N448UA

Part: FIRE LOOP — OUT OF POSITION (ZONE 400) · airframe 81,357 hrs · 34,434 cycles

NUMBER 2 ENG FIRE WARNING APPEARED TO ROLL 100 KTS. INDICATIONS CEASED CREW DEBRIEF: AFTER FIRE WARNING INDICATION, FO PULLED THROTTLES BACK AND WARNING STOPPED. GOT AN AVERAGE OF 1 TURN ON BOTH CLAMPS FOR THE 5TH STAGE CHECK VALVE, UPPER CLAMP ON THE PRSOV AND THE UPPER CLAMP ON THE TRUMPET TUBE. ALL OTHER PNEUMATIC CLAMPS WERE TIGHT. NO OBVIOUS SIGNS OF A DUCT LEAK. LEAK CKECKED NR 2 ENGINE PNEUMATIC SYSTEM USING ACOUSTIC IMAGER KIT NO LEAK NOTED. FOUND LOOPS CONTACTING ROUTING RAIL IN SEVERAL LOCATIONS, ADJUSTED LOOPS FOR CLEARANCE, SUGGEST ENGINE RUN TO CONFIRM FAULT. RAN ENG AT OR ABOVE 1.25 EPR FOR MORE THAN 10 MIN, BLEED TEMP NORMAL AND NO FIRE WARNING.

Part: FILTER — CLOGGED (ZONE 100) · airframe 81,223 hrs · 34,362 cycles

CABIN AND FLIGHT DECKHAVE STRONG ODOR OF POSSIBLE TOXIC FUMES FOUND THAT THE SMELL WAS FROM THE APU BLEED. REPLACED BOTH RECIRCULATION FILTER CARTRIDGE REF AMM 21-21-41. RAN BOTH ENGINES FOR PACK BURN OFF AND REPLACED BOTH FILTERS AGAIN. SMELL NO LONGER PRESENT. APU BLEED SYSTEM PLACED ON MEL REF LOGPAGE 6599602

Part: UNKNOWN — ODOR (CABIN) · airframe 81,020 hrs · 34,250 cycles

FLIGHT CREW CLAIMS TO HAVE SMELLED A LIGHT ODOR IN CABIN AREA WHEN TURNING ON APU BLEED FOR AIR COND, IN COCKPIT AREA AND GALLEY AREAS FLIGHT CREW EXPOUNDED THAT ODOR WAS NOT THAT OF BURNING OR OF SMOKE, BUT A DIFFERENT KIND OF ODOR. RAN APU WITH APU BLEED OPEN AND RAN BOTH PACKS REF AMM 49-00-00-710-008-A. NO NOTICEABLE ODOR DETECTED. NO PRIOR HISTORY IN LAST 30 DAYS.

Part: NONE — NONE (NONE) · airframe 81,007 hrs · 34,241 cycles

ODD SMELL NOTICED BY MULTIPLE CREW MOSTLY IN COCKPIT, GLUEY-ISH IN NATURE UPON INSPECTION FOUND SMELL COMING FROM JET BRIDGE /PC AIR. COULD NOT FIND ANY ISSUES WITH ACFT. INSPECTED E&E BAYS, NO DEFECTS NOTED AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 79,103 hrs · 33,272 cycles

STRONG FUEL SMELL IN BACK OF PLANE DURING TAXIIN INSPECTED CABIN WITH APU RUNNING AND PACKS ON. NO FUEL SMELL NOTED. INSPECTED FUSELAGE FOR FUEL LEAKS NO EVIDENCE FOUND. FUEL SMELL MOST LIKELY CAME FROM ENGINE SHUTDOWN

Part: FUEL CAP — MISSING (WING) · airframe 77,740 hrs · 32,608 cycles

PDA 1 FUEL CAP REPORTED MISSING BY FUELER IN PHL WILL FOLLOW UP WITH PHL STATION IF LEFT BEHIND.IF FOUND WILL UPDATE LOGPAGE. FUEL CAP MISSING FUELING AND DEFUELING CAP MISSING. REQUESTING DEFERAL. APPROVED BY TOMC OK TO CONTINUE. C/W DDP DISPATCH DESK: 12 NAME: CB DATE: 12-MAY-24- OK TO DEFER FUEL CAP MISSING CAP, COUPLING R OFF 31-2825-9-0001 1994 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 1994 ON 31-2825-9-0001 1332 REPLACED MISSING REFUELING CAP PARTS USED: 1515137,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1515137 SN OFF 1994

Part: FUEL CAP — MISSING (REFUEL COUPLING) · airframe 75,602 hrs · 31,581 cycles

PDA 2 REFERENCE 5387814 FUEL CAP MISSING PDA 3 LOG CREATED IAW GMM 02-30-95 . VARGAS TOMC DOCUMENTED IAW GMM 02-30-95 FUEL CAP MISSING , VARGAS TOM. REPLACED FUEL CAP.ROTABLE PARTS CHANGE WAS INDICATED - TT # 1509941 SN OFF 2794 CAP, COUPLING R OFF 31-2825-9-0001 2794 ON 31-2825-9-0001 2993 CAP, COUPLING R OFF 31-2825-9-0001 2794 ON 0000

Part: ACTUATOR — WARNING LIGHT (ENG #2 COMPRESSO) · airframe 75,205 hrs · 31,403 cycles

ABORTED T/O AT 90 KIASFOR ENG 2 COMPRESSOR VANE ECAM. NO OTHER P ROBLEMS NOTED RAN PFR AND CFDS TEST, VERIFIED FAULT CODE PER FAULT FINDER VSV REPLACED VSV ACTUATOR ON ENGINE TWO PER AMM 75-32-41 UP TO STEP VERIFIED ENG 2 REVERSER AND COWLINGS CLOSED AND LATCHED. LOCK ACTUATOR FAIL. SEE ATTACHED PHOTO. 5D(1). NEED TO PERFOR POWER ASSURANCE TEST PER TASK RELEASE RETURNED TO FLIGHTDECK STOWAGE COMPARTMENT. 71-00-00-710-013-C. REVERSERS AND COWLINGS CLOSED. PARTS USED: 31-7532-9-0002,QTY :1 ADD EMP:187550 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1721339 SN OFF 7064 ACTUATOR, VARIA OFF 31-7532-9-0002 7064 ON 31-7532-9-0002 9722 ACCOMPLISHED HIGH POWERASSURANCE TEST, TEST 11. NO ECAM OR CFDS FAULTS NOTED. ADD EMP:U108809

Part: CROSSBEAM — UNKNOWN (FR16/FR20) · airframe 74,581 hrs · 31,117 cycles

DURING ACCOMPLISHMENT EA 5310-06784 REV A OP 003 (SB 53-1286 REV 01), HOLE DISCREPANCIES WERE NOTED ON LH/RH FR16/FR20 CROSSBEAMS. 5311-02962 PT 1 WITH NO DEVIATIONS. "PLANNING TO CONTACT ENGINEERING AFTER 69,917FC''S, REQUIREMENTS ON THE LHS FR16 + LH/RH FR16/FR20 BUT BEFORE 70,917FC''S FOR PART 2 INSPECTION CROSSBEAM HOLES PER THE LATEST REV OF EC/RA 5311-02962." ACCOMPLISHED INTERIM REPAIR INSTRUCTIONS PER VT MAE EA 320-5310-13-A3133 REV. ORIG. IAW UAL ECRA PLACED ON DIP IAW ECRA 5311-02962 PART1 PLANNING TO CONTACT TOMC-APPROVAL FROM SC1ELBYC COMMENT ENGINEERING AFTER 69,917 TOTAL FLIGHT CYCLES, BUT BEFORE 70,917 TOTAL FLIGHT CYCLES FOR PART 2 INSPECTION REQUIREMENTS ON THE LHS FR16 + LH/RH FR16/FR20 CROSSBEAM HOLES PER / THE LATEST REVISION OF EC/RA 5311-02962 QC QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: BEAM — UNKNOWN (L/R FR16/20) · airframe 74,582 hrs · 31,117 cycles

