N621JB

Part: HINGE ARM — CORRODED (ZONE 300) · airframe 75,160 hrs · 27,064 cycles

DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ5 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00040) REMOVED AND REPLACED HINGE FITTING #5 LOC. VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008 ALL WORK ACCOMPLISHED ON AEROMAN WO 2025195/1 NR542203."

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 75,160 hrs · 27,064 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING Ñ1. CRACK DIRECTION 5 OCLOCK. CRACK D= 0.160 INCH; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00037) PERFORMED PERMANENT REPAIR ON LOC. ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING #1 IAW SRM 53-41-12-300-008 FIGURE 003 SHEET 1 & SRM 53-41-12-300-010. THIS REPAIR IS CATEGORY B. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC SUBSEQUENT INSPECTION AT INTERVALS 10700 FC (FH NOT RELEVANT) INSPECTION METHOD HFEC (REFER TO NTM CHAPTER 51-10-08) AND ROTOTEST (REFER TO NTM 51-10-01) IAW A320 SRM 53-41-12-205-009 TABLE 2. FUR-A320-53-02620ALL WORK ACCOMPLISHED ON AEROMAN WO 2025195/1 NR542181.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 75,160 hrs · 27,064 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING Ñ1. CRACK DIRECTION 5 OCLOCK. CRACK D= 0.160 INCH; PERFORMED PERMANENT REPAIR ON LOC. ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING #1 IAW A320 SRM 53-41-12-300-008 FIGURE 003 SHEET 1 AND A320 SRM 53-41-12-300-010. THIS REPAIR IS CATEGORY B. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC. SUBSEQUENT INSPECTION AT INTERVALS 10700 FC (FH NOT RELEVANT) INSPECTION METHOD HFEC (REFER TO NTM CHAPTER 51-10-08) AND ROTOTEST (REFER TO NTM CHAPTER 51-10-01) IAW SRM 53-41-12-205-009 TABLE 2. FUR-A320-53-02620ALL WORK ACCOMPLISHED ON AEROMAN WO 2025195/1 NR542181.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 75,160 hrs · 27,064 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB HOLE OF FR 68 LH DOOR STOP FITTING Ñ1. CRACK DIRECTION 5 AND 11 OCLOCK. CRACK D= 0.160 INCH; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00036) PERFORMED PERMANENT REPAIR ON FR68 LH AT LOWER INBOARD HOLE OF DOOR STOP FITTING #1 IAW SRM 53-41-12-300-008 FIG 002 (SHEET 1/2) FIGURE 003 (SHEET 1) AND IAW SRM 53-41-12-300-010 STEP 2.A. REPAIR IS CATEGORY B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC, SUBSEQUENT INSPECTION AT INTERVALS 10700 FC (FH NOT RELEVANT) INSPECTION METHOD HFEC (REFER TO NTM 51-10-08) AND ROTOTEST (REFER TO NTM 51-10-01) IAW SRM 53-41-12-205-009 TABLE ALL WORK ACCOMPLISHED ON WO 2025195/1 NR542180 FUR-A320-53-02619.

Part: BEARING — CORRODED (ZONE 300) · airframe 75,160 hrs · 27,064 cycles

DURING HEAVY MAINTENANCE: AFTER REMOVE BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ4 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00041) REMOVED AND REPLACED HINGE FITTING #4 LOC. VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008. ALL WORK ACCOMPLISHED ON AEROMAN WO 2025195/1 NR542202."

Part: BEAM — CORRODED (ZONE 200) · airframe 75,160 hrs · 27,064 cycles

DURING HEAVY MAINTENANCE: CORROSION ON LONGITUDINAL BEAM LOCATED BTW FR. 40 TO FR.41 AND AT LEVEL STR 20A . R/H SIDE EMERGENCY EXIT DOOR AREA IN PASSENGER CABIN; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00038) REMOVED AND REPLACED LONGITUDINAL BEAM LOC. BTW FR40 TO FR41 AND AT LEVEL STR 20A RH SIDE EMERGENCY EXIT DOOR AREA PASSENGER CABIN I.A.W A320 SRM 51-42-11 AND DRAWING# D53370200. ALL WORK ACCOMPLISHED ON AEROMAN WO 2025195/1 NR522462.

