N851NW

Part: ELEC CONNECTOR — DAMAGED (ZONE 200) · airframe 85,550 hrs · 11,169 cycles

EMERGENCY PATH LIGHT SEAT 43J INOPERATIVE. REPAIRED CONNECTOR PER A330 AMM 33-51. OK FOR SERVICE. (7979274)

Part: FITTING — LACK OF LUBE (GIRT BAR) · airframe 85,591 hrs · 11,173 cycles

SHIP 3351 DOOR 3L WILL NOT ARM OR DISARM. LUBRICATED L3 GIRT FITTINGS REF A330 AMM 12-22. L3 ARM/ DISARM LEVER OPERATES SMOOTHLY. (1258707).

Part: GIRT BAR — FOD (ZONE 800) · airframe 85,534 hrs · 11,167 cycles

L3 DOOR WOULD NOT ARM. CLEANED DEBRIS FROM GIRT BAR. OPS GOOD. (7979254)

Part: LIGHT — DAMAGED (ZONE 200) · airframe 83,044 hrs · 10,871 cycles

SHIP 3351 42HJ EMERGENCY PATHWAY LIGHT HOUSING DAMAGED. CORRECTIVE ACTION: R/R EMERGENCY LIGHT HOUSING PER A330 CMM 25-21-56. OK FOR SVC. (0920770)

Part: SUBFRAME — CRACKED (ZONE 100) · airframe 82,570 hrs · 10,802 cycles

SHIP 3351 CRACK IN BELLY FAIRING LATERAL FRAME AT FR53.2. CORRECTIVE ACTION: COMPLIED WITH ERA 608483-14 REV A. (0874126)

Part: SKIN — NICKED (ZONE 100) · airframe 82,570 hrs · 10,802 cycles

SHIP 3351 NICK AT AFT CGO DOOR SURROUNDING SKIN AT 14" AFT FR65. 6" BELOW STGR 35RH. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-41-11. (0853762)

Part: DEU — FAULTED (ZONE 800) · airframe 81,678 hrs · 10,694 cycles

SHIP 3351 DOOR SLIDE MESSSAGE FOR 4L DOOR. CORRECTIVE ACTION: R/R DEU B PER A330 AMM 23-73-47.OPS CHECK GOOD. (6918252)

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 81,650 hrs · 10,687 cycles

SHIP 3351 4L DOOR ASSIST LOW. CORRECTIVE ACTION: SERVICED DOOR ASSIST BOTTLE PER A330 AMM 52-15. (0723087)

Part: GIRT BAR — FOD (ZONE 800) · airframe 81,549 hrs · 10,675 cycles

SHIP 3351 4R EMERGENCY EXIT DOOR SLIDE WILL NOT DISARM. CORRECTIVE ACTION: CLEANED FOD FROM GIRT BAR. OPS CHECK GOOD. (6918206)

Part: ELEC CONNECTOR — DISCONNECTED (ZONE 200) · airframe 80,737 hrs · 10,571 cycles

SHIP 3351 ROW 48AB, 49AB,50AB EMERGENCY LIGHTS NOT ILLUMINATING. CORRECTIVE ACTION: FOUND CONNECTOR AT ROW 50AB DISCONNECTED. RECONNECTED AS REQUIRED 48AB,49AB,50AB LIGHTS ILLUMINATE NORMAL. OKAY FOR SERVICE. (6628663)

Part: OXYGEN PANEL — LOOSE (ZONE 200) · airframe 80,430 hrs · 10,533 cycles

SHIP 3351 OXYGEN PANEL LOOSE / LOCATION:203. CORRECTIVE ACTION: REPACKED MASKS PER A330 AMM 35-23. OK FOR SERVICE. (0570088)

Part: RELIEF VALVE — FAULTED (HYD SYS) · airframe 80,361 hrs · 10,523 cycles

SHIP 3351 - MISC/DE - INTO ATL DUE TO MULTIPLE GREEN HYDRAULIC SYSTEM ECAM FAULTS. CORRECTIVE ACTION: REPLACED HSMU, PRESSURE RELIEF VALVE, DRAINED AND SERVICED HYDRAULIC SYSTEM, AND REPLACED WC2 WIRE HARNESS ON #1 ENG. OK FOR SERVICE.

Part: DOOR — UNSECURE (OXYGEN PANEL) · airframe 80,344 hrs · 10,521 cycles

SHIP 3351 O2 STORAGE DOOR PANEL FELL/SWUNG OPEN ABOVE 38 G. F. D. C. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (4008857)

Part: PANEL — LOOSE (ZONE 200) · airframe 79,902 hrs · 10,462 cycles

SHIP 3351 OXYGEN PANEL LOOSE / LOCATIONS:38C. CORRECTIVE ACTION: SECURED PANEL IAW A330 AMM 35-21. OK FOR SVC. (0501567)

Part: GROUND WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 79,468 hrs · 10,404 cycles

SHIP 3351 SEAT EMERGENCY LIGHTS @ SEATS 48,49, AND 50 INOP. CORRECTIVE ACTION: FOUND BROKEN GROUND WIRE @ SEAT 50, INSTALLED SPLICE PER A330 ESPM 20-43-11. OPS CHECK NML. (6042047)

Part: ARMING LEVER — BINDING (R4 DOOR) · airframe 79,032 hrs · 10,351 cycles

SHIP 3351 4R ENTRY DOOR ARMING LEVER HARD TO OPERATE. CORRECTIVE ACTION: FOUND DEBRIS JAMMED IN AFT DOOR FRAME GIRT BAR CLEAT. REMOVED, DOOR ARMS NORMALLY. OK FOR SERVICE PER A330 AMM 52-13. (0396925)

Part: DRAIN LINE — LEAKING (HYD SYSTEM) · airframe 79,032 hrs · 10,351 cycles

SHIP 3351 - MISC/DE - INTO LHR DUE TO THE LOSS OF THE YELLOW HYDRAULIC SYSTEM QUANTITY. CORRECTIVE ACTION: RESECURED CASE DRAIN LINE AND REPLACED ALL REQUIRED FILTERS. OPS AND LEAK CHECK GOOD. (5960586)

Part: LATCH — BROKEN (OXYGEN PANEL) · airframe 78,564 hrs · 10,293 cycles

SHIP 3351 OXYGEN PANEL LATCH BROKEN / LOCATIONS:202. CORRECTIVE ACTION: RESECURED LATCH AND RE-PACKED MASKS PER A330 AMM 35-23. (0338361)

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 78,323 hrs · 10,263 cycles

SEAT FLOOR PROXY LIGHTS INOP. REPAIRED WIRING HARNESS PER A330 AMM 33-52.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 77,830 hrs · 10,208 cycles

SHIP 3351 ROWS 48-50 A/B AISLE EMER LT INOP. CORRECTIVE ACTION: FOUND BROKEN WIRE AT SEAT 50A. REPAIRED WIRE PER A330 ESPM 20-43. CHECKS GOOD. (5404161)

Part: DOOR — STIFF (R4) · airframe 77,199 hrs · 10,126 cycles

SHIP 3351 4R DOOR HARD TO DISARM. CORRECTIVE ACTION: PERFORMED FUNCTIONAL CHECK OF 4R DOOR ARM AND DISARM. OPS CHECK GOOD. (0157011)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 77,130 hrs · 10,116 cycles

SHIP 3351 AFTER PARKING, COULD NOT DISARM DOOR 4R. CORRECTIVE ACTION: CYCLED DOOR ARMING COVER DISARM INDICATION NOW NORMAL. (8497126)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 77,060 hrs · 10,107 cycles

