N715JB

Part: UNKNOWN — ODOR (CABIN) · airframe 63,405 hrs · 22,399 cycles

FLT 1962, PBI-LGA, DURING CLIMB, STRONG PERSISTENT & INCREASING INDICATION OF OIL FUMES. LEVEL 3 DETERMINED USING FOM AND ISOLATION CHECKLIST. PACK 1 ISOLATED. CAPTAIN & FO AFFECTED. IRRITATED BURNING EYES, SCRATCHY THROAT, HEAVY RAIN DURING TAKEOFF AND CLIMB. C/W INFO NOTICE 2017-T015, SECTION B2. ODOR NOT PRESENT BUT IDENTIFIED AS POSSIBLE TYPE 1 ODOR DUE TO CREW DESCRIPTION. APU PLACED ON DEFFERAL AS PRECAUTION. DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-831A. A/C IS OK FOR SVC."

Part: UNKNOWN — ODOR (CABIN) · airframe 62,480 hrs · 22,036 cycles

FLT#813, HPN-FLL. '1/2 WAY THOURGH FLT F1 SAID MILD DIRTY SOCK SMELL ROWS 7 8 9 HE SAID HE NOTED IT DURING FINAL COMPLIANCE AS WELL (BEFORE T/O) (IT WAS NOT NOTIFIED) NO SMELL I THE COCKPIT UNTIL 4000 FT (DIRTY SOCK) COMPLIED W/ FCOM VOL 1 PROCEDURE FUMES WENT AWAY PUT PACK 1 BACK ON THE GROUND SMELL CAME BACK.' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: A/C PACK — FUMES (ZONE 100) · airframe 61,986 hrs · 21,843 cycles

FLT#1588, SXM-JFK. 'LEVEL 1 FUMES EVENT FROM PACK 1 IN THE DESCENT AT 11000FT DID ISOLATION PROCEDURE AND AFTER 3-5 MIN THE SMELL BACK SO LEFT PACK 1 OFF AND BLEED SHUT FOR THE REST OF THE FLIGHT . FA DID NOT SMELL ANYTHING ; ACCOMPLISHED LEVEL C DECONTAMINATION PER AMM 21-00-00-615-804-A REF LP 4238668 (ACCOMPLISHED LEVEL C DECONTAMINATION OF THE APU PER AMM 21-00-00-710-056A REF NEXT ITEM CONTAMINATION WITH C DECONTAMINATION. ACCOMPLISHED LEVEL C DECONTAMINATION PER AMM 21-00-00-710-056A NO ODOR PRESENT.) , 4238667 (REMOVED AND REPLACED #1 PACK CONDENSER PER AMM 21-52-32 OPS CHECK GOOD LEAK CHECK GOOD)', 4238666 (AS PER CABIN ODOR REPORT FORM DECISION TABLE THE MOST POSSIBLE SOURCE OF ODOR IS COMING FROM ENG 1 NO OIL BEHIND INLET CONE PERFORM LP COMPRESSOR STAGE 2.0 2.3 2.5 VANES & COMPRESSOR 3&4 AT NO3 BEARING REAR SEAL BORO INS& FOUND NO OIL CONTAMINATION CHECK PACK 1 CONDENSER OZONE FILTER ACM FOUND NO OIL CONTAMINATION FURTHER TS REQ ),4238663 (PERFORMED BSI OF #1 ENG LPC & HPC 3-4-5-6 FOUND NO EVIDENCE OF OIL WETNESS OR POOLING IN ANY SECTION PER AMM 72-00-00-200-016) FOR ALL ACCOMPLISHED WORK ODOR EXTINGUISHED A/C OK FOR SVC.'

Part: UNKNOWN — ODOR (CABIN) · airframe 61,934 hrs · 21,826 cycles

FLT#2904, RSW-BDL. 'ODOR/ FUME EVENT. DURING DESCENT FA'S IN AFT GALLEY REPORTED A FUEL SMELL IN THE FLIGHT DECK WE SMELLED A DIRTY SOCK SMELL. ( PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: APU — ODOR (ZONE 100) · airframe 61,131 hrs · 21,501 cycles

FLT# 8360, SJU-FLL. 'FUMES SMELL ON DESCENT AT ABOUT 10,000MSL UNTIL LANDING APU WAS OFF; C/W INFORMATION NOTICE 2017-T015, SECTION B2. DECONTAMINATION LEVEL 2(B) WAS ACCOMPLISHED PER TSM 05-50-00-810-085-B/D. APU FOUND TO BE SOURCE OF ODOR AND WAS DEFFERRE. ALL PACKS BURN C/W USING AIRTRT CART & ENGINES. RE-CIRCULATION FILTER CHANGED AS PRECAUTIONARY. NO ODOR PRESENT. A/C SAFE FOR RETURN TO SERVICE.'

