N331NW

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,776 hrs · 42,359 cycles

SHIP3231 DISC: UPON REMOVAL OF THE R-2 DOOR SLIDE COVER, FOUND SLIDE UNRAVELED. C/A: REMOVED AND REPLACED R-2 DOOR SLIDE PER AMDS TASK CARD 2561-4002 -RA. REFERENCE JOB 26-0001. (LP: 0071564)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,679 hrs · 42,309 cycles

SHIP 3231 L/H MLG TOOLING MARKS IN LOWER WING SKIN JUST FWD OF REAR PINTLE FITTING. CORRECTIVE ACTION: REMOVED TOOLING MARKS IN AFOREMENTIONED AREA B THE FWD OF REAR FITTING DONE IAW SRM A320 SRM 51-73 AND REAPPLIED PROTECTIVE COATING PAINT. (2998659)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,566 hrs · 42,235 cycles

SHIP 3231 - ATO - AT LESS THAN 10 KTS DUE TO BRAKES SYS 1 FAULT ECAM MESSAGE. CORRECTIVE ACTION: BSCU CHANNEL 1 PLACED ON MEL DEFERRAL. OK TO CONTINUE. (9629806)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,112 hrs · 41,993 cycles

SHIP 3231 - ATO - AT APPROXIMATELY 50KTS DUE TO ENG 1 REV UNLOCK MESSAGE. CORRECTIVE ACTION: DEFERRED #1 T/R PER MEL AND CONTINUED. (9651684)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,984 hrs · 41,914 cycles

SHIP 3231 PLASTIC EMERG LIGHT HOUSING ON SEAT 31D HANGING DOWN. CORRECTIVE ACTION: R/R PLASTIC EMERG LIGHT HOUSING AT 31D. OK FOR SERVICE. (9956797)

Part: NONE — NONE · airframe 89,051 hrs · 41,392 cycles

SHIP 3231 ON APPROACH TO KMSO SEVERE ICING AT 17000 FT IMMEDIATELY EXIT ICING CONDITIONS, WING PLUS ENG ICE ON FOR SEVERAL MINUTES PRIOR TO ICING CONDITIONS. IN SEVERE ICE FOR 45 SECONDS N1 VIBE 9.9 FOR ABOUT 30 SECONDS N1 VIBE DECREASE TO NORMAL OVER THE NEXT FOUR MINUTES. THIS OCCURRED ON THE NBR.2 ENG. THE NBR.1 ENG HAD NORMAL VIBRATION DURING THE EVENT. DIVERT TO KGEG. CORRECTIVE ACTION: PERFORMED VISUAL INSPECTION OF NBR.2 ENG IAW A320 AMM 05-51-45-200-001-A. NO DAMAGE WAS FOUND PER TSM NO DAMAGE FOUND NO FURTHER MAINTENANCE ACTION REQUIRED. A/C OK FOR SERVICE. (9850278)

Part: PROXIMITY SENSOR — FAULTED (EMERGENCY EXIT) · airframe 88,307 hrs · 41,022 cycles

RIGHT FWD EMERGENCY EXIT DOOR ILLUMINATED ON FINAL APPROACH. REMOVED AND REPLACED PROX SENSOR 19WV2 IAW AMM 52-71-13. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — FALSE INDICATION · airframe 88,223 hrs · 40,976 cycles

SHIP 3231 ECAM DOOR PAGE INDICATIONS-OVERWING EMERGENCY EXITS-OPEN INDIC DOOR R FWD EMER EXIT. CORRECTIVE ACTION: ADJUSTED PROXIMITY SWITCH CLEARANCE (E) PER A320 AMM 57-71-13, OPS TEST GOOD. (9086142)

Part: WARNING LIGHT — FALSE ACTIVATION (RT DOOR) · airframe 88,181 hrs · 40,951 cycles

SHIP 3231 SHORTLY AFTER TAKE OFF FROM ROC GOT DOOR R FWD EMERG EXIT ECAM MESSAGE WHICH WENT OUT AFTER 5 MINUTES. CORRECTIVE ACTION: PERFORMED INSPECTION OF R FWD EMER EXIT DOOR FROM EXTERIOR & INTERIOR NO DEFECTS NOTED. RESEATED DOOR ARM REST/EMER DOOR COVER. NO INDICATION. OPS CK NORMAL PER A320 AMM 52-20. (9086130)

Part: WARNING LIGHT — FALSE ACTIVATION (RT DOOR) · airframe 88,181 hrs · 40,951 cycles

SHIP 3231 SHORTLY AFTER TAKE OFF FROM ATL ECAM MASTER CAUTION DOOR R FWD EMERGENCY EXIT. ECAM AND QRH PROCEEDURES FOLLOWED. MADE WITH CONTACT WITH MXC VIA ATL RADIO. DECISION WASMADE TO CONTINUE. CORRECTIVE ACTION: INSPECTED DOOR FROM AND EXTERIOR, NO DEFECTS NOTED. RESEATED DOOR ARMREST/ EMERGENCY HANDLE COVER. NOW INDICATION OPS CKS NORMAL PER A320 AMM 52-20. (9086128)

Part: NONE — NONE · airframe 87,240 hrs · 40,389 cycles

SHIP 3231 BURNING SMELL AROUND IFE UNITS AT SEAT 3A AND 3B. CORRECTIVE ACTION: DEFERRED INFLIGHT ENTERTAINMENT SYSTEM PER MEL 26-36-01A. SYSTEM CURRENTLY DEACTIVATED. (8687802)