SHIP 3351 ROW 33-34 EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: FOUND CONNECTOR DAMAGED AT ROW 33 REPLACED CONNECTOR. (5547548)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 77,005 hrs · 10,102 cycles

SHIP 3351 4R DOOR REQUIRES NUMEROUS CYCLES IN ORDER TO DISARM SLIDE. CORRECTIVE ACTION: CYCLED DOOR - ALL CHECKS NORMAL. (5547526)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,473 hrs · 10,030 cycles

SHIP 3351 NO NOSE WHEEL STEERING PRIOR TO DEPARTURE. CORRECTIVE ACTION: PROPERLY INSTALLED HYDRAULIC HOSES OF THE NWS SERVO VALVE BLOCK. OPERATIONAL TEST PASS GOOD. (5098646)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,471 hrs · 10,029 cycles

SHIP 3351 RED EMER LIGHT AT SEAT 34B INOP. CORRECTIVE ACTION: T/S. FOUND WIRE BROKEN AT SEAT DISCONNECT CONNECTOR. REPLACED PIN AT CONNECTOR. (5098629)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,471 hrs · 10,029 cycles

SHIP 3351 WHITE EMER LIGHTS UNDER SEAT 33B, 34B, 41B, 42B, 43B INOP. CORRECTIVE ACTION: FOUND WIRE PULLED OUT AT SIDEWALL CONNECTOR AT SEAT 33B. RETERMINATED. 41,42,43 STILL INOP. OPERATED EMERGENCY LIGHTS FOUND SEAT 34B WORKING. T/S SEATS 41B, 42B AND 43B, FOUND BROKEN WIRE. REPAIRED WIRE. EMERGENCY LIGHTS AT SEATS 41B, 42B, AND 43B OPS CHECK GOOD. (5098628)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,471 hrs · 10,029 cycles

SHIP 3351 CEILING EMERGENCY LIGHT AT 3G INOP. CORRECTIVE ACTION: T/S. FOUND CONNECTOR OFF AT LIGHT 32WL. RECONNECTED CONNECTOR. (5098632)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,011 hrs · 9,972 cycles

SHIP 3351 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 5A. CRRECTIVE ACTION: REMOVED DEBRIS FROM SUITE 5A WASH LIGHT. (2990992)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,011 hrs · 9,972 cycles

SHIP 3351 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 8C. CORRECTIVE ACTION: REMOVED DEBRIS FROM SEAT 8C SUITE WASH LIGHT. (2990996)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,011 hrs · 9,972 cycles

SHIP 3351 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 6A. CORRECTIVE ACTION: REMOVED DEBRIS FROM SUITE 6A WASH LIGHT. (2990995)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,011 hrs · 9,972 cycles

SHIP 3351 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 4A. CORRECTIVE ACTION: REMOVED PAPER FROM SUITE 4A WASH LIGHT. (2990988)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,011 hrs · 9,972 cycles

SHIP 3351 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 9J. CORRECTIVE ACTION: REMOVED DEBRIS FROM SEAT 9J SUITE WASH LIGHT. (2990997)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 76,059 hrs · 9,978 cycles

SHIP 3351 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. LOCATIONS 5C. CORRECTIVE ACTION: DEFERRED. (2990993)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,993 hrs · 9,970 cycles

SHIP 3351 SLIDE BOTTLE PRESSURE INDICATION ON FAP INOP. CORRECTIVE ACTION: REPLACED THE FWD FAP (120RH). DOOR BOTTLE PRESSURE INDICATION ON FAP OPS CHECK GOOD. (4584538)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,993 hrs · 9,970 cycles

SHIP 3351 DOOR BOTTLE PRESSURE INDICATION ON FAP INOP (DOORS SLIDE). CORRECTIVE ACTION: REPLACED THE FWD FAP (120RH). DOOR BOTTLE PRESSURE INDICATION ON FAP OPS CHECK GOOD. (4584539)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,865 hrs · 9,954 cycles

SHIP 3351 302 FWD COAT CLOSET HAD ELECTRICAL BURNING SMELL AND SMOKE. CORRECTIVE ACTION: INVESTIGATION WAS DONE FOUND NO SMELL OR ANY SIGN OF ELECTRIC DAMAGE AROUND THE OML ALL THE WIRES ARE GOOD NO FAULT OR SMELL. CAN'T DUPLICATE FAULT. R&R OML. MCC REQUEST TO FURTHER INVESTIGATE. UPON FURTHER INVESTIGATION FOUND " HAND SANITIZER" IN BAG LEAKING IN CLOSET LOCATED ABOVE PANASONIC IFE OML DRIVE. CLEANED & RESEALED CLOSET MATINF SURFACE. RAN IFE SYSTEM FOR 40MIN WITHOUT FURTHER DEFECTS TO NOTE. (4584500)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,384 hrs · 9,896 cycles

SHIP 3351 FAP SHOWS LOW PRESSURE DOOR 2L. CORRECTIVE ACTION: RESET CIDS RAN BITE TEST, BITE TEST GOOD. CYCLED DOOR MULTIPLE TIMES, CANT DUPLICATE FAULT. R&R DEU (300RH3). (4390816)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 75,303 hrs · 9,886 cycles

SHIP 3351 ENTRY DOOR HARD TO OPEN OR CLOSE. LOCATIONS 606. CORRECTIVE ACTION: REMOVED DEBRIS AND LUBRICATED GUST LOCK BUTTON. (2909221)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,900 hrs · 9,836 cycles

