# Service difficulty reports: N524JB

A list on [N524JB](https://openairdocs.org/aircraft/N524JB.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 · 84 reports

- [SDR YENA2026042900444](https://openairdocs.org/sdr/YENA2026042900444.md): Skin · cracked · Apr 29, 2026 · N524JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STR 30R SIDESHELL AREA / HOLE #2 / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ AAR-LCQ FINAL REO-L25784 REV. IR /2/ AIRBUS DOSSIER 81748154 /3/ AIRBUS RDAF 81748154/003/2026#B /4/ AIRBUS SB A32
- [SDR YENA2026042900443](https://openairdocs.org/sdr/YENA2026042900443.md): Pressure Panel · cracked · Apr 29, 2026 · N524JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36RH / PRESSURE PANEL HOLE #7 / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ REO-L25791.IR /2/ AIRBUS RDAF 81742124/003/2026#B /3/ AIRBUS SB A320-53-1263 REV 05 /4/ MX-244. DESC
- [SDR YENA2026042900442](https://openairdocs.org/sdr/YENA2026042900442.md): Skin · cracked · Apr 29, 2026 · N524JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / SB 53-1372 / LH CENTER FUSELAGE / FR35 STGR30 / MULTIPLE HOLES -CRACK & ELONGATION - TEMPORARY REPAIR; REFERENCES: /1/ AAR-LCQ FINAL REO-L25785 REV. IR /2/ AIRBUS DOSSIER 81750093 /3/ AIRBUS RDAF 81750093/003/2026 ISSUE B /
- [SDR YENA2026042900441](https://openairdocs.org/sdr/YENA2026042900441.md): Stiffener · cracked · Apr 29, 2026 · N524JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / FLOOR BEAM JUNCTION TO FRONT SPAR VERTICAL STIFFENER / @ LEVEL OF FR36 & Y+254, Y+765, Y-254 & Y-765 / HOLES #1 & #2 / CRACKS – PERMANENT REPAIR; REFERENCES: /1/ AAR-LCQ FINAL REO-L25783 REV. IR /2/ AIRBUS DO
- [SDR YENA2026042900440](https://openairdocs.org/sdr/YENA2026042900440.md): Pressure Panel · cracked · Apr 29, 2026 · N524JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FR 35-36LH / PRESSURE PANEL ATTACHMENT HOLES / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ REO-L25792.IR /2/ AIRBUS TD/ 80535017/029/2026#B /3/ AIRBUS RDAF 80535017/027/2026#A /4/ AI
- [SDR YENA2026042900439](https://openairdocs.org/sdr/YENA2026042900439.md): Floorbeam · corroded · Apr 29, 2026 · N524JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: INSIDE CABIN WET AREA RH Y-1292 FLOOR BEAM 66+ 10" HAS CORROSION; REF AAR WO 440619, NR 34341. REMOVED AND REPLACED OUT OF LIMIT CORRODED FLOOR BEAM Y1292 AT FRAME 66 + 10" R/H SIDE IAW SRM 51-72-11-911-001"
- [SDR YENA2026042900438](https://openairdocs.org/sdr/YENA2026042900438.md): Floorbeam · corroded · Apr 29, 2026 · N524JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: INSIDE CABIN WET AREA LEFT SIDE Y1292 CORROSION FLOORBEAM FRAME 66 + 3; REF AAR WO 440619, NR# 34345, REMOVED AND REPLACED CORRODED Y1292 LEFT SIDE FRAME 66 + 3" IAW A320 SRM 51-42-11 AND SRM 53-41-14-01-A"
- [SDR YENA2025122201244](https://openairdocs.org/sdr/YENA2025122201244.md): Unknown · odor · Dec 19, 2025 · N524JB · Airbus A320232 · Air Distribution System
  > FLT#21, BOS-PBI. "DURING VECTORS FOR APPROACH DESCENDING FROM 7000 FT WE SMELLED A "GYM" SHIRT ODOR. DONNED O2 MASKS NO TIME TO RUN ODOR PROCEDURE WE WERE #3 FOR LANDG. AFTER LANDG FRONT AND BACK FA CONTINUED ODOR; COMPLIED WITH INFORMATION NOTICE 2017-T015, S