Part: NONE — NONE · airframe 87,240 hrs · 40,389 cycles

SHIP 3231 BURNING SMELL AROUND OUTLETS AT SEAT 3A AND 3B. CORRECTIVE ACTION: DEACTIVATED POWER OUTLETS PER NEF 24-58-04. CURRENTLY DEFERRED. (8687803)

Part: ACTUATOR — FAILED · airframe 87,047 hrs · 40,259 cycles

SHIP 3231 F/CTL FLAPS LOCKED WARN MESSAGE WITH EMERGENCY LANDING. CORRECTIVE ACTION: #1 FLAP ROTARY ACTUATOR BAD AND REPLACED. (2269894)

Part: NONE — NONE · airframe 86,110 hrs · 39,686 cycles

SHIP 3231 FOUND ACCESS PANEL 622WB MISSING ON RIGHT WING OUTBOARD OFF PYLON. CORRECTIVE ACTION: INSTALLED NEW PANEL. OK FOR SERVICE. (8312807)

Part: NONE — NONE · airframe 85,438 hrs · 39,285 cycles

SHIP 3231 L-2 DOOR SHOWS OPEN WHEN CLOSED. CORRECTIVE ACTION: REPLACED PROX SENSOR PER A320 IPC 52-71-04. (7377626)

Part: NONE — NONE · airframe 85,446 hrs · 39,292 cycles

SHIP 3231 L1 DOOR WOULD NOT ARM CORRECTLY. CORRECTIVE ACTION: CLEANED AND ADJUSTED DOOR PER A320 AMM 52-00. OK FOR SERVICE. (7377630)

Part: CONTROL UNIT — FAULTED (MAIN BRAKING) · airframe 85,076 hrs · 39,056 cycles

SHIP 3231 ONCE ON THE RUNWAY FOR TAKEOFF, ECAM BRAKES SYS 1 FAULT APPEARED RAN QRH 14.7 WHICH DIRECTED A BSCU RESET PER COMPUTER RESET ADDENDUM,. RESET SEEMED SUCCESSFUL HOWEVER 10-15 MINUTES LATER WHEN BACK ON THE RUNWAY FOR SECOND ATTEMPT BRAKES SYS 1 FAULT ECAM MESSAGE RETURNED. CORRECTIVE ACTION: REPLACED BSCU PER A320 AMM 32-42 ALL BITE PASSES & NO FURTHER FAULTS NOTED (7767040)

Part: PSU — NO TEST (SEAT 1 DC) · airframe 84,527 hrs · 38,720 cycles

SHIP 3231 PSU OXY PANEL FOR SEAT 1 DC NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7313326)

Part: PSU — NO TEST (SEAT 13 DEF) · airframe 84,527 hrs · 38,720 cycles

SHIP 3231 DURING TEST PSU OXY PANEL FOR SEAT 13 DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7313327)

Part: DOOR — NO TEST (SEAT 25DEF PSU) · airframe 83,707 hrs · 38,341 cycles

SHIP 3231 DURING TEST PSU O2 PANEL IN SEAT 25DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPS CK GOOD.

Part: DOOR — NO TEST (SEAT 3AB PSU) · airframe 83,707 hrs · 38,341 cycles

SHIP 3231 DURING TEST PSU 02 PANEL IN SEAT 3AB DID NOT OPEN. CORRECTIVE ACTON REPACKED MASKS. OPS CK GOOD.

Part: DOOR — NO TEST (SEAT 15ABC PSU) · airframe 83,707 hrs · 38,341 cycles

DURING TEST PSU/O2 PANEL IN SEAT 15ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.

Part: DOOR — NO TEST (SEAT 30ABC PSU) · airframe 83,707 hrs · 38,341 cycles

SHIP 3231 DURING TEST PSU O2 PANEL IN SEAT 30ABC DID NOT OPEN. CORRECTIVE ACTION REPACKED MASKS. OK FOR SERVICE.

Part: DOOR — NO TEST (SEAT 3CD PSU) · airframe 83,707 hrs · 38,341 cycles

SHIP 3231 DURING TEST PSU O2 PANEL IN SEAT 3CD DID NOT OPEN. CORRECTIVE ACTION REPACKED MASKS. OPS CK GOOD.

Part: DOOR — NO TEST (SEAT 10ABC PSU) · airframe 83,707 hrs · 38,341 cycles

DURING TEST PSU/O2 PANEL IN SEAT 10ABC DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.

Part: DOOR — NO TEST (SEAT 19DEF PSU) · airframe 83,707 hrs · 38,341 cycles

DURING TEST PSU/O2 PANEL IN SEAT 19DEF DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPERATIONS CHECK GOOD.

Part: DOOR — NO TEST (SEAT 27DEF PSU) · airframe 83,707 hrs · 38,341 cycles

SHIP 3231 DURING TEST PSU O2 PANEL IN SEAT 27DEF DID NOT OPEN. CORRECTIVE ACTION REPACKED MASKS. OPS CK GOOD.

Part: PSU — NO TEST (CABIN) · airframe 83,428 hrs · 38,207 cycles

MULTIPLE PSU'S FAIL DROP, PER WC 2527-01041-02. CORRECTIVE ACTION: RESET AND REPACKED PSU'S THAT DID NOT FALL, OPERAITONS CHECK GOOD.