DURING ACCOMPLISHMENT EA 5310-06784 REV A OP 003 (SB 53-1286 REV 01), HOLE DISCREPANCIES WERE NOTED ON LH/RH FR16/FR20 CROSSBEAMS. 5311-02962 PT 1 WITH NO DEVIATIONS. "LHS FR16 WAS REPLACED + LH/RH FR16/FR20 CROSSBEAM REPAIR IS A PERMANENT SOLUTION WITH INSPECTION PER PART 2 OF LATEST REVISION OF EC/RA 5311-02962 ON HOLES WERE REPAIRED WHILE SUBJECTA/C WAS AT BFM. REQUIREMENTS. ACCOMPLISHINSPECTION REQUIREMENTS OR BEFORE THE AC REACHING 73,917FC''S." ACCOMPLISHED INTERIM REPAIR INSTRUCTIONS PER VT MAE EA 320-5310-13-A3133 REV. ORIG. IAW UAL ECRA APPROVED FOR DIP IAW ECRA 5311-02962 INTERIM REPAIR PER PART 1 , TOMC-APPROVAL FROM SC1ELBYC COMMENT PER PART 2 INSPECTION REQUIREMENTS TBD, PER PART 3 PART 1 REPAIR REPETATIVE INSPECTION REQUIREMENTS STATED IN PARTS, NO TERMINATIING ACTION, REQUIREMENTS PER PART 2 OF LATEST REVISION OF EC/RA 5311-02962 ON OR BEFORE THE AIRCRAFT REACHING 73,917 TOTAL FLIGHT CYCLES." QC QC REVIEWED. T/A : 73917 TAFC....HC/U389717 RECORDS UPDATE......HC

Part: CROSSBEAM — UNKNOWN (L/R FR16/20) · airframe 74,582 hrs · 31,117 cycles

DURING ACCOMPLISHMENT EA 5310-06784 REV A OP 003 (SB 53-1286 REV 01), HOLE DISCREPANCIES WERE NOTED ON LH/RH FR16/FR20 CROSSBEAMS. 5311-02962 PT 1 WITH NO DEVIATIONS. "PLANNING TO CONTACT ENGINEERING AFTER 69,917FC''S, REQUIREMENTS ON THE LHS FR16 + LH/RH FR16/FR20 BUT BEFORE 70,917FC''S FOR PART 2 INSPECTION CROSSBEAM HOLES PER THE LATEST REV OF EC/RA 5311-02962." ACCOMPLISHED INTERIM REPAIR INSTRUCTIONS PER VT MAE EA 320-5310-13-A3133 REV. ORIG. IAW UAL ECRA PLACED ON DIP IAW ECRA 5311-02962 PART1 PLANNING TO CONTACT TOMC-APPROVAL FROM SC1ELBYC COMMENT ENGINEERING AFTER 69,917 TOTAL FLIGHT CYCLES, BUT BEFORE 70,917 TOTAL FLIGHT CYCLES FOR PART 2 INSPECTION REQUIREMENTS ON THE LHS FR16 + LH/RH FR16/FR20 CROSSBEAM HOLES PER THE LATEST REVISION OF EC/RA 5311-02962 QC QC REVIEWED. T/A : PLN/ENG (>69917<70917 TAFC)......HC/U389717 RECORDS UPDATE.....HC

Part: UNKNOWN — DAMAGED (LH FRAME 35) · airframe 74,582 hrs · 31,117 cycles

DURING ACCOMPLISHMENT OF EA 5310-07772 REV. ORIG OP 001 (SB 53-1383 R00), HOLES 2 &4 ON THE LH FRAME 35 AND HOLES 1, 2 & 3 ON THE RH FRAME 35 WERE FOUND DAMAGED. DURING REPAIR EMBODIMENT, HOLES #10 ON BOTH THE LH / RH SIDE WERE FOUND TO BE OUTSIDE OF EA 5310-07772 REV. ORIG OP 004 (SB 53-1372 R01) REQUIREMENTS. PT 1 WITH NO DEVIATIONS. "PLANNING TO CONTACT ENGINEERING AFTER 13-JULY-2023, BUT STGR30 LH/RH HOLES PER THE LATEST REVISION OF EC/RA 5330-07066." BEFORE 13-AUG-2023 FOR PART 3 PERMANENT REPAIR ON THE FR35 ACCOMPLISHED INTERIM REPAIR INSTRUCTIONS PER REF /J/ VT MAE EA 320-5321-13-A3111 REV. ORIGINAL IAW UAL ECRA 5330-07066 REV A ENGINEERING AFTER 13JUL23, BUT PRIOR TO 13AUG23 FOR FINAL REQUIREMENTS ON THE FR35 STGR30 LH/RH HOLES PER THE LATEST DISPOSITION OF INTERIM REPAIR, OR, PERMANENT REPAIR INSPECTION REVISION OF ECRA 5330-07066 PART 3. ARMENTA TOMC REF INTRIM REPAIR ACCOMPLISHED ON LOG PAGE 4191692: PLANNING TO TOMC-APPROVAL FROM SC1ELBYC COMMENT CONTACT ENGINEERING AFTER 13JUL23, BUT PRIOR TO 13AUG23 FOR FINAL DISPOSITION OR INTERIM REPAIR OR PERMANENT REPAIR INSPECTION REQUIREMENTS ON THE FR35 STGR30 LH/RH HOLES PER THE LATEST REVISION OFECRA 5330-07066 PART 3. ARMENTA TOMC CORRECTION TOMC TEXT SHOULD READ: REF INTERIM REPAIR QC RECORDS UPDATE ACCOMPLISHED ON LOG PAGE 4191692: PLANNING TO CONTACT QC REVIEWED T/A: PLN/ENG >13JUL23 <13AUG23...KJB

Part: FRAME — DAMAGED (LH FR 35) · airframe 74,582 hrs · 31,117 cycles

DURING ACCOMPLISHMENT OF EA 5310-07772 REV. ORIG OP 001 (SB 53-1383 R00), HOLES 2 &4 ON THE LH FRAME 35 AND HOLES 1, 2 & 3 ON THE RH FRAME 35 WERE FOUND DAMAGED. DURING REPAIR EMBODIMENT, HOLES #10 ON BOTH THE LH / RH SIDE WERE FOUND TO BE OUTSIDE OF EA 5310-07772 REV. ORIG OP 004 (SB 53-1372 R01) REQUIREMENTS. PT 1 WITH NO DEVIATIONS. "FUSELAGE FRAME 35, STGR 30LH HOLES 2, 4 & 10 & FUSELAGE FRAME INTERIM PENDING, FINAL REPAIR EVALUATION TO BE COMPLETED ON PER PART 3 OF THE LATEST REVISION OF EC/RA 5330-07066 ON OR 35, STGR 30RH HOLES 1, 2, 3 & 10 WERE REPAIRED AT BFM. REPAIR IS OR BEFORE 13TH SEPTEMBER 2023. ACCOMPLISH A PERMANENT REPAIR BEFORE 13-SEPT-2023." ACCOMPLISHED INTERIM REPAIR INSTRUCTIONS PER REF /J/ VT MAE EA 320-5321-13-A3111 REV. ORIGINAL IAW UAL ECRA 5330-07066 REV A OKAY TO CARRY FORWARD WITH AN INTERIM REPAIR ACCOMPLISHED AT TOMC-APPROVAL FROM SC1ELBYC COMMENT FUSELAGE FRAME 35, STGR 30LH HOLES #2, #4 & #10 AND FUSELAGE FRAME 35, STGR 30RH HOLES #1, #2, #3 & #10 AS AUTHORIZED PER ECRA 5330-07066. REPAIR IS INTERIM PENDING EG EVALUATION. A PERMANENT REPAIR MUST BE APPROVED OR ACCOMPLISHED PER PART 3 OF ECRA 5330-07066 PRIOR TO 13SEPT23. ARMENTA TOMC QC'' RECORDS UPDATE QC REVIEWED T/A: 13SEP23...KJB