- [SDR YENA2025100901014](https://openairdocs.org/sdr/YENA2025100901014.md): Skin · corroded · Oct 7, 2025 · N524JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION ON TOP SKIN LOWER SURFACE ON TRAILING EDGE OVERHANG AREA BTW RIB8 AND RIB9 ON RH WING (CPCP FINDING); ACCOMPLISH REPAIR OF THE CORROSION ON THE RH WING TOP SKIN PANEL 2 LOWER SURFACE TRAILING EDGE OVERHANG BETWEEN WX3494.5-W
- [SDR YENA2025100901013](https://openairdocs.org/sdr/YENA2025100901013.md): Skin · corroded · Oct 7, 2025 · N524JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION ON TOP SKIN LOWER SURFACE ON TRAILING EDGE OVERHANG AREA BTW RIB 8 AND RIB 9 ON LH WING (CPCP FINDING); ACCOMPLISHED REPAIR OF THE CORROSION ON THE LH WING TOP SKIN PANEL 2 BETWEEN RIBS 8-9 LOWER SURFACE IN ACCORDANCE WITH
- [SDR YENA2025051400492](https://openairdocs.org/sdr/YENA2025051400492.md): Oil Cooler · leaking · May 11, 2025 · N524JB · Airbus A320232 · APU Oil System
  > FLT#2879, PVD-MCO. 'ODOR FUMES EVENT STRONG ODOR IN FLIGHT DECK ON DESCENT TO TAXI INTO GATE ( APU SYSTEM); REMOVED AND REPLACED APU OIL COOLER IAW AMM 49-91-44. OPS & LEAK CHECK OK. THIS ACTION CLEARS THIS MDDR. MX-4 UPDATED, PLACARD REMOVED, MCC NOTIFIED.'
- [SDR YENA2025050500463](https://openairdocs.org/sdr/YENA2025050500463.md): Cooling Fan · leaking · May 1, 2025 · N524JB · Airbus A320232 · APU Oil System
  > FLT#525, PVD-SJU. 'NOTICE OILY/FUEL SMELL AT FL200 ON DECENT WITH PWR AT IDLE SMELL CONTINUE UNTIL 10,000 WHEN APU WAS STARTED AND APU BLEED USED. DIDN'T SEEM ASSOCIATED WITH APU; COMPLIED WITH INFORMATION NOTICE 2017-T015K SECTION B2, IDENTIFIED TYPE 1 LEVEL
- [SDR YENA2025041000383](https://openairdocs.org/sdr/YENA2025041000383.md): Unknown · odor · Apr 5, 2025 · N524JB · Airbus A320232 · Air Distribution System
  > FLT#525, PVD-SJU. 'DIRTY SOCK SMELL THROUGHOUT CABIN DURING ARRIVAL COMING FROM ENGINES BLEED AIR/PACKS; COMPLIED WITH INFORMATION NOTICE 2017-T015K SECTION B2, IDENTIFIED TYPE 1 LEVEL A DECONTAMINATION WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A AIRCRAFT IS O
- [SDR YENA2024121801567](https://openairdocs.org/sdr/YENA2024121801567.md): Apu · odor · Dec 17, 2024 · N524JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#2133, MCO-SJU. 'FUME EVENT DURING DESCENT FROM 12,000 FT UNTIL AFTER LANDING, CA + FO + FWD + AFT FA'S SMELLED FUMES (DIRTY SOCK); COMPLIED WITH INFORMATION NOTICE 2017-T015,SECTION B2,FOUND APU TO BE THE SOURCE OF ODOR,DECONTAMINATION LEVEL A WAS ACCOMP
- [SDR YENA2024120201523](https://openairdocs.org/sdr/YENA2024120201523.md): Pressure Switch · leaking · Nov 26, 2024 · N524JB · Airbus A320232 · Aileron Control System
  > FLT#1203, EWR-SDQ. (AIRCRAFT DIVERTED TO MCO) 'HYD Y RSVR LO LVL ECAM AT FL 350 1 HOUR INTO FLIGHT. PERFORMED ECAM ACTIONS AND QRH; FOUND YELLOW HYD MANIFOLD PRESS SWITCH LEAKING OUT OF SPLIT ORING AT (10CE1) REPLACED ORING PER AMM 27-92-01 REPLENISHED Y HYD R
- [SDR YENA2024090301201](https://openairdocs.org/sdr/YENA2024090301201.md): Apu · contaminated · Aug 31, 2024 · N524JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT#874, TPA-EWR. 'FUMES SMELT AFTER ENGINE START, VERY FAINT, DURING CRUISE FAINT, AND IN DESCENT VERY STRONG, COULD NOT DETERMINE WHICH PACK USING ISOLATION TECHNIQUE; C/W INFO NOTICE 2017- T015 SECTION B2. IDENTIFIED ODOR COMING FROM APU. DECONTAMINATION LE
