# Service difficulty reports: N568JB

A list on [N568JB](https://openairdocs.org/aircraft/N568JB.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 · 114 reports

- [SDR YENA2026070900558](https://openairdocs.org/sdr/YENA2026070900558.md): Skin · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 (FUSELAGE SIDE SHELL) AFT POSITION BELOW STRG 30 R H SIDE, CRACK DIRECTION: 07 OCLOCK, D1-D2= 0.165 INCH APPROX, AD RELAT ED TASK CARD NO. A320-
- [SDR YENA2026070900557](https://openairdocs.org/sdr/YENA2026070900557.md): Frame · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND (BY ROTOTEST INSPECTION) IN OPEN FASTENER HOLE LOCATED ON FRAME 35 COUPLING AREA BULKHEAD ABOVE STR 30RH, CRACK DIREC TION: 07 OCLOCK, D1-D2= 0.073 INCH APPROX AD RELATED TASK CARD NO. A32 0-53-1372-01. ACCOMPL
- [SDR YENA2026070900556](https://openairdocs.org/sdr/YENA2026070900556.md): Frame · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 6, OPEN FASTENER H OLE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.110 INCH, IN FWD CARGO COMPARTMENT (1 EA)(-Y1292); ACCOMPLISHED REPAIR OF CRACK DAMAGES ON THE CENTE
- [SDR YENA2026070900555](https://openairdocs.org/sdr/YENA2026070900555.md): Floorbeam · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 2 ZONE 2 CRACK LENGTH IS 0.650 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2026-299175 WO 2026 196/1
- [SDR YENA2026070900553](https://openairdocs.org/sdr/YENA2026070900553.md): Floorbeam · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 3 ZONE 2 CRACK LENGTH IS 0.380 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAM
- [SDR YENA2026070900552](https://openairdocs.org/sdr/YENA2026070900552.md): Floorbeam · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 3 ZONE 1 CRACK LENGTH IS 0.850 INCH APPROX, IN FWD CARGO COMPARTMENT. ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON
- [SDR YENA2026070900551](https://openairdocs.org/sdr/YENA2026070900551.md): Floorbeam · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 4 ZONE 2 CRACK LENGTH IS 0.510 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA)(-Y254); ACCOMPLISHED PERMANENT REPAIR OF C
- [SDR YENA2026070900550](https://openairdocs.org/sdr/YENA2026070900550.md): Frame · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 4,OPEN FASTENER HOLE ON ZONE1, CRACK DIRECTION IS 1 OCLOCK, CRACK DEPTH IS 0.095 INCH,IN FWD CARGO COMPARTMENT (1EA)(-Y254); REF AEROMAN WO 2026-196/1 NR 299010 ACCOMPLISHED PERMANENT
- [SDR YENA2026070900549](https://openairdocs.org/sdr/YENA2026070900549.md): Beam · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CENTER WING BOX FRONT SPAR HORIZONTAL BEAMS AT LEVEL FR36 (Y-254)(RADIUS ON ZONE 1) IAW AEROMAN EA 57-0036-26, REV. 0 (COVER PLUS PARTS 1 AND 2); AIRBUS RDAF 81801723/003/2026,
- [SDR YENA2026070900548](https://openairdocs.org/sdr/YENA2026070900548.md): Floorbeam · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 5 ZONE 2 CRACK LENGTH IS 0.520 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN NR 2026 299168 WO 2026 196/1
- [SDR YENA2026070900547](https://openairdocs.org/sdr/YENA2026070900547.md): Frame · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 5 ZONE 1 CRACK LENGTH IS 0.480 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA), REF AEROMAN NR 2026 299167 WO 2026 196/1
