N523JB

Service difficulty reports · 124

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N523JB' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR YENA2026091800855Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ2 FRAME 36. CRACK L= 0.315 INCH.; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00031 ) REF AEROMAN WO# 2026-279/1 NR# 2026-348509 ACCOMSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800854Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ3 FRAME 36. CRACK L= 0.375 INCH.; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00032 ) REF AEROMAN WO# 2026-279/1 NR# 2026-348510 ACCOMSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800853Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ4 FRAME 36. CRACK L= 0.640 INCH.; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00033 ) REF AEROMAN WO# 2026-279/1 NR# 2026-348511 ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800852Floorbeam · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE FRONT SPAR VERTICAL STRINGER Ñ5 FRAME 36. CRACK L= 0.435 INCH; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00034 ) REF AEROMAN WO# 2026-279/1 NR# 2026 348512 ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800851Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD RH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACKED DIRECTION IS 9OCLOCK, CRACK DEPTH IS 0.120 INCH APPROX., IN FWD CARGO COMPARTMENT (1EA); (RESOSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800850Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION ARE 4 AND 9OCLOCK, CRACKDEPTH IS 0.120 INCHAPOROX., IN FWD CARGO COMPARTMENT (2EA); (RESep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800849Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 RH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER AFT COMMON TO SKIN,CRACK DIRECTIONS ARE 2 AND 6 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456 TSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800848Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER AFT COMMON TO SKIN,CRACK DIRECTIONS ARE 11 AND 6 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800847Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 2 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 14Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800846Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 3 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1435Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800845Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FASTENER HOLE 5 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 143Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800844Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 20, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00058 ) ACCOMSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800843Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 19, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.081 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00059 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800842Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 14, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.094 IN CH APPROX., IN FWD CARGO COMPARTMENT ALL WORK ACCOMPLISHED ON AEROMAN WO 2026 279/1 NR2026-3Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800841Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 22, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00061 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800840Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 23, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.079 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00062 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800839Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 24, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.082 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00063 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800838Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 27, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.095 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00064 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800837Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 26, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.085 I NCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00065 