Part: UNKNOWN — ODOR (CABIN) · airframe 61,128 hrs · 21,500 cycles

FLT# 2933, MCO-SJU. 'FUME DIRTY SOCK SMELL FOUND IN CABIN BEFORE FLIGHT; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2 IDENTIFIED ODOR. DECONTAMINATION LEVEL B ACCOMPLISHED PER TSM 05-50-00-810-831-A. REF LOGPAGE 4073850 ITEM 1 AND 2. LOGPAGE 4073849 ITEM 2 FOR CORRECTION ACTION.'

Part: A/C PACK — ABNORMAL (CABIN AIR) · airframe 60,826 hrs · 21,376 cycles

FLT#1009, JFK-SDQ. 'GOING THROUGH APPROXIMATELY 15000 ON DESCENT TEH CAPT SMELLED AN ACRID ODOR DIRTY SMELL. NOT DIRTY SOCKS. APPROX 10000 # 4 INFLIGHT CALLED AND ADVISED "WE WERE HAVING A FUMES EVENT THAT WAS LIKE A BURNING WIRE SMELL." ALSO DESCRIBED AN ACRID BURNING EYES , NOSE , THROAT IRRITATION. BEGAN ABOUT ROW 15 AND WORSE FURTHER BACK. CUSTOMERS ALSO COMPLAINED ABOUT THE SMELL. LASTED THROUGHOUT DESCENT AND AGENT AT GATE CAME ON BOARD AFTER DEPLANING AND COULD STILL SMELL THE FUMES/ ODOR; COMPLIED WITH INFORMATION NOTICE 2107-TO15 , SECTION A ISOLATED FAULT TO TYPE 10 PER TSM 05-50-00-810-085-B/ TSM .05-50-00-810-085-D. ALSO ACCOMPLISHED WITH TSM TASK 24-00-00-810-823-A. MCC SAI NOTIFIED A/C OK FOR SVC.'

Part: FRAME — CRACKED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD AND AFT SIDE OF THE FRAME SEGMENT (1) THE EEH 844 PASSENGER CABIN CRACK LENGTH IS 0.350 INCHES; CORRECTIVE ACTION: REMOVED AND REPLACED THE FRAME SEGMENTS ON THE EMERGENCY EXIT DOOR 844 I.A.W EC. A320-52-1144 AND A320 SRM 51-72-11. FOR INSTALLATION REFERENCE AND SEE TASK CARD A320-52-1144-04-JB.

Part: SKIN — DAMAGED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: MISSING MATERIAL ON EXTERNAL SKIN LOCATED BTW FRAME 78 TO FRAME 80 PLUS 4 INCH AND BTW STRINGER 1 LH TO 1RH THS COMPARTMENT; (RESOLVED ON W/O: 1289680 TASKCARD: NR-00036) PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW FRAME 78 TO FRAME 81 BTW STRINGER 2L TO STRINGER 2R ON THS COMPARTMENT IAW A320 SRM 53-51-11-300-002 WITH DEVIATIONS AND EA #53-9042-24 EA COVER REVISION# 0, EA PART 1, EA PART 2, EA PART 3. THIS REPAIR IS CATEGORY A NO ADDITIONAL REQUIREMENTS IS REQUIRED. PERFORMED LAY OUT ON EXTERNAL SKIN, BTW FR78 AND FR82, BTW STR3R TO STR3L I.A.W. EA #53-9042-24, PART #2, PART C, STEP 1. PERFORMED DOUBLER REPAIR LOC. FROM FR78 TO FR81, BTW STR2L AND STR2R, I.A.W A320 SRM 53-51-11-300-002 AND STEP 1 OF EA # 53-9042- 24 PART# 2 PART C ITEM (A),(B),(D) DRILLED AND COUNTERSUNK OPEN HOLES ON DOUBLER REPAIR I.A.W A320 SRM 51-44-11 AND A320 SRM 51-46-11. PERFORMED CHAMFER ON EDGE OF DOUBLER REPAIR I.A.W A320 51-47-00. MATERIAL USE: SHEET METAL CLAD 2024 T3 AND THICKNESS 1.80 MM (0.071 INCH) PO: 2023-278719/001. APPLIED PROTECTIVE TREATMENT ON NEW DOUBLER REPAIR AND REPAIR AREA LOC. FROM FR78 TO FR81, BTW STR2L TO STR2R, I.A.W A320 SRM 51-21-11 AND A320 51-23-11.