Part: COMPUTER — FAILED (NR 1 ELAC) · airframe 75,118 hrs · 27,051 cycles

FLT # 2427 FLL-MBJ, AIR RETURN BACK INTO FLL. DUAL INPUT CALL AT ABOUT 2500FT, WHEN THERE WAS NO DUAL INPUT ECAM FOR ELAC 2 PERFORMED THE RESET PROCEDURE BUT THE ECAM CAME BACK THE AIRCRAFT DID TWO SHARP JERKS AFTER TAKEOFF TO THE RIGHT;TWO AIRCRAFT MOVEMENTS ARE DUE TO ENGAGEMENT + DISENGAGEMENT OF ELAC #2 SE ITEM 4318548-1 FOR REFERNCE BOTH ELAC1& 2 REPLACEMENT DUE TO SHIPSET TO UPGRADE SOFTWARE TO L104 ELAC #2 REMOVEED AND REPLACE REF 2793-34-400-001-A OPS CHK GOOD SEE ITEM 4318549-2 FOR CATIII

Part: COMPUTER — FAILED (NR 2 ELAC) · airframe 75,118 hrs · 27,051 cycles

FLT # 2427 FLL-MBJ, AIR RETURN BACK INTO FLL. DUAL INPUT CALL AT ABOUT 2500FT, WHEN THERE WAS NO DUAL INPUT ECAM FOR ELAC 2 PERFORMED THE RESET PROCEDURE BUT THE ECAM CAME BACK THE AIRCRAFT DID TWO SHARP JERKS AFTER TAKEOFF TO THE RIGHT;TWO AIRCRAFT MOVEMENTS ARE DUE TO ENGAGEMENT + DISENGAGEMENT OF ELAC #2 SE ITEM 4318548-1 FOR REFERNCE BOTH ELAC1& 2 REPLACEMENT DUE TO SHIPSET TO UPGRADE SOFTWARE TO L104 ELAC #2 REMOVED AND REPLACE REF 2793-34-400-001-A OPS CHK GOOD SEE ITEM 4318549-2 FOR CATIII.

Part: BATTERY — NO TEST (ZONE 200) · airframe 74,193 hrs · 26,662 cycles

FLT#591, BOS-TPA. 'EPSU 10WL BATTERY FAILS OPERATIONAL TEST; REMOVED AND REPLACED EPSU 10WL BATTERY IAW AMM 33-51-38 OPS CHECKS GOOD.'

Part: UNKNOWN — ODOR (CABIN) · airframe 70,338 hrs · 25,070 cycles

FLT#613, HPN-FLL. 'AFT FLIGHT ATT SAID HE SMELLED SMOKE OR BURNING WHEN WE LOWERED THE GEAR; PERFORMED INSPECT FOR SMOKE OR BURN SMELL PER TSM 05-50-00-810-8310A. NO HISTORY OR SIGNS OF ODOR . CLASSIFIED AS A TYPE 10 . A/C OK FOR SERVICE.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,466 hrs · 24,732 cycles

FLT#36, PHX-JFK. '#1 FA REPORTS CHEMICAL ODOR IN FWD CABIN ONLY ON FINAL APPROACH LASTED 1 MIN; COMPLIED WITH INFO NOTICE 2017-T015 SECTION B2 DECONTAMINATION LEVEL A WAS ACCOMPLISHED PER TSM 05-50-00-810-085 AC OK FOR SVC.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,319 hrs · 24,668 cycles

FLT#261, BOS-SJU. (AIRCRAFT DECLARED AN EMERGENCY INTO SJU) 'HYD G RSVR LO LVL HYD G RSVR LO PR.' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,628 hrs · 23,988 cycles

FLT#2613, ATL-LGA. 'DIRTY SOCK SMELL THROUGHOUT THE AIRCRAFT; COMPLIED WIITH INFO NOTICE 2017-T015J SECTION B2 DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER AMM 25-00-00-615-803A VERIFIED SOURCE OF ODOR TO BE APU. FOUND OIL TRACES IN APU COMPARTMENT APU PLACED ON MEL 49-10-01A C/W MX PROCEDURE. MX-4 UPDATED. PLACARD INSTALLED OK FOR MX MDDR 19760.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,440 hrs · 23,910 cycles