- [SDR YENA2024071601002](https://openairdocs.org/sdr/YENA2024071601002.md): O-Ring · leaking · Jul 14, 2024 · N524JB · Airbus A320232 · Hydraulic System, Main
  > FLT#2357, EWR-MBJ. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR). 'HYD B RSVR LO LVL ECAM IN FLIGHT LOST ALL FLUID IN BLUE SYSTEM; UPON INSPECTION OF THE T FITTING ASSY WHERE THE ELEC PUMP PRESS. SWITCH(2074GJ) IS INSTALLED, FOUND THE O-RING OFF THE PRESSURE SW
- [SDR YENA2023120601550](https://openairdocs.org/sdr/YENA2023120601550.md): Unknown · unknown · Dec 4, 2023 · N524JB · Airbus A320232 · Pneumatic System
  > FLT#2295, EWR-MIA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO EWR) 'AT CRUISE AIR L WING LEAK; ACCOMPLISHED TSM TASK 36-22-00-810-825-A. FOUND LEAK AT #1 ACM INLET DUCT SQUARE PAD GASKET. REPLACED GASKET IAW 21-52-21. ACCOMPLISHED ENG RUN, APU AND ENG BLEED SYS
- [SDR YENA2023011800055](https://openairdocs.org/sdr/YENA2023011800055.md): None · none · Jan 14, 2023 · N524JB · Airbus A320232 · Standard Practices/Structures
  > DURING HEAVY MAINTENANCE: ACCOMPLISH SB A320-53-1158. ACCOMPLISHED REPAIR IN ACCORDANCE WITH SB A320-53-1158 AND EA 53-0652-22 REV 0. AND PART 1 THRU 4 AND RDAF 80263435/045/2022#A,
- [SDR YENA2023011800054](https://openairdocs.org/sdr/YENA2023011800054.md): Frame · damaged · Jan 14, 2023 · N524JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: ELONGATED HOLE ON FRAME SECTION AT LEVEL FR 4 AND COMMON TO UPPER CONNER FITTING UPPER SIDE POST ATTACHMENT; REF TO AEROMAN WO 2022 454/1 NR 2022-663023, REMOVED AND REPLACED FRAME SECTION AT LEVEL FR 4 RH AND COMMON TO UPPER CORNER F
- [SDR YENA2023011800053](https://openairdocs.org/sdr/YENA2023011800053.md): Rib · corroded · Jan 14, 2023 · N524JB · Airbus A320232 · Horizontal Stabilizer, Spar/Rib
  > DURING HEAVY MAINTENANCE: CORROSION ELEVATOR OUTBOARD RIB ON RH HORIZONTAL STABILIZER; REF TO AEROMAN WO 2022 454/1 NR 2022-662981, REMOVED AND REPLACED OUTBOARD RIB 10 ON RH HORIZONTAL STABILIZER I.A.W A320 SRM 55-21-12-300-002 RIB 10 REPLACEMENT, A32O SRM 51
- [SDR YENA2023011800052](https://openairdocs.org/sdr/YENA2023011800052.md): Window Frame · cracked · Jan 14, 2023 · N524JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACH CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT; REF AEROMAN N/R 2022-662819 WO 2022 454/1, REMOVED ADN REPLACED CONTINUITY FITTING ON FRAME 2 W
- [SDR YENA2023011800051](https://openairdocs.org/sdr/YENA2023011800051.md): Window Frame · cracked · Jan 14, 2023 · N524JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT AR EA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT; REF N/R 2022-662818 WO 2022454/1, R&R CONTINUITY FITTING FROM FRAME 2 WINDSHIELD CEN
- [SDR YENA2023011800050](https://openairdocs.org/sdr/YENA2023011800050.md): Fitting · cracked · Jan 14, 2023 · N524JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE INTERCOSTAL FITTING OPEN FASTENER HOLE 3 AT DOOR STOP 7 POSITION, CRACK DIRECTION IS 9 OCLOCK, AT FWD G ALLEY AREA (1 EA); REF AEROMAN N/R 2022-662874, REMOVED AND REPLACED INTERCOSTAL FITTING LOC.