SHIP 3351 DURING W/A ON A/C ARRIVAL NOTICED THA EXCESSIVE SMOKECOMES OUT OF APU'S EXHAUST. CORRECTIVE ACTION: PERFORMED APU R/R. (4932846)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DONT PASS OPERATIONAL TEST EPSU-EMERGENCY POWER SUPPLY UNIT POSITION 19WL IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED EPSU (19WL). (2789304)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DONT PASS OPERATIONAL TEST EPSU-EMERGENCY POWER SUPPLY UNIT POSITION 16WL. CORRECTIVE ACTION: REPLACED EPSU (16WL). (2789341)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER P ANEL AT HOLE 263 RH SIDE AA 5716-01017, SB A330-57-3115 REV 02, AD 201 9-16-07. CORRECTIVE ACTION: REF ER/A 608202-14AD. (2788933)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CRACK SUPPORT WEB BELLY FAIRING LOC. ON FR53.2 L/H SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REF ER/A 608483-14. (2787995)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 EROSION ACCESS PANEL 575BB AROUND HOLE ON LH WING. CORRECTIVE ACTION: EVALUATED ACCESS PANEL 575BB AND FOUND OUT ALLOWABLE DAMAGE LIMITS AS PER A330 SRM 57-53-37-283-001. ER/A 608664-14 NO LONGER REQUIRED DUE TO ACCESS PANEL HAS BEEN REPLACED. THE ACCESS PANEL HAS BEEN REPLACED AND INSTALLATION PROCEDURES WAS COMPLETED. (2788875)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CRACK FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER P ANEL AT HOLE H260 RH SIDE. CORECTIVE ACTION: COMPLIED WITH PRI 608202-14AD, VALIDATED ER/A 608202-14AD MATCHES WITH PRI 608202-14AD. (2788927)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 INTRODUCTION: DURING H CHECK, WHILE EXECUTION OF JIC 5322-2006 REGARDING THE INSPECTION OF MID AND FWD CABIN FLOOR STRUCTURE, CORROSION WAS FOUND AT THE SEAT TRACKS -Y1959 AND +Y1959 PN F53276430200 M/F ABS5080A536. THE PARTS ARE OUT OF A330 SRM 53-00-15-283-001 LIMITS AND MUST BE REPLACED. AS PER A330 SRM 53-21-15-02A, SEAT TRACK PN F53276430202 CAN BE USED AS SPARE, BUT THERE IS AN ISSUE ABOUT TWO HOLES BETWEEN FR37.1-37.2 AND TWO HOLES BETWEEN 37.2-37.3 THAT ATTACH THE COVER PLATE F53979638200 ON EACH SIDE (-Y1959 AND +Y1959). THE SEAT TRACK PN F53276430202 DOES NOT HAVE THE HOLES TO ATTACH THESE COVER PLATES. CORRECTIVE ACTION: REF ER/A 608907-14. (2788000)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF EM 5330-01152-03B FOUND FASTENERS THAT INTERF ERENCE WITH THE COLLAR OF FASTENERS COMMON TO THE SKIN/ ANGLE JOINT ON FR 86 BTW STR 5A TO 15 RH. CORRECTIVE ACTION: COMPLIED WITH PRI 609094-14AD, VALIDATED ER/A 609094-14AD MATCHES PRI 609094-14AD. (2787459)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF EM 5330-01152-03A FOUND FASTENERS THAT INTERFERENCE WITH THE COLLAR OF FASTENERS COMMON TO THE SKIN/ ANGLE JOINT ON FR 86 BTW STR 5A TO 15 LH. CORRECTIVE ACTION: REF ER/A 608932-14AD. (2787479)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF EM 5330-01152-03B FOUND FASTENERS THAT INTERFERENCE WITH THE COLLAR OF FASTENERS COMMON TO THE SKIN/ ANGLE JOINT ON FR 87 BTW STR 5A TO 15 RH. CORRECTIVE ACTION: COMPLIED WITH PRI 609094-14AD, VALIDATED ER/A 609094-14AD MATCHES PRI 609094-14AD. (2787454)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF EM 5330-01152-02B FOUND FASTENERS THAT INTERFERENCE WITH THE COLLAR OF FASTENERS COMMON TO THE SKIN/ANGLE JOINT ON FR84 BTW STR5A TO STR15 RH. CORRECTIVE ACTION: REF ER/A 609094-14AD. (2787470)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF EM 5330-01152-02B FOUND FASTENERS THAT INTERF ERENCE WITH THE COLLAR OF FASTENERS COMMON TO THE SKIN/ ANGLE JOINT ON FR 85 BTW STR 5A TO 15 RH. CORRECTIVE ACTION: COMPLIED WITH PRI 609094-14AD, VALIDATED ER/A 609094-14AD MATCHES PRI 609094-14AD. (2787473)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF EM 5330-01152-02A FOUND FASTENERS THAT INTERFERENCE WITH THE COLLAR OF FASTENERS COMMON TO THE SKIN/ ANGLE JOINT ON FR 85 BTW STR 5A TO 15 LH. CORRECTIVE ACTION: REF ER/A 608932-14AD. (2787491)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 VA 101000 TO BE ACCOMPLISHED SIMULTANEOUSLY WITH EM 5330-01152. CORRECTIVE ACTION: ACCOMPLISHED AS PER VA 101000 AND ACCOMPLISHED SIMULTANEOUSLY WITH EM 5330-01152. (2787148)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF EM 5330-01152-03A FOUND FASTENERS THAT INTERF ERENCE WITH THE COLLAR OF FASTENERS COMMON TO THE SKIN/ ANGLE JOINT ON FR 87 BTW STR 5A TO 15 LH. CORRECTIVE ACTION: COMPLIED WITH PRI 608932-14AD, VALIDATED ER/A 608932-14AD MATCHES PRI 608932-14AD. (2787495)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF EM 5330-01152-02A FOUND FASTENERS THAT INTERFERENCE WITH THE COLLAR OF FASTENERS COMMON TO THE SKIN/ ANGLE JOINT ON FR 84 BTW STR 5A TO 15 LH. CORRECTIVE ACTION: COMPLIED WITH PRI 608932-14AD, VALIDATED ER/A 608932-14AD MATCHES PRI 608932-14AD. (2787482)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 56R SPLICE BTW FR60 TO FR64 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: ACCOMPLISHED DVI ON AREA LOC STR 56R BTW FR60 TO FR64 IN AFT CARGO COMPARTMENT AND NOT FOUND SIGN OF DEGRADATION (CRACKS, CORROSION, PULLED FASTENERS OR DENTS) AND ACCOMPLISHED GENERAL VISUAL INSPECTION ON STR 56R BTW FR60 AND FR64 AREA AND REPAIR WAS NOT FOUND IN THE AIRCRAFT STRUCTURE THEREFORE DOES NOT MATCHES WITH THE DESCRIPTION DETAILED ON ER/A561284-14 AND MASTER ER/A 608134-14. (REPAIR IS NOT PRESENT ON AIRCRAFT) ENGINEERING WAS CONTACTED AND AFTER ASSESSMENT OF THE REPORTED DATA ITEM #24 OF MASTER ER/A 608134-14 PRI REV 0 WAS ELIMINATED AND IS NOT MORE INCLUDED ON THE NEW MASTER ER/A 608134-14. (2784931)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR PASSENGER CREW DOOR L4 AFT LOWER CORNER IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER A330 SRM 52-13-00-300-013, WHICH IS A CAT B REPAIR. DELTA LP 4059486 IS ALREADY TRACKING SUPPLEMENTAL INSPECTIONS; HOWEVER, THE INCORRECT REFERENCE WAS REGISTERED. SINCE REPAIR WAS PERFORMED AS PER A330 SRM 52-13-00-300-013, LP 4059486 IS UPDATED TO TRACK INSPECTIONS AS PER THE CORRECT REFERENCE A330 SRM 52-13-00-205-13. (2784927)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 54R SPLICE BTW FR60 TO FR64 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14 REV 0, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLEDPER DELTA ER/A 561284-14, APPROVED PER AIRBUS RDAS. (2784131)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL AREA DOUBLER INSTALLED FR86, STR2BL IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. DEVIATIONS FOR SHORT EDGE MARGINS TO MODIFICATION AS PER EM 5330- 01151-05B ARE INSTALLED PER DELTA ERA 544195-14AD. (2784527)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR53 TO FR5 4 BTW STR1L TO STR1R ON UPPER FUSELAGE. COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING ALTERATION INSTALLED PER 2330-01325-01C. INSTALLATION IS APPROVED BY STC ST03143CH-D AND ST03236CH. (2784331)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR 1, DOOR 2, DOOR 3 AND DOOR 4 FLOOR STRUCTURE; DOOR 4 VESTIBULE STRUCTURE, EMERGENCY HATCH STRUCTURE AND BCCR STRUCTURE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING ALTERATION INSTALLED PER 5320-01136. INSTALLATION IS APPROVED BY STC ST02281SE. (2784339)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 51R SPLICE BTW FR60 TO FR64 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 561284-14, APPROVED PER AIRBUS RDAS. (2784142)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL AREA DOUBLER INSTALLED FR84, STR2AL IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14. VALIDATED ER/A 608134-14 REV ORIGINAL MATCHES PRI 608134-14. EXISTING MODIFICATION INSTALLED PER EM 5330-01151-05C. MODIFICATION IS APPROVED AS PER FAA AD 2015-23-06 IN COMPLIANCE WITH SB A330-53-3160 R03. ADDITIONALLY, DEVIATIONS FOR SHORT EDGE MARGINS WERE APPROVED AS PER DELTA ERA 544202-14AD. (2784573)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 55R SPLICE BTW FR60 TO FR64 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLEDPER DELTA ER/A 561284-14, APPROVED PER AIRBUS RDAS. (2784132)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR30 TO FR3 1 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING ALTERATIONINSTALLED PER 2325-01059-03. INSTALLATION IS APPROVED BY STC ST09893AC. (2784338)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 62 SPLICE LOCATE 56R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 561151-14, APPROVED PER AIRBUS RDAS. (2784138)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 53R SPLICE BTW FR60 TO FR64 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 561284-14, APPROVED PER AIRBUS RDAS. (2784244)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR19 TO FR20 BTW STR 49R TO STR51R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 608134-14. EXISTING REPAIR INSTALLED PER A330 SRM 53-21-11 PARA. 5.C FIGURE 204, WHICH IS CURRENTLY A330 SRM 53-21-11-300-015. (2784595)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR26 TO FR26.1 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING ALTERATION INSTALLED PER 2325-01059-01. INSTALLATION IS APPROVED BY STC ST09893AC. (2784314)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SLAT 5 EXTERNAL SKIN ON LH WING. