# Service difficulty reports: N623JB

A list on [N623JB](https://openairdocs.org/aircraft/N623JB.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 2 · 66 reports

- [SDR YENA2026071400571](https://openairdocs.org/sdr/YENA2026071400571.md): Filter · odor · Jul 11, 2026 · N623JB · Airbus A320232 · Air Distribution System
  > FLT # 789, DTW-FLL. CREW REPORTED ODOR IN REAR OF CABIN ONLY DURING DESCENT (TRANSIENT) AND TAXI IN. APU ONLY IMMEDIATELY PRIOR TO GATE ARRIVAL; C/W INFO NOTICE 2017-TO15M. R/R L+R OZONE FILTERS IAW AMM 21-55-00 & L+R HEPA CABIN FILTERS IAW AMM 21-21-41DECONT
- [SDR YENA2026070700516](https://openairdocs.org/sdr/YENA2026070700516.md): Unknown · odor · Jul 6, 2026 · N623JB · Airbus A320232 · Air Distribution System
  > FLT # 1468, PBI-HPN. LEVEL 2 FUME EVENT. STRONG PERSISTENT MAGIC MARKER SMELL DESCENDING THROUGH12,000; CLOUDS AND PRECIPITATION IN THE AREA. SMELLED BY BOTH PILOTS, BUT NO F/A. SUSPECT PACK 1. SHUT OFF PACK 1 AND CLOSED X BLEED. SMELL GOT WEAKER AFTER SEVERAL
- [SDR YENA2026062200487](https://openairdocs.org/sdr/YENA2026062200487.md): Unknown · odor · Jun 20, 2026 · N623JB · Airbus A320232 · Air Distribution System
  > FLT 1797 ATL-FLL. DURING DESCENT L280 STRONG ODOR OF INK PENS IN COCKPIT, FA DID NOT SMELL IT LEVEL 2 DISSAPATED WHWN PACK 1 TURNED OFF; COMPLIED WITH INFO NOTICE 2017-T015M REF LOGPAGE 4547023 ITEM #2 FOR LEVEL B ECS DECONTAM ACCOMPLISHED. ENGINE RUNS, BOTH
- [SDR YENA2026052800490](https://openairdocs.org/sdr/YENA2026052800490.md): Apu · odor · May 27, 2026 · N623JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#39, FLL-SJO. "CABIN ODOR ON DESCENT ( APU SYSTEM)" OPEN
- [SDR YENA2026050500446](https://openairdocs.org/sdr/YENA2026050500446.md): Unknown · odor · May 4, 2026 · N623JB · Airbus A320232 · Air Distribution System
  > FLT 580, MBJ-JFK. ODOR OF DITY SOCKS DURING DESENT AND LANDING AND ODOR OF ENG OIL AFTER 2 SHUT DOWN.
- [SDR YENA2026040600382](https://openairdocs.org/sdr/YENA2026040600382.md): A/C Pack · odor · Apr 6, 2026 · N623JB · Airbus A320232 · Cabin Cooling System
  > FLT 1791, PVD-RSW. FUMES PRESENT AFTER TAKEOFF NOTICED IN FLIGHT DECK AND AFT CABIN. ODOR ISOLATION CHECK LIST PERFORMED AND PACK 2 ISOLATED LEVEL 2. APU OFF FUMES RETURNED ON DESCENT. LEVEL 3 SMOKE/ FUMES REMOVAL QRH COMPLETED; ACCOMPLISHED INFO NOTICE 20
- [SDR YEN2026F00003](https://openairdocs.org/sdr/YEN2026F00003.md): A/C Pack · odor · Apr 6, 2026 · N623JB · Airbus A320232 · Cabin Cooling System
  > FLT#1791, PVD-RSW, FUMES PRESENT AFTER TAKEOFF NOTICED IN FLIGHT DECK AND AFT CABIN. ODOR ISOLATION CHECK LIST PERFORMED AND PACK 2 ISOLATED LEVEL 2. APU OFF FUMES RETURNED ON DESCENT. LEVEL 3 SMOKE/ FUMES REMOVAL QRH COMPLETED; ACCOMPLISHED INFO NOTICE 20
- [SDR YENA2026040600376](https://openairdocs.org/sdr/YENA2026040600376.md): Unknown · fumes · Apr 5, 2026 · N623JB · Airbus A320232 · Air Distribution System
  > FLT 1791, PVD-RSW. FUMES PRESENT AFTER TAKEOFF. NOTICED IN FLIGHT DECK AND AFT CABIN. OPEN.
