# Service difficulty reports: N505JB

A list on [N505JB](https://openairdocs.org/aircraft/N505JB.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 · 102 reports

- [SDR YENA2025121501203](https://openairdocs.org/sdr/YENA2025121501203.md): A/C Pack · odor · Dec 13, 2025 · N505JB · Airbus A320232 · Cabin Cooling System
  > FLT#1505, EWR-FLL. BLACK MAGIC MARKER ODOR APPROX 5,000 FT DURGIN DESCENT. ODOR ISOLATION PROCEDURE APPLIED. DISSIPATED WITH PACK 1 OFF; COMPLIED WITH INFO NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-08
- [SDR YENA2025072300751](https://openairdocs.org/sdr/YENA2025072300751.md): Uplock · failed · Jul 22, 2025 · N505JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > FLT#488, MCO-ORH. (AIRCRAFT DIVERSION TO BOS) "ON GA AFTER PREVIOUS MDG NOSE LG WOULD NOT RETRACT. RECYCLED GEAR PER EICAM + GEAR RETRACTED; PER TSM 32-31-00 REMOVED AND REPLACED NLG UPLOCK ASSY IAW AMM 32-31-21. OPERATIONAL CHECK AND LEAK CHECK REQUIRED.)
- [SDR YENA2025021800166](https://openairdocs.org/sdr/YENA2025021800166.md): Unknown · odor · Feb 15, 2025 · N505JB · Airbus A320232 · Air Distribution System
  > FLT#1134, SJU-MCO. 'ON DESCENT COCKPIT HAD DIRTY SOCK SMELL BELOW 10,000 FT, WE UTILIZED THE ISOLATION PROCEDURE BY TURNING OFF PACK 1 & SMELL DISSIPATED CABIN CREW HAD NO SMELL; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B. IDENTIFY ODOR TYPE 1 (APU)
- [SDR YENA2025011600066](https://openairdocs.org/sdr/YENA2025011600066.md): Light · no test · Jan 15, 2025 · N505JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: OVERWING EMERGENCY EXIT LIGHTS NOT WORKING ROW 10/11 ABC, DEF BOTH SIDES; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00030) REF AE WO 2024-413/1. N/R# 2024 - 748718. REMOVED AND REPLACED OVERWING EMERGENCY EXIT LIGHTS ROW 10/11ABC, IAW AM
- [SDR YENA2025011600065](https://openairdocs.org/sdr/YENA2025011600065.md): Skin · damaged · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: LIGHTNING STRIKE EXTERNAL SKIN LOC. FR17 TO FR18 STR3L TO STR4L ON UPE ER FUSELAGE ( THIS TASK CARD IS GENERATED FOR PURPOSES TRACKING); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00024) REF TO AEROMAN W/O:2024 413/1 NR 2024 - 749295, PER
- [SDR YENA2025011600064](https://openairdocs.org/sdr/YENA2025011600064.md): Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 R/H SIDE HOLE 6 (CONFIRM INDICATION USIN G BOROSCOPE) IN PASSENGER CABIN (1 EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00031) REF AE WO 2024-413/1. N/R# 2024 - 749156 PERFORMED REPAIR ON HOLE 6 LOC. FRAME
- [SDR YENA2025011600063](https://openairdocs.org/sdr/YENA2025011600063.md): Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE HOLE A (CONFIRM INDICATION USING BOROSCOPE) IN PASSENGER CABIN (2 EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00032) REF AE WO 2024-413/1. N/R# 2024 - 749159. PERFORMED REPAIR ON HOLE A LOC. FRAME
- [SDR YENA2025011600062](https://openairdocs.org/sdr/YENA2025011600062.md): Skin · gouged · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: GOUGE EXTERNAL SKIN BTW FRAME 58 AND FRAME 59 AND BTW STRINGER 28L AN D 29L AT LOWER FUSELAGE; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00034) REF AEM WO 2024-413/1, NR 2024-748769, PERFORMED REPAIR LOC EXTERNAL SKIN BTW FRAME 58 AND FR
- [SDR YENA2025011600061](https://openairdocs.org/sdr/YENA2025011600061.md): Door Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 LH. CRACK DIRECTION 5 AND 11 OCLOCK. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00036) REF AEM WO 2024-413/1, NR 2024-749227, PERFOR
- [SDR YENA2025011600060](https://openairdocs.org/sdr/YENA2025011600060.md): Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 RH SIDE HOLE C (CONFIRM INDICATION USING BOROSCOPE) IN PASSENGER CABIN (1 EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00037) REF AEM WO 2024-413/1, NR 2024-749160,PERFORMED PERMANENT REPAIR ON HOLE C(LEAD
- [SDR YENA2025011600059](https://openairdocs.org/sdr/YENA2025011600059.md): Door Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER OUTB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 LH. CRACK DIRECTION 10 O'CLOCK. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00038) REF AE WO 2024-413/1.N/R# 2024 - 749228. PERFORME
