# Service difficulty reports: N523JB

A list on [N523JB](https://openairdocs.org/aircraft/N523JB.md).

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

Page 1 of 3 · 124 reports

- [SDR YENA2026091800855](https://openairdocs.org/sdr/YENA2026091800855.md): Floorbeam · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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 ACCOM
- [SDR YENA2026091800854](https://openairdocs.org/sdr/YENA2026091800854.md): Floorbeam · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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 ACCOM
- [SDR YENA2026091800853](https://openairdocs.org/sdr/YENA2026091800853.md): Floorbeam · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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 ACCOMP
- [SDR YENA2026091800852](https://openairdocs.org/sdr/YENA2026091800852.md): Floorbeam · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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 ACCOMP
- [SDR YENA2026091800851](https://openairdocs.org/sdr/YENA2026091800851.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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); (RESO
- [SDR YENA2026091800850](https://openairdocs.org/sdr/YENA2026091800850.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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); (RE
- [SDR YENA2026091800849](https://openairdocs.org/sdr/YENA2026091800849.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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 T
- [SDR YENA2026091800848](https://openairdocs.org/sdr/YENA2026091800848.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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: 1435456
- [SDR YENA2026091800847](https://openairdocs.org/sdr/YENA2026091800847.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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: 14
- [SDR YENA2026091800846](https://openairdocs.org/sdr/YENA2026091800846.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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: 1435
- [SDR YENA2026091800845](https://openairdocs.org/sdr/YENA2026091800845.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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: 143
- [SDR YENA2026091800844](https://openairdocs.org/sdr/YENA2026091800844.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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) ACCOM
- [SDR YENA2026091800843](https://openairdocs.org/sdr/YENA2026091800843.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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) ACCOMP
- [SDR YENA2026091800842](https://openairdocs.org/sdr/YENA2026091800842.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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 NR2026-3
- [SDR YENA2026091800841](https://openairdocs.org/sdr/YENA2026091800841.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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) ACCOMP
- [SDR YENA2026091800840](https://openairdocs.org/sdr/YENA2026091800840.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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) ACCOMP
- [SDR YENA2026091800839](https://openairdocs.org/sdr/YENA2026091800839.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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) ACCOMP
- [SDR YENA2026091800838](https://openairdocs.org/sdr/YENA2026091800838.md): Pressure Deck · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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) ACCOMP
- [SDR YENA2026091800837](https://openairdocs.org/sdr/YENA2026091800837.md): Pressure Deck · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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) ACCOMP
- [SDR YENA2026091800836](https://openairdocs.org/sdr/YENA2026091800836.md): Pressure Deck · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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: 14
- [SDR YENA2026091800835](https://openairdocs.org/sdr/YENA2026091800835.md): Pressure Deck · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 W
- [SDR YENA2026091800834](https://openairdocs.org/sdr/YENA2026091800834.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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: 143545
- [SDR YENA2026091800833](https://openairdocs.org/sdr/YENA2026091800833.md): Pressure Deck · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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: 143
- [SDR YENA2026091800832](https://openairdocs.org/sdr/YENA2026091800832.md): Frame · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Frame
  > DURING 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) ACCOMP
- [SDR YENA2026091800831](https://openairdocs.org/sdr/YENA2026091800831.md): Pressure Deck · corroded · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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 W
- [SDR YENA2026091800830](https://openairdocs.org/sdr/YENA2026091800830.md): Pressure Deck · corroded · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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: 1435
- [SDR YENA2026091800829](https://openairdocs.org/sdr/YENA2026091800829.md): Pressure Deck · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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: 143
- [SDR YENA2026091800828](https://openairdocs.org/sdr/YENA2026091800828.md): Pressure Deck · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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) ACCOMP