- [SDR YENA2025102801072](https://openairdocs.org/sdr/YENA2025102801072.md): Door Frame · cracked · Oct 27, 2025 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 6 POSITION, CRACK DIRECTION IS 3 OCLOCK, CRACK DEPTH IS 0.095 INCH, AT AFT GALLEY AREA (1 EA); EVALUATED DIAMETER HOLES D1 TO D4 AND FOUND
- [SDR YENA2025102801071](https://openairdocs.org/sdr/YENA2025102801071.md): Door Frame · cracked · Oct 27, 2025 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME SEGMENTS 1 AT DOOR / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT RH SIDE ZONE 844) CRACK LENGTH= 0.2 55 INCHES; REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR DOOR 844 FOLLOWING INST
- [SDR YENA2025102801070](https://openairdocs.org/sdr/YENA2025102801070.md): Door Frame · cracked · Oct 27, 2025 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME SEGMENTS 1 AT DOOR / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT RH SIDE ZONE 843) CRACK LENGTH= 0.2 95 INCHES; REF AEROMAN WO# 2025-262/1 NR# 2025-608615 REMOVED AND REPLACED FRAME SEGMENTS ON
- [SDR YENA2025102801069](https://openairdocs.org/sdr/YENA2025102801069.md): Door Frame · cracked · Oct 27, 2025 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME SEGMENTS 1 AT DOOR / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT LH SIDE ZONE 834) CRACK LENGTH= 0.2 75 INCHES; REF AEROMAN WO@ 2025-262/1 NR# 2025-608616 REMOVED AND REPLACED FRAME SEGMENTS ON
- [SDR YENA2025102801068](https://openairdocs.org/sdr/YENA2025102801068.md): Door Frame · cracked · Oct 27, 2025 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME SEGMENTS 1 AT DOOR / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT LH SIDE ZONE 833) CRACK LENGTH= 0.3 05 INCHES; REF AEROMAN WO 2025-262/1 NR# 2025-608617 REMOVED AND REPLACED FRAME SEGMENTS ON E
- [SDR YENA2025102801067](https://openairdocs.org/sdr/YENA2025102801067.md): Hinge Arm · worn · Oct 27, 2025 · N623JB · Airbus A320232 · Vertical Stabilizer Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: WEAR ON HINGE ARM FORK END FITTING # 6 ON VERTICAL STABILIZER (1EA); REF AEROMAN WO# 2025-262/1 NR# 2025-608758 REMOVED AND REPLACED HINGE ARM FORK END FITTING #6 ON VERTICAL STABILIZER I.A.W. A320 SRM 51-42-11 AND I.A.W A320 SRM 55-3
- [SDR YENA2025102801066](https://openairdocs.org/sdr/YENA2025102801066.md): Door Frame · cracked · Oct 27, 2025 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.115 INCH, AT AFT GALLEY AREA (1 EA); REF AEROMAN WO# 2025-262/1 NR2025-608762 PER
- [SDR YENA2025041000384](https://openairdocs.org/sdr/YENA2025041000384.md): Secu · failed · Apr 4, 2025 · N623JB · Airbus A320232 · Drag Control System
  > FLT# 548, TPA-HPN. (AIRCRAFT DIVERTED TO JFK). 'FLT CTL GRD SPOILER # 2 FAULT SPOILER 1& 2 DID NOT DISPLAYED ON LANDING; REMOVED AND REPLACED OF THE SEC 3 COMPUTER OPS CHECK PASS REF AMM 27-94-34-400-001A OPERATIONAL TEST REF AMM 27-94-00-710-001A.'
- [SDR YENA2025033100344](https://openairdocs.org/sdr/YENA2025033100344.md): Unknown · odor · Mar 28, 2025 · N623JB · Airbus A320232 · Air Distribution System
  > FLT#1453, FLL-SJU. 'VOMIT / RANCID SMELL ON TAKE OFF ROLL; PERFORMED DECONTAMINATION BOTH PACKS AND REPLACEMENT BOTH EPA FILTER ALSO PACK BURN ALSO OPEN APU CLEAN WITH ALCOHOL RUN INSPECTED NO LEAK AT THIS TIME CLOSED AND SECURED BOTH DOORS AS PER INFO.NOTICE
- [SDR YENA2024091101261](https://openairdocs.org/sdr/YENA2024091101261.md): Slide · no test · Sep 9, 2024 · N623JB · Airbus A320232 · Escape Slide
  > FLT#40, MDE-FLL. 'REF. LOGPAGE 4059972 ITEM #1. FWD EPSU INTERIOR / EXTERIOR LIGHT FAULT; PERFORMED TSM TASK 33-51-00-810-808-A. REPLACED FWD R/H ESCAPE SLIDE PER M/M 25-62-44. OPS CHECK GOOD OF EPSU 10WL PER M/M 33-51-00.'