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 586030-14. APPROVED PER AIB RDAS WITH NO SUPPLEMENTAL INSPECTIONS REQUIRED. JOB COMPLETE. (2784588)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 0 TO FR1 LH SIDE STRINGER AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 504502-14. (2784584)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 47R SPLICE BTW FR57/FR58 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 502642-14. (2784618)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SLAT 3 EXTERNAL SKIN ON RH WING. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER A330 SRM 57-40-00 PARA 5.C FIGURE 203, WHICH IS CURRENTLY A330 SRM 57-40-00-300-008. AS PER A330 SRM 57-40-00-300-008, REPAIR IS CONSIDERED AS CAT A. (2784605)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 50R SPLICE LOCATED FR59 TO FR62 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 561284-14, APPROVED PER AIRBUS RDAS. (2784146)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL AREA DOUBLER INSTALLED FR86, STR 2BR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. DEVIATIONS FOR SHORT EDGE MARGINS TO MODIFICATION AS PER EM 5330- 01151-05B ARE INSTALLED PER DELTA ERA 544196-14AD. APPROVAL IS BY MEANS OF INSTRUCTIONS ALREADY CONSIDERED IN AIRBUS SB. (2784563)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL AREA DOUBLER INSTALLED FR84, STR2AR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING MODIFICATION INSTALLED AS PER EM 5330-01151-05C. MODIFICATION IS APPROVED AS PER FAA AD 2015-23-06. IN COMPLIANCE WITH SB. ADDITIONALLY, DEVIATIONS FOR SHORT EDGE MARGINS WERE APPROVED AS PER DELTA ERA 544203-14AD BY MEANS OF AIRBUS RDAS. (2784543)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL AREA DOUBLER INSTALLED FR84, STR2AL, FR84, STR 2AR, FR84, STR 5AL, FR84, STR 5AR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING MODIFICATION INSTALLED IS APPROVED AS PER FAA AD. IN COMPLIANCE WITH SB. (2784535)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC FR57 TO FR58 AND STR47R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 502642-14, APPROVED AS CAT B PER AIRBUS RDAS. (2784549)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK RIB 6 AFT ON LH WING. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER EM 5720-01066-04A. REPAIR IS APPROVED PER SB A330-57-3088 R02 ACCORDING TO FAA AD 2006-22-14. EM5720-01066-04A TERMINATE INSPECTION AND MODIFICATION REQUIREMENTS. (2784324)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 52R SPLICE BTW FR59 TO FR64 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 REV ORIGINAL MATCHES PRI 608134-14. EXISTING REPAIR INSTALLEDPER DELTA ER/A 561284-14, APPROVED PER AIRBUS RDAS. (2784136)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC FR79 TO FR80 BTW STR31R /STR34R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 479795-14. (2784600)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC FR61 TO FR63 BTW STR50R TO STR56R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 561221-14. (2784554)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR30, STR27L AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA 520211-14 (2784548)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK RIB6 AFT ON RH WING. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER EM 5720-01066-04B. REPAIR IS APPROVED PER SB A330-57-3088 R02 ACCORDING TO FAA AD 2006-22-14. (2784264)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL AREA DOUBLER INSTALLED FR86, STR2BL, FR86, STR2BR, FR86, STR5AL, FR86, STR5AR IN UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14. EXISTING MODIFICATION INSTALLED PER EM 5330-01151-05B. MODIFICATION IS APPROVED AS PER FAA AD 2015-23-06, IN COMPLIANCE WITH SB A330-53-3160 R03. (2784537)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 61 SPLICE LOCATED STR55R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 608134-14, VALIDATED ER/A 608134-14 MATCHES PRI 608134-14. EXISTING REPAIR INSTALLED PER DELTA ER/A 561151-14, APPROVED PER AIRBUS RDAS. (2784151)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING HCK AT AEROMAN (SAL) AND ACCOMPLISHMENT OF EM 5330-01152, SEVERAL FASTENERS AT FR 84R, 85R, 86R, AND 87R REINFORCEMENT AN GLES COULD NOT BE INSTALLED. CORRECTIVE ACTION: REF ER/A 609094-14AD. (2782735)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING HCK AT AEROMAN (SAL) AND ACCOMPLISHMENT OF EM 5330-01152, SEVERAL FASTENERS AT FR84L, FR85L, FR 86L, AND FR 87L REINFORCE MENT ANGLES COULD NOT BE INSTALLD PER EM. DELTA ERA 608932-14AD WAS WRITTEN TO ALLOW FASTENER INSTALLATION. CORRECTIVE ACTION: REF ERA 608932-14AD. (2781002)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DONT PASS TEST OF DOOR DAMPING AT PASSENGER CREW DOOR 3R. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR DAMPER AT PASSENGER CREW DOOR 3R. (2779456)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DONT PASS TEST OF DOOR DAMPING AT PASSENGER CREW DOOR 3L. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR DAMPER AT PASSENGER CREW DOOR 3L. (2779464)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM -Y2462 LOCATED FR31 TO FR37 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON FLOOR BEAM -Y2462 LOCATED BTW FR 31 TO FR 37 RH SIDE ON PASSENGER CABIN. SEAT SECTION AND SPLICES (4 EA) WAS MACHINED AND DOCUMENTED. RII INSPECTION COMPLETE. (2772040)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM +Y2462 LOCATED FR31 TO FR37 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON FLOOR BEAM Y2462 LOC BETWEEN FR32 TO FR37 LH SIDE ON PASSENGER CABIN AS PER A330 SRM 53-00-15-300-004. RII INSPECTION COMPLETE. (2761046)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 REMOVE AND REPLACE FLOOR BEAM -Y450 LOCATED FR31 TO FR37 RH SIDE IN PASSENGER CABIN DUE TO MISSDRILLED HOLES FOUND. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y450 LOC. BTW FR26 TO FR37.4 IN PASSENGER CABIN AS PER A330 SRM 51-72-11-911-001. RII INSPECTION COMPLETE. (2760152)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM +Y1959 LOCATED FR31 TO FR37 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PLUS Y1959 LOC. FR 26 TO FR 37.4 IN PASSENGERS CABIN. RII INSPECTION COMPLETE. (2756894)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM -Y1959 LOCATED FR31 TO FR37 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1959 LOC. FR31 TO FR37 RH SIDE IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2756369)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM YC1 LOCATED FR72 TO FR73 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM YC1 LOCATED FR72 TO FR73 AT AFT GALLEY AREA. RII INSPECTION COMPLETE. (2746552)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM YB1 LOCATED FR72 TO FR73 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM YB1 LOCATED FR72 TO FR73 AT AFT GALLEY AREA. RII INSPECTION COMPLETE. (2746557)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM YB1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM YB1 LOCATED ON FR73 TO FR74 AFT GALLEY AREA. RII INSPECTION COMPLETE. (2746545)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHI 3351 CORROSION FLOOR BEAM YC1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM YC1 LOCATED FR73 TO FR74 AT AFT GALLEY AREA AND APPLIED CIC ON FLOOR BEAM YC1. RII INSPECTION COMPLETE. (2746522)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM YB LOCATED FR73 TO FR74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM YB LOCATED FR73 TO FR74 AT AFT GALLEY AREA. RII INSPECTION COMPLETE. (2745263)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM -Y450 LOCATED FR31 TO FR37 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y450 LOC. FR31 TO FR37 RH SIDE IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2743747)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CORROSION FLOOR BEAM -Y953 LOCATED FR31 TO FR37 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y953 LOC. FR31 TO FR37 RH SIDE IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2743749)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CRACK SUPPORT ANGLE LOCATED FR79 TO FR80 AT LEVEL STR26 LH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE LOCATED FR79 TO FR80 AT LEVEL STR26 LH AT AFT GALLEY AREA. (2738757)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 CRACK SUPPORT ANGLE LOCATED FR79 TO FR80 AT LEVEL STR26 RH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE LOCATED FR79 TO FR80 AT LEVEL STR26 RH AT AFT GALLEY AREA. RII INSPECTION COMELETE. (2738765)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,476 hrs · 9,783 cycles

