N709JB

Part: UNKNOWN — ODOR (CABIN) · airframe 64,613 hrs · 22,800 cycles

FLT 2219 EWR-AUA. "FUME EVENT ON APPROACH & LANDING FROM ROW 15-25, STRONG RUBBER ODOR SEVERAL PEOPLE EXPERIENCED NASEA.; C/W INFO NOTES 2017-TO15L. DISICON RE VOLT OF ORDOR TO ELECTRICALS MOST PROBABLE CAUSE CRYPRES TSM TASK 05-50-00-810-085 FOLLOW NO ABNORMALITY END AC OK TO CVONT SVC NO 30D HISTORY MCC NOTIFIED."

Part: UNKNOWN — ODOR (CABIN) · airframe 63,714 hrs · 22,411 cycles

FLT # 861, BOS-SJU. ODOR EVENT ON DESCENT WITH MILD ODOR, DIRSTY SOCKS / MUSKY-ISLOATED PALK ONE OFF, AFTER 5 MIN ODOR DISSIPATED WITH PACK ONE OFF; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2 SEE LOG PG 4349298-2 FOR ENGINE 1 BLEED DEFERAL. DECONTAMINATIONB LEVEL A ACCOMPLISHED PER TSM 21-00-00-615-802

Part: ROD END — DAMAGED (ZONE 800) · airframe 61,715 hrs · 21,622 cycles

FLT#240, NAS-MCO. 'L2 DOOR ARMING/DISARMING LEVER HAS VERY LITTLE TENSION AND DROPS DOWN AUTOMATICALLY WHEN IN THE UP POSITION; REMOVED AND REPLACED L2 DOOR ARMING CABLE EYE ROD END BOTTOM DOOR IAW AMM 52-13-22. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THE MOMENT.'

Part: E LIGHT SYS — FAILED (13WL-BATT) · airframe 61,612 hrs · 21,587 cycles

FLT#40, MDE-FLL. 'DURING WEEKLY EMER LIGHT TEST BITE CHECK FOUND " ESCAPE SLIDE LT /EPSU (10WL) FWD L" FAULT ( ESCAPE SLIDE LIGHTING ); REMOVED AND REPLACED LEFT ESCAPE SLIDE BATTERY LIGHT IAW AMM 33-51-38. OPS CHECK GOOD. MCC NOTIFIED. MX-4 UPDATED. PLACARD RMVD. MDDR CLEARED.'

Part: UNKNOWN — ODOR (CABIN) · airframe 60,697 hrs · 21,233 cycles

FLT#1733, DCA-PBI. 'CABIN CREW REPORTED UNUSUAL OREGANO ODOR IN AFT CABIN STARTING AT ROW 24; C/W INFO NOTICE 2017-T015K PERFORMED TSM TASK 05-50-80-810-831-A. FOUND NO OIL IN APU COMPARTMENT PERFORMED DECONTAMINATION OF PACK 1 & PACK 2 NO ODOR PRESNET. REPLACED HEPA FILTERS W/REF TO A320 AMM 22-21-41. A/C OK FOR SVC. NO FURTHER DEFECTS NOTED.'

Part: YAW DAMPER — FAULTED · airframe 59,933 hrs · 20,967 cycles

FLT#1265, MCO-STI. (ACFT DIVERTED TO PLS) ACFT AGGRESSIVELY WITH INCREASING FREQUENCY YAW TO THE LT IN CALM AIR DURING CRUISE & DESCENT WITH BOTH AUTOPILOTS AS WELL AS AUTO PILOT OFF. YAW ESTIMATED 5 DEGREES WITH A FREQUENCY OF EVERY 10- 15 SECONDS. HYDS PAGE NORMAL RANGE. FLT CONTROL PAGE SHOWED RUDDER YAW TO LT AS WELL TRIM SHOWED L 0.4 THROUGHOUT ALL YAWING DURING TO ABNORMALITY. REDUCING SPEED HELPED DECREASE AGGRESSIVENESS OF YAW BUT STILL CONTINUED, REF TSI 554632. R & R OF YAW DAMPER #1 (13C1). R & R YAW DAMPER #1 IAW AMM 27-26-51. OPS LEAK AND RIGGING CHECK GOOD. FOUND NO DEFLECTION COMING FROM RUDDER. RUDDER ALIGNED TO TRUE CENTER. NO FURTHER ACTION REQ. A/C OKAY FOR SVC.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE OF TOP SKIN OVERHANG ON RIB 7 ON RH WING; ACCOMPLISHED REPAIR IAW AEROMAN EA 57-9004-24 REV 0 AND AIRBUS RDAF 81405159/020/202#A REF AEROMAN NR 2024-314659.

Part: FRAME — CRACKED (ZONE 200) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION IN FRAME SEGMENT 1 AT DOOR 833; REF: ARM W/O 2024-178/1 NR 2024-314583. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 833 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 SRM 51-42-11 AND 320 SRM 51-72-11.

