N793JB

Part: ENGINE — FAILED (NR 2) · airframe 52,584 hrs · 18,589 cycles

FLT#2922, NAS-JFK. (AIRCRAFT PERFORMED AIR TURNBACK TO NAS) "ENGINE #2 BANG AND SEIZE. INSPECTED ENGINE #2 IAW AMM 05-51-26 FOUND NO AIRFRAME DEFECTS ENGINE #2 METAL, DEBRIS FOUND IN EXHAUST REMOVED AND REPLACED #2 ENGINE IAW AMM 71-00-20-400-040. REFERENCE WO #1426688.

Part: EPSU — FAILED (ZONE 200) · airframe 49,687 hrs · 17,483 cycles

FLT#2534, PBI-DCA. 'FWD ENTRY DOOR EMERGENCY LIGHTS INOP; REMOVED AND REPLACED FWD EPSU (10WL) REF AMM 33-51-38,OPS CHECK GOOD.'

Part: FLAP SYSTEM — LOCKED · airframe 49,043 hrs · 17,241 cycles

FLT#1251, HPN-PBI. (AIRCRAFT DIVERTED TO JFK) .' FLAPS LOCKED FLAPS INOP; REF LP 4041509-1 (REF AWN 27-51-14 AND ASM 27-51-07 CHECK WIRING FOUND WIRE # 2751-4528 DAMAGE BETWEEN 34 CV R WING TIP BROKE AND 4008 VS ACCOMPLISHED A GRADE 1A REPAIR IAW ESPM 20-53-21 OPS TEST OF THE WING TIP BRAKE IAW AMM 27-51-00 EXTENSION AND RETRACTION OF THE FLAPS IAW 27-50-00 ALL OPS CHK OKAY AC OKAY FOR SVC) AND LP 4041508-2 (PERFORMED TS PER TSM 27-51-00-810-837- A DURING CONTINUITY CHECK FOUND OPEN BETWEEN SFCC-2 PIN 14K AND 34 CVB PIN A SOLENOID CONNECTOR CONFIRMED CONTINUITY BETWEEN SFCC 2 PIN 14K AND 94 VC PIN 2 FUTHER TS REQUIRED) FOR CORRECTIVE ACTIONS.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,934 hrs · 16,817 cycles

FLT#363,BOS-UVF. ' LEVEL 1 TRANSIENT ODOR REPORTED BY AFT FA'S DURING DESCENT; COMPLIED WITH INFO NOTICE 2017 - T015 SECTION A ISOLATION FAULT TYPE 101 (A) 1X PCD TSM 05 -50 -00 -810 -085B -055D. A/C OK FOR SERVICE.'

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,260 hrs · 16,553 cycles

FLT#1570, LAX-CUN. 'INBOUND INFLT CREW REPORTED THAT ON SHORT FINAL FOR FLIGHT 1570 A STRONG CHEMICAL ODOR WAS IN THE GALLEY. IT CAUSED MED BURNING SENSATION TO THEIR NOSE AND THROAT. SUBSIDED IN 10 MINS; COMPLIED WITH INFORMATION NOTICE 2017-T015J SECTION A ISOLATED FAULT.A/C IS OK FOR SVC.MCC BOB NOTIFIED.'

Part: THERMOSTAT — FAILED (7170HM2) · airframe 46,562 hrs · 16,303 cycles

FLT#361, JFK-BGI. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'AIR ENG 2 BLEED FAULT; REMOVED AND REPLACED THERMOSTAT (7170HM2) ON ENG #2 IAW AMM 36-11-43. OPS CHECK GOOD. AIR ENG 2 BLEED FAULT MSG NOT DISPLAY ON ECAM.'

Part: WARNING MESSAGE — FALSE ACTIVATION (ALTERNATE BRAKE) · airframe 43,781 hrs · 15,028 cycles

FLT 1942, LGA-DEN. AIRCRAFT DECLARED AN EMERGENCY. AFTER LOWERING LANDING GEAR. BRAKES ALTN LT BRAKE RELEASED, RESET ALTERNATE BRAKES AND PERFORMED BITE TEST IAW AMM 32-43-00-710-002-A. NO FAULTS NOTED.