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 12.500 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK . (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PR ESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV ORIGINAL AND PRO 582610-14 REV 0 TO 9 SEC

Part: PRESSURE PANEL — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON PLATE PRESSURE PANEL OPEN HOLE FR36RH Y-773, CRACK DIRECTION 12 OCLOCK LOOKING AFT. THE CRACK EXCEEDS THE AUTHORIZED REPAIR AREA AT THE PRESSURE PANEL BETWEEN FR35RH AND FR36RH. PERFORMED SECTION 1AS REPAIR AS PER ERA 582610-14AD REV. ORIGINAL AND PRI 582610-14 REV. 0 TO 9 SEC

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 9 INCH OB FROM -Y1292, CRACK DIRECTION IS 12 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV.ORIGINAL AND PRI 582610-14 REV.0 TO 9

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 3.2 INCH OB FROM +Y1292, CRACK DIRECTION ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV. ORIGINAL AND PRI 582610-14 REV. 0 TO 9

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 5.2 INCH OB FROM +Y1292, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-14AD REV. ORIGINAL AND PRI 582610-14 REV 0 TO 9 SEC

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 8.750 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK. (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PRE SSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PERFORMED SECTION 1 AS REPAIR ASPER ERA 582610-KA0 REV ORIGINAL AND PRO 582610-14 REV 0 TO 9

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 ON PRESSURE PANEL AREA AND 17.625 INCHES APPROX. INBOARD POSITION FROM Y +1292.0 ( CRACK DIRECTIONS 7 & 1 OCLOC K, 2 EA IN THE SAME HOLE) IN FWD CARGO COMPARTMENT (1 EA) (A CRACK TH AT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PERFORMED SECTION 1 AS REPAIR ASPER ERA 58610-14AD REV. ORIGINAL AND PRI 582610-14 REV.0 TO 9

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL AREA AND 15.250 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK. (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PR ESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, REPAIR PER AA 5311-01171. SB A320-53-1263. AD-2018-06-04. IN FWD CARGO COMPARTMENT (1 EA) ASSOCIATED ER/A 582610-14

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 IN OPEN FASTENER HOLE ON PRESSURE PANEL A REA AND 11.325 INCHES INBOARD FROM +Y1292, CRACK DIRECTION IS 7 OCLOCK . (A CRACK THAT EXCEEDS THE AUTHORIZED REAPIR AREA WAS FOUND AT THE PR ESSURE PLATE PANEL BETWEEN FR35LH AND FR36LH, PERFORMED SECTION 1 AS REPAIR ASPER ERA 582616-14 AD REV. ORIGINAL AND PRI 582610-14 REV O TO 9 SEC

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 5.2 INCH OB FROM -Y1292, CRACK DIRECTION IS 6 OCLOCK IN FWD CARGO COMPARTMENT (1 EA), PERFORMED SECTION 1 AS REPAIR AS PER ERA 582610-14AD REV. ORIGINAL AND PRI 58210-14 REV. 0 TO 9 SEC

Part: FRAME — CRACKED (FRM 36) · airframe 81,673 hrs · 37,272 cycles

CRACK INDICATION ON FRAME 36 PRESSURE PANEL OPEN FASTENER HOLE AT 9 INCH OB FROM +Y1292, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (2 EA), REPAIR PER ER/A 00-582610

Part: SHEAR TIE — CORRODED (FRAME 34) · corrosion level 2 · airframe 81,673 hrs · 37,272 cycles

CORROSION SHEAR TIE LOCATED FR34 AND FROM STR42L TO STR43L IN FWD CARG O COMPARTMENT, REPLACED SHEAR TIE LOCATED FR 34 AND FROM STR-42L TO STR 43L IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-42-11-801 AND DRAWING NO 53231626

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 68 TO FR 69 AND + Y1292 IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEM +Y1292 LOCATED BTW FR 68 TO FR 69 IN PASSENGER CABIN AS PER A320 SRM 51-72-11 DWG #D53472000

Part: SHEAR TIE — CORRODED (FRAME 34) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION SHEAR TIE LOCATED FR34 AND BETWEEN STR41R TO STR42R IN FWD CARGO COMPARTMENT, REPLACED SHEAR TIE LOCATED FR.34 AND BETWEEN STR.41R TO STR.42R IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-72-11 AND DWG D53231586

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 66 TO FR 67 +18 INCH +Y1292 AFT IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEAM +Y1292 LOCATED BTW FR66 TO FR67+18 INCH IN PASSENGER CABIN ASPER A320 SRM 51-72-11 DWG # D53472000

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 66 TO FR 70 AND -Y 765 A FT IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEAM -Y765 LOCATED FLOOR STRUCTURE BTW FR66 TO FR70 IN PASSENGER CABIN ASPER A320 SRM 51-72-11 AND DRAWING D53472B16

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 81,650 hrs · 37,261 cycles

CORROSION SHEAR TIE LOC. FR32 BTW STR 42 TO STR 43 L/H IN FWD, REPLACED SHEAR TIE LOC FR 32 BTW STR 42 TO STR 43 L/H FWD CARGO COMPARTMENT AS PER SRM A320 51-72-11 AND DRAWING D53231626

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 81,650 hrs · 37,261 cycles

CORROSION SHEAR TIE LOCATED FR32 AND BETWEEN STR41R TO STR42R IN FWD CARGO COMPARTMENT, REPLACED SHEAR TIE LOC FR 72 AND BTW STR 41R TO STR 42R IN FWD CARGO COMPARTMENT AS PER SRM A320 51-72-11 AND D53231626

Part: SPLICE — CORRODED (FRAMES 30-31) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION INTERNAL STRUCTURE SPLICE LOCATED BETWEEN FR30 TO FR 31 AND STR 41R IN FWD CARGO COMPARTMENT, REPLACED SPLICE LOCATED BTW FR 30 TO FR31 AND STR 41R IN FWD CARGO COMPARTMENT AS PER A320 SRM 51-72-11 AND DRAWING # D53231586

