N352NW

Part: FITTING — DAMAGED (ZONE 100) · airframe 80,436 hrs · 38,314 cycles

LH UPPER ACTUATOR FITTING HAS TWO FASTENERS PULLED THROUGH FITTING. REPAIRED PER PRI 604353-14AD REV. 0, 1, 2, 3, 4, 5 AND 6 AND COMPLIED WITH ER/A 604353-14AD REV. B SECTION III. (LP: 1316696)

Part: ENGINE — BIRD INGESTION (NR 2) · airframe 80,334 hrs · 38,259 cycles

BIRD STRIKE IN #2 ENGINE ON FINAL APPROACH. NO ABNORMAL ENGINE INDICATIONS. ENGINE WAS AT LOW POWER. SMELLED LIKE FOOD COOKING IN OVEN ACCORDING TO FAS. LATER LATER SMELLED LIKE FRIED CHICKEN. PERFORMED AMM 05-51-14. CLEARED ENGINE OF DEBRIS REF A320 AMM 72-00 AND CARRIED OUT A LEVEL A DECONTAMINATION PER AMDS WORK CARD 2100-2007. NO DAMAGE FOUND TO ANY AC COMPONENTS OR ANY ENGINE COMPONENTS. RAN EACH ENGINE INDIVIDUALLY, AND TOGETHER, AND NO DISCERNIBLE SMELL IS PRESENT IN THE BLEED AIR SYSTEM. APU BLEED SOURCE ALSO VERIFIED NO SMELL PRESENT. ENGINE BORO AND WETWASH TO BE DEFERRED ON SUBSEQUENT LOG PAGES. AC OK FOR SERVICE.

Part: CONTROL UNIT — FAULTED (THROTTLE) · airframe 80,190 hrs · 38,180 cycles

DIV - DIVERTED TO RDU DUE TO AN ENG 2 THROTTLE LEVER DISAGREE MESSAGE. REPLACED THROTTLE CONTROL UNIT PER A320AMM 76-11. OPERATIONAL CHECK GOOD, NO FAULTS.(LP: 7403542)

Part: OIL SYSTEM — LEAKING (APU) · airframe 80,158 hrs · 38,161 cycles

AFTER APU START UP AND WARM UP AT THE GATE WHEN THE APU BLEED SELECTED ON THE DIRTY SOCK SMELL FILLED THE COCKPIT AND ENTIRE CABIN. SMELL WAS VERY STRONG. PERFORMED GVI OF APU COMPARTMENT. FOUND EVIDENCE OF AN OIL LEAK ON PLENUM. OK FOR SVC. (LP: 7403510)

Part: LIGHT — DETACHED (ZONE 200) · airframe 79,946 hrs · 38,058 cycles

EMERGENCY EXIT LIGHTING UNIT UNDER SEAT 28D LOOSE/HANGING DOWN. FOUND 28D SEAT EMER LIGHT BOX BROKEN, REPLACED BOX, OP CHECKS GOOD, OK FOR SERVICE. (LP: 7848226)

Part: FILTER — ODOR (CABIN) · airframe 79,887 hrs · 38,024 cycles

SHIP 3252 DISC: WITH APU BLEED "ON" DIRTY SOCK ODOR STRONGER IN FLIGHT DECK AFT F/A ALSO COMPLAINED ABOUT ODOR IN AFT CABIN, APU BLEED WAS TURNED OFF SMELL DISSIPATED. C/A: AFTER COMPARTMENT WASH, RAN APU FOR 30+ MINUTES-NO LEAKS FOUND. C/W AMDS WORK CARD 4916-2001 AND 4900-2001. APU OK FOR SVC. R/R BOTH AIR RECIRC FILTERS REF A320 AMM 21-21 ( 541149) RAN BOTH PACKS OFF APU FOR 2 HRS, NO SMELL NOTED AT THIS TIME.

Part: BRACKET — EXCESS PLAY (ZONE 700) · airframe 79,863 hrs · 38,009 cycles

ATB DUE TO L/G DOORS NOT CLOSED, L/G GEAR NOT UPLOCKED, AND L/G SHOCK ABSORBER FAULT ECAM WARNINGS. FOUND EXCESSIVE PLAY OF FLIGHT/GROUND SENSING MECHANISM BRACKET DUE TO LOOSE BOLT AND WORN-OUT BUSHINGS. REPLACED FLIGHT/GROUND SENSING MECHANISM BUSHED LEVER, RIGGED, AND SERVICED NLG STRUT. OPS CHECK GOOD. (LP: 7286058)

Part: COMPUTER — FAULTED (FUEL QTY) · airframe 79,504 hrs · 37,787 cycles

SHIP 3252 - MISC - DECLARED EMERGENCY FOR SUSPECTED FUEL LEAK. CENTER TANK QUANTITY FLUCTUATING. MEL ALREADY APPLIED FOR CENTER TANK AUTO FEED SYSTEM. CORRECTIVE ACTION: REPLACED FQIC. (LP: 7745944)

Part: BUSS — ABNORMAL (AC SYSTEM) · airframe 78,956 hrs · 37,500 cycles

SHIP 3252 DISC: WHILE CLOSING CIRCUIT BREAKERS FOR BREAK SELECTOR VALVE REPLACEMENT, AC 2 BUS DROPPED OFF-LINE. ATTEMPTED RESETS, NO HELP. UPON INITIATING BPCU BITE THROUGH CFDS, THE 123VU PANEL SPARKED. C/A: REF HANGAR VISIT P334905220250503 NR 32 FOR CORRECTIVE ACTIONS. (LP: 7166697)

Part: HYDRAULIC LINE — LEAKING (ZONE 100) · airframe 78,944 hrs · 37,488 cycles

SHIP 3252 DISC: PASSING N8000' ON DESCENT, GOT A DIRTY SOCK SMELL. SMELL SEEMED TO GO AWAY AFTER ABOUT 1 MINUTE. C/A: PERFORMED OPS TEST OF LT + RT PACK PER A320 AMM 21-00. COULD NOT DUPLICATE. FOUND HYD FLUID THROUGHOUT A/C BELLY ORIGINATING FROM FWD CARGO BELLY DRAIN. FOUND FWD CARGO DOOR HYD LINE MPN D5931003600200 LEAKING. R/R HYD PRESSURE LINE D5931003600200 ON N/R LOG 0942307. PERFORMED APU INTAKE AND COMPARTMENT CLEANING PER A320 J/C 4916-2001. PER MCC REQUEST, PERFORMED #1 & #2 ENG OIL FIME ODOR CHECK PER A320 J/C 7900-2001. NTF. PERFORMED LEVEL A AND LEVEL B ECS DECONTAMINATION PER J/ C 2100-2007, 2100-2005 AND A320 AMM 36-10-00-615-802-A VARIATN 1 . NO ODOR NOTED. MCC NOTIFIED. (LP: 7166678)

Part: FAIRING — DAMAGED (ZONE 100) · airframe 78,824 hrs · 37,426 cycles

SHIP 3252 DISC: PANEL 197GB WING TO BODY FAIRING HAS SEVERAL FASTENER HOLES DAMAGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 016-0001:10-0553-8-6853/001 00007 ACCOMPLISHED HOLE REPAIR PER A320 SRM 51-77-12. (LP: 0910179)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 78,634 hrs · 37,320 cycles

SHIP 3252 DISC: FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 29D INOP. C/A: WRONG LIGHT SENT. RECIEVED RED LIGHT. NEEDS WHITE LIGHT FIXTURE MPN# BR9471-4FS STK# 31-2500-3-2311 IAW REF AIPC FIG. 33 -51-09-80 ITEM 010A. NASI LGA. INSTALLED NEW LIGHT HOUSING AS PER A320 CMM 25-23-51. STILL NEEDS LIGHT. OK TO CONT ON MEL. REPLACED MISSING FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 29D IAW CMM 25-23-51. OPS NORMAL AND OK FOR SERVICE. NO (M) PROC, PLACARD REMOVED. (LP: 6522600)

Part: UNKNOWN — ODOR (CABIN) · airframe 77,455 hrs · 36,658 cycles

WORKING ACARS DUE TO F/A REPORT OF BURNING RUBBER ODOR IN THE AFT GALLEY AND AFT CABIN. C/A: C/W WC 0550-2003 VERIFICATION CHECK FOR RESIDUAL ODOR . NO ODOR PRESENT AT THIS TIME.