Part: PROXIMITY SENSOR — MISSING · airframe 39,776 hrs · 13,726 cycles

FLT #1505, EWR-FLL. (EMERGENCY DECLARED)PUT LG DOWN FOR LANDING RECEIVED ECAM "LG DOORS NOT CLOSED" FOR RIGHT NOSE GEAR DOOR ; AFTER SECOND APPROACH RECEIVED "L/G SYSTEM DISAGREE UPON LANDING. INSP NLG AREA AND FOUND NLG PROX SNSR 19GA TARGET ASSY MISSING. INSTALLED NEW TARGET ASSY IAW 32-31-73-400-005A. PERFORMED LGCIU 1 & 2 BITE CHK IAW AMM 32-69-00-740-001A. OPS CHK GOOD

Part: LIGHT — LOOSE · airframe 39,677 hrs · 13,689 cycles

FLT # 38, SJO-FLL. OVERHEAD EMERGENCY ISLE LIGHT ABOVE ROW 18 INOP ; FOUND GROUND WIRE LOOSE - SECURED + OPS CHECK GOOD REF 35-50-00 A/C OK FOR SVC

Part: FRAME — CRACKED (FRM 43) · airframe 37,692 hrs · 13,015 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FR43 RH SIDE AFT FASTENER OF SIDE BOX BEAM; (REF AEROMAN NR 2021-73/1-2021-62557) ACCOMPLISHED EC A320-53-1251 FR43 RH SIDE AFT HOLE OF SIDE BOX BEAM

Part: BATTERY — FAILED (12WL-BATT) · airframe 37,692 hrs · 13,015 cycles

DURING HEAVY MAINTENANCE, FAULT EPSU 12WL; (REF AEROMAN NR 2021-62693 WO 2021 73/1) R &R BATTERY EPSU 12WL IAW AMM 33-51-38 OPS CHECKS OK IAW AMM 33-51-00-710-001-A

Part: FLOOR SUPPORT — CORRODED (FRAME 16-20) · airframe 37,692 hrs · 13,015 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM +Y1292 BTW FRAME 16 AND FRAME 20 AT FWD GALLEY AREA CPC RELATED 531189-01; REMOVED AND REPLACED FLOOR BEAM +Y1292 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA IAW A320 SRM 51-42-11 AND DWG D53110984, D53110920, AND EA 53-0055-21 PART #1 AND EC A21-159-01 TOOL USED CALIPER PN 500-197-30 SN A18234378 DUE DATE JUL-30-21 COMPLETED MX-220

Part: SKIN — CORRODED (RT WING TE) · airframe 37,692 hrs · 13,015 cycles

DURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG BETWEEN RIB7 TO RIB 8 RELATED CPCP MPD TASK 572178-1 ON RH WING REF AEROMAN NR 2021-62518; PERFORMED PERMANENT REPAIR ON EXACTLY LOCATION BTW WX3622 OUTER JACK RIB AND RIB7A WX4013 TRAILING EDGE TOP SKIN LOWER SURFCE ON RH WING IAW EA 57-0044-21 PART #1 PART#2 AND EC A21-165-01. THIS REPAIR IS CLASSIFIED CATAGORY A AND NO FURTHER INSPECTION IS REQUIRED. TOOL USED CALIPER PN 500-197-30 SN A18234378 DUE DATE JUL 20-21 NDT EQUIPMENT PN NORTEC600D SN 60009161631 DUE DATE DEC 01-21 THICKNEWSS GUAGE PN 45MG SN 1300633701 DUE DATE APR 13-21 COMPLETED MX 220 FORM BY CPCP PROGRAM. ALL WORK PERFOMED ON AEROMAN NR 2021-62518

