# Service difficulty reports: N563JB

A list on [N563JB](https://openairdocs.org/aircraft/N563JB.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 · 59 reports

- [SDR YENA2026081400679](https://openairdocs.org/sdr/YENA2026081400679.md): A/C Pack · odor · Aug 13, 2026 · N563JB · Airbus A320232 · Cabin Cooling System
  > FLT 953, JFK-PBI. DURING TAKEOFF, HAD FUME EVENT, SEEMED ISOLATED TO FWD GALLEY & FLIGHT DECK. FUMES DISAPATED IN FLIGHT DECK AFTER 5 MIN. F/A SMELLED FUMES, PERSISTED IN FWD GALLEY. RAN ISOLATION CHKLST, CONFIGURED WITH PACK 2 OFF & BLEED VALVE SHUT. ACCO
- [SDR YENA2024110801441](https://openairdocs.org/sdr/YENA2024110801441.md): Bleed Valve · unknown · Nov 5, 2024 · N563JB · Airbus A320232 · Engine Pressure Ratio (EPR)
  > FLT#787, JFK-SXM. "DESCENDING THROUGH 10,000 INFLIGHT CALLED TO INFORM A DIRTY SOCK SMELLIN THE CABIN COMMING FROM ROW 16 TO THE FWD CABIN. CUSTOMERS ALSO NOTIFIED THE ODOR, INFLIGHT DESCROBED THE SMELL AS PERSISTANT AND SAID ODOR REMAINED TILL AFTER BLOCKING
- [SDR YENA2024082201137](https://openairdocs.org/sdr/YENA2024082201137.md): Unknown · fumes · Aug 21, 2024 · N563JB · Airbus A320232 · Air Distribution System
  > FLT#256, BZN-BOS. 'FUMES IN CABIN AT 1500` ON APPROACH. NO APU IN USE.' OPEN
- [SDR YENA2024020600242](https://openairdocs.org/sdr/YENA2024020600242.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH DOOR STOP Ñ7 HOLE H3 (LWR / INB), CRAC K DIRECTION AT 4 AND 6 O CLOCK. D= 0.150 INCH; REF AEROMAN NR 2023-741034 WO 2023 362/1 REMOVED AND REPLACED INTERCOSTAL FITTING BTW FR 15 LH TO FR 16 LH AT LEVEL
- [SDR YENA2024020600241](https://openairdocs.org/sdr/YENA2024020600241.md): Window Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX, IN COCKPIT (1 EA); REFAEROMAN NR 2023-741053 REMOVED AND REPLACED CONTINUITY FITTINGS IAW RE
- [SDR YENA2024020600240](https://openairdocs.org/sdr/YENA2024020600240.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH, DOUBLE JOGGLE AREA, HOLE C. CRACK DI RECTION AT 3 AND 10 O CLOCK. D= 0.110 INCH; REF AEROMAN NR 2023-741037 WO 2023 362/1 PERFORMED REPAIR ON HOLE C LOCATED ON FRAME 16 LH, DOUBLE JOGGLE AREA IAW REPAI
- [SDR YENA2024020600239](https://openairdocs.org/sdr/YENA2024020600239.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE Ñ6. CRACK D IRECTION AT 1 O CLOCK. D= 0.130 INCH; REF AEROMAN NR 2023-741038 WO 2023 362/1 PERFORMED REPAIR ON HOLE #6 LOCATED ON FOR 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INST
- [SDR YENA2024020600238](https://openairdocs.org/sdr/YENA2024020600238.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE A. CRACK DI RECTION AT 9 O CLOCK. D= 0.160 INCH; REF AEROMAN NR 2023-741039 WO 2023 362/1 PERFORMED REPAIR ON HOLE #A LOCATED ON FOR 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INSTR
- [SDR YENA2024020600237](https://openairdocs.org/sdr/YENA2024020600237.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH, DOUBLE JOGGLE AREA, HOLE C. CRACK DI RECTION AT 9 O CLOCK. D= 0.150 INCH; REF AEROMAN NR 2023-741040 WO 2023 362/1 PERFORMED REPAIR ON HOLE C LOCATED ON FRAME 16 RH, DOUBLE JOGGLE AREA, IAW REPAIR INST