Part: DOOR — CORRODED (FR24 TO FR28) · airframe 74,581 hrs · 31,117 cycles

FWD CARGO DOOR CUTOUT LOWER AREA BETWEEN FR24 TO FR28 ABOVE STRI NGER 38RH SHOWS SEVERAL CORROSION AS MARKED. REMOVED CORROSION IAW SRM 51-74-00 FROM FWD CARGO DOOR CUTOUT LO STA: ST ENG BFM WER AREA BETWEEN FR24 AND FR28 L=2" W=1.1" D=0.065" FOUND TO BE OUT OF LIMIT IAW SRM 53-21-29-283-001 REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-42-11. EMP: V934143 WC: 45539

Part: UNKNOWN — CORRODED (FR24-28/STR38RH) · airframe 74,582 hrs · 31,117 cycles

FWD CARGO DOOR CUTOUT LOWER AREA BETWEEN FR24 TO FR28 ABOVE STRI NGER 38RH SHOWS SEVERAL CORROSION AS MARKED. REMOVED CORROSION IAW SRM 51-74-00 FROM FWD CARGO DOOR CUTOUT LO STA: ST ENG BFM WER AREA BETWEEN FR24 AND FR28 L=2" W=1.1" D=0.065" FOUND TO BE OUT OF LIMIT IAW SRM 53-21-29-283-001 REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-42-11. EMP: V934143 WC: 45539

Part: FLANGE — CRACKED (FR68/STR22) · airframe 74,582 hrs · 31,117 cycles

DURING HMV4 VISIT AT BFM ACCOMPL''G EA5341-01231 (B) CRACKS WERE FOUND AT FR68 LH STGR 22 WEB HORIZ FLANGE UPPER & LWR BOTTOM RADIUS. ADDITIONALLY, WHILE ACCOMPL''G EA5340-01724(C) OP2 A CRACK WAS NOTED AT FR68 LH DOOR STOP FITTING #1 WORK ACCOMPLISHED ON VTAERO N/RS 45467 & 45724 EA IS INCLUDED WITHIN THIS ECRA. ECRA REQUIRES DIP THAT STATES T ENGINEERING FOR INSPECION REQUIREMENTS PER PART 2 OF THE LASTE 800/003/2023#A FOR NECESSARY INSPECTIONS. ON OR BEFORE ACFT 4248 REACHES 45,000 TTL FC, PLANNING TO CONTAC ST REVISION OF ECRA5341-01369. ENGINEERING REFER TO RDAF 81170 ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA5341-01369 REV ''A'' AND VT MAE EA320-5341-13-A3104 FINAL WITH NO DEVIATIONS. VT MAE LOG PAGE IS FOR DIP REPORTING

Part: STOP — CRACKED (FR66 LH) · airframe 74,582 hrs · 31,117 cycles

EA 5340-01724 REV C, STEP 3.1-- FR 66 LEFTHAND AFT DOORSTOP #1 LOWER INBOARD FITTING HOLE CRACKED IN 2 PLACES "REPAIR BEFORE NE XT FLIGHT"

Part: STOP — CRACKED (LH FR68) · airframe 74,582 hrs · 31,117 cycles

DURING ROTO INSP ON LH FR68 DOOR STOP #1. CRACK INDICATION NOTED IN LWR I/B HOLE. REPAIR BEFORE NEXT FLIGHT, REPAIRED LH FR68 DOOR STOP #1 LOWER I/B HOLE PER SRM 53-41-12-30 0-011. EMP: V934143 WC: 45467 STA: ST ENG BFM

Part: SEAT TRACK — CORRODED (FRM 20) · airframe 74,582 hrs · 31,117 cycles

CABIN FED PASSENGER FR20 BETWEEN FLOOR PANEL 232DF AND 232EF THE SEAT TRACK FWD AREA HAS CORROSIOON DOT 68-39

Part: SEAT TRACK — CORRODED (FRM 20) · airframe 74,582 hrs · 31,117 cycles

CABIN FWD PASSENGER FRAME 20 BETWEEN FLOOR PANEL 232FF AND 232EF THE SEAT TRACK FWD AREA HAD CORROSION. REMOVED AND REPLACED FLOOR BEAM Y-1292 BETWEEN FR12 TO FR24 IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FRM 20) · airframe 74,582 hrs · 31,117 cycles

CABIN FWD PASSENGER FRAME 20 UNDER FLOOR PANEL 232DF THE FLOORBEAM FWD AREA HAD CORROSION.

Part: FLOORBEAM — CORRODED (FRM 20) · airframe 74,582 hrs · 31,117 cycles

CABIN FWD FLOOR STUCTURE RH FR20 THE FLOOR BEAM HAS CORROSION (0 1 EA) PLACE.

Part: STRINGER — CORRODED (FRMS 54-58 S43L) · airframe 74,582 hrs · 31,117 cycles

AFT CARGO COMPARMENT FLOOR STRUCTURE THE STRINGER 43LH HAS SEVER AL CORROSION BETWEEN FR54 TO FR58.

Part: SEAT TRACK — CORRODED (FRMS 16-20) · airframe 74,582 hrs · 31,117 cycles

FWD CABIN BETWEEN FR16 TO FR20 SEAT TRACK Y1292 HAD CORROSION (10EA) PLACES.

Part: FLOOR SUPPORT — CORRODED (FRMS 16-20) · airframe 74,582 hrs · 31,117 cycles

CABIN FWD FLOOR SUPPORT LT BETWEEN FRAMES 16 - 20 THE FLOOR SUPPORT Y254 WAS CORRODED NINE PLACES.

Part: NONE — NONE (Y HYD SYS) · airframe 73,888 hrs · 30,761 cycles

HYD Y RSVR LO LVL INFLIGHT. FLASHED SEVERAL TIMES AT CRUISE. MSG RETURNED AND INITIAL T/S FOUND HYD RES LEVEL WITHIN LIMITS, POST FLIGHT STAYED ON. REPLACED YELLOW RESERVOIR LOW LIMIT SWITCH. OPS CK NORMAL. NO LEAKS.

Part: FUEL CAP — MISSING (NA) · airframe 72,988 hrs · 30,337 cycles

PDA 1 FUEL CAP MISSING ON ARRIVAL. OPBLM CHRISTIANSEN FUEL CAP PLACED ON CDL # 8636283.