Part: NONE — NONE (NONE) · airframe 76,226 hrs · 36,006 cycles

SHIP 3252 DISC: ON APPROACH WITH/ STORMS IN WAY DISCONTINUED APPROACH HAD A 10KT GAIN THAT CAUSED APPROX. 2 KT OVERSPEED WITH FLAPS TRANSITIONING FROM 1 TO 0. PERFORMED FLAP OVERSPEED INSPECTION IAW A320 AMM 05-51-13. NO DEFECTS NOTED. OK FOR SERVICE. (LP: 5883442)

Part: FILTER — DAMAGED (DEMISTER) · airframe 76,187 hrs · 35,989 cycles

SHIP 3252 DISC: ON TAXI IN, BOTH PILOTS SMELLED A FAINT PLASTIC BURNING SMELL IN COCKPIT. 5 MIN LATER ECAM SMOKE LAV DET FAULT (1626, AUS). C/A: C/W W/C 0550-2002, UPON INSP FOUND DEMISTER FILTER IN BAD CONDITION W/PLASTIC SMELL. R&R AS PER A320 AMM 21-26. PER W/C RAN LEFT ENG & PACK & FOUND NO MORE SMELL. INSPECTED ALL COCKPIT PANELS, NO SMELL DETECTED. PERFORMED VIS INSP OF APU COMPARTMENT, NO SIGN OF CONTAMINATION. R&R SDCU AS PER A320 AMM 26-17. CHK OK. FAULTS CLEARED. (LP: 5883436)

Part: RIB — CORRODED (LT NACELLE) · airframe 75,819 hrs · 35,787 cycles

SHIP 3252 DISC: CORROSION RIB 8 ON REFORCING PLATE ON LH PYLON. C/A: COMPLIED WITH ER/A 616310-14AD REV.ORIGINAL. JOB COMPLETE. ASSOCIATED ER/A 00-616310 ADDED FOR AC 3252. (LP: 0251584)

Part: SLIDE RAFT — NO TEST · airframe 75,819 hrs · 35,787 cycles

SHIP 3252 DISC: DO NOT PASS TEST SLIDE RAFT 831 AT FWD GALLEY AREA. C/A: REPLACED SLIDE RAFT ON UNSERVICEABLE CONDITION P/N: D30664-709, S/N:M20728, FTN: 5G6221, FOR NEW SLIDE RAFT ON SERVICEABLECONDITION P/N: D30664-705, S/N: A5089RP, FTN: 1F6597 ON PASSENGER CREW AS PER AMDS CARD 2561-4001-LF DOOR 831. AND PERFORMEDOPERATIONAL TEST OF EMERGENCY LIHTGS, TEST IS GOOD. RII INSPECTION COMPLETE 0065344. FOR PART CHANGE SEE LOG # 250846. JOB COMPLETE. (LP: 0252904)

Part: SLIDE RAFT — NO TEST (GALLEY DOOR) · airframe 75,819 hrs · 35,787 cycles

SHIP 3252 DISC: DONT PASS OPERATIONAL TEST SLIDE RAFT PASSENGER CREW DOOR 832 AT AFT G ALLEY AREA. C/A: REPLACED SLIDE RAFT 832 PN D30665-705, SN A5584RP ON UNSERVICEABLE CONDITION BY SLIDE RAFT PN D30665-705, SN A5562RP ON SERVICEABLE CONDITION AS PER AMDS CARD 2561-4003-LA TOOL USED TORQUE P/N J6064C S/N DVF25419 DUE DATE 27 DEC 24 RII INSPECTIONCOMPLETE 0682622 (AE114QC) JOB COMPLETE. (LP: 0252486)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,796 hrs · 35,776 cycles

SHIP 3252 DISC: INOP EPSU 10WL AT FWD GALLEY AREA. C/A: REMOVED EMERGENCY POWER SUPPLY UNIT 10WL IN UNSERVICEABLE CONDITION P/N: 3214-54-10 S/N: 1395 ON FWD GALLEY AREA AS PER A 320 FAM AMM 33-51-38-000-001-A STEP 3.C AND 4.A (1) THRU 4.A. (4 ) JOB IN PROGRESS. EPSU, W/ BATTER OFF 31-3350-9-0001

Part: PLATE — CORRODED (RT NACELLE) · airframe 75,796 hrs · 35,776 cycles

SHIP 3252 DISC: CORROSION RIB 8 REFORCIN PLATE ON RH PYLON. C/A: OMPLIED WITH ER/A 616311-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 616311-14AD REV.0 AND PRI 616311-14AD REV.1 IT HASBEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON RH WING RIB 8 AND STRINGER 5 REINFORCING PLATE BOTTOM SKIN AS PER ER/A616311 -14AD REV. ORIGINAL SECTION I HAS BEEN COMPLIED WITH. APPROVED DATE: 15-MAR-24. TOOL USED CALIPER P/N: 500-196-30; S/N:A2103359 ; DUE DATE 21-NOV-24. SMALL HOLE GAUGE: P/N: 154-901; S/N: AE- 403298; DUE DATE: 23-SEP-24. MICROMETER P/N: 293-344-30;S/N: 72747780; DUE DATE: 04-JAN-25. EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022235; DUE DATE:07-SEP-24. ULTRASONIC EQUIPMENT P/N: EPOCH650 S/N: 190984811; DUE DATE: 11- JAN-25. TORQUE P/N: QD2R1000 S/N: 0711051944; DUEDATE: 08-NOV-24 . JOB COMPLETE. (LP: 0248052)

Part: BEARING — MIGRATED (DOOR) · airframe 75,796 hrs · 35,776 cycles

SHIP 3252 DISC: MIGRATED BEARING ON LOWER CONNECTION NEXT TO DOOR STRUCTURE REFER TO AMDS CARD 5210-7089-LA RII AT AFT GALLEY AREA. C/A: 3 CORR BY NOYOLA 00943462 SAL 13MAR24 ATA 5214 RII: Y ENTR 02156330 W REPLACED BEARING ON LOWER CONNECTION NEXT TO DOOR STRUCTURE REFER TO AMDS CARD 5210-7089-LA RII AT AFT GALLEY AREA AS PER A320 FAM AMM 52-13-21-000-001-A AND AS PER A320 FAM AMM 52-13-21-400-001-A, AND AS PER 52-10-00-915-802-A, TOOL USED: CALIPER, P/N:8647A42, S/N: A22356048, DUE DATE: 27-AUG-24, TOOL USED: FEELER GAUGE, P/N: FB335, S/N: AE- 411784, DUE DATE: 02-APR-24, TOOL USED: TORQUE, P/N: QD2R200A, S/N: 0523711808, DUE DATE: 12-MAY-24, TOOL USED: TORQUE, P/N: 501MRMH, S/N: 0821901792, DUE DATE:21-SEP-24 TOOL USED: DIAL FORCE GAUGE, P/N: LG-050, S/N: R17203, DUE DATE: 16-FEB-25 RII INSPECTION COMPLETE 0943462 AE362QC JOB COMPLETE. (LP: 0243468)

