 hrs · 10,520 cycles

SHIP 3357 OXYGEN MASKS HAVE FALLEN OUT OF CONTAINER IN FWD LAV. CORRECTIVE ACTION: RESTOWED FWD LAV O2 MASKS PER A330 AMM 35-21. OK FOR SVC. (7562573)

Part: SKIN — GOUGED (ZONE 100) · airframe 82,104 hrs · 10,520 cycles

SHIP 3357 FORWARD FUSELAGE FOUND GOUGE ON FR35A-FR36, STGR 27L-28L. CORRECTIVE ACTION: COMPLIED WITH A330 SRM 53-21-11. OK TO CONTINUE. (0956968)

Part: WIRE — LOOSE (ZONE 200) · airframe 81,094 hrs · 10,386 cycles

SHIP 3357 FOUND SEATS 42JH, 43JH, 44JH, 47JH, AND 48AB EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: RESECURED LOOSE CONNECTIONS TO RESTORE EMERGENCY LIGHT FUNCTION. (6756588)

Part: GIRT BAR — FOD (ZONE 800) · airframe 80,037 hrs · 10,254 cycles

SHIP 3357 2R DOOR WILL NOT STAY ARMED. CORRECTIVE ACTION: CLEANED DEBRIS FROM GIRT BAR. OPS CHECK GOOD. (6353826)

Part: TRANSCEIVER — FAULTED (WX RADAR SYS) · airframe 78,494 hrs · 10,053 cycles

ATO - AT 15 KNOTS DUE TO A (NAV PRED W/S DET FAULT). FLIGHT CREW PLACED PREDICTIVE WINDSHEAR ON MEL. LHR PERFORMED BITE TEST OF WXR 1 AND 2 WITH NO FAULTS. CONTINUED ON MEL DUE TO PREVIOUS WXR2 FAULT. THEN R/R WX TRANSCEIVER 2 (1SQ2) PER A330 AMM 34-31. OK FOR SERVICE. MEL/PLAC REMOVED.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 77,428 hrs · 9,921 cycles

SHIP 3357 EEPL WHITE LIGHTS INOP AT POS 39AB, 35JH, 36JH AND 37JH. CORRECTIVE ACTION: RECONNECTED WIRES AT SEATS 35JH AND 37JH AND OPS CHK GOOD. 36JH AND 39AB. (5681797)

Part: FUEL LINE — CHAFED (APU) · airframe 77,210 hrs · 9,895 cycles

SHIP 3357 WITH APU BLEED "ON" STRONG OIL SMELL IN FLIGHT DECK. CORRECTIVE ACTION: REPLACED CHAFED FUEL LINE AND REPLACED RECIRC FILTERS. CLEANED APU COMPT AND DUCTS. OK FOR SERVICE. (0297760)

Part: FUEL LINE — CHAFED (APU) · airframe 77,210 hrs · 9,895 cycles

SHIP 3357 WITH APU BLEED "ON" STRONG OIL SMELL IN FLIGHT DECK. CORRECTIVE ACTION: REPLACED CHAFED FUEL LINE AND REPLACED RECIRC FILTERS. CLEANED APU COMPT AND DUCTS. OK FOR SERVICE. (5592998)

Part: BOTTLE — LOW PRESSURE (R3 DOOR) · airframe 77,193 hrs · 9,893 cycles

DOOR PRESSURE LOW AT R3 DOOR. SERVICED IAW AMM 52-15.

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 77,193 hrs · 9,893 cycles

R3 DOOR ASSIST BOTTLE IN YELLOW BAND. SERVICED PER A330 AMM 52-15. OK FOR SERVICE.

Part: DIAPHRAGM — FAULTED (R3 DOOR BOTTLE) · airframe 77,037 hrs · 9,874 cycles

SHIP 3357 3R DOOR- DOOR PRESSURE LOW MSG ON CIDS PANEL. AFTER ARMING DOORS. CORRECTIVE ACTION: R/R DIAPHRAGM ON PERCUSSION MECH OF DOOR DAMPER IAW A330 AMM 52- 20. SERVICED DOOR 3R DAMPER IAW A330 AMM 52-22. OPS AND LEAK CHECK GOOD. (5592906)

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 77,019 hrs · 9,872 cycles

SHIP 3357 3R DOOR ASSIST BOTTLE LOW. CORRECTIVE ACTION: SERVICED BOTTLE PER A330 AMM 52-15. OK FOR SERVICE, (5592902)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 76,981 hrs · 9,866 cycles

SHIP 3357 43B, 36H, 42H, 43H, 44H, SEAT MOUNTED EMERGENCY ESCAPE LIGHTS INOP. CORRECTIVE ACTION: REPAIRED SEAT EMERGENCY LIGHT CONNECTIONS AT LOCATIONS 43B, 36H, 42H, 43H, 44H, AND 34B REF A330 ESPM 20-20. ALL EMERGENCY LIGHTS OPS CHECK OKAY REF A330 AMM 33-51-12. (5538068)

Part: BOTTLE — LOW PRESSURE (R3 DOOR ASSIST) · airframe 76,938 hrs · 9,860 cycles

SHIP 3357 R3 DOOR ASSIST BOTTLE PRESSURE IN YELLOW. CORRECTIVE ACTION: SERVICED DOOR DAMPER PER A330 AMM 52-10. (5538051)

Part: STIFFENER — CORRODED (FRM 53.2 S49-50R) · airframe 76,580 hrs · 9,818 cycles

SHIP 3357 FUSELAGE / BULKHEADS / HORIZONTAL STIFFENERS / TEE AT FR53.2, BTWN STR49R-50R / CORROSION. CORRECTIVE ACTION: COMPLIED WITH ERA 611450-14 REV A CONTINUE ON MON. (0203171)

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 76,250 hrs · 9,768 cycles

SHIP 3357 WHITE ESCAPE PATH LIGHT INOP AT 36JH. CORRECTIVE ACTION: REMOVED AND REPLACED THE FLOOR PATH LIGHT ASSY AT SEAT 36JH AND REPAIRED WIRING PER A330 AMM 33-51. (5151144)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,785 hrs · 9,709 cycles

SHIP 3357 - ATB/DE - DUE TO AIR ENG 1 BLEED FAULT. CORRECTIVE ACTION: T/S. FOUND DEACTIVATION SCREW ON FAV LOOSE AND ORING DAMAGED. REPLACED FAV, PRSOV AND FAN AIR THERMOSTAT. (5151360)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,127 hrs · 9,624 cycles

SHIP 3357 FLT CREW REPORTS OVERHEAD EMERGENCY EXIT SIGNS HANGING DOWN DOOR 2R & 3R. CORRECTIVE ACTION: REPLACED BOTH EMERGENCY LIGHT ASSEMBLIES. (5010595)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,009 hrs · 9,608 cycles