Part: NONE — NONE (#1) · airframe 72,415 hrs · 30,083 cycles

AFTER TAKEOFF POWERUP AT LESS THAN 50KTS PACK1FAULT LIGHT ECAM A NDMASTER CAUTION. RTO. CREW CONFIRMED WITH PACK #1 SWITCH OFF VLV IS CLOSED ON ECAM CREW COMPLIED WITH MEL STICKER APPLIED. REJECTED TAKEOFF BELOW 50 KTS. DEFERRED DIRECTLY BY TOMC APPLY MEL 2152Y. REF LOG PAGE 8134891 : DUE TO ABORTED TAKEOFF FOR UPPER ECAM PACK 1 OFF WITH NO ASSOCIA TED FAULT MSG''S PLEASE ACCOMPLISH TSM 73-25-00-810-817-A FAULT ISOLATION WORK WITH LP 8128736 IF NO FAULTS ARE NOTED THEN SUGGE ST REPLACING PACK 1 CONT REF AMM 21-61-34-000-001-A. REPORT FIND INGS AND ACTIONS TAKEN IN SIGN OFF. PERFORMED TSM 73-25-00. NO FAULT ON EIU. ALSO PERFORMED ZONE TEMP BITE FAULTS #2 CONTROLLER. REMOVED AND REPLACED #1,AND #2 CONTROLLER PER AMM 21-63-34.ALSO DUE TO EXTENSIVE HISTORY REM OVED AND REPLACED PACK VALVE 21-51-51. OPS AND LEAK CHKS GOOD ROTABLE PARTS CHANGE WAS INDICATED - TT # 1000883 SN OFF 1544 TT # 1008872 SN OFF 1370 TT # 1136462 SN OFF 1400 IPC REFERENCE #CONTROLLER, PAC OFF 31-2162-9-0002 1370 ON 31-2162-9-0002 1549 CONTROLLER, PAC OFF 31-2162-9-0002 1370 ON 0000 VALVE, FLOW CON OFF 31-2153-9-0001 1400 ON 31-2153-9-0001 1510 VALVE, FLOW CON OFF 31-2153-9-0001 1400 ON 0000 CONTROLLER, PAC OFF 31-2162-9-0001 1544 ON 0000 CONTROLLER, PAC OFF 31-2162-9-0001 1544 ON 31-2162-9-0001 0816.

Part: NONE — MISSING (MLG) · airframe 71,363 hrs · 29,579 cycles

PDA 3 RIGHT LANDING LIGHT BULB AND RETAINING RING MISSING AFTER LANDING AT MSY, LIGHT ASSEMBLY REPLACED REPLACED LANDING LIGHT ASSY

Part: SPOILER — INOPERATIVE (RT) · airframe 70,819 hrs · 29,331 cycles

SPOILER SURFACE 1 RIGHT INOP - F-CTL SPLR 1L/1R FAULT. 1R IS EXTENDED. 1L IS RETRACTED.VIBRATION FELT . UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. OP[S CHECK SPOILERS PER AMM 27-64-00, DEFER PER MEL 2764A IF REQUIRED DEACTIVATED SPOILER SERVOCONTRO PER AMM 27-64-00-040-001. FOUND IN THE MAINTENANCE POSITION, REJECTING FOR SIGN OFF REACTIVACTED RT SPOILER #1 REF MM 27-64-00-440-001 ACP GRD TEST CHKS OK

Part: PRESSURE PANEL — DAMAGED (FRAMES 35-36) · airframe 69,363 hrs · 28,690 cycles

EA5330-05216 REV B OP 003 RT SIDE PRESSURE PANEL BETWEEN FR 35-3 6. ACCOMPLISHED EA 5330-05216 REV B OP 003 RT SIDE PRESSURE PANEL BETWEEN FR 35-36. THIS LOG PAGE WAS CREATED TO CORRECT ERROR ON LP 5613857, LOG WAS INCORRECTLY GENERATED AGAINST AIRCRAFT 4249. CORRECT AIRCRAFT FOR EA ACCOMPLISHMENT IS 4248.

Part: PRESSURE PANEL — DAMAGED (FRAMES 35-36) · airframe 69,343 hrs · 28,690 cycles

EA 5330-05216 REV B OP 003 R/H SIDE PRESSURE PANEL BETWEEN FR 35-36. ACCOMPLISHED EA 5330-05216 REV B OP003 RT SIDE PRESSURE PANEL BETWEEN FR 35-36. ADD EMP:V894270 INSP C/W THIS ITEM WAS ENTERED IN ERROR WAS FOR A/C N4248 ADD EMP:V891438. THIS ITEM WAS CREATED IN ERROR ON 4249, CORRECT AIRCRAFT WAS 4248. NEW LOG PAGE TO RECORD DETAILS OF EA ACCOMPLISHMENT ON 4248 IS 5620309.

Part: UNKNOWN — VIBRATION (NR 1 ENGINE) · airframe 69,035 hrs · 28,545 cycles

HIGH VIBE NO 1 ENGINEHIGHEST READING 1.0CURRENTLY 0.7 AT CRUISEF L 200 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE DEBRIEF THE FLIGHT CREW FOR MORE INFORMATION. TAIL CLIMBING THROUGH FL220. IT WAS A MEDIUM FREQUENCY VIBRATION. ASKED THEM TO FILL OUT THE VIBRATION REPORTING FORM. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. DEBRIEFED THE FLIGHT CREW. THEY FELT A SUDDEN VIBRATION IN THE PERFORMED TEST NO 8 VIBRATION SURVEY REF TASK 71-00-00-700-022-B. NO DESCREPANCIES NOTED AT THIS TIME. ALL PARAMETERS WITHIN LIMITS.

Part: COWLING — PEELING (NR 1 ENGINE) · airframe 66,679 hrs · 27,493 cycles

PIECE OF ENGINE COWLING NR 1 ENGINE IS PEELED BACK INTO AIR STREAM. ON RIGHT OF PYLON ADDED PARTS NEEDED INFO TAPED SECURED PANEL STOPPED DRILL CRACK. INSPECT AFTER EACH FLIGHT FOR TAPE BEING SECURED. MUST BE REPLACED WITHIN 50 HOURS. INTERIM REPAIR ACCOMPLISHED TO ENGINE 1 INBOARD FLEX SEAL PER SRM 54-57-11-283-003. REPAIRS OR REPLACEMENT REQUIRED WITHIN 50 FLT HOURS. TAPE REQUIRES INSPECTION FOR SECURITY PRIOR TO EACH FLIGHT. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED QC REVIEWED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.

Part: SEAL — NOT REPORTED (RT WING) · airframe 66,371 hrs · 27,366 cycles

REAL BAD SHUDDER FROM ACFT AT .79IMN AND 28300FT. RETURNED TO IAH. REFERENCE LOGPAGE 9247300, RT UNDERWING PANEL BULB SEAL REPLACED. ITEM IDENTIFIED ON AIRFRAME INSPECTION REFERENCE TSM 05-50-00-810-801-A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,247 hrs · 25,952 cycles

LT AFT DOOR ENTRANCE HAS EVIDENCE OF CORROSION UNDER THE FWD GIRT BAR BLANKING PLATE. REMOVED AND REPLACED DOOR SILL BEAM AT LT AFT DOOR AS PER SRM 51-42-11 AND DRAW D53480043.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 63,070 hrs · 25,857 cycles

EMERGENCY LIGHT SYSTEM FAILED TO TEST. SHOWS EPSU UNIT FWD LT. RESET SYSTEM. THE EMERGENCY LIGHTS SYSTEM TESTED OK.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,742 hrs · 24,375 cycles

AFT CABIN EEL BATTERY PACK FAILS CAPACITY CHECK. REPLACED BATTERY PACK REF AMM 33-51-38-000-002A AND 33-51-400- 002A. OPS CHECKED OK.