Part: INTERCOSTAL — CRACKED (FRAME 16) · airframe 81,650 hrs · 37,261 cycles

CRACK INDICATION ON FRAME 16 INTERCOSTAL AREA RH SIDE DOOR STOP FITTING 7 (LOWER AND UPPER INBOARD HOLES) ON UPPER FUSELAGE (2E/A), REPLACED INTERCOSTAL ON FRAME 16 AREA RH SIDE DOOR STOP FITTING 7 UPPER FUSELAGE AS PER A320 SRM 51-72-11 AND DRAWING #D531742-23001

Part: CYLINDER — NO TEST (PAX DOOR) · airframe 81,673 hrs · 37,272 cycles

DONT PASS TEST PASSENGER CREW DOOR 842 DAMPER CYLINDER AT AFT GALLEY AREA (1 EA), REPLACED PASSENGER CREW DOOR DAMPER CYLINDER AT AFT GALLEY AREA (1E/A) AS PER FAM A320 AMM 52-13-14-400-001-A

Part: CYLINDER — NO TEST (PAX DOOR) · airframe 81,650 hrs · 37,261 cycles

DONT PASS TEST PASSENGER CREW DOOR 841 DAMPER CYLINDER REFER TO AMDS C ARD 5210-7089-RF (RII) AT FWD GALLEY AREA (1 EA) , REPLACED DOOR DAMPER CYLINDER OF PASS/CREW DOOR 841 AS PER A320 FAM AMM 52-11-14-400-001-A AND CHECKED ADJUSTMENT OF THE PERCUSSION BELLCRANK AND THIS IS GOOD

Part: CYLINDER — NO TEST (PAX DOOR) · airframe 81,673 hrs · 37,272 cycles

DONT PASS TEST PASSENGER CREW DOOR 832 DAMPER CYLINDER REFER TO AMDS CARD 5210-7089-LA AT AFT GALLEY AREA (1 EA), REPLACED PASSENGER CREW DOOR 832 DAMPER AS PER A320 FAM AMM 52-13-14-400-001-A

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION FLOOR STRUCTURE WEB LOCATED AT FR 20 AND -Y 1732 IN PASSENGER CABIN (1 EA), REPLACED WEB LOCATED AT FR 20 AND -Y1732 IN PASSENGER CABIN (1EA ) AS PER A320 SRM 51-72-11 AND DRAWING #D53112785202

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 12 TO FR 24 AND -Y765 IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEAM AND FASTENERS LOCATED BTW FR12 TO FR24 AND -Y765 IN PASSENGER CABIN AS PER SRM A320 51-72-11 AND DRAWING D53110920 AND D53112812

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 12 TO FR 24 AND-Y 1292 IN PASSENGER CABIN (1 EA), REPLACED FLOOR STRUCTURE BEAM LOC BTW FR 12 TO FR 24 IN PASSENGER CABIN FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG D53112812

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 68 TO FR 69 AND -Y 1292 AFT IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEAM -Y1292 LOCATED BTW FR.68 TO FR.69 AFT IN PASSENGER CABIN (1E/A) AS PER A320 SRM 51-72-11 AND DWG #D53472001

Part: FRAME — CRACKED (FRM 68) · airframe 81,650 hrs · 37,261 cycles

CRACK INDICATION ON FRAME 68 ON OPEN FASTENER HOLE DOOR STOP 1, HOLE 4 AT LH SIDE. CRACK DIRECTION IS 6 OCLOCK, PERFORMED PERMANENT REPAIR LOCATED ON FR68 ON OPEN FASTENER HOLE DOOR STOP 1, HOLE 4 AT LH SIDE AT AFT GALLEY AREA, AS PER SRM A320 53-41-12-300-010

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · corrosion level 2 · airframe 81,650 hrs · 37,261 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 66 TO FR 67+18 INCH AND -Y 1292 IN PASSENGER CABIN (1 EA), REPLACED FLOOR BEAM LOCATED BTW FR.66 TO FR.67+18 INCH AND -Y1292 IN PASSENGER CABIN (1E/A) AS PER A320 SRM 51-72-11 AND DWG#53472780

Part: LIGHT — BROKEN (SEAT 21D) · airframe 80,066 hrs · 36,469 cycles

SEAT 21D EMERG PATH LIGHT BROKEN, RE-ATTACHED EMERGENCY LIGHT ASSEMBLY

Part: BATTERY — DISCHARGED (CABIN) · airframe 79,442 hrs · 36,184 cycles

(LP# 5069295) LEFT EPSU BATTERY FAULT. REMOVED AND REPLACED EPSU BATTERY IAW MM. OPERATION CHECKS OK.

Part: OIL SYSTEM — LEAKING (APU) · airframe 79,369 hrs · 36,147 cycles

(LP# 5069234) STRONG DIRTY SOCK SMELL IN FLIGHT DECK WITH PACKS RUNNING. FOUND OIL LEAKING FROM APU COMPRESSOR. APU ASSEMBLY REMOVED AND REPLACED ON LP 5069235.

Part: CLAMP — NOT REPORTED (BLEED AIR SYS) · airframe 79,335 hrs · 36,129 cycles

IFSD & ATB - RIGHT ENGINE SHUT DOWN DUE TO FIRE INDICATION. MAINTENANCE FOUND LEAK AT HP BLEED DUCT CLAMP. REPLACED SAME. PERFORMED HIGH POWER RUN. NO LEAKS NOTED. SYSTEM CHECKS NORMAL.