SHIP 3357 DURING WALK AROUND FOUND #1 ENG INBOARD THRUST REVERSER BLOCKER DOOR CLOSE OUT MISSING, LOWER. CORRECTIVE ACTION: REPAIRED PER A330 AMM 78-32-25 INSTALLATION OF BLOCKER DOOR CLOSE OUT PANEL FAIRING. (5010514)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CRACK SUPPORT WEB BELLY FAIRING FR53.2 LH LATERAL SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON SUPPORT WEB BELLY FAIRING FR53.2 LH LATERAL SIDE AT LOWER FUSELAGE AS PER A330 SRM 53-35-14. (2952835)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE 260, AA 5716-01017, SB A330-57-3115 REV 02, AD 2019-16-07 CRACK DIRECTIONS ARE 6 OCLOCK AND 10 OCLOCK VIEW LOOKING AFT, DEPTH IS 0.149 INCH APPROX. ON RH SIDE. CORRECTIVE ACTION: ACCOMPLISHED ER/A 611088-14AD. ACCOMPLISHED REPAIR INSTRUCTIONS ON CENTER WING FRAME 40 BULKHEAD HOLE #260 RH SIDE AS PER ER/A 611088-14AD. (2948330)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE 263, AA 5716-01017, SB A330-57-3115 REV 02, AD 2019 -16-07 CRACK DIRECTIONS ARE 2 OCLOCK AND 6 OCLOCK VIEW LOOKING AFT, DEPTH IS 0.203 INCH APPROX. ON RH SIDE. CORRECTIVE ACTION: ACCOMPLISHED WITH ER/A 611088-14AD. ACCOMPLISHED REPAIR INSTRUCTIONS ON CENTER WING FRAME 40 BULKHEAD HOLE #263 RH SIDE. (2948365)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,380 hrs · 9,532 cycles

SHIP 3357 DURING FUNCTIONAL CHECK LANDING GEAR FREE FALL EXTENSION NLG DOORS NOT CLOSE. CORRECTIVE ACTION: PERFORMED TROUBLESHOOTING OF FREE FALL SYSTEM AND REPLACED FREE FALL ACTUATOR OF NLG. PERFORMED OPERATIONAL TEST. (2948147)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 DURING HCK AND INSPECTION PER EM 5716-01017, HOLE 260 RH WAS FOU ND CRACKED. A REPAIR WAS ACCOMPLISHED PER SECT I OF ERA 611088-14. CORRECTIVE ACTION: ACCOMPLISH THE SECT III INSPECTIONS OF DELTA ERA 611088-14 AT HOLE 260 RH. (2946454)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 DURING HCK AND INSPECTION PER EM 5716-01017, HOLE 263 RH WAS FOU ND CRACKED. A REPAIR WAS ACCOMPLISHED PER SECT II OF ERA 611088-14. CORRECTIVE ACTION: ACCOMPLISH THE SECT IV INSPECTIONS OF ERA 611088-14 AT HOLE 263 RH AT A THRESHOLD. (2946466)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION INTERNAL STRUCTURE ON REINFORCER PLATE AT LEVEL FR 53.2 AND BTW STR 49R TO STR 50R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 611450-14. VALIDATED ER/A 611450-14 MATCHES PRI 611450-14. PERFORM REPAIR ON INTERNAL STRUCTURE ON REINFORCER PLATE AT LEVEL FR 53.2 AND BTW STR 49R TO STR 50R IN AFT CARGO COMPARTMENT AS PER ER/A 611450-14. (2945386)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK Y1959 LOCATED FR31 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1959, BRACKETS (16E/A), SPLICE(4E/A) AND COUPLINGS (14E/A) LOC ON PASSENGER CABIN FR26/28 TO FR37.4. (2935077)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN FROM FRAMES FR30 TO FR31, AND BTW STR1L AND STR1R ON UPPER FUSELAGE. COMPLIED WITH PRI 610895-14, VALIDATE ER/A 610895-14 MATCHES WITH PRI 600895-14. EXISTING ALTERATION INSTALLED PER 2325-01059-03. INSTALLATION IS APPROVED BY STC ST09893AC. (2926336)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK RIB 6 AFT ON L H WING (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIRINSTALLED 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 ). (2926371)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK RIB 6 AFT ON R H WING (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIR INSTALLED PER EM 5720-01066-03B. REPAIR IS APPROVED PER AIRBUS REPAIR DRAWING R57257026 ACCORDING TO FAA AD 2006-22-14, PARA.(K). (2926364)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR LOWER SKIN SLAT 1 ON LH WING (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIR INSTALLED PER ER/A 594008-14. (2926346)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 84 STR2AL, FR84 STR2AR, FR84 STR5AL, FR84 STR5AR ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14 REV 0, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING MODIFICATION INSTALLED AS PER EM 5330-01151-05C. MODIFICATION IS APPROVED AS PER FAA AD 2015 23-06, PARA (J), (0)(1), (Q)(3)(II) AND AMOC 15-310. (2926370)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR INTERNAL SKIN AND 3 3 INCH FROM AFT LOWER EDGE IN AFT CARGO COMPARTMENT (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 525479-14. (2926348)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR ETERNAL SKIN AND 3 INCH ABOVE AFT LOWER EDGE IN FWD CARGO COMPARTMENT (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 572554-14. (2926353)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FLOOR STRUCTURE DOOR 1, DOOR 2, DOOR 3 AND DOOR 4; DOOR 4 VESTIBULE STRUCTURE, EMERGENCY HATCH STRUCTURE AND BCCR STRUCTURE IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTINGALTERATION INSTALLED PER 5320-01136, WORK SECTIONS 01 THROUGH -04,10,11 AND 12. INSTALLATION IS APPROVED BY STC ST02281SE. STC IS APPROVED FOR DAMAGE TOLERANCE IN ACCORDANCE WITH FAR 25.47 AND 25.571; ADDITIONALLY, ICA FOR THIS MODIFICATION IS APPROVED PER NAT DOCUMENT N0387-D70-1 AND IS BEING TRACKED PER AA 2520-01902. (2926342)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN FUSELAGE AT FR84, STR2A RH ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING MODIFICATION INSTALLED AS PER EM 5330-01151-05C. MODIFICATION IS APPROVED AS PER FAA AD 2015-23-06, PARA (J), (O)(1), (Q)(3)(II) AND AMOC 15-310, IN COMPLIANCE WITH SB A330-53-3160 R03. ADDITIONALLY, DEVIATIONS FOR SHORT EDGE MARGINS WEREAPPROVED AS PER 550531-14AD REV A BY MEANS OF AIRBUS RDAS 80212142/005/2016 ISSUE B. (2926323)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN FUSELAGE A T FR84, STR2A LH ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING MODIFICATION INSTALLED AS PER EM 5330-01151-05C. MODIFICATION IS APPROVED AS PER FAA AD 2015-23-06 , PARA (J),(O)(1), (Q)(3)(II)AND AMOC 15-310 , IN COMPLIANCE WITH SB A330-53-3160 R03. ADDITIONALLY DEVIATIONS FOR SHORT EDGE MARGINS WERE APPROVED AS PER 550530-14AD. (2926345)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN FR53 AND FR54 BTW STR1L AND STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 610895-14, VALIDATE ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING ALTERATION INSTALLED PER 2330-01325-01C. INSTALLATION IS APPROVED BY STCS ST03143CH-D AND ST03236CH. STCS ARE APPROVED FOR DAMAGE TOLERANCE IN ACCORDANCE WITH FAR 25.47 AND 25.571. (2926374)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR 4L OUTER SKIN LOWER AFT EDGE AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 505383-14. (2926312)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN FROM FRAMES FR26 TO FR26.1 AND BETWEEN STRINGERS 1R/1L ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 610895-14, VALIDATE ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING ALTERATION INSTALLED PER 2325-01059-01. (2926357)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 86 STR2BL, FR86 ST R2BR, FR86 STR5AL, FR86 STR5AR ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING MODIFICATION INSTALLED AS PER EM 5330-01151-05B. MODIFICATION IS APPROVED AS PER FAA AD 2015-23-06, PARA (J) , (O)(1),(Q)(3)(II) AND AMOC 15-310. (2926373)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR 4L OUTER SKIN LOWER AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIR INSTALLED PER A330 SRM 53-13-00, FIGURE 214, WHICH IS CURRENTLY A330 SRM 52-13-00-300-014. (2926318)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK Y1552.5 LOCATED FR31 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1552.5, COUPLINGS (12E/A), BRACKETS (12E/A) LOCATED FR31 TO FR37 IN PASSENGER CABIN. (2922876)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK -Y1959 LOCATED FR31 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1959, BRACKETS (28E/A), SPLICE(4E/A) AND COUPLINGS (14E/A) LOC ON PASSENGER CABIN FR26/28 TO FR37.4. (2922754)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK Y2462 LOCATED FR31 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK Y2462 LOC. BETWEEN FR26/28 TO FR37.4 IN PASSENGER CABIN SPLICES (4E/A), COUPLING (14E/A) AND BRACKETS (10E/A) ON SEAT TRACK Y2462. (2922983)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CRACK COUPLING LOCATED FR79 TO FR80 AT LEVEL STRINGER 26R AT AFT GALLE Y AREA. CORRECTIVE ACTION: REPLACED COUPLING LOCATED FR79 TO FR80 AT LEVEL STRINGER 26R AT AFT GALLEY AREA. (2922867)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK -Y450 LOCATED FR74 TO FR75 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y450 LOCATED FR74 TO FR75 AT AFT GALLEY AREA. (2915390)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CRACK PLATE LOCATED FR76 TO FR77 AT LEVEL STR26L AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED NEW WEB LOCATED FR76 TO FR77 AT LEVEL STR26L AT AFT GALLEY AREA. (2915387)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK Y953 LOCATED FR31 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK Y953 LOCATED FR31 TO FR37 IN PASSENGER CABIN. (2913815)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK -Y1552.5 LOCATED FR31 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1552.5 LOCATED FR31 TO FR37 IN PASSENGER CABIN. (2913820)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS EXISTING DOUBLER REPAIR DOOR 4L OUTER SKIN LOWER EDGE AT LOWER FUSELAGE. CORRECTIVE ACTION: ACCOMPLISHED DETAILED VISUAL VISUAL INSPECTION FOR EXISTING DOUBLER REPAIR LOC. DOOR 4L EXTERNAL SKIN LOWER EDGE AREA AND ENSUREDTHAT REPAIR FOUND ON AIRCRAFT MATCHES WITH DESCRIPTIONS DETAILED IN THE COMMENTS AND MEET ALL REQUIREMENTS AS PER A330 SRM52-13-00-300-014 AND ER/A # 610895-14. (2911659)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK Y450 LOCATED FR31 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK Y450, COUPLINGS (17E/A) AND BRACKETS(9E/A) AND FASTENERS LOCATED FR31 TO FR37.4 IN PASSENGER CABIN. (2909923)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK YC1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK YC1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. (2908537)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK YC1 LOCATED FR72 TO FR73 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED ADAPTER SEAT RAIL YC1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. (2908092)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK YA LOCATED FR73 AT AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED SEAT TRACK YA LOCATED FR73 AT AFT GALLEY AREA. (2903115)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 CORROSION SEAT TRACK YB1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. CORRECITVE ACTION: REPLACED SEAT TRACK YB1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. (2902101)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,343 hrs · 9,526 cycles