- [SDR YENA2024020600236](https://openairdocs.org/sdr/YENA2024020600236.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE UPPER INBOA RD AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 12 OCLOCK, AT A FT GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00013) REF AEROMAN NR 2023-741
- [SDR YENA2024020600235](https://openairdocs.org/sdr/YENA2024020600235.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 2 POSITION, CRACK DIRECTION IS 6 OCLOCK, AT AF T GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00014) REF AEROMAN NR 2023-7412
- [SDR YENA2024020600234](https://openairdocs.org/sdr/YENA2024020600234.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 66 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, AT AF T GALLEY AREA (1 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00015) REF AEROMAN NR 2023-7412
- [SDR YENA2024020600233](https://openairdocs.org/sdr/YENA2024020600233.md): Frame · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 3 AND 6 OCLOC K, AT AFT GALLEY AREA (2 EA); (RESOLVED ON W/O: 1254356 TASKCARD: NR-00016) REF AEROMAN NR 2
- [SDR YENA2024020600232](https://openairdocs.org/sdr/YENA2024020600232.md): Flange · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ONN FR68 LH SIDE HORIZONTAL FLANGE RADIUS AT STR 22LH, CRACK LENGTH.300 INSCH APPROX, AT AFT GALLEY AREA; REF AEM WO: 2023 362/1, NR 2023-741036. ACCOMPLISHED REPAIR ON RADIAL FLANGE STOP FITTING AT FR68,STR22L
- [SDR YENA2024020600231](https://openairdocs.org/sdr/YENA2024020600231.md): Flange · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND AO FR 68RH HORIZONTAL FLANGE RADIUS AT STR22RH. CRACK LENGTH 300 INCH, AT AFT GALLEY AREA; REF AEM WO: 2023 362/1, NR 2023-741035. ACCOMPLISHED REPAIR ON HORIZONTAL FLANGE FR 68RH AT STR 22RH. PER JB EC: A24-111
- [SDR YENA2024020600230](https://openairdocs.org/sdr/YENA2024020600230.md): Skin · corroded · Feb 1, 2024 · N563JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION ON LH WING TOP SKIN LOWER SURFACE OVERHANG AT TRAILING EDGE AREA BTW RIB 6 AND RIB 7; ACCOMPLISHED THE REPAIR OF CORROSION ON LH WING TOP SKIN PANEL 2 FALSE REAR SPAR TE OVERHANG LOWER SURFACE BETWEEN WX3622-WX4013 IN ACCOR
- [SDR YENA2024020600229](https://openairdocs.org/sdr/YENA2024020600229.md): Stop Fitting · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 RH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2024020600228](https://openairdocs.org/sdr/YENA2024020600228.md): Stop Fitting · cracked · Feb 1, 2024 · N563JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 LH & STR 22 / DOOR STOP FITTING #1 / RADIAL FLANGE FILLET RADIUS / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023112201440](https://openairdocs.org/sdr/YENA2023112201440.md): Unknown · unknown · Nov 17, 2023 · N563JB · Airbus A320232 · Passenger/Crew Doors
  > FLT#1692, LIR-JFK. 'REF L/P 3757835 ITEM # 2 L2 DOOR EMERG. CONTROL HANDLE VERY STIFF WHEN MOVED TO ARM/DISARMED POSITIONS; RE-ADJUSTED AFT L2 DOOR SLIDE GIRT BAR PLACEMENT. REF AMM 25-62-44-420-065-A. ALL OPS NORMAL.'