Part: BEARING — MIGRATED (PAX DOOR) · airframe 75,796 hrs · 35,776 cycles

SHIP 3252 DISC: MIGRATED BEARING ON UPPER AND LOWER CONNECTION LINK FROM SUPPORT ARM OF PASSENGER CREW DOOR 832 REFER TO AMDS CARD 5210-7089-LA RII AT AFT GALLEY AREA. C/A: REPLACED BEARING ON UPPER AND LOWER CONNECTION LINK FROM SUPPORT ARM OF PASSENGER CREW DOOR 832 REFER TO AMDS CARD 5210-7089-LA RII AT AFT GALLEY AREA AS PER A320 FAM AMM 52-13-21-000-001-A AND AS PER A320 FAM AMM 52-13-21-400-001-A, AND AS PER A320 FAM AMM 52-10-00-915-001-A, TOOL USED TORQUE, PIN:QD2R200A, S/N: 0523711808, DUE DATE: 12-MAY-24, TOOL USED: DIAL FORCE GAUGE, P/N:LG-050, S/N: R17203, DUE DATE: 16-FEB-25 RII INSPECTION COMPLETE 0943462 AE362QC JOB COMPLETE. (LP: 0243509)

Part: SHEAR TIE — NOT REPORTED (FRM 43 S18-24L) · airframe 75,796 hrs · 35,776 cycles

SHIP 3252 DISC: REPLACE FR43 LH, FRAME FOOT COUPLING BTW STRINGER 18L TO STRINGER 24L IN PASSENGER CABIN (ONLY FOR PORPOSES SDR REPORTABLE CHECK BOX). C/A: REPLACED FR43 LH, FRAME FOOT COUPLING BTW STRINGER 18L TO STRINGER 24L IN PASSENGER CABIN (ONLY FOR PORPOSES SDR REPORTABLE CHECK BOX) IN CONJUNCTION WITH AMDS CARD 5311-01239-02A STEP 18 JOB COMPLETE.(LP: 0243390)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,724 hrs · 35,198 cycles

SHIP 3252 - ATB - DUE TO NOSE GEAR FAILING TO RETRACT. FOUND 24 AND 25GA PROXIMITY SENSOR TARGET MOUNTS LOOSE. CORRECTIVE ACTION: REPLACED NLG STRUT EXTEND PROXIMITY SENSOR TARGET HARDWARE. OPS CHECK GOOD. (4860148)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,676 hrs · 35,176 cycles

SHIP - 3252 - DIV TO SLC DUE TO INTERMITTENT LOSS OF RT FUEL QTY INDICATION AND FUEL QTY DEGRADED ECAM MESSAGE. CORRECTIVE ACTION: DEFERRED RT FUEL QTY INDICATION SYSTEM PER MEL AND CONTINUED. R/R FUEL QTY INDICATING COMPUTER PER AMM 28-42. (4385084)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,501 hrs · 35,075 cycles

SHIP 3252 SEAT 29D EXIT PATH LIGHTING BROKEN HANGING. CORRECTIVE ACTION: SECURED LIGHTING ASSY. OK FOR SERVICE. (4516540)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 74,403 hrs · 35,022 cycles

SHIP 3252 - DIV - TO RIC DUE TO F/CTL SLATS LOCKED ECAM MESSAGE AND WEATHER IN RDU. CORRECTIVE ACTION: PERFORMED SLATS AND FLAPS OPERATIONAL TEST. OPS CHECK GOOD. CONTINUED IN SERVICE. (4398562)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,853 hrs · 34,734 cycles

SHIP 3252 - ATO - DISCONTINUED TAKE OFF IN MSP AT APPROXIMATELY 10-15KTS DUE TO BRAKES SYS 1 FAULT. CORRECTIVE ACTION: REPLACED BSCU. OPS CHECK GOOD. (LP 9485062)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,705 hrs · 34,644 cycles

SHIP 3252 ON DECENT, R FWD CABIN DOOR MESSAGE. CORRECTIVE ACTION: FOUND OBSTRUCTION ON R FWD/PAX CREW DOOR HOOK PROX. SW. AND DOOR FRAME. REINSTALLED TRIM AROUND DOOR AS REQUIRED. PERFORMED OPERATIONAL TEST OF THE DOOR WARNING SYSTEM OF R FWD PAX/CREW DOOR PER A320 AMM 52-71. MULTIPLE OPS TESTS OK. (4813462)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,440 hrs · 34,521 cycles

SHIP 3252 AT 3000FT AGL MASTER CAUTION L FWD CABIN DOOR. WENT OUT AFTER 3 SECONDS. OCCURRED AGAIN ON FINAL APPROACH. CORRECTIVE ACTION: CLEANED L1 DOOR SILL AREA. L1 DOOR GND OPS CKD NML. ALL INDICATIONS NML. NO 90 DAYS HISTORY. A/C OK FOR SVC. (4706132)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,190 hrs · 34,372 cycles

SHIP 3252 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:21D. CORRECTIVE ACTION: RECONNECTED ELECTRICAL CONNECTOR. OK FOR SERVICE. (2684412)

Part: LIGHT — UNSECURE (SEAT 24D) · airframe 72,681 hrs · 34,090 cycles

EMERGENCY EXIT PATH LIGHT AT SEAT 24D WAS DAMAGED. SECURED EMERGENCY EXIT PATH LIGHT IAW AMM 33-50.

Part: FITTING — MECHANIC ERROR (RT MLG) · airframe 72,485 hrs · 33,983 cycles

RIGHT MLG FWD ACTUATOR FITTING FASTENERS HOLE FOUND TOOLING MARKS. CORRECTIVE ACTION: COMPLIED WITH MULTIPLE ERA'S.

Part: FITTING — MECHANIC ERROR (RT MLG) · airframe 72,485 hrs · 33,983 cycles

RIGHT MLG ACTUATOR AFT FITTING FASTENERS HOLE FOUND TOOLING MARKS AD RELATED. CORRECTIVE ACTION: COMPLIED WITH MULTIPLE ERA'S.

Part: FASTENER — LOOSE (RT MLG DOOR) · airframe 72,485 hrs · 33,983 cycles

RT LANDING GEAR DOOR ACTUATOR UPPER FITTING HAS NUMEROUS LOOSE FASTENERS. AD RELATED. COMPLIED WITH MULTIPLE ERAS.

Part: NOT REPORTED — CRACKED (NOT REPORTED) · airframe 72,485 hrs · 33,983 cycles

HOLE #18 FOUND CRACK FIRST LAYER. CORRECTIVE ACTION: COMPLIED WITH MULTIPLE ERA'S.

Part: NOT REPORTED — DAMAGED (NOT REPORTED) · airframe 72,485 hrs · 33,983 cycles

HOLE #17 FOUND DAMAGED BETWEEN 1ST-2ND LAYERS. COMPLIED WITH MULTIPLE ERA'S. (2553277)

Part: NOT REPORTED — DAMAGED (NOT REPORTED) · airframe 72,485 hrs · 33,983 cycles

HOLE #19 FOUND CRACK ON 3RD LAYER. COMPLIED WITH MULTIPLE ERA'S. (2553279)

Part: PLATE — MECHANIC ERROR (RT MLG) · airframe 72,485 hrs · 33,983 cycles

RIGHT MLG ACTUATOR FITTING CONNECTOR PLATE AFT AND FWD FASTENERS HOLE FOUND TOOLING MARKS. COMPLIED WITH MULTIPLE ERA'S.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,912 hrs · 34,761 cycles

SHIP 3252 RH MLG DOOR ACTUATOR FITTING HAD 8 LOOSE FASTENERS. CORRECTIVE ACTION: CORRECTIVE ACTION: COMPLIED WITH ERA 604408-14AD REV A. (2552393)

Part: NONE — NONE (NONE) · airframe 72,485 hrs · 33,983 cycles

NEED TO COMPLY WITH PRI 604353-14AD REV 0, PRI 604353-14AD REV 1, PRI 604353-14AD REV 2, PRI 604353-14AD REV 3, PRI 604353-14AD REV 4, PRI 604353-14AD REV 5 AND FINAL ERA 604353-14AD REV ORIGINAL. COMPLIED WITH. (2551196)

Part: STRINGER — CRACKED · airframe 72,476 hrs · 33,979 cycles

SHIP 3252 FOUND CRACK INDICATION AT STGR22 AFT SIDE LOWER RADIUS NEAR THE DOOR-STOP. CORRECTIVE ACTION: COMPLIED WITH ER/A 604431-14AD. (2545769)

Part: NONE — NONE (NONE) · airframe 72,496 hrs · 33,988 cycles

MUST COMPLY WITH ERA 604353-14 SECTION I. CORRECTIVE ACTION: COMPLIED WITH.