SHIP 3357 3L EMERGENCY EXIT LIGHT INOP. CORRECTIVE ACTION: FOUND LIGHT ASSY 25WL DIODE BLOWN. FOUND EPSU 15WL INTERNAL FAULT. R&R 15WL & 25WL. (4835388)

Part: NONE — NONE · airframe 72,395 hrs · 9,279 cycles

SHIP 3357 DOOR 2R WILL NOT ARM. CORRECTIVE ACTION: DEBRIS REMOVED DOOR. FUNCTIONED OPS OK. (4127610)

Part: NONE — NONE · airframe 72,395 hrs · 9,279 cycles

SHIP 3357 CREW REPORTS SMELL IN CABIN OVHD PANEL "AIR OVHT COND FANS RESET" FAULT LIGHT ON. CLASS 1 CABIN AIR EXTRACT FAN (245HU) ON SYS TEST. CORRECTIVE ACTION: REMOVED AND REPLACED CABIN AIR EXTRACT FAN. OPS CKS GOOD. OK FOR SVC. (4127600)

Part: NONE — NONE · airframe 70,745 hrs · 9,079 cycles

SHIP 3357 CREW REST FLIGHT ATTENDANT SIDE MISSING EXIT SIGN LENS COVER. CORRECTIVE ACTION: REMOVED AND REPLACED EXIT LIGHT SIGN IAW A330 AMM 33-51. (7294620)

Part: NONE — NONE · airframe 70,690 hrs · 9,071 cycles

SHIP 3357 EXIT LENS AT 2L DEGRADED. CORRECTIVE ACTION: REPLACED EXIT SIGN LENS AS REQUIRED. (2439062)

Part: NONE — NONE · airframe 70,690 hrs · 9,071 cycles

SHIP 3357 EQUIPMENT AND FURNISHINGS MANUAL NEEDS WORKSHEETS / 2L EXIT SIGN COVER DETACHED. CORRECTIVE ACTION: REPLENISHED EFM WORK SHEETS AS REQUIRED. (2438674)

Part: NONE — NONE · airframe 70,745 hrs · 9,079 cycles

'SUPPLAMENTAL INFOMATION' SHIP 3357 - MISC/DE - DUE TO SPOILER FAULT ON APPROACH. CORRECTIVE ACTION: R/R NO. 1 SPOILER ACTUATOR PER A330 AMM 27-64. (9220778)

Part: NONE — NONE · airframe 69,726 hrs · 8,943 cycles

SHIP 3357 WITH EMERGENCY LIGHT IN THE ARMED POSITION SOME OF THE EMERGENCY LIGHTS ARE ILLUMNITAED AND SOME ARE NOT. CORRECTIVE ACTION: RESECURED CONNECTOR ON 34H. FOUND 36 H LIGHT INOP. R&R EMERGENCY LIGHT IAW A330 AMM 33-51. (9305394)

Part: NONE — NONE · airframe 69,802 hrs · 8,954 cycles

SUPPLEMENTAL INFORMATION SHIP 3357 BURNING SMELL AFT GALLEY. WHEN TAPE HEATER CB'S WERE PULLED, SMELL STOPPED. CORRECTIVE ACTION: PERFORMED ADJUSTMENT OF THE POTENTIOMETERS. NO SMELL/SMOKE NOTED. TESTS GOOD . (9305380)