FLT#1799, LGA-MCO. 'DIRTY SOCK ODOR FROM COCKPIT TO AFT AIRCRAFT ON DESCENT THROUGH 8000; COMPLIED WITH INFORMATIONAL NOTICE 2017-T015, SECTION B2 DECONTAMINATION LEVEL A WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. A/C IS OK FOR CONTINUED SERVICE. ODOR COMING FROM APU COMP APU PLACED ON MEL.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,444 hrs · 23,912 cycles

FLT#2433, DCA-PBI. 'FLIGHT ATTENDANTS (ALL) GOT THE DIRTY SOCK (OLD DEICING FLUID) SMELL IN THE CABIN ON DESCENT (APU DEFERRED); COMPLIED W/ INFO NOTICE 2017-T015, SECTION B2, DECONTAMINATION LEVEL 1 WAS ACCOMPLISHED PER TSM 05-50-00-810-085-B. A/C IS OK FOR SERVICE.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,192 hrs · 23,823 cycles

FLT#1529, JFK-RSW. 'UPON ARRIVAL AT GATE INFLIGHT NOTIFIED ME OF A 'FUME EVENT ' ON DESCENT PASSING THRU 10,000 AND LASTING 5-7 MINUTES. NO ODOR WAS DETECTED IN THE FLIGHT DECK ( APU SYSTEM ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 67,074 hrs · 23,767 cycles

FLT#1971, LGA-FLL. 'VERY STRONG ODOR/FUME ON DESCENT AND FINAL. SMELLED ACRID OIL COMING OUT OF BLEEED SYS WITH AND WITHOUT APU; ACCOMPLISHED TSM 05-50-00-810-831-A, FOUND TO BE THE APU. PERFORMED SUBTASK 05-50-00-810-085B. COMPLIED WITH INFO NOTICE 2017-T015, SECTION 'A", ISOLATED TO APU, APU TO BE PLACED ON MEL. AIRCRAFT OK FOR SERVICE. PERFORMED ECS DECON 9 WITH ENGINES), NO ODOR WAS DETECTED.

Part: NONE — NONE · airframe 65,649 hrs · 23,238 cycles

DURING HEAVY MAINTENANCE: REF AEROMAN W/O 2022-283/1 NR 2022-557900. CRACK INDICATION ON FRAME 16 LH SIDE OPEN FASTENER HOLE H3 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 2 AND 3 O'CLOCK ON INTERCOSTAL FITTING LAYER AT FWD GALLEY; REF AEROMAN W/O 2022-283/1 NR 2022-557900. REMOVED AND REPLACED INTERCOSTAL FITTING LOC. FR16 LH SIDE DOOR STOP FITTING #7 I.A.W A320 SRM 51-42-11 AND DWG D53112300 AND TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC600D, S/N: 210138103, DUE DATE: APR-11-2023, TOOL USED: TORQUE P/N: QD2R200 S/N: 0219122547 DUE DATE: MAY-20-2023 AND TOOL USED: CALIPER P/N: 500-196-30 S/N: B22072476 DUE DATE: JUN-26-2023.

Part: NONE — NONE · airframe 65,649 hrs · 23,238 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 INSIDE INNER FRAME SEGMENT FORWARD POSITIONS. THE LONGEST CRACK IS 2.23 INCHES APPROX. PASSENGER CABIN; REF AEROMAN W/O 2022-283/1 NR 2022-557954. PERFORMED PERMANENT REPAIR ON EMERGENCY EXIT DOOR 844 INSIDE INNER FRAME SEGMENT FORWARD POSITIONS ON PASSENGER CABIN I.A.W EC NO.A320-52-1144. COMPLETED BY: M. CARRILLO 8673420 CHECKED BY: L. OSTORGA 8619517.'