Part: FRAME — CRACKED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD AND AFT SIDE OF THE FRAME SEGMENT (1) THE EEH 834 PASSENGER CABIN CRACK LENGTH IS 0.280 INCH; REMOVED AND REPLACED THE FRAME SEGMENTS ON THE EEH 834 (1EA) IAW EC. A320-52-1144 A320 SRM 51-72-11. FOR INSTALLATION REFERENCE AND SEE TASK CARD A320-52-1144-03.

Part: FRAME — CRACKED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR16 AT FWD GALLEY AREA, DOOR STOP FITTING 7 UPPER I/B RH SIDE, CRACK POSITION 7 O'CLOCK; REF: ARM W/O 2024 314/1 N/R 2024-526804 R&R INTERCOSTAL FITTING IAW A320 SRM 53-11-12-300-010 & A320 DWG D53114223. THIS REPAIR IS CAT A.

Part: FRAME — CRACKED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR16 AT FWD GALLEY AREA, DOOR STOP FITTING 7 UPPER I/B LH SIDE, AT 6 O'CLOCK; REF: ARM W/O 2024 314/1 N/R 2024-526805 R&R INTERCOASTAL FITTING IAW A320 SRM 53-11-12-300-010 AND DWG D53114223. THIS REPAIR IS CAT A.

Part: FRAME — CRACKED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR16 AT FWD GALLEY AREA DOOR STOP FITTING 7 LOWER INBOARD RH SIDE POSITION AT 6 O'CLOCK; REF: ARM W/O 2024 314/1 N/R 2024-526803 R&R INTERCOATAL FITTING IAW A320 SRM 53-11-12-300-010 & DWG D53114223. THIS IS CAT A.

Part: FRAME — CRACKED (ZONE 100) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD AND AFT SIDE OF THE FRAME SEGMENT (1) THE EEH 843 PASSENGER CABIN CRACK LENGTH IS 0.315 INCH; REMOVED AND REPLACED THE FRAME SEGMENTS ON THE EMERGENCY EXIT DOOR 843 I.A.W EC. A320-52-1144 AND A320 SRM 51-72-11. FOR INSTALLATION REFERENCE AND SEE TASK CARD A320-52-1144-02-JB.

Part: TAIL CONE — DAMAGED (ZONE 100) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: FUSELAGE/ REAR FUSELAGE/ TAIL CONE/ FR 78-81 STGR 2L-2R/ MULTIPLE DAMAGE- PERMANENT REPAIR; REFERENCES /1/ AEROMAN EA 53-9042-24 COVER R0 AND PARTS 1-3 /2/ RDAF 81457190/005/2024 ISSUE A /3/ TD/81457190/058/2024#A. DURING CURRENT (10/2024) H3 HEAVY CHECK AT SAL, N715JB (MSN 03554) WAS REPORTED WITH MULTIPLE DAMAGES TO THE REAR FUSELAGE TAIL CONE. SEE REF /1/ EA FOR DETAILS. THERE WAS MISSING MATERIAL AT CONE/REAR FUSELAGE TAIL CONE SKIN PANEL BETWEEN FR 78-81 AND STGR 2L-2R. FURTHER DVI PER NTM 51-90-00 WAS PERFORMED ON INTERNAL AND EXTERNAL DAMAGE AREA AND CRACKS WERE NOTED AT FR 79 AND STRINGER 1. ADDITIONALLY, STGR 1 AND 2R WERE REPORTED BENT. THE ROOT CAUSE OF THE DAMAGE IS UNKNOWN. AIRBUS WAS CONTACTED AND PROVIDED REPAIR INSTRUCTIONS PER REF /3/ TD INSTRUCTING TO INSTALL A DOUBLER REPAIR ON SKIN DAMAGES, PERFORM SPLICE REPAIRS ON DAMAGES AT FR79, AND PERFORM SRM TASK 53-00-13-300-001 ON STGR 1 AND 2R DAMAGES. SUBSTANTIATION: AIRBUS APPROVED THESE REPAIRS PER REF /2 RDAF AND IS CLASSIFIED AS MAJOR. (E/C: A24-1283-01)

Part: FRAME — CRACKED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FR16 AT FWD GALLEY AREA DOOR STOP FITTING 7 LOWER I/B, LH SIDE CRACK POSITION AT 1 O'CLOCK; (RESOLVED ON W/O: 1289680 TASKCARD: NR-00022) REF: ARM W/O 2024 341/1 N/R 2024-526806 PERFORMED PERMANENT REPAIR IAW A320 SRM 53-11-12-300-010. THIS REPAIR IS CAT B, ADL/REPAIR EMBODIMENT 12700FC/FH NOT RLEVANT. SUB INSP 12700FC/FH NOT RELEVANT. INSP METHOD TASK53-11-12-300-010 FIG 009. FUR-A320-53-01744 ASSIGNED.