Part: NONE — NONE · airframe 69,436 hrs · 8,907 cycles

SUPPLEMENTAL INFORMATION SHIP 3357 FLOOR TRACK LIGHTING LEFT SIDE AISLE, LAST TWO ROWS IS LOOSE, NEEDS TO BE REATTACHED. CORRECTIVE ACTION: REPLACED DAMAGED HOUSING PER A330 AMM 33-51. (9242812)

Part: LIGHT — INOPERATIVE · airframe 69,153 hrs · 8,869 cycles

SHIP 3357 SEATS 38ABC RED EXIT LT INOP. CORRECTIVE ACTION: REPAIRED WIRING NEAR SEAT 38 ABC FLOOR DISCONNECT. (9265521)

Part: UNKNOWN — UNKNOWN · airframe 68,158 hrs · 8,734 cycles

SHIP 3357 EMER LIGHTS AT 43AB INOP. CORRECTIVE ACTION: RE-PINNED CONNECTOR AT 43AB IAW A330 ESPM 20-44. (8868033)

Part: UNKNOWN — UNKNOWN · airframe 68,158 hrs · 8,734 cycles

SHIP 3357 EMER LIGHTS AT 20AB INOP. CORRECTIVE ACTION: RE-PINNED CONNECTOR AT 20AB IAW A330 ESPM 20-44. (8868032)

Part: NONE — NONE · airframe 67,188 hrs · 8,568 cycles

SHIP 3357 - GEAR/ATB - DUE TO ECAM LGCIU 1 MESSAGE AND THREE RED LANDING GEAR UNLOCKED LIGHTS AFTER SELECTING LANDING GEAR UP. PERFORMED QRH & COMPUTER RESET WITH NO RESULTS. CORRECTIVE ACTION: REPLACED LGCIU #1 AND LANDING GEAR CONTROL UNIT. PERFORMED GEAR SWING WITH NO FAULTS. (8207185)

Part: NONE — NONE · airframe 67,020 hrs · 8,535 cycles

SHIP 3357 ON DESCENT 1R SLIDE DISARMED AND CHECK DOOR PRESSURE MESSAGE. CORRECTIVE ACTION: SERVICED #1RT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. (8338283)

Part: NONE — NONE · airframe 66,752 hrs · 8,474 cycles

SHIP 3357 38 C TO G O2 PANEL DOWN. CORRECTIVE ACTION: STOWED O2 PANEL PER AMM 35-21. (8349463)

Part: NONE — NONE · airframe 66,496 hrs · 8,426 cycles

SHIP 3357 FAULT EPSU 13WL IN PASSENGER CABIN 1EA. CORRECTIVE ACTION: REPLACED EPSU 13WL IN PASSENGER CABIN ASPER A330 AMM 33-51. (1957794)

Part: NONE — NONE · corrosion level 2 · airframe 66,496 hrs · 8,426 cycles

SHIP 3357 CORROSION SUPPORT STRUCTURE BELLY FAIRING LOCATED AT FR39.1 AND BETWEEN STR55L TO STR50R AT LOWER FUSELAGE. CORRECTIVE ACTION: REPLACED SUPPORT STRUCTURE BELLY FAIRING AS PER ER/A 593838-14. (1955973)

Part: NONE — NONE · airframe 66,496 hrs · 8,426 cycles

SHIP 3357 DENT EXTERNAL SKIN FR30 AND STR3R TO STR4R UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ER/A 593727-14. (1956498)

Part: NONE — NONE · airframe 66,496 hrs · 8,426 cycles

SHIP 3357 AIRCRAFT DAMAGED DUE TO CONTACT WITH GSE EQUIPMENT DENT ON LEADING EDGE OF SLAT 1 LH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOCATED ON EXTERNAL NOSE SKIN AT LEVEL OF RIB WFX865 ON SLAT#1 L/H WING AS PER ER/A 594008-14. (1955400)

Part: NONE — NONE · airframe 66,496 hrs · 8,426 cycles

SHIP 3357 ELONGATED HOLE ACCESS PANEL 453AR. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON ACCESS PANEL 453AR ON LH PYLON ASPER ER/A 594032-14. (1954186)

Part: NONE — NONE · airframe 66,496 hrs · 8,426 cycles

SHIP 3357 A DENT WAS FOUND ON THE FUSELAGE SKIN AND STRINGER AT FR30, STR 28L. CORRECTIVE ACTION: REF ERA 593817-14. (1951888)

Part: NONE — NONE · airframe 66,496 hrs · 8,426 cycles

SHIP 3357 A DENT WAS FOUND ON THE FUSELAGE SKIN AT FR32, STR 2RH. CORRECTIVE ACTION: REF 593727-14. (1951848)

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 66,076 hrs · 8,308 cycles

SHIP 3357 27JH OVERHEAD AISLE EMERGENCY LIGHT INOP. CORRECTIVE ACTION: FOUND WIRE LOOSE ON BACK OF UNIT. RESEATED WIRE. (7687355)

Part: NONE — NONE · airframe 66,496 hrs · 8,426 cycles

SHIP 3357 TIRE TIE BOLT FOUND IMPACTED & STUCK IN OVERWING PANEL, RH MLG BAY. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON R/H WING OVERWING FIXED T/E PANEL ASPER ER/A NO.590238-14. (6924323)

Part: SLIDE — INOPERATIVE (R1 DOOR) · airframe 65,902 hrs · 8,258 cycles

SHIP 3357 SLIDE AT D 1R INOPERATIVE. CORRECTIVE ACTION: DOOR SLIDE REPLACED AT DOOR 1R. (6924306).

Part: CIDS — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 63,157 hrs · 7,931 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. RESET CIDS, OPERATIONAL CHECK OK. LP 1206761

Part: LIGHT — DISCONNECTED (CABIN) · airframe 62,877 hrs · 7,895 cycles

EMERGENCY LIGHTS AT 29L AND 32R WERE FOUND INOPERATIVE. RECONNECTED LIGHTS AT SEAT DISCONNECT. LP6137654

Part: COVER — MISSING (TE FLAP) · airframe 60,680 hrs · 7,614 cycles

NBR 2 LEFT WING FLAP COVER MISSING. DEFERRED PER CDL 57-00-07 AND APPLIED SPEED TAPE UNTIL COVER AVAILABLE TO BE REPLACED. LP 5609138

Part: ACCESS PANEL — MISSING (LT WING) · airframe 61,107 hrs · 7,670 cycles

LEFT NR 4 FIXED FLAP TRACK FAIRING ACCESS PANEL 533BL MISSING. DEFERRED PER CDL 57-00-07 AND INSTALLED SPEED TAPE UNTIL COVER IS AVAILABLE TO INSTALL.