- [SDR YENA2024091101260](https://openairdocs.org/sdr/YENA2024091101260.md): Slide · no test · Sep 9, 2024 · N623JB · Airbus A320232 · Escape Slide
  > FLT#40, MDE-FLL. 'REF TASK CARD # A320-33-51-00-710-003 EMERGENCY BATTERY TEST FIN 10 WL NEEDS REPLACEMENT; REPLACED EMERGENCY BATTERY ON FIN 10WL IN REF TO AMM 33-51-8 TEST FAILED P/N TRANS C/W UNDER W.O # 1358429 FURTHER T/S REQUIRED.'
- [SDR YENA2024091101259](https://openairdocs.org/sdr/YENA2024091101259.md): Slide · no test · Sep 9, 2024 · N623JB · Airbus A320232 · Escape Slide
  > FLT#40, MDE-FLL. 'REF TASK CARD # A320-33-51-00-710-003 EMERGENCY BATTERY TEST & LP 4059972-1 (REFERRED TO LOG PAGE 4059975-1 FOR R/R R1 SLIDE & LOGPAGE 4059975-2 (PERFORMED TSM, TASK 33-51-00-310-808-A, REPLACED AFT L/H L2 ESCAPE SLIDE PER AMM 25-62-44 OPS CH
- [SDR YENA2024091101256](https://openairdocs.org/sdr/YENA2024091101256.md): Slide · no test · Sep 9, 2024 · N623JB · Airbus A320232 · Escape Slide
  > FLT#40, MDE-FLL. 'REF TASK CARD # A320-33-51-00-710-003 EMERGENCY BATTERY TEST FIN 11WL NEEDS REPLACEMENT; REPLACED EMERGENCY BATTERY ON FIN 11WL IN REF TO AMM 33-51-38 TEST OK P/N TRANS C/W UNDER W.O 1358429.'
- [SDR YENA2024091101255](https://openairdocs.org/sdr/YENA2024091101255.md): Slide Raft · no test · Sep 9, 2024 · N623JB · Airbus A320232 · Escape Slide
  > FLT#40, MDE-FLL. 'WHILE PERFORMING TASK # A320-33-51-00-710-003 CHECK OF EMERGENCY BATTERY CHK FOUND AFT & FWD EPSU INTERIOR,EXTERIOR LIGHT FAULT; REFERED TO LOG PAGE 4059975-1 FOR REMOVED AND REPLACED R1 SLIDE & LOGPAGE 4059975-2 (PERFORMED TSM, TASK 33-51-00
- [SDR YENA2024091101254](https://openairdocs.org/sdr/YENA2024091101254.md): Battery · no test · Sep 9, 2024 · N623JB · Airbus A320232 · Emergency Lighting
  > FLT#40, MDE-FLL. 'REF TASK CARD # A320-33-51-00-710-003 EMERGENCY BATTERY TEST FIN 12WL NEEDS REPLACED; REPLACED EMERGENCY BATTERY ON FIN 12WL IN REF TO AMM 33-51-38 TEST OK P/N TRANS C/W UNDER WO # 1358429.'
