# Service difficulty reports: N588JB A list on [N588JB](https://openairdocs.org/aircraft/N588JB.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 · 126 reports - [SDR YENA2026101500974](https://openairdocs.org/sdr/YENA2026101500974.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450763. CRACK INDICATION FOUND ON FASTENER HOLE #5 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 12 O'CLOCK LOOKING AFT. CRACK D = 0.172 INCHES.; "(RESOLVED ON W/O: 1486589 TASK - [SDR YENA2026101500973](https://openairdocs.org/sdr/YENA2026101500973.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450762. CRACK INDICATION FOUND ON FASTENER HOLE #6 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 1 O'CLOCK LOOKING AFT. CRACK D= 0.145 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCA - [SDR YENA2026101500972](https://openairdocs.org/sdr/YENA2026101500972.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450761. CRACK INDICATION FOUND ON FASTENER HOLE #7 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 6 O'CLOCK LOOKING AFT. CRACK D= 0.141 INCHES;"(RESOLVED ON W/O: 1486589 TASKCARD - [SDR YENA2026101500971](https://openairdocs.org/sdr/YENA2026101500971.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450562. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 7 ( CPCP FINDING).; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00043) REF AEROMAN WO# 2026-228/1. NR# 2026-450562. ACCOMPLI - [SDR YENA2026101500970](https://openairdocs.org/sdr/YENA2026101500970.md): Skin · damaged · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE FOR A/C N558JB - SRM REPAIR SURVEY, DEFECT 4400 62-29919; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00047) REF AEROMAN WO 2026-228/1 NR # 2026-450636 COMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER - [SDR YENA2026101500969](https://openairdocs.org/sdr/YENA2026101500969.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00049) REF AEROMAN WO # 2026-228/1 NR # 2026-450566 ACCOMPLISHED REPAIR OF THE LH WING TOP SK - [SDR YENA2026101500968](https://openairdocs.org/sdr/YENA2026101500968.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00050) REF AEROMAN 2026 228/1 NR2026-450552 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWE - [SDR YENA2026101500967](https://openairdocs.org/sdr/YENA2026101500967.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00051) REF AEROMAN WO # 2026-228/1 NR # 2026-450544 ACOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH - [SDR YENA2026101500966](https://openairdocs.org/sdr/YENA2026101500966.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450569. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 13 PLUS 3 INCHES. (CPCP FINDING).; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00052) REF AEROMAN WO# 2026-228/1. NR# 2026-45 - [SDR YENA2026101500965](https://openairdocs.org/sdr/YENA2026101500965.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDING; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00053) REF AEROMAN WO # 2026-228/1 NR # 2026-450553 ACCOMPLISHED REPAIR OF THE LH WING TOP SKI - [SDR YENA2026101500964](https://openairdocs.org/sdr/YENA2026101500964.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450551. CORROSION ON LH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 PLUS 16 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00054) REF AEROMAN WO# 2026-228/1. NR# 2026-450551. ACCOMPLISH - [SDR YENA2026101500963](https://openairdocs.org/sdr/YENA2026101500963.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Leading Edge Devices > DURING HEAVY MAINTENANCE, CORROSION ON SLAT 1 UPPER SURFACE ON LH WING; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00055) REF AEROMAN WO 2026 228/1 NR 2026-450462. REPAIRED SLAT 1 UPPER SURFACE ON LH WING IAW EC NO. A26-840-01, EA # 57-0089-26 REV 0 AND # 57-008 - [SDR YENA2026101500962](https://openairdocs.org/sdr/YENA2026101500962.