Part: COVER — MISSING (FLAP FAIRING) · airframe 60,400 hrs · 7,577 cycles

THE OUTBOARD FLAP NBR 2 FAIRING COVER MISSING. INSTALLED SPEED TAPE AND DEFERRED PER CDL 57-00-07, UNTIL ACCESS COVER IS REPLACED. LP5367675

Part: COVER — MISSING (FLAP FAIRING) · airframe 59,830 hrs · 7,505 cycles

RIGHT WING NR 2 FLAP FAIRING AFT HINGE COVER MISSING. COVERED AREA WITH SPEED TAPE PER CDL 57-00-07.

Part: SKIN — DENTED (CARGO DOOR) · airframe 59,706 hrs · 7,487 cycles

WHILE IN CHECK IN MSP, DAMAGE WAS FOUND ON THE OUTER SKIN ON THE AFT (LOWER CORNER) EDGE OF THE FWD CARGO DOOR. THE DENT IS LOCATED AT FR 25A JUST ABOVE BEAM 4 (REFERENCE 52-31-00-281-011 FIG 10117) IN THE EXCLUDED AREA. THERE IS ALSO DAMAGE TO THE EDGE MEMBER AT THE DENT LOCATION. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLER AND DOUBLERS PER ER/A 572554-14.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,358 hrs · 9,528 cycles

SHIP 3357 INSPECTION OF #1 LHS DOOR CORNER. CORRECTIVE ACTION: REF ER/A 572476-14AD. (0797591)

Part: RELEASE MECH — DETACHED (GIRT BAR) · airframe 56,211 hrs · 7,082 cycles

R2 DOOR SLIDE WOULD NOT ARM. FOUND QUICK RELEASE BAR DETACHED FROM GIRT BAR, REMOVED AND REPLACED SLIDE PACK IAW AMM 25-62.

Part: CIDS — MALFUNCTIONED (CABIN) · airframe 52,953 hrs · 6,745 cycles

EMERGENCY EXIT SIGNS AT DOOR 3L UNABLE TO EXTINGUISH. RESET CIDS ACC AIM 23-73-00-710.

Part: SEAT TRACK — CORRODED (FRAMES 35-37) · airframe 50,738 hrs · 6,531 cycles

DURING M CHECK, FOUND CORROSION ON MID CABIN FRAMES 35-37 Y1959 SEAT TRACK. REPLACED THE SEAT TRACK IAW SRM 53-00-15, 51-42-11, DRAWING F53276430, AND F53276421000.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 50,738 hrs · 6,531 cycles

DURING M CHECK, RIGHT WING FLAP TRACK DDS NR 2 WAS FOUND CORRODED. REPLACED NR 2 FLAP TRACK PER WORK CARD 2756-01000-01B AND AMM 27-54-57-000/400-801-A.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 50,738 hrs · 6,531 cycles

DURING M CHECK, LEFT WING FLAP TRACK DDS NR 3 WAS FOUND CORRODED. REPLACED NR 3 FLAP TRACK PER WORK CARD 2756-01000-01A.

Part: FLAP TRACK — CORRODED (TE FLAP) · airframe 50,738 hrs · 6,531 cycles

DURING M CHECK, RIGHT WING FLAP TRACK DDS NR 3 WAS FOUND CORRODED. REPLACED NR 3 FLAP TRACK PER WORK CARD 2756-01000-01B AND AMM 27-54-57-000/400-801-A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 50,738 hrs · 6,531 cycles

DURING M CHECK, CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE LONGITUDINAL AT FR 15A-18, -Y953. REPLACED SEAT TRACK PER DRAWINGS F53114437,F53114410,F53116745,F53111987,F5311 0720, F25310257,F53116751,F53111243,F53114695, F53114450 AND SRM 51-42-11 REV 91.

Part: SEAT TRACK — CORRODED (FRAMES 32-34) · airframe 50,738 hrs · 6,531 cycles

DURING AN M CHECK, FOUND SEAT TRACK CORRODED AT MID CABIN FRAMES 32-34, Y1552.5. REPLACED SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53275887.

Part: SEAT TRACK — CORRODED (FRAME 35) · airframe 50,738 hrs · 6,531 cycles

DURING AN M CHECK, THE SEAT TRACK WAS FOUND CORRODED AT MID CABIN FRAME 35, Y-2462. REPLACED THE SEAT TRACK IAW SRM 53-11-15.

Part: SEAT TRACK — CORRODED (FRAMES 32-34) · airframe 50,738 hrs · 6,531 cycles

DURING AM M CHECK, THE SEAT TRACK WAS CORRODED AT MID CABIN FRAMES 32-34, -Y1552.5. REPLACED THE SEAT TRACK IAW SRM 53-21-15 AND DRAWING F53275827.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 50,738 hrs · 6,531 cycles

DURING M CHECK, FOUND CORROSION IN AFT CABIN FRAMES 73-74, -YC1 SEAT TRACK. REPLACED THE SEAT TRACK IAW SRM, 51-42-11 REV. 91 AND DRAWING F53478007 AND F53478101.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,930 hrs · 6,224 cycles

DURING FLIGHT COMPARTMENT HFA CHECK, EMERGENCY LIGHT USING MDCU FAULTED, EPSU BATTERY 19WL. REPLACED 19WL BATTERY IAW AMM 33-51-38.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 44,332 hrs · 5,885 cycles

DOOR 3-R EMERGENCY BATTERY FAULT. R & R DOOR 3R EMERGENCY LIGHT BATTERY.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 42,375 hrs · 5,709 cycles

AFT CARGO DOOR INNER LOWER SURFACE FOUND CHAFED. CHAFE BLENDED OUT IAW SRM.

Part: SEAT TRACK — CORRODED (FRAME 57) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK -Y2462 FOUND CORRODED AT FRAME 57. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND EXCEED LIMIT IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 45-46) · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK Y450 FOUND CORRODED AT FRAMES 45-46. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 73) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

SEAT TRACK -Y1959 FOUND CORROSION AT FRAME 73. CORROSION REMOVED IAW SRM 51-74-0 AND FOUND OUT OF LIMITS SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 74) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK YC FOUND CORRODED AT FRAME 74 . CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM-00-15, FIG 102. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 17) · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACKY953 FOUND CORROSION AT FRAME 17. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-11-15, FIG 101. REPAIRED IAW ER/A 483241-14MA, REV ORIGNIAL.

