# Service difficulty reports: N586JB

A list on [N586JB](https://openairdocs.org/aircraft/N586JB.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 YENA2026051500461](https://openairdocs.org/sdr/YENA2026051500461.md): Battery · no test · May 14, 2026 · N586JB · Airbus A320232 · Emergency Lighting
  > FLT 1752, SJU-TPA. EMERGENCY LIGHT BATTERY FIN 12WL FAILED TEST, REMOVED AND REPLACED EMERG LIGHT BATTERY FIN 13WL IAW AMM 33-51-38.
- [SDR YENA2026021800221](https://openairdocs.org/sdr/YENA2026021800221.md): Engine · slow · Feb 17, 2026 · N586JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > FLT 2008, FLL-FLL. STARTED OUT TAKE-OFF ROLL, SPOOLED EPR ON BOTH ENG'S TO 1.05, ALTHOUGHT ENG'S STARTED TO ACCELERATE BOTH ENG;S LAGGED IN THRUST, SLOWER THEN NORMAL WITH THE RIGHT ENGINE ACCELERATING SOMEWHAT FASTER THEN THE LEFT. WE REJECTED T/O, LOW SPEED
- [SDR YENA2025022500208](https://openairdocs.org/sdr/YENA2025022500208.md): Door Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) (ON DOOR STOP FITTING 7 HOLE 1 FR16LH. LENGTH 0.100 INCH. CRACK DIRECTION 9 O’CLOCK); REF AEROMAN NR 2025 – 29477, W/O: 2025 13/1 PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT L
- [SDR YENA2025022500207](https://openairdocs.org/sdr/YENA2025022500207.md): Door Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) ON DOOR STOP FITTING 7 HOLE 1 FR16RH. LENGTH 0.100 INCH. CRACK DIRECTION 3 O’CLOCK; REF AEROMAN W/O: 2025 13 / 1, NR 29476, PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT LEVEL DO
- [SDR YENA2025022500206](https://openairdocs.org/sdr/YENA2025022500206.md): Door Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE:CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) ON DOOR STOP FITTING 7 HOLE 3 FR16RH. LENGTH 0.100 INCH. CRACK DIRECTION 6 O’CLOCK.; REF AEROMAN W/O: 2025 13 / 1, NR 29478, PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT LEVEL DO
- [SDR YENA2025022500205](https://openairdocs.org/sdr/YENA2025022500205.md): Stringer · corroded · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L AT LEVEL FR55 IN AFT CARGO COMPARTMENT; REMOVED AND REPLACED STRINGER 43L AND FASTENERS LOC. BTW. FRAME 54 TO FRAME 60 I.A.W. A320 SRM 51-42-11 AND DRAWING E53470342. ALL WORK WAS PERFORMED ON AEROMAN WO2025-13
- [SDR YENA2025022500204](https://openairdocs.org/sdr/YENA2025022500204.md): Skin · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR16 RH SIDE AT HOLE A. CRACK DIRECTION 9 OCLOCK (VIEW FROM OUTSIDE) AND CRACK LENGTH 0.100 INCHES (1EA); PERFORMED PERMANENT REPAIR LOC. ON DOUBLE JOGGLE AREA HOLE A ON FR16 RH SIDE IAW A320 SRM 53-11-12-30
- [SDR YENA2025022500203](https://openairdocs.org/sdr/YENA2025022500203.md): Skin · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION FRAME 66 AT LEVEL STR23 L AND BETWEEN Y1292 TO Y1732 AT AFT GALLEY AREA; REMOVED AND REPLACED INTERNAL STRUCTURE SECTION CONNECTION AND FASTENERS LOCATED FRAME 66 AT LEVEL STR23L AND BETWEEN
- [SDR YENA2025022500202](https://openairdocs.org/sdr/YENA2025022500202.md): Door Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND DOOR STOP 1 HOLE H3 FR68LH. CRACK DIRECTION 11 OCLOCK. CRACK LENGTH 0.100 INCH; REF AEROMAN WO 2025 13/1 NR 2025-29474; ACCOMPLISHED THE REPAIR OF THE CRACK DAMAGE FOUND ON THE REAR FUSELAGE FR68 LHS ( NEAR STR
- [SDR YENA2025022500201](https://openairdocs.org/sdr/YENA2025022500201.md): Window Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND WINDSHIELD CENTER POST LH SIDE LOC UPPER CORNER.CRACK DIRECTION 1 O'CLOCK. CRACK LENGTH 0.250 INCH.REF AEROMAN WO 2025 13/1 NR 2025-29453; ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACK DAMAGE ON THE LH WINDSHI