- [SDR YENA2023011800049](https://openairdocs.org/sdr/YENA2023011800049.md): Fitting · cracked · Jan 14, 2023 · N524JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE INTERCOSTAL FITTING OPEN FASTENER HOLE 2 AT DOOR STOP 7 POSITION, CRACK DIRECTION IS 12 OCLOCK, AT THE FWD GALLEY AREA (1 EA); REF AEROMAN N/R 2022-662873, REMOVED AND REPLACED INTERCOSTAL FITTING
- [SDR YENA2023011800048](https://openairdocs.org/sdr/YENA2023011800048.md): Fitting · cracked · Jan 14, 2023 · N524JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE INTERCOSTAL FITTING OPEN FASTENER HOLE 3 AT DOOR STOP 7 POSITION, CRACK DIRECTION IS 3 OCLOCK, AT FWD G ALLEY AREA (1 EA); REF AEROMAN N/R 2022-662872, REMOVED AND REPLACED INTERCOSTAL FITTING LOC
- [SDR YENA2023011800047](https://openairdocs.org/sdr/YENA2023011800047.md): Frame · cracked · Jan 14, 2023 · N524JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE INTERCOSTAL FITTING OPEN FASTENER HOLE 2 AT DOOR STOP 7 POSITION, CRACK DIRECTION IS 3 OCLOCK, AT FWD G ALLEY AREA (1 EA); REF AEROMAN N/R 2022-662871, R&R INTERCOSTAL FITTING LOC. FRAME 16 LH SIDE
- [SDR YENA2023011800046](https://openairdocs.org/sdr/YENA2023011800046.md): Fitting · not reported · Jan 14, 2023 · N524JB · Airbus A320232 · Fuselage, Landing Gear Attach Fittings
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / MLG ACTUATOR FITTING. STRUCTURAL REINFORCEMENT. (CONSIDERED AS MAJOR REPAIR)
- [SDR YENA2022082500818](https://openairdocs.org/sdr/YENA2022082500818.md): None · none · Aug 24, 2022 · N524JB · Airbus A320232 · Pneumatic System
  > FLT#285, JFK-RDU. 'MULTIPLE INFLIGHT & FLIGHT DECK CREW REPORTED SMELLING "DIRTY SOCK AND BOX OF CRAYON" SMELL ON DESCENT AND AT THE GATE WITH AND WITHOUT APU BLEED ( APU BLEED AIR SUPPLY SYSTEM).' (SUPPLEMENTAL TO FOLLOW)
- [SDR YENA2022062900635](https://openairdocs.org/sdr/YENA2022062900635.md): None · none · Jun 28, 2022 · N524JB · Airbus A320232 · Air Distribution Fan
  > FLT#1484, RDU-BOS. 'DISTINCT OIL SMELL FROM APU BLEED.' (SUPPLEMENTAL TO FOLLOW)
- [SDR YENA2022040400329](https://openairdocs.org/sdr/YENA2022040400329.md): A/C Pack · odor · Apr 3, 2022 · N524JB · Airbus A320232 · Cabin Cooling System
  > FLT#2085, BDL-MIA. 'DIRTY SOCK SMELL AROUND 10K FEET ISOLATED THE PACKS WITH NO DIFFERENCE IN RESULTS; COMPLIED WITH INFORMATION NOTICE 2017-T015I, SECTION A (A), ISOLATED FAULT TO TYPE 10, (A), 1, C PER TSM 05-50-00-810-085-B. FOUND #1 PACK AT FAULT. AIRCRA
- [SDR YENA2022040100322](https://openairdocs.org/sdr/YENA2022040100322.md): None · none · Mar 31, 2022 · N524JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#108, MBJ-EWR. 'DIRTY SOCK SMELL. SUSPECT PACK 2 OR ENGINE 2 WITH ENG RUN IN JAMAICA; REF. LOG PAGE 3270652 ITEM 1 & 2 (PERFORMED HOT PACKS BURN AND DECONTAMINATION AND INSPECTION OF THE APU, ENG #1 AND #2 FOR OIL EVIDENCE IAW STM 05-50-00-810-831-A. FALLOW
- [SDR YENA2022040100323](https://openairdocs.org/sdr/YENA2022040100323.md): None · none · Mar 30, 2022 · N524JB · Airbus A320232 · Air Conditioning System
  > FLT#107, EWR-MBJ. ' DIRTY SOCK SMELL ON FINAL APPROACH TO MBJ ABOUT 10,000 FEET. ODOR REPORT COMPLETE WITH DETAILS. (PACKS); PERFORMED OPS CHECK OF THE 2 PACK AND PACK DECONTAMINATION IAW AMM 21-52-41 AND TSI 05-50-00-810-830-A. ALL CHECK OK MX-4 UPDATED PLACA
- [SDR YENA2021120800832](https://openairdocs.org/sdr/YENA2021120800832.md): Strap · unsecure · Dec 6, 2021 · N524JB · Airbus A320232 · Emergency Equipment