Part: SEAT TRACK — CORRODED (FRAMES 70-71) · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK -Y450 FOUND CORRODED AT FRAMES 70 - 71. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 62-65) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK -Y450 FOUND CORRODED AT FRAMES 62 - 65. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 40-42) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK -Y1959 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 R & R IAW SRM.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK Y1456, FOUND CORRODED AT FRAME 17. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-11-15, FIG 101. REPAIRED IAW ER/A 483291-14MA, REV ORIGINAL.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 40,256 hrs · 5,454 cycles

DURING NON-ROUTINE CHECK, SEAT TRACK Y953 FOUND CORROSION AT FRAME 37.1. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK -YB FOUND CORRODED AT FRAME 74. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 54) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK Y450 FOUND CORRODED AT FRAME 54. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 74) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK FOUND CORRODED AT FRAME 74. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 63-65) · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 63-65. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53- 00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 78) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK FOUND CORRODED AT FRAME 78. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 36) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

-Y450 SEAT TRACK FOUND CORRODED AT FRAME 36. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 60-61) · airframe 40,256 hrs · 5,454 cycles

NON ROUTINE CHECK, -Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 60-61. CORROSION REMOVED IAW SRM 51-74-00, AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 59-60) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK -Y2462 FOUND CORRODED AT FRAMES 59-60. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (FRAMES 78-80) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, Y450 SEAT TRACK FOUND CORRODED AT FRAMES 78-80. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 53) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, Y1959 SEAT TRACK FOUND CORRODED AT FRAME 53.3. CORROSION REMOVED IAW SRM 51-74-00, AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 56-57) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK -Y1959 FOUND CORRODED AT FRAMES 56 - 57. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 53) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK -Y1959 FOUND CORRODED AT FRAME 53.3. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK FOUND CORRODED FRAME 73. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, Y450 SEAT TRACK FOUND CORRODED AT FRAMES 68-69. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53 -00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 66-69) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON-ROUTINE CHECK, - Y1959 SEAT TRACK FOUND CORRODED AT FRAMES 66 - 69. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 56-57) · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, Y450 SEAT TRACK FOUND CORRODED AT FRAMES 56-57. CORROSION REMOVED SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 31-33) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

Y1456 SEAT TRACK FOUND CORRODED AT FRAMES 31-33. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS SRM 53- 00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 57) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK Y1959 FOUND CORRODED AT FRAME 57. CORROSION REMOVED IAW SRM 51-74-0 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 74) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

NON ROUTINE CHECK, SEAT TRACK Y 1447.8 FOUND CORRODED FR 74. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 56-57) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

NON ROUTINE CHECK, -Y450 SEAT TRACK FOUND CORRODED AT FRAMES 56-57. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 53) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

-Y1959 SEAT TRACK FOUND CORRODED AT FRAME 53-53.1. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK, R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 75-76) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK Y400 FRAMES 75-76. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 60-63) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, SEAT TRACK Y450 FOUND CORRODEDN AT FRAMES 60-63. CORROSION REMOVED IAW SRM 51-74-00 AND AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 48-75) · airframe 40,256 hrs · 5,454 cycles

SEAT TRACK -Y400 FOUND CORRODED AT FRAMES 48-75. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 63-66) · airframe 40,256 hrs · 5,454 cycles

DURING NON ROUTINE CHECK, -Y2462 SEAT TRACK FOUND CORRODED AT FRAMES 63-66. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 76) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

DURING A NON ROUTINE CHECK, SEAT TRACK FOUND CORRODED AT FRAME 76. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 40,256 hrs · 5,454 cycles

Y1959 SEAT TRACK FOUND CORRODED AT FRAME 33. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 53-54) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

Y2462 SEAT TRACK FOUND CORRODED FRAMES 53.9 - 54. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 33) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

SEAT TRACK -Y1959 FOUND CORRODED AT FRAME 33. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 73) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

-Y2462 FLOOR SUPPORT FOUND CORRODED AT FRAME 73. FLOOR SUPPORT R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 43-45) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

CORROSION FOUND ON SEAT TRACK Y450, FRAMES 43 - 45. CORROSION REMOVED IAW SRM 51-74-00 . AND FOUND OUT OF LIMITS IAW SRM 51-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 33-36) · airframe 40,256 hrs · 5,454 cycles

-Y1552.5 SEAT TRACK FOUND CORRODED AT FRAMES 33-36. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 40,256 hrs · 5,454 cycles

-Y1456 SEAT TRACK FOUND CORRODED AT FRAME 33. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 39) · airframe 40,256 hrs · 5,454 cycles

-Y450 SEAT TRACK FOUND CORRODED AT FRAME 39.1. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 51-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 50-53) · airframe 40,256 hrs · 5,454 cycles

SEAT TRACK Y450 FOUND CORRODED AT FRAMES 50 - 53.1.

Part: SEAT TRACK — CORRODED (FRAME 53) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

SEAT TRACK Y953 FOUND CORRODED AT FRAME 53.

Part: SEAT TRACK — CORRODED (FRAMES 49-53) · corrosion level 2 · airframe 40,256 hrs · 5,454 cycles

SEAT TRACK -Y450 FOUND CORRODED AT FRAMES 49 - 53.1.

Part: SEAT TRACK — CORRODED (FRAME 53) · airframe 40,256 hrs · 5,454 cycles

SEAT TRACK -Y1959 FOUND CORRODED AT FRAME 53 - 53.1.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,731 hrs · 5,132 cycles

EPSU CAPACITY TEST FAILED. R & R BATTERY 11WL AT 1L DOOR. R & R BATTERIES IAW AMM 33-51.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 35,675 hrs · 4,855 cycles

EPSU TEST FAILED BATTERY (13L) DOOR 2L. REPLACED 13WL BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 7,872 hrs · 1,016 cycles

EMERGENCY LIGHT FAILED BATTERY TEST AT DOOR 1 RIGHT. REPLACED BATTERY PACK AT DOOR 1 RIGHT.

Part: BATTERY — FAILED (CABIN) · airframe 29,613 hrs · 4,140 cycles

BATTERY EPSU (11WL) DOOR 1L AND EPSU (17WL) DOOR 4L FAILED SYSTEM CHECK. REPLACED BATTERY AND TESTS OK.

Part: BATTERY — FAULTED (EMERGENCY LIGHT) · airframe 2,361 hrs · 305 cycles

DURING EMERGENCY LIGHT TEST, 11WL (EPSU) EMERGENCY POWER SUPPLY UNIT FAULTED, REPLACED BATTERY AND TESTS OK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

CORROSION ON SEAT-TRACK ZONE 220 -Y953 FR15 REMOVED AS PER SRM 51-74-00 MAT'L REMOVED 0.042" (L-1.5" W-0.5"). ORIGINAL THICKNESS MEASURED 0.180" AND FOUND OUT OF LIMIT AS PER SRM 53-11-15 FIG 101. REPAIR CARRIED OUT AS PER PRI 486601-14 REV 0.

Part: RIB — CRACKED (NR 2 PYLON) · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND NR 2 PYLON AFT LWR FAIRING (LAPF) INTERIOR RT FWD BULKHEAD FIRST RIB FROM FWD FOUND WEB CRACKED AS MARKED. PYLON NR 2 LOWER AFT PYLON FAIRING (LAPF) INTERIOR RT FWD BULKHEAD FIRST RIB FROM FWD WEB CRACK AREA REPAIR CARRIED OUT AS PER PRI 486996-14 REV 0.