Part: FRAME — CRACKED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD AND AFT SIDE THE FRAME SEGMENTS (1) THE EEH 833 CRACK LENGTH IS 0.330 INCH; REMOVED AND REPLACED THE FRAME SEGMENTS ON THE EEH 833 (1EA) IAW EC. A320-52-1144 A320 SRM 51-72-11. FOR INSTALLATION SEE TASK CARD A320-52-1144-01.

Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 60,620 hrs · 21,299 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE H2, LOCATED ON CROSSBEAM SPLIC AREA FR16 LH SIDE ON PASSENGER CABIN; REF; ARM W/O 2024 314/1 N/R 2024-526802 PEFORMED PERMANENT REPAIR ON HOLE 2 LOC CROSSBEAM SPLIC IAW DWG R53112926 ISSUE E. THIS IS CAT A REPAIR.

Part: OIL COOLER — LEAKING (APU) · airframe 59,843 hrs · 20,984 cycles

FLT#1167, HPN-PBI. 'F/A REPORT DIRTY SOCK SMELL MID AND AFT CABIN; REMOVED AND REPLACED APU OIL COOLER IAW AMM 49-91-44. OPS / LEAK CHK GOOD. RAN APU FOR 45 MIN, NO DIRTY SOCKS SMELL. A/C OK FOR SVC.'

Part: OIL SYSTEM — LEAKING (APU) · airframe 59,825 hrs · 20,976 cycles

FLT#1287, PVD-PBI. FA REPORTED DIRTY SOCK SMELL AFT GALLEY ON DESCENT AT 4000'; COMPLIED WITH INFO NOTICE 2017-015K. IDENTIFIED ODOR CAUSED BY APU OIL LEAK. (SEE DEFECT 3906135, ITEM 2 (WO 1338238 ACCOMPLISHED)) REMOVED AND REPLACED L/H & R/H PACK OZONE CONVERTERS IAW AMM 21-58-42. DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-085B, AIRCRAFT IS OK FOR SVC.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,598 hrs · 20,129 cycles

FLT#2188, BNA-LGA. 'DESCENDING FROM ALTITUDE FROM 25000-18000 SMELLED DIRTY SOCKS IN COCKPIT AND REAR CABIN THRUST IDLE CLEAR AIR APU OFF ODOR INCREASE AS POWER CAME IN DURING LEVEL OFFS STARTED DISSIPATING LOWERAPU INOP ( APU SYSTEM ); PERFORMED APU INSPECTION PER AMM 49-00-00-200-811-A. APU HAS BEEN REPLACED ON 10/16/2023 NO EVIDENCE OF OIL OR FUEL FOUND, RAN APU FOR COUPLE HOURS AND NO SMELL OR FUMES INSIDE CABIN NOTED. MDDR 527763 CLEARED. MX-4 UPDATED, PLACARD REMOVED. MCC NOTIFIED.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,402 hrs · 20,049 cycles

FLT#1248, TPA-LGA. 'DIRTY SOCK SMELL TURNED OFF PACK 1 AND SMELL SUBSIDED ( APU BLEED AIR SUPPLY SYSTEM ); T/S APU ODOR PER AMM 49-00-00-200-811-A, AND FOUND NO PRESENCE OF OIL IN APU COMPARTMENT, ALSO NO PRESENCE OF ODOR COMING FROM APU. APU OK FOR SVC. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,379 hrs · 20,041 cycles

FLT#1248, TPA-LGA. 'ON TAKEOFF VERY STRONG CHEMICAL /MUSTY ODOR IN FLIGHT DECK.FUMES/ODOR WERE MAGIC MARKER /SWEET SMELLING. ODOR WAS MODERATE AND INTENSITY PERSISTENT AND INCREASING FROM AIR VENTS. FCOM ODOR /ISOLATION PROCEDURE ACCOMPLISHED. ODOR BEGAN TO DISIPATE AFTER PACK 1 ISOLATED AND TURNED OFF. CONSIDERED LEVEL 2 BY FLIGHT CREW ( PACKS ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,281 hrs · 20,000 cycles

FLT#39, FLL-SJO. 'DURING DESCENT BELOW 10000 CABIN CREW REPORTED DIRTY SOCKS ODOR MID CABIN AND REAR LEVEL 1 - APU OFF; COMPLIED WITH INFO NOTICE 2017 - T015 SECTION B1 AND PERFORMED INSPECTION OF APU AND BOTH ENGINES WITH NO EVIDENCE OF LEAKS OR DUPLICATION OF SMELL. A/C OK FOR SVC.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,908 hrs · 19,850 cycles

FLT#299, LGA-MCO. 'INFLIGHT REPORT DIRTY SOCK ODOR IN CABIN; COMPLIED WITH INFO NOTICE 2017-T015, SECTION B2. DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. AIRCRAFT IS OK FOR SERVICE.'