- [SDR YENA2025022500200](https://openairdocs.org/sdr/YENA2025022500200.md): Window Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOUND WINDSHIELD CENTER POST LH SIDE LOC LOWER CORNER.CRACK DIRECTION 5 O'CLOCK. CRACK LENGTH 0.500 INCH.); REF AEROMAN WO 2025 13/1 NR 2025-29454; ACCOMPLISHED THE P
- [SDR YENA2025022500199](https://openairdocs.org/sdr/YENA2025022500199.md): Window Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOUND CONTINUITY FITTING WINDSHIELD RH SIDE. CRACK DIRECTION VERTICAL. CRACK LENGTH 0.200 INCH.); REF AEROMAN WO 2025 13/1 NR 2025-29455; ACCOMPLISHED THE PERMANENT R
- [SDR YENA2025022500198](https://openairdocs.org/sdr/YENA2025022500198.md): Access Panel · damaged · Feb 23, 2025 · N586JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: ELONGATED HOLES ON FUEL ACCESS PANEL 640MB CUT OUT BTW RIB 17 TO RIB 18 ON RH WING (2 EA); (RESOLVED ON W/O: 1348393 TASKCARD: NR-00025) REF AEROMAN WO 2025 13/1 NR 2025-29526; PERFORMED PERMANENT REPAIR ON BOTTOM SKIN CUT-OUT BTW RI
- [SDR YENA2025022500197](https://openairdocs.org/sdr/YENA2025022500197.md): Support · corroded · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION LOWER SILL LH LOC. BTW FRAME 66 AND FRAME 68 AT AFT GALLEY AREA (CPCP FINDING); REF AEROMAN WO 2025 13/1 NR 2025-29665; PERFORMED PERMANENT REPAIR ON LOWER SILL LH LOC. BTW FRAME 66 AND FRAME 68 AT AFT GALLEY AREA I.A.W. A3
- [SDR YENA2025022500196](https://openairdocs.org/sdr/YENA2025022500196.md): Firewall · not reported · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / SB-53-1500 TAIL CONE / LH/RH FIREWALL / BTWN FR81-83 / DEVIATION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2025022500195](https://openairdocs.org/sdr/YENA2025022500195.md): Window Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ FWD WINDSHIELDS / CENTER POST LOWER NODE & CONTINUITY FITTING LH/RH AREAS / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2025022500194](https://openairdocs.org/sdr/YENA2025022500194.md): Door Frame · cracked · Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 LH AND STGR 22 / DOOR STOP FITTING #1 / LOWER INBD HOLE / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED AS A MAJOR REPAIR)
- [SDR YENA2025010600029](https://openairdocs.org/sdr/YENA2025010600029.md): Skin · corroded · Jan 3, 2025 · N586JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION EXTERNAL SKIN LOC.AFT VENT OUTLET BETWEEN FR69 TO FR70 AND S TR 30R TO 33R LOWER FUSELAGE; REF AEROMAN N/R 2024-652123, PERFORMED PERMANENT REPAIR LOC. EXTERNAL SKIN AFT VENT OUTLET BETWEEN FR69 TO FR70 AND STR 30R TO 33R LO
- [SDR YENA2025010600028](https://openairdocs.org/sdr/YENA2025010600028.md): Door · cracked · Jan 3, 2025 · N586JB · Airbus A320232 · Service Doors
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND OPEN HOLE H3 ON DOOR STOP 1 FR68RH. CRACK DIREC TION 6 OCLOCK AND DEPTH 0.100 INCH; REF AEROMAN N/R 2024-652650, PERFORMED PERMANENT REPAIR ON FR68 RH AT LOWER INB FASTENER HOLE OF DOOR STOP FITTING #1 IAW A320
- [SDR YENA2025010600027](https://openairdocs.org/sdr/YENA2025010600027.md): Placard · missing · Jan 3, 2025 · N586JB · Airbus A320232 · Lavatories
  > DURING HEAVY MAINTENANCE: REF VTASK CARD A1124092-01 E/F WASTE FLAP DOOR PLACARD INSTALLATION- SPACEFLEX LAVATORIES- A320M / A321HD; AEROMAN ACCOMPLISHED TC A1124092-01 W/O 1353055. MAJOR ALTERATION.