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING); "REF AEROMAN 2026 228/1 NR2026-450552 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDANCE WITH AEROMAN E - [SDR YENA2026101500961](https://openairdocs.org/sdr/YENA2026101500961.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDING); "REF AEROMAN WO # 2026-228/1 NR # 2026-450566 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORD - [SDR YENA2026101500960](https://openairdocs.org/sdr/YENA2026101500960.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING); "REF AEROMAN WO # 2026-228/1 NR # 2026-450544 ACOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDANCE WITH AEROM - [SDR YENA2026101500959](https://openairdocs.org/sdr/YENA2026101500959.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDING; REF AEROMAN WO # 2026-228/1 NR # 2026-450553 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TE OH LOWER SURFACE RIB 9-18 IN ACCORDAN - [SDR YENA2026101500958](https://openairdocs.org/sdr/YENA2026101500958.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, EA A26-876-01 WING / LH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 9-18 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR) - [SDR YENA2026101500957](https://openairdocs.org/sdr/YENA2026101500957.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE, EA A26-816-01 FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 LHS / ATTACHMENT HOLES / CRACKS – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR) - [SDR YENA2026101500956](https://openairdocs.org/sdr/YENA2026101500956.md): Frame · damaged · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Frame > DURING HEAVY MAINTENANCE, EA A26-843-01 FUSELAGE / NOSE FWD FUSELAGE / FR16 RHS / DOUBLE JOGGLE AREA / HOLE #6 / CRACK DAMAGE – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR) - [SDR YENA2026101500955](https://openairdocs.org/sdr/YENA2026101500955.md): Pressure Blkhd · damaged · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Bulkhead > DURING HEAVY MAINTENANCE, EA A26-842-01 FUSELAGE / CENTER FUSELAGE / FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT / @ LEVEL OF STGR 30LH / FASTENER HOLES W1 & H2 / CRACK DAMAGE – TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR) - [SDR YENA2026101500954](https://openairdocs.org/sdr/YENA2026101500954.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, EA 26-872-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 13 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR) - [SDR YENA2026101500953](https://openairdocs.org/sdr/YENA2026101500953.md): Floorbeam · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE, EA 26-807-01 WINGS / CENTER WING / FRONT SPAR / VERTICAL STRINGERS & HORIZONTAL FLOOR BEAMS / Y±254, Y±765, AND Y±1292 / AT FR36 / CRACKS (SB 57-1178) – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR) - [SDR YENA2026101500952](https://openairdocs.org/sdr/YENA2026101500952.md): Pressure Panel · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure > DURING HEAVY MAINTENANCE, EA 26-817-01 FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR) - [SDR YENA2026100200921](https://openairdocs.org/sdr/YENA2026100200921.md): Ife Equipment · odor · Oct 1, 2026 · N588JB · Airbus A320232 · Audio Integrating System > FLT 1033, MCO-SJU. REF LOG PAGE 4702454 ITEM 1. DURING CLIMB FA REPORT ELECTRICAL ODOR. COMPLIED WITH INFORMATION NOTICE 2017-T015N. IDENTIFIED ODOR AS A TYPE 9, FOLLOWED TSM 05-50-00-810-085-B. ITEM FOUND TO BE FROM THE IFE SYST. PLACED ON NEF N44-20-02E REF - [SDR YENA2026092300899](https://openairdocs.org/sdr/YENA2026092300899.md): Pylon · no discrepancy · Sep 21, 2026 · N588JB · Airbus A320232 · Standard Practices/Structures > DURING HEAVY MAINTENANCE, ELONGATED CENTER HOLE ENTRANCE AFT POSITION PYRAMID MATING FACE FWD MOUNT ON RH PYLON; (RESOLVED ON W/O: 1477496 TASKCARD: NR-00012) FUR-A320-54-03371, REF AEROMAN N/R 2026-432556, PERFORMED DETAIL VISUAL INSPECTION ON CENTER HOLE EN - [SDR YENA202609230089](https://openairdocs.org/sdr/YENA202609230089.md): Pylon · no discrepancy · Sep 21, 2026 · N588JB · Airbus A320232 · Standard Practices/Structures > DURING HEAVY MAINTENANCE, ELONGATED CENTER HOLE ON FWD MOUNT OF RT PYLON. PERFORMED DETAIL VISUAL INSPECTION ON CENTER HOLE ENTRANCE AFT POSITION PYRAMID MATING FACE FWD MOUNT ON RT PYLON IAW NTM 51-90-00 AND FOUND NO ELONGATED HOLE ONLY FOUND EXISTING REWORK - [SDR YENA2026092300898](https://openairdocs.org/sdr/YENA2026092300898.md): Floor Support · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORRODED FLOOR SUPPORT +Y1292, BTWN FR 12 - 24. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11-911-001, DWG D53112813, & DWG D53110876. - [SDR YENA2026092300897](https://openairdocs.org/sdr/YENA2026092300897.md): Floor Support · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORRODED FLOOR SUPPORT, BTWN FR 12 - 24. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11-911-001, DWG D53112813, AND DWG D53110876. - [SDR YENA2026092300896](https://openairdocs.org/sdr/YENA2026092300896.md): Floor Support · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION FLOOR SUPPORT +Y765. REMOVED AND REPLACED THE FLOOR SUPPORT BTWN FR 66 - 70 IAW SRM 51-72-11, SRM 51-42-11, DWG D53472794, DWG D53472777, AND DWG 53472809804. - [SDR YENA2026092300895](https://openairdocs.org/sdr/YENA2026092300895.md): Frame · cracked · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Frame > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE C LOCATED AT DOUBLE JOGGLE AREA, FR16 RT SIDE. CRACK DIRECTION IS 9 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERFORMED - [SDR YENA2026092300894](https://openairdocs.org/sdr/YENA2026092300894.md): Frame · cracked · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Frame > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND IN HOLE 7 LOCATED AT DOUBLE JOGGLE AREA, FR 20 R H SIDE. CRACK DIRECTION IS 3 OCLOCK VIEW FROM OUTSIDE. CRACK DEPTH IS 0.165 INCH APPROX. CONFIRM CRACK INDICATION USING BOROSCOPE VIEW IAW NTM 51-90-00. PERMANE - [SDR YENA2026092300893](https://openairdocs.org/sdr/YENA2026092300893.md): Frame · cracked · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Frame > DURING HEAVY MAINTENANCE, A CRACK INDICATION WAS FOUND IN HOLE B IN DOUBLE JOGGLE AREA, FR 16. CRACK DIRECTION IS 3 OCLOCK VIEWED FROM OUTSIDE. CONFIRMED CRACK INDICATION USING BOROSCOPE IAW NTM 51-90-00. PERFORMED A PERMANENT REPAIR OF FRAME 16 IAW SRM 53 - [SDR YENA2026092300892](https://openairdocs.org/sdr/YENA2026092300892.md): Floor Support · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION FLOOR SUPPORT -Y464.8 IN AFT GALLEY. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, & SRM 51-42-11. - [SDR YENA2026092300891](https://openairdocs.org/sdr/YENA2026092300891.md): Floorbeam · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE, CORROSION ON FLOORBEAM -Y765 IN THE AFT GALLEY AREA. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-72-11, SRM 51- 42-11, DWG D53472809, DWG D53472777, & DWG D53472195. - [SDR YENA2026092300890](https://openairdocs.org/sdr/YENA2026092300890.md): Fitting · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Attach Fittings > DURING HEAVY MAINTENANCE, CORRODED CENTER FITTING, BTWN FR 66 - 68, STR 23R. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53480505. - [SDR YENA2026092300889](https://openairdocs.org/sdr/YENA2026092300889.md): Shear Plate · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION SHEAR PLATE BTWN FRAMES 69 TO 70, STR 23R. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11, SRM 51-42-11, & DWG D53474180. - [SDR YENA2026092300888](https://openairdocs.org/sdr/YENA2026092300888.md): Skin · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION ON EXTERNAL SKIN UPPER SURFACE BTWN RIBS 2 & 3, STR 11 RT WING. TOOK MEASURES OF CORROSION L= 1.023 IN, W= 0.826 IN, MEASURES AFTER REWORK ARE L= 2.780 IN, W= 2.418 IN. EVALUATED REWORK ON SKIN & FOUND WITHIN LIMITS IAW S - [SDR YENA2026092300887](https://openairdocs.org/sdr/YENA2026092300887.md): Skin · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION UPPER SKIN, BTWN RIBS 8 & 