Part: RIB — CRACKED (NR 1 PYLON) · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND NR 1 PYLON/ AFT FAIRING (454AL) LT FWD RIB FOUND LOWER LT CORNER WITH 01EA CRACKS AS MARKED PYLON NR 1 AFT FAIRING (454AL) LT FWD RIB CRACK AREA REPAIR CARRIED OUT AS PER PRI 486995-14 REVISION O.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND FLOOR STRUCTURE AT Y1959 FR17 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 MAT'L REMOVED 0.051" (L-2" W-1"). ORIGINAL THICKNESS MEASURED 0.080" AND FOUND OUT OF LIMIT AS PER SRM 53-11-14 FIG 101. REPAIR CARRIED OUT AS PER PRI 486602-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK AT Y450 FR56, FR57 AND FR58 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 ORIGINAL THK: 0.180", MATERIAL REMOVED 0.042", L-1.5", W=0.5" FOUND EXCEED LIMIT AS PER SRM 53-00-15 FIG 102 AND REPAIR CARRIED OUT AS PER PRI 486597-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y-1959 FR57-58 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 MAT'L REMOVED 0.043" (L-2" W-0.5"). ORIGINAL THICKNESS MEASURED 0.180" AND FOUND OUT OF LIMIT AS PER SRM 53-00-15 FIG 102. NEW SEAT-TRACK FABRICATED AND INSTALLED AS PER PRI 486597-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y-2462 FR55-56, FR57-58 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 FR55-FR56 MAT'L REMOVED 0.050" (L-2" W-0.5"), FR57-FR58 MAT'L REMOVED 0.047" (L-2" W-0.5"). ORIGINAL THICKNESS MEASURED 0.180" AND FOUND OUT OF LIMIT AS PER SRM 53-00-15 FIG 102. NEW SEAT-TRACK FABRICATED AND INSTALLED AS PER PRI 486597-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y450 FR41, FR44 AND FR46 CORRODED. REMOVED CORROSION AS PER SRM51-74-00 FR41 MAT'L REMOVED 0.048" (L-0.8" W-0.55" FR44 MAT'L REMOVED 0.051" (L-0.75" W-0.45"), FR46 MAT'L REMOVED 0.044" (L-0.9" W-0.5") AND FOUND OUT OF LIMIT AS PER SRM 53-31-15 FIG 101. NEW SEAT TRACK FABRICATED AND INSTALLED AS PER PRI 486597-14 REV 0.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND RT Z-PROFILE CRACKED ZONE 270 RT CRACKED Z-PROFILE. REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK AT Y450 FR60, FR63 AND FR66 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 FR60 MATERIAL REMOVED 0.040", L=2", W=1" FR63 MATERIAL REMOVED 0.040", L=2", W=1", FR66 MATERIAL REMOVED 0.032", L=2", W=1"ORIGINAL THK 0.120" FOUND EXCEED LIMIT AS PER SRM 51-31-15 FIG 101, SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y-450 FR39.1-39.2 CORROSION AT SEAT TRACK Y-450 FR39.1-39.2. REMOVED AS PER SRM 51-74-00 (EMMA). FR39.1-39.2 MATERIAL REMOVED 0.042", L=1.5", W=0. 5". ORIGINAL THK 0.180" FOUND EXCEEDED LIMIT AS PER SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND FLOOR SUPPORT STRUCTURE WEB AT Y1959 FR66 FOUND FASTENER HOLE CRACKED AT ZONE 260 FLOOR SUPPORT WEB STA Y1959 FR66. REMOVED AS PER SRM 51-42-11 (EMMA). NEW SHEAR WEB FABRICATED AND INSTALLED AS PER PRI 486997-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y953 FR18 CORRODED REMOVED AS PER SRM 51-74-00 FR18 MATERIAL REMOVED 0.040", L=2" W=0.5", ORIGINAL THK 0. 120" FOUND EXCEED LIMIT AS PER SRM 53-00-15 FIG 102 SEAT TRACK CUT BETWEEN FR15-15A AND REMOVED. NEW SEAT TRACK SEGMENT AND REPAIR SPLICE INSTALLED PER ER/A 483241-14MA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK YC1 CORRODED. REMOVED AS PER SRM 51-74-00 MATERIAL REMOVED 0.041", L=2" W=0.5", ORIGINAL THK 0.180", FOUND EXCEED LIMIT AS PER SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK AT Y-450 FR53.8, FR53.9 AND FR54 CORRODED. REMOVED AS PER SRM 51-74-00 (EMMA). MATERIAL REMOVED ON FR53.8, 0.040" L=1", W=0.5", FR53.9, MATERIAL REMOVED 0.042", L=1.5", W=0.5" FR54 MATERIAL REMOVED 0.038" L=1", W=0.5". ORIGINAL THK 0.120" FOUND EXCEED LIMIT AS PER SRM 51-31-15 FIG 101, SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK, FOUND SEAT TRACK Y-1959 FR65, FR68, AND FR71 CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FR65, MATERIAL REMOVED: 0.039", L=2", W=0.5". FR68 MATERIAL REMOVED: 0.038", L=2", W=0.5". FR71 MATERIAL REMOVED: 0.039", L=2", W=0.5". ORIGINAL THK: 0.120" FOUND EXCEED LIMIT IAW SRM 51-31-15. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — DAMAGED (ZONE 100) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK AT Y450, FR53.8, FR53.9 AND FR54 CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FR53.8 MAT'L REMOVED 0.037" (L=2" W=0.5") FR53.9 MAT'L REMOVED 0.037" (L=2" W=0.5") FR 54 MAT'L REMOVED 0.040" (L=2" W=0.5") ORIGINAL THICKNESS MEASURED 0.120" AND FOUND OUTOF LIMIT IAW SRM 53-31-15, FIG 101, DAMAGED SEAT-TRACK R & R NEW SEAT-TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK, FOUND SEAT TRACK AT Y-450 FR 60, FR 63 AND FR 66 CORRODED. REMOVED MATERIAL, REMOVED 0.035", L=1.0", W=0.5", FR66 MATERIAL REMOVED 0.040", L=1.0", W=0.5". ORIGINAL THK 0.120" FOUND EXCEED LIMIT IAW SRM 53-00-15, FIG 102 SEAT TRACK. R & R IAW SRM 51-42-11.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK, FOUND SEAT TRACK Y1959 FR65, FR68 AND FR71 CORRODED. CORROSION ON SEAT-TRACK ZONE 260 Y1959 REMOVED IAW SRM 51-74-00 FR65 MAT'L REMOVED 0.039" (L-1.5" W-0.5"), FR68 MAT'L REMOVED 0.037" (L-1.5" W-0.5"), FR71 MAT'L REMOVED 0.041" (L-2" W-0.5"). ORIGINAL THICKNESS MEASURED 0.180" AND FOUND OUT OF LIMIT IAW SRM 53-00-15 FIG 102 (EMMA). DAMAGED SEAT-TRACK R & R IAW PRI 486597-14, REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y-1959 FR33 CORRODED 1959. REMOVED AS PER SRM 51-74-00 MAT'L REMOVED 0.039" (L-2.5" W-0.5"). ORIGINAL THICKNESS MEASURED 0.180" AND FOUND OUT OF LIMIT AS PER SRM 53-00-15 FIG 102). REPAIR CARRIED OUT AS PER SRM 53-00-15 FIG 204 AND ERA 486605-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y-1959 FR45-46, FR46-47 CORRODED, REMOVED IAW SRM 51-74-00 FR45-46, MATERIAL REMOVED 0.041", L=2.5", W=0.5", FR46-47 MATERIAL. REMOVED 0.039", L=2", W=0.5". ORIGINAL THK 0.180" FOUND EXCEED LIMIT IAW SRM 51-31-15, FIG 101 (EMMA). SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y-2462 FR48, FR52-53 CORRODED. REMOVED AS PER SRM51-74-00 FR48 MATERIAL REMOVED 0.039", L=0.8", W=0.5"FR52-53 MATERIAL REMOVED 0.045", L=0.8", W=0.5". ORIGINA 0.180" FOUND EXCEED LIMIT AS PER SRM 51-31-15 FIG 101 SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK, FOUND CORROSION AT SEAT TRACK Y1959 FR48, FR51 AND FR53.1 REMOVED IAW SRM 51-74-00. FR48 MATERIAL REMOVED 0.047", L=0.75", W=0.5", FR51 MATERIAL REMOVED 0.044", L=0.6", W=0.46", FR53.1 MATERIAL REMOVED 0.049", L=0.75", W=0.43", ORIGINAL THK 0.180", FOUND EXCEED LIMIT IAW SRM 53-31-15 FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — WORN (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y1959 FR60-61, FR62 CORRODED ZONE 260. REMOVED CORROSION AS PER SRM 51-74 MAT'L, REMOVED 0.039" (L-1" W-0.5") FR62 MAT'L, REMOVED 0.039" (L-2" W-0.5"). ORIGINAL THICKNESS MEASURED 0.120" AND FOUND OUT OF LIMIT AS PER SRM 53-00-15 FIG 102. DAMAGED SEAT-TRACK REMOVED AND REPLACED NEW SEAT-TRACK AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