- [SDR YENA2023051900541](https://openairdocs.org/sdr/YENA2023051900541.md): Unknown · unknown · May 16, 2023 · N563JB · Airbus A320232 · Standard Practices/Structures
  > FLT#2332, PUJ-SJU. 'BIRD STRIKE ON L.E OF LEFT WING JUST OUTBOARD OF ENG#1.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023021700175](https://openairdocs.org/sdr/YENA2023021700175.md): Control Unit · failed · Feb 16, 2023 · N563JB · Airbus A320232 · Landing Gear Brake System
  > FLT#706, FLL-EWR. 'ON TAKE OFF AROUND 70KTS WE GOT A BRAKE AUTOBRAKE FAULT BRAKE RELEASED; AS PER TSM 32-42-00-810-819A. PERFORMED BITE TEST OF BSCU IAW AMM 32-46-00 AND FUNCTIONAL TEST OF #2 TACHOMETER IAW AMM 32-42-00-720-002. ALL CHECKS ARE GOOD, COULD NOT
- [SDR YENA2021110300741](https://openairdocs.org/sdr/YENA2021110300741.md): Selector Valve · odor · Nov 2, 2021 · N563JB · Airbus A320232 · Cargo/Baggage Doors
  > FLT 152, LGA-DEN. CABIN ODOR DURING APPROACH AND LANDING BY FLIGHT ATTENDANTS AND PASSENGER LEVEL 2 PERSISTENT. FOUND AFT CARGO DOOR SELECTOR VALVE LEAKING HYD FLUID REPLACED SELECTOR VALVE AS PER AMM 53-36-00 REPLACED BOTH CABIN RECERC FILTERS ACCOMPLISHED P
- [SDR YENA2021102100708](https://openairdocs.org/sdr/YENA2021102100708.md): Apu · odor · Oct 20, 2021 · N563JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT # 648, SLC-BOS. FA'S STATED THAT MUSTY FUMES WERE PRESENT IN THE MID TO AFT CABIN DURING LOW ALT DESCENT AND REMAINED UNTIL THE ENGINES WERE SHUT DOWN; DETERMINED APU TO BE AT FAULT FOR CABIN ODOR. REFERENCE LP 3242713 ITEM 1 FOR APU DEFECT. DECONTAMINATI
- [SDR YENA2021091700599](https://openairdocs.org/sdr/YENA2021091700599.md): Line · leaking · Sep 14, 2021 · N563JB · Airbus A320232 · Hydraulic System, Main
  > FLT 1460, FLL-BDL. GREEN HYD RSVR LOW LEVEL AFTER LANDING EXTENSION FOUND LEAK NEAR MAIN GEAR ON RIGHT SIDE POST RIGHT; R/R R/H GEAR DOOR ACTUATOR FWD BRAIDED HYD LINER IAW AMM 32-31-35 LEAK + OPS CHECKS GOOD. (AN EMERGENCY WAS DECLARED)
- [SDR YENA2021091000566](https://openairdocs.org/sdr/YENA2021091000566.md): Apu · odor · Sep 6, 2021 · N563JB · Airbus A320232 · APU Core Engine
  > FLT 939, JFK-SJD. STRONG OIL ODOR ON A/C FIRST ASSITANCE FAS REPORTED SLIGHT ON DESCENT BUT EXTREMELY STRONG ON GROUND ( APU SYSTEM); PERFORMED INFO NOTICE 2017-T015I AND PLACED APU ON MEL 49-10-01A CAT C.MX4 UPDATED.PLCARD INSTALLED. OPEN
- [SDR YENA2021032500188](https://openairdocs.org/sdr/YENA2021032500188.md): Shear Plate · cracked · Mar 21, 2021 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, FUSELAGE / CENTER FUSELAGE / WING TO FUSELAGE FAIRING RH SUPPORT STRUCTURE FR41-42 SHEAR PLATE / CRACK - PERMANENT REPAIR; THIS REPAIR IS CLASSIFIED AS MAJOR PER JETBLUE EC A21-228-01
- [SDR YENA2021032500187](https://openairdocs.org/sdr/YENA2021032500187.md): Angle · damaged · Mar 21, 2021 · N563JB · Airbus A320232 · Aerodynamic Fairings
  > DURING HEAVY MAINTENANCE, R/H TI ANGLE AT FR 40-41 HAS LWR AFT HOLE OUT OF ROUND; (REF FAS SO# N563JB-01-01 NR# 00283 FAS EO# 21018 & JB E# A321-226) ACCOMPLISHED REPAIR OF ELONGATED HOLE AT THE WING FUSELAGE FAIRING R/H SUPPORT STRUCTURE SHEAR WEB BETWEEN FR
- [SDR YENA2019100710560](https://openairdocs.org/sdr/YENA2019100710560.md): Power Supply · inoperative · Oct 1, 2019 · N563JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, INOPERATIVE EPSU AT THE EMERGENCY EXIT LT IN PASSENGER CABIN. REPLACED THE EPSU IAW 33-51-38-400-001-A.