Part: LIGHT — DETACHED (SEAT 14D) · airframe 79,196 hrs · 36,058 cycles

(LP# 3837194) EMERGENCY TRACK FLOOR LIGHT DANGLING. LIGHT AT 14D PLACED ON MEL. 25NOV, REMOVED AND REPLACED TRACK LIGHT. OPERATIONS CHECK OKAY. MEL CLEARED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,765 hrs · 35,854 cycles

FOUND SKIN CORROSION IMMEDIATELY AFT OF VACUUM OVERBOARD VENT ON RIGHT HAND SIDE OF AIRCRAFT. REMOVED CORRODED SKIN. FABRICATED AND INSTALLED REPAIR IAW SRM 53-41-11.

Part: FRAME — DAMAGED (CARGO DOOR) · airframe 79,927 hrs · 36,403 cycles

FWD CARGO DOOR DURING SHOP VISIT INSTALLED OVERSIZED FASTENERS ON FR 26 AND FR26A AT THE FORK ENDS AND REPLACED FR25 FRAME FORK, PER ERA 571094-14AD SECTION I.

Part: SKIN — DENTED (FRAME 69) · airframe 76,952 hrs · 35,022 cycles

LOWER EXTERNAL SKIN DENTED, FRAME 69, BETWEEN STRINGERS 30L & 31L. REPAIRED IAW PRI 565255-14, REV 0-1, AND ERA 565255-14AD, REV ORIGINAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,300 hrs · 34,710 cycles

ALL 4 OVERWING EXIT DOOR EMERGENCY LIGHTS INOP BEHIND ACCESS PANELS, RELAMPED ALL 4 OVERWING EXIT DOOR HANDLE EMERGENCY LIGHTS.

Part: UNKNOWN — ODOR (CABIN) · airframe 74,943 hrs · 34,034 cycles

PAX & F/A COMPLAINED OF ODOR IN CABIN. SUBSIDED AT CRUISE FLIGHT, BUT STILL MILD PRESENCE. REPLACED RT AND LEFT PACK OZONE CONVERTER, REPLACED BOTH RECIRCULATION FILTERS, REPLACED APU.

Part: OIL SYSTEM — LEAKING (APU) · airframe 74,943 hrs · 34,034 cycles

A/C PACK SCRUBBER HAD A BAD ODOR EMITTING DURING DESCENT, CHANGED RECIRCULATION FILTERS, REPLACED NR 1 OZONE CONVERTER, HISTORY OF APU OIL CONSUMPTION, LEAK CHECKED APU & FOUND OIL LEAK AT APU OIL FILTER DELTA P SWITCH, REPLACED DPI SWITCH.

Part: LIGHT — BROKEN (ROW 11D) · airframe 74,291 hrs · 33,743 cycles

11D EMERGENCY LIGHT ASSY FOUND BROKEN, REPLACED THE EMERGENCY LIGHT .

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · airframe 73,799 hrs · 33,513 cycles

CORROSION ON FLOOR SUPPORT +Y160 FROM FRAME 68 TO FRAME 70 AT AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-70) · airframe 73,799 hrs · 33,513 cycles

CORROSION ON FLOOR SUPPORT -Y160 FROM FRAMES 68 TO 70 AT AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53474250.

Part: WEB — DENTED (FUSELAGE) · airframe 73,799 hrs · 33,513 cycles

DENT ON WEB LOCATED ON FRAME 25 INTERNAL FLOOR STRUCTURE AT LEVEL OF CENTER LINE IN FWD CARGO COMPARTMENT. REPLACED WEB LOCATED ON FRAME 26 INTERNAL FLOOR STRUCTURE AT LEVEL OF CENTER LINE FWD CARGO COMPARTMENT AS PER SRM 51-72-11 AND DRAWING D53230808.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 72,166 hrs · 32,665 cycles

LT EMERGENCY POWER SUPPLY UNIT FAULT LIGHT. R & R LT EMERGENCY POWER SUPPLY IAW AMM 33-51.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 71,612 hrs · 32,408 cycles

PAX SEAT EMERGENCY LIGHT INOP, FOUND BROKEN WIRE ON SEAT BOTTOM HARNESS. REPAIRED WIRE.

Part: FEEDER CABLE — DISCONNECTED · airframe 70,599 hrs · 31,875 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 8 ABC. CONNECTED FEEDER WIRES AT SEAT DISCONNECT. OPS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 68,079 hrs · 30,682 cycles

DURING NON ROUTINE CHECK, FOUND ROW 24ABC EMERGENCY LIGHT AISLE WIRE NEEDS RECRIMPING. MAINTENANCE REINSTALLED WIRE INTO SEAT MOUNTED LIGHT ASSEMBLY AND FUNCTIONAL CHECK WAS NORMAL.

Part: LIGHT — INOPERATIVE (SEATS 13-15ABC) · airframe 66,299 hrs · 29,798 cycles

DURING A NON ROUTINE CHECK, FOUND AISLE EMERGENCY LIGHTS AT 13 AND 15 ABC INOPERATIVE. MAINTENANCE INSTALLED LIGHT ASSEMBLY AND FUNCTIONAL CHECKED NORMAL.

Part: SLIDE — NO TEST (LT FWD) · airframe 65,779 hrs · 29,553 cycles

DURING OPS TEST OF THE EMERGENCY LIGHTS, FOUND FWD LT SLIDE LIGHT INOPERATIVE. MX REPLACED SLIDE AND FUNCTIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,779 hrs · 29,553 cycles

DURING NON-ROUTINE CHECK, FOUND EPSU FWD LT SIDE PAX CABIN INOPERATIVE. MAINTENANCE REPLACED EPSU AND FUNCTIONAL CHECKED NORMAL.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR PLATE BETWEEN FRAMES 69 AND 70 STRINGER 23R. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D53470100.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 16-20. REPLACED FLOOR SUPPORT IAW ERA 521945-14, REV ORIGINAL AND PRI 521945-14 REV O. AND SRM 51-72-11, DWG D53112819.

