# Service difficulty reports: N559JB

A list on [N559JB](https://openairdocs.org/aircraft/N559JB.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 · 86 reports

- [SDR YENA2024100801355](https://openairdocs.org/sdr/YENA2024100801355.md): Support Web · corroded · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION SUPPORT WEB LOCATED BTR FR 69 AND FR 70 AT LEVEL STR 23R AT AFT GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1311389 TASKCARD: NR-00042) REF AEROMAN WO 2024-214/1 NR 2024-446420. REMOVED AND REPLACED SUPPORT WEB LOCATED BTW
- [SDR YENA2024100801354](https://openairdocs.org/sdr/YENA2024100801354.md): Support Web · corroded · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION SUPPORT WEB LOCATED BTW FR 69 AND FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA (CPCP FINDING); (RESOLVED ON W/O: 1311389 TASKCARD: NR-00043) REF AEROMAN WO 2024 214/1 NR 2024-446422. REMOVED AND REPLACED NEW SUPPORT WEB LOCATED
- [SDR YENA2024100801353](https://openairdocs.org/sdr/YENA2024100801353.md): Crossbeam · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 2, LOCATED ON CROSSBEAM SPLICING AREA FR16 LH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.106 INCHES, CRACK DIRECTION: 1 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00051) REF AE W/O
- [SDR YENA2024100801352](https://openairdocs.org/sdr/YENA2024100801352.md): Door Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE AT HOLE A OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00052) REF AE W/O# 2024-214/1. N/R# 2024 - 446434.PERFORMED PERMANENT REP
- [SDR YENA2024100801351](https://openairdocs.org/sdr/YENA2024100801351.md): Door Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE AT HOLE C OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00053) REF AE W/O# 2024-214/1. N/R# 2024 - 446435. PERFORMED PERMANENT RE
- [SDR YENA2024100801350](https://openairdocs.org/sdr/YENA2024100801350.md): Door Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE AT HOLE 6 OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00054) REF AE W/O# 2024-214/1. N/R# 2024 - 446436. PERFORMED PERMANENT RE
- [SDR YENA2024100801349](https://openairdocs.org/sdr/YENA2024100801349.md): Door Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 20 LH SIDE AT HOLE 6 OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00048) REF AE W/O# 2024-214/1. N/R# 2024 - 446433. PERFORMED PERMANENT RE
- [SDR YENA2024100801348](https://openairdocs.org/sdr/YENA2024100801348.md): Fitting · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL FITTING LAYER AT THE UPPER AND LOWER INBOARD HOLES OF DOOR STOP FITTING 7 LOCATED FRAME 16 RH AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00055) REF AE W/O# 2024-214/1. N/R# 2024 - 446432
- [SDR YENA2024100801347](https://openairdocs.org/sdr/YENA2024100801347.md): Door Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE AT HOLE C OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00056) REF AE W/O# 2024-214/1. N/R# 2024 - 446437. PERFORMED PERMANENT RE