Part: STRINGER — CORRODED (ZONE 100) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CORROSION STG 37L FR 60 +19 INCHES TO STG 37L FR 62 +20 INCHES. FOUND OUT OF LIMITS; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00054)(RESOLVED ON W/O: 1307953 TASKCARD: NR-00054 ) ACCOMPLISHED REPAIR IAW EC 24-790-01. REF AEROMAN NR 2024-314900.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CORROSION LOWER SILL EXISTING REPAIR LOCATED AT STR 23L FR 68 AFT GALLEY AREA; PERFORMED REPAIR LOCATED ON LOWER SILL AT STR 23L AND BETWEEN FR 67 TO FR 68 AFT GALLEY AREA IAW A320 SRM 53-41-14-300-001 FIGURE 001(SHEET) 3. REF AEROMAN NR 2024-314791 (CONSIDERED A MAJOR REPAIR)

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE ON TOP SKIN OVERHANG ON RIB 8 ON RH WING; ACCOMPLISHED REPAIR IAW AEROMAN EA 57-9004 REV 0. AND AIRBUS RDAF 81405159/020/202#A. REF AEROMAN NR 2024-314659. (CONSIDERED A MAJOR REPAIR)

Part: SKIN — CORRODED (ZONE 600) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE OF TOP SKIN OVERHANG LOCATED ON RIB 14 ON RH WING;(RESOLVED ON W/O: 1307953 TASKCARD: NR-00047) REF AEROMAN WO 2024 178/1 NR 2024-3114797 REMOVED CORROSION LOC. ON RIB 14 PLUS 15 INCHES LOWER SURFACE OF TOP SKIN OVERHANG AREA RH WING I.A.W. A320 SRM 51-73-00 AND A320 SRM 51-74-00, EVALUATED REWORKED AREA I.A.W. A320 SRM 57-21-11-283-007 STEP 2.A ITEM 1 REFER FIGURE 003 SHEET 1 WITH DEPTH PERCENT 25.38% AND FOUND WITHIN LIMITS. AS A RESULT, REPAIR CATEGORY IS B: INSPECTION INSTRUCTIONS TASK 57-21-11-205-006: INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLIGHT FC=11,000 /FH=19,000HRS, SUB SEQUENT INSPECTION AT INTERVALS OF FC=11,000 /FH=19000, METHOD OF INSPECTION DETAIL VISUAL INSPECTION I.A.W. A320 NTM 51-90-00.

Part: FRAME — CRACKED (ZONE 200) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / FR68 RHS / DOOR STOP FITTING #1 / LOWER INBOARD HOLE / CRACK - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9007-24 REV. 0 (COVER + PART 1) /2/ AIRBUS RDAF 81404539/004/2024#A/3/ AIRBUS DOSSIER 81404539 /4/ A320 SRM 53-41-12-300-008 DURING THE CURRENT (06/2024) H3 CHECK AT SAL FOR A/C N709JB (MSN03488), WHILE ACCOMPLISHING SB A320-53-1288, A CRACK WAS FOUND ON THE AFT FUSELAGE FR68 RHS DOOR STOP FITTING #1 LOWER INBOARD HOLE. . SEE REF /1/ AEROMAN EA FOR DETAILS. THE DAMAGE WAS EVALUATED AGAINST REF /4/ SRM REPAIR AND FOUND OUT OF SCOPE DUE TO THE DISTANCE BETWEEN THE HOLE EDGE AND FILLET RADIUS BEING LESS THAN 0.177 INCHES. AEROMAN REPORTED TO AIRBUS VIA REF /3/ DOSSIER AND AIRBUS PROVIDED THE REF /2/ RDAF APPROVING THE USE OF REF /4/ SRM WITH DEVIATIONS, TO REPAIR THIS DAMAGE. THE REPAIR CONSISTED OF TRIMMING THE FRAME HORIZONTAL STIFFENER AND INSTALLATION OF A REINFORCE FITTING (MACHINED REPAIR PART) ALONG WITH A BUSHING REPAIR AND NDT INSPECTIONS. THE REF /2/ RDAF APPROVES THESE REPAIR INSTRUCTIONS AS PERMANENT WITH POST REPAIR INSTRUCTIONS REQUIRED NOTE: SBS A320-53-1288 AND A320-53-1491 ARE AFFECTED BY THIS REPAIR AND ARE NO LONGER APPLICABLE AT THE REPAIRED LOCATION. EC A24-773-01 ACCOMPLISHES THE PERMANENT REPAIR AS PER REF /1/ EA COMPLIES WITH REF /2/ RDAF WITHOUT DEVIATION. THIS PERMANENT, CATEGORY B, REPAIR IS APPROVED PER REF /2/ RDAF AND IS CLASSIFIED AS MAJOR. (EC: A27-773-01)

Part: SKIN — CRACKED (ZONE 200) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: FUSELAGE / AFT FUSELAGE / FR54-64 & STGR 37L-38L / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9012-24 COVER AND P1-P3 /2/ AIRBUS RDAF 80524263/050/2024 ISSUE A /3/ AIRBUS TD/80524263/054/2024#A /4/ AIRBUS RDAF 80524263/038/2021 ISSUE A DESCRIPTION: DURING THE CURRENT (6/2024) H3 CHECK FOR A/C N709JB (MSN 03488) AT SAL, WHILE ACCOMPLISHING MPD ZL-161-02 INSPECTION, CORROSION WAS FOUND ON THE AFT FUSELAGE SKIN BETWEEN FR60-63 & STGR 37L. SEE REF /1/ EA FOR DETAILS. THE DAMAGE AREAS ARE MEASURED AS FOLLOWS: DAMAGE 1: FR60+19 INCHES & STGR37L - L=2.903 INCHES W=0.498 INCHES DAMAGE 2: FR61+20 INCHES & STGR37L – L=1.569 INCHES W=0.351 INCHES DAMAGE 3: FR62+20 INCHES & STGR37L – L=0.937 INCHES W=0.437 INCHES NOTE: IN THE PAST, CORROSION DAMAGES WERE FOUND ON REAR FUSELAGE STRINGER 37LH BETWEEN FR60-61 AND STRINGER 38LH BETWEEN FR54-60 AT FC: 14627 AND FH: 42529. AND ADDITIONAL DAMAGES WERE FOUND ON STRINGER 38LH BETWEEN FR56-60 AT FC: 17586 AND FH: 50858. REPAIR WAS DONE AS PER REF /4/ RDAF AT THAT TIME.THE DAMAGE WAS REPORTED TO AIRBUS FOR REPAIR DISPOSITION. AIRBUS PROVIDED REF /3/ TD WITH INSTRUCTIONS TO REMOVE THE FASTENERS, PERFORM NDT INSPECTIONS, PERFORM STRINGER SPLICE REPAIR PER DWG R534-70620. NOTE: THE REF /2/ RDAF SUPERSEDES REF /4/ RDAF SO IT ALSO COVERS THE PREVIOUSLY REPAIRED AREAS BETWEEN FR54-54 & STGR 37L & 38L. EC A24-790-01 IS ISSUED TO ACCOMPLISH PERMANENT REPAIR IAW REF /1/ EA AND COMPLIES WITH REF /2/ RDAF WITHOUT DEVIATION. SUBSTANTIATION: THIS REPAIR IS APPROVED PER REF /2/ RDAF AND IS CLASSIFIED AS MAJOR. (E/C: A24-790-01)