Part: NONE — NONE · airframe 65,649 hrs · 23,238 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT(1EA); REF AEROMAN W/O 2022-283/1 NR 2022-557868. REMOVED AND REPLACED CONTINUITY FITTING RH SIDE (1 EA) ON FRAME 2 WINDSHIELD CENTER POST LOWER AREA IAW A320 SRM 51-42-11 AND REPAIR INSTRUCTION R53112919 AND R53113426. TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D, S/N: 210138103, DUE DATE: APR-11-2023. TORQUE P/N: QD1R200A S/N: 0821901575, DUE DATE: SEP-01-2023. COMPLETED BY: E. RODRIGUEZ 8633115 CHECKED BY: E. ARGUETA 8619800.'

Part: NONE — NONE · airframe 65,649 hrs · 23,238 cycles

DURING HEAVY MAINTENANCE: DONT PASS TEST EMERGENCY LIGHT TEST THROUGH PTP AT THE FWD GALLEY AREA; REF AEROMAN WO 2022-283/1 NR 2022-558319 REMOVED AND REPLACED EMERGENCY EVACUATION DOOR SLIDE RAFT 831 IAW AMM 25-62-44-000-012-A. AND AMM 25-62-44-400-007-A. AND PERFORMED OPERATIONAL TEST OF THE SCAPE-FACILITIES IS OK. TOOL USED: TORQUE: PN: QD1R200. SN:1017900546. DUE DATE: MAY/28/2023. TORQUE APPLIED:57LBS.IN. DONE BY R. ALEGRIA 8629512 CHECKED BY J. NOLASCO 8602011.

Part: NONE — NONE · airframe 65,649 hrs · 23,238 cycles

DURING HEAVY MAINTENANCE: REF AEROMAN W/O 2022-283/1 NR 2022-557867. CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX. IN COCKPIT (1EA); REF AEREOMAN W/0 2022-283/1 NR 2022-557867. REMOVED AND REPLACED CONTINUITY FITTING LH SIDE (1 EA) ON FRAME 2 WINDSHIELD CENTER POST LOWER AREA IAW A320 SRM 51-42-11 AND REPAIR INSTRUCTION R53112919 AND R53113426. TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D, S/N: 210138103, DUE DATE: APR-11-2023. TORQUE P/N: QD1R200A S/N: 0821901575, DUE DATE: SEP-01-2023 COMPLETED BY: E. RODRIGUEZ 8633115 CHECKED BY: E. ARGUETA 8619800.

Part: NONE — NONE · airframe 65,649 hrs · 23,238 cycles

DURING HEAVY MAINTENANCE: DON'T PAST TEST EMERGENCY LIGHT PTP SHOWS EPSU EXT LOAD AFT L BATTERY; REF AEROMAN WO 2022-283/1 NR2022-558321. REMOVED AND REPLACED THE BATTERY OF THE EMERGENCY POWER SUPPLY UNIT FIN 13WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A DONE BY C. GOMEZ 8616907 CHECKED BY M. CALDERON 8612315.'

Part: APU — COKED · airframe 62,998 hrs · 22,326 cycles

FLT # 1557, FLL-BOG. STRONG ODOR DIRTY SOCK SMELL PASSING 17,000 INTO BOGOTA. FOLLOWED ISOLATION PROCEDURE. SUSPECT PACK #1 SMELL DISSIPATED. SMELT BY BOTH FLIGHT CREW AND #1 F/A SMELT LEVEL 2 ( PACKS ) ; REF L/P 3253928 FOR CORRECTIVE ACTION. MX-4 UPDATED, PLACARD REMOVED, MEL CLEARED. MCC NOTIFIED.ACCOMPLISHED WO# 1158120. COMPLIED W/ TSI. TRACED OIL CONTAMINATION TO APU, NO ACTIVE LEAKS. RESIDUAL COKED UP OIL WAS CLEANED. ACCOMPLISHED ECS DECONTAMINATION PER AMM: 21-00-00-615-804. R/R RECIRC FILTER'S PER SAME AMM. C/W INFO NOTICE 2017-T015I. AIR QUALITY GOOD ON BOTH PACKS. A/C OK TO CONT.

