# Service difficulty reports: N564JB

A list on [N564JB](https://openairdocs.org/aircraft/N564JB.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 · 99 reports

- [SDR YENA2025102801064](https://openairdocs.org/sdr/YENA2025102801064.md): Epsu · failed · Oct 26, 2025 · N564JB · Airbus A320232 · Emergency Lighting
  > FLT#1761, LGA-PBI. "OVERWING EMER EXIT LIGHT NOT ILLUMINATING; MESSAGE "EPSU INT LOAD EMER R" ON CIDS 1 GRD SCAN. R/R 12WL EPSU AND BATT IAW AMM 33-51-38. EMER BATT TEST NOW OK BUT LOWER O/W EMER EXIT LTS STILL DON'T WORK. T/S TO CONT."
- [SDR YENA2025041000385](https://openairdocs.org/sdr/YENA2025041000385.md): Unknown · noise · Apr 5, 2025 · N564JB · Airbus A320232 · Standard Practices/Structures
  > FLT#1853, JFK-PBI. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'WHEN CLIMBING THR 10000 FT STARTER TP HEAR LOUD POPPING NOISE AT L1 DOOR AS IF SOMETHING HITTING FUSELAGE; ACCOMPLISHED A GVI "CHAP 5" INSPECTION FOUND NO LOOSE PANELS OR ADDITIONAL SEIGHT AS DIS
- [SDR YENA2025012200097](https://openairdocs.org/sdr/YENA2025012200097.md): Contactor · faulted · Jan 17, 2025 · N564JB · Airbus A320232 · Electrical Power System
  > FLT#821, JFK-NAS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' ELEC BCL 2 FAULT ECAM APPEARED WHILE IN CRUISE; AS PER TSM 24-38-00-810-848-A & ASM 24-38-02, REPLACED CONTACTOR 6PB2 IAW AMM 24-38-58. OPS TEST OK. NO FAULTS NOTED. (REPLACED RELAY 16XC - NO FI
- [SDR YENA2025010700026](https://openairdocs.org/sdr/YENA2025010700026.md): O-Ring · leaking · Jan 5, 2025 · N564JB · Airbus A320232 · Hydraulic System, Main
  > FLT#1736, STI-JFK. (AIRCRAFT DECLARED AN EMERGENCY) 'DURING CRUISE FLIGHT " HYD Y RSVR LO LVL" ECAM + QRH PROCEDURES APPLIED; REF. L.P. ' S 4156052 ITEMS 1 (REPLACED EDP IAW AMM 29-13-51 LEAK CHECK REQUIRED REF LGP 4156054 ITEM 1 (LEAK CH'D # 2 HYD EDP, REF.
- [SDR YENA2024042900668](https://openairdocs.org/sdr/YENA2024042900668.md): Unknown · odor · Apr 25, 2024 · N564JB · Airbus A320232 · Air Distribution System
  > FLT#1173, EWR-TPA. 'ODOR/FUME EVENT REPORTED BY INFLIGHT DURING DECENT AT 6K FEET; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION, ISOLATED FAULT TO TYPE 10,(A)1,C PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-085-D. AIRCRAFT IS OK FOR SERVICE.'
- [SDR YENA2024041700635](https://openairdocs.org/sdr/YENA2024041700635.md): Slide Raft · failed · Apr 12, 2024 · N564JB · Airbus A320232 · Escape Slide
  > FLT#1281, BOS-RIC. 'PASSENGER OR OVER WING DOOR SLIDE/SLIDE RAFTS (WITHOUT PASSENGERS; INSTALLED L1 SLIDE PER AMM 25-62-44. REACTIVATED L1 DOOR ASSIST BOTTLE. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED.'