- [SDR YENA2025011600058](https://openairdocs.org/sdr/YENA2025011600058.md): Door Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON UPPER INB FASTENER HOLE OF DOOR STOP FITTING Ñ7 AREA FR 66 RH. CRACK DIRECTION 5 AND 11 O'CLOCK. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00039) REF AE WO 2024-413/1. N/R# 2024 - 749229. PE
- [SDR YENA2025011600057](https://openairdocs.org/sdr/YENA2025011600057.md): Door Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 RH. CRACK DIRECTION 6 AND 12 O'CLOCK. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1347560 TASKCARD: NR-00040) REF AE WO 2024-413/1. N/R# 2024 - 749231. PE
- [SDR YENA2025011600056](https://openairdocs.org/sdr/YENA2025011600056.md): Door Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER OUTB FASTENER HOLE OF DOOR STOP FITTIN G Ñ1 AREA FR 68 LH. CRACK DIRECTION 10 OCLOCK. CRACK D= 0.170 INCH.(THIS TASK CARD IS GENERATED FOR PURPOSES TRACKING AREA 4); (RESOLVED ON W/O: 1347560 TASKCARD:
- [SDR YENA2025011600055](https://openairdocs.org/sdr/YENA2025011600055.md): Door Frame · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 RH. CRACK DIRECTION 6 AND 12 OCLOCK. CRACK D= 0.170 INC H.(THIS TASK CARD IS GENERATED FOR PORPUSES TRACKING AREA 2); (RESOLVED ON W/O: 1347560 TASKC
- [SDR YENA2025011600054](https://openairdocs.org/sdr/YENA2025011600054.md): Stop Fitting · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB FASTENER HOLE OF DOOR STOP FITTING Ñ1 AREA FR 68 RH. CRACK DIRECTION 6 AND 12 OCLOCK. CRACK D= 0.170 INC H. (THIS TASK CARD IS GENERATED FOR PORPUSES TRACKING AREA 4); (RESOLVED ON W/O: 1347560 TASK
- [SDR YENA2025011600053](https://openairdocs.org/sdr/YENA2025011600053.md): Fitting · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON ATTACHMENT FITTINGS ON UPPER FASTERNER HOLE ON AFT FITTING ON RH MAIN LANDING GEAR ( 1EA); (RESOLVED ON W/O: 1347560 TASKCARD: NR-00045) REF AEROMAN W.O. 2024 413/1 NR 2024-748954 * PERFORMED PERMANENT REPAIR LOCA
- [SDR YENA2025011600052](https://openairdocs.org/sdr/YENA2025011600052.md): Slide Raft · no test · Jan 15, 2025 · N505JB · Airbus A320232 · Escape Slide
  > DURING HEAVY MAINTENANCE: DOOR 831 SLIDE RAFT DURING OPERATIONAL TEST EMERGENCY EXIT LIGHTS DO N OT PASS TEST DUE TO ESCAPE SLIDE RAFT ELECTRICAL FAILURE AND MUST BE REPLACED; REF AEROMAN W.O. 2024-413/1 NR 749345 ** REMOVED AND REPLACED ESCAPE SLIDE RAFT SERV
- [SDR YENA2025011600051](https://openairdocs.org/sdr/YENA2025011600051.md): Fitting · cracked · Jan 15, 2025 · N505JB · Airbus A320232 · Fuselage Main, Attach Fittings
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE RH MLG DOOR ACTUATOR FITTING / CRACK - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9065-24 (COVER & PART 1 REV 0), /2/ AIRBUS DOSSIER REFERENCE: 81507163, /3/ RDAF 81507163/004/2024#B, /4/ AIRBUS TECHNIC
- [SDR YENA2024022600292](https://openairdocs.org/sdr/YENA2024022600292.md): Warning Light · illuminated · Feb 25, 2024 · N505JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > FLT#1247, LGA-TPA. 'UPON GEAR RETRACTION, THE NOSE GEAR SHOWED UNLK AND THE ECAM SHOWED L/G DOORS AND L/G UNLK MESSAGES. GEAR RECYCLED, CLEARED FAULTS.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023070300752](https://openairdocs.org/sdr/YENA2023070300752.md): Unknown · unknown · Jun 30, 2023 · N505JB · Airbus A320232 · Cabin Pressure Control System
  > FLT#1812, RSW-EWR. (AIRCRAFT DIVERTED TO MCO) 'CLIMBING OUT OF RSW, GOT A "CABPR SYS 1 FAULT, WHILE DOING QRC, GOT A SECOND "CAB PR 1&2 FAULT. FOLLOWED THE ECAM ACTIONS; PERFORMED PRESSURE CONTROL AND MONITORING TESTS, OPS CHECK VIA MCDU, OPS TEST OF MANUAL SE
- [SDR YENA2023010600015](https://openairdocs.org/sdr/YENA2023010600015.md): Battery Pack · no test · Jan 4, 2023 · N505JB · Airbus A320232 · Emergency Lighting
  > FLT#391, BOS-TPA. EMERG LIGHT BATTERY FIN 12WL FAILED TEST. REMOVED AND REPLACED THE BATTERY 12WL IAW AMM 33-51-38.