- [SDR YENA2025010600026](https://openairdocs.org/sdr/YENA2025010600026.md): Stringer · corroded · Jan 3, 2025 · N586JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 31R LOC, BTW FR, 65 TO FR, 66 IN BULK CARGO COMPARTMENT (CPCP RELATED), (RESOLVED ON W/O: 1342223 TASKCARD: NR-00033) REF AEROMAN N/R 2024-652843, EVALUATED CORROSION LOCATED ON STRINGER 31R AT LEVEL FR65 AND NOT FO
- [SDR YENA2025010600025](https://openairdocs.org/sdr/YENA2025010600025.md): Fitting · cracked · Jan 3, 2025 · N586JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING LH SIDE. CRACK LENGTH: 0. 200 INCHES APPROX; ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMING CENTER POST LOWER ATTACHMENT AT AREAS A1 (LHS) AND D1 (RHS) IN ACCORDA
- [SDR YENA2025010600024](https://openairdocs.org/sdr/YENA2025010600024.md): Windshield · cracked · Jan 3, 2025 · N586JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON THE WINDSHIELD CENTRAL LOWER NODE, AROUND UP PER TENSION BOLT LH SIDE. CRACK DIRECTION: 1 OCLOCK, CRACK LENGTH: 0.1 50 INCHES APPROX; ACCOMPLISH THE PERMANENT REPAIR OF THE CRACKS ON THE WINDSHIELD FRAMING CE
- [SDR YENA2025010600023](https://openairdocs.org/sdr/YENA2025010600023.md): Panel · elongated · Jan 3, 2025 · N586JB · Airbus A320232 · Fuel Storage
  > DURING HEAVY MAINTENANCE: ELONGATED HOLE CUT OUT AREA FUEL TANK ACCESS PANEL BTW RIB 14 AND RIB 15 RH WING; (RESOLVED ON W/O: 1342223 TASKCARD: NR-00035) REF WO 2024 292/1 NR 2024-652732 PERFORMED PERMANENT REPAIR ON BOTTOM SKIN PANEL 2 LOCATED BTW RIB 14-RIB
- [SDR YENA2025010600022](https://openairdocs.org/sdr/YENA2025010600022.md): Light · inoperative · Jan 3, 2025 · N586JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: EMERGENCY LIGHT AT EPSU 12WL FAILED TEST; REF AEROMAN WO 2024 292/1 NR 2024-652950 REMOVED AND REPLACED EPSU AT 12WL IAW AMM 33-51-38-000-001 AND AMM 33-51-38-400-001-A. EMERGENCY LIGHT TEST GOOD IAW AMM 33-51-00-710-006-A.