Part: FLOOR SUPPORT — CRACKED (FRAMES 24-35) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CRACK ON FLOOR SUPPORT Y 254 BETWEEN FRAMES 24-35. REPAIRED IAW SRM 53-00-14, PARA 4.G, FIG 207, PAG 250-254.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG NR D53472816.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472831.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 FRAMES 67+15" - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472089.

Part: PLATE — CORRODED (RT AILERON) · airframe 73,799 hrs · 33,513 cycles

CORROSION ON I/B PLATE LOCATED AT RT AILERON LOWER SURFACE L/E AREA, MEASURES L 10" , W 1" , D 0.001 APPROX. REPLACED I/B PLATE LOCATED AT RT AILERON LOWER SURFACE L/E AREA AND FASTENERS AS PER SRM 51-72-11 AND DWG D57640040.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y122 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER FLOOR SUPPORT IN AFT PAX CABIN BETWEEN FRAMES 66-68 AT STR 23R. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53480505.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER FLOOR SUPPORTLOCATED AT FRAME 20 STRINGER 23R FWD PAX CABIN. REPLACED LOWER FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112190.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE IN FWD CARGO BAY AT FRAME 31 BETWEEN STRINGERS 40-41R. REPLACED SHEAR TIE IAW SRM 51-72-11, 51-42-11 AND DWG D53231583.

Part: FITTING — CORRODED (FRAME 66) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER FITTING AT FRAME 66 STRINGER 23L. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53480505.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT IN AFT PAX CABIN BETWEEN FRAMES 66 - 68 AT S23L. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWGS D53480019 AND D53480076.

Part: FITTING — CORRODED (FRAME 68) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER FITTING AT FRAME 68 STRINGER 23L. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53480505.

Part: FITTING — CORRODED (FRAME 20) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER FITTING LOCATION IN FRAME 20 AT STRINGER 23R. REPLACED LOWER CORNER FITTING IAW SRM 51-72-11 AND DWG D53112109.

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATION BETWEEN FRAMES 16 TO 20 AT STRINGER 23R. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG NR D53112109.

Part: FITTING — CORRODED (FRAME 16) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER FITTING LOCATION IN FRAME 16 AT STR 23R. REPLACED LOWER CORNER FITTING LOCATION IN FR16 AT LEVEL OF STR 23R IAW SRM 51-72-11 AND DWG 53112109.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-70) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y512 BETWEEN FRAMES 64 AND 70. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472000.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE LOCATED FWD CARGO COMPARTMENT, AT FR31 BETWEEN S41-42R. REPLACED SHEAR TIE IAW SRM 51-72-11, 51-42-11 AND DWG D53231582.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE, LOCATED FWD CARGO BAY AT FR32 BETWEEN, S40-41R. REPLACED SHEAR TIE IAW SRM 51-72-11, 51-42-11 AND DWG D53231583.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR PLATE IN AFT PAX CABIN FLOOR STRUCTURE LOCATED BETWEEN FR69 AND FR70 AT LEVEL STR 23L, MEASURES L=1", W=0.700", D=0.003 APPROXIMATELY. REPLACED SHEAR PLATE IN AFT PAX CABIN FLOOR STRUCTURE LOCATED BETWEEN FR69 AND FR70 AT LEVEL STR 23L IAW SRM 51-72-11 AND DWG D53470100.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-67) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y318 BETWEEN FRAMES 65-67. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472305.

Part: FITTING — CORRODED (FRAMES 16-20) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING BETWEEN FRAMES 16-20 AT S23L. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112109.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 66+5-70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 64 & 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472815 AND DWG D53472831.

Part: COVER — CORRODED (FUSELAGE) · airframe 73,799 hrs · 33,513 cycles

CORROSION ON JOINT COVER LOCATED AT LEVEL -Y81 FWD PAX CABIN FLOOR STRUCTURE BTW FR 12 TO FR 16 MEASURES APPROX L:0.450" W:O.300" D:0.002". REPLACED JOINT COVER LOCATED AT LEVEL -Y81 FWD PAX CABIN FLOOR STRUCTURE BTW FR 12 TO FR 16 IAW SRM 51-72-11 AND DWG D53112620.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y81 BETWEEN FRAMES 12 TO 16. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112828.

Part: FITTING — CORRODED (FRAMES 66-68) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FRAMES 66-68 STRINGER 23L. REPLACED CENTER FITTING LOCATION IAW SRM 51-72-11 AND DWG D53480019,.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 64 TO 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472831.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 73,799 hrs · 33,513 cycles

CORROSION ON SUPPORT ANGLE LOCATED FR13 INTERNAL STRUCTURE AT LEVEL LT UPPER SIDE STRINGER. REPLACED SUPPORT ANGLE LOCATED FR13 INTERNAL STRUCTURE AT LEVEL LT UPPER SIDE STRINGER AS PER SRM 51-72-11 AND DRAWING D53110218.

Part: WEB — CORRODED (FRAMES 69-70) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN AFT PAX CABIN FLOOR STRUCTURE BETWEEN FRAMES 69 - 70 STRINGER 23R. REPLACED WEB IAW SRM 51-72-11 AND DWG D53470100.

Part: FITTING — CORRODED (FRAME 20) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER FITTING AT FRAME 20 STRINGER 23L. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53112109.