Part: POWER SUPPLY — FAULTED (CABIN) · airframe 59,734 hrs · 24,371 cycles

LT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT IS FAULTING DURING EEL TEST. REPLACED EPSU REF AMM 33-51-38-000-001A AND 33-51-38-400-001A. OPS CHECKED OK.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,633 hrs · 21,788 cycles

R2 DOOR SILL CORRODED JUST AFT OF FRAME 68. R2 DOOR SILL WAS FOUND CORRODED OUT OF LIMITS BETWEEN FRAME 66 & 68 IAW SRM 53-41- 14 FIG 101. R & R R2 DOOR SILL BEAM IAW SRM 51-42-11.

Part: SKIN PANEL — CONTAMINATED (RT ELEVATOR) · airframe 53,633 hrs · 21,788 cycles

MAJOR REPAIR & SDR. RT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION 101.5 FROM INBD, 4.5 INCHES FROM TE, 3 INCHES DIAMETER. CUT OUT THE DAMAGED SKIN & CORE. REMOVED WATER APPLIED REPAIR & RESTORED FINISH IAW SRM 55-21-11 PARA 5E. REQUIRES RE-INSPECTION IAW SRI 55-21-11-2-002-00 TABLE 203.

Part: ADIRU — OUT OF ALIGNMENT · airframe 52,184 hrs · 21,230 cycles

IR 2 & 3 FAULT. REALIGNED ADIRUS RESET FMGC 1 & 2 RETURNED TO NORMAL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 51,525 hrs · 20,983 cycles

EMERGENCY LIGHT TEST FAILED ON 2 SERVICE. RE SEATED CONNECTOR ON LT EMERGENCY EXIT POWER SUPPLY, OPERATIONS CHECKED GOOD IAW 33-51-38.

Part: FLEX LINE — DAMAGED (NR 2 ENGINE) · airframe 51,011 hrs · 20,781 cycles

NR 2 ENG P5 FLEXIBLE TUBE TO EEC DAMAGED. R & R P5 FLEX LINE IAW MM.

Part: COWLING — PUNCTURED (NR 2 ENGINE) · airframe 50,863 hrs · 20,723 cycles

NR 2 ENG INLET COWL HAS A 3-16"X 1" PUNCTURE AT 10 O'CLOCK POSITION ON ACOUSTICAL LINER. ACCOMPLISHED REPAIR 2 IAW MT 71-006 ITEMS A THRU I, FINISHED REPAIR IAW MT71-006 ITEM L. REPAIR NEEDS A GRAPHITE COVER AT NEXT C CHECK IAW SRM 54-10-00 REPAIR 15.

Part: PROXIMITY SENSOR — FAULTY (LT MLG) · airframe 50,772 hrs · 20,679 cycles

NR 1 ADR & NR 3 ADR SHOW FAULTS. FAULTS RELATED NR 2 LGCIU FAILURE. REPLACED NR 2 LGCIU IAW MM32-31-71-400-001. NO MESSAGE FOR ADR'S. LGCIU SHOW SENSOR 23GA FAILURE. REPLACED NR 2 LT MLG EXT PROX SENSOR 23GA IAW AMM 32-31-73 PB401. NR 2 LGCIU BITE CHECKED OK.

Part: INTERFACE UNIT — FAULTY (NR 2) · airframe 50,772 hrs · 20,679 cycles

LGCIU NR 2 INOPERATIVE. NO FAULT CODE FROM LGCIU UNIT, WILL NOT RESPOND. FOUND NR 2 LGCIU REPLACED. ACCOMPLISHED LGCIU TEST IAW AMM TASK 32-69-00-740-001-A. TEST PASSED & NO FAULT. PERFORMED CAT III TEST & TEST PASSED.

Part: CONNECTOR — DIRTY (NLG) · airframe 50,695 hrs · 20,650 cycles

LGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. LG CLEANED CONNECTOR ON NOSE GEAR PROX SENSOR 24GA & ACCOMPLISHED LGCIU 1 TEST, ALL OKAY.

Part: OXYGEN MASK — FAULTY (COCKPIT) · airframe 50,430 hrs · 20,549 cycles

FIRST OFFICERS O2 MASK DOES NO INFLATE ON TOP LT SIDE. SWAPPED WITH 1ST OBSERVERS.

Part: NUT PLATE — DAMAGED (FAIRING) · airframe 50,010 hrs · 20,395 cycles

ONE FASTENER WILL NOT SECURE ON WING TO BODY FAIRING 191BB, FASTENER IN TOP EDGE 5TH FROM LEADING EDGE. TAPED OVER FASTENER, TO BE REPAIRED WITHIN CYCLES, PTC IS 20387. REPLACED DAMAGED NUTPLATE.

Part: ELECTRICAL SYS — FAILED (APU) · airframe 49,635 hrs · 20,255 cycles

LOST APU ELECTRICAL POWER. APU ELECTRICAL INOPERATIVE. PNEUMATICS OPERATES OK.

Part: WINDSHIELD — FAULTY (POSIT 1RH) · airframe 49,570 hrs · 20,233 cycles

MULTIPLE RESETS OF THE RT WINDSHIELD HEAT CONTROLLER DUE TO RT WINDSHIELD HEAT MESSAGE. REMOVED LOWER CENTER EXTERIOR WINDSHIELD PLATE AND WINDSHIELD WIPER. REMOVED LOWER RT WINDSHIELD BOLTS. REMOVED ALL REQUIRED COCKPIT PANELS TO REPLACE RT WINDSHIELD. ACP UP TO 4.J, REF MM-56-11-11-400-001A.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 36DEF) · airframe 49,540 hrs · 20,222 cycles

THREE OXYGEN MASKS DEPLOYED AT 36DEF. REPACKED MASKS IAW MT 350 03.

Part: CAP — DAMAGED (SEAT 20F) · airframe 49,428 hrs · 20,172 cycles

SECOND REPORT ON SEAT 20F INDICATES PHYSICAL DAMAGE TO SEAT ARM. MADE INTERIM REPAIR WITH TAPE. DAMAGED ARMCAP IS AT 20F, LT SIDE WHICH HOLDS PCU. REPLACED ARMCAP.

Part: SEAL — DAMAGED (RT WING FAIRING) · airframe 49,148 hrs · 20,062 cycles

NR 1 RT MOVABLE FAIRING - AFT INBD OF FAIRING MISSING 5" OF SEAL. REPAIRED.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,228 hrs · 17,625 cycles

FUSELAGE FRAMES 12 TO 15 BELOW STR 7R LAP, ABOVE DOOR 1 RT, 3 DENTS IN SKIN REPAIRED WITH DOUBLERS INSTALLED WITH BLIND FASTNERS. BLIND FASTENERS WERE REMOVED AND VERIFIED CRACK-FREE AND REPLACED WITH SOLID FASTENERS PER ECRA 5310-05713.

Part: WINDOW — FAULTY (COCPKIT) · airframe 48,500 hrs · 19,797 cycles

LEFT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. REMOVED CAPT WINDSHIELD BREAKERS PULLED AND COLLARED AS FOLLOWING 49VU H04, 121VU K13, 122VU W14 W13 X14 X13, 123VU AF10 AF03. REMOVED AND REPLACED L1 WINDOW PER AMM, OPS CHECK GOOD.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,058 hrs · 19,619 cycles

EMERGENCY SYSTEM TEST FAILS RIGHT EPSU MESSAGE. REPLACED BATTERY PACK.