- [SDR YENA2025010600021](https://openairdocs.org/sdr/YENA2025010600021.md): Window Frame · cracked · Jan 3, 2025 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ WINDSHIELD FRAME / CENTER POST / LOWER NODE AREA / CRACK DAMAGE - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9061-24 (COVER + PARTS 1-5) /2/ AIRBUS SB A320-53-1331 (REF. FAA AD 2020-17-03) /3/ AIRBUS R
- [SDR YENA2024060700841](https://openairdocs.org/sdr/YENA2024060700841.md): Control Unit · failed · Jun 4, 2024 · N586JB · Airbus A320232 · Landing Gear System
  > FLT#1844, BGI-BOS. (AIRCRAFT DECLARED AN EMERGENCY AND DID AN AIR TURN BACK TO BGI). 'EIU 1 FAIL; LGCIU 1 FAIL, MULTIPLE ABNORMAL ECAMS ND ALERTS. UNABLE TO DECIPHER WHICH PROCEDURE TO FOLLOW. DELARED EMERGENCY AND RETURNED TO BGI. LANDING WAS NOT OVERWEIGHT;
- [SDR YENA2024050600709](https://openairdocs.org/sdr/YENA2024050600709.md): Tachometer · failed · May 4, 2024 · N586JB · Airbus A320232 · Landing Gear Brake System
  > FLT#1694, MCO-HPN. (AIRCRAFT DIVERTED TO JFK) 'BRAKES AUTO BRK FAULT. BRAKE RELEASED. AFTER TAKEOFF CLIMBING OUT OF MCO; FOUND #1 TIRE TACH (19GG) AT FAULT REMOVED AND REPLACED TACH 19GG IAW AMM 32-47-57. ALL OPS CHECK GOOD CHECK FOR CONTINUED SVC.'
- [SDR YENA2023091501087](https://openairdocs.org/sdr/YENA2023091501087.md): Unknown · unknown · Sep 12, 2023 · N586JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > FLT#1447, HPN-TPA. ' USED EMERGENCY GEAR EXTENSION FOR LANDING PER QRH PROCEDURE FOR ABOVE ENTRY; RESTORED GRAVITY GEAR EXTN TO RIGGED POSITION (SYSTEM RESET) IAW AMM 32-33-00-710-001-A.
- [SDR YENA2023062700739](https://openairdocs.org/sdr/YENA2023062700739.md): Unknown · unknown · Jun 26, 2023 · N586JB · Airbus A320232 · Pneumatic System
  > FLT#1902, FLL-MCO. 'DURING CLIMBOUT AIR ENG 2 BLEED LEAK COORDINATING WITH MAINT CONTROL & AFTER COMPLYING WITH QRH 2-27, THREE RESETS WERE ATTEMPTED. THE THIRD RESET LASTED FOR TEN MINUTES AND THEN FAILED; FOUND ENG 2 PRECOOLER SEAL TORN, REPLACED SEAL PER AM
- [SDR YENA2023061900676](https://openairdocs.org/sdr/YENA2023061900676.md): Unknown · unknown · Jun 18, 2023 · N586JB · Airbus A320232 · Air Conditioning System
  > FLT#371, LGA-FLL. 'LEVEL 1 ODOR/FUME EVENT COCKPIT ISOLATION PROCEDURE ACCOMPLISHED - ODOR DISSIPATED. ODOR WAS DETECTED DESCENDING THROUGH APPROX 10,000 FEET.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2022092700974](https://openairdocs.org/sdr/YENA2022092700974.md): None · none · Sep 23, 2022 · N586JB · Airbus A320232 · Fuselage, Stabilizer Attach Fittings
  > DURING HEAVY MAINTENANCE: REF. AEROMAN N/R 2022-486863 - CRACK INDICATION ON FRAME 35 PRESSURE BULKHEAD LH SIDE FROM FASTENER L OWER OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTIONS ARE 3 AND 9 O'CLOCK, CRACK LENGTH IS 0.500 INCHES APPROX, IN FWD CARGO COM
- [SDR YENA2022092700973](https://openairdocs.org/sdr/YENA2022092700973.md): None · none · Sep 23, 2022 · N586JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 35 & STR 30L / PRESSURE BULKHEAD / CRACK AT FASTENER HOLE – TIME-LIMITED REPAIR. (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2022042800420](https://openairdocs.org/sdr/YENA2022042800420.md): None · failed · Apr 18, 2022 · N586JB · Airbus A320232 · Air Conditioning System