Part: FRAME — CRACKED (FRM 43) · airframe 37,692 hrs · 13,015 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FR43 LH SIDE MIDDLE HOLE OF SIDE BOX BEAM; (REF AEROMAN 2021-73/1/2021-62553) ACCOMPLISHED EC A320-53-1251 FR43 LH SIDE MIDDLE HOLE OF SIDE BOX BEAM

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 37,692 hrs · 13,015 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y1292 BTW FRAME 16 AND FRAME 20 AT FWD GALLEY AREA CPCP RELATED 531189-01; REMOVED AND REPLACED FLOOR BEAM -Y1292 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA IAW A320 SRM 51-72-11 DWG D53110920 AND D53110984, TOOL USED CALIPER PN 500-752-20 SN B1610263 DUE DATE AUG 06-21 COMPLETED MX-220 FORM BY CPCP PROGRAM. ALL WORK ACCOMPLISHED ON AEROMAN NR 2021-62675

Part: SUPPORT — CORRODED (FRM 68) · airframe 37,692 hrs · 13,015 cycles

DURING HEAVY MAINTENANCE, CORROSION LOWER SILL ON FR68 AT LEVEL STR 23R AT AFT GALLEY AREA RELATED CPCP 534143-01; PERFORMED PERMANENT REPAIR ON LOWER SILL ON FR68 AT LEVEL STR 23R AT AFT GALLEY IAW A320 SRM 53-41-14-300-001 REPAIR PRICCIPLE 5 TOOL USED DIGITAL CALIPER PN 500-197-30 SN A18234378 AND DUE DATE JUL 30 -21 ALL WORK ACCOMPOLISHED ON AEROMAN NR 2021-62689

Part: BATTERY — FAILED (10WL-BATT) · airframe 37,692 hrs · 13,015 cycles

DURING HEAVY MAINTENANCE, FAULT EPSU 10WL; (REF AEROMAN NR 2021 62778 WO 2021 73/1) R & R EPSU BATTERY 10WL IAW AMM 33-51-38 OPS CHECKS OK IAW AMM 33-51-0-710-001-A

Part: FLOORBEAM — CORRODED (FRAME 68) · airframe 37,677 hrs · 13,007 cycles

DURING HEAVY MAINTENANCE, CORROSION IN AFT WET AREA ON FLOOR BEAM -Y1292 AT FR68. EVALUATED CORROSION ON FLOOR BEAM -Y1292 AT FR 68, MATERIAL LOSS OF .035 IS OUT OF LIMITS. REMOVED AND REPLACED FLOOR BEAM IAW A320 SRM 51-42-11 AND 53-00-14

Part: FLOORBEAM — CORRODED (FRAME 68) · airframe 37,677 hrs · 13,007 cycles

DURING HEAVY MAINTENANCE, CORROSION IN AFT WET AREA ON FLOOR BEAM -Y765 AT FRAME 68; (RESOLVED ON W/O: 1056627 TASKCARD: NR-00011 ) EVALUATED AREA FLOOR BEAM -Y765 AT FR 68 CORROSION MATERIAL LOSS OF .037 IS OUT OF LIMITS REMOVED AND REPLACED FLOOR BEAM IAW A320 SRM 51-42-11 AND 53-00-14

Part: FLOOR SUPPORT — CORRODED (FRAMES 69-70) · airframe 37,677 hrs · 13,007 cycles

DURING HEAVY MAINTENANCE, AFT CABIN FLOOR LH SIDE FR 69-70 Y1292FLOOR SUPPORT WEB CORRODED; (RESOLVED ON W/O: 1056627 TASKCARD: NR-00015 ) UPON EVALUATION OF SHEAR PLATE AT FR 69-70 Y1292 FOUND SHEAR PLATE TO BE CRACKED. REMOVED AND REPLACED SHEAR PLATE IAW A320 SRM 51-42-11