Part: FRAME — CRACKED (ZONE 200) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION IN FRAME SEGMENT 1 AT DOOR 834; REF: ARM W/O 2024-178/1 NR 2024-314582. ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 834 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 SRM 51-42-11 AND 320 SRM 51-72-11.

Part: FRAME — CRACKED (ZONE 200) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION IN FRAME SEGMENTS 1 AT DOOR 844; REF: ARM W/O 2024-178/1 NR 2024-314584 ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 844 IAW EC# A320-52-1144 AND REMOVED AND REPLACED SEGMENTS IAW A320 SRM 51-42-11 AND 320 SRM 51-72-11.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN FRAME SEGMENTS 1 AT OVERWING EMERGENCY EXIT DOOR 843; REF: ARM W/O 2024-178/1 N/R 2024-314581 ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 843 IAW EC# A320-52-1144 AND R&R SEGMENTS IAW A320 SRM 51-42-11 AND 320 SRM 51-72-11. TECH 8619800.

Part: HINGE FITTING — CORRODED (ZONE 300) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 5 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00035) REMOVED AND REPLACED HINGE FITTING #5 LOCATED ON VERTICAL STABILIZER IAW A320 SRM 51-72-11-911-001 AND DRAWING #D 5571052 ISSUE E. REF AEROMAN NR 2024-314970.

Part: HINGE FITTING — CORRODED (ZONE 300) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CORROSION FOUND ON BORE HINGE FITTING 4 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00036) REMOVED AND REPLACED HINGE FITTING #4 ON VERTICAL STABILIZER IAW A320 SRM 51-72-11-911-001 AND DRAWING #D 55371052 ISSUE E. REF AEROMAN NR 2024-314969.

Part: FRAME — CRACKED (ZONE 200) · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE AT AFT GALLEY AREAA, DOOR STOP 1 INBOARD LOWER HOLE. CRACK INDICATION LOCATED A 5 OCLOCK VIEW LOOKING FROM FWD. DEPTH IS 0.067 INCHES; (RESOLVED ON W/O: 1307953 TASKCARD: NR-00053) ACCOMPLISHED REPAIR IAW EC A24-773-01. REFAEROMAN NR 2024-314688.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,842 hrs · 20,938 cycles

DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LOCATED BTW FRAME 60 AND FRAME 62 IN BULK CARGO COMPARTMENT; PERFORMED REPAIR ON LOWER SILL BULK CARGO COMPARTMENT LOACTED BTW FR 60 PLUS 19 IN IAW A320 SRM 53-41-49-300-003. THIS REPAIR IS CATEGORY B AT DEFINED INTERVALS REFER TO INSPECTION THRESHOLD FROM TOME OF ADL/REPAIR EMBODIMENT FC 60000, FH 120000, SUBSEQU. (CONSIDERED A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,762 hrs · 20,140 cycles

FLT#894, STI-EWR. 'OIL OR "DIRTY SOCK" ODOR NOTICED AFTER TAKEOFF CLIMBING THROUGH 10,000'. ISOLATED TO PACK 1 AS THE PRIMARY CAUSE. NO ODOR WHEN RUNNING ON PACKS ALONE; REFER TO LP: 3680351, ITEM 1 (REPLACED SEALING RING ON LP TURBINE SHAFT BLIND CAP AND INSTALLED BLIND CAP AND NO.5 BEARING COMPARTMENT COVER IAW AMM 72-51-41 REFER LOGPAGE 3680351, ITEM 2 (PERFORMED IDLE LEAK CHECK REFER AMM 71-00-00. OPS CHECK GOOD OK FOR CONT SVC) FOR IDLE LEAK CHECK): A/C OKAY FOR SERVICE. NO DEFECTS NOTED AT THIS TIME.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,327 hrs · 19,960 cycles

FLT#1510, PUJ-FLL. 'APU OFF- STRONG ACRID / BURNING OIL/DIRTY SOCK TOXIC FUMES THROUGHOUT AIRCRAFT WITH STRONGEST SMELL IN COCPIT. DESCENT PHASE BELOW 10,000' FROM PACKS, AND PRESENT UNTIL LANDING. USING COCKPIT/CABIN ODOR RECOGNITION AND ISOLATION CHECKLIST- UNABLE TO ISOLATE SOURCE TO PACK 1 OR PACK 2; FOUND APU OIL COOLING FAN TO BE THE SOURCE OF ODOR CONTAMINATION, REF LOG PAGE 3688568-1 FOR APU DEFERRAL. "COMPLIED WITH INFO NOTICE 2017-T015J, SECTION B2. DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. A/C IS OK FOR SERVICE. REMOVED AND REPLACED RECIRC FILTERS IAW AMM: 21-21-41 AS PRECAUTION.'