- [SDR YENA2024082101130](https://openairdocs.org/sdr/YENA2024082101130.md): Unknown · odor · Aug 19, 2024 · N623JB · Airbus A320232 · Air Distribution System
  > FLT#362, SJU-BOS. 'INFLIGHT CREW REPORTED BURNING SMELL NEAR ROW 13 DURING CRUISE. SMELL DISSIPATED AFTER FEW MINUTES FDU POWER BUTTON WAS TURNED OFF; COMPLIED WITH INFO NOTICE 2017.TO15, SECTION A ISOLATED FAULT TO TYPE 10 BURING SMELL PER TSM 05-50-00-810-0
- [SDR YENA2024020800252](https://openairdocs.org/sdr/YENA2024020800252.md): Unknown · odor · Feb 7, 2024 · N623JB · Airbus A320232 · Air Distribution System
  > FLT#761, LGA-PBI. ' DESCENDING THROUGH ABOUT 5000' INFLIGHT CALLED AND ADVISED OF A DIRTY SOCK ODOR MID CABIN AND AFT; BAGGED LOAD COMPRESSOR DRAIN NO FINDINGS. CLEANED APU INTAKE DUCT AND THOROUGHLY CLEANED INTAKE SEAL COMPARTMENT & DOOR INSPECTED IAW 49-00-2
- [SDR YENA2024012400097](https://openairdocs.org/sdr/YENA2024012400097.md): Unknown · odor · Jan 23, 2024 · N623JB · Airbus A320232 · Air Distribution System
  > FLT#613, HPN-FLL. 'LEVEL II FUME EVENT.STRONG PERSISTENT FOUL ODOR FROM TOD ALL THE WAY THROUGH LANDING. SMELLED BY ALL FLIGHT CREW. ( APU SYSTEM).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024011100024](https://openairdocs.org/sdr/YENA2024011100024.md): Unknown · unknown · Jan 10, 2024 · N623JB · Airbus A320232 · Air Distribution System
  > FLT#171, LGA-FLL. 'CABIN ODOR DURING INITIAL CLIMB AND DESCENDING THRU 10,000 MUSTY ODOR ONLY ON FLIGHT DECK; COMPLIED WITH INFO NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10 (A), 1C PER TSM 05-50-00-810-835-B/ TSM 05-50-810-085-D. AIRCRAFT IS OK FOR
- [SDR YENA2023111701400](https://openairdocs.org/sdr/YENA2023111701400.md): Unknown · unknown · Nov 14, 2023 · N623JB · Airbus A320232 · Dependent Position Determining System
  > FLT#627, JFK-POP. (AIRCRAFT DIVERTED TO FLL) ' NAV ADS-B RPTG 1 FAULT ON ECAM. ADS-B RPTG 2 FAULT ON ECAM. FAULT INTERMITTENTLY CORRECTED ITSELF WHEN WE EXITED OCEANIC AIRSPACE. ( AUTOMATIC DEPENDENT SURVEILLANCE BROADCAST (ADS-B) SYSTEM).' (SUPPLEMENTAL INF
- [SDR YENA2023111001364](https://openairdocs.org/sdr/YENA2023111001364.md): Unknown · unknown · Nov 8, 2023 · N623JB · Airbus A320232 · Air Distribution System
  > FLT#2465, BUF-FLL. 'DIRTY SOCK SMELL PASSING 8000 A ON ARRIVAL TO FLL; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10 (A), 1, C PER TSM 05-50-00-810-085 B.'
- [SDR YENA2023081100933](https://openairdocs.org/sdr/YENA2023081100933.md): Unknown · unknown · Aug 10, 2023 · N623JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#869, JFK-PUJ. ' AIRSTAIRS STRUCK THE AIRCRAFT AT THE L1 DOOR, AFTER OPENING THE L1 DOOR WE WERE TOLD BY PUJ GROUND PERSONAL THE AIRSTAIR PUT A DENT ON THE AIRCRAFT; DAMAGE WITHIN LIMITS IAW SRM TASK 53-11-11-283-012, FIGURE 007 SHEET 9/10 ZONE 1 AREA 1. DE
- [SDR YENA2023062700735](https://openairdocs.org/sdr/YENA2023062700735.md): Slide Raft · deployed · Jun 24, 2023 · N623JB · Airbus A320232 · Escape Slide
  > FLT#1334, SJU-MCO. 'R-2 AFT SLIDE DEPLOYED, BY INFLIGHT CABIN CREW MEMBER; REMOVED AND REPLACED AFT R/H SLIDE IAW AMM CH 25-62-44, SERVICED ASSIST BOTTLE & REPLACED DIAPHRAGM IN THE PERCUSSION MECHANISM IAW 52-10-00.'
