N705JB

Part: SKIN — CORRODED (ZONE 100) · airframe 63,400 hrs · 22,681 cycles

DURING HEAVY MAINTENANCE: FUSELAGE SKIN HAS CORROSION AT LAV VENT FR69-70 STR 32R-31R. RESOLVED ON W/O: 1428515 TASKCARD: NR-00002. REF HAECO WO 440633 NR 40009. PERFORMED REPAIR IAW SRM 53-41-11-300-004. TO BE REINSPECTED AT 60000FC FROM ACFT FIRST FLIGHT PER SRI 53-41-11-205-134 TABLE 5. WORK PERFORMED AT LAV VENT FR 69-70. WORK ACCOMPLISHED FUR-A320-53-02483.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 62,642 hrs · 22,368 cycles

FLT#2080, FLL-DCA. 'L/H & R/H EWD OTW DOOR EMER LIGHT (ONE BULB INOP); L/H & R/H FWD OTW DOOR EMER LIGHT (ONE BULB) R/R BULB - OPS CHECK GOOD IAW 33-50-00.'

Part: GIRT BAR — DAMAGED (L1 DOOR) · airframe 61,037 hrs · 21,766 cycles

FLT#521, BOS-PBI. 'HORRENDOUS FUMES/OIL ODOR ON T/O FUMES STOPPED ABRUPTLLY W/ PACK 1 OFF DURNING ODOR ISOLATION CHECKLIST; C/W INFO NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TYPE 1 INSPECTTED APU COMPARTMENT AND FOUND TO BE CLEAN WITH NO OIL . PERFORMED DECONTAMINATION WITH APU BLEED AND ENG 1 AND 2 REPLACED RECERC FILTERS AS PRECAUTION. A/C OK FOR SVC, NO FURTHER DEFECTS NOTED.'

Part: A/C PACK — FAILED · airframe 61,031 hrs · 21,764 cycles

FLT#1441, BOS-SRQ. 'CLIMBING THRU FL260, DIRTY SOCK SMELL FROM COCKPIT AIR VENTS. RAN COCKPIT ODOR ISOLATION PROC. PACK 1 TURNED OFF. ODOR DISSIPATED. MX-270 COMPLETED;C/W INFO NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TYPE 10 ODOR WAS A DIRTY SOCK SMELL PERFORMED DECON LEVEL C PER TSM 05-50-00-810-085B A/C IS OK FOR SVC AND THAT CLEARS MDDR #656277 MX4 UPDATED PLACARD REMOVED.'

Part: APU — CONTAMINATED (ZONE 100) · airframe 60,431 hrs · 21,538 cycles

FLT#1433, MCO-SJU. 'DESCENDING THUR FL200 FO SMELL DIRTY SOCKS SMELL. CA NOTICE IT AROUND 17000 FEET, IT WAS A MILT BUT PERSITING ODOR. WE TENT TO THINK IT WAS A LVL 1 ENV.SYST ODOR. INFLIGHT DIDNT SMELL IT. WE RAN DID ESOLATION CHECK AND COULD TELL A DECREASE IN ODOR WITH PACK 1 OFF. NO ONE IN THE CREW EXPERIENCE ANY PHYSIOLOGICAL EFECTS, NOR ANY CUSTOMER COMPLAINS; COMPLIED WITH INFO NOTICE 2017-T015 SECTION A ISOLATED TO FAULT TYPE 1 (APU). PERFORMED LEVEL A DECONTAMINATION PER AMM 21-00-00-615-802A R/R HEPA FILTERS. NO ODOR PRESENT AT THIS TIME.

Part: SEAL — LEAKING (NR 1 TURBINE) · airframe 60,422 hrs · 21,534 cycles

FLT#128, MCO-EWR. STRONG ACRIT/METALLIC SMELL NOTED WHILE DESCENDING THROUGH 17,000 FT. PLEASE SEE ATTACHED FORM MX-270; FOLLOW INFO NOTICED 2017-T15K AND BY TSM 05-50-00-810-813-A. FOUND ENG #1 BEING THE SOURCE OF THE SMELL. INSPECTED ENG #1 AND FOUND OIL ON THE INLET CONE IAW TSM 71-00-00-810-801A. REMOVED AND REPLACED LP TURBINE SHAFT BLIND SEAL ON ENG #1 IAW AMM 72-38-11. NO LEAKS NOTED. DECONTAMINATION ACCOMPLISHED IAW AMM 36-10-00615-803. W/ ENG #1 AND #2 BLEED. NO ODOR NOTED IAW AMM 71-00-00.'