- [SDR YENA201906104304](https://openairdocs.org/sdr/YENA201906104304.md): Lens · missing · Jun 4, 2019 · N563JB · Airbus A320232 · Emergency Lighting
  > FT 1796, L1 DOOR EMERGENCY EXIT LIGHT COVER MISSING; RE-SECURED L1 DOOR THRESHOLD EMERGENCY EXIT LIGHT ASSY PER AMM. CHECKS OK.
- [SDR YENA2019040127163](https://openairdocs.org/sdr/YENA2019040127163.md): Fan · contaminated · Mar 27, 2019 · N563JB · Airbus A320232 · Turbine Engine Accessory Drive
  > FT # 1452, LEVEL 2 FUMES EVENT. ODER NOTICED AT CRUISE AND WAS SPORADIC DIRTY SOCK. ODER NOTIFIED IN COCKPIT AND FRONT GALLEY; EVIDENCE OF OIL FOUND IN THE INNER RIM OF FAN DISC CLEANED OIL AND RE-INSTALLED CONE AND FAIRING AS PER AMM 72-38-11-400-010-A. AS P
- [SDR YENA2018123126890](https://openairdocs.org/sdr/YENA2018123126890.md): Outflow Valve · failed · Dec 26, 2018 · N563JB · Airbus A320232 · Pressure Regulator/Outflow Valve
  > FT # 319, FLL-SLC. RETURNED TO FIELD. CABIN PRESSURE CONTROL 1+2 FAIL. AIR RETURN; R & R OUTFLOW VALVE IAW AMM 21-31-51.
- [SDR YENA201802080086](https://openairdocs.org/sdr/YENA201802080086.md): Floorbeam · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 HAS CORROSION AT FRAME 66 + 2" FORWARD OF BEAM REF NR 440458-30599, REMOVED AND REPLACED FLOORBEAM -Y1292 FRAME 66 IAW SRM 51-72-11 PARA 2D REF SCR 884892-00018.
- [SDR YENA201802080085](https://openairdocs.org/sdr/YENA201802080085.md): Door Sill · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE R2 DOOR SILL FWD OF FRAME 66. REMOVED THE DOOR SILL. FABRICATED TWO ANGLES AND ONE FILLER. TREATED, PRIMED, AND TOP COATED THE REPAIR. INSTALLED IAW SRM 53-41-14-300-001, FIG 001, SHT 5, REPAIR P
- [SDR YENA201802080084](https://openairdocs.org/sdr/YENA201802080084.md): Floor Support · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR SUPPORT, -Y1292, FRAMES 68-69. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, PARA 2D.
- [SDR YENA201802080083](https://openairdocs.org/sdr/YENA201802080083.md): Seat Track · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN SEAT TRACK, Y-765, AT FRAME 20. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-72-11, PARA 2D.
- [SDR YENA201802080082](https://openairdocs.org/sdr/YENA201802080082.md): Door Sill · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE L2 DOOR SILL. REMOVED AND REPLACED THE DOOR SILL IAW AMM SRM 51-71-11, AND 51-42-11.
- [SDR YENA201802080081](https://openairdocs.org/sdr/YENA201802080081.md): Door Sill · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE L2 DOOR SILL. REMOVED AND REPLACED THE DOOR SILL IAW AMM SRM 51-71-11, AND 51-42-11.
- [SDR YENA201802080080](https://openairdocs.org/sdr/YENA201802080080.md): Door Sill · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE L2 DOOR SILL. REMOVED AND REPLACED THE DOOR SILL IAW AMM SRM 51-71-11, AND 51-42-11.
- [SDR YENA201802080079](https://openairdocs.org/sdr/YENA201802080079.md): Floor Support · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FWD CABIN FLOOR SUPPORT, INBD OF THE SEAT TRACK, Y504, FRAME 15. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR YENA201802080078](https://openairdocs.org/sdr/YENA201802080078.md): Floor Support · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE AFT CABIN FLOOR SUPPORT -765, 2 INCHES FORWARD OF FRAME 66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, PAR 2D.