Part: NONE — NONE (NONE) · airframe 72,476 hrs · 33,979 cycles

SHIP 3252 NEED TO COMPLY WITH ERA 604431-14AD SECTION I CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH. OK TO CONTINUE ON MON. (2541735)

Part: NONE — NONE (NONE) · airframe 72,476 hrs · 33,979 cycles

SHIP 3252 COMPLY WITH ERA 604431-14AD SECTION I CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH. CONTINUE ON MON. (2541754)

Part: NONE — NONE (NONE) · airframe 72,476 hrs · 33,979 cycles

SHIP 3252 NEED TO COMPLY WITH ERA 604431-14AD SECTION I CRACK INSP. CORRECTIVE ACTION: COMPLIED WITH. OK TO CONTINUE ON MON. (2541742)

Part: NONE — NONE (NONE) · airframe 72,476 hrs · 33,979 cycles

SHIP 3252 NEED TO COMPLY WITH ERA 604431-14AD SECTION I CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH. OK TO CONTINUE ON MON. (2541749)

Part: ACTUATOR — WORN (TE FLAPS) · airframe 72,476 hrs · 33,979 cycles

FLAP ACTUATOR WORN. R & R FLAP ACTUATOR PER DELTA WORK DOCUMENT 2754-4001-LT.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 72,306 hrs · 33,897 cycles

SHIP 3252 - ATB/MISC - TO SLC DUE TO MULTIPLE BIRD STRIKES ON CLIMB. CORRECTIVE ACTION: BORO-SCOPED #2 ENGINE. REPLACED BENT FAN BLADE. REPLACED RECIRCULATION FILTERS AND PERFORMED DUCT BURN-OUT. PERFORMED OVERWEIGHT LANDING INSPECTION. REPLACED LANDING LIGHT. OK FOR SERVICE. (9815743)

Part: NONE — NONE · airframe 72,306 hrs · 33,897 cycles

SHIP 3252 #35 AND #17 FAN ROTOR BLADE DAMAGED DUE TO BIRD STRIKE. CORRECTIVE ACTION: R/R FAN BLADES PER A320 AMM 72-21. (9815747)

Part: NONE — NONE · airframe 72,011 hrs · 33,713 cycles

SHIP 3252 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:21D. CORRECTIVE ACTION: REATTACHED LIGHTING ASSY. OK FOR SERVICE. (2430009)

Part: NONE — NONE · airframe 71,444 hrs · 33,389 cycles

SHIP 3252 F/A REPORTED DIRTY SOCK SMELL ON DESCENT. AFT GALLEY IS MORE PRONOUNCED THAN THE REST OF THE CABIN. ENTIRE AIRCRAFT SMELLS LIKE A GYM LOCKER ROOM WHEN APU BLEED IS ON. CORRECTIVE ACTION: OIL FOUND IN APU COMPARTMENT. DECONTAMINATED APU COMPARTMENT AND BURNED OUT DUCTS. REPLACED CABIN FILTERS. OK FOR SERVICE. (9165154)

Part: NONE — NONE · airframe 70,348 hrs · 32,767 cycles

SHIP 3252 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS:601. CORRECTIVE ACTION: CLEANED + LUBED GIRT BAR ARMING ASSY. OPS CK OK. (2117463)

Part: NONE — NONE · airframe 69,697 hrs · 32,357 cycles

SHIP 3252 RIGHT BELLY FAIRING PANEL MISSING. CORRECTIVE ACTION: DEFERRED TO CDL, SLIDING PANEL P/N D5337189600500 ON ORDER. (8168906)

Part: FRAME — CRACKED (FRM 20) · airframe 68,831 hrs · 31,827 cycles

SHIP 3252 DURING INSPECTION PER 5310-3024 (ALI 531155-02-1) CRACKS FOUND IN FR 20 LHS IN HOLES #8,#A, AND #C. CORRECTIVE ACTION: COMPLIED WITH ERA 589650-14AD. OK TO CONTINUE ON MONITOR INSPECTION. (1750640)

Part: FRAME — OUT OF LIMITS (FWD GALLEY AREA) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 OUT OF LIMIT FRAME 20 RH HOLE 11 DOOR STOP 1 AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER SECTION III PRI 550431-14AD REV.0 REV.1 REV.2 AND ER/A 550431-14AD REV.B. (1742183)

Part: FRAME — CRACKED (FWD GALLEY AREA) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 20 RH SIDE ON HOLE A OF INSPECTION AREA AT L EVEL OF DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 550431-14AD REV.0 PRI REV1 PRI REV2 AND ER/A 550431-14AD REV.B. (1742193)

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 20 LH SIDE ON HOLE C OF INSPECTION AREA AT LEVEL OF DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 589650-14REV.0, RRV:1, REV: 2, AND ERA 589650-14AD REV : ORIGINAL. (1741906)

Part: FRAME — CRACKED (FWD GALLEY) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 20 LH SIDE ON HOLE A OF INSPECTION AREA AT LEVEL OF DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 589650-14 REV:0, REV:1, REV:2 AND ERA :589650-14AD REV: ORIGINAL. (1741925)

Part: FRAME — CRACKED (FWD GALLEY) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 20 LH SIDE ON HOLE 8 OF INSPECTION AREA AT LEVEL OF DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 589650-14 REV:0, REV:1, REV:2, AND ERA 589650-14AD REV: ORIGINAL. (1741920)

Part: FRAME — CORRODED (FRM 20) · corrosion level 2 · airframe 67,722 hrs · 31,288 cycles

SHIP 3252 DURING INSPECTION CRACKS AND CORROSION FOUND ON SEVERAL HOLES #5,#6,#11,#12 IN FR20 RHS. CORRECTIVE ACTION: INSPECTED. REQUIRES REPETITVE INSPECTION PER ER/A 32-550431. OK FOR SERVICE AT THIS TIME. (1742017)

Part: FRAME — CRACKED (FWD GALLEY) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 16 LH SIDE ON HOLE 7 AT LEVEL OF DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 589659-14AD REV:0, 1, 2, AND ERA: 589659-14AD REV: ORIGINAL. (1741951)

Part: FRAME — CRACKED (FWD GALLEY AREA) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 16 LH SIDE ON HOLE 8 OF INSPECTION AREA AT LEVEL OF DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED REPAIR PER PRI 589659-14AD REV D,1,2 AND ER/A 589659-14AD REV ORIGINAL. (1741954)