SHIP 3351 DURING ACCOMPLISHMENT OF THE MOCK-UP FOR EM 5330-01152 MTC HAS REPORTED SEVERAL DEVIATIONS THAT REQUIRED ADDITIONAL OR ALTERNATE INSTRUCTIONS TO THE EXISTING WORK STEPS TO BE ABLE TO ACCOMPLISH THEM. CORRECTIVE ACTION: REF VA 101000. (2717632)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,296 hrs · 9,759 cycles

SHIP 3351 EXIT SIGN DAMAGED IN AFT CREW REST. CORRECTIVE ACTION: RESOLDERED EXIT SIGN CONNECTIONS. (4758937)

Part: NONE — NONE (NONE) · airframe 73,443 hrs · 9,654 cycles

DOOR 3L WOULD NOT DISARM AFTER MULTIPLE CYCLES, AND THEN FINALLY DISARMED. CHECKED DOOR 3L FOR OPERATION AND INDICATION ALL CK GOOD.

Part: INDICATOR — INACCURATE (L2 DOOR SLIDE) · airframe 73,252 hrs · 9,630 cycles

GROUND AGENT OPEN DOOR 2L BEFORE IT WAS DISARMED. FA FORWARD PANEL STILL SHOWS ARM DOOR L2 WHILE THE L2 DOOR IS OPEN. DOOR WAS NOT ARMED WHEN OPENED, DOOR DOES NOT SHOW ARMED ON FAP PANEL. CYCLED DOOR, NO FALSE INDICATIONS SHOWN, OPS NORMAL AT THIS TIME. (9174270)

Part: NONE — NONE (NONE) · airframe 72,761 hrs · 9,570 cycles

SHIP 3351 LH FRONT FIXED SGS WINDOWS REQUIRES DETAILED INSPECTION AND ELECTRICAL TEST MEASUREMENT PER AMDS 5611-01020-02A. CORRECTIVE ACTION: LH FRONT FIXED SGS WINDOWS REQUIRES DETAILED INSPECTION AND ELECTRICAL TEST MEASUREMENT PER AMDS 5611-01020-02A. (2503114)

Part: UNKNOWN — UNKNOWN · airframe 71,645 hrs · 9,427 cycles

SHIP 3351 SEAT 4J, 2J, 3G FAILED INFLATABLE SEAT BELT TEST. CORRECTIVE ACTION: R/R INFLATABLE SEAT BELT IN LOC 4J, 2J, AND 3G. (9233816)

Part: UNKNOWN — UNKNOWN · airframe 71,645 hrs · 9,427 cycles

SHIP 3351 SEAT 2A,4A FAILED INFLATABLE SEAT BELT TEST. CORRECTIVE ACTION: R/R EMA AT LOC 4A. R/R GAS GENERATOR AT LOC 2A. (9233817)

Part: NONE — NONE · airframe 71,360 hrs · 9,388 cycles

SHIP 3351 -ATB- DUE TO AIR ENG 2 BLEED FAULT. C/W FB 20.27. CORRECTIVE ACTION: REPLACED PRV. FOUND LOOSE SENSE LINE. RE-SECURED LINE. OPS & LEAK CHECKS OK. (8980891)

Part: NONE — NONE · airframe 71,323 hrs · 9,384 cycles

SHIP 3351 LOUD SQUEAL NOTED WHILE IN CREW BUNK AT CRUISE. CORRECTIVE ACTION: PRESSURIZED A/C FOUND AFT OUTFLOW VALVE SQUEALING. UPON REMOVAL OF AFT OUTFLOW VALVE, FOUND GASKET TO BE ELONGATED. REPLACED GASKET AND INSTALLED OUTFLOW. PERFORMED A/C PRESSURIZATION. (8980879)

Part: DOOR — DAMAGED · airframe 70,609 hrs · 9,291 cycles

SHIP 3351 RAMP REPORTED DAMAGE AT LOWER RIGHT FWD OF FWD CARGO DOOR. CORRECTIVE ACTION: FOUND WITHIN REWORK LIMITS AND REWORKED LOWER RIGHT DAMAGE FORWARD OF FWD CARGO DOOR PER A330 SRM 53-21-11. (8511193)

Part: NONE — NONE · airframe 70,123 hrs · 9,229 cycles

SHIP 3351 ROW 45H EMERGENCY LIGHT OUT. CORRECTIVE ACTION: RESEATED CONNECTOR FOR ROW 45H EMERGENCY LIGHT. (8660694)

Part: NONE — NONE · airframe 70,041 hrs · 9,214 cycles

SHIP 3351 O2 MASK AT 50CDG HOSE DAMAGED IN CLAMP. CORRECTIVE ACTION: O2 MASK REPLACED AS REQUIRED. (8660653)

Part: NONE — NONE · airframe 69,498 hrs · 9,133 cycles

SHIP 3351 ELEC CB B54 LEFT RECIRC FAN FIN 1HG1 TRIPPED. CREW REPORTED SMOKE/FUME AFT CABIN SMELL WAS DESCRIBED TO BE PLASTIC. CORRECTIVE ACTION: NO FUMES NOTED IN CABIN. DISCONNECTED LEFT RECIRC FAN PER A330 AMM 21-21. RESET RCCB-B54(1HG1). PFR SHOWS "COND L CAB VENT FAULT". REPLACED LEFT RECIRCULATION FAN REF A330 MM 21-21, C/W ALL "NO GO" ODI PREVENTION STEPS NO OTHER SMOKE/FUME CONDITIONS NOTED. (2162590)

Part: NONE — NONE · airframe 69,461 hrs · 9,125 cycles

SHIP 3351 DENT EXTERNAL SKIN BULK CARGO DOOR FWD LOWER SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: REF ER/A 597720-14. (2151823)

Part: NONE — NONE · airframe 69,434 hrs · 9,117 cycles

SHIP 3351 A DENT WAS FOUND ON THE BULK CARGO DOOR OUTER SKIN AT THE LOWER FWD CORNER. CORRECTIVE ACTION: REWORKED REF ERA 597720-14. (2147545)