- [SDR YENA2024100801346](https://openairdocs.org/sdr/YENA2024100801346.md): Stringer · corroded · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOC, BWT FR, 55 TO FR, 57 IN AFT CARGO COMPARTMENT (CPCP FINDING);(RESOLVED ON W/O: 1311389 TASKCARD: NR-00057) REF AE W/O# 2024-214/1. N/R# 2024 - 446603. REMOVED AND REPLACED STRINGER 43L LOC, BET FR 55 TO FR
- [SDR YENA2024100801345](https://openairdocs.org/sdr/YENA2024100801345.md): Window Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA RH SIDE FROM UPPER TENSION BOLT IN INBORD VERTICAL FLANGE. CRACK DIRECTION IS 10 O'CLOCK, CRACK LENGTH IS 0.080 INCH APPROX IN COCKPIT; (RESOLVED O
- [SDR YENA2024100801344](https://openairdocs.org/sdr/YENA2024100801344.md): Window Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA LH SIDE FROM UPPER TENSION BOLT IN I/B VERTICAL FLANGE. CRACK DIRECTION IS 2 O'CLOCK LENGTH IS 0.140 INCH APPROX IN COCKPIT; ARM W/O 2024 214/1 N/R
- [SDR YENA2024100801343](https://openairdocs.org/sdr/YENA2024100801343.md): Door Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68RH SIDE AT LOWER I/B HOLE OF DOOR STOP FITTING 1 AT AFT GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00066) REF: ARM W/O 2024 214/1 N/R 2024-446438. PERFORMED REPAIR ON FRAME 68 RH SIDE AT LOWER INBO
- [SDR YENA2024100801342](https://openairdocs.org/sdr/YENA2024100801342.md): Door Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE AT LOWER INBOARD HOLE OF DOOR STO P FITTING 1 AT AFT GALLEY AREA; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00067) PERFORMED REPAIR ON FRAME 68 LH SIDE AT LOWER INBOARD HOLE OF DOOR STOP FITTING 1 AT
- [SDR YENA2024100801341](https://openairdocs.org/sdr/YENA2024100801341.md): Web · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 LH WEB AFT FACE HORIZONTAL FLANGE LEVEL OF STR 22L. CRACK L= 0.580 INCH; (RESOLVED ON W/O: 1311389 TASKCARD: NR-00068) PERFORMED REPAIR ON FR68 LH WEB AFT FACE HORIZONTAL FLANGE LEVEL OF STR 22L I.A.W. E
- [SDR YENA2024100801340](https://openairdocs.org/sdr/YENA2024100801340.md): Window Frame · cracked · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FORWARD FUSELAGE / WINDSHIELD FRAME / CENTER POST LH & RH LOWER FASTENERS AREA / CRACKS - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9035-24 COVER REV.0 & PART 1-6 /2/ AIRBUS SB A320-53-1331 (REF. FAA AD 2020-17-03
- [SDR YENA2024100801339](https://openairdocs.org/sdr/YENA2024100801339.md): Door Frame · damaged · Oct 5, 2024 · N559JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, REAR FUSELAGESB53-1491 DOOR STOP FITTING NR 1 STR 22L FR 68 HOLE FILLET RADIUS CRACKED PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-9041-24 REV 0 (COVER, PARTS 1-4) /2/ AIRBUS RDAF 81468047/003/2024#B /3/ AIRBUS DOSSIER 81468047 /4/ AI
- [SDR YENA2024051400728](https://openairdocs.org/sdr/YENA2024051400728.md): Warning Message · illuminated · May 12, 2024 · N559JB · Airbus A320232 · Central Warning
  > FLT#1584, MCO-JFK. (AIRCRAFT DECLARED AN EMERGENCY INTO JFK) ' HYD Y RSVR LO LVL ECAM NO HYDL FLUID INDICATED ON ECAM.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023030600206](https://openairdocs.org/sdr/YENA2023030600206.md): None · none · Mar 6, 2023 · N559JB · Airbus A320232 · Air Conditioning System