- [SDR YENA2023010600014](https://openairdocs.org/sdr/YENA2023010600014.md): Battery · failed · Jan 4, 2023 · N505JB · Airbus A320232 · Emergency Lighting
  > FLT#391, BOS-TPA. 'EMERG LIGHT BATTERY FIN10WL FAILED TEST; REMOVED AND REPLACED EMERG LIGHT BATTERY 10WL IAW AMM 33-51-38.'
- [SDR YENA2022121201243](https://openairdocs.org/sdr/YENA2022121201243.md): Light · inoperative · Dec 11, 2022 · N505JB · Airbus A320232 · Emergency Lighting
  > FLT#1952, MCO-BOS. 'FLOOR PROX EMERGENCY LIGHTS AT ROWS 3, 7, 15, 19, 23, 25 ABC INOPERATIVE. REMOVED AND REPLACED EPSU 11WL REF AMM 33-51-38. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED. '
- [SDR YENA2022072100677](https://openairdocs.org/sdr/YENA2022072100677.md): Floorbeam · corroded · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Floor Panel
  > DURING HEAVY MAINTENANCE, CORROSION FLOORBEAM -Y1292 LOCATED BTW FR 66 AND FR 68 AT AFT GALLEY AREA (CPCP RELATED 534195-01) REPORTED BY CERT#: 99999; REMOVED AND REPLACED FLOORBEAM -Y1292 LOCATED BTW FR66 AND FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND DRAWI
- [SDR YENA2022070700658](https://openairdocs.org/sdr/YENA2022070700658.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 PRESSURE DECK PANEL ON OPEN FASTENER HOLE 2 INCH OUTBOARD Y1292, CRACK DIRECTION IS 6 OCLOCK IN FWD CARGO COMPA RTMENT (1 EA); REF AEROMAN N/R 2021-491740, ACCOMPLISHED MODIFICATION/REPAIR IN ACCORDANCE W
- [SDR YENA2022070700657](https://openairdocs.org/sdr/YENA2022070700657.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON LOWEST FASTENER HOLE OF BELLY FAIRING WEB AFT TI ANGLE LOCATION FR 41-42 RH. CRACK LENGTH IS 0.210 INCH; REF AEROMAN N/R 2021-491794, PERFORMED REPAIR PER AEROMAN EA53-0560-21 COVER RO AND PART 1. JETBLUE EC
- [SDR YENA2022031100170](https://openairdocs.org/sdr/YENA2022031100170.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 2) AND Y765 LOCATED ON FLOOR BEAM. AEROMAN TECH 8640408 / 8612107 QC STAMP 238; REF AEROMAN NR 2021-491725 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/
- [SDR YENA2022031100169](https://openairdocs.org/sdr/YENA2022031100169.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 1) AND Y765 LOCATED ON FLOOR BEAM LAYER; REF AEROMAN NR 2021-491724 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 861210
- [SDR YENA2022031100168](https://openairdocs.org/sdr/YENA2022031100168.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 2) AND Y254 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491723 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC S
- [SDR YENA2022031100167](https://openairdocs.org/sdr/YENA2022031100167.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 1) AND Y254 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491722 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC S
- [SDR YENA2022031100166](https://openairdocs.org/sdr/YENA2022031100166.md): Floorbeam · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 2) AND -Y254 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491721 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC
- [SDR YENA2022031100165](https://openairdocs.org/sdr/YENA2022031100165.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 1) AND -Y254 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491720 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC S
- [SDR YENA2022031100164](https://openairdocs.org/sdr/YENA2022031100164.md): Floorbeam · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 2) AND -Y76 5 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491718 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC
- [SDR YENA2022031100163](https://openairdocs.org/sdr/YENA2022031100163.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 ON OPEN HOLE ( ZONE 1) AND -Y765 LOCATED ON FLOOR BEAM.; REF AEROMAN NR 2021-491717 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC
- [SDR YENA2022031100162](https://openairdocs.org/sdr/YENA2022031100162.md): Door Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK EMERGENCY EXIT DOOR 833 FWD FRAME SEGMENT 1 IN PASSENGER CABIN (1 EA) (CRACK LENGHT: 0.950 INC; REF AEROMAN N/R 2021-491634, REPLACED SEGMENT (2EA), BEAM (3EA) AND FASTENER LOC ON EMERGENCY EXIT DOOR 833 PASSENGER CABIN IAW SRM