Part: UNKNOWN — ODOR (ZONE 200) · airframe 60,398 hrs · 21,526 cycles

FLT#746, PSE-JFK. 'CREW REPORTED BURNT CRAYON SMELL ON ON DECENT.' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: COOLING FAN — LEAKING (APU) · airframe 60,367 hrs · 21,515 cycles

FLT#1575, FLL-KIN. 'LIGHT DIRTY SOCK SMELL FLT DECK IN DESCENT. FA REPORTS ODOR PRESENT MID-CABIN IN DESCENT. WITH APU USE, PRE-BOARDING ENTIRE CABIN HAS MODERATE PUNGENT ODOR. CLEANERS AND GATE AGENTS NOTIFIED. (APU WAS OFF IN DESCENT); C/W INFO NOTICE 2017-T015K. DUE TO APU CAUSE OF CABIN ODOR. APU COOLING FAN PREVIOUSLY FOUND LEAKING AND WAS REMOVED AND REPLACED. PERFORMED APU WASH CLEANING. LEVEL A DECONTAMINATION ACCOMPLISHED PER TSM 05-50-00-810-831-A. AIRCRAFT IS OK FOR CONT SERVICE. NO ODOR PRESENT AT THIS TIME.

Part: BLEED AIR SYS — CONTAMINATED (APU) · airframe 60,248 hrs · 21,459 cycles

FLT#1033, MCO-SJU. 'ON DEPARTURE OUT OF MCO HAD DIRTY SOCK SMELL DISSIPATED DURING FLIGHT. ON DESCENT SMELL RETURNED. ON BLOCK IN W/ APU SMELL PERSISTED AND WAS MORE PREVALENT THE FURTHER AFT YOU MOVE INTO THE CABIN; C/W INFO NOTICE 2017-T015 SECTION B-2. IDENTIFIED ODOR TO APU BLEED. DECONTAMINATION LEVEL A,B WAS PERFORMED PER AMM 49-00-00-200-811A. ACFT OK FOR SERVICE.'

Part: MANIFOLD — FAILED (HYD SYSTEM) · airframe 59,740 hrs · 21,264 cycles

FLT#869, JFK-PUJ. (AIRCRAFT DECLARED AN EMERGENCY AND DIVERTED TO SJU).' HYD Y RSVR LO LVL , LOST FLUID IN FLIGHT; FOUND TO BE LEAKING FROM HP MANIFOLD OF THE YELLOW HYD SYSTEM, REMOVED AND REPLACED YELLOW HYD SYSTEM HP MANIFOLD IAW AMM 29-13-14, OPS CHECK OK LEAK CHECK OK, SERVICED YELLOW HYD SYSTEM REF AMM 12-12-29. A/C OK FOR SVC.'

Part: UNKNOWN — ODOR (CABIN) · airframe 59,284 hrs · 21,079 cycles

FLT#1302, PHX-BOS. 'INFLIGHT REPORTED ODOR IN CRUISE. STRONGEST IN AFT GALLEY WHILE IN FLIGHT. ODOR REPORT FORM COMPLETED; REMOVED AND INSTALLED RECIRCULATION FILTERS IAW AMM 21-21-41. OPS NORMAL COMPLIED WITH INFORMATION NOTICE 2017-T015J SECTION A, ISOLATED FAULT TO TYPE 10 (A),1,C PER TSM 05-50-00-810-085D. AIRCRAFT IS OK FOR SERVICE. ALSO CHECKED A/C HISTORY FOR FOR LAST 30 DAYS, WITH NO HISTORY.'