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800836Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 7 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 14Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800835Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 5 INCH O/B FROM Y1292 APPROX., CRACK DIRECTIONS ARE 6 AND 12 OCLOCK, CRACK DEPTH IS 0.080 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON WSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800834Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 6 INCH O/B FROM Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOCK , CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA);(RESOLVED ON W/O: 143545Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800833Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 4 INCH O/B FROM Y1292 APPROX., CRACK DIRECTION IS 12 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 143Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800832Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 16, CRACK DIRECTION IS 12 OCLOCK , CRACK DEPTH IS 0.080 INCH APPROX., IN FWD CARGO COMPARTMENT; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00070 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2026091800831Pressure Deck · corrodedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 2 INCH O/B FROM Y1292 APPROX., CRACK DIRECTION ARE 6 AND 1 2 OCLOCK, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (2 EA); (RESOLVED ON WSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800830Pressure Deck · corrodedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 3 INCH O/B FROM Y1292 APPROX.,CRACK DIRECTION IS 12 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1435Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800829Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE OPEN F ASTENER HOLE 9 INCH O/B FROM Y1292 APPROX.,CRACK DIRECTION IS 12 OCLO CK, CRACK DEPTH IS 0.105 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA ); (RESOLVED ON W/O: 143Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800828Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE Ñ 28, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.084 IN CH APPROX., IN FWD CARGO COMPARTMENT ; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00074 ) ACCOMPSep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800827Pressure Panel · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 LH SIDE IN PRESSURE DECK MEMBRANE A REA IN OPEN FASTENER HOLE Ñ 13 CRACK DIRECTION: 05 OCLOCK , CRACK DEPT H=0.113 INCH; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00075 ) ACCOMPLISH MAJOR REPAIR ON THE Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800826Pressure Deck · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 RH SIDE IN PRESSURE DECK MEMBRANE OPEN FA STENER HOLE 6 INCH O/B FROM -Y1292 APPROX.,CRACK DIRECTION IS 6 OCLOC K, CRACK DEPTH IS 0.085 INCH APPROX., IN FWD CARGO COMPARTMENT (1 EA); (RESOLVED ON W/O: 1435Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800825Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON BOTTOM SKIN PANEL ON INBOARD SIDE FLAP TRACK CENTERLINE LH WING BTW RIB 5 THRU RIB 6; (RESOLVED ON W/O: 1435456 TASKCARD: NR-00077 ) ACCOMPLISHED MEJOR REPAIR OF CORROSION AFFECTING LA WING BOTTOM SKIN PANEL 3, UPPER SURFSep 18, 2026 · N523JB · Airbus A320232 · Trailing Edge FlapsSDR YENA2026091800824Fire Bottle · dischargedDURING HEAVY MAINTENANCE, AEROMAN DISCHARGED FIRE EXTINGUISHER BOTTLE APU; REF: ARM W/O 2026-279/1 N/R 2026-348729 R&R DISHARGED FIR BOTTLE IAW AMM 26-22-41-000-001-A AND 26-22-42-400-001-A TEST OK IAW 26-13-00-710-001-ASep 18, 2026 · N523JB · Airbus A320232 · Extinguishing SystemSDR YENA2026091800823Pressure Panel · crackedDURING HEAVY MAINTENANCE, EA A26-699-01, CENTER FUSELAGE, FR36 LH PRESSURE PANEL ATTACHMENT HOLES CRACKED. TIME LIMITED REPAIR (CONSIDERED AS A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800822Floorbeam · crackedDURING HEAVY MAINTENANCE, EA A26-595-01, CENTER BOX / FRONT SPAR VERTICAL STRINGERS & HORIZONTAL FLOORBEAMS, AT LEVEL OF FR36. CRACKS – PERMANENT REPAIR (CONSIDERED AS A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2026091800821Pressure Blkhd · crackedDURING HEAVY MAINTENANCE, EA A26-716-01, FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT @ LEVEL OF STGR 30RH, FASTENER HOLES W1 & H2, CRACK DAMAGE – TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, BulkheadSDR YENA2026091800820Pressure Panel · damagedDURING HEAVY MAINTENANCE, EA A26-700-01, FR36 RH PRESSURE PANEL ATTACHMENT HOLES CRACKED - TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2026091800819Skin · corrodedDURING HEAVY MAINTENANCE, EA A26-815-01. LH WING BOTTOM SKIN PANEL 3 UPPER SURFACE RIBS 6A BTWN FALSE SPAR TO REAR SPAR CORRODED. TIME LIMITED REPAIRSep 18, 2026 · N523JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026091800818Pressure Blkhd · crackedDURING HEAVY MAINTENANCE, EA A26-710-01, FR35 PRESSURE BULKHEAD CRACKED - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, BulkheadSDR YENA2026040600383Lamp · inoperativeFLT 2324, MCO-MCO. OVERHEAD EMERGENCY EXIT LIGHTS OVER R1 AND R2 PARTIALLY ILLUMINATED. REPLACED THE LAMPS OVERHEAD EXIT SIGNS IAW AMM 33-51-16"Apr 7, 2026 · N523JB · Airbus A320232 · Emergency LightingSDR YENA2026040800381Lamp · inoperativeFLT# 2324, MCO-MCO. "OVERHEAD EMERGENCY EXIT LIGHTS OVER R1 AND R2 PARTIALLY ILLUMINATED; REPLAMPED OVER HEAD EXIT SIGNS IAW AMM 33-51-16"Apr 7, 2026 · N523JB · Airbus A320232 · Emergency LightingSDR YENA2025121501200A/C Pack · odorFLT#927, EWR-MCO. ENVIRONMENTAL SYSTEM EMITTED FUMES IN COCKPIT SHORTLY AFTER TAKEOFF AND DURING CLIMB. FUMES ISOLATION GUIDES APPLIED. FUMES DISSIPATED WITH PACK 1 OFF. PACK 2 ON AND CROSS BLEED SHUT . APU BLEED AIR SUPPLY SYSTEM. OPENDec 14, 2025 · N523JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2025102301055Lubrication Unit · failedFLT#487, ORH-MCO. "FA REPORTS STRONG MUSTY ODOR IN AFT GALLEY REPEAT EVENT; COMPLETED WITH INFO NOTICE + DECON (LEVEL A) FOUND TUBE MODULE ON APU LEAKING REMOVED AND REPLACED LUBE MODULE IAW AMM 49-91-45. OPS & LEAK CK GOOD. NO ODOR PRESENT."Oct 22, 2025 · N523JB · Airbus A320232 · APU Oil SystemSDR YENA2025102301054A/C Pack · odorFLT#195, HPN-MCO. "APPROACHIN 3000' PACKS DELIVERED STRONG MUSTY SMELL. INFLIGHT NOTIFIED CREW THAT ODOR WAS STRONG IN REAR OF AIRCRAFT AS WELL AS FRONT; PERFORMED INSPECTION ON APU, FOUND NO LEACKS. PERFORMED APU OPS TEST & RAN BOTH PACKS. NO SMELLS NOTED. " Oct 21, 2025 · N523JB · Airbus A320232 · Cabin Cooling SystemSDR YENA2024052100771Radar · failedFLT#1384, SDQ-STI. (AIRCRAFT DIVERTED TO STI) 'ON APPROACH TO SDQ WEATHER RADAR INOP; REMOVED AND REPLACED WX RADAR TRANSCEIVER AS PER AMMM 34-41-33 PERFORMED WX RADAR TEST AS PER AMM 34-41-00-740-002. NO FAULTS NOTED.'May 21, 2024 · N523JB · Airbus A320232 · Weather Radar SystemSDR YENA2023122101621Unknown · unknownFLT#927, EWR-MCO. 'INFLIGHT REPORTED ODOR THAT INTENSIFIED DURING APPROACH & LANDING STARTING IN REAR MOVING FORWARD IN CABIN CAUSING BURNING EYES AND NOSE; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TYPE 10(A), 1C PER TSM 05-50-00-Dec 18, 2023 · N523JB · Airbus A320232 · Air Distribution SystemSDR YENA2023101801271Unknown · unknownFLT#1151, BOS-MCO. ' FA REPORTED FUME "DIRTY SOX" SMELL UPON LEVEL OFF ON FINAL APP 2000' PWR UP; COMPLIED WITH INFORMATION NOTICE 2017- TO15, SECTION A. ISOLATED FAULTTO TYPE10(A) 1C PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-085D. AIRCRAFT IS OK FOR SERVIOct 15, 2023 · N523JB · Airbus A320232 · Air Distribution SystemSDR YENA2023072700872Unknown · unknownFLT#1954, DCA-BOS. 'AIRBORNE FUME EVENT AFT GALLEY; NO MX-270 PROVIDED. COMPLIED WITH INFO NOTICE 2017-T015 SECTION A, ISOLATED TO FAULT TYPE 10 PER TSM 05-50-00-810-085-B. APU WAS REPLACED ON 6-13-23 DUE TO ODOR EVENTS. THE PREVIOUS EVENT TO THIS ON 7-16-23 WJul 24, 2023 · N523JB · Airbus A320232 · Air Distribution SystemSDR YENA2023062700742Unknown · unknownFLT#423, BOS-STI. (AIRCRAFT DIVERTED TO JFK) 'ON DEPARTURE CLIMBING THROUGH 1,000' AIRCRAFT PITCHED UP GENTLY UNCOMMANDED AND PITCH TRIM WAS MOVING NOSE UP W/ NO COMMANDS FROM; AS PER TSM 27-30-00 R/R ELAC 2 IAW AMM 27-93-34. OPS CHECK IS GOOD. A/C OK TO CONT Jun 23, 2023 · N523JB · Airbus A320232 · Flight Control SystemSDR YENA2023060700589Unknown · unknownFLT#461, LGA-PBI. 'LEVEL 3 ODOR EVENT ISOLATED PACK 1 OFF REDUCED SMELL; ACCOMPLISHED INFO NOTICE 2017-TO15J IDENTIFIED APU LEAKING AS CAUSE REF ITEM # 2 FOR DEFERRAL DECONTAMINATION LEVEL 1 WAS ACCOMPLISHED NO ODOR PRESENT A/C OK FOR SERVICE.'May 31, 2023 · N523JB · Airbus A320232 · Standard Practices/StructuresSDR YENA2023053000561Unknown · unknownFLT#484, RDU-BOS. 'ON APPROACH BELOW 8K FEET DIRTY DOCK SMELL.' (SUPPLEMENTAL INFORMATION TO FOLLOW)May 26, 2023 · N523JB · Airbus A320232 · Standard Practices/Structures
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