  > FLT 1865, BOS-RSW. GROUND CREW REPORTED BLACK STRAP HANGING OUT FROM BOTTOM OF L1 DOOR; REMOVED & REPLACED L/H FWD ESCAPE SLIDE IAW AMM 25-62-44 OPS CHECK GOOD
- [SDR YENA2021101100668](https://openairdocs.org/sdr/YENA2021101100668.md): Ecs · contaminated · Oct 10, 2021 · N524JB · Airbus A320232 · Cabin Cooling System
  > FLIGHT ATTENDANT REPORTS "DIRTY SOCKS" SMELL IN THE AFT PART OF A/C DESCENDING THROUGH 3000' ON ARRIVAL.; FOLLOWING TSM 05-50-00-810-085-B PERFORMED LEVEL A DECONTAMINATION OF ECS IAW AMM 21-00-00-615-802. NO FURTHER ODORS NOTED IN CABIN/COCKPIT. OK FOR CONTI
- [SDR YENA2021011900068](https://openairdocs.org/sdr/YENA2021011900068.md): Pin · binding · Jan 13, 2021 · N524JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE, SLIDE RAFT PASSENGER CREW DOOR 832 CONTROLLED DEPLOYMENT DUE TO THE PIN DOES NOT GO INTO THE REGULATOR VALVE ASSEMBLY IN PASSENGER RT CABIN (1 EA). R & R ESCAPE SLIDE RAFT DOOR 832, IAW AMM 25-62-44-400-007A AND AMM 25-62-44-000-011-
- [SDR YENA2020102900505](https://openairdocs.org/sdr/YENA2020102900505.md): Seat Track · corroded · Oct 25, 2020 · N524JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING BRIDGE CHECK, (REF AIRBORNE N/R 10049-0231) UPON OK TO INSTALL FOUND EVIDENCE OF CORROSION ON INBOARD SEAT TRACK IN MAIN CABIN FR 44-47 LBL 29.5, PER AIRBORNE N/R 10049-0231. SEAT TRACK ASSEMBLY FLOOR BEAM REPLACED, IAW ARM-A320-51-72-11-911-001.
- [SDR YENA2019061960335](https://openairdocs.org/sdr/YENA2019061960335.md): Apu · odor · Jun 16, 2019 · N524JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT 179, DIRTY SOCK SMELL REPORTED BY NR 1, 2 AND 3 FA'S AFTER SHUT DOWN AT GATE. FA'S NOTICED ODOR DURING CLIMB, CRUISE & DESCENT. COCKPIT CREW NOTICE ODOR AT 4,000' AND ARRIVAL LASTING REMAINDER OF FLIGHT, NO ACTION TAKEN. C/W INFO NOTICE 2017-T015E SEC "
- [SDR YENA201902228082](https://openairdocs.org/sdr/YENA201902228082.md): Battery · failed · Feb 18, 2019 · N524JB · Airbus A320232 · Emergency Lighting
  > FT # 225, EMERGENCY LIGHT TEST FAILED. REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT 11WL PER AMM 33-51-38.
- [SDR YENA201811100955](https://openairdocs.org/sdr/YENA201811100955.md): Pressure Panel · cracked · Nov 10, 2018 · N524JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE AT LCQ WHILE ACCOMPLISHING REF /3/ SB, CRACK DAMAGE WAS FOUND ON THE NR 4 HOLE AT FR35/FR36 OF THE CENTER WING BOX PRESSURE PANEL - LT. PROVIDED REF /2/ TO EXTEND THE PRESSURE DECK MEMBRANE CUT OUT TOWARDS OUTBOARD TO INCLUDE AFFECTED
- [SDR YENA201811100954](https://openairdocs.org/sdr/YENA201811100954.md): Structure · damaged · Nov 10, 2018 · N524JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING C10 CHECK AT LCQ, REJECTABLE INDICATIONS WERE NOTED ON HOLES ‘A’ & ‘7’ DURING ACCOMPLISHMENT OF JBU TASK CARD A320-53-11-00-210-027-221 (ALI 531155-02). SEE FIGURE 1 PER REF/1/ FOR AFFECTED LOCATION DETAILS. REWORKED THE HOLES TO REMOVE THE DAMAGE AND
- [SDR YENA2018111400775](https://openairdocs.org/sdr/YENA2018111400775.md): Power Supply · inoperative · Nov 10, 2018 · N524JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, AFT LEFT EMERGENCY LIGHT EPSU (13WL) FAILS. SEVERAL LIGHT DO NOT ILLUMINATE; REF HAECO NR 440530-22560, REMOVED AND REPLACED 13WL ESPU IAW A320 AMM 33-51-38. SYSTEM OPS CKS GOOD. SUPPLEMENTAL INFORMATION TO FOLLOW.