Part: FILTER — ODOR (100HM) · airframe 58,132 hrs · 20,660 cycles

FLT#503, JFK-SJU. 'FA'S COMPLINED ABOUT DIRTY SOCKS ODOR ON DESCENT AND TAXI IN THE CABIN FAINT ODOR IN COCKPIT; COMPLIEDWITH INF.NOTICE 2017-15,SECTION B2 DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 21-00-00-615-803 A. REMOVED AND REPLACED OZONE FILTERS IAW AMM 21-51-41. REMOVED AND REPLACED HEPA FILTERS IAW AMM 21-21-41.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,625 hrs · 20,461 cycles

DURING HEAVY MAINTENANCE: FWD CABIN FLOOR SUPPORT Y-254 HAS CORROSION BTW FR16/FR20; REMOVED AND REPLACED FLOOR BEAM SUPPORT Y-254 AT FWD CABIN AT FR 12 - FR 24 IAW A320 SRM 51-42-11. (CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 57,625 hrs · 20,461 cycles

DURING HEAVY MAINTENANCE: FWD CABIN FLOOR SUPPORT Y254 HAS CORROSION FR 16; REMOVED AND REPLACED FLOOR SUPPORT RAIL AT FWD CABIN Y254. REMOVED AND REPLACED FLOOR SUPPORT RAILMAT FWD CABIN 7254. (CONSIDERED AS A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,173 hrs · 20,302 cycles

FLT#85, BUF-MCO. 'FUMES SMELT BY ENTIRE CREW. F/O SMELLED FUMES IN DECENT. ( APU SYSTEM ); FOUND APU OIL SCAVENGE FILTER BOWL LEAKING. REMOVED AND REPLACED APU OIL SCAVENGE FILTER BOWL O-RING PER AMM 49-91-45. LEAKS CHECKS GOOD. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,233 hrs · 19,936 cycles

FLT#1867, HPN-PBI. '"DIRTY SOCK SMELL" VERY STRONG ON DESCENT APU WAS OFF; COMPLIED WITH INFO NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, (A), 1, C PER TSM 05-50-00-810-085-B, D. A/C IS OK FOR SERVICE. NO DEFECTS OR ODOR PRESENT.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,199 hrs · 19,924 cycles

FLT#1691, JFK-LIR. (AIRCRAFT DIVERTED TO FLL) 'MEL 36-11-02-B APPLIED. THE VALVE WAS CLOSED BY MX. DURING THE FLIGHT HP VLV SHOWS OPEN. IP VLV SHOWS CLOSED. NO2 ENG BLEED AND NO APCK #2 AIR. X-BLEED SELECTED OPEN. LOW PACK FLOW. DESCENT TO FL 300. MEL 36-11-01-A ACTIONED PER MX/DISP; INSP ENG2 HP BLEED VLV FOR INDICATION & LEAK CHECK'S. NO LEAKS WERE NOTED. FOUND INDICATION INTERMITTENT. FOUND CONN/BACKSHELL LOOSE. RE-SECURED CONN/BACKHELL. PERFORMED ENG2 IDLE RUN. ENG2 HP BLEED VLV FUNCTIONAL CHK NORMAL. PER TSM 36-11-00-810-810-A AND AMM 71-00-00.'

Part: ACTUATOR — FAILED · airframe 55,588 hrs · 19,681 cycles

FLT#236, STI-JFK. (AIRCRAFT DIVERTED TO SDQ) 'ENGINE 1 EGT EXCEEDED ON TAKEOFF (TOGA) (630 C) THAN ON CLIMB (605 C). FUEL FLOW +800; REMOVED AND REPLACED ENG 1 LPC BLEED MASTER ACTUATOR IAW A320 AMM 75-31-42. THE LEAK CHECK IS OK AT THIS TIME. PERFORMED A HIGH POWER RUN IAW A320 AMM 71-00-00-710-013, PASSED. NO FAULTS AT THIS TIME. A/C OK FOR CONT SERVICE.