Part: NONE — NONE · airframe 52,426 hrs · 18,120 cycles

FLT#2320, SLC-FLL. ' LEVEL 1 ODOR EVENT IN CRUISE 2 AND HOURS INTO FLT. INFLIGHT REPORTED A STRONG DIRTY SOCK SMELL IN THE AFT RIGHT GALLEY. THE SMELL WOULD COME AND GO EVERY FEW MINUTES. AFTER SHUTDOWN AND SELECTION OF APU BLEED, DIRTY SOCK SMELL IN COCKPIT; "COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A (A), ISOLATED FAULT TO TYPE 10,(A) I, C PER TSM 05-50-00-810-085-B/TSM 05-50-000-810-085-D AIRCRAFT IS OK FOR SERVICE." THE LAST TRANSIENT ODOR WAS REPORTED 47 F/C AGO. '

Part: NONE — NONE · airframe 52,270 hrs · 18,056 cycles

FLT#655, SYR-MCO. 'FUMES STRONG CHEMICAL BURNING SMELL DESCENDING THROUGH 5,000; AS PRECAUTIONARY PERFORMED ENGINE RUNS (ENG 1-2)- WITH ASSOCIATED PACKS, COULD NOT DUPLICATE. COMPLIED WITH INFO. NOTICE 2017-T015, SECTION A. ISOLATED FAULT TO TYPE 10A. PER TSM 05-50-00-810-085-B/TSM 05-50-00-810-0885D. A/C IS OK FOR SERVICE.'

Part: NONE — FAILED (101HM) · airframe 52,221 hrs · 18,037 cycles

FLT#149, JFK-GND. 'AFTER LANDING FLIGHT ATTENDANTS REPORTED DIRTY SOCKS SMELL PASSING THROUGH 10,000FT UNTIL LANDING REPORTING HEADACHES. APU WAS OFF. THE FLIGHT DECK DID NOT SMELL (PACKS); PERFORMED LEVEL C DECONTAMINATION PER TSM 05-50-00-810-831A REPLACED OZONE FILTER 1 2 PER AMM 21-51-41-PB 401 REPLACE RECIRC FILTER PER AMM 21-21-410.'

Part: ECS — CONTAMINATED · airframe 52,190 hrs · 18,025 cycles

FLT#1447, HPN-TPA. 'ACRID SMELL ORIGINATING FROM BLEED ENG 1 ISOLATED SYSTEM AND SMELL WENT AWAY; COMPLIED WITH INFORMATION NOTICE 2017-T015I, SECTION A. ISOLATED TO TYPE 10 PER TSM 05-50-00-810-085B & D. AIRCRAFT OK FOR SERVICE. ALSO C/W LEVEL B DECONTAMINATION OF ECS PER AMM 21-00-00-615-803A FOR LEVEL 2. RECIRCULATION FILTERS REPLACED. NO FAULTS FOUND OK FOR SERVICE.'

Part: NONE — NONE · airframe 51,968 hrs · 17,951 cycles

FLT#1521,LGA-FLL. 'LEVEL 2 FUMES EVENT ON LEVEL OFF BEOLW 800O', PILOTS & BACK F/A DETECTED IT. ISOLATED PACK 1, WENT AWAY UPON TOUCHDOWN; RAN ENGINES #1 AND #2- NO ODOR FOUND. INSPECTED APU AND FOUND MULTIPLE OIL LEAKS AND OIL RESIDUE ON APU AIR DUCTS. DECONTAMINATION OF BLEED AIR DUCTS IAW AMM 36-13-00. APU TO BE PLACED ON MEL. REF L/P 3251188-2 MDDR 466593. COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B(2). AIRCRAFT IS OK FOR SERVICE.'

Part: UNKNOWN — ODOR (CABIN) · airframe 51,434 hrs · 17,765 cycles

FLT # 1853, JFK-PBI. INBD CABIN CREW REPORTS ELETIRC ODOR ON PREVIOUS DESCENT FROM 10,00 FEET TO TOUCH DOWN ODOR THROUGHOUT CABIN. ( THALES-AVANT IFE (ENTIRE SYSTEM) ) ; PERFORMED 05-50-00 INSPECTION NO FAULTS FOUND AS PRECAUTIONARY PLACING ITEM ON NEF N44-20-02D MX-4 UPDATED PLACARD INSTALLED MCC GEORGE NOTIFIED. DEACTIVATED AVANT IFE SYSTEM, PULLED AND COLLARD LAIC, VCC/ICMT, TSU, ACS, DSI 1 & 2, SEAT POWER MCU 1, SEAT POWER MCU 2 CIRCUIT BREAKERS (M) PROCEDURE COMPLIED WITH.REF LP 3246877 ITEM 1 FOR MX INSPECTION REENERGIZED AVANT IFE SYS PER AMMS TASK 44-21-00-860-801 NO FAULTS FOUND OPS CHK OK MDDR CLRD MX-4 UPDATED PLACARD REMOVED JB MCC GAULDA NOTIFIED. ENERGIZED THE IN-SEAT POWER SUPPLY SYSTEM REF AMMS 44-22-00-860-801 OPS CHK OK MDDR CLRD MX-4 UPDATED PLCARD REMOVED.