- [SDR YENA2026070900546](https://openairdocs.org/sdr/YENA2026070900546.md): Frame · cracked · Jul 5, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 2, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 11 OCLOCK, CRACK DEPTH IS 0.100 INCH, IN FWD CARGO BAY (1 EA)(+Y765). REF AEROMAN NR 2026 299015 WO 2026 196/1 ACCOMPLISHED PERMA
- [SDR YENA2026070900545](https://openairdocs.org/sdr/YENA2026070900545.md): Frame · cracked · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 2, OPEN FASTENER HO LE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.095 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y765); (RESOLVED ON W/O: 1457737 TASKCARD: NR-00041) REF
- [SDR YENA2026070900544](https://openairdocs.org/sdr/YENA2026070900544.md): Frame · cracked · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 3, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.110 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y254); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON T
- [SDR YENA2026070900543](https://openairdocs.org/sdr/YENA2026070900543.md): Frame · cracked · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 3, OPEN FASTENER HO LE ON ZONE 1, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.120 INCH, IN FWD CARGO COMPARTMENT (1 EA)(+Y254); ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON T
- [SDR YENA2026070900542](https://openairdocs.org/sdr/YENA2026070900542.md): Frame · cracked · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 4, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 11 OCLOCK, CRACK DEPTH IS 0.100 INCH, IN FWD CARGO COMPARTMENT (1 EA)(-Y254); (RESOLVED ON W/O: 1457737 TASKCARD: NR-00044) REF
- [SDR YENA2026070900541](https://openairdocs.org/sdr/YENA2026070900541.md): Skin · damaged · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN IN FROM O FFR28 PLUS1.487 IN AT LEVEL STR32 PLUS 1.795 INCH UNDER,LH LOWER FUSELAGE. ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON FR28 PLUS 1.487 IN AT LEVEL STR32 PLUS 1.795 INCH U
- [SDR YENA2026070900540](https://openairdocs.org/sdr/YENA2026070900540.md): Skin · damaged · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR26 PLUS1.681 IN AT LEVEL STR 32 PLUS 2.567 IN UNDER, LT LOWER FUSELAGE. REF AEROMAN WO 2026-196/1NR 299252.ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON EXTERNAL SKIN BTW FR26 PL
- [SDR YENA2026070900539](https://openairdocs.org/sdr/YENA2026070900539.md): Skin · damaged · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR27 TO FR28 AT LEVEL STR32 TO STR33 LH LOWER FUSELAGE;(RESOLVED ON W/O: 1457737 TASKCARD: NR-00047) REF AEROMAN WO 2026 196/1 NR 299041.ACCOMPLISHED REPAIR ON EXISTING REWORK ON EXACT
- [SDR YENA2026070900538](https://openairdocs.org/sdr/YENA2026070900538.md): Skin · damaged · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR 28 TO FR 29 AT LEVEL STR 32 LH LOWER FUSELAGE; (RESOLVED ON W/O: 1457737 TASKCARD: NR-00048) REF AEROMAN WO 2026 196/1 NR 299042 ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON
- [SDR YENA2026070900537](https://openairdocs.org/sdr/YENA2026070900537.md): Skin · damaged · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN BTW FR26 TO FR 27 AT LEVEL STR 32 TO STR 33 LH LOWER FUSELAGE; (RESOLVED ON W/O: 1457737 TASKCARD: NR-00049) REF AEROMAN WO 2026-196/1 NR 299039 ACCOMPLISHED REPAIR ON EXISTING REWORK ON