Part: BLEED VALVE — FAILED (NR 1 ENGINE) · airframe 55,536 hrs · 19,663 cycles

FLT#1858, AUA-SJU. ' IN CLIMB TO FL33 IN DOING SYSTEM SCAN. WE NOTICED #1 & #2 HP VALVES OPEN NO ECAM. INCREASE POWER BOTH STAYED OPEN DECREASE POWER BOTH STILL OPEN PSI #1 24 PSI #2 44 PSI TEMP 195 TEMP 205; FOUND HPV ON ENG #1 ELECTRICAL CONNECTOR CROSSTHREADED. REMOVED AND REPLACED HPV ON ENG 1 PER AMM 36-11-51. OPS AND LEAK CHECK OK PER AMM 71-00-00-710-043. ON ENG #2 FOUND ELECTRICAL CONNECTOR DAMAGE. REMOVED AND REPLACED ELECTRICAL CONNECTOR PER ESPM 20-44-11. OPS CHECK OK PER AMM 71-00-00-710-043.'

Part: NONE — NONE · airframe 54,851 hrs · 19,384 cycles

FLT#1348, SJU-DCA. 'EMERGENCY EXIT LIGHTS CAME ON DURING FLIGHT WITH SWITCH IN "ARM" POSITION; REMOVED AND REPLACED EMER LIGHT CONTROL SWITCH ON / OFF ALL GOOD. ACCOMPLISHED SATISFACTORY EMER LIGHT CHECK OUT AMM 33 51 00 810 881 A.'

Part: NONE — NONE · airframe 54,453 hrs · 19,227 cycles

FLT#471, LGA-FLL. 'L1 DOOR R/H SIDE LOWER EMERGENCY EXIT LT INOP; REMOVED AND REPLACED EMERGENCY EXIT LIGHT I/A/W 33-51-16 OPS CHECK GOOD.'

Part: NONE — NONE · airframe 52,537 hrs · 18,520 cycles

FLT#1696, SJO-MCO. 'DESCENDING THROUGH 13000FT DIRTY SOCK ODOR . ODOR WAS PRESENT IN COCKPIT AND CABIN. SMELL WENT AWAY DESCENDING THROUGH 10,OOO. APU OFF PACKS ON; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A (A) ISOLATED FAULT TO TYPE 10 (A) 1,C PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-085-D. AIRCRAFT IS OK FOR SERVICE.'

Part: A/C PACK — ODOR (NR 2) · airframe 50,614 hrs · 17,822 cycles

FLT# 871, JFK-SLC. DIRTY SOCK FUMES FROM 19.0 - 11.5 ON DESCENT ( PACKS ) ; IAW INFO NOTED 20-17-T015G FOUND #2 PACK OF FAULT ITEM PLACED ON MEL 21-52-01 COND C CAT C MX-4 UPDATED MCC MARIO NOTIFIED (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: FAN — FAILED (BLOWER)

FLT 959, BDL-CHS. LOUD POP UNDER FLIGHT DECK FLOOR SMOKE FUMES IN FLIGHT DECK RAM FMR QRH FOR SMOKE SMELL AND SMOKE DISSAPATED ECAM FOR VENT BLOWER & VENT EXTRACT FAN WHEN PUT TO OVRD SMELL AND SMOKE RETURNED PLACED BOTH SWITCHES BACK IN FAULT MODE SMOKE SMELL CEASED LANDED. PERFORMED CHAPTER 5 SMOKE INSPECTION PER AMM 05-50-00-810-831-A FOUND AEVC BLOWER AS CAUSE SEE MDDR 442064 AC OK FOR SERVICE.AVEC BLOWER FAIL ( BLOWER FAN - NO AVNCS SYS FAULT ECAM CAUTION ) VERY LOUD HUMMING SOUND ON FLIGHT DECK GETTING INCREASINGLY LOUDER AS FLIGHT PROGRESSES SOUNDS LIKE COMING FROM BELOW FLIGHT DECK FLOOR AND AS IF IT COMING AND POWER CHANGES DO NOT AFFECT IT NO ASSOCIATED VIBRATION JUST A LOUD HUM ; REMOVED AND REPLACED BLOWER FAN 20HQ- AS PER AMM 21-26-51. OPS CK NORMAL- MDDR CLEARED.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 48,902 hrs · 17,237 cycles