Part: DOOR — DAMAGED (L-1 DOOR) · airframe 51,431 hrs · 17,763 cycles

FLT # 894, STI-EWR. WHILE AGR WAS MOVING THE AIRCRAFT OFF THE GATE, THE AIRCRAFT ROLLED BACK DUE TO MAIN LANDING GEAR WHEELS NOT BEING CHOCKED. L1 DOOR MADE IMPACT WITH JETBRIDGE. DAMAGE FOUND ON BOTTOM OF DOOR ON THE RIGHT-HAND CORNER.; ACCOMPLISHED REPAIR ON L-1 DOOR IAW/SRM 51-73-00 QC PERFORMED HFEC REF 4P3246875 ITEM #1 NO CRACKS FOUND APPLIED SURFACE PROTECTION IAW SRM 51-75-11 MX-4 UPDATED

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 50,336 hrs · 17,375 cycles

FLT 1076, MCO-PVD. EXIT SIGN ON DOOR 2R IS NOT ILLUMINATED; R & R BATTERY OF THE EPSU. OPS CHECK GOOD. REF AMM 33-51-38

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 50,331 hrs · 17,373 cycles

DURING HEAVY MAINTENANCE, EPSU BATTERY 10WL DON'T PASS TEST; (REF ARM W/O 2021-197/1 N/R 2021-381719) R & R EPSU 10WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A PERFORMED OPERATIONAL TEST. TEST IS OK

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 50,331 hrs · 17,373 cycles

DURING HEAVY MAINTENANCE, EPSU BATTERY 11WL DON'T PASS TEST; (REF ARM W/O 2021-197/1 N/R 2021-381720) R & R EPSU 11WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A PERFORMED OPS TEST. TEST IS OK

Part: COVER — DISPLACED (DOOR SLIDE) · airframe 50,331 hrs · 17,373 cycles

DURING HEAVY MAINTENANCE, PUSHED ENCLOSURE OFF WING SCAPE SLIDE . ALL THE BALLS ARE IN ON LH WING; (REF ARM W/O 2021-197/1 N/R 2021-355368) R & R OFFWING SCAPE SLIDE IAW AMM 25-62-42-000-001-A AND AMM 25-62-42-400-001-A TEST IS OK. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 50,331 hrs · 17,373 cycles

DURING HEAVY MAINTENANCE, EXIT SIGN ON DOOR 2R DID NOT ILLUMINATE; R & R BATTERY OF THE EPSU. OPS CHECK GOOD. REF AMM 33-51-38

Part: FAN — FAILED (E/E BAY) · airframe 48,698 hrs · 16,796 cycles

FLT 110, SDQ-JFK. FELT VIBRATION WITH ELECTRICAL BURNING SMELL VENT EXTRACT FAULT ECAM CAUTION; R & R EXTRACT FAN REF AMM 21-26-51 OPS CCHECK OK FAULTS CLEARED A/C OK FOR CONT SVC

Part: UNKNOWN — ODOR · airframe 44,448 hrs · 15,218 cycles

FT # 499, LGA-MCO. TRICRESYL PHOSPHATE ODOR/ FUME STARTED IN DECENT AT 12,000 FUMES DISSIPATED WITH PACK 2 OFF FUME REPORT ATTACHED; ODOR IS DETERMINED TO BE A LEVEL 1 ODOR COND. COMPLIED WITH INFO NOTICE 2017-T015E SECTION A. RAN BOTH ENGINES IAW SECTION C TABLE 1. NO ODOR NOTED A/C OK FOR SVC.