- [SDR YENA2026070900536](https://openairdocs.org/sdr/YENA2026070900536.md): Skin · damaged · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, EVIDENCE OF REWORK LOCATED ON EXTERNAL SKIN FR27 AT LEVEL STR 32 TO STR 33 LH LOWER FUSELAGE IAW AEROMAN WO 2026-196/1 NR 299040 ACCOMPLISHED REPAIR ON EXISTING REWORK LOCATED ON EXTERNAL SKIN FR27 BTW STR 32LH AND STR 33LH IAW EA 53-
- [SDR YENA2026070900535](https://openairdocs.org/sdr/YENA2026070900535.md): Frame · cracked · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FRAME 36 CWB VERTICAL STRINGER 5,OPEN FASTENER HOLE ON ZONE 2,CRACK DIRECTION IS 12 OCLOCK,CRACK DEPTH IS 0.105 INCH,IN FWD CARGO BAY (1EA)(-Y765) REF AEROMAN WO 2026 196/1 NR 299009 ACCOMPLISHED PERMANENT REPAIR O
- [SDR YENA2026070900534](https://openairdocs.org/sdr/YENA2026070900534.md): Frame · cracked · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 5, OPEN FASTENER HOLEON ZONE 2, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.105 INCH, IN FWD CARGO COMPARTMENT (1EA)(-Y765). (RESOLVED ON W/O: 1457737 TASKCARD: NR-00031) REF AE
- [SDR YENA2026070900533](https://openairdocs.org/sdr/YENA2026070900533.md): Frame · cracked · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER5,OPEN FASTENER HOLEON ZONE1, CRACK DIRECTION IS 12OCLOCK, CRACK DEPTH IS 0.080 INCH, INF WD CARGO COMPARTMENT (1EA)(-Y765: (RESOLVED ON W/O: 1457737 TASKCARD: NR-00029) ACCOMPLISH
- [SDR YENA2026070900532](https://openairdocs.org/sdr/YENA2026070900532.md): Skin · damaged · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, EA A26-514-01. FUSELAGE FWD FUSELAGE EXTERNAL SKIN BTWN FR26-FR29 & STGR 32LH-33LH, EXISTING REWORKS – TIME LIMITED REPAIR(CONSIDERED MAJOR REPAIR)
- [SDR YENA2026070900531](https://openairdocs.org/sdr/YENA2026070900531.md): Floorbeam · cracked · Jul 4, 2026 · N568JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CENTER BOX, FRONT SPAR HORIZONTAL FLOORBEAMS, @ LEVEL OF FR36 & Y-765, Y-254, Y+254, Y+765 & Y-1292. CRACKS PERMANENT REPAIR (CONSIDERED MAJOR REPAIR)
- [SDR YENA2025012900119](https://openairdocs.org/sdr/YENA2025012900119.md): Warning Message · illuminated · Jan 27, 2025 · N568JB · Airbus A320232 · Central Warning
  > FLT#2930, SJU- EWR. (AIRCRAFT PERFORMED AN AIR TURN BACK TO SJU) 'AT FL280 ENG 1 STALL ECAM DISPLAYED MOMENTARILY.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2025012700108](https://openairdocs.org/sdr/YENA2025012700108.md): Wire Harness · damaged · Jan 25, 2025 · N568JB · Airbus A320232 · Fire Protection System Wiring
  > FLT#2390, SJU-EWR. (AIRCRAFT PERFORMED AN AIR TURN BACK TO SJU) 'CLIMBING ABOVE 30,000 HAD ENG 1 STALL. EPR ROLLBACK, ENG STALL ECAM ENGINE RECOVERED WITHOUT REDUCING THRUST. WE HAD ENGINE STALL 4 MORE TIMES INFLIGHT; REPAIR ELEC CONNECTOR ON VSV ACT REF LP 42
- [SDR YENA2025010300007](https://openairdocs.org/sdr/YENA2025010300007.md): Sdac · failed · Dec 28, 2024 · N568JB · Airbus A320232 · Central Warning
  > FLT#2024, MCO-DCA. (AIRCRAFT PERFORMED AN AIRTURN BACK TO MCO) 'FWS SDAC 1 FAULT AFTER TAKEOFF; T/S SYSTEM IAW TSM 31-54-00 FOUND A FAULTY #1 SDAC. REMOVED AND REPLACED SDAC #1 IAW AMM 31-55-34 ALL OPS CHECK OK.'
- [SDR YENA2024100101318](https://openairdocs.org/sdr/YENA2024100101318.md): Duct · contaminated · Sep 26, 2024 · N568JB · Airbus A320232 · Pneumatic Distribution System
  > FLT#2202, FLL-JFK. 'DIRTY SOX SMELL DETECTED DURING DESCENT; REF L/P 4113966-2 (ACCOMPLISHED LEVEL B DECON IAW AMM BLEED DUCT 36-10-00-615-801 & 21-00-615-803) FOR COMPLETION OF LEVEL B DECONTAMTION REF TSM 05-50-00-810-831-A. NO SMELL NOTED. A/C OK FOR SVC.'