Part: NONE — NONE · airframe 69,360 hrs · 9,100 cycles

SHIP 3351 LG DOOR STAYED OPEN ON APPROACH LEFT MAIN GEAR. DOOR CLOSED ON ITS OWN AFTER LANDING. CORRECTIVE ACTION: INSPECTED GEAR DOORS FOR GROUND IMPACT DAMAGE. NONE FOUND. FOUND MED SIZE BIRD WEDGED ON LH DOOR UPLOCK AND ROLLER. CLEANED AND INSPECTED LH UPLOCK, ATTACH ROLLER AND PROX SWITCHES. NO TROUBLE FOUND. CYCLED GEAR DOOR WITH EXT HANDLE AND IN COCKPIT PER A330 AMM 32-31. ALL COCKPIT INDICATIONS NORMAL. (8420626)

Part: NONE — NONE · airframe 68,120 hrs · 8,878 cycles

SHIP 3351 EXIT SIGN INSIDE PILOT CREW REST MODULE IS HANGING. CORRECTIVE ACTION: RESECURED SIGN. (8023511)

Part: COMPRESSOR — LEAKING (APU) · airframe 67,341 hrs · 8,767 cycles

SHIP 3351 ON DESCENT AIRCRAFT HAD OILY SMELL THROUGH CABIN AND COCKPIT WITH PACK FLOW IN NORM AND LOW. FIRST CABIN CONTROL BEHIND COCKPIT WAS 124 DEGREES C BELOW 10,000 COULD NOT REDUCE W/CNTRLS. CORRECTIVE ACTION: NO OIL NOTED IN APU BLEED AIR ELBOW. NO TROUBLE FOUND WITH ENGINES. INSPECTED BOTH PACK BAY DUCTS LEFT AND RIGHT NO EVIDENCE OF CONTAMINATION. FOUND LOW PRESSURE COMPRESSOR AND GEAR BOX CASE LEAKING OIL. REPLACED APU. REPLACED LT AND RT PACK FLOW CONTROL VALVE AND PACK WATER EXTRACTOR. COMPLETED DECONTAMINATION OF APU, PACKS AND ENGS. (7906268)

Part: OIL SYSTEM — LEAKING (APU) · airframe 67,331 hrs · 8,764 cycles

SHIP 3351 CREW REPORT OF OILY SMELL IN CABIN DURING FLIGHT. CORRECTIVE ACTION: FOUND APU OIL LEAK INTO THE RAM AIR SCOOP. REPLACED APU. (1907474)

Part: GIMBAL JOINT — BROKEN (R4 DOOR) · airframe 66,569 hrs · 8,623 cycles

SHIP 3351 4R DOOR GIMBAL ASSY BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED SPRING ROD ASSY. (7334560)

Part: CABIN PRESSURE — FALSE INDICATION · airframe 66,569 hrs · 8,623 cycles

SHIP 3351 -ATB- DUE TO CABIN PRESSURIZATION CONTROL. CORRECTIVE ACTION: NO FAULTS FOUND ON CPC 1&2. PERFORMED CPC 1&2 AUTO AND MAN OPERATIONAL TESTS WITH NO FAULTS FOUND.(7334554)

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 66,302 hrs · 8,549 cycles

SHIP 3351 EMER EXIT LIGHT STUCK ON WITH SW IN ARM POSITION. CORRECTIVE ACTION: COULD NOT DUPLICATE. CYCLED EMERGENCY LIGHT SWITCH AND OPS CK SYSTEM ALL CK GOOD. (7647319)

Part: SKIN — DENTED (L4 DOOR) · airframe 66,071 hrs · 8,483 cycles

SHIP 3351 L4 DOOR LWR AFT EDGE DENT APPROX .5 IN DEEP THRU SKIN DOUBLER AND SEAL RETAINER. CORRECTIVE ACTION: REMOVED DAMAGE FABRICATED REPAIR DOUBLER AND SPACER. INSTALLED DOUBLER. PRIMED AND PAINTED. (4059486)

Part: LIGHT — INOPERATIVE (SEAT 26B) · airframe 65,308 hrs · 8,350 cycles

SEAT 26B ESCAPE PATH LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 26B. LP 7149552

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,993 hrs · 7,953 cycles

DURING EMERGENCY LIGHT TEST STEP 10L LIGHTS AT ROW 12-21H AND DOOR 3R DID NOT ILLUMINATE WITH CIRCUIT BREAKERS E72, E73, E71 PULLED. REPLACED BATTERY PACK 16WL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 61,993 hrs · 7,953 cycles

EMERGENCY LIGHTS AT ROW 13H, 14H, 15H, AND 29H DO NOT LIGHT UP ON TEST. RE-SECURED CONNECTORS AT SEAT 12H AND 29H. LP 5033420.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 55,362 hrs · 7,164 cycles

EMERGENCY EXIT SIGN COVER LOOSE AT DOOR 3R. RE-INSTALLED EXIT SIGN COVER. LP 0334083

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 52,841 hrs · 6,906 cycles

NR 2 ASPSU BATTERY FAILED A BIT TEST. REPLACED THE BATTERIES.

Part: SIGN — MISSING (CABIN) · airframe 52,479 hrs · 6,867 cycles

EMERGENCY EXIT SIGN MISSING. REPLACED EMERGENCY EXIT SIGN LENS COVER.

Part: FAN — FAILED (RECIRCULATION) · airframe 51,085 hrs · 6,725 cycles

DURING CRUISE, REPORTED AN ELECTRICAL ODOR THROUGHOUT THE CABIN. SUSPECTED THE RIGHT RECIRCULATION FAN WAS AT FAULT. ODOR HAS DISSIPATED, FLIGHT CONTINUED TO DESTINATION. REPLACED RIGHT RECIRCULATION FAN IAW AMM 21-21-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,009 hrs · 6,420 cycles

DURING MCDU TEST, EPSU 17WL BATTERY FAULTED. REPLACED BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,009 hrs · 6,420 cycles

DURING MCDU TEST, EPSU 15WL BATTERY FAULTED. REPLACED BATTERY PACK.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 47,725 hrs · 6,390 cycles

DURING TAXI IN, EXIT LIGHTS AT L1 & R1 DOOR DID NOT ILLUMINATE. FOUND WIRES REVERSED ON GROUND CONNECTIONS. RE-INSTALLED WIRE CORRECTLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, DOOR 4R EPSU FAILED TEST. REPLACED EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-38-400-801-A.

Part: SKIN — DAMAGED (FRAME 84) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, WHILE PERFORMING VTP MOD INSPECTION HOLE NR 58 UPPER SIDE AT FRAME 84, STR 2A LT SIDE AT UPPER FUSELAGE FOUND OUT OF LIMITS EDGE MARGIN. INSTALLED REINFORCEMENT DOUBLERS, AND SHIME IAW ER/A 544202-14AD, LP 2429329.

Part: SKIN — DAMAGED · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK WHILE PERFORMING VTP MOD INSPECTION, HOLE NR 169 UPPER SIDE OF SKIN WAS FOUND OUT OF LIMITS. INSTALLED REPAIR DOUBLERS AND SHIMS IAW ER/A 544196-14AD.

Part: FLOOR SUPPORT — CRACKED (FRAMES 71-74) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, FOUND FLOOR SUPPORT CRACKED AT -Y794.3, FRAME 71-74 IN AFT GALLEY. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG NR 10N00344.

Part: FLOORBEAM — CORRODED (FRAME 71) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, FLOORBEAM IN PASSENGER CABIN AT 794.3, FRAME 71 FOUND CORRODED. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG F5347700.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 47,801 hrs · 6,397 cycles

DURING M-CHECK, CORROSION WAS FOUND IN THE COUNTERSINK HOLES OF ACCESS PANEL 642GB ON THE RT WING. REPLACED FUEL TANK ACCESS PANEL 642GB.