- [SDR YENA2024022900306](https://openairdocs.org/sdr/YENA2024022900306.md): Unknown · odor · Feb 29, 2024 · N564JB · Airbus A320232 · Air Distribution System
  > FLT#765, JFK-GCM. 'CABIN ODOR ON DESCENT INTO GCM (DIRTY SOCK); FOLLOWED INFORMATION NOTICE 2017-T015J FOR REPORTED CABIN ODOR. PERFORMED ENGINE RUNS WITH FLIGHT CREW IAW AMM 71-00-00-710-012-B. RAN BOTH ENGINES WITH BLEEDS AND PACKS ON. NO CABIN ODOR / FUME
- [SDR YENA2024020800254](https://openairdocs.org/sdr/YENA2024020800254.md): Unknown · odor · Feb 6, 2024 · N564JB · Airbus A320232 · Air Distribution System
  > FLT#1480, FLL-DCA. 'DIRTY SOCK ODOR SMELLED IN AFT CABIN.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024020500225](https://openairdocs.org/sdr/YENA2024020500225.md): Unknown · odor · Feb 5, 2024 · N564JB · Airbus A320232 · Air Distribution System
  > FLT#1509, FLL-PAP. 'CABIN CREW REPORTS DIRTY SOCK MELL IN AFT CABIN ON FINAL DESCENT MILD ODOR IN FWD CABIN ( PACKS).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024011600059](https://openairdocs.org/sdr/YENA2024011600059.md): Unknown · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 42L BTW FR 56 TO FR 59 IN AFT CARGO COMPARTMENT / (RESOLVED ON W/O: 1258020 TASKCARD: NR-00022) REF AEROMAN N/R 2023-708948,PERFORMED REPAIR STRINGER 42L LOC. BTW FR 57 TO FR 59 IN AFT CARGO COMPARTMENT IAW A320 SR
- [SDR YENA2024011600058](https://openairdocs.org/sdr/YENA2024011600058.md): Unknown · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON UPPER INB FASTENER HOLE OF INTERCOSTAL FITTI NG AT DOOR STOP Ñ7 AREA FR16 LH. CRACK DIRECTION 5 OCLOCK. CRACK D= 0. 150 INCH. / REF AEROMAN NR 2023 708769 WO 2023 361/1 REMOVED AND REPLACED INTERCOSTAL FITTIN
- [SDR YENA2024011600057](https://openairdocs.org/sdr/YENA2024011600057.md): Door Frame · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON UPPER INB FASTENER HOLE OF INTERCOSTAL FITTING AT DOOR STOP N7 AREA FR16 RH. CRACK DIRECTION 8 OCLOCK. CRACK D= 0. 135 INCH. / REF AEROMAN NR 2023-708768 WO 2023 361/1 REMOVED AND REPLACED INTERCOSTAL FITTING
- [SDR YENA2024011600056](https://openairdocs.org/sdr/YENA2024011600056.md): Unknown · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE H2 ON CROSS BEAM SPLICING AREA, CRACK DIRCTION IS 12 OCLOCK, AT FWD GALLEY AREA (1 EA) / REF AEROMAN NR 2023-708962 WO 2023 361/1 PERFORMED PERMANENT REPAIR FR16R/H ON CROSSBE
- [SDR YENA2024011600055](https://openairdocs.org/sdr/YENA2024011600055.md): Unknown · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION EXISTING COUPLING REPAIR LOC ON STR 43L BTW FR 56 TO FR 57 I N AFT CARGO COMPARTMENT / (RESOLVED ON W/O: 1258020 TASKCARD: NR-00031) REF AEROMAN NR 2023-708943 WO 2023 361/1 PERFORMED PERMANENT REPAIR LOCATED ON STR 43L BTW