Part: BATTERY — FAILED (10WL-BATT) · airframe 56,861 hrs · 19,797 cycles

FLT#1302, PHX-BOS. 'AFT ISLE EMERGENCY EXIT LIGHT INOP; REPLACED PSU BATTERY PACK IAW AMM 33-51-38. OPS CHECK GOOD.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,600 hrs · 19,701 cycles

FLT#1252, CUN-JFK. 'DURING DESCENT AT 10,000 FT WITH ENGINE BLEED SOURCE FLT CREW ONLY DETECTED A LEVEL 1 TRANSIENT (ELECTRIC PLASTIC) BURNS TYPE ODOR, LASTED ABOUT 4 MINS. ON THE GROUND WITH A CHANGEOVER TO APU BLEED SOURCE A SHORT LEVEL 1 TYPE (DIRTY SOCK) SMELL ODOR LASTED ABOUT 3 MINS. INFLIGHT CREW AND CUSTOMERS SAID NOTHING WAS OBSERVED. ON THE FLIGHT TO CUN NOTHING WAS DETECTED EVEN THE MOISTURE LATCH ENVIRONMENT. THE ONLY DIFFERENCE ON DESCENT WAS LANDING IN CUN, CABIN TEMP KNOBS WERE SLOWLY PLACED IN FULL COLD TO 30 C+ TEMPS. AT JFK CABIN TEMP ZACS WERE AS FOLLOWED. FLIGHT DECK 11 'O'CLOCK, FWD /AFT CABIN 9'/9 'O'CLOCK FOR BOTH. ( APU SYSTEM ). (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,454 hrs · 19,648 cycles

FLT#1252, RSW-HPN. 'DURING DESCENT & APPROACH MILD TO MODERATE SMELLY SOCK ODOR FUME EVIDENT IN MID CABIN, MILD OROD IN COCKPIT. PACK 1 SELECTED OFF SEEMED TO HELP BUT NOT ELIMINATE IT; PERFORMED INFO NOTICE 2017-T015J SECTION B2, DECONTAMINATION LVL 2 WAS ACCOMPLISHED PER TSM 05-50-00-810-831-0-A, REPLACED ALL HEPA FILTER IAW AMM 21-21-41 AND 21-51-41. NO ODORS ARE PRESENT. A/C IS OK FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,393 hrs · 19,627 cycles

FLT#505, EWR-FLL. 'FLIGHT ATTENDANT SAID THERE WAS A DIRTY SOCKS SMELL ON DESCENT AT THE END OF THE FLIGHT; PERFORMED A LEVEL A DECONTAMINATION OF THE ECS IRW A320 AMM 21-00-00-615-802-A. COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A. ISOLATED TO TYPE 1, LEVEL 1 AS PER TSM 05-50-00-810-831-A: ISOLATED OIL LEAK TO BE THE APU COOL FAN SECTION.A/C O.K TO CONT SERVICE AT THIS TIME.'

Part: UNKNOWN — UNKNOWN · airframe 56,387 hrs · 19,623 cycles

FLT #2747, LGA-SAV. "FUMES EVENT; COMPLIED WITH INFO NOTICE 2017 T015 SECA ISOLATED FAULT TO TYPE 10 A/C PER TSM 05 -50 -00 A/C OK FOR SERVICE."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,289 hrs · 19,580 cycles

FLT#1256, FLL-GYE. 'DURING DESCENT INFLIGHT CREW NOTICED A DIRTY SOCK SMELL MID CABIN. THE ODOR CONTINUED UNTIL AFTER LANDING ( PACKS ). (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 55,936 hrs · 19,443 cycles

FLT#149, JFK-GND. 'FA'S ADVISE OF ODOR EVENT ON FINAL DESCENT AT 6000 FT CHEMICAL SMELL (STRONG AND LASTED UNTIL GATE ARRIVALIN REAR CABIN ( PACKS ); REF INFO NOTICE 2017-T015J LEVEL A. INSP APU FOR LEAKS, NO DEFECT NOTED. ACCOMPLISHED APU COMPRESSOR WASH PER AMM 49-20-00. ACCOMPLISHED LEVEL A DECONTAMINATION PER TSM TSK 21-00-00-615-802A. NO ODOR WAS NOTICED. BOTH RECIR FILTERS WERE REPLACED PER AMM 21-21-41. THIS CLEARS MDDR 505947. MX-4 UPDATED. PLACARD REMOVED. MCC NOTIFIED.'

Part: NONE — NONE · airframe 55,803 hrs · 19,390 cycles

FLT#2092, MIA-JFK. 'ELECTRICAL SMELL OUT OF 5000' INTO JFK. LASTED APROX 5 MIN. 1.9 (DELTA)P; PERFORMED INSP FOR "ELEC BURNING SMELL" IAW TSM 24-00-00-810-823-A. NO DISCREPANCIES WERE FOUND. REMOVED AND REPLACED AVIONICS FILTER IAW AMM 21-26-43. AS PRECAUTIONARY PERFORMED A LEVEL A ECS DECONTAMINATION IAW AMM 21-00-00-615-802-A.'

Part: NONE — NONE · airframe 55,791 hrs · 19,385 cycles

FLT#1141, BDL-PBI. ' AFT CABIN EMERGENCY EXIT LIGHT INOP; FOUND CONNECTOR 7250VC FOR AFT CABIN EMERG LOOSE SECURED IAW 33-51-04. ALL OPS CHECK NORMAL.'

Part: NONE — NONE · airframe 55,633 hrs · 19,333 cycles

FLT#595, HPN-MCO. ' FLIGHT ATTENDANT IN AFT GALLEY STATED SHE SMELLED "HYDRAULIC FLUID" DESCENDING THROUGH 10, 000 FEET; PER INFO NOTICE 2019-T015J NO HISTORY PAST 30 DAYS. SECTION A OPS BOTH PACKS ON APU BLEED NO ODOR PRESENT. INSP APU NO OIL CONTAMINATION PRESENT. NO PACK CONTAMINATION IS VISIBLE. TYPE 10 PER TSM 05-50-00-00-810-085 AC OK FOR SERVICE.'