Part: UNKNOWN — VIBRATION (AIRFRAME) · airframe 48,019 hrs · 19,602 cycles

MODERATE AIRFRAME VIBRATION FELT IN CLIMB. WORKED TSM 05-50-00-810-801 VIBRATION MATRIX. INSPECTED ELEVATOR FOR EXCESS FREE PLAY, PERFORMED ELEVATOR FREE PLAY INSPECTION, WITHIN LIMITS. NO OBVIOUS DEFECTS SEEN IAW AMM.

Part: FIRE BOTTLE — LEAKING (CABIN) · airframe 47,580 hrs · 19,420 cycles

CREW REPORT: AFT HALON FIRE EXTINGUISHER LEAKING. REMOVED HALON 1211 EXTINGUISHER FROM CABIN. REPLACED FIRE EXTINGUISHER.

Part: HANDSET — UNKNOWN (CABIN) · airframe 47,491 hrs · 19,384 cycles

CABIN HANDSET. REPLACED AFT HANDSET.

Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 36 DEF) · airframe 47,415 hrs · 19,357 cycles

36DEF OXYGEN MASKS ALL FELL DOWN. PACKED MASKS IAW AMM. ACCOMPLISHED OXYGEN MASK DROP PER MM.

Part: DRAIN LINE — BROKEN (OIL COOLER) · airframe 47,029 hrs · 19,196 cycles

NR 2 ENGINE ACOC DRAIN LINE BROKEN OFF AT DRAIN MAST. REPLACED NR 2 ENGINE DRAIN MAST ASSY.

Part: CONTROLLER — OSCILLATES (AILERON SERVO) · airframe 46,465 hrs · 18,975 cycles

ABNORMAL OSCILLATION IN AIRFRAME NOTED DURING CLIMB-OUT. FLIGHT DIVERTED. REPLACED AILERON SERVO CONTROL.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 46,099 hrs · 18,834 cycles

FLUID STREAKING ON LEFT SIDE BELLY, SOME LOOKS LIKE HYD FLUID OTHER IS BLACK COLOR. FABRICATED LINE AND REPLACED.

Part: SLEEVE — GROOVED (NLG) · airframe 45,784 hrs · 18,711 cycles

NOSE GEAR HAS EXCESS VIBRATION ABOVE 100KTS AND THROUGH RETRACTION. VIBRATION FELT THROUGH FIRST CLASS. NR 1 VIBRATION FWD NOSE WHEEL DOORS DUE TO WORN HINGE BUSHING. REMOVED BOTH L-R ROTATING ROD ASSY IAW, REF AMM. NEED TO REINSTALL NEW ASSY LEFT AND RIGHT AFT NLG DOORS HAVE PLAY AT FWD HINGES. REMOVED FWD HINGE ARMS FROM RT AFT NLG DOOR AND ACFT NOSE GEAR TORQUE LINKS HAVE PLAY AT UPPER AND LOWER ATTACH POINTS. REPLACED UPPER AND LOWER TORQUE LINKS. INSPECTED NLG AXLE SLEEVES PER TSM, FOUND BOTH LEFT & RIGHT SLEEVES ARE GROOVED. REPLACED LEFT AND RIGHT SLEEVES.

Part: SERVO CONTROL — MALFUNCTIONED · airframe 43,597 hrs · 17,791 cycles

MOD - TO HEAVY MOD VIBRATION FELT DURING CLIMB 339IAS. FL250 CLIMBING VIBRATION CAME ON ABRUPTLY AND FELT AS IF SOMETHING WAS GOING TO COME OFF. AFT FLT ATTENDANT THOUGHT IT WAS SEVERE, 100 TIMES STRONGER THAN ANYTHING SHE HAS EVER FELT. OPBLM FIELDS. SAMC TEXT: CREW UPDATE; VIBRATION STOPPED AFTER SLOWING BELOW 320KTS AND LEVELING OFF. STAYING AT FL240.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,228 hrs · 17,625 cycles

EMERGENCY EXIT PATH LIGHTS ON SEATS 7C 12C AND 35C ARE BURNED OUT. BULBS WERE REPLACED. SEAT 12C SOCKET WAS REPLACED. OP CHECKED GOOD.

Part: DOOR — FAULTY (OXYGEN MASK) · airframe 43,228 hrs · 17,625 cycles

CABIN OXYGEN MASK DOORS 2LH, 24 RT, 27 LT AND 30 LT FAILED THE RELEASE TEST. ACCOMPLISHED ON DOCK W.U. R5699N.

Part: UNKNOWN — DAMAGED · airframe 43,225 hrs · 17,624 cycles

HAIL DAMAGE, WILL CONTINUE TO MAP OUT AND EVAL DAMAGE.

Part: ACTUATOR — LEAKING (LT MLG) · airframe 43,060 hrs · 17,559 cycles

LEFT MAIN LANDING GEAR DOWNLOCK ACTUATOR LEAKING 75 DROPS PER MIN. REPLACED LT MLG STAY-LOCK ACTUATOR.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 43,027 hrs · 17,544 cycles

EMERGENCY LIGHT TEST FAILS 3 SERVICE TEST. CLEANED AND RESEATED CONNECTOR AT EPSU 13WL, PERFORMED BITE TEST PER AMM. CHECKED NORMAL.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 42,399 hrs · 17,276 cycles

CREW REPORTED A BIRD STRIKE ON TAKEOFF. 140KTS AT ROTATION JUST BELOW RADOME. ACCOMPLISHED INSP REF AMM, DAMAGE FOUND TO RADOME ONLY. REPLACED RADOME.

Part: UNKNOWN — VAPOR (CABIN) · airframe 41,828 hrs · 17,025 cycles

AVIONICS SMOKE MSG, RTFL CREW REPORT: AVIONICS SMOKE ECAM INDICATION BUT NO ACTUAL SMOKE. APPEARS TO BE FALSE INDICATION. OPENED AND INSPECTED THE AVIONICS COMPARTMENT, NO SMOKE AND NO DEFECTS NOTED. SUSPECT THE HUMIDITY CAUSED VISUAL EFFECT. RESET SDCU'S AND FWC'S. ALL CHECKS OK.

Part: GCU — FAILED (NR 1) · airframe 41,489 hrs · 16,884 cycles

ELECTRICAL ODOR IN CABIN, FLIGHT DIVERTED. INSPECTED IDG HARNESS: NO OBVIOUS FAULT. INSPECTED INSIDE OF 123VU PANEL FOR OBVIOUS FAULTS. PERFORMED IDG TEST IAW JRH, TEST OF GCU IAW AMM AND OPS TEST OF TRANSFER INHIBITION IAW AMM. REPLACED GENERATOR CONTROL UNIT IAW AMM, OPS CK NORMAL.

Part: WINDOW — LEAKING (L1) · airframe 38,828 hrs · 15,755 cycles

CAPT FWD WINDOW SQUEAL AT TOP MIDDLE THIRD OF WINDOW JUST BELOW FRAME. IAW CREW, BETWEEN 33000FT AND 35000 FT 7.9 DIFF PSI TO 8.0 DIFF PSI. NOISE HAPPENS AT LOCATION SPECIFIED. BELOW 33,000 FT 7.9 DIFF PSI OR LESS NOISE GOES AWAY. REMOVED CAPT WINDOW, INSTALLED NEW WINDOW. NEED TO INSTALL CTR RETAINER, TORQUE ALL FASTENERS, RESEAL AND INSTALL FLIGHT DECK SHROUDS. SQUEAL RETURNED. REPLACED CAPTS WINDSHIELD (2ND TIME).

Part: DAMPER — LOW (R1 DOOR) · airframe 36,013 hrs · 14,371 cycles

R1 DOOR DAMPER AND EMERGENCY, OPERATION CYLINDER PN FE240-004 PRESSURE GAUGE READING LOW. REMOVED AND REPLACED DAMPER. SERVICED DAMPER.