- [SDR YENA201802080077](https://openairdocs.org/sdr/YENA201802080077.md): Floor Support · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FWD CABIN FLOOR SUPPORT AT Y-254, REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-42-11.
- [SDR YENA201802080076](https://openairdocs.org/sdr/YENA201802080076.md): Seat Track · corroded · Feb 8, 2018 · N563JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FWD CABIN SEAT TRACK Y1292. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 52-42-11.
- [SDR YENA201710180851](https://openairdocs.org/sdr/YENA201710180851.md): Fuel Sys · leaking · Oct 18, 2017 · N563JB · Airbus A320232 · Aircraft Fuel Distribution System
  > EMERGENCY DECLARED, DIVERTED PASSING FL 240 AND APPROX 330 KTS, AIRCRAFT BEGAN A SIGNIFICANT VIBRATION. AIRCRAFT WAS SLOWED, AND VIBRATION CEASED AT APPROX 290 KTS. PASSING FL 240, RECEIVED FUEL AUTO FEED FAULT. FUEL PAGE SHOWED 12,000 LBS LEFT INNER TANK, 9,
- [SDR YENA201708300725](https://openairdocs.org/sdr/YENA201708300725.md): Engine · failed · Aug 30, 2017 · N563JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > REJECTED TAKE-OFF. NR 2 ENGINE FAIL ECAM AT 80 KTS. PERFORMED 05-51-26 INSPECTION IAW AMM 05-51-26 PB 601, NO DISCREPANCY. R & R THE 2 ENGINE.
- [SDR YENA20161023944](https://openairdocs.org/sdr/YENA20161023944.md): Coffeemaker · failed · Oct 23, 2016 · N563JB · Airbus A320232 · Buffet/Galleys
  > PILOT REPORTED AN ELECTRICAL BURNING ODOR WHEN FRONT COFFEE POTS WERE ON. ODOR DISAPPEARED WHEN COFFEE POTS WERE DEACTIVATED. R & R FWD GALLEY NR 1 COFFEEMAKER IAW AMM 25-35-15. PERFORMED OPS TEST. OPS TEST PASSED.
- [SDR YENA20160626600](https://openairdocs.org/sdr/YENA20160626600.md): Floorbeam · corroded · Jun 26, 2016 · N563JB · Airbus A320232 · Fuselage Main, Floor Beam
  > LT FLOORBEAM CORRODED AT FRAME 66; STR 23L. REPLACED FLOORBEAM IAW SRM REF 51-42-11 REF NR 440322-32307.
- [SDR YENA20160626599](https://openairdocs.org/sdr/YENA20160626599.md): Door Sill · corroded · Jun 26, 2016 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL CORRODED AROUND FASTENER HOLES FWD OF FRAME 66. REPAIRED IAW SRM REF 53-41-14, INSTALLED 2EA ANGLES REF NR 440322-32242.
- [SDR YENA20160626598](https://openairdocs.org/sdr/YENA20160626598.md): Floorbeam · corroded · Jun 26, 2016 · N563JB · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN RT SIDE FLOORBEAM -Y765 CORRODED AT FR 66+14". REPLACED BEAM IAW SRM REF 51-72-11, REF NR 440322-32200.
- [SDR YENA20160626597](https://openairdocs.org/sdr/YENA20160626597.md): Floorbeam · corroded · Jun 26, 2016 · N563JB · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM CORRODED AT FRAME 67 AND 67+10; Y765. REPLACED BEAM IAW SRM REF 51-72-11, REF NR 440322-32199.
- [SDR YENA20160626596](https://openairdocs.org/sdr/YENA20160626596.md): Door Sill · corroded · Jun 26, 2016 · N563JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL CORRODED AROUND FASTENER HOLE FRAME 68. REPAIRED SILL IAW SRM REF 53-41-14 REF NR 440322-32194.

Next page: https://openairdocs.org/aircraft/N563JB/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 = 'N563JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N563JB/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.