Part: CROSSBEAM — CRACKED (UNKNOWN) · airframe 75,800 hrs · 35,778 cycles

DURING INSPECTION PER 5310-3024 (ALI 531155-02) CRACKS AND CORROISON FOUND ON SEVEAL HOLES #5,#6,#11,#12 IN FR20 RHS FOUND DAMAGED. C/A: PER SECTION DTE OF 550431-14AD, REV B, THE REPAIR OF SECTION III AT CROSSBEAM SPLICE AREA IS LIMITED TO 87,700 FC SERVICE AFTER SECTION III. ADDITIONAL ENG'G AUTHORIZATION RQUIRED FOR SERVICE BEYOND THIS LIMIT. ASSOCIATED ER/A 32-550431 ADDED FOR AC 3252. THIS LOG PAGE IS SUPERSEDED BY LOG PAGE 0252469, OK TO CLOSE LOG PAGE 1742020. (LP: 1742020)

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 16 RH SIDE ON HOLE 7 OF INSPECTION AREA AT LEVEL OF DOOR STOP 7 AT FWD GALLEY AREA. CORRECTIVE ACTION: PERFORMED TIME LIMITED REPAIR ON FRAME PER PRI #589654-14AD REV.0,1 AND ER/A #589654-14AD REV.ORIGINAL. (1741070)

Part: SKIN — GOUGED (FUSELAGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 GOUGE EXTERNAL SKIN LOC. BTW FR 50 TO FR 51 STR 40L TO STR 42 AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 51-42-11 AND A320 SRM 51-72-11 AND ER/A 589897- 14 REV. ORIGINAL AND PRI 589897-14 REV.0. OK FOR SERVICE. (1737427)

Part: FRAME — CRACKED (FRM 16) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA ON FRAME 16 LT DOOR STOP 7 HOLE 3. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ERA 589599-14 REV. ORIGINAL AND PRI 589599-14 REV.0. (1737411)

Part: FRAME — CRACKED (FRM 16) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 16 AT FWD GALLEY AREA ON FRAME 16 RT DOOR STOP 7 HOLE 3. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ERA 589607-14 REV. ORIGINAL AND PRI 589607-14 REV.0. RII. (1736005)

Part: FRAME — CRACKED (FRM 16) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 16 LT DOOR STOP 7 HOLE 1. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER PRI 589599-14 REV 0 AND ER/A 589599-14 REV. ORIGINAL. (1736013)

Part: FRAME — CRACKED (FRM 16) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK INDICATION ON FRAME 16 RT DOOR STOP 7 HOLE 1. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER PRI 589607-14 REV.0 ERA 589607-14 REV ORIGINAL. (1736000)

Part: BEARING — CORRODED (RUDDER HINGE) · corrosion level 2 · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION BEARING HINGE 6 ON THE RUDDER SIDE ON VERTICAL STABILIZER (1 EA). CORRECTIVE ACTION: REPLACED BEARING HINGE PER A320 AMM 55-46-11. (1735997)

Part: ROD END — DETERIORATED (PAX DOOR) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 DETERIORATED PASSENGER CREW DOOR 831 ROD END. CORRECTIVE ACTION: REPLACED AND RIGGED ROD END PER A320 AMM 52-11-21. OK FOR SERVICE. (1735478)

Part: BUSHING — CORRODED (LT WG FLAP TRACK) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION BUSHING FITTING ATTACH FLAP TRACK 3 CARRIAGE ON LT WING (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS PER AIRBUS CMM 27-54-46. (1734469)

Part: FLAP TRACK — CORRODED (RT WING) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION FLAP TRACK 2 PIVOT BOLT ON RT WING (1EA). CORRECTIVE ACTION: REMOVED AND INSTALLED NEW FLAP TRACK 2 PIVOT BOLT RT WING CARRIAGE BOLT AS PER A320 FAM AMM 27-54-61. (1734488)

Part: BEARING — CORRODED (RT WING TE FLAP) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION OB FLAP AT MAIN ECCENTRIC BEARING ON RT WING (1 EA). CORRECTIVE ACTION: REMOVED AND REPLACED ATTACHMENT BEARING PER A320 FAM AMM 57-53-21. (1734479)

Part: BEARING — CORRODED (RT WING TE FLAP) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION BEARING IB FLAP (MAIN ECCENTRIC BEARING) ON RT WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING PER AIRBUS CMM 57-52-21. (1733632)

Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION FLAP TRACK 3 PIVOT BOLT OB FLAP ON RT WING (1EA). CORRECTIVE ACTION: REPLACED FLAP TRACK 3 PIVOT BOLT PER A320 FAM AMM 27-54-62. (1733664)

Part: ATTACH FITTING — CORRODED (RUDDER HINGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION RUDDER HINGE FIXED BUSHING ATTACH FITTING HINGE NR 5 (RUDDER SIDE) ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHINGS (2EA) PER A320 SRM 51-72-12. (1733687)

Part: BUSHING — CORRODED (RUDDER HINGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION RUDDER HINGE FIXED BUSHING ATTACH FITTING HINGE NR 7 ( RUDDER SIDE) ON VERTICAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS PER AIRBUS SRM 51-72-12. (1733651)

Part: ATTACH FITTING — CORRODED (RUDDER HINGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION RUDDER HINGE FIXED BUSHING ATTACH FITTING HINGE NR 1 (RUDDER SIDE) ON VERTICAL STABILIZER (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 SRM 51-72-12. (1733672)

Part: ATTACH FITTING — CORRODED (RUDDER HINGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION RUDDER HINGE FIXED BUSHING ATTACH FITTING HINGE NR 2 (RUDDER SIDE) ON VERTICAL STABILIZER (2EA). CORRECTIVE ACTION: REPLACED BUSHING PER A320 SRM 51-72-12. (1733682)

Part: ATTACH FITTING — CORRODED (RUDDER HINGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION RUDDER HINGE FIXED BUSHING ATTACH FITTING HINGE NR 3 (RUDDER SIDE) ON VERTICAL STABILIZER (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2EA) PER A320 SRM 51-72-12. (1733680)

Part: ATTACH FITTING — CORRODED (RUDDER HINGE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION RUDDER HINGE FIXED BUSHING ATTACH FITTING HINGE NR 4 ( RUDDER SIDE) ON VERTICAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 SRM 51-72-12. (1733657)

Part: BOLT — CORRODED (LT FLAP TRACK) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION PIVOT BOLT OB FLAP TRACK 4 ON LT WING (1EA). CORRECTIVE ACTION: REMOVED AND REPLACED PIVOT BOLT PER A320 FAM AMM 27-54-62. (1733668)

Part: SUPPORT BRACKET — CORRODED (LT NACELLE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION AFT ATTACHMENT SUPPORT BRACKET BEARING AT PYLON LT (2EA). CORRECTIVE ACTION: REMOVED AND INSTALLED NEW BEARING PER A320 FAM AMM 54-51-17.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CRACK ON EMERGENCY EXIT DOOR 844 RH AFT LOAD TRANSMITTING PROFILE FWD. DOOR LOCATED IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FWD LOAD TRANSMITTING PROFILE PER A320 SRM 51-72-11 AND 51-42-11. OK FOR SERVICE. (1732082)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION FLOOR BEAM -Y1292 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (1732182)

Part: STRUT — CORRODED (LT WING TE FLAP) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION IB FLAP INTERCONNECTING STRUT ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT PER DELTA WORKCARDS AMDS 2750-6010-LT AND 2750-6020-LT. (1730439)

Part: CONTROL CABLE — DETERIORATED (PAX DOOR) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 DETERIORATED PASSENGER CREW DOOR 832 FLEXIBLE CONTROL CABLE OF EMERGENCY ESCAPE SLIDE MECHANISM. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 832 FLEXIBLE CONTROL CABLE PER DELTA WORK CARD AMDS 5210-7089. OPS CK GOOD. (1730655)