- [SDR YENA2026091800827](https://openairdocs.org/sdr/YENA2026091800827.md): Pressure Panel · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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
- [SDR YENA2026091800826](https://openairdocs.org/sdr/YENA2026091800826.md): Pressure Deck · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING 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: 1435
- [SDR YENA2026091800825](https://openairdocs.org/sdr/YENA2026091800825.md): Skin · corroded · Sep 18, 2026 · N523JB · Airbus A320232 · Trailing Edge Flaps
  > DURING 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 SURF
- [SDR YENA2026091800824](https://openairdocs.org/sdr/YENA2026091800824.md): Fire Bottle · discharged · Sep 18, 2026 · N523JB · Airbus A320232 · Extinguishing System
  > DURING 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-A
- [SDR YENA2026091800823](https://openairdocs.org/sdr/YENA2026091800823.md): Pressure Panel · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, EA A26-699-01, CENTER FUSELAGE, FR36 LH PRESSURE PANEL ATTACHMENT HOLES CRACKED. TIME LIMITED REPAIR (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2026091800822](https://openairdocs.org/sdr/YENA2026091800822.md): Floorbeam · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING 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)
- [SDR YENA2026091800821](https://openairdocs.org/sdr/YENA2026091800821.md): Pressure Blkhd · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING 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)
- [SDR YENA2026091800820](https://openairdocs.org/sdr/YENA2026091800820.md): Pressure Panel · damaged · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, EA A26-700-01, FR36 RH PRESSURE PANEL ATTACHMENT HOLES CRACKED - TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026091800819](https://openairdocs.org/sdr/YENA2026091800819.md): Skin · corroded · Sep 18, 2026 · N523JB · Airbus A320232 · Wing, Plate/Skin
  > DURING 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 REPAIR
- [SDR YENA2026091800818](https://openairdocs.org/sdr/YENA2026091800818.md): Pressure Blkhd · cracked · Sep 18, 2026 · N523JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE, EA A26-710-01, FR35 PRESSURE BULKHEAD CRACKED - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026040600383](https://openairdocs.org/sdr/YENA2026040600383.md): Lamp · inoperative · Apr 7, 2026 · N523JB · Airbus A320232 · Emergency Lighting
  > FLT 2324, MCO-MCO. OVERHEAD EMERGENCY EXIT LIGHTS OVER R1 AND R2 PARTIALLY ILLUMINATED. REPLACED THE LAMPS OVERHEAD EXIT SIGNS IAW AMM 33-51-16"
- [SDR YENA2026040800381](https://openairdocs.org/sdr/YENA2026040800381.md): Lamp · inoperative · Apr 7, 2026 · N523JB · Airbus A320232 · Emergency Lighting
  > FLT# 2324, MCO-MCO. "OVERHEAD EMERGENCY EXIT LIGHTS OVER R1 AND R2 PARTIALLY ILLUMINATED; REPLAMPED OVER HEAD EXIT SIGNS IAW AMM 33-51-16"
- [SDR YENA2025121501200](https://openairdocs.org/sdr/YENA2025121501200.md): A/C Pack · odor · Dec 14, 2025 · N523JB · Airbus A320232 · Cabin Cooling System
  > FLT#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. OPEN
- [SDR YENA2025102301055](https://openairdocs.org/sdr/YENA2025102301055.md): Lubrication Unit · failed · Oct 22, 2025 · N523JB · Airbus A320232 · APU Oil System
  > FLT#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."
- [SDR YENA2025102301054](https://openairdocs.org/sdr/YENA2025102301054.md): A/C Pack · odor · Oct 21, 2025 · N523JB · Airbus A320232 · Cabin Cooling System
  > FLT#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. "
- [SDR YENA2024052100771](https://openairdocs.org/sdr/YENA2024052100771.md): Radar · failed · May 21, 2024 · N523JB · Airbus A320232 · Weather Radar System
  > FLT#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.'
- [SDR YENA2023122101621](https://openairdocs.org/sdr/YENA2023122101621.md): Unknown · unknown · Dec 18, 2023 · N523JB · Airbus A320232 · Air Distribution System
  > FLT#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-
- [SDR YENA2023101801271](https://openairdocs.org/sdr/YENA2023101801271.md): Unknown · unknown · Oct 15, 2023 · N523JB · Airbus A320232 · Air Distribution System
  > FLT#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 SERVI
- [SDR YENA2023072700872](https://openairdocs.org/sdr/YENA2023072700872.md): Unknown · unknown · Jul 24, 2023 · N523JB · Airbus A320232 · Air Distribution System
  > FLT#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 W
- [SDR YENA2023062700742](https://openairdocs.org/sdr/YENA2023062700742.md): Unknown · unknown · Jun 23, 2023 · N523JB · Airbus A320232 · Flight Control System
  > FLT#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
- [SDR YENA2023060700589](https://openairdocs.org/sdr/YENA2023060700589.md): Unknown · unknown · May 31, 2023 · N523JB · Airbus A320232 · Standard Practices/Structures
  > FLT#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.'
- [SDR YENA2023053000561](https://openairdocs.org/sdr/YENA2023053000561.md): Unknown · unknown · May 26, 2023 · N523JB · Airbus A320232 · Standard Practices/Structures
  > FLT#484, RDU-BOS. 'ON APPROACH BELOW 8K FEET DIRTY DOCK SMELL.' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Next page: https://openairdocs.org/aircraft/N523JB/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N523JB/reports

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