9, LT WING T/E. MEASURES OF CORROSION ARE L=3.377IN W=1.465IN, REWORKED CORROSION ON LT WING UPPER SKIN IAW SRM 51-74-00 AND MEASURES AFTER REWORK ARE P1 L=4.042IN, W=2.842IN, EVALUATED REWORK & - [SDR YENA2026092300886](https://openairdocs.org/sdr/YENA2026092300886.md): Skin · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION ON UPPER SKIN, BTWN RIBS 6 - 7, STRINGER 11, LT WING. REWORKED POINTS OF CORROSION (3E/A) IAW SRM 51-74-00, MEASURES OF POINTS OF CORROSION AFTER REWORK ARE P1 L= 1.858 IN, W= 1.232 IN, P2 L= 2.063 IN, W= 1.354, P3 L= 2.1 - [SDR YENA2026092300885](https://openairdocs.org/sdr/YENA2026092300885.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, CORROSION ON STRINGER 30L, BTWN FR 61 - 62, IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 30L IAW SRM 53-00-13-300-001. THIS REPAIR IS CAT B. - [SDR YENA2026092300884](https://openairdocs.org/sdr/YENA2026092300884.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L, BTWN FR 57 - 59 IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 57 - 58 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B. - [SDR YENA2026092300883](https://openairdocs.org/sdr/YENA2026092300883.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L, BTWN FR 60 - 61. IN AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 60 +14 INCHES, & 2 INCHES AFT FACE OF FR 61 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B. - [SDR YENA2026092300882](https://openairdocs.org/sdr/YENA2026092300882.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, CORROSION ON STRINGER 32L. BTWN FR 60 - 61 IN THE CARGO BAY. PERFORMED A REPAIR ON STRINGER 32L, BTWN FR 60 + 14 INCHES & 2 INCHES AFT FACE FR 61 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B. - [SDR YENA2026092300881](https://openairdocs.org/sdr/YENA2026092300881.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, CORROSION IN STRINGER 33L, FR57 - 58 IN THE AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 33L BTWN FR 57 - 58 IAW SRM 53-00-13-300-001. THIS REPAIR IS CLASSIFIED CATEGORY B. - [SDR YENA2026092300880](https://openairdocs.org/sdr/YENA2026092300880.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, CORROSION STRINGER 33L LOCATED AT FR59 IN AFT CARGO BAY. PERFORMED A REPAIR ON STRINGER 33L, FR 59 IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B, - [SDR YENA2026092300879](https://openairdocs.org/sdr/YENA2026092300879.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, STRINGER 36L CORRODED, BTWN FR 57 - 58. REPAIRED STRINGER 36L AND FR57 PLUS 18 INCHES IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B. - [SDR YENA2026092300878](https://openairdocs.org/sdr/YENA2026092300878.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, CORRODED STRINGER 37L, BTWN FRAMES 56 & 57. REPAIRED THE STRINGER 37L AND 15 INCHES PLUS FR56, IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B. - [SDR YENA2026092300877](https://openairdocs.org/sdr/YENA2026092300877.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, STRINGER 43L CORRODED BTWN FR 56 - 58. REPAIRED STRINGER 37L IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B. - [SDR YEN2026F00005](https://openairdocs.org/sdr/YEN2026F00005.md): Stringer · corroded · Sep 21, 2026 · N588JB · Airbus A320232 · Fuselage Main, Longeron/Stringer > DURING HEAVY MAINTENANCE, STRINGER 43L CORRODED, BTWN FRAMES 56 - 58. REPAIR STRINGER 37L, IAW SRM 53-00-13-300-001, THIS REPAIR IS CLASSIFIED CATEGORY B. - [SDR YENA2026092300876](https://openairdocs.org/sdr/YENA2026092300876.md): Skin · damaged · Sep 21, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin > DURING HEAVY MAINTENANCE, ELONGATED HOLE LOWER SKIN BTWN RIBS 18 - 19, RT WING. PERFORMED A REPAIR TO THE RT WING SKIN. IAW SRM 57-27-11-283-002, AND SRM 57-21-11-300-002. Next page: https://openairdocs.org/aircraft/N588JB/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 = 'N588JB' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N588JB/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.