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,156 hrs · 19,155 cycles

FLT#225, JFK-TPA. 'EMERG LIGHT BATTERY 13WL FAILED BATTERY TEST; REMOVED AND REPLACED EMERG LIGHT BATTERY FIN 13WL IAW AMM 33-51-38.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,156 hrs · 19,155 cycles

FLT#225, JFK-TPA. EMERGENCY LIGHT BATTERY 10WL FAILED BATTERY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY FIN 10WL IAW AMM 33-51-38.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,156 hrs · 19,155 cycles

FLT#225, JFK-TPA. EMERGENCY LIGHT BATTERY FIN 11WL FAILED BATTERY TEST. REMOVED AND REPLACED EMERG LIGHT BATTERY 11WL IAW AMM 33-51-38.

Part: CHECK VALVE — FAILED (2525GM) · airframe 53,305 hrs · 18,443 cycles

FLT#163, JFK-SRQ. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO JFK). ' YELLOW HYDRAULIC SYSTEM OVERHEAT AFTER TAKEOFF; R/S REF TSM 29-13-00. REMOVED AND REPLACED CHECK VALVE Y REF AMM 29-24-21. ON OPS CHECK OF ENG #2 EDP. ENGINE-DRIVEN PUMP WORKS NORMALLY ON SELECTION OF ELECTRIC PUMP YELLOW. NO JOY. POSSIBLE YELLOW ELECTRIC PUMP DAMAGED FROM REVERSE FLOW REF TSM.'

Part: STRINGER — CORRODED (FRMS 56-57 S38L) · airframe 50,858 hrs · 17,586 cycles

DURING HEAVY MAINTENANCE, CORROSION STRINGER 38L BTW FRAME 56 AND FRAME 57 IN AFT CARGO COMPARTMENT; REF AEROMAN N/R 2021-371028, ACCOMPLISHED REPAIR ON THE AFT FUSELAGE STGR 37LH BTW FR 60-61 AND STGR 38L , BTW FR 54-60 IAW EA 53-0440-21, RDAF 80524263/038/2021# A. AND EC A21-951-01.THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR CATEGORY A AND NO RE-INSPECTION IS NECESSARY.

Part: STRINGER — CORRODED (FRM 59-60 S38L) · airframe 50,858 hrs · 17,586 cycles

DURING HEAVY MAINETNANCE, CORROSION STRINGER 38L BTW FRAME 59 AND FRAME 60 IN AFT CARGO COMPARTMENT; REF AEROMAN N/R 2021-371030, ACCOMPLISHED REPAIR ON THE AFT FUSELAGE STGR 37LH BTW FR 60-61 AND STGR 38L , BTW FR 54-60 IAW EA 53-0440-21, RDAF 80524263/038/2021# A. AND EC A21-951-01.THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR CATEGORY A AND NO RE-INSPECTION IS NECESSARY.

Part: GCU — FAILED (NR 1) · airframe 50,286 hrs · 17,398 cycles

FLT 1853, JFK-PBI. EMERGENCY DECLARED. ELEC GEN 1 OFF. ATTEMPTED TO RESET IT. WORKED FOR TWO MINUTES THEN FAILED. AFTER THAT IT WOULD NO LONGER RESET; PERFORMED TSM 24-00-00-810-819A NO FAULTS NOTED. R & R #1` GCU IAW 24-22-34. RAN ENGS 1/ 2 AT IDLE & NO FAULTS NOTED AT THIS TIME OPS CK OK AMM 71-00-00.

Part: FILTER — CONTAMINATED (RECIRCULATION) · airframe 50,234 hrs · 17,376 cycles

FLT 2292, MIA-JFK. ODOR IN COCKPIT DURING DESCENT . MUSTY DRY SMELL COMING FROM AIR VENTS . HAPPENED TWICE AT FL 230 & 13,000 WHILE ENGINES WERE GOING TO IDLE; MX ACTION CARRIED OUT PER TASK CARD A 2117101-03. DID NOT SMELL ODOR IN COCKPIT. INSPECTED PACK DUCTS AS OUTLINED IN TSAK CARD A2117101-03. NO OIL FOUND. REPLACED R/H RECIRC FILTER PRECAUTIONARY . NOTE : ON COCKPIT ODOR REPORT PILOT INBOUND ITEM COMPLAINT OF DRY SMELL NOT OIL ODOR.

Part: SLIDE — MALFUNCTIONED (L2 DOOR) · airframe 49,002 hrs · 16,925 cycles

FLT 1052, SJU-TPA. OBSERVED WHEN CABIN ALT WAS ABOVE 7000FT L2 DOOR NOT ARMED WHEN HANDLE IS IN ARMED POSITION. CONTACTED MX CONTR INFLIGHT AT THE REQUEST OF MCC. REMOVED AND REPLACED L2 DOOR ESCAPE SLIDE RAFT, IAW AMM 25-62-44. OPERATIONS CHECK GOOD.

Part: DEU — FAILED (EMERGENCY LIGHTS) · airframe 47,365 hrs · 16,353 cycles

FLT 514, ALL AFT GALLEY EMERGENCY SIGNS & LIGHTS FAILED TO ILLUMINATE ON POWER FAILURE. R & R DEU B IAW 23-73-47. EMERGENCY LIGHTS IN AFT GALLEY OPS CHECKED GOOD

Part: POWER SUPPLY — NO TEST (ESCAPE SLIDE) · airframe 47,365 hrs · 16,353 cycles

FLT 514, AFT LEFT ESCAPE SLIDE CAUSING ESPU 13WL FAILED ON ESPU SYSTEM TEST. R & R AFT LEFT ESCAPE SLIDE IAW AMM 25-62-44. OPS CHECKED GOOD.