  > FLT#1287, PVD-PBI. ' DIRTY SOCK SMELL ON DESCENT RAN ODOR REC 3 ISOLATION PROCEDURES SEEMED LIKE PACK 1 WAS AT FAULT; PERFORMED PACKS BURN PROCEDURE IAW TSM TASK 05-50-810-831A AND INFORMATION NOTICE 2017-T051 1.NO ODOR PRESENT IN THE CABIN OR FLIGHT DECK. THI
- [SDR YENA2022040600338](https://openairdocs.org/sdr/YENA2022040600338.md): Proximity Sensor · failed · Apr 4, 2022 · N586JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > FLT#1834, PAP-JFK. (AIRCRAFT DECLARED AN EMERGENCY). 'NOSEGEAR "UNLOCKED " LIGHT STARTED FLASHING ABOUT(.5 HOURS INTO FLIGHT. NEXT, IT CAME ON STEADY W/"L/G CTRL & RED TRIANGLE ON THE ECAM WHEEL PAGE. NEXT, THE "LGCIU (2) 'ECAM MESSAGE CAME ON. UNEVENTFUL L
- [SDR YENA2021061600369](https://openairdocs.org/sdr/YENA2021061600369.md): Bleed Air Sys · odor · Jun 11, 2021 · N586JB · Airbus A320232 · Engine Bleed Air System
  > FLT 1080, LAX-LAS. AT APPLICATION OF TAKE OFF POWER STRONG DIRTY SOCK ODOR SEEMS TO DISAPATE AFTER 5 MIN BUT REMAINED. RAN ISO CHECK LIST THINK IT WAS WORSE WITH PACK 1 BOTH PILOT & #1 FA CONFIRMED ODOR. ( BLEED AIR SUPPLY SYSTEMS); PLACED ON MEL 36-11-01 CON
- [SDR YENA201909080532](https://openairdocs.org/sdr/YENA201909080532.md): Floorbeam · corroded · Sep 8, 2019 · N586JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION DISCOVERED ON FLOORBEAM -Y254 FR 19 FWD GALLEY; REF NR 2019-257795. REPLACED FLOORBEAM -Y254 ON FR 12 TO FR 24 RT SIDE IAW SRM 51-72-11 & DRAWING D53111462 AT FWD GALLEY.
- [SDR YENA201909080529](https://openairdocs.org/sdr/YENA201909080529.md): Frame · cracked · Sep 8, 2019 · N586JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, CRACK FRAME SECTION CONNECTION LOCATED FR68 LT SIDE; REF NR 2019-197/1-2019-257858 - REPLACED FR SECTION 68 CONNECTION LT SIDE AT STR 24L IAW SRM 51-72-11 AND 51-42-11, DRAWING E53474250.
- [SDR YENA2018110830766](https://openairdocs.org/sdr/YENA2018110830766.md): Exhaust Vent · corroded · Oct 31, 2018 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > FT # 344, STI-FLL. FOUND LAV EXHAUST VENT CORRODED DURING WALK AROUND; REF HAECO NR 440531-32003, REMOVED CORROSION AND INSTALLED REPAIR IAW A320 SRM 53-41-11-300-004. AT FR 69 TO 70 STR 31 RH. REPAIR IS A CAT A PERMANENT NO SRI REQUIRED.
- [SDR YENA201712110996](https://openairdocs.org/sdr/YENA201712110996.md): Door Sill · corroded · Dec 11, 2017 · N586JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN R2 DOOR SILL Y-1732 23R FR 68; REPAIRED MAIN CABIN R2 DOOR SILL AT Y-1732 STR 23R FR 68 IAW A320-41-14-300-001.
- [SDR YENA201712110995](https://openairdocs.org/sdr/YENA201712110995.md): Floorbeam · corroded · Dec 11, 2017 · N586JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN FLOOR BEAM Y-1292 FR68 + 2 STR 23R; REMOVED AND REPLACED MAIN CABIN FLOOR BEAM Y-1292 FR 68 + 2 STR 23R. IAW A320 SRM 53-41-14, 53-00-14-283-002, 51-72-11.
- [SDR YENA201712110994](https://openairdocs.org/sdr/YENA201712110994.md): Floorbeam · corroded · Dec 11, 2017 · N586JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FLOORBEAM Y-1292 FR 68 STR 23; REMOVED AND REPLACED MAIN CABIN FLOOR BEAM Y-1292 FR 68 STR23R IAW A320 SRM 53-00-14-283-002, 53-41-14 FIG 110.