  > FLT#87, ALB-FLL. 'INFLIGHT ADVISED DURING DESCENT THAT THERE WAS A STRONG AND PERSISTENT DIRTY SOCK ODOR. MX -270 FILLED OUT; PERFORMED LEVEL B REMOVAL OF THE CONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM (ECS) IAW AMM 21-00-00-615-803A. REMOVED AND REPLAC
- [SDR YENA2022072500706](https://openairdocs.org/sdr/YENA2022072500706.md): None · none · Jul 22, 2022 · N559JB · Airbus A320232 · Emergency Equipment
  > FLT#149, JFK-CHS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' R1 DOOR SHOWED DISARMED AFTER TAKEOFF. SLIGHT PRESSURE ON THE ARMING LEVER WOULD SHOW ARMED BUT WOULD NOT STAY; PERFORMED VISUAL INSPECTION OF R1 DOOR SLIDE, FOUND THE RIGHT TELESCOPIC FORK NOT F
- [SDR YENA2022062800624](https://openairdocs.org/sdr/YENA2022062800624.md): Proximity Sensor · failed · Jun 27, 2022 · N559JB · Airbus A320232 · Nose/Tail Landing Gear Attach Section
  > DURING HEAVY MAINTENANCE, AFTER TAKE-OFF AFTER GEAR RETRACTION ECAM MESSAGE: L/G GEAR NOT UPLOCKED FOLLOW ECAM ACTIONS AND QRH PROCEDURES STILL L/G NOT LOCKED UP. AT GEAR EXTENSION NORMAL GEAR DOWN AND LOCK 3 GREEN LIGHTS; PERFORMED TSM OF LG UPLOCK TGT POSITI
- [SDR YENA2022052700532](https://openairdocs.org/sdr/YENA2022052700532.md): Idg · failed · May 18, 2022 · N559JB · Airbus A320232 · AC Generator-Alternator
  > FLT#1597, JFK-DEN. 'DESCENDING ON ARRIVAL OUT 13,00 FEET GEN #1 FAILED ALSO A/P2 AND AUTO THRUST DISCONNECTED AS WELL AS FLIGHT DIRECTORS. THE TOP MCDU SCREEN FAILED MOMENTARILY ALSO. ( IDG 1 DISCONNECTED (N503-N655)); REPLACED #1 ENG IDG IAW AMM 24-21-51. OP
- [SDR YENA2021081600515](https://openairdocs.org/sdr/YENA2021081600515.md): Elevator System · out of rig · Aug 6, 2021 · N559JB · Airbus A320232 · Elevator Control System
  > FLT 222, PBI-BOS. AIRCRAFT VIBRATION ON CLIMBOUT FROM PBI STARTED AROUND FL170 FILLED OUT AIRCRAFT VIVRATION SURVEY FOR MORE DETAILS VIBRATION INTENSITY SCALE 4; PERFORMED AMM TASK 05-50-00-810-801-A. FOLLOWED DECISION TABLE AND LEAD TO BELIEVE ELEVATORS ARE T
- [SDR YENA2020081700424](https://openairdocs.org/sdr/YENA2020081700424.md): Flap Track · failed · Aug 11, 2020 · N559JB · Airbus A320232 · Trailing Edge Flap Control System
  > FLT 789, EMERGENCY DECLARED. ON APPROACH TO LANDING RECEIVED A FLAPS FAULT WHEN GOING FROM FLAP 1 TO FLAP 2. SLATS DEPLOYED BUT FLAPS DID NOT. ECAM RECYCLE DID NOT WORK. NORMAL LANDING WITHOUT FLAPS. R & R THE FLAP TRACK IAW AMM 27-54-49 & ADJUSTED FLAP TRA
- [SDR YENA2019101840594](https://openairdocs.org/sdr/YENA2019101840594.md): Fan · failed · Oct 14, 2019 · N559JB · Airbus A320232 · Air Distribution Fan
  > FT # 227, EWR-JFK. EMERGENCY DECLARED. DIVERTED TO JFK. AVIONIC SMOKE ECAM WITH ASSOCIATED LOUD NOISE AND ELECTRICAL BURNING SMELL. AFTER LANDING NOTED CABIN EXTRACT FAN CIRCUIT BREAKER POPPED; R & R AVIONIC FAN EXTRACT IAW AMM 21-26-51. OPS CHK GOOD. NO DEFEC
- [SDR YENA201906090320](https://openairdocs.org/sdr/YENA201906090320.md): Unknown · odor · Jun 9, 2019 · N559JB · Airbus A320232 · Air Distribution System