Part: POWER SUPPLY — NO TEST (ESCAPE SLIDE) · airframe 47,365 hrs · 16,353 cycles

FLT 514, AFT RIGHT ESCAPE SLIDE CAUSING ESPU 13WL FAILED ON ESPU SYSTEM TEST. R & R AFT RIGHT ESCAPE SLIDE IAW AMM 25-62-44. OPS CHECKED GOOD.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 47,365 hrs · 16,353 cycles

FLT 514, CIDS ONE EPSU BITE TEST FAILS 12WL ESPU BAT FAILURE. R & R EPSU 12WL BATTERY IAW AMM 33-51-38. EPSU BITE TEST CHECKS OK IAW AMM 33-51-00-710-001-A.

Part: FAN — FAILED (E/E BAY) · airframe 47,059 hrs · 16,234 cycles

FT # 1667, BOS-CHS. BLOWER FAN MAKING SCREECHING NOISES AND BURNING SMELLS (ELECTRICAL SMELL). ALL GOES AWAY WHEN SELECTED OFF; REMOVED AND REPLACED AVIONIC BLOWER I.A.W AMM 21-26-01. MDDR CLEARED MX-4 UPDATED PLACARD REMOVED MCC NOTIFIED.

Part: ADIRU — FAILED (NR 3) · airframe 45,984 hrs · 15,869 cycles

FLT 72, SLC-JFK. EMERGENCY DECLARED. THE FLIGHT CREW REPORTED THAT IRS #3 FAILED IN CRUISE, THE #2 IR IS CURRENTLY ON MEL. WHILE IN CRUISE IRS 3 FAILED; R & R ADIRU #3 (1FP3) IAW AMM TASK 34-12-34. OPS CK NORMAL. A/C OK FOR SVC

Part: FLANGE — CORRODED (FRMAES 54-55) · corrosion level 2 · airframe 42,530 hrs · 14,628 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE OUTER FLANGE, FRAMES 54 - 55 STRINGER 38. REWORKED THE OUTER FLANGE IAW EO A32F-53-5231-00.

Part: FLANGE — CORRODED (FRAMES 56-57) · corrosion level 2 · airframe 42,530 hrs · 14,628 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE OUTER FLANGE, FRAMES 56 - 57, STRINGER 38L. REWORKED THE OUTER FLANGE IAW EO A32F-53-5231-00.

Part: FLANGE — CORRODED (FRAMES 60-61) · corrosion level 2 · airframe 42,530 hrs · 14,628 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON OUTER FLANGE FOUND AT FRAMES 60 - 61, STRINGER 37. REWORKED THE OUTER FLANGE IAW EO A32F-53-5231-00.

Part: SKIN — CORRODED (FRAMES 60-61) · corrosion level 2 · airframe 42,530 hrs · 14,628 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE SKIN AT THE ANTENNA CUTOUT, FRAMES 60 - 61, STRINGERS 1L - 1R. REPAIRED IAW SRM 53-41-11-283-001, REPAIR CATEGORY B, AND SRM 53-41-11-283-001, DIAGRAM 1, SHEET 2.

Part: FLANGE — CORRODED (FRAMES 59-60) · corrosion level 2 · airframe 42,530 hrs · 14,628 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE OUTER FLANGE, FRAMES 59 - 60, STRINGER 38L. REWORKED THE OUTER FLANGE IAW EO A32F-53-5231-00.

Part: SKIN — CORRODED (APU DOOR) · airframe 14,627 hrs · 42,529 cycles

DURING C6 CHECK AT SAL, THE RT APU DOOR (PN: D5248570001000 SN: 13500) WAS FOUND WITH CORROSION WITH SKIN PENETRATION AT THE OUTER SKIN. DUE TO THE DAMAGE LOCATION (ZONE 2) AND MAGNITUDE OF THE CORROSION, NO REPAIR IS AVAILABLE ON THE SRM, HENCE THE REASON FOR THIS REPORT. NO DAMAGE WAS OBSERVED AT THE INTERNAL STRUCTURE. SEE THE REF/1/ EO FOR MORE DETAILS. CONSULTED AND PROVIDED THE REF/2/ REPAIR INSTRUCTIONS AND REF/3/ RDAS APPROVAL. THE REPAIR CONSISTS OF TRIMMING THE SKIN TO COMPLETELY REMOVE THE DAMAGE, ACCOMPLISHING NDT INSPECTIONS, INSTALLING A DOUBLER USING PRINCIPLES OF A321 SRM TASK 52-41-21-300-004 AND RESTORING THE SURFACE PROTECTION IN ACCORDANCE WITH SRM 51-21-11 AND SRM 51- 75-12. THIS EC ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ EO AND COMPLIES WITH REF /3/ RDAS WITHOUT DEVIATION; THIS REPAIR IS CATEGORY "A" (PERMANENT REPAIR WITH NO ADDITIONAL REQUIREMENTS) AND HAS BEEN APPROVED VIA REF /3/ RDAS AND IS CLASSIFIED AS MAJOR.