- [SDR YENA2024011600054](https://openairdocs.org/sdr/YENA2024011600054.md): Door Frame · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACKDIRECTIONS ARE 6 AND 12 OCLO CK, AT AFT GALLEY AREA (2 EA) / RESOLVED ON W/O: 1258020 TASKCARD: NR-00032 REF AEROMAN NR 20
- [SDR YENA2024011600053](https://openairdocs.org/sdr/YENA2024011600053.md): Unknown · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Service Doors
  > DURING HEAVY MAINTENANCE: WEAR ON HANDLE CUT OUT ACCESS DOOR 824 AFT AVIONIC COMPARTMENT / EVALUATED REWORK LOCATED ON HANDLE CUT OUT ACCES DOOR 824 AFT AVIONIC COMPARTMENT AND FOUND WITHIN ALLOWABLE DAMAGE LIMITS IAW A320 SRM 52-41-00-283-001 FIG 001 SHEET 1-
- [SDR YENA2024011600052](https://openairdocs.org/sdr/YENA2024011600052.md): Window Post · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA INTERNAL AREA, FROM UPPER TENSION BOLT LH SIDE, CRACK DIRECTION IS 2 OCLOCK, CRACK LENGTH IS 0.110 INCH, IN COCKPIT (1 EA) / REF AEROMAN WO 2023 361/1 NR 2
- [SDR YENA2024011600051](https://openairdocs.org/sdr/YENA2024011600051.md): Window Frame · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT AREA INTERNAL AREA, FROM UPPER TENSION BOLT RH SIDE, CRACK DIRECTION IS 10 OCLOCK, CRACK LENGTH IS 0.135 INCH, IN COCKPIT (1 EA) / REF AEROMAN WO 2023 361/1 NR
- [SDR YENA2024011600050](https://openairdocs.org/sdr/YENA2024011600050.md): Window Frame · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA INTERNAL AREA, LOWER INBOARD RADIUS RH SIDE, CRACK LENGTH ARE 0.120 INCH AND 0.105 INCH, IN COCKPIT (2 EA) / REF AEROMAN WO 2023 361/1 NR 2023-708960, PERFO
- [SDR YENA2024011600049](https://openairdocs.org/sdr/YENA2024011600049.md): Stringer · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 42L BTW FR 56 TO FR 59 IN AFT CARGO COMPARTMENT / REF AEROMAN N/R 2023-708948,PERFORMED REPAIR STRINGER 42L LOC. BTW FR 57 TO FR 59 IN AFT CARGO COMPARTMENT IAW A320 SRM 53-00-13-300-001 AND DWG E53470342, E534703
- [SDR YENA2024011600048](https://openairdocs.org/sdr/YENA2024011600048.md): Window Frame · unknown · Jan 14, 2024 · N564JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ WINDSHIELD FRAME CENTER POST LOWER ATTACHMENT/ CRACKS- PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023083001007](https://openairdocs.org/sdr/YENA2023083001007.md): Unknown · unknown · Aug 30, 2023 · N564JB · Airbus A320232 · Air Conditioning System
  > FLT #943, RNO-LAX." "DIRTY SOCK" ODOR WAS NOTICED ON DESCENT INTO LAX AT 2500FT IN COCKPIT, WAS EXTREMELY STRONG, IN CABIN NOTICED BY FA'S AND CUSTOMERS; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2. DECONTAMINATION LEVEL C WAS ACCOMPLISHED PER TSM
- [SDR YENA2023071100776](https://openairdocs.org/sdr/YENA2023071100776.md): Unknown · failed · Jul 7, 2023 · N564JB · Airbus A320232 · Ice/Rain Protection System
  > FLT#1695, MCO-SJO. (AIRCRAFT PERFORMED AN AIR TURN BACK TO MCO) 'ANTI ICE STBY PROBES; REMOVED & REPLACED PHC 3 IAW AMM 30-31-34. SYS OPS CHECK NORMAL.'