Part: FITTING — CORRODED (FRAME 16) · airframe 65,777 hrs · 29,552 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER FITTING AT FRAME 16, STRINGER 23L. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53112109.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,232 hrs · 29,292 cycles

FOUND ON SERVICE CHECK. EMERGENCY LIGHTS TEST FAILS. FAULTS "BATTERY AFT L". FOUND 13WL EPSU BATTERY BAD. REPLACED IAW AMM 33-51. OPS OK AND EMERGENCY LIGHTS TEST PASSES.

Part: LIGHT — MISSING (CABIN) · airframe 63,131 hrs · 28,246 cycles

DURING NON ROUTINE CHECK SEAT 18C ESCAPE PATH LIGHT ASSY MISSING. INSTALLED REPAIRED EMERGENCY LIGHT AT SEAT 18C AND FUNCTIONAL IS NORMAL.

Part: LIGHT — MISSING (CABIN) · airframe 62,828 hrs · 28,113 cycles

DURING NON ROUTINE CHECK, FOUND IN SEAT ESCAPE PATH LIGHTING MISSING AT SEAT 5C. MX INSTALLED A NEW IN SEAT ESCAPE PATH LIGHT AND FUNCTIONAL TEST WAS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,202 hrs · 27,311 cycles

DURING NON ROUTINE CHECK, FOUND SEVERAL EMERGENCY EXIT LAMPS INOPERATIVE. MAINTENANCE REPLACED LAMPS AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 5,743 hrs · 2,529 cycles

DURING NON ROUTINE CHECK, FOUND FLOOR EMERGENCY PATH LIGHT AT ROW 22ABC INOPERATIVE. MAINTENANCE RE-TERMINATED WIRES AND OPERATIONAL CHECK WAS NORMAL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

FRAME 1 CHORD ANGLE DAMAGED BY BIRD STRIKE. CUT OUT DAMAGED SECTION OF FRAME 1 CHORD MPN D5311085201. CUT NEW SECTION OF CHORD, FABRICATED .080" AND .100" 2024-0 REPAIR ANGLES. INSTALLED NEW CHORD SECTION AND REPAIR.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

DURING NON ROUTINE CHECK, FRAME 1 BULKHEAD WEB DAMAGED BY BIRD STRIKE TRIMMED OUT DAMAGED WEB. HFEC NO CRACKS. FABRICATED .063" WEB SECTION AND .071" 2024-T3 WEB DOUBLER. DRILLED AND INSTALLED PER ER/A 497863-14.

Part: POST — DAMAGED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

DURING NON ROUTINE CHECK, VERTICAL POST Y-675 LOWER WEB AT FRAME 1 DAMAGED DUE TO BIRD STRIKE. FABTRICATED LOWER WEB FROM 2024-0,.071" AS PER AIRBUS DWG ASNA 3042-8644. INSTALLED AS PER DWG BOD53110066. SEALED AND PAINTED.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

HORIZONTAL STIFFENER AT FRAME 1 AND VERTICAL STATION Z-1159 DAMAGED DUE TO BIRD STRIKE. REPLACED STIFFENER MPN D53113100214 PER MPR D5311310021213 AND DRAWING D53113140.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

HORIZONTAL STIFFENER AT FRAME 1 AND VERTICAL STATION Z-1329 DAMAGED DUE TO BIRD STRIKE. REPLACED STIFFENER MPN D53113100214 PER SRM 53-11-16 AND DRAWING D53113140.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

DURING NON ROUTINE CHECK, FWD FUSELAGE LWR SKIN BENT FROM Y-330 TO 22.50 INCHES RT OF CENTER AT FR 1 MARKED IN RED. TRIMMED OUT DAMAGED AREA 3" BY 12". FABRICATED AND INSTALLED.09 0" 2024-T3 DOUBLER PER SRM 53-11-11 FIG 221.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

ON DEPARTURE A/C SUSTAINED SEVERAL BIRD STRIKES IN NOSE AREA. RETURNED TO MSP. DAMAGE TO FRAME 1 BULKHEAD OUTER CHORD ANGLE. REPAIR IN PROGRESS PER ER/A 497824-14 ON N/R CARD #59(L/P 0398836).

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

ON DEPARTURE FROM MSP A/C HAD MULTIPLE BIRD STRIKES IN RADOME AREA. RESULTING IN DAMAGE TO RADOME AND FRAME 1 BULKHEAD WEB. REPAIR IN PROGRESS PER ER/A 497863-14.

Part: VERTICAL SUPPORT — CRACKED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

ON DEPARTURE FROM MSP, A/C SUSTAINED DAMAGE IN NOSE AREA BY SEVERAL BIRD STRIKES. FRAME 1 BULKHEAD VERT SUPPORT AT STA Y-675 WAS DEFORMED AND CRACKED. REPAIRS IN PROGRESS PER ER/A497784-14. N/R #44.

Part: VERTICAL SUPPORT — CRACKED (FUSELAGE) · airframe 5,161 hrs · 2,243 cycles

ON DEPARTURE FROM MSP, A/C SUSTAINED DAMAGE TO NOSE AREA FROM SEVERAL BIRD STRIKES. FRAME 1 BULKHEAD VERTICAL SUPPORT AT STA Y-330 DEFORMED AND CRACKED. REPAIR IN PROGRESS PER ER/A 497783-14. N/R #45.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 56,892 hrs · 25,319 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT ROW 16 AND 25 INOPERATIVE. REPAIRED BROKEN WIRING AND TESTS OK, REF LOG PAGE 6191017.

Part: SKIN — CRACKED (TE FLAP) · airframe 55,575 hrs · 24,777 cycles

DURING LINE CHECK FOUND CRACK IN RIGHT LEADING EDGE FLAP SKIN 57.5 INCHES OUTBOARD OF INBOARD END OF FLAP. REPAIRED PER SRM 57-52-00.