Part: COMPUTER — MALFUNCTIONED (E&E BAY) · airframe 35,207 hrs · 13,993 cycles

AVIONICS ECAM MESSAGE. RTFL. REPLACED AVIONIC EQUIPMENT VENTILATION COMPUTER, AVIONIC FILTER AND SMOKE DETECTOR PRECAUTIONARY, BITE TEST OK. INSPECTED E&E BAY AREA'S AND FOUND NO EVIDENCE OF ANY SMOKE.

Part: SMOKE WARNING — FALSE INDICATION (E&E BAY) · airframe 34,954 hrs · 13,870 cycles

AVIONICS SMOKE ECAM. FLIGHT DIVERTED. FLT ATTENDS REPORTED TO FLT CREW LOTS OF CONDENSATION IN THE ACFT. HOWEVER NO SMOKE WAS REPORTED. NO FAULTS REPORTED ON PREVIOUS LEGS RPT OR POST FLT REPORT. ACCOMPLISHED VISUAL INSPECTION OF E&E AND PAX CABIN WITH NO SMOKE OR DEFECTS NOTED. ACP GRD TEST OF AEVC AND GRD CHECK TESTED OK. RECYCLED FWC 1 & 2 CB'S PRECAUTIONARY AND ALL FWCS GRD CHECKED OK.

Part: BATTERY — FAULTY (CABIN) · airframe 34,745 hrs · 13,778 cycles

EPSU BATTERY EMERGENCY RIGHT FAULT DISPLAYED AFTER EMERGENCY LIGHT TEST. REPLACED BATTERY.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 34,674 hrs · 13,750 cycles

FWD LT ESPU FAILED TEST. REPLACED FWD LT EPSU. OPS CHECK NORMAL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 34,621 hrs · 13,726 cycles

TWENTY ONE (21) STRINGERS CUT FOR REMOVAL ACCESS TO REAR PRESSURE BULKHEAD LOWER FRAME 70 SECTION 5.25 INCHES AFT OF FRAME 70 BETWEEN STRINGERS 24L AND STRINGER 24R. MAJOR REPAIR ACP'D: ALL STRINGERS REINSTALLED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,621 hrs · 13,726 cycles

AFT LOWER FUSELAGE FR70 TO FR72 HAS TAIL STRIKE DAMAGE TO EXTERNAL SKIN BETWEEN STR 42R TO STR 41L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED & INSTALLED EXTERNAL DOUBLER.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 34,621 hrs · 13,726 cycles

AFT PRESSURE BULKHEAD FRAME (LWR) IS CREASED AT FR70 BETWEEN STR 42L AND STR 43R. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME.

Part: BULKHEAD — BENT (FUSELAGE) · airframe 34,621 hrs · 13,726 cycles

AFT PRESSURE BULKHEAD WEB AT FR70 IS BENT BETWEEN STRINGERS 42L TO 43R, (K8847B). MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED AFT PRESSURE BULKHEAD LOWER CENTER SECTION WEB BETWEEN STR 42L & 43R.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,621 hrs · 13,726 cycles

MAJOR REPAIR. REPLACE BELLY SKIN FR 64-70 STR 40R-31L ACCT TAIL STRIKE ON LANDING. MAJOR REPAIR ACCOMPLISHED. REMOVED AFT POTABLE WATER SERVICE PANEL. REMOVED & REPLACED DAMAGED SKIN WITH HEAT TREATED FASTENERS WHERE REQUIRED. 11/24/2008 REINSTALLED POTABLE WATER SERVICE PANEL.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 34,621 hrs · 13,726 cycles

FUSELAGE STR 43RT AT FR67 + 2 HAS EXCESSIVE MAT'L LOSS FROM GRINDING. MAJOR REPAIR. STRINGER TO BE REPLACED. REPLACE BELLY SKIN FRAME 64-70 STR 40R-31L. REMOVED DAMAGED STRINGER & REPLACED WITH NEW.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 34,621 hrs · 13,726 cycles

FUSE STR 43RT AT FR67 + 2 HAS EXCESSIVE MAT'L LOSS FROM GRINDING. MAJOR REPAIR. STRINGER TO BE REPLACED.

Part: WARNING LIGHT — ILLUMINATED · airframe 33,948 hrs · 13,394 cycles

THE "SLIDE PRESS LOW. CHECK SLIDE PRESS EMER R, EMER L" DISPLAYED ON PTP PANEL AFTER INSTALLATION OF AFT LEFT SIDE EMERGENCY OVERWING EXIT. *S/D* RESET AIRCRAFT PWR MSG DISAPPEARED. OPS TEST EMERGENCY LIGHTS NORMAL.

Part: TRANSDUCER — FAILED (NR 1 BLEED) · airframe 33,795 hrs · 13,318 cycles

NR 1 ENG BLEED AIR TRIPPED OFF AND WOULD NOT RESET. RTFL. *S/D* BMC1 FAULTED 8HA1, AIR REGULATOR TRANSDUCER. REPLACED AIR REGULATOR TRANSDUCER, 8HA1, OPS CHECKED NORMALLY.

Part: SILL — CORRODED (FUSELAGE) · airframe 33,327 hrs · 13,101 cycles

CORROSION ON R2 DOOR SILL AT FRAME 68. REPLACED SILL.

Part: SILL — CORRODED (FUSELAGE) · airframe 33,327 hrs · 13,101 cycles

CORROSION ON R2 DOOR FWD OF FRAME 66. REPLACED SILL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 33,327 hrs · 13,101 cycles

FOUND CORROSION IN FLOOR SUPPORT STRUCTURE AT FRAME 68 UNDER DOOR 2R THRESHOLD. MAJOR REPAIR ACCOMPLISHED, REPLACED FLOORBEAM -Y1292 FROM FR 64-69.

Part: SILL — CORRODED (FUSELAGE) · airframe 33,327 hrs · 13,101 cycles

L2 DOOR SILL HAS CORROSION FWD OF FR68. MAJOR REPAIR, CORROSION OUT OF LIMITS. REPAIRED PER SRM 53-41-14 NR 4.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,327 hrs · 13,101 cycles

FLOORBEAM CORROSION WHERE BEAM Y254 CROSSES FRAME 68 THIS LOCATION IS JUST AFT OF LAV WASTE TANK AND TO LEFT OF AIRCRAFT CENTERLINE ON LEFT SIDE OF FLOORBEAM. REMOVED CORROSION IAW SRM 51-74-00. REMOVED FLOORBEAM IAW SRM 51-42-11. LOCATED , DRILLED AND DEBURRED IAW SRM 51-44-11. TREATED, PRIMED & TOP COATED IAW SRM 51-21-11.

Part: SEAL — LOOSE (ELEVATOR) · airframe 33,154 hrs · 13,025 cycles

VIBRATION WITH VERTICAL BOUNCE NOTICEABLE ABOVE 320KTS. WHEN ELEVATOR LOADED UP IN DESCENT, VIBRATION STARTED AND WHEN LOADED FOR CLIMB VIBRATION STOPPED. FIRST OFFICER NOTICED RIGHT ELEVATOR INDICATION HAD SLIGHT FLUCTUATION WHEN VIBRATION PRESENT. CAUSE: LOOSE SEALS ON ELEVATOR PANELS. REPLACED SEALS WITH NEW. A/C HASN'T REPEATED SINCE.