- [SDR YENA2024090501227](https://openairdocs.org/sdr/YENA2024090501227.md): Tube · leaking · Sep 3, 2024 · N568JB · Airbus A320232 · APU Oil System
  > FLT#1480, FLL-DCA. 'PREVIOUS I/F CREW REPORTED FUME EVENT ON FINAL DESCENT; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2. IDENTIFIED ODOR CAUSED BY APU-SEE LOGPAGE 4076339, ITEM 1 (INSPECTED APU AND FOUND FRESH OIL AROUND DIFFUSER ASSY AND ELBOW ASSY
- [SDR YENA2024072201016](https://openairdocs.org/sdr/YENA2024072201016.md): Selector Valve · failed · Jul 20, 2024 · N568JB · Airbus A320232 · Landing Gear Position and Warning
  > FLT#673, FLL=PUJ. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL). 'AIR RETURN ECAM L/G DOORS NOT CLOSED CYCLED GEAR TWICE BEFORE ECAM MESSAGE DISAPPEARED; PER TSM 32-31-00-810-836A. REMOVED AND REPLACED ELECTRO-HYDRAULIC SELECTOR GEAR VALVE (40GA) IAW AMM 32-31-
- [SDR YENA2024060300803](https://openairdocs.org/sdr/YENA2024060300803.md): Unknown · fumes · May 31, 2024 · N568JB · Airbus A320232 · Air Distribution System
  > FLT#2903, JFK-SJU. 'INFLIGHT CREW, MULTIPLE NON-REV AND MULTIPLE CUSTOMERS COMPLAINED OF FUMES SMELLING OF DIRTY SOCKS. THEY ALSO COMPLAINED OF BURNING EYES AND SCRATCHY THROAT. THE FUME SMELL WAS CONTINUOUS BELOW 10,000 FT AND UNCOMFORTABLE FOR THEM. THE FUME
- [SDR YENA2024032800477](https://openairdocs.org/sdr/YENA2024032800477.md): Pump · faulted · Mar 27, 2024 · N568JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > FLT#2781, JFK-BZE (AIRCRAFT DIVERTED TO MCO). 'WHILE IN CRUISE, BLUE ELEC PUMP OVHT ECAM MASTER CAUTION; PLEASE REFER TO LOG PAGE 3943375-1 (PERFORMED REMOVAL AND INSTALLATION OF THE ELECTRIC PUMP BLUE HYDRAULIC SYSTEM IAW AMM 29-12-51 OPS CHECK GOOD SYSTEM O
- [SDR YENA2023112001432](https://openairdocs.org/sdr/YENA2023112001432.md): Unknown · unknown · Nov 17, 2023 · N568JB · Airbus A320232 · Air Distribution System
  > FLT#8368, PUJ-JFK. 'FERRY FLIGHT FROM PUJ, SMELL OF DIRTY SOCKS ON DESCENT INTO JFK BETWEEN 11,000FT AND 10,000FT THEN DISAPATED. SMELL OCCURRED AGAIN BETWEEN 4,000FT AND 3,000FT THEN DISAPATED AGAIN. DURING BOTH EVENTS SELECTED PACK #1 OFF AND XBLEED OPEN. OD
- [SDR YENA2023111701401](https://openairdocs.org/sdr/YENA2023111701401.md): Unknown · unknown · Nov 15, 2023 · N568JB · Airbus A320232 · Air Distribution System
  > FLT#2625, RDU-FLL. 'ELECTRICAL ODOR NOTED IN CABIN, BEGINNING IN AFT AND WORKED FORWARD. NOTED AT 15K IN DECENT AND REMAINED TILL LANDING. IMC CONDITIONS ENTIRE TIME; PERFORMED TSM TASK 24-00-00-810-823-A AND 05-50-00-810-831-A. NO ODORS NOTED AT THIS TIME. CO
- [SDR YENA2023080300891](https://openairdocs.org/sdr/YENA2023080300891.md): Unknown · unknown · Aug 2, 2023 · N568JB · Airbus A320232 · Air Conditioning System
  > FLT#2625, RDU-FLL. 'FUME EVENT - OIL FUMES IN COCKPIT AT 8K ' AS THRUST WENT FROM IDLE TO ABOUT 70% N1 & BACK TO IDLE; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B1. FOUND APU WITH EVIDENCE OF OIL LEAK. APU PLACED ON MEL. DECONTAMINATION LEVEL A ACCOMP
- [SDR YENA2023061600662](https://openairdocs.org/sdr/YENA2023061600662.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Auto Flight System
  > DURING HEAVY MAINTENANCE: ACCOMPLISH OPS TEST OF THE LAND CAT III CAPABILITY; C/W AS REQ PER TC #A320-22-97-00-710-001. AIRCRAFT OK FOR CAT III (FO) STATUS.
- [SDR YENA2023061600661](https://openairdocs.org/sdr/YENA2023061600661.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: ACCOMPLISH TASK CARD A320-52-1144-01, EC A320-52-1144 DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (FWD LH EEH) FRAME / REINFORCE DOOR STRUCTURE-MODIFICATION. FOR TRACKING PURPOSES; REF AEROMAN W/O 2023-200/1 NR 2023-252485.