Part: FLOORBEAM — CORRODED (FRAME 68) · airframe 37,677 hrs · 13,007 cycles

DURING HEAVY MAINTENANCE, CORROSION IN AFT WET AREA ON FLOOR BEAM Y1292 AT FR 68; (RESOLVED ON W/O: 1056627 TASKCARD: NR-00013 ) EVALUATED CORROSION ON FLOOR BEAM Y 1292 AT FR 68 MATERIAL LOSS OF .026 IS OUT OF LIMITS. REMOVED AND REPLACED FLOOR BEAM IAW A320 SRM 51-42-11 AND 53-00-14

Part: FLOORBEAM — CORRODED (FRAME 68) · airframe 37,677 hrs · 13,007 cycles

DURING HEAVY MAINTENANCE, CORROSION IN AFT WET AREA ON FLOOR BEAM Y765 AT FR 68; (RESOLVED ON W/O: 1056627 TASKCARD: NR-00012 ) REMOVED AND REPLACED FLOOR BEAM AFT WET AREA Y765 AT FR 68 IAW A320 SRM 51-42-11 MATERIAL LOSS OF .022 IS OUT OF LIMITS IAW A320 SRM 53-00-14

Part: FLOORBEAM — CORRODED (FRAME 68) · airframe 37,677 hrs · 13,007 cycles

DURING HEAVY MAINTENANCE, AFT WET AREA FR68 -Y300 FLOOR BEAM SMALL SPOT OF CORROSION; (RESOLVED ON W/O: 1056627 TASKCARD: NR-00016 ) EVALUATED CORROSION AT FLOOR BEAM -Y300 FR 68 MATERIAL LOSS OF .029 IS OUT OF LIMITS. REMOVED AND REPLACED FLOOR BEAM IAW A320 SRM 51-42-11 AND 53-00-14

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-70) · airframe 37,677 hrs · 13,007 cycles

DURING HEAVY MAINTENANCE, AFT CABIN FLOOR RH SIDE FR 69-70 -Y1292 FLOOR SUPPORT WEB CORRODED; (RESOLVED ON W/O: 1056627 TASKCARD: NR-00014) UPON EVALUATION OF SHEAR PLATE AT FR 69-70 -Y1292 FOUND SHEAR PLATE CRACKED. REMOVED AND REPLACED SHEAR PLATE IAW A320 SRM 51-42-11

Part: BLOWER — FAILED (COCKPIT) · airframe 37,589 hrs · 12,972 cycles

FLT 739, EMERGENCY DECLARED. LOUD NOISE AND VIBRATION UNDER OUR FEET ON BOTH SIDES WHEN SMOKE AND FUMES INITIATED BLOWER MOTOT, SWITCHED OFF, VIBRATION STOPPED AND FUMES DISSIPATED AFTER A FEW MINUTES . AT TOP OF DESCENT FUMES CAME BACK OXYGEN MASKS DONNED AGAIN.

Part: EPSU — FAILED (CABIN) · airframe 34,056 hrs · 11,667 cycles

FLT 2894, MBJ-BOS. CIDS 1 FAULT ON 11WL EMERGENCY LIGHT BATTERY; REMOVED & REPLACED EMERGENCY BATTERY & POWER SUPPLY IAW AMM 33-51-38. OPS CHECKS GOOD.

Part: BATTERY — FAILED (CABIN) · airframe 34,056 hrs · 11,667 cycles

FLT 2894, MBJ-BOS. CIDS 1 FAULT ON 11WL EMERGENCY LIGHT BATTERY; REMOVED & REPLACED EMERGENCY BATTERY & POWER SUPPLY IAW AMM 33-51-38. OPS CHECKS GOOD.

Part: BATTERY — FAILED (CABIN) · airframe 33,546 hrs · 11,483 cycles

FLT 391, BOS-TPA. EMERG LIGHT TEST BATTERY FAULT AT 10WL; REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT 10 WL PER AMM 33-51-38.