FLT 1973, EWR - TPA. EMERGENCY LIGHT TEST FAILED 11WL BATTERY FAULT. REMOVED & REPLACED EPSU BATTERY AT FIN 11WL, PER AMM 33-51-38.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 48,902 hrs · 17,237 cycles

FLT 1973, EWR - TPA. EMERGENCY LIGHT TEST FAILED 10WL BATTERY FAULT. REMOVED & REPLACED EPSU BATTERY AT FIN 10WL, PER AMM 33-51-38.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 41,411 hrs · 14,351 cycles

EMERGENCY LIGHT FAILED TO TEST. R & R EMERGENCY LIGHT BATTERIES AT 10WL,11WL,12WL, AND 13WL IAW AMM 33-51-38. TESTED OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 41,411 hrs · 14,351 cycles

EMERGENCY LIGHT FAILED TO TEST. R & R EMERGENCY LIGHT BATTERIES AT 10WL,11WL,12WL, AND 13WL IAW AMM 33-51-38. TESTED OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 41,411 hrs · 14,351 cycles

EMERGENCY LIGHT FAILED TO TEST. R & R EMERGENCY LIGHT BATTERIES AT 10WL,11WL,12WL, AND 13WL IAW AMM 33-51-38. TESTED OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 41,411 hrs · 14,351 cycles

EMERGENCY LIGHT FAILED TO TEST. R & R EMERGENCY LIGHT BATTERIES AT 10WL,11WL,12WL, AND 13WL IAW AMM 33-51-38. TESTED OK.

Part: TERMINAL — DAMAGED (EMERGENCY LIGHT) · airframe 40,590 hrs · 14,028 cycles

MID CABIN OVERHEAD EXIT LIGHT NOT WORKING. REPAIRED THE EMERGENCY LIGHT TERMINAL ENDS IAW ESPM 20-48-10. OP CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-70) · corrosion level 2 · airframe 40,446 hrs · 13,968 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, + Y765, FRAMES 66 TO 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 40,446 hrs · 13,968 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, -Y1292, FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53110900.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 40,446 hrs · 13,968 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, -Y1162, FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11, DWG D53470150, AND DWG 53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 40,446 hrs · 13,968 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT +Y 1292, FRAMES 64 TO 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472831.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,230 hrs · 13,146 cycles

MILD ODOR NOTED BY FLIGHT CREW AND PASSENGERS IN THE AFT CABIN DURING DESCENT . ODOR DETECTED BY FLIGHT CREW WHEN IDLE SELECTED AT TOP OF DESCENT (35000) AND AGAIN WHEN IDLE SELECTED DESCENDING THROUGH 10,000. THE APU WAS NOT OPERATING AT THE TIME. ACCOMPLISHED ECS DECONTAMINATION PROCEDURE IAW AMM 21-00-00-615-004-A, AND AMM 21-00-00-615-002-A. NO ODOR OR CONTAMINATION FOUND. CLEANED PACKS 1 AND 2 PLUMBING IAW AMM. ALL OPS CHECKS AND LEAK CHECKS GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,228 hrs · 13,145 cycles

DIRTY SOCK ODOR AT VARIOUS TIMES FOR THE DURATION OF FLIGHT. COMPLIED WITH INFO NOTICE 2017-T015A , SEC B, TABLE 1. ACFT OK FOR SERVICE. ACCOMPLISHED ECS DECONTAMINATION. BORESCOPE ACCOMPLISHED. NO FINDINGS. REPLACED OZONE, RECIRCIRCULATION & AVIONICS FILTERS. AFTER ALL CORECTIONS, NO ODOR NOTED IAW 21-26-43, 21-21-41, 21-51-41.

Part: SERVO VALVE — FAILED (RT ELEVATOR) · airframe 36,335 hrs · 12,448 cycles

FLT 368, PUJ-JFK, DIVERTED TO SJU. EMERGENCY DECLARED. CLIMBING THROUGH 310 AT MACH .76 VERY STRONG VIBRATIONS WERE FELT THROUGHOUT THE AIRCRAFT. SLOWED DOWN TO MACH .72 AND VIBRATION DISAPPEARED. ACCOMPLISHED TSM 05-50-00-810-801 (VIBES). R & R RT B ELEV SERVO (34CE4), R & R EYE END ASSY, R & R SERVO VALVE IAW AMM 27-34-51. OPS CHECK PERFORMED. OPS CHECK PASSED. NO LEAKS NOTED.