Part: BOX BEAM — CRACKED (FUSELAGE) · airframe 42,529 hrs · 14,267 cycles

DURING HEAVY MAINTENANCE, C6 CHECK AT LHT (BQN), LHT REPORTED THAT AFTER ACCOMPLISHMENT OF ROTOTEST INSPECTION REQUIRED PER REF /4/ SB & REF /6/ AD- CRACKS WERE FOUND ON THE UPPER FLANGE OF THE LT SIDE (CENTER & AFT HOLE) AND RT SIDE (AFT HOLES) SIDE BOX BEAMS, SEE FIGURE 1 & 2 OF THE REF /1/ EO. IN ORDER TO COMPLY WITH REF /6/ FAA AD - CONTACTED FOR REPAIR APPROVAL. PROVIDED THE REF /2/MESSAGE WHICH PROVIDES INSTRUCTIONS TO REAM THE AFFECTED HOLES AND COLD EXPAND IN ALL LAYERS, TO RESTORE SURFACE PROTECTIONS AND TO PERFORM ALL OTHER REQUIREMENTS PER THE REF /5/ SB. THE REPAIR WAS PERFORMED AS DETAILED IN REF /2/MESSAGE AND REF /5/ SB AND THE REF /1/ EO PROVIDED THE INSTRUCTIONS FOR THIS REPAIR AND IS APPROVED BY THE REF /3/ RDAS. THE REF /3/ RDAS HAS A 6 MONTH RESTRICTION FOR FURTHER DAMAGE TOLERANCE ANALYSIS (DTA) TO BE ACCOMPLISHED. THIS EC ACCOMPLISHES THE TIME LIMITED REPAIR AND COMPLIES WITH REF /3/ RDAS WITHOUT DEVIATION. THIS EC A18-839-01 IS ISSUED TO ACCOMPLISH THE TIME LIMITED REPAIR INSTRUCTIONS. EC A18-839-02 IS ISSUED TO TRACK THE 6 MONTH LIMITATION OF THE REPAIR, AFTER WHICH DTA IS REQUIRED TO BE COMPLETED; THIS TIME LIMITED REPAIR HAS BEEN APPROVED VIA REF /3/ RDAS, PENDING DTA WITHIN 6 MONTHS, AND IS CLASSIFIED AS MAJOR.

Part: FLANGE — CORRODED (FRAMES 55-56) · corrosion level 2 · airframe 42,530 hrs · 14,628 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON OUTER FLANGE, FRAMES 55 - 56, STRINGER 38. REWORKED OUTER FLANGE IAW EO A32F-53-5231-00.

Part: BATTERY — FAULTED (CABIN) · airframe 42,288 hrs · 14,542 cycles

FLT 1730, RSW-JFK. WHILE PREFORMING TASK CARD A320-33-51-00-710-003 FOUND ROW II ABC EMERGENCY BATTERY FAULTED. REPLACED EMERGENCY BATTERY AND EPSU. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: EPSU — FAULTED (CABIN) · airframe 42,288 hrs · 14,542 cycles

FLT 1730, RSW-JFK. WHILE PREFORMING TASK CARD A320-33-51-00-710-003 FOUND ROW II ABC EMERGENCY BATTERY FAULTED. REPLACED EMERGENCY BATTERY AND EPSU.

Part: EPSU — FAULTED (CABIN) · airframe 42,288 hrs · 14,542 cycles

FLT 1730, RSW-JFK. WHILE PREFORMING TASK CARD A320-33-51-00-710-003 FOUND 2L DOOR CEILING EPSU FAULTED. REPLACED EMERGENCY BATTERY & EPSU IAW 33-51-38 OPS CK OKAY.

Part: EPSU — FAULTED (CABIN) · airframe 42,288 hrs · 14,542 cycles

FLT 1730, RSW-JFK. WHILE PREFORMING TASK CARD A320-33-51-00-710-003 FOUND 1L DOOR CEILING EPSU FAULTED. REPLACED EMERGENCY BATTERY & EPSU IAW AMM 33-51-38. OPS CK OKAY. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: BATTERY — FAILED (CABIN) · airframe 42,288 hrs · 14,542 cycles

FLT 1730, RSW-JFK. WHILE PREFORMING TASK CARD A320-33-51-00-710-003 FOUND 2L DOOR CEILING EPSU FAULTED. REPLACED EMERGENCY BATTERY & EPSU IAW 33-51-38 OPS CK OKAY.

Part: BATTERY — FAULTED (CABIN) · airframe 42,288 hrs · 14,542 cycles

FLT 1730, RSW-JFK. WHILE PREFORMING TASK CARD A320-33-51-00-710-003 FOUND ROW II ABC EMERGENCY BATTERY FAULTED. REPLACED EMERGENCY BATTERY AND EPSU.

Part: BATTERY — FAILED (CABIN) · airframe 42,288 hrs · 14,542 cycles

FLT 1730, RSW-JFK. WHILE PREFORMING TASK CARD A320-33-51-00-710-003 FOUND 1L DOOR CEILING EPSU FAULTED. REPLACED EMERGENCY BATTERY & EPSU IAW AMM 33-51-38. OPS CK OKAY.

Part: FAN — FAILED (E&E BAY) · airframe 41,705 hrs · 14,341 cycles

FLT 358, SLC-JFK. DIVERTED TO DEN. AT A CRUISE ALT OF 37000, STRONG ELECTRICAL SMOKE ODOR FOLLOWED BY NOISE & VIBRATION (EXTRACT FAN - NO AVNCS SYS FAULT ECAM CAUTION) PERFORMED TSM TASK 05-50-00-810-831-A AND FOUND CAUSE OF ODOR TO BE AVIONICS EXTRACT FAN WITH BREAKER AE2 ON 123VU TRIPPED. PLACED EXTRACT FAN ON MEL 21-26-02 COND A CAT C. MCC ROB NOTIFIED. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: COFFEEMAKER — EXPLODED (GALLEY) · airframe 40,878 hrs · 14,064 cycles

COFFEEMAKER AFT GALLEY EXPLODED. REMOVED AND REPLACED THE COFFEEMAKER IAW MM 25-25-00. OPS CHECKED OK. COMPLETE BREW CYCLE. NO DEFECTS NOTED.