SEAT TRACK Y-450, FR41, FR44 AND FR 46 CORRODED IAW SRM 51-74-00, FR41 MATERIAL. REMOVED 0.042", L=0.60", W=0.5", FR44 MATERIAL REMOVED 0.044", L=0.7", W=0.45", FR46 MATERIAL REMOVED 0.045", L=0.65", W=0.5". ORIGINAL THK=0.180", FOUND EXCEED LIMIT IAW SRM 53-31-15, FIG 101. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND SEAT TRACK Y-450 FR48, FR50 AND FR53.1 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 FR48 MATERIAL REMOVED 0.048", L=0.75" W=0.5", FR50 MATERIAL REMOVED 0.052", L=0.9", W=0.45", FR53.1 MATERIAL REMOVED 0.050", L=0.82", W=0.55". ORIGINAL THK 0.180"FOUND EXCEED LIMIT IAW SRM 51-31-15, FIG 101 SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 56, FR 57 & FR 58. REPAIRED PER SRM 53-00-15 FIGURE 102, ERA 486597-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 53.3, FR 53.4, FR 53-5. REPAIRED PER SRM 51-74-00, SRM 53-31-15 FIGURE 101, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 55- FR 56, FR 57- FR 58. REPAIRED PER SRM 53-00-15, ERA 486597-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 58- FR 59, FR 59- FR 60 & FR 62. REPAIRED PER SRM 53-00-15 FIGURE 102, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 48, FR 50 & SR 53.1. REPAIRED PER SRM 53-31-15 FIGURE 101 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 36. REPAIRED PER SRM 53-00-15 FIGURE 102, SRM 53-00-15 FIGURE 204 & ERA 486606-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y953 FR 51 TO FR 53.1. REPAIRED PER SRM 51-74-00, SRM 53-31-15 FIGURE 1 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y953 FR 33, FR 35 & FR 36. REPAIRED PER SRM 53-00-15 FIGURE 204 & ERA 486994-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 48- FR 49, FR 50- FR 51. REPAIRED PER ERA 486597-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 33 TO FR 36. REPAIRED PER SRM 51-74-00, SRM 53-00-15 FIGURE 102 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y 1959 FR 33. REPAIRED PER SRM 53-00-15 FIGURE 102, ERA 486993-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1552 FR 33. REPAIRED PER SRM 53-00-15 FIGURE 102, ERA 486597-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 33. REPAIRED PER SRM 53-00-15 FIGURE 102, SRM 53-00-015 FIGURE 204 & ERA 486604-14 REV 0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1552 FR 33. REPAIRED PER SRM 53-00-15 FIGURE 102, ERA 486597-14 REV 0.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CRACK IN LEFT Z PROFILE IN ZONE 270. REPAIRED PER SRM 51-42-11 AND AA 5322-01022.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 54- FR 55. REPAIRED PER SRM 53-00-15 FIGURE 204 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 68 FR 71. REPAIRED PER SRM 51-74-00, SRM 53-00-15 FIGURE 204 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1456 FR 19. REPAIRED PER SRM 51-74-00, SRM 53-00-15 FIGURE 102 & SRM 51-42-11. REPLACEMENT FOR SDR DALA1033572901.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 72-FR 73. REPAIRED PER SRM 51-74-00, SRM 53-00-15 FIGURE 102 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR 72- FR 73. REPAIRED PER SRM 51-74-00, SRM 53-00-15 FIGURE 102 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 60-FR 62. REPAIRED PER SRM 51-74-00, SRM 53-00-15 FIGURE 102 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1456 FR 19. REPAIRED PER SRM 51-74-00, SRM 53-00-15 FIGURE 102 & SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR63- FR 68. REPAIRED PER SRM 51-42-11.

Part: SKIN — DENTED (CARGO DOOR) · airframe 26,270 hrs · 3,694 cycles

DURING H-CHECK, FOUND BULK CARGO DOOR EXTERIOR SKIN LWR AREA, FOUND DENT AS MARKED. BULK CARGO DOOR EXTERIOR SKIN LWR AREA , DENT MEASURED 1.5"LONG, 0.700" WIDE, DEPTH:0.050".REPAIR CARRIED OUT PER ERA 487004-14 REV 0 DATED 11 NOV 2010, 10:42HRS, AND IDENTIFIED REPAIR AS ENGINEERING APPROVED AND PERMANENT IAW PROCESS STANDARD 900-5-1 NR 4 AWAITING FINAL ER/A. PRI 487004-14 REV 0. COMPARED WITH ER/A 487004-14 REV 0 FOUND IN COMPLIANCE.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 24,159 hrs · 3,426 cycles

DURING TEST OF EPSU (15WL) AT DOOR 3 FAILED CAPACITY CHECK. MX REPLACED POWER SUPPLY UNIT AND BATTERY. OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 24,159 hrs · 3,426 cycles

DURING TEST OF EPSU (16WL) AT DOOR 3 FAILED CAPACITY CHECK. MX REPLACED POWER SUPPLY UNIT AND BATTERY. OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,159 hrs · 3,426 cycles

DURING TEST OF EPSU (18WL) AT DOOR 4 FAILED CAPACITY CHECK. MX REPLACED POWER SUPPLY UNIT AND BATTERY. OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: CONTROL PANEL — SMOKE (VIDEO SYSTEM) · airframe 23,548 hrs · 3,352 cycles

BURNING RUBBER ODOR IN CABIN, DEACTIVATED VIDEO CONTROL CTR IAW QRH SMOKE CABIN VIDEO SMOKE PROCEDURE, ODOR DISSIPATED AND LANDING WAS UNEVENTFUL. INSPECTED AND TESTED IFE AND NO BURNING ODOR DETECTED, ACFT CHECKS OK.