Part: FITTING — FAILED (RT ELEVATOR) · airframe 36,335 hrs · 12,448 cycles

FLT 368, PUJ-JFK, DIVERTED TO SJU. EMERGENCY DECLARED. CLIMBING THROUGH 310 AT MACH .76 VERY STRONG VIBRATIONS WERE FELT THROUGHOUT THE AIRCRAFT. SLOWED DOWN TO MACH .72 AND VIBRATION DISAPPEARED. ACCOMPLISHED TSM 05-50-00-810-801 (VIBES). R & R RT B ELEV SERVO (34CE4), R & R EYE END ASSY, R & R SERVO VALVE IAW AMM 27-34-51. OPS CHECK PERFORMED. OPS CHECK PASSED. NO LEAKS NOTED.

Part: CONTROL SERVO — FAILED (RT ELEVATOR) · airframe 36,335 hrs · 12,448 cycles

FLT 368, PUJ-JFK, DIVERTED TO SJU. EMERGENCY DECLARED. CLIMBING THROUGH 310 AT MACH .76 VERY STRONG VIBRATIONS WERE FELT THROUGHOUT THE AIRCRAFT. SLOWED DOWN TO MACH .72 AND VIBRATION DISAPPEARED ; ACCOMPLISHED TSM 05-50-00-810-801 (VIBES). R & R RT B ELEV SERVO (34CE4), R & R EYE END ASSY, R & R SERVO VALVE IAW AMM 27-34-51. OPS CHECK PERFORMED. OPS CHECK PASSED. NO LEAKS NOTED.

Part: CONTROL UNIT — FAILED (CABIN) · airframe 19,137 hrs · 6,616 cycles

FLT 148 PBI-JFK, IN FLIGHT CREW REPORTED BURNING SMELL. CONDUCTED FUME / BURNING TEST OF ELECTRICAL AND LIVE TV SYSTEMS. NO BURNING SMELL DETECTED IAW 24-00-00-810-823A AND 23-39-00-810-801. PERFORMED ODOR SYSTEM INTEGRITY CHECK FOUND CAMERA CONTROL UNIT NR 4 INOP. REMOVED AND REPLACED CCU IAW LTV MM 23-39-00. OPS CHECK OK.

Part: RELEASE CABLE — DEFECTIVE (OVERWING EXIT) · airframe 17,360 hrs · 6,050 cycles

FLT 6405 JFK-LCQ DURING HEAVY MAINTENANCE, RIGHT OVERWING EXIT CABLE FAILS TEST. RIGHT EMERGENCY SLIDE RELEASE CABLE REPLACED, RIGGED & OPS CHECKED ON CARD A320-53-1227-02. REF N/R 29840.

Part: RELEASE CABLE — DEFECTIVE (OVERWING EXIT) · airframe 17,360 hrs · 6,050 cycles

FLT JFK-LCQ, DURING HEAVY MAINTENANCE, THE LEFT OVERWING EXIT CABLE FAILS TEST. LEFT EMERGENCY SLIDE CABLE RELEASE, RIGGED & OPS CHECKED ON CARD A320-53-1227-01. REF NR 29841.

Part: ELECTRICAL BOX — FAILED (TV SYSTEM) · airframe 5,406 hrs · 1,967 cycles

FLT 1784, PLASTIC/ELECTRICAL ODOR IN THE VICINITY OF ROW 21, TURNED OFF TV/ASSC POWER BUT ODOR REMAINS. MET WITH BOTH CABIN CREW MEMBERS CONFIRMED PRESENCE OF ODOR AROUND ROW 19 RT AND ALL CONNECTORS ROW 19 RT TO 25 RT. FOUND DAMAGE PINS AT ROW 20 RT XEB. REMOVED AND REPLACED XEB AND SEAT TO SEAT CABLES AT 20 RT. OPS CHECK OK. NO OTHER FAULTS NOTED IAW 44-20-17. OPS CHECK OK.