Part: SKIN — GOUGED (FRM 51 S40-42L) · airframe 75,800 hrs · 35,778 cycles

A GOUGE WAS FOUND IN EXTERNAL FUSELAGE SKIN BETWEEN FR50 - FR51 AND STR 40L - STR 42L. C/A: ***DTE REQUIRED*** PER SECTION DET OF 589897-14, THE REPAIR OF SECTION I IS LIMITED TO 63,000 FC / 132,000 FH TOTAL FROM FIRST FLIGHT (WHICHEVER COMES FIRST). ADDITIONAL ENG'G AUTHORIZATION IS REQUIRED FOR SERVICE BEYOND THIS LIMIT. CONTACT S. SOBIECH ASSOCIATED ER/A 32-589897 ADDED FOR AC 3252. (P: 1730403)

Part: SHEAR TIE — GOUGED (FRAME 25) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 GOUGE SHEAR TIE LOCATED AT FR 25 AND BTW STR 36L TO STR 37L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (1729201)

Part: STRUT — CORRODED (RT WING) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION IB FLAP INTERCONNECTING STRUT ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT RH PER DELTA WORKCARD AMDS 2750-6010-RT AND 2750-6020-RT. (1728301)

Part: SKIN — DAMAGED (NR 2 SLAT TE) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 BROKEN SLAT 2 TRAILING EDGE AND IB SIDE ON LH WING. PERFORMED PERMANENT REPAIR PER A320 SRM 57-43-21. (1725165)

Part: DOOR — OUT OF ADJUST (MAIN PAX) · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 PASSENGER CREW DOOR 841 OUT OF ADJUSTMENT. CORRECTIVE ACTION: PERFORMED ADJUSTMENT ON PASSENGER CREW DOOR PER A320 FAM AMM 52-11-14. OK FOR SERVICE. (1725109)

Part: WEB — CORRODED (FWD GALLEY) · corrosion level 2 · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION WEB LOCATED -Y1732 AND FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION REPLACED WEB PER A320 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 67,698 hrs · 31,278 cycles

SHIP 3252 CORROSION SEAT TRACK +Y765 AND FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION REPLACED SEAT TRACK PER A320 SRM 51-72-11.

Part: GUST LOCK — INOPERATIVE (PAX DOOR) · airframe 66,917 hrs · 30,853 cycles

SHIP 3252, MAIN DOOR GUST LOCK WILL NOT ENGAGE. CORRECTIVE ACTION: CLEANED AND EXERCISED GUST LOCK MECHANISM. OPS CHK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,608 hrs · 30,653 cycles

EXTERIOR LEFT OVERWING EMERGENCY EXIT LIGHTS INOP, REPLACED THE LAMPS FOR THE LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS

Part: FITTING — DAMAGED (LT WING TE FLAP) · airframe 65,860 hrs · 30,299 cycles

L/H INBD FLAP TRUNNION FITTING FOUND DAMAGED BEYOND REPAIR, REPLACED L/H INBD FLAP TRUNNION FITTING PER ERA 584216-14AD REV " O"

Part: LIGHT — BROKEN (SEAT 12D) · airframe 65,358 hrs · 30,046 cycles

SEAT 12D EMERGENCY LIGHT HOLDER ASSY BROKEN, REPLACED SEAT 12D EMERGENCY PATH LIGHT ASSY

Part: PLENUM — ABNORMAL (APU) · airframe 65,269 hrs · 29,986 cycles

BURNED OIL TYPE ODOR ON BOARD WITH APU SUPPLY BLEED TO PACKS, FOUND APU COMPARTMENT INTAKE PLENUM CONTAMINATED WITH OIL, DEEP CLEANED APU COMPARTMENT AND REPLACED APU

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 65,192 hrs · 29,948 cycles

EMERGENCY LIGHT TEST FAULT "EPSU BATT EMER R" MSG DISPLAYED, REPLACED BATTERY PACK (12WL)

Part: PRESSURE PANEL — CRACKED (FRAME 36) · airframe 63,688 hrs · 29,157 cycles

CRACK INDICATION ON INTERNAL STRUCTURE FITTING HOLE #7 OF THE PRESSURE PANEL LOC. FR 36 AND Y+1295 LEFT SIDE IN FWD CARGO COMPARTMENT .(CRACK INDICATION 6 O"CLOCK), REPLACED FITTING OF THE PRESSURE PANEL LOC. AT FR.36 AND AT LEVEL STR.30 Y+1295 ON INTERNAL STRUCTURE IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-72-11 AND DWG #D57130101, RELEASE DATE 30-NOV-12 D53370500 RELEASE DATE 11-JAN-01, ISSUE J DWG #D57130101 AND ISSUE AQ DWG #D53370500

Part: BEAM — CRACKED (FRAMES 35-36) · airframe 63,688 hrs · 29,157 cycles

CRACK INDICATION ON FRAME 35 TO FR 36 LH SIDE LOCATED AT LONGITUDINAL BEAM AT HOLE ''A'' PRESSURE FLOOR PANEL ON LOWER FUSELAGE (1 EA) .(CR ACK POSITION AT 9 O'CLOCK. REPAIR IN ACCORDANCE WITH WORK CARD 5311-01 171-04A PRIOR TO FURTHER FLIGHT,"AA 5311-01171","SB A320-53-1264 ", "AD-2018-06-04".) PERFORMED REPAIR ON FR35 TO FR36 4H SIDE LOC. AT LONGITUDINAL BEAM PRESSURE FLOOR PANEL ON LOWER FUSELAGE. HOLE "A". REPAIR WAS ACCOMPLISCHED IN ACCORDANCE WITH WORK CARD 5311-01171-04A, AA5311-01171, SBA320-53-1264: AD-2018-06-04.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 63,455 hrs · 29,058 cycles

EMERGENCY CABIN LIGHTS CAME ON AND WENT TO OFF DURING FLIGHT. ON TOUCHDOWN LIGHTS RE-ILLUMINATED. RESET BOTH EMERGENCY LIGHT SWITCHES. OPERATION CHECKS OKAY.

Part: UNKNOWN — FUMES (NR 1 ENGINE) · airframe 63,269 hrs · 28,979 cycles

CLIMBING THROUGH 300 AGL COCKPIT BEGAN TO SMELL LIKE WET MOLDY MILDEW SOCK. GOT STRONGER UNTIL 8000FT WHEN SMELL TAPERED OFF. GONE Y 23000FT. MAINTENANCE ISOLATED SOURCE OF FUMES TO ENGINE NR 1. PERFORMED WC 7900-2001. NO DEFINITE FINDINGS. PERFORMED VERIFICATION FLIGHT.

Part: FILTER — ODOR (CABIN) · airframe 62,128 hrs · 28,436 cycles

OIL SMELL IN COCKPIT CLOSE TO LANDING IN MCO. SMELL CLEARED AFTER LANDING. MAINTENANCE COMPLIED WITH NO GO ODI PREVENTION PROGRAM. BOROSCOPED BOTH ENGINES. REPLACED OZONE AND RECIRC FAN FILTERS. PERFORMED HIGH POWER RUNS. NO ODOR. MCC NOTIFIED.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,698 hrs · 31,278 cycles

TOP SKIN CORROSION REPAIRED, PER ERA 533453-14 SECT I, APPROVED AS PERM, CAT 'B'. NEW RDAS CHANGES REP INSP INTERVAL, A/C TYPE EFFECT. CORRECTIVE ACTION: PERFORMED DVI ON REWORKED AREA LOCATED CENTER WING BOX UPPER SKIN PANEL UPPER SURFACE FR 42 AND Y1292, AS PER NTM 51-90-00, ER/A 533453-14 REV A, SECTION II, OK TO CONTINUE MONITOR JOB COMPLETE.