Part: APU — FAILED · airframe 36,930 hrs · 12,702 cycles

INBOUND FA CREW REPORTED TOXIC FUMES, AND ODOR WERE NOTED DURING DECENT, HIGHEST CONCENTRATION SEEMED TO BE TOWARD CENTER OF CABIN BUT WAS NOTICED THROUGHOUT WITH AIRCRAFT ON GROUND AND BOTH PACKS RUNNING. THE TOXIC ODOR WAS NOTED THROUGHOUT CABIN. HIGHEST CONCENTRATION AT MIDDLE OF CABIN BUT BOTH FWD AND REAR DOORS OPEN ( PACKS - BOTH ); UPON ACCOMPLISHING BORESCOPE INSPECTION OF #1 AND #2 ENG LPC PER AMM 72-00-00-200-017B, NO OIL CONTAMINATION WAS NOTED. HOWEVER, INSPECTION OF APU INLET SCREEN REVEALED OIL CONTAMINATION. NO BORESCOPE PLUGS WERE REMOVED. ACCESSED LPC THROUGH 1.0 STATOR VANE. R & R APU IAW AMM 49-11-11, REPLACED CABIN FILTERS. PERFORMED GROUND RUN UP OF BOTH ENGINE . AIRCRAFT IS OK FOR SERVICE.

Part: BATTERY — FAULTED (CABIN) · airframe 35,266 hrs · 12,161 cycles

FLT 691, BOS-TPA. DURING ROUTINE MAINTENANCE, EMERGENCY LIGHT TEST FAULTED EMERGENCY BATTERY FIN 12WL. R & R EMERGENCY LIGHT BATTERY FIN 12WL IAW AMM 33-51-38.

Part: EEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 30,363 hrs · 10,629 cycles

DIVERTED, WHILE IN CRUISE ENGINE EPR MODE 1 FAULTED ENGINE SYS 1 FAULTED AUTO THROTTLE MESSAGE SWITCHED TO N1 MODE. COULD MAINTAIN PARTIAL POWER ENGINE 1 IN CLIMB DETENT N1 NO GREATER THAN 79 PERCENT. N1, ENGINE 1 AVAILABLE EGT ENGINE FOUND TO BE 100-200 DEGREES WARMER THAN ENGINE 2 EPR MODE MESSAGE WAS FIRST NOTED. R & R ELECTRONIC ENGINE CONTROL IAW 73-22-34. R & R P2/T2 SENSOR IAW AMM 73-22-11-000. THESE PARTS WERE REPLACED FOR TROUBLESHOOTING PURPOSES BUT DID NOT CORRECT THE PROBLEM.

Part: PROBE — FAILED (NR 1 ENGINE) · airframe 30,363 hrs · 10,629 cycles

AIR RETURNED BACK TO DEPARTURE DUE TO ENGINE 1 EPR MODE FAULTED DURING CLIMB. CREW REVEALED THAT AT THROTTLE BACK AT TOP OF CLIMB NR 1 ENGINE THRUST LOCKED AND EPR MODE FAULT APPEARED. NO FURTHER FAULTS FOR THE REST OF THE FLIGHT WITH N1 MATCHED HALF KNOB SPLIT WITH ALL REMAINING PARAMETERS MATCHED. R & R FMU IAW AMM 73-22-52-400-010-B FOR TROUBLESHOOTING PURPOSES. R & R FUEL PUMP FOR TROUBLESHOOTING PURPOSES. POWERPLANT ENGINEERING SUSPECTED T2/P2 ON NR 1 ENGINE WAS RECENTLY REPLACED WITH A ROUGE UNIT. R & R T2/P2 SENSOR, TOTAL PRESSURE PROBE, IAW AMM 73-22-11-000. OPS CHECKED GOOD.

Part: FMU — FAILED (NR 1 ENGINE) · airframe 30,366 hrs · 10,630 cycles

RETURNED TO DEPARTURE, ENGINE 1 EPR MODE FAULTED DURING CLIMB. CREW REVEALED THAT AT THROTTLE BACK AT TOP OF CLIMB NR 1 ENGINE THRUST LOCKED AND EPR MODE FAULT APPEARED. R & R FMU IAW AMM 73-22-52-400-010-B IAW AMM ACCOMPLISHED FMU/STARTER VALVE TEST IAW 80-13-51 AND FADEC SELF TEST IAW AMM 73-22-00. OPS CHECK GOOD.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 30,363 hrs · 10,629 cycles

DIVERTED, WHILE IN CRUISE, ENGINE EPR MODE 1 FAULTED ENGINE SYSTEM 1, FAULTED AUTO THROTTLE MESSAGE, SWITCHED TO N1 MODE. COULD MAINTAIN PARTIAL POWER ENGINE 1 IN CLIMB DETENT N1 NO GREATER THAN 79 PERCENT. N1 ENGINE 1 AVAILABLE EGT ENGINE FOUND TO BE 100-200 DEGREES WARMER THAN ENGINE 2 EPR MODE MESSAGE WAS FIRST NOTED. R & R ELECTRONIC ENGINE CONTROL IAW 73-22-34. ACCOMPLISHED TEST II HIGH POWER ASSURANCE RUN TEST NORMAL.

Part: HYDRAULIC LINE — BROKEN (RT MLG) · airframe 15,025 hrs · 5,279 cycles

FLT 822 SDQ-JFK, CREW DECLARED EMERGENCY DUE TO ON GEAR EXTENSION ECAM G LOW RSVR LO LVL. CREW FOLLOWED QRH AND PERFORMED L/G GRAVITY EXTENSION. FOUND BROKEN LINE ON RT MLG DOOR, REPLACED LINE, SWIVEL FITTING THREAD WHERE NICKED AS WELL. REMOVED AND REPLACED SWIVEL FITTING (2764GM). NO LEAKS NOTED AND MLG DOORS CHECKS NORMAL IAW AMM 32-31-38. LANDING GEAR SYSTEM BACK TO NORMAL MADE AFTER FREE FALL EXTENSION IAW 32-00-00-860-003.