Part: SLIDE — DEFECTIVE (PAX DOOR) · airframe 42,631 hrs · 14,576 cycles

DURING HEAVY MAINTENANCE, BUMP IN PAX DOOR SLIDE 832; REF AEM NR 2019-14/1 - 2019-50048. REPLACED ESCAPE SLIDE RAFT AT 832 IAW AMM 25-62-44-400-002-A. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: VENT — CORRODED (FUSELAGE) · airframe 42,574 hrs · 14,550 cycles

FLT 2191. BOS-TPA. AIRCRAFT WAS FOUND WITH CORROSION DAMAGE AT THE LAVATORY VENT LOCATED IN THE REAR FUSELAGE BETWEEN FR 69-70 AND STR 31R-32R. THE AIRCRAFT WAS FERRIED TO LHT IN BQN WHERE THE DAMAGE WAS EVALUATED AGAINST THE REF /4/ SRM AND FOUND TO BE OUT OF LIMITS, DUE TO THE EXTENT OF THE DAMAGE REQUIRING A LARGER CUTOUT THAN ALLOWED IN THIS SRM. THEREFORE, LHT CONTACTED FOR REPAIR DISPOSITION. PROVIDED THE REF/3/ TD WHICH INSTRUCTS THE DAMAGE TO BE REPAIRED PER THE REF /4/ WITH THE DEVIATION OF THE EXTENDED CUTOUT ONE FASTENER ROW IN THE DOWN DIRECTION. LHT PERFORMED THE REPAIR PER THE INSTRUCTIONS IN THE REF /3/ TD AND THIS PERMANENT REPAIR IS APPROVED PER REF /2/ RDAS. THIS EC ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ EO AND COMPLIES WITH REF/2/ RDAS WITHOUT DEVIATION; THIS PERMANENT CATEGORY A REPAIR HAS BEEN APPROVED VIA REF /2/ RDAS AND IS CLASSIFIED AS MAJOR.

Part: VENT — CORRODED (FUSELAGE) · airframe 42,574 hrs · 14,550 cycles

FLT 2191,BOS-TPA. ON 1/9/2019 WAS FOUND WITH CORROSION DAMAGE AT THE LAVATORY VENT LOCATED IN THE REAR FUSELAGE BETWEEN FR 69-70 AND STR 31R-32R. THE AIRCRAFT WAS FERRIED TO LHT IN BQN WHERE THE DAMAGE WAS EVALUATED AGAINST THE REF /4/ SRM AND FOUND TO BE OUT OF LIMITS, DUE TO THE EXTENT OF THE DAMAGE REQUIRING A LARGER CUTOUT THAN ALLOWED IN THIS SRM. THEREFORE, LHT CONTACTED FOR REPAIR DISPOSITION. PROVIDED THE REF /3/ TD WHICH INSTRUCTS THE DAMAGE TO BE REPAIRED PER THE REF /4/ WITH THE DEVIATION OF THE EXTENDED CUTOUT ONE FASTENER ROW IN THE DOWN DIRECTION. LHT PERFORMED THE REPAIR PER THE INSTRUCTIONS IN THE REF /3/ TD AND THIS PERMANENT REPAIR IS APPROVED PER REF /2/ RDAS. THIS EC ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ EO AND COMPLIES WITH REF /2/ RDAS WITHOUT DEVIATION; THIS PERMANENT CATEGORY A REPAIR HAS BEEN APPROVED VIA REF /2/ RDAS AND IS CLASSIFIED AS MAJOR.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,574 hrs · 14,550 cycles

FLT 2191. BOS-TPA. AIRCRAFT WAS FOUND WITH CORROSION DAMAGE AT THE LAVATORY VENT LOCATED IN THE REAR FUSELAGE BETWEEN FR 69-70 AND STR 31R-32R. THE AIRCRAFT WAS FERRIED TO LHT IN BQN WHERE THE DAMAGE WAS EVALUATED AGAINST THE REF /4/ SRM AND FOUND TO BE OUT OF LIMITS, DUE TO THE EXTENT OF THE DAMAGE REQUIRING A LARGER CUTOUT THAN ALLOWED IN THIS SRM. THEREFORE, LHT CONTACTED FOR REPAIR DISPOSITION. PROVIDED THE REF /3/ TD WHICH INSTRUCTS THE DAMAGE TO BE REPAIRED PER THE REF /4/ WITH THE DEVIATION OF THE EXTENDED CUTOUT ONE FASTENER ROW IN THE DOWN DIRECTION. LHT PERFORMED THE REPAIR PER THE INSTRUCTIONS IN THE REF /3/ TD AND THIS PERMANENT REPAIR IS APPROVED PER REF /2/ RDAS. THIS EC ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ EO AND COMPLIES WITH REF /2/ RDAS WITHOUT DEVIATION; THIS PERMANENT CATEGORY A REPAIR HAS BEEN APPROVED VIA REF /2/ RDAS AND IS CLASSIFIED AS MAJOR.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 39,190 hrs · 13,332 cycles

EPSU BATTERY 10WL FAILED AN EMERGENCY LIGHT TEST. R & R THE BATTERY IAW AMM 33-51-38, SYSTEM OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 36,173 hrs · 12,383 cycles

DURING HEAVY MAINTENANCE, EMERGENCY LIGHTS FAILED AN EPSU SYSTEM TEST. CLEANED AND RECONNECTED 43WL, 42WL, 44WL AND 45WL IAW AWM 33-51-03 SHEET 02. OPS CHECK GOOD IAW AMM 33-51-00-710-001-A.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 34,514 hrs · 11,828 cycles

EMERGENCY LIGHTS IN AUTO DID NOT ILLUMINATE WHEN POWER DROPPED OFF. R & R THE BATTERY PACK AT 10WL IAW AMM 33-51-00. OPS CHECKED GOOD.