- [SDR YENA2022121501255](https://openairdocs.org/sdr/YENA2022121501255.md): Frame · cracked · Dec 14, 2022 · N623JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 4LH UPPER SIDE POST ATTACHMENT OPEN FASTENER HOLE IN VERTICAL FLANGE, CRACK DIRECTION IS 2 O'CLOCK; REF: ARM W/O 2022 450/1 N/R 2022-639660. REPAIRED IAW AEROMAN EA# 53-0589-22 REV 0 (COVER PLUS PART 1) AND A
- [SDR YENA2022121501254](https://openairdocs.org/sdr/YENA2022121501254.md): Stringer · corroded · Dec 14, 2022 · N623JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION: STR 32L FR59 AFT CARGO; REF AEROMAN NR 2022-639768 W/O:2022 450/1: ACCOMPLISHED PERMANENT REPAIR ON STR 32L FR59LH AFT CARGO IAW SRM 53-00-13-300-001 FIG 001 SH1. REQUIRES INSP AT 60,000FC / 120,000FH (FROM EMBODIMENT) WITH
- [SDR YENA2022121501253](https://openairdocs.org/sdr/YENA2022121501253.md): Intercostal · cracked · Dec 14, 2022 · N623JB · Airbus A320232 · Passenger/Crew Doors
  > DURING HEAVY MAINTENANCE: CRACK: FR16LH INTERCOSTAL FASTENER HOLE 3 AT DOOR STOP FITTING 7; REF AEROMAN NR 2022-639641 W/O:2022 450/1: REMOVED AND REPLACED INTERCOSTAL DOOR STOP FITTING 7 AND FASTENERS FR16RH IAW SRM 51-42-11, 51-72-11, DWG D53112300 & D531144
- [SDR YENA2022121501252](https://openairdocs.org/sdr/YENA2022121501252.md): Intercostal · cracked · Dec 14, 2022 · N623JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK: FR16RH INTERCOSTAL FASTENER HOLE 3 AT DOOR STOP FITTING 7; REF AEROMAN NR 2022-639640 W/O:2022 450/1: REMOVED AND REPLACED INTERCOSTAL DOOR STOP FITTING 7 AND FASTENERS FR16RH IAW SRM 51-42-11, 51-72-11, DWG D53112300 & D531144
- [SDR YENA2022121501251](https://openairdocs.org/sdr/YENA2022121501251.md): Intercostal · cracked · Dec 14, 2022 · N623JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK: FR16RH INTERCOSTAL AND STOP FITTINGS 7 HOLE 2; REF AEROMAN NR 2022 - 639639 W/O:2022 450/1: REMOVED AND REPLACED INTERCOSTAL FITTING, DOOR STOP FITTING 7 AND FASTENERS FR16 RH IAW A320 SRM 51-42-11 AND SRM 51-72-11, DWG D531123
- [SDR YENA2020042280317](https://openairdocs.org/sdr/YENA2020042280317.md): Stringer · corroded · Apr 18, 2020 · N623JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION STRINGER 44 FRAME 33+ 18 INCHES IN FWD CARGO COMPARTMENT; (REF AEROMAN N/R 2020-100319) PERFORMED PERMANENT REPAIR LOCATED BTW FR 32 TO FR 35 IAW SRM A320- 53-00-13-300-001 AND SRM 51-72-11 AND DRAWING D53231712. REPAIR IS C
- [SDR YENA2020042280316](https://openairdocs.org/sdr/YENA2020042280316.md): Shear Plate · cracked · Apr 18, 2020 · N623JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CRACK WAS FOUND AT KEEL BEAM SHEAR PLATE PANEL PER INSPECTIONS CONTAINED ON REF /4/ SB WHICH REQUIRES AIRBUS TO BE CONTACTED IF A CRACK IS FOUND AFTER TI-ANGLE REMOVAL AND INSPECTION OF THE AFFECTED HOLES ON THE FUSELAGE (SEE REF /1/
- [SDR YENA2020042280315](https://openairdocs.org/sdr/YENA2020042280315.md): Skin · dented · Apr 18, 2020 · N623JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, DENT EXTERNAL SKIN LOC FR 4 TO FR 5 AND 5 INCHES BELOW R/H SIDE STRINGER AT LOWER FUSELAGE; REF AEROMAN N/R 2020-100283, PERFORMED PERMANENT REPAIR IAW EC NO. A20-401-01 AND EA # 53-0291-20 PART 1 AND PART 2 AND AIRBUS RDAS 8076776010
- [SDR YENA2019100493558](https://openairdocs.org/sdr/YENA2019100493558.md): Battery Pack · no test · Sep 30, 2019 · N623JB · Airbus A320232 · Emergency Lighting
  > FT # 391, EPSU BATTERY EMER R/H BATTERY FAIL TEST; REMOVED AND REPLACED EPSU EMER R BATTERY PER AMM 33-51-38.