- [SDR YENA2023061600660](https://openairdocs.org/sdr/YENA2023061600660.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 IN FRAME SEGMENT 1, LONGER CRACK LENGTH IS 4.130 INCHES IN AFT FRAME SEGMENT, CONTACT STRUCTURES ENGINEERING, AND AIRBUS PRIOR TO FURTHER ACTION, IN PASSENGER CABIN (5 EA); REF AEROMAN W/O
- [SDR YENA2023061600659](https://openairdocs.org/sdr/YENA2023061600659.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 834 IN FRAME SEGMENT 1, LONGER CRACK LENGTH IS 4.062 INCHES IN FWD FRAME SEGMENT, CONTACT STRUCTURES ENGINEERING, AND AIRBUS PRIOR TO FURTHER ACTION, IN PASSENGER CABIN (4 EA); REF AEROMAN W/O
- [SDR YENA2023061600658](https://openairdocs.org/sdr/YENA2023061600658.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 843 IN AFT FRAME SEGMENT 1, CRACK LENGTH IS 0.700 INCH, IN PASSENGER CABIN (1 EA); REF AEROMAN W/O 2023-200/1 NR 2023-252321. ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 843 FOR REPLACE
- [SDR YENA2023061600657](https://openairdocs.org/sdr/YENA2023061600657.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR 66 LEVEL STRINGER 23L AT AFT GALLEY AREA: REF. AERO NR 2023-252550 - R&R NEW STRUCTURE SECTION CONNECTION LOCATED FR66 LEVEL STRINGER 23L AT AFT GALLEY AREA I.A.W A320 SRM 51-72-1
- [SDR YENA2023061600656](https://openairdocs.org/sdr/YENA2023061600656.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR66 LEVEL STRINGER 23R AT AFT GALLEY AREA; REF. AERO NR 2023-252552- R&R INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR66 LEVEL STRINGER 23R AT AFT GALLEY AREA IAW A320 SRM 51-42-
- [SDR YENA2023061600655](https://openairdocs.org/sdr/YENA2023061600655.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: SHEAR PLATE STR23L AT FR69-70 AFT GALLEY; REF AEROMAN NR 2023-252548 W/O:2023 200/1: R & R SHEAR PLATE STR23L AT FR69-70 AFT GALLEY AREA IAW SRM 51-72-11, 51-42-11, AND DWG D53470100.
- [SDR YENA2023061600654](https://openairdocs.org/sdr/YENA2023061600654.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE FR35 FWD FACE AT LEVEL OF THE STR30L. L=0.500"; REF AEROMAN NR 2023-252426 W/O: 2023 200/1: REPAIRED CRACK @ FR35 PRESSURE BULKHEAD WEB AND STR30L IAW EA53-0169-23, RDAF 81219770/004/2023#A, PARTS 1 AND 2, DWG R53
- [SDR YENA2023061600653](https://openairdocs.org/sdr/YENA2023061600653.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FR16RH DOOR STOP FITTING #7 INBD. UPPER 7 O'CLOCK DIRECTION LOOKING FORWARD; REF AEROMAN NR 2023-252292 W/O:2023 200/1: R & R INTERCOSTAL FITTING ON FR16RH DOOR STOP FITTING #7 IAW SRM 53-11-12-300-010, 51-72-11, 51-42-11, AND
- [SDR YENA2023061600652](https://openairdocs.org/sdr/YENA2023061600652.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: FR16RH DOOR STOP FITTING #7 LOWER INBD FASTENER HOLE 11 O'CLOCK LOOKING FORWARD; REF AEROMAN NR 2023-252293 W/O:2023 200/1: R & R INTERCOSTAL FITTING ON FR16RH DOOR STOP FITTING #7 IAW SRM 53-11-12-300-010, 51-72-11, 51-42-11,
- [SDR YENA2023061600651](https://openairdocs.org/sdr/YENA2023061600651.md): Unknown · unknown · Jun 14, 2023 · N568JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK: OPEN HOLE #5 LOCATED ON FR16RH. CRACK DIRECTION 6 O'CLOCK; REF AEROMAN NR 2023-252299 W/O:2023 200/1: PERFORMED REPAIR HOLE #5 FR16RH IAW JETBLUE EC A23-436-01, DWG R53-13041, EA 53-0212-23 REV 0, AND AIRBUS RDAF 81229902/003/2

Next page: https://openairdocs.org/aircraft/N568JB/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 = 'N568JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N568JB/reports

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