Part: SEAT TRACK — NOT REPORTED (FRAMES 33-34) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, SEAT TRACK IN PASSENGER CABIN AT 1959, FRAMES 33-34. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53276421.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 47,801 hrs · 6,397 cycles

DURING M-CHECK, CORROSION WAS FOUND IN THE COUNTERSINK HOLES OF ACCESS PANEL 650BB ON THE RT WING. REPLACED FUEL TANK ACCESS PANEL 650BB.

Part: SEAT TRACK — CORRODED (FRAMES 74-75) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, SEAT TRACK -Y450, FRAME 74-75 AFT AFT GALLEY INSTALLED INPROPERLY. REPLACED SEAT TRACK SRM 51-72-11 AND DWG F53478040.

Part: SEAT TRACK — CORRODED (FRAMES 74-75) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, SEAT TRACK AT -Y450, FRAME 74-75 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53478040.

Part: SEAT TRACK — CORRODED (FRAMES 32-34) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, SEAT TRACK IN PASSENGER CABIN AT 1552.5 BETWEEN FR 32-34 FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53275878.

Part: SKIN — DENTED (FRAMES 19-20) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, FOUND EXTERNAL SKIN DENTED BETWEEN FRAME 19 - 20, STRINGERS 48-49R. PERFORMED PERMANENT REPAIR IAW SRM 53-21-11, FIG 204.

Part: SEAT TRACK — CORRODED (FRAMES 72-74) · airframe 47,662 hrs · 6,381 cycles

DURING M CHECK, SEAT TRACK -Y450 FROM FRAMES 72 - 74 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG 10N00344.

Part: SEAT TRACK — CORRODED (FRAMES 72-73) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, THE SEAT TRACK IN PASSENGER CABIN AT +Y1959 BETWEEN FRAMES 72 - 73.8 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG F53478100.

Part: SEAT TRACK — CORRODED (FRAMES 32-37) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, SEAT TRACK IN PASSENGER CABIN AT +Y1552.5 BETWEEN FRAME 32 -FRAME 37 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG F53275878.

Part: FLOORBEAM — CORRODED (FRAME 16) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, FLOORBEAM AT Y953-Y1456 AT, FRAME 16A IN FORWARD GALLEY WAS FOUND CORRODED. REPLACED FLOORBEAM ASSY IAW SRM 51-72-11 AND DWG F25310251.

Part: FLOOR SUPPORT — CORRODED (FRAMES 74-77) · airframe 47,662 hrs · 6,381 cycles

DURING M-CHECK, FLOORBEAM -Y1447.8 FROM FRAME 74-77.10 AT AFT GALLEY AREA FOUND CORRODED. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWGS F53478015, F5347804, F53970337.

Part: BATTERY PACK — DAMAGED (EMERGENCY LIGHTS) · airframe 46,200 hrs · 6,240 cycles

DURING A B1 CHECK, FOUND EPSU BATTERY PACKS DAMAGED. REPLACED THE BATTERY PACKS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,900 hrs · 6,030 cycles

WHILE ACCOMPLISHING WC 0591-0204, TEST FAULTED BAT/ESPU, 14WL, DOOR 2. REPLACED BATTERY PACK.

Part: WARNING MESSAGE — ACTIVATED (NR 2 ENGINE) · airframe 43,166 hrs · 5,959 cycles

FLIGHT DIVERTED DUE TO NR 2 ENGINE "OIL FILTER CLOG" AND OTHER ENGINE RELATED MESSAGES, ALONG WITH AN "ENGINE SHUTDOWN" MESSAGE APPEARED DURING CRUISE, ENGINE SHUT ITSELF DOWN. OIL QUANTITY REMAINED NORMAL, ROTATION INDICATED ZERO, CREW COMPLETED QRH PROCEDURE FOR ENGINE FAIL/SHUTDOWN. REPLACED ENGINE.

Part: SKIN — DAMAGED (FRAME 30) · airframe 51,570 hrs · 6,774 cycles

DURING LINE CHECK, A CREASE AND PENETRATION TO THE FUSELAGE SKIN WAS FOUND EXTENDING 16 INCHES FWD OF FRAME 30 AND 1 INCH ABOVE STR 2L. REMOVED DAMAGED AREA, PERFORMED HFEC INSPECTION AND EDDY CURRENT, INSTALLED REPAIR DOUBLER AND SHIM, AND INSTALLED STRINGER SPLICE PER ER/A 520-211-14.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 37,714 hrs · 5,324 cycles

DURING INSPECTION, FOUND EMERGENCY LIGHT POWER SUPPLY 19WL HAS AN INTERNAL FAULT. REPLACED POWER SUPPLY 19WL.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

CABIN FLOOR SUPPORT AT Y450 FR75 FOUND CORRODED. REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

CABIN FLOOR SUPPORT AT Y1447.8 FR74 FOUND CORRODED. REPLACED CABIN FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

CABIN FLOOR SUPPORT AT -Y450 FR75 FOUND CORRODED. REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

TWO CABIN FLOOR SUPPORTS AT Y1456 FR 73 TO FR74 FOUND CORRODED. REPLACED 2 CABIN FLOOR SUPPORTS.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

CABIN FLOOR SUPPORT AT INBD ON -Y450 FR 76 FOUND CORRODED. REPLACED CABIN FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

CABIN FLOOR SUPPORT INBD OF Y450 FR75 FOUND CORRODED. REPLACED CABIN FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

CABIN FLOOR SUPPORT AT -Y1959 FR 73 TO FR 74 FOUND CORRODED. REPLACED CABIN FLOOR SUPPORT.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT Y2462 FR56 AND FR58 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT -Y953 FR60 TO FR 62 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 240 AT Y450 FR 29 AND FR36 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

ZONE 260 SEAT TRACK AT -Y450 FR55 AND FR58 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT -Y1959 FR 60 TO FR 62 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT -Y1959 FR 63 AND FR 69 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 250 AT -Y1959, FR53.2 AND FR 53.9 FOUND CORRODED. REPLACED SEAT TRACK

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT -Y2462 FR56 AND FR58 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT Y1959 FR63 AND FR66 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

ZONE 250 SEAT TRACK AT Y-450 FR 53.8 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT -Y450 FR68 AND FR70 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT -Y1959 FR 55 AND FR57 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT -Y2462 FR 65 AND FF70 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 250 AT -Y450 FR40 AND FR46 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 250 AT Y1959 FR 40 AND FR47 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT Y450 FR59 AND FR66 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 240 AT -Y1456 FR33 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT -Y450 FR 59 AND FR 65 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT Y1959 FR 56 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT Y2462 FR63 TO FR 68 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 250 AT Y450 FR40 AND FR45 FOUND CORRODED. REPLACED SEAT TRACK

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 250 AT -Y2462 FR40.1 AND 40.2 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 250 AT Y1959 FR 53.2 TO FR53.3 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK AT Y1959, FOUND CORRODED AT FR 48 AND FR 53.1. CORROSION REMOVED IAW SRM 51-74-00, FOUND EXCEED LIMITS IAW SRM 5 3-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT Y450 FR 55 AND FR 58 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT Y2462 FR59 TO FR61 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK IN ZONE 260 AT Y1959 FR 59 TO FR62 FOUND CORRODED. REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK AT Y1959 FOUND CORRODED AT FR47 & FR53. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMIT IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK, R & R IAW SRM 51-42-11.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK AT -Y450 FOUND CORRODED AT FR48 & FR53. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMIT SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 37,152 hrs · 5,242 cycles

SEAT TRACK AT Y450 FOUND CORRODED AT FR48 & FR53. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMIT IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW-SRM 51-42-11.