- [SDR YENA2022031100161](https://openairdocs.org/sdr/YENA2022031100161.md): Door Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK EMERGENCY EXIT DOOR 844 FWD FRAME SEGMENT 1 IN PASSENGER CABIN (1 EA) (CRACK LENGTH: 0.700 INCH); REF AEROMAN N/R 2021-491635, REPLACED SEGMENT (2EA), BEAM (3EA), AND FASTENER LOC ON EMERGENCY EXIT DOOR 844 PASSENGER CABIN IAW S
- [SDR YENA2022031100160](https://openairdocs.org/sdr/YENA2022031100160.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Emergency Exits
  > DURING HEAVY MAINTENANCE, CRACK EMERGENCY EXIT DOOR 843 AFT FRAME SEGMENT 1 IN PASSENGER CABIN (1 EA) (CRACK LENGTH: 0.750 INCH); REF AEROMAN N/R 2021-491638, REPLACED SEGMENT (2EA), BEAM (3EA) AND FASTENER LOC ON EMERGENCY EXIT DOOR 843 PASSENGER CABIN IAW S
- [SDR YENA2022031100159](https://openairdocs.org/sdr/YENA2022031100159.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH IN COCKPIT (1 EA); REF AEROMAN N/R 2021-491505, ACCOMPLISH MODIFICATION/REPAIR IN ACCORDANCE WITH AEROMAN 53-0549-21
- [SDR YENA2022031100158](https://openairdocs.org/sdr/YENA2022031100158.md): Frame · cracked · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH IN COCKPIT (1 EA); REF AEROMAN N/R 2021-491504, ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH AEROMAN EA 53-0564-21 REV
- [SDR YENA2022031100157](https://openairdocs.org/sdr/YENA2022031100157.md): Frame · corroded · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION STRINGER 41L LOCATED NWT FR 28 TO FR 30 INTERNAL AREA IN FWD CARGO COMPARTMENT; REF AEROMABN N/R 2021-491693, - PERFORMED REPAIR OF STRINGER 41L LOCATED BTW FRAME27 AND FRAME 31 IN FORWARD CARGO COMPARTMENT IAW A320 SRM 53-0
- [SDR YENA2022031100156](https://openairdocs.org/sdr/YENA2022031100156.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION UPPER SURFACE OF UPPER SKIN OF THE CENTER WING BOX AT LEVEL+Y1292 AND FR 41 PLUS11 INCHES IN PASSENGER CABIN; ACCOMPLISHES REPAIR ON CENTER WING BOX UPPER SKIN PANEL IAW EC A21-1360-01. WORK ACCOMPLISHED ON AEROMAN NR 2021-4
- [SDR YENA2022031100155](https://openairdocs.org/sdr/YENA2022031100155.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION UPPER SURFACE OF UPPER SKIN OF THE CENTER WING BOX BTW +Y1292 AND +Y1732 IN PASSENGER CABIN; ACCOMPLISHED REPAIR ON ON CENTER WING BOX IAW EC A21-1360-21. WORK ACCOMPLISHED ON AEROMAN NR 2021-491731 (CLASSIFIED A MAJOR REPAI
- [SDR YENA2022031100154](https://openairdocs.org/sdr/YENA2022031100154.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 52 PLUS 13.375 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492033 (CLASSIFIED A MAJOR REPAIR)
- [SDR YENA2022031100153](https://openairdocs.org/sdr/YENA2022031100153.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED BTW FR 47 PLUS 16 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-491810 (CLASSIFIED A MAJOR REPAIR)
- [SDR YENA2022031100152](https://openairdocs.org/sdr/YENA2022031100152.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED BTW FR 59 PLUS 2 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 57-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492037 (CLASSIFIED A MAJOR REPAIR)
- [SDR YENA2022031100151](https://openairdocs.org/sdr/YENA2022031100151.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 51 IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492032 (CLASSIFIED A MAJOR REPAIR)
- [SDR YENA2022031100150](https://openairdocs.org/sdr/YENA2022031100150.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 55 PLUS 16 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492035 (CLASSIFIED A MAJOR REPAIR)
- [SDR YENA2022031100149](https://openairdocs.org/sdr/YENA2022031100149.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 54 PLUS 5 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492034(CLASSIFIED A MAJOR REPAIR)
- [SDR YENA2022031100148](https://openairdocs.org/sdr/YENA2022031100148.md): None · none · Jan 23, 2022 · N505JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 49 PLUS 8 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-71-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492031 (CLASSIFIED A MAJOR REPAIR)

Next page: https://openairdocs.org/aircraft/N505JB/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 = 'N505JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N505JB/reports

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