- [SDR YENA2018111400774](https://openairdocs.org/sdr/YENA2018111400774.md): Floorbeam · corroded · Nov 10, 2018 · N524JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FLOOR BEAM Y1292 ATTACHMENT POINT AT FR 16; REMOVED AND REPLACED FLOORBEAM Y1292 IAW A320 SRM 53-11-15. WORK ACCOMPLISHED ON HAECO NR 22522
- [SDR YENA2018111400773](https://openairdocs.org/sdr/YENA2018111400773.md): Floorbeam · corroded · Nov 10, 2018 · N524JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FLOOR BEAM Y765 ATTACHMENT POINT AT FR 16; REMOVED AND REPLACED FLOOR BEAM Y765 IAW A320 SRM 53-11-15. WORK ACCOMPLISHED ON HAECO NR 22523.
- [SDR YENA201805110918](https://openairdocs.org/sdr/YENA201805110918.md): Fitting · damaged · May 11, 2018 · N524JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > FLT 932, HOU-BOS. REFER EC A18-402-02. FUSELAGE / CENTER FUSELAGE / RT MLG DOOR ACTUATOR FITTING ON KEEL BEAM / WEAR DAMAGE– TIME LIMITED REPAIR (PENDING DTA); PROVIDED INSTRUCTIONS (REF. /1/) TO ACCOMPLISH PERMANENT REPAIR BY SPOT FACING THE WEAR MARKS FOUND
- [SDR YENA201804130175](https://openairdocs.org/sdr/YENA201804130175.md): Skin · corroded · Apr 13, 2018 · N524JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING WALK AROUND, FOUND INTER-GRANULAR CORROSION AT LAVATORY VENT OUTLET SKIN LOCATED AT LOWER FWD CUTOUT L 1.5" W 1.75" DEPTH.100 FRAME 69 STRINGERS 31 - 32R. REPAIRED THE SKIN IAW SRM 53-41-11-300-004, FIG 001, SHEET 1.
- [SDR YENA201804100175](https://openairdocs.org/sdr/YENA201804100175.md): Skin · corroded · Apr 13, 2018 · N524JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING A WALK AROUND, FOUND INTER-GRANULAR CORROSION AT THE LAVATORY VENT OUTLET SKIN, LOCATED AT LOWER FWD CUTOUT L 1.5" W 1.75" DEPTH.100 FRAME 69, STRINGERS 31 - 32R. REPAIRED THE SKIN IAW SRM 53-41-11-300-004, FIG 001, SHEET 1.
- [SDR YENA201707150577](https://openairdocs.org/sdr/YENA201707150577.md): Eec · failed · Jul 15, 2017 · N524JB · Airbus A320232 · Fuel Controlling System
  > DURING CLIMBOUT, RECIEVED AN ECAMS NR ENGINE SENSOR FAULT AND NR 2 ENGINE FADEC B FAULT. N1 INDICATOR ON ENG 2 SHOWED AMBER FOR A FEW SECONDS ALL OTHER ENGINE INDICATIONS NORMAL. NR 2 ENGINE OVERSPEED PROT FAULT ECAM ON. RETURN TO FIELD. ENGINE SHUTDOWN AFTE
- [SDR YENA201702160103](https://openairdocs.org/sdr/YENA201702160103.md): Stringer · corroded · Feb 16, 2017 · N524JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON STRINGER 42L FR54 TO FR 55; REF NR 2017-47293 REPAIR IAW SRM A320 53-00-13.
- [SDR YENA201702160102](https://openairdocs.org/sdr/YENA201702160102.md): Floorbeam · corroded · Feb 16, 2017 · N524JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY CHECK MAINTENANCE, CORROSION WAS DISCOVERED ON FLOORBEAM AT Y1292 FR 12 TO FR 24. R & R FLOORBEAM IAW SRM51-72-11.

Next page: https://openairdocs.org/aircraft/N524JB/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 = 'N524JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N524JB/reports

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