Part: UNKNOWN — ODOR (CABIN) · airframe 62,679 hrs · 22,217 cycles

FLT 2295, EWR-MIA. BURNING OL SMELL IN AFT PORTION OF AIRCRAFT REPORTED BY ACFT F/A'S DURING CLIMB OUT SMELL WAS REPORTED AROUND 12,000FT SMELL DISAPPEARED SEVERAL MINUTES LATER DURING ARRIVAL SMELL REPORTED AROUND 11,000FT AND DISSIPATED PRIOR TO LANDING FLIGHT CREW SMELLED NOTHING ; COMPLIED WITH INFORMATION NOTICE 2017-T015F SECTION A ISOLATED FAULT TO TYPE 10 A,1,C PER TSM 05-50-00-810-085B ACFT IS OK FOR SERVICE

Part: UNKNOWN — ODOR (CABIN) · airframe 62,217 hrs · 22,043 cycles

FLT 939, JFK-SJD. ON FINAL DES ENTIRE CABIN CREW REPORTED DIRTY SOCK ODOR IN CABIN ; COMPLIED WITH INFORMATION NOTICE ON SB. 2017-T015 SECTION B 1 OK A/C OK FOR SERVICE MCC MARIO NOTIFIED

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 59,814 hrs · 21,209 cycles

FLT 1391, BOS-TPA. EMERGENCY LIGHT BATTERY 10 WL FAILED BATTERY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY, IAW AMM 33-51-38.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 59,814 hrs · 21,209 cycles

FLT 1391, BOS-TPA. EMERGENCY LIGHT BATTERY 10WL FAILED BATTERY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 10WL, IAW AMM 33-51-38.

Part: BATTERY — FAILED (CABIN) · airframe 54,641 hrs · 19,373 cycles

FLT 391, BOS-TPA. EPSU BATTERY 11WL FAILS EMERG LIGHT SYSTEM TEST; R & R BATTERY AT EPSU 11WL IAW AMM 33-51-38, SYSTEM OPS CHECKS GOOD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 53,380 hrs · 18,902 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR STRUCTURE, SEAT TRACK Y765, FR 62 +8.00", STR 23L. CORROSION MEAS. 3.90"L X .772"W X .063" D. MATERIAL LOSS = 29%; CORROSION THAT IS BEYOND ALLOWABLE LIMITS, PER SRM 53-41-15-283-001 ON SEAT TRACK Y765, FR 62, STGR23L. REMOVED AND REPLACED NOTED FLOOR TRACK PER SRM 51-72-11, SRM 51-42-11 AND DWG D53472770.

Part: FLAP — LOCKED (WING) · airframe 49,158 hrs · 17,227 cycles

FT 1522, LGB-PDX. F/CTL FLAPS LOCKED ALIGNMENT FAULT" ECAM DURING APPROACH. FLAPS LOCKED BETWEEN 0 AND 1; RESET FLAP C/B OPS CHECK GOOD PER AMM 27-51-00. A/C OK FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 48,670 hrs · 17,038 cycles

EMERGENCY DECLARED. F/CTL FLAP LOCKED. ALIGNMENT FAULT ECAM ON APPROACH; PERFORMED TSM 27-51-00-810-849-A. RESET FAULT, NO FAULT NOTED. ACC BITE TEST OF SFCC-1 AND SFCC-2 IAW AMM 27-51-00-740-002, NO FAULT NOTED. PERFORMED FLAPS OPERATIONAL TEST IAW AMM 27-50-00, CHECKED OK AND RESET WING TIP BRAKE IAW AMM 27-50-869-006-A. NO FAULT NOTED. CONCURRED WITH MX, ACFT OK FOR SERVICE.

Part: PROXIMITY SENSOR — FAULTED (TE FLAP SYS) · airframe 48,435 hrs · 16,949 cycles

DURING FINAL APPROACH, FLAPS LOCKED, ALIGNMENT FAULT SLATS 2 FLAPS <1. R & R 37CV PROXIMITY SENSOR IAW AMM 27-51-44-000-002A, OPS CHECKED NORMAL.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 48,198 hrs · 16,876 cycles

AFT LEFT EPSU BATTERY FAULTED. R & R THE BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,052 hrs · 16,826 cycles

EMERGENCY LIGHTS AT ROWS 15, 19, 23 INOPERATIVE. R & R 11WL EPSU IAW AMM 33-51-38-000-002. OPS CHECKED GOOD IAW AMM 33-51-00-710-007.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 47,695 hrs · 16,695 cycles