Part: SKIN — DAMAGED (L4 DOOR) · airframe 36,565 hrs · 5,171 cycles

FOUND DAMAGE TO L4 DOOR LOWER AFT CORNER 1" TEAR IN SKIN AND DENTED THRU 6" RADIUS WITH SEAL RETAINER DEFORMED. REMOVED DAMAGE AND FABRICATED REPAIR PARTS IAW SRM 52-13-00. DRILLED NEW AFT CORNER SEAL RETAINER FITTING OK TO INSTALL REPAIR IAW SRM. INSTALLED REPAIR AND AFT CORNER SEAL RETAINER IAW SRM 52-13-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 33,994 hrs · 4,863 cycles

SKIN DAMAGED AT FR 0- FR 1 AND APPROXIMATELY 33 INCHES UP/DOWN AND 10 INCHES FWD/AFT. REPAIRED AS PER ERA 504502-14REV.0.

Part: SKIN — MISREPAIRED · airframe 33,896 hrs · 4,850 cycles

DURING K CHECK, FOUND A DOUBLE DRILLED FASTENER AT A EXISTING TEMPORARY LIGHTING STRIKE REPAIR, FR-57, STR-46R. REPAIR WAS ACCOMPLISHED PER SEC 1 OF ERA50264-14.

Part: BATTERY — DISCHARGED (CABIN) · airframe 6,252 hrs · 843 cycles

AIRCRAFT 3351. DURING EMERGENCY LIGHT TEST, MAINTENANCE FOUND BATTERY 11WL AND 17WL FAULTED. MAINTENANCE REPLACED BOTH BATTERIES (11WL, 17WL) PER AMM. ALL TEST PER AMM GOOD.

Part: BRAKE SYS — WARNING LIGHT (MLG) · airframe 28,732 hrs · 4,205 cycles

IMMEDIATELY AFTER INITIATING TAKEOFF POWER AND ROLL (RUNWAY 24), AMS TOWER DIRECTED US TO ABORT TAKEOFF DUE TO AN UNEXPECTED GO-AROUND ON RUNWAY 18C. RECEIVED CAUTION FOR "BRAKE NR 5 RELEASED"; EXITED RUNWAY AND THEN RECEIVED ANOTHER CAUTION "GREEN HYDRAULIC SYSTEM LOW"; GREEN SYSTEM QUANTITY INDICATOR DISPLAYED LOW LEVEL AND CONTINUING TO DECREASE. BRAKES NR 5 AND NR 6 AND WHEEL NR 5 WERE REPLACED AND THE GREEN HYDRAULIC WAS SERVICED AND CHECKS OK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR54-FR58. REPAIRED IAW ERA 481432-14 AND ASSOCIATED ERA 13-481432.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK IAW SRM 51-42-11, AT Y450, FROM FR58-FR67 DUE TO CORROSION REMOVED EXCEEDED ALLOWABLE LIMITS IAW SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR54-FR58. REPAIRED IAW ERA 481432-14, REV 0.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON FLOOR STRUCTURE AT Y1456 FR17. REPAIRED IAW ERA 481359-14, REV O.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK AT Y450 FROM FR40 TO FR47, IAW ER/A 4814 & ER/A 13-481432 DUE TO CORROSION BEYOND LIMITS AS SPECIFIED IN SRM 53-31-15, FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1552.5, FR32-FR37. REPAIRED IAW ERA 481432-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK AT Y1959 FROM FR26 TO FR38, IAW SRM 53-00-15, FIG 204 DUE TO CORROSION BEYOND LIMITS AS SPECIFIED IN SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR55-FR58. REPAIRED IAW ERA 481432-14.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK IAW ER/A 481432-14, AT Y1959, FROM FR58-FR62 DUE TO CORROSION REMOVED EXCEEDED ALLOWABLE LIMITS IAW SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR40-FR47. REPAIRED IAW ERA 481432-14.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK IAW ER/A 481435-14, REV O, AT Y953, FROM FR11-FR18 DUE TO CORROSION REMOVED EXCEEDED ALLOWABLE LIMITS IAW SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK AT Y1959 FROM FR62 TO FR72, IAW SRM 51-42-11 DUE TO CORROSION BEYOND LIMITS AS SPECIFIED IN SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK IAW SRM 51-42-11, AT Y450, FROM FR55-FR58 DUE TO CORROSION REMOVED EXCEEDED ALLOWABLE LIMITS IAW SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK IAW ER/A 481432-14, REV O, AT Y450, FROM FR53-FR55 DUE TO CORROSION REMOVED EXCEEDED ALLOWABLE LIMITS IAW SRM 53-31-15, FIG 101.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK AT Y953 FROM FR18 TO FR24, PER SRM 53-00-15, FIG 204 DUE TO CORROSION BEYOND LIMITS AS SPECIFIED IN SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R SEAT TRACK IAW SRM 51-42-11, AT -Y1959, FROM FR58-FR62 DUE TO CORROSION REMOVED EXCEEDED ALLOWABLE LIMITS IAW SRM 53-00-15, FIG 102.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR62-FR72. REPAIRED IAW SRM 53-00-15 FIGURE 102, 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR47-FR53. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR72-FR73. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR39.2-FR40. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR58-FR67. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

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

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR53.2-FR54. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR58-FR62. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR62-FR72. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR47-FR53. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y450 FR68-FR72. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT -Y450 FR68-FR72. REPAIRED IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

DURING H-CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR47-FR53. REPAIRED IAW SRM 51-42-11.

Part: PROFILE — CRACKED (CABIN) · airframe 24,952 hrs · 3,673 cycles

R & R THE RT Z-PROFILE AT FR80 FROM Y1137.1 TO Y1447.8 IAW SRM 51-42-11, DUE TO IT BEING CRACKED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R FLOOR SUPPORT NR 271MF AT Y450 BETWEEN FR75 AND FR78 IAW SRM 51-42-11, DUE TO IT BEING CORRODED BEYOND LIMIT.

Part: PROFILE — CRACKED (CABIN) · airframe 24,952 hrs · 3,673 cycles

R & R THE LT Z-PROFILE AT FR80 FROM Y1137.1 TO Y1447.8 IAW SRM 51-42-11, DUE TO IT BEING CRACKED.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 24,952 hrs · 3,673 cycles

R & R FLOOR SUPPORT AT -Y1447 AFT OF FR75 IAW SRM 51-42-11, DUE TO IT BEING CORRODED BEYOND LIMITS SPECIFIED IN SRM 53-41-14, FIG 103.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,545 hrs · 3,597 cycles

DURING LINE CHECK FOUND FUSELAGE SKIN DAMAGE FORWARD OF BULK CARGO COMPARTMENT DOOR AT FR80-FR82 S34R. REPAIRED IAW ERA 479795-14 & SRM 53-00-11.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,123 hrs · 2,687 cycles

DURING 1/2 A-CHECK, FOUND EPSU BATTERY FOR LOWER DECK CREW REST BAD. REPLACED BATTERY PACK IN EPSU 19WL, CHECKS GOOD. (S)

Part: FAN — ODOR · airframe 16,448 hrs · 2,490 cycles

JUST PRIOR TO LEVEL OFF AFTER TAKE OFF THE FLIGHT ATTENDANT AT DOOR 4R CALLED TO REPORT SHE SMELLED ELECTRICAL SMOKE AND IT WAS HAZY. RECEIVED "COND R CAB VENT FAULT" FOLLOWED COM AND SHUT OFF CABIN FANS AND THE SMELL AND HAZE DISSIPATED AND LANDING WAS UNEVENTFUL. FOUND RECIRCULATION FAN RT (210HG) FAULT AND FAN FROZEN.