Part: ENGINE — LEAKING · airframe 58,371 hrs · 26,619 cycles

CONDITION AIR STINKS, BORESCOPED HPC1 AND 2, DISCOVERED OIL ON ALL BLADES, PRESENCE OF OIL AT BOOSTER OUTLET. REPLACED POWERPLANT AND REPLACED LT AND RT CABIN AIR RECIRCULATION FILERS AND LEFT PACK OZONE FILTER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATIONS FWD RT PASSENGER DOOR FASTENER. OVERSIZE REAMED HOLE AND INSTALLED FASTENER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATION AT FWD RT PASSENGER DOOR FASTENER. REAM OVERSIZED HOLE, INSTALLED FASTENER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATION AT FWD LT PASSENGER DOOR FASTENER. OVERSIZED REAM AND INSTALLED FASTENER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATION AT FWD LT PASSENGER DOOR FASTENER. REAM OVERSIZED HOLE AND INSTALLED FASTENER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATIONS FWD RT PASSENGER DOOR FASTENER FWD 2ND FASTENER DOWN AREA B FR 20. REAM OVERSIZED HOLE, INSTALLED FASTENER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATION AT FWD LT PASSENGER DOOR FASTENER. REAM OVERSIZED HOLE AND INSTALLED FASTENER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATION AT FWD RT PASSENGER DOOR FASTENER. OVERSIZE REAMED AND INSTALLED FASTENER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATION AT FWD LT PASSENGER DOOR FASTENER. OVERSIZED REAMED HOLE AND INSTALLED FASTENER.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 57,341 hrs · 26,118 cycles

CORROSION AND CRACK INDICATION AT FWD RT PASSENGER DOOR FASTENER. REAM OVERSIZED HOLE AND INSTALLED FASTENER.

Part: GEARBOX — LEAKING · airframe 54,347 hrs · 24,659 cycles

PILOT REPORTED VERY STRONG ODOR, CHEMICAL LIKE, PRESENT IN CABIN AND COCKPIT UPON BOARDING AND ALL OF FLIGHT. IRRITATING TO EYES, CAPTAIN, AND VERY BOTHERSOME. APU GENERATOR OIL DRAIN PLUG DRIPPING ON TO PLENUM. REPLACED SEAL WASHER, FOUND OIL LEAKING FROM GEARBOX AT COOLING FAN DUCT. INSIDE DUCT GOING TO OIL COOLER SOAKED IN OIL. COOLING FAN SOAKED IN OIL AND COKING APPEARS. REPLACED OIL COOLER FAN.

Part: SUPPORT — CORRODED (MLG) · airframe 57,341 hrs · 26,118 cycles

CORROSION FOUND ON RIB GEAR SUPPORT AT RIB 5 AREA OF LT WING. REPAIRED IAW ER/A.

Part: FRAME — CORRODED (FRM 20) · airframe 57,341 hrs · 26,118 cycles

OUT OF LIMITS CORROSION SPOTS FOUND ON THE INBD FLANGE OF FRAME 20 RT. REPAIRED IAW ER/A.

Part: WEB — CORRODED (FRAMES 58-59) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON WEB LOWER SURFACE AT LEVEL STR 38L IN AFT CARGO COMPARTMENT BETWEEN FRAME 58 TO FRAME 59, L=1.500", W=1.000", D=0.002". MEASURES APPROXIMATELY SSI 534107. REPLACED WEB LOWER SURFACE AT LEVEL STR 38L IN CARGO COMPARTMENT BETWEEN FRAME 58 TO FRAME 59 IAW SRM 51-72-11 AND DWG D53470320, E53470320.

Part: STRINGER — CORRODED (FRAMES 56-58) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN AFT CARGO COMPARTMENT BETWEEN FRAME 56 TO FRAME 58+3", L=7.000", W=1.000", D=0.004", MEASURES APPROXIMATELY SSI 534107, CARD 534107. CARD 5320-5012-DE ATTACH FROM 5100-3201. IF CORROSION IS LEVEL 2 OR GREATER. REPLACED STRINGER 43L BETWEEN FRAME 54 TO FRAME 60 IN AFT CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53470345, MEASURES OF CORRODED AREA L=7", W=1", D=0.004". TOOL USED, CALIPER, PN 500-196-30, SN 14333405, DUE DATE FEB-14-2016, ATTACHED SSI FROM REPORT 5100-3201.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-67) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM -Y310 AT AFT GALLEY AREA FROM FRAME 65 TO FRAME 67, L=2", W=1", D=0.003". REPLACED FLOORBEAM -Y318 AT AFT GALLEY AREA FROM FRAME 65 TO FRAME 67 IAW SRM 51-72-11, DWG D534 72814.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM, Y1292 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66, L=5", W=2", D=0.003". REPLACED FLOORBEAM Y1292 LOCATED AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66 IAW SRM 51-72-11 AND DWG D53472815.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LT SIDE AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68, L=2", W=1", D=0.003". REPLACED LOWER SILL LT SIDE AND FASTENERS LOCATED ON AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 IAW SRM 51-72-11 AND DWG NR D53480019.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1162 AT AFT GALLEY AREA FROM FRAME 68 TO FRAME 69, L=5", W=3", D=0.003". REPLACED FLOORBEAM -Y1162 AT AFT GALLEY AREA FROM FRAME 68 TO FRAME 69 IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM -Y1292 AT AFT GALLEY AREA ON FRAME 66, L=1", W=0.50", D=0.002". REPLACED FLOORBEAM -Y1292 AT AFT GALLEY AREA LOCATED BETWEEN FRAME 64 TO FRAME 66 IAW SRM 51-72-11 AND DWG D534 72816.

Part: SUPPORT — CORRODED (FRAMES 66-68) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL AT STR 23R AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68, L=0.500", W=0.300", D=0.002". REPLACED LOWER SILL AT STR 23R AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FRAME 66) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM BETWEEN Y1292 AND Y1162 AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68, L=8", W=3", D=0.004". REPLACED FLOORBEAM BETWEEN Y1292 AND Y1162 AFT GALLEY AREA FROM FRAME FR 68 IAW SRM 51-72-11 AND DWG D534 72800 AND D534 72815.

Part: FITTING — CORRODED (FRAME 68) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68 LT SIDE AT AFT GALLEY AREA. REPLACED CORNER FITTING LOCATED FRAME 68 LT SIDE AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.

Part: FITTING — CORRODED (FRAME 68) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68 RT AT AFT GALLEY AREA, MEASURES APPROXIMATELY L:1", W:0.437", D:0.002". REPLACED CORNER FITTING AT FRAME 68 RT AFT GALLEY AREAS IAW SRM 51-72-11 AND DWG D534-80019.

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER COUPLING AT STR 42L BETWEEN FR 30 AND 31 IN FWD CARGO COMPARTMENT. MEASURES APPROXIMATELY L:0.5", W:0.339, D:0.002". REPLACED COUPLING AT STR 42L BETWEEN FR 30 AND FR 31 IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231712.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1162 AT AFT GALLEY AREA FROM FRAME 68 TO FRAME 69, L=3", W=2", D=0.003". REPLACED FLOORBEAM +Y1162 AT AFT GALLEY AREA FROM FRAME 68 TO FRAME 69 IAW SRM 51-72-11 AND DWG D53472800.