Part: TIRE — SEPARATED (NR 3 MLG) · airframe 42,525 hrs · 18,894 cycles

ON LANDING THE NR 3 MAIN TIRE RECAP SEPARATED FROM THE TIRE BODY, CAUSING ACFT DAMAGE.

Part: TIRE — SEPARATED (MLG) · airframe 55,572 hrs · 24,776 cycles

AT GATE AND SUBSEQUENCE DEPLANING, THE NR 3 BRAKE CAUGHT ON FIRE. MAINTENANCE AND FIRE DEPT EXTINGUISHED FLAMES. FOUND SECTION OF NR 3 TIRE CAP WRAPPED AROUND BRAKE CAUSING THE FIRE AND TIRE DAMAGE TO THE FLAP AND A 10X6 INCH HOLE IN T/E WING PANEL. THE NR 3 AND NR 4 WHEELS AND BRAKE ASSEMBLY WERE REPLACED. AIRCRAFT IS STILL IN THE HANGAR FOR FURTHER REPAIR.

Part: B-NUT — LOOSE (RT MLG WW) · airframe 27,346 hrs · 11,953 cycles

DURING TAKEOFF ROLL AT 60 KNOTS RECEIVED ''HYD Y RSVR LO LVL'' MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE SECURED LOOSE PARKING BRAKE PRESSURE RETURN LINE AT MANIFOLD WITH HP TRANSMITTER. LEAD CHECKED OK.

Part: PUMP — FAILED (NR 2 ENGINE)

DURING CLIMBOUT FROM LAX, RECEIVED HYD Y ENG PUMP LOW PR MESSAGE. PLACED THE NR 2 ENGINE DRIVEN YELLOW HYDRAULIC PUMP OFF AND THE YELLOW SYSTEM ELECTRIC PUMP ON PER COM PROCEDURES. LATER DURING CRUISE, RECEIVED HYD Y RSVR LOW LVL MESSAGE AND PLACED THE YELLOW SYSTEM ELECTRIC PUMP OFF PER COM PROCEDURES. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP, FILTERS AND FLUSHED SYSTEM AND OPERATIONAL CHECK OK.

Part: ANTI-ICE VALVE — MALFUNCTIONED (ENGINE)

EN ROUTE, POSSIBLE ICING CONDITIONS WERE REPORTED. THE NR 1 ENGINE ANTI-ICE VALVE WOULD NOT OPEN. FLIGHT CREW DIVERTED TO COS. MAINTENANCE REPLACED THE ANTI-ICE VALVE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING TEST OF EMERGENCY FLOOR PATH LIGHTING, FOUND LIGHTS INOPERATIVE AT SEAT ROWS 19-21 AND 25-27. MAINTENANCE REPLACED THE BATTERY PACK, OPERATIONAL CHECK OK.

Part: SILL — CORRODED (LT AFT DOOR)

DURING PERIODIC CHECK, FOUND CORROSION ON LEFT AFT DOOR SILL FRAME 2 AND 5 FORWARD OF FRAME NR 68. REPAIRED PER EA 32-150502.

Part: DRAIN — PLUGGED (AFT GALLEY)

DURING CLIMBOUT, FLIGHT ATTENDANT HEARD A LOUD NOISE IN THE AFT GALLEY AREA. NOISE STOPPED WHEN THE AFT GALLEY DRAIN WAS USED. AIRCRAFT RETURND TO LAX AND LANDED WITHOUT INCIDENT. THE AFT GALLEY DRAIN WAS BLOCKED OFF AND DEFERRED.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTED INT LOADS L, EXT LOADS FWD L, BATTERY FWD L AND UNIT FWD L. REPLACED POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK OK.

Part: STEERING UNIT — CORRODED (RT COCKPIT)

WHILE ADDING POWER FOR TAKEOFF ROLL, LOST NOSE WHEEL STEERING. TAKEOFF WAS ABORTED AT APPROXIMATELY 10 KNOTS. AFTER COMING TO A STOP, CREW RESET THE ANTI-SKID NOSE WHEEL STEERING SWITCH, CLEARED THE RUNWAY, AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE FIRST OFFICER'S STEERING CONTROL UNIT WITH NO HELP. AFTER CONFERRING WITH THE SHOP, REMOVED COVER FROM THE NEW STEERING UNIT AND FOUND CORROSION BUILD-UP INSIDE ON CONNECTOR. CLEANED CORROSION FROM THE UNIT. OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, ROWS 13, 14, 15, 19, 20, 21, 25, 26, AND 27 ESCAPE PATH LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK.

Part: ENGINES — MALFUNCTIONED (LT/RT)

DURING TAKEOFF ROLL, THE ENGINES WERE NOT ACCELERATING EVENLY. TAKEOFF WAS ABORTED AT APPROXIMATELY 10 TO 15 KNOTS. MAINTENANCE INSPECTION REVEALED NO DISCREPANCIES. ENGINES OPERATIONAL CHECK OK.

Part: COMPUTERS — MALFUNCTIONED (FLIGHT CONTROL)

AT 25,000 FEET DURING CLIMB, THE AIRCRAFT ROLLED RIGHT AND ELAC NR 1 FAULTED. RESET WAS OK, THREE MINUTES LATER THE AIRCRAFT ROLLED AGAIN WITH FAULT DISPLAY SYSTEM INDICATING ELAC NR 2 MALFUNCTION. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED BOTH SIDE STICK CONTROLLERS AND NR 1 AND NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTERS AND NR 1 AND NR 2 ELEVATOR AILERON COMPUTERS. DURING TEST FLIGHT, ALL SYSTEMS CHECKED NORMAL.