  > FT # 179, AFTER LANDING F/A'S COMPLAINED ALONG WITH PAX THROUGHOUT CABIN OF MUSTY/DIRTY SOCK SMELL AS DESCENT STARTED INTO LGB AT APPROXIMATELY 8000 UPON LANDING IN LGB FLIGHT CREW NOTICED SMELL ONCE COCKPIT DOOR WAS OPEN. C/W INFO NOTICE 2017-T015E, T/S TO B
- [SDR YENA201905317289](https://openairdocs.org/sdr/YENA201905317289.md): Unknown · odor · May 27, 2019 · N559JB · Airbus A320232 · Air Distribution System
  > FT # 477, LEVEL ONE ODOR DETECTED BY INFLIGHT CREW ON DESCENT BETWEEN 10.000 AND THE SURFACE, ROW 15 TO AFT OF CABIN DESCRIBED AS DIRTY SOCKS ODOR. STRONG BUT CLASSIFIED AS TRANSIENT AS IT DISSIPATED UPON LANDING; COMPLIED WITH INFORMATION NOTICE 207-T015D SE
- [SDR YENA2019041950200](https://openairdocs.org/sdr/YENA2019041950200.md): Filter · failed · Apr 15, 2019 · N559JB · Airbus A320232 · Air Distribution System
  > (RESOLUTION): FT # 71, FUMES IN AFT CABIN TURNED OFF PACK 2 AND FUMES DISSIPATED. FUMES CLAMINATION CHECK LIST C/W. ( PACKS - SINGLE (SPEEDBRAKES OK) (N503-N665)); R & R RH OZONE FILTER IAW AMM 21-51-41. OPS CHECKED NORMAL MX-4 UPDATED PLACARD REMOVED.
- [SDR YENA201808120612](https://openairdocs.org/sdr/YENA201808120612.md): Door Sill · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON R2 DOOR SILL AT FR66. REMOVED CORROSION ON R2 DOOR SILL AT FR66 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14-283-002 FIG 001 SHT 01. REMOVED AND REPLACED DOOR SILL IAW SRM 51-42-11 AND 51-72-11.
- [SDR YENA201808120611](https://openairdocs.org/sdr/YENA201808120611.md): Fitting · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR RT AFT SHEAR ANGLE FITTING AT FR69-70 HAS LOWER SURFACE CORROSION. REMOVED & REPLACED RT AFT SHEAR WEB ANGLE FITTING IAW SRM 51-72-11-911-001.
- [SDR YENA201808120610](https://openairdocs.org/sdr/YENA201808120610.md): Fitting · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR RT AFT SHEAR ANGLE FITTING AT FR69-70 HAS LOWER SURFACE CORROSION. REMOVED & REPLACED RT AFT SHEAR WEB ANGLE FITTING IAW SRM 51-72-11-911-001.
- [SDR YENA201808120609](https://openairdocs.org/sdr/YENA201808120609.md): Fitting · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR LT AFT SHEAR WEB ANGLE FITTING AT FR69+17 LOWER SURFACE CORROSION. REMOVED & REPLACED SHEAR WEB ANGLE FITTING AT LT FR 69 IAW SRM 51-72-11 PARA C.
- [SDR YENA201808120608](https://openairdocs.org/sdr/YENA201808120608.md): Bracket · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM ANGLE BRACKET AT FLOORBEAM -Y1732 AND FRAME 18. REMOVED & REPLACED FLOORBEAM ASSEMBLY - Y1732 IN ACCORDING TO SRM 51-42-11.
- [SDR YENA201808120607](https://openairdocs.org/sdr/YENA201808120607.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1162.5 AT FR 66. REMOVED AND REPLACED FLOORBEAM Y1162.5 AT FR 66 STR 23L IAW SRM 51-42-11 & 53-00-14-283-002.
- [SDR YENA201808120606](https://openairdocs.org/sdr/YENA201808120606.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM - Y 81 AT FR 17 + 10". REMOVED CORROSION VERIFIED BEYOND.024" LOSS LIMITS IAW SRM 53-11-14-283-004. REMOVED & REPLACED BEAM -Y81 AT FR 17 + 10" ON NR 440500-30481.