- [SDR YENA201712110993](https://openairdocs.org/sdr/YENA201712110993.md): Floor Support · corroded · Dec 11, 2017 · N586JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOOR BEAM Y1292 FRAME 68 STR 23LH; REMOVED AND REPLACED FLOORBEAM FROM FR68 TO FR 69 AT Y1292 STR 23 LH AFT CABIM IAW A320 SRM 51-72-11, 53-41-14 FIG 001, 53-00-14-283-002.
- [SDR YENA201712110992](https://openairdocs.org/sdr/YENA201712110992.md): Floorbeam · corroded · Dec 11, 2017 · N586JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED INSIDE CABIN, LEFT SIDE FRAME 68 STR23L, BEAM Y765; REMOVED AND REPLACED MAIN CABIN FLOOR BEAM Y765 FR 68 SRT 23L IAW A320 SRM 53-41-14 FIG 001, 53-00-14-283-002.
- [SDR YENA201711090889](https://openairdocs.org/sdr/YENA201711090889.md): Computer · failed · Nov 9, 2017 · N586JB · Airbus A320232 · Flight Control System
  > JUST AFTER LEVEL OFF, IN CRUISE FL 350, RECEIVED A FLT CNTL ELAC 2 FAULT. PERFORMED QRH PROCEDURE WITH UNSUCCESSFUL RESET. DIVERTED. FOR CHECK PITCH CHANGE OVER OF ELAC 2. R & R THE NR 2 ELAC IAW AMM 27-93-34. TESTED GOOD AND OPERATIONAL.
- [SDR YENA201709040737](https://openairdocs.org/sdr/YENA201709040737.md): Transducer · malfunctioned · Sep 4, 2017 · N586JB · Airbus A320232 · Engine Vibration Analyzer
  > NR 2 ENGINE N1 AND N2 VIBRATION HIGH. MAX N1 9.9. MAX N2 VALUE 6.2. VIBRATION FELT IN CABIN FLOOR ALL OTHER INDICATION NORMAL. QRH PROCEDURE APPLIED. DIVERTED. TROUBLESHOT IAW TSM 77-32-00-810-807. R & R VIBRATION TRANSDUCER OF THE NR 2 ENGINE. WIRING FRO
- [SDR YENA20151227665](https://openairdocs.org/sdr/YENA20151227665.md): Actuator · inoperative · Dec 27, 2015 · N586JB · Airbus A320232 · Landing Gear Actuator
  > AIR TURNBACK TO DEPARTURE, L/G GEAR NOT UP LOCKED AFTER GEAR RETRACTION; R & R NLG RETRACTION ACTUATOR CYLINDER IAW AMM 32-31-22-04. OPS & LEAK CHECK NORMAL. ACFT OK FOR SERVICE.
- [SDR YENA20150830402](https://openairdocs.org/sdr/YENA20150830402.md): Battery · failed · Aug 30, 2015 · N586JB · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE, AFT EMERGENCY LIGHTS FAILED TEST, R & R AFT POWER SUPPLY AND BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR YENA20141101240](https://openairdocs.org/sdr/YENA20141101240.md): Power Supply · no test · Nov 1, 2014 · N586JB · Airbus A320232 · Emergency Lighting
  > DURING ACCOMPLISHMENT OF TC A320-33-51-00-710-003, FOUND 13WL EPSU FAILED CAPACITY TEST. R & R EPSU AT POSITION 13WL IAW AMM 33-51-38. OPS CHECK GOOD.
- [SDR YENA20130608123](https://openairdocs.org/sdr/YENA20130608123.md): Gcu · faulty · Jun 8, 2013 · N586JB · Airbus A320232 · AC Generation System
  > DIVERTED, DURING CLIMBOUT OF 19,000 FT POSSIBLE LIGHTNING STRIKE. MULTIPLE ELECTRICAL FAILURES. NR 1 GENERATOR, ALL EFIS DISPLAYES WENT BLANK. F/O'S CAME BACK FOLLOWED BY CAPTAINS 1 MINUTE LATER. LIGHTNING STRIKE INSPECTION PERFORMED IAW AMM 05-51-200-001-

Next page: https://openairdocs.org/aircraft/N586JB/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 = 'N586JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N586JB/reports

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