Part: CONTROL PANEL — MISSING (EMERGENCY LIGHTS) · airframe 31,697 hrs · 12,381 cycles

DOOR 2L EMERGENCY EXIT LIGHT COVER MISSING. 10-26-07 REPLACED CABIN LIGHT CONTROL PANEL.

Part: CONNECTOR — DIRTY (EPSU) · airframe 31,568 hrs · 12,321 cycles

EPSU INT LOAD EMER L. *S/D* DIRTY CONNECTOR AT 13A POWER SUPPLY. CLEANED POWER SUPPLY CONNECTOR.

Part: FIRE WARNING — ILLUMINATED (CARGO BAY) · airframe 31,217 hrs · 12,144 cycles

LANDED UNDER AMBER ALERT DUE TO REAR CARGO COMPARTMENT FIRE INDICATION. NORMAL LANDING AND TAXIED TO GATE. REPLACED SMOKE DETECTION CONTROL UNIT.

Part: CIRCUIT BREAKER — FAULTY (EMERGENCY LIGHTS) · airframe 30,621 hrs · 11,893 cycles

DURING 3 SERVICE CHECK, EMERGENCY LIGHT CHECK HAD EPSU BATT EMER R FAULT. RESET EMERGENCY LIGHT C/B`S, PERFORMED OPS CHECK REF AMM 33-51-38, CHECKS NORMAL.

Part: ENGINE — OVERSPEED (NR 2) · airframe 30,508 hrs · 11,839 cycles

RTFL DUE TO NR 2 ENGINE N2 OVERSPEED.

Part: BLEED VALVE — DIRTY (NR 2 ENGINE) · airframe 29,862 hrs · 11,550 cycles

ENG 2 COMPRESSOR VANE IMPENDING ENG STALL. WARNING CAME ON-OFF 3 TIMES DURING DESCENT. *S/D* REPLACED LPC BLEED MASTER ACTUATOR. FOUND HEAVY FUEL LACQUERING ON PRESSURE DROP REGULATOR DURING OVERHAUL.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 28,847 hrs · 11,058 cycles

NR 1 ENGINE FAILED STARTER, RAMP REPORTED SPARKS COMING OUT OF ENGINE DURING ENGINE START. REPLACED STARTER AND ACCOMPLISHED DRY MOTOR OPS CHECK.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 27,956 hrs · 10,634 cycles

LOST CABIN PRESSURE. DESCENDED TO FL120 AND STABILIZED. SAMC BELIEVES CARGO DOOR SEAL WAS BLOWN. FLT DIVERTED. SUPPLEMENTAL DATA UPDATE REPLACED CPC NR 1 PRECAUTIONARY ON ACCOUNT OF PREVIOUS LEG PRESSURIZATION PROBLEM. SYSTEM 1 FAULT DISPLAYED ON UPPER ECAM. SWAPPED CONTOLLERS BETWEEN NR 1 AND 2. FAULT SWAPPED WITH SYSTEM 2. REPLACED CPC NR 2. ACCOMPLISHED PRESS CHECK OF AIRCRAFT. PRESSURIZATION CK FAILS. INSPECTED CPC 1 & 2 FOR PROPER INSTALLATION. NO DISCREPANCIES NOTED. DUE TO PRESSURIZATION LOSS FWD CARGO DOOR SEAL REPLACED. ACCOMPLISHED LEAK CHECK OF DOOR SEAL. NO LEAKS NOTED. DURING PRESSURIZATION CHECK. AIRCRAFT WAS NOT ABLE TO ACHIEVE MORE THAN 4.4-PSI DIFFERENTIAL PRESS. REPLACED OUTFLOW VA

Part: RADOME — BIRD STRIKE (FUSELAGE) · airframe 26,806 hrs · 10,100 cycles

BIRD STRIKE AFTER TAKEOFF. IMPACT BELOW NOSE. RADAR ANTENNA MAKES GRINDING NOISE DURING SWEEP. RADOME DAMAGED.

Part: LIGHT — MISSING (SEAT 10C) · airframe 26,278 hrs · 9,857 cycles

SEAT 10C HAS THE EMERGENCY PATHWAY LIGHT MISSING.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,946 hrs · 9,268 cycles

LEFT AFT MED EMERGENCY LIGHT SWITCH IS INOPERATIVE. REPLACED CIDS AFT PANEL.

Part: WIRE HARNESS — FAILED (LT WING TANK) · airframe 20,828 hrs · 7,324 cycles

FLIGHT DIVERTED DUE TO A POSSIBLE FUEL LEAK. UNWANTED FUEL TRANSFER AND DEGRADED FUEL INDICATIONS CAUSED BY LEFT HAND WING INNER FUEL QUANTITY HARNESSES FAILURE. REPLACED LEFT HAND WING INNER FUEL QUANTITY HARNESSES. OPERATIONS CHECK NORMAL.

Part: CHECK VALVE — OVERHEATED (HYD SYSTEM) · airframe 20,029 hrs · 7,019 cycles

RETURN TO FIELD DUE TO YELLOW HYDRAULIC SYSTEM OVERHEAT. REPLACED THE YELLOW ELECTRIC PUMP CHECK VALVE 3083GM. CHECK VALVE WAS BROKEN INTERNALLY.

Part: DAMPER — LEAKING (AUTOPILOT SYS) · airframe 15,643 hrs · 5,309 cycles

LANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. NR 1 YAW DAMPER WAS FOUND LEAKING HYDRAULIC FLUID. NEW YAW DAMPER ACTUATOR WAS INSTALLED AND OPERATIONAL CHECK WAS GOOD.

Part: SMOKE — DETECTED (LAVATORY) · airframe 14,989 hrs · 5,043 cycles

ON DESCENT, FLIGHT ATTENDANT RELEASED HALON EXTINGUISHER IN AFT LAV DUE TO LIGHT HAZE/SMOKE AND HEAT. EMERGENCY PROCEDURES WERE PUT INTO EFFECT. SMOKE/HEAT HAD DISSIPATED ON LANDING. RAN ENGINES AND APU. CHECKED AFT FWD LAV FOR SIGNS OF SMOKE, ELECTRICAL SMELL NONE NOTED. CHECKED LAV WATER HEATER, OPEN UP PANEL IN AFT PIT AND CHECK APU DUCTING FOR POSSIBLE LEAK, NONE NOTED. REPLACED BOTH THE LEFT AND RIGHT PACK OZONE FILTERS. RAN PACKS FOR FIVE HOURS. ALSO RAN GALLEY CHILLERS, OVENS, COFFEEPOT, HEATERS AND COFFEEMAKERS. CHECKED THE HOT WATER HEATERS UNDER SINK CHECKED GOOD. UNABLE TO POSITIVELY IDENTIFY HAZE/SMOKE/HEAT SOURCE.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 6,929 hrs · 2,181 cycles

F/A REPORTS ACRID SMOKE SMELL IN AFT GALLEY. STRONGEST AROUND EYEBALL VENT. *S/D* FOUND ELECTRICAL SMELL COMING FROM RIGHT AFT COFFEEMAKER. REPLACED COFFEEMAKER (P/N:3510 0032 01U2). OPERATIONAL CHECK NORMAL.

Part: LGCIU — MALFUNCTIONED (NLG DOOR)

CREW REPORTS LANDING GEAR DID NOT COMPLETELY EXTEND ON FIRST ATTEMPT. CYCLED GEAR, OPS NORMAL. *S/D* LGCIU REPORTED NLG R DOOR PROX SENSOR 38GA TARGET POSITION. CHECKED GAPS AND FOUND WITHIN TOLERANCE PER AMM 32-31-73. BITE TEST OK. NO FURTHER PROBLEMS.