- [SDR YENA201808120605](https://openairdocs.org/sdr/YENA201808120605.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y765 AT FR 66. REMOVED CORROSION. OUT OF LIMITS IAW SRM 53-00-14-283-002. REMOVED & REPLACED FLOORBEAM IAW SRM 53-41-14 FIG 016.
- [SDR YENA201808120604](https://openairdocs.org/sdr/YENA201808120604.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1292 FR66+2. RPL AFT CABIN FLOORBEAM Y1292 PER SRM 53-00-14-283-002.
- [SDR YENA201808120603](https://openairdocs.org/sdr/YENA201808120603.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM -Y81 FR17 +16. RPL FWD CABIN FLOORBEAM -Y81 PER SRM 53-11-14, 51-44-11.
- [SDR YENA201808120602](https://openairdocs.org/sdr/YENA201808120602.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 AT FR68 +9. AFT CABIN FLOORBEAM -Y1292 FR68 +9 CORR RPL ON NR 30453.
- [SDR YENA201808120601](https://openairdocs.org/sdr/YENA201808120601.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 FR66 +6. REPLACED BEAM -Y1292 FR66+6 IAW SRM 51-42-11.
- [SDR YENA2018100920600](https://openairdocs.org/sdr/YENA2018100920600.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y1292 FR66+3; REF NR 440500-30452: CORR BEYOND BLEND LIM AFT CABIN FLR BEAM RPL ON NR 30453.
- [SDR YENA2018100920599](https://openairdocs.org/sdr/YENA2018100920599.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1292 AT FR67+10; REMOVED AND REPLACED BEAM IAW SRM 53-41-14 REF NR 30444 FOR ALL WORK ACCOMPLISHED.
- [SDR YENA2018100920598](https://openairdocs.org/sdr/YENA2018100920598.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOORBEAM -Y1732 AT FR18; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30482 FOR ALL WORK ACCOMPLISHED.
- [SDR YENA2018100920597](https://openairdocs.org/sdr/YENA2018100920597.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y765 AT FR66+2; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30456 FOR ALL WORK ACCOMPLISHED.
- [SDR YENA201808120596](https://openairdocs.org/sdr/YENA201808120596.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y765 AT FR66; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30447 FOR WORK ACCOMPLISHED.
- [SDR YENA2018100920595](https://openairdocs.org/sdr/YENA2018100920595.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y765 AT FR68; REMOVED AND REPLACED BEAM IAW SRM 51-42-11 REF NR 30455 FOR ALL WORK ACCOMPLISHED.
- [SDR YENA2018100920594](https://openairdocs.org/sdr/YENA2018100920594.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM -Y765 AT FR66+8 TO 67+8; REMOVED AND REPLACED BEAM IAW SRM 51-42-11 REF NR 30454 FOR WORK ACCOMPLISHED.
- [SDR YENA2018100920593](https://openairdocs.org/sdr/YENA2018100920593.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y512 AT FR66; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30458 FOR ALL WORK ACCOMPLISHED.
- [SDR YENA2018100920592](https://openairdocs.org/sdr/YENA2018100920592.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y512.5 AT FR66; REMOVED AND REPLACED BEAM IAW SRM 51-72-11 REF NR 30462 FOR WORK ACCOMPLISHED.
- [SDR YENA2018100920591](https://openairdocs.org/sdr/YENA2018100920591.md): Floorbeam · corroded · Aug 12, 2018 · N559JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y1292 AT FR67+16; REMOVED AND REPLACED BEAM IAW SRM 51-42-11 REF NR 30445 FOR WORK ACCOMPLISHED.

Next page: https://openairdocs.org/aircraft/N559JB/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 = 'N559JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N559JB/reports

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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.