FOUND NO COMM BETWEEN CID'S & EPSU. R & R THE EPSU (10WL) IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAME 65) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y1732 FR 65+10. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: DOOR SILL — CORRODED (FRAME 67) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FRAME 67 + 19 R2 DOOR SILL. R & R DOOR SILL IAW SRM 53-41-14-300-001.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED FLOOR SUPPORT AT FRAME 68, -Y1292. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON TWO SCREW HOLES ON FLOOR SUPPORT AT -Y1292, FRAME 66. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AROUND SCREW HOLE ON THE FLOOR SUPPORT AT Y1292 FROM FRAME 64 TO 66. R & R FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON AT BARREL NUT HOLES ON FR 66 FLOOR SUPPORT Y464. R & R FLOOR BEAM Y464 IAW A302 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AT SCREW HOLES FR 68+11ON FLOOR SUPPORT AT Y1292. R & R FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-68) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVEREDS ON FLOOR SUPPORT AT Y1292 FRAMES 67 - 68. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT -Y1292 +8 INCHES FROM FR 16. R & R FLOOR SUPPORT IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 66) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AT L2 DOOR FWD LOWER CORNER, SMALL AFT PIECE OF INBD SEAT TRACK Y1732, FRAME 66. R & R THE SEAT TRACK IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 46,215 hrs · 16,094 cycles

DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AROUND SCREW HOLE ON THE FLOOR SUPPORT AT -Y1292, FR 66+8. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 44,836 hrs · 15,644 cycles

DURING INSPECTION, FOUR OVERWING RED EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK PASSED.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 38,760 hrs · 13,524 cycles

DURING MAINTENANCE, EPSU EMERGENCY EXIT AT LT POSITION FAULTED. R & R EPSU AT LT EMERGENCY EXIT, IAW AMM 33-51-38. OPS CHECK AND TEST OK.

Part: COMPUTER — FAILED (NR 2) · airframe 34,916 hrs · 12,248 cycles

AIRCRAFT DIVERTED, LOSS OF GPS DATABASE 180 DEGREES OFF IN FLIGHT. ACCOMPLISHED AFS TEST AND FOUND FMGC NR 2 FAILED. R & R NR 2 FMGC IAW MM 22-83-34. AFS TEST NORMAL.

Part: FILTER — FAILED (OZONE) · airframe 33,427 hrs · 11,774 cycles

HEAVY OIL & DIRTY SOCKS ODORS THROUGHOUT CABIN. CHECKED APU FOR OIL LEAKS AND BLEED DUCTS CONTAMINATION CHECKED OK. PERFORMED PACK BURN ECS CONTAMINATION IAW AMM 21-00-00-615-002, REPLACED BOTH OZONE FILTERS (100HM & 101HM) IAW AMM 21-51-41, OK FOR SERVICE.

Part: STRUT — OUT OF ADJUST (TE FLAP) · airframe 27,881 hrs · 9,866 cycles

FLT 393 LGA-MCO, CREW DECLARED EMERGENCY DUE TO FLAPS LOCKED (STOPPED LESS THAN ZERO). PERFORMED FULL CHECK OF LEFT AND RIGHT FLAPS ZERO RIGGING CHECK. ALL CHECKS NORMAL. ADJUSTED RIGHT INTERCONNECT STRUT PER AMM 27-51-44-865-062A. PERFORMED TEST OF FLAP INTERCONNECT STRUT FAILURE DETECTION SENSORS PER 27-51-44-710-058. ALL CHECKS OK.

Part: PROXIMITY SENSOR — OUT OF ADJUST (TE FLAP) · airframe 27,864 hrs · 9,859 cycles

FLT 510 FLL-EWR, CREW DECLARED EMERGENCY DUE TO F/CTRL ECAM FLAPS LOCKED ALIGNMENT FAULT DURING APPROACH. FLAPS LOCKED JUST PRIOR TO THE FIRST SETTING AT APPROX 190 KIAS AS FLAPS 2 WERE SELECTED. FOUND FLAP RIGHT PROX SENSOR 38 CV MISADJUSTED. ADJUSTED PER AMM 27-51-44, NO FAULTS.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 27,836 hrs · 9,850 cycles

FLT 448 TPA-BOS, CREW DECLARED AN EMERGENCY DUE TO FLIGHT CONTROL FLAPS LOCKED - ALIGNMENT FAULT. ACCOMPLISHED TSM TASK 27-51-00-810-830-A. SYSTEM CHECK NORMAL.