Part: BATTERY — FAILED (CABIN) · airframe 33,546 hrs · 11,483 cycles

FT # 391, BOS-TPA. EMERG LIGHT TEST BATTERY FAULT AT 13WL; REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT 13WL PER AMM 33-51-38.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 31,191 hrs · 10,594 cycles

FLT 894, STI-EWR. PASSING THRU 14,000 ON DECENT, CAPT SMELLED DIRTY SOCK ODOR ALSO NOTICED HP VALVES WERE OPEN, ON BLEED PAGE. ISOLATED NR 1 PACK AND SMELL WENT AWAY CABIN ATTENDANTS DID NOT SMELL ANYTHING. COMPLIED WITH INFO NOTICE 2017-T015C SECTION A. A/C OK FOR SERVICE RUN ENG NR 1 AND PACK 1 FOR 10MINS. COULD NOT DUPLICATE ODOR.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 27,530 hrs · 9,184 cycles

FLT 1097, BOS-PHL. DURING CRUISE FLIGHT AT FL 380, AFT CARGO SMOKE DET OCCURRED. DECLARED AN EMERGENCY. DIVERTED TO PHL. PERFORMED ECAS ACTIONS - DISCHARGED AFT CARGO AGENT 1. GOT ANOTHER RED SMOKE DET ECAM, THEN AFT CRG BTL 1 FAULT AND AFT VRG DET FAULT ECAM. AS PRECAUTION, DISCHARGED BTL 2 ECAM 1 CONTINUED! ALL QRH + ECAM COMPLIED WITH. LANDED UNDERWEIGHT AT 1300,000LBS. FIRE/RESCUE PERFORMED IR CHECK OF AFT CARGO COMPARTMENT- CHECKED OK. THEN THEY PERFORMED A VISUAL INSPECTION OF FWD + AFT CARGO COMPARTMENTS, CHECKED OK; INSPECTED BOTH FWD AND AFT CARGO COMPARTMENTS. NO EVIDENCE OF SMOKE OR FIRE. BOTH COMPARTMENTS ARE CLEAN . R & R CARGO FIRE BOTTLE PER AMM 26-23-42: TESTS OK AT THIS TIME. ITEM CLEARED, MX-4 UPDATED, PLACARD REMOVED, MCC NOTIFIED. R & R CARGO FIRE BOTTLE PER AMM 26-23-42: TESTS OK AT THIS TIME. ITEM CLEARED, MX-4 UPDATED, PLACARD REMOVED, MCC NOTIFIED. PER PFR SMOKE DETECTOR 3WH FAULT. REPLACED 3WH CARGO SMOKE DETECTOR PER MM 26-16-15 CHK OK. CLEARED MEL MDDR.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 26,078 hrs · 8,625 cycles

EPSU (12WL) FAILED CAPACITY CHECK IAW T/C 33-51-00-710-003. R & R THE EPSU IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: LAMP — FAILED (SIDEWALL LIGHT) · airframe 24,978 hrs · 8,227 cycles

DISCOVERED 23F CABIN SIDEWALL LIGHT BURNED OUT. THERE WAS AN ASSOCIATED BURNED ELECTRICAL ODOR IN GALLEY; REPLACED THE LAMP. OPS CHECK PASSED. ACCOMPLISHED TSM 24-00-00-810-823. NO OTHER ELECTRICAL ODORS NOTED IN CABIN OR GALLEY AREA. NO BREAKERS TRIPPED. INSPECTION OF WIRING IN AREA OF 23F SIDEWALL FOUND TO BE OK IAW AMM 33-21-11.

Part: CONNECTOR — BACKED OUT (CABIN) · airframe 22,723 hrs · 7,391 cycles

DURING ROUTINE MAINTENANCE, OVERHEAD EMERGENCY LIGHT AT ROW 18 WAS FOUND TO BE INOPERATIVE. FOUND THAT CONNECTOR HAD BACKED OFF FROM CONNECTION POINT. RECONNECTED WIRES AND PERFORMED OPS CHECK. OPS CHECK PASSED.