Part: FLOOR SUPPORT — CORRODED (GALLEY) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL CENTER FITTING RT AT AFT GALLEY AREA . MEASURES APPROXIMATELY L=0.376", W=0.231", D=0.002", SSI 534147. REPLACED CENTER FITTING RT AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1292 AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20, L=2", W=1", D=0.005". REPLACED FLOORBEAM -Y1292 AT FWD GALLEY AREA FROM FR 12 TO FR 24 IAW SRM 51-72-11 AND DWGS D53112812, D53110920, D53110984.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1292 AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 20, L=0.500", W=0.300", D=0.002. REPLACED FLOORBEAM +Y1292 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWGS D53112812, D53110920.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM -Y465 AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 67, L=8", W=3", D=0.006". REPLACED FLOORBEAM -Y465 LOCATED AFT GALLEY AREA FROM FRAME 64 TO FRAME 67+5" IAW SRM 51-72-11 AND DWG D53472816.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM-Y765 AT AFT GALLEY AREA ON FRAME 68, L=1", W=0.50", D=0.003". REPLACED FLOORBEAM -Y765 AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 70 IAW SRM 51-72-11 AND DWG D53472800.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT AFT GALLEY AREA ON FRAME 66 L =3", W=1", D=0.003". EVALUATED FLOORBEAM -Y765 AT AFT GALLEY AREA FROM FR 64 TO FRAME 66 IAW SRM 51-72-11 AND DWG D5347832, D53472816.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-21) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y254 AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 21, L=0.700", W=0.300", D=0.003". REPLACED FLOORBEAM +Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53112816.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE LONGITUDINAL BEAM RT SIDE AT AFT GALLEY AREA FROM FRAME 65 TO FRAME 66, L=3", W=1", D=0.004". SSI 534147. REPLACED FLOORBEAM LOCATED BTE FRAME 65 TO FRAME 66 AND -Y1450 TO -Y1589 AND FASTENERS IAW SRM 51-72-11 AND DWGS D53474250 AND D53472750.

Part: FLOORBEAM — CORRODED (FRAME 68) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND ELONGATED HOLE FLOOR STRUCTURE CROSS SECTION + Y1162 AT AFT GALLEY AREA ON FRAME 68, SSI 534147. REPLACED CROSS SECTION FLOOR STRUCTURE Y1162 AT AFT GALLEY AREA ON FRAME 68 IAW SRM 51-72-11 DWG D53474250.

Part: FITTING — CORRODED (FRAMES 16-19) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 19 AND STRINGER 23. LT SIDE SSI 531180, REPLACED CENTER FITTING AND FASTENERS LOCATED AT FWD GALLEY AREA FROM FRAME 16 TO FRAME 19 AND STR 23L IAW SRM 51-72-11 AND DWG D53112225.

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON RAIL DUMMY -Y81 AT FWD GALLEY AREA FROM FRAME 12 TO FRAM E 16, L=2", W=1", D=0.003", 531189. REPLACED RAIL DUMMY -Y81 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 16 IAW SRM 51-72-11 AND DWG D53112828.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE LONGITUDINAL LT SIDE AT AFT GALLEY AREA FROM FRAME 65 TO FRAME 66, L=1", W=0.50", D=0.003". SSI 534147. REPLACED FLOOR STRUCTURE LONGITUDINAL LT SIDE AT AFT GALLEY AREA FROM FRAME 65 TO FRAME 66 IAW SRM 51-72-11 AND DWG D53474250,D53472750.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y765 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 16, L=3", W=2", D=0.002", SSI 531189. REPLACED FLOORBEAM +Y765 LOCATED ON FWD GALLEY AREA FROM FR 12 TO FR 24 IAW SRM 51-72-11 AND DWG D53110984 AND D53110920.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y765 AT AFT GALLEY AREA ON FRAME 68 L=2", W=1", D=0.002", SSI 534147. REPLACED FLOORBEAM Y765 AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 70 IAW SRM 51-72-11 AND DWG D53472816, D53472800.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM Y765 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66, L=2", W=1", D=0.002". SSI 534147. REPLACED FLOOR STRUCTURE BEAM Y765 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66 IAW SRM 51-72-11 AND DWG D53472832.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 34 BETWEEN STR 43R AND STR 44 IN FWD CARGO COMPARTMENT, MEASURES APPROXIMATELY L:0.559", W:0.219", D:0.002", SSI 532180. REPLACED CLEAT AT FRAME 34 BETWEEN 43R AND STR 44 IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231626.

Part: DUMMY RAIL — CORRODED (FRAMES 20-21) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON RAIL DUMMY -Y189 AT FWD GALLEY AREA FROM FRAME 20 TO FRAME 21, L=2", W=1", D=0.004", SSI 531189. REPLACED RAIL DUMMY -Y189 AT FWD GALLEY AREA FROM FRAME 20 TO FRAME 24 IAW SRM 51-72-11 AND DWG D53112834.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 31 BETWEEN STR 42R AND STR 43R IN FWD CARGO COMPARTMENT. MEASURES APPROXIMATELY L:0.762", W:0.596", D:0.002", SSI 532180. REPLACED CLEAT AT FR 31 BETWEEN STR 42R AND STR 43R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231712.

Part: SHEAR TIE — CORRODED (FRAME 34) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 34 BETWEEN STR 42R AND STR 43R IN FWD CARGO COMPARTMENT. MEASURES APPROXIMATELY L:0.718", W:0.250", D:0.002", SSI532180. FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231712.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y512 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66, L=12", W=3", D=0.004", SSI 534147. REPLACED FLOORBEAM +Y512 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66 IAW SRM 51-72-11 AND DWG D53472815.

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · airframe 52,326 hrs · 23,696 cycles

DURING INSPECTION, FOUND CORROSION ON RAIL DUMMY Y503.2 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 16, L=2", W=1", D=0.004". REPLACED RAIL DUMMY Y503.2 AT FWD GALLEY AREA FROM FR12 TO FR16 IAW SRM 51-72-11 AND DWG D53112825 AND D53110984.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,906 hrs · 19,642 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 15 INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AND OPS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 5,319 hrs · 2,331 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 10C INOPERATIVE. MAINTENANCE RE-SEATED LOOSE CONNECTOR UNDER SEAT 10C AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · airframe 40,495 hrs · 18,096 cycles

FUSELAGE FROM FR 69 TO 70 AROUND VACUUM OUTLET HAS CORROSION. BLENDED AREA IAW SRM 51-73-00. DIM; L=1.0" W=0.3" D=0.009" OUT OF LIMITS IAW SRM 53-41-11. CUT OUT IAW SRM 53-41-11 FIG 205. FABBED REPAIR PARTS IAW SRM 53-41-11. PERFORMED HFEC IAW NTM 51-00-08, INSTALLED REPAIR PARTS IAW SRM 51-42-11 & SRM 53-41-11, REPAIRED IAW SRM 53-41-11. FIRST INSP AFTER REPAIR REQ AT 53900 FC & SUB INSP AT INTERVALS OF 18000 FC.

Part: BOTTLE — EMPTY (DOOR ASSIST) · airframe 39,181 hrs · 17,545 cycles

DURING LINE CHECK FOUND DOOR 1R, DOOR ASSIST BOTTLE IS DEPRESSURIZED FRANGIBLE DISK IS RUPTURED. R & R 1R DOOR DAMPER EMERGENCY OPERATING CYLINDER IAW AMM 52-11-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,506 hrs · 16,804 cycles

DURING A NON ROUTINE CHECK, THE EMERGENCY POWER SUPPLY UNIT FAILED TEST. REPLACED EPSU AND CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: PACKING — LEAKING (YELLOW PTU MANIF) · airframe 8,946 hrs · 3,932 cycles

DURING CRUISE RECEIVED "HYD Y RSVR LO LVL" MESSAGE. SHUT DOWN THE YELLOW HYDRAULIC SYSTEM PER COM PROCEDURES AND CONTINUED TO FINAL DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING O-RING ON LINE BETWEEN PTU MANIFOLD AND PTU. RESERVICED SYSTEM. NO LEAKS NOTED.