Part: APU — ODOR · airframe 34,512 hrs · 11,827 cycles

FLIGHT ATTENDENTS AND PAX SMELLED A STRONG FOUL ODOR PASSING THROUGH 10,000 FT DURING DESCENT; FOUND APU TO BE THE SOURCE OF THE ODOR. R & R THE APU.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 30,936 hrs · 10,756 cycles

CORROSION FOUND ON LT WING UPPER SURFACE AT RIB 2, STR 11, FASTENER HOLE 606 IN UPPER LAYER OF BORE. REF DWG 571183A57120, SHEET 01; REPAIRED IAW ECA16-294-01 AND REO-L19823.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 30,936 hrs · 10,756 cycles

CORROSION FOUND ON RT WING T/E TOP SKIN OF RIB 15, UNDER ATTACH POINT FOR GLASS CLOTH SEAL PLATE. REPAIRED ECA16-287-01 AND REO L19816RI.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 30,032 hrs · 10,438 cycles

EMERGENCY LIGHT FAILS TEST. R & R EMERGENCY LIGHT BATTERY AT 12WL. EMERGENCY LIGHT, OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 18,827 hrs · 6,428 cycles

FLT 374 FLL-LGA, AIRCRAFT DIVERTED TO JFK DUE TO UPON GEAR SELECTION DOWN GOT ECAM L/G DOOR NOT LOCKED FOLLOWED BY LANDING GEAR NOT DOWN INDICATION (LDG GEAR DOWN WAS SHOWING DOWN & LOCKED). T/S REVIEWED CFDS PFR & LAST REPORTS/ PREVIOUS HISTORY. LGCIU 2 REPORTS R L/G DOWNLOCK PROX SENSOR 16GA. REPLACED 16GA SENSOR IAW AMM 32-31-73-04.

Part: BATTERY — FAILED (CABIN) · airframe 11,427 hrs · 4,009 cycles

FLT 654 SJU-TPA EPSU BATT FIN 11WL FAILS BATT CAP TEST. REPLACED BATTERY AT EPSU FIN 11WL PER AMM 33-51-38, OPS CHECKED OK.

Part: PROXIMITY SENSOR — FAILED (RT MLG) · airframe 11,404 hrs · 3,997 cycles

FLT 61 JFK-FLL, CREW DECLARED EMERGENCY DUE TO UPON GEAR EXTENSION INDICATION OF GEAR DOORS NOT CLOSED AND ON LOWER ECAM RT MAIN GEAR 1/2 OF GEAR TRIANGLE INDICATED RED AFTER GEAR RECYCLE. THE SECOND TIME GEAR DOORS CLOSED BUT 1/2 OF TRIANGLE STILL RED. AT ABOUT 500FT IN FINAL GOT THE CRC AND UPPER ECAM OF GEAR UNSAFE. TECHNICIAN FOUND 16GA PROXIMITY SENSOR RT MAIN LDG GEAR AT FAULT REMOVED AND REPLACED 16 GA SENSOR IAW AMM 32-31-73, ALL FUNCTIONS NORMAL.

Part: GCU — FAILED (NR 2) · airframe 11,296 hrs · 3,950 cycles

FLT 47 JFK-FLL, AIR RETURN BACK TO JFK- GEN 2 FAULT ON ECAM AFTER TAKEOFF AT 5000FT 250 KNOTS. CYCLE PUSH BUTTON GEN 2, NEVER CAME BACK ONLINE. REMOVED AND REPLACED ENGINE NR 2 GCU IAW AMM 24-22-34. OPS CHECK OK.

Part: POWERPLANT — FLAMED OUT (NR 1) · airframe 259 hrs · 77 cycles

FLT 354, BUR-JFK, UPON LANDING NR 1 ENG FLAMED OUT ON ROLL OUT, AFTER ENG 1 COMP FAIL ECAM FOLLOWED BY ENG 1 FAIL ECAM. DVDR ANALYSIS DETERMINED NR1 ENG REQUIRES ENG REPLACEMENT DUE TO EGT OVERLIMIT. REMOVED AND REPLACED NR1 ENG PER TC A320-71-00-20-400-040. OPS CHECK OK. (S)