- [SDR YENA201806240925](https://openairdocs.org/sdr/YENA201806240925.md): Skin · dented · Jun 24, 2018 · N623JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING CURRENT (6/2018) C7 HEAVY CHECK AT LHT-PR, REPORTED WITH A DENT AT REAR FUSELAGE BETWEEN FR 63 AND 64, STGR 4L AND 5L MEASURING 67MM L X 46MM W X 2.6MM D (SEE REF /1/ EO FOR DETAILS). THIS AREA IS CLASSIFIED AS AN EXLUDED AREA WITHOUT REPAIR ALLOWANCES,
- [SDR YENA201803140966](https://openairdocs.org/sdr/YENA201803140966.md): Skin · warped · Mar 14, 2018 · N623JB · Airbus A320232 · Landing Gear Doors
  > THE RT MLG DOOR (P/N D5288016500500 SN FB3911) WAS FOUND WITH THE OUTER CONTOUR DISTORTED/WARPED. THE DOOR WAS SENT FOR REPAIR AND COULD NOT SUPPORT. SUBSEQUENTLY THE MLG DOOR WAS SENT FOR REPAIR UNDER RO2060418 (WO:W13081). ASSESSED THE DAMAGE AND DEVELOPED A
- [SDR YENA201710030814](https://openairdocs.org/sdr/YENA201710030814.md): Unknown · unknown · Oct 3, 2017 · N623JB · Airbus A320232 · Emergency Lighting
  > ALL EMERGENCY EXIT LIGHTS ILLUMINATED AFTER FIRST ENGINE START WHILE ON THE GROUND. TROUBLESHOOT THE SYSTEM AND PERFORMED ENGINE RUN IAW AMM 71-00-00 AND SYSTEM BITE TEST IAW AMM 35-50-00. COULD NOT DUPLICATE FAULT. ACFT OK FOR SERVICE.
- [SDR YENA201611111003](https://openairdocs.org/sdr/YENA201611111003.md): Door Frame · corroded · Nov 11, 2016 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON R1 PAX DOOR LOWER CUT OUT CORNER INTERNAL STRUCTURE FRAME 16+2 STR 23R. CORROSION WAS REMOVED. SPOT FACED AT R1 FWD GIRT BAR LATCH HOLES. INSTALLED BUSHINGS AND REPAIR WASHERS IAW SRM 53-11-14.
- [SDR YENA201611111008](https://openairdocs.org/sdr/YENA201611111008.md): Fitting · corroded · Nov 11, 2016 · N623JB · Airbus A320232 · Emergency Equipment
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON L2 CREW DOOR AFT GIRT BAR FITTING; R & R DOOR LWR SILL IAW A320 SRM 51-72-11, 53-41-14-283-002, 53-41-14.
- [SDR YENA201611111007](https://openairdocs.org/sdr/YENA201611111007.md): Fitting · corroded · Nov 11, 2016 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON L2 DOOR CORNER FITTING AT FRAME 68. R & R CORNER FITTING AND INSTALLED IAW SRM 51-72-11.
- [SDR YENA201611111006](https://openairdocs.org/sdr/YENA201611111006.md): Floorbeam · corroded · Nov 11, 2016 · N623JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN WET AREA FLOORBEAM Y1292 FRAME 69; R & R THE FLOORBEAM IAW SRM 51-72-11- PG 3-4 AND 51-42-11-PG 1-10.
- [SDR YENA201611111005](https://openairdocs.org/sdr/YENA201611111005.md): Floorbeam · corroded · Nov 11, 2016 · N623JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN WET AREA FLOORBEAM Y1292 FRAME 66. REMOVED AND REPLACED IAW SRM 51-72-11.
- [SDR YENA201611111004](https://openairdocs.org/sdr/YENA201611111004.md): Door Frame · corroded · Nov 11, 2016 · N623JB · Airbus A320232 · Fuselage Main, Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON R1 DOOR LOWER CUT OUT CORNER INTERNAL STRUCTURE FRAME 19+6 STR 23RH 4 EA AROUND THE FASTERNERS HOLES (FWD GIRT BAR AFT I/B HOLE, AFT O/B HOLE, FWD I/B HOLE, FWD O/B HOLE); REMOVED CORROSION BY SPOT FAC
- [SDR YENA201611111002](https://openairdocs.org/sdr/YENA201611111002.md): Floor Support · corroded · Nov 11, 2016 · N623JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN WET AREA FLOOR SUPPORT Y-254 FRAME 70; R & R THE FLOOR SUPPORT IAW SRM 53-00-14-283-002 AND SRM 51-75-12.

Next page: https://openairdocs.org/aircraft/N623JB/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 = 'N623JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N623JB/reports

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