Part: CONNECTOR — BURNED (CABIN) · airframe 22,196 hrs · 7,879 cycles

FLT 779 JFK-MBJ, ELECTRICAL BURNING SMELL REPORTED IN AFT CABIN FROM GALLEY FWD TO ROW 22. NOTICED BY INFLIGHT AND CUSTOMER. STRONG ODOR FOR APPROX 4 MINS THEN BECAME LESS FOR THE REMAINDER OF THE FLIGHT. PERFORMED BURNING SMELL INSPECTION AS PER TSM 24-00-00-810-823 AND TSM 23-39-00-810-801. REPLACED 23LH XEB DUE BURNT CONNECTOR, ALSO REPLACED SEAT TO SEAT CABLE.

Part: CONTROL UNIT — FAILED (FUEL SYSTEM) · airframe 17,179 hrs · 6,104 cycles

FLT 259 FLL-FLL - FUEL LEAK STARBOARD WING, FLL OPS REPORTED THAT A/C ON TAKEOFF HAD A FUEL SPILL ON RUNWAY. THE FLIGHT CREW RETURNED TO FLL WITH NO INCIDENT. REMOVED AND REPLACED FUEL LEVEL SENSOR FLSCU (9QJ) FOR RT WING IAW AMM 28-46-34, OPS CHECK GOOD. ACCOMPLISHED FUEL WING TRANSFER IAW 28-15-00, OPS CHECK GOOD WITH RT WING FULL OF FUEL CAPACITY, NO LEAKS NOTED.

Part: VALVE — LEAKING (NR 1) · airframe 13,300 hrs · 4,694 cycles

FLT NR 26 FLL-JFK AIR RETURN TO FLL, DUAL ENG BLEED FAULT 1 FAILED AT 1200`, 2 FAILED AT 11,200`. FOUND NR 1 ENG FAN AIR VALVE LEAKING FROM DIAPHRAGM. REMOVED AND REPLACED NR 1 FAN AIR VALVE IAW 36-11-54. OPS AND LEAK CHECK OK. ENG RUN-UP IAW AMM 71-00-00, SATISFACTORY.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,037 hrs · 4,230 cycles

IN CRUISE, BURNING RUBBER TYPE ODOR IN AREA OF ROWS 18 TO 21, AFTER TURNING OFF LTV ODOR WENT AWAY, C/W TSM 23-39-810-801. NO LTV DISCREPANCIES NOTED, OP CHECK OF LTV SYS NML IAW MM 23-39-00. (K)

Part: COMPUTER — UNKNOWN (FLT MANAGE) · airframe 6,675 hrs · 2,386 cycles

FLT 515 EWR-FLL, ON ROTATION, -WARNING LANDING GEAR NOT DOWN- LOST SPEED A-THR, AP DISCONNECT. LOSS OF DATA ON PDF CONDUCTED. AIR RETURN TO EWR, OVERWEIGH LANDING. INTERROGATED PFR. T/S CENTRAL WARNING SYS AMM 31-50-00. NO DEFECTS. PERFORMED AFS/LAND TEST. NO DEFECTS. REPLACED FMGC 1 1CA1& 1CA2 PRECAUTIONARY PER AMM 22-83-34, PERFORMED OVERWEIGHT LANDING CHECK PER AMM 05-51-11. NO DEFECTS.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 370 hrs · 124 cycles

F/A REPORTED ACRID BURNING ODOR (NO SMOKE) FROM FWD GALLEY. ODOR SUBSIDED WHEN COFFEE POTS TURNED OFF. PERFORMED TSM TASK 24-00-00-810-823, CHECKED PINS AND NOSE TERMINALS BEHIND COFFEEEMAKERS. OK TO CONTINUE. PRECAUTIONARY REPLACED BOTH COFFEE MAKERS (S/N 191002510, 191002509).