- [SDR YENA2023005020500](https://openairdocs.org/sdr/YENA2023005020500.md): Unknown · unknown · May 8, 2023 · N564JB · Airbus A320232 · Air Conditioning System
  > FLT#882, UVF-JFK. 'TEMPORARY DIRTY SOCK ODOR NOTICED DURING DESCENT THROUGH APPROX 5000 MIL. INTENSITY FLIGHT DECK ONLY. TURNING OFF PACK 1 HELPED DISSIPATE ODOR. (SUPPLEMENTAL TO FOLLOW)
- [SDR YENA2021112200774](https://openairdocs.org/sdr/YENA2021112200774.md): Filter · odor · Nov 21, 2021 · N564JB · Airbus A320232 · Air Distribution System
  > FLT 1201, JFK-FLL. DIRTY SOCK FUMES ODOR PREVALENT IN DESCENT FROM 9000 FT TO LANDING. APU WAS OFF ( APU SYSTEM); R&R BOTH RECIRC FILTERS IAW AMM 21-21-00. ODOR LEVEL DEEMED LEVEL 2 PER TSM 05-50-00-810-831-A. FAULT ISOLATED TO APU BLEED AIR. PERFORMED ECS D
- [SDR YENA2021110300739](https://openairdocs.org/sdr/YENA2021110300739.md): Unknown · odor · Nov 1, 2021 · N564JB · Airbus A320232 · Air Distribution System
  > FLT 768, PSE-MCO. DIRTY SOCK SMELL ON APPROACH BELOW 3000 IN COCKPIT NOT REPORTED IN CABIN; ACCOMPLISHED ENG RUNS FOR 20 MIN. ISOLATING BLEED SYS ALSO A 10 MIN DUEL ENGINE TAXI USING BLEEDS VISUAL INSPECTION OF AVIONICS COMPARTMENTS NO DEFECTS NOTED COMPLIED
- [SDR YENA2021081100508](https://openairdocs.org/sdr/YENA2021081100508.md): Unknown · odor · Aug 6, 2021 · N564JB · Airbus A320232 · Air Distribution System
  > FLT 1009, JFK-SDQ. LEVEL 1 FUME EVENT IN FLIGHT; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION (A). ISOLATED FAULT TO TYPE 10 A, 1C PER TSM 05-50-00-810-085-B. AC OK TO CONTINUE.
- [SDR YENA2021073000490](https://openairdocs.org/sdr/YENA2021073000490.md): Unknown · odor · Jul 26, 2021 · N564JB · Airbus A320232 · Air Distribution System
  > FLT 2156, DEN-LGA. ON DESCENT INTO LGA AT ABOUT 7000 FT IN CLEAR BUT HAZY AIR IN FLIGHT REPORTED DIRTY SOCK SMELL FOR REST OF FLIGHT ( PACKS); ACCOMPLISHED ENG RUN IAW AMM 71-00-00 AND PERFORMED OPS TEST ON BOTH PACKS 1 AND 2 PER AMM 21-52-00. NO CABIN ODOR N
- [SDR YENA2021072200471](https://openairdocs.org/sdr/YENA2021072200471.md): Unknown · odor · Jul 8, 2021 · N564JB · Airbus A320232 · Air Distribution System
  > FLT 204, BDA-BOS. STRONG ODOR IN AIRCRAFT DURING DESCENT. FAINT IN COCKPIT, INFLIGHT SAYS VERY STRONG IN REAR OF AIRCRAFT. ( APU SYSTEM); (REF W/O 1125473) APU R & R ON TASK CARD A320-49-11-11-400-004. MDDR CLEARED. PLACARD REMOVED. MX-4 UPDATED
- [SDR YENA2021060300348](https://openairdocs.org/sdr/YENA2021060300348.md): A/C Pack · odor · May 30, 2021 · N564JB · Airbus A320232 · Cabin Cooling System
  > FLT 329, JFK-RSW. ( PACKS) N564JB OPERATING FLIGHT 329 JFK - RSW REPORTED THE FOLLOWING CABIN ODOR EVENT UPON ARRIVAL INTO RSW, "" F/A'S REPORTED DIRTY SOCK SMELL ROW 14 AND FWD BELOW 10,000 IN DESCENT"". NO 30 DAY HISTORY; C/W INFO NOICE 2017-T015F. FOUND
- [SDR YENA2021043000298](https://openairdocs.org/sdr/YENA2021043000298.md): Control Valve · loose · Apr 29, 2021 · N564JB · Airbus A320232 · APU Bleed Air System
  > FLT # 192, TPA-BOS. LEVEL 2 ODOR EVENT DETECTED BY PREVIOUS FLIGHT CREW AND CURRENTLY DETECTED IN CABIN AND COCKPIT ( APU BLEED VALVE); PER INFO NOTICE 2017-T015F, APPLIED MEL 36-12-02-A CAT C PER MCC. APU BLEED/LOAD CONTROL VALVE SECURED IN THE CLOSED POSI
- [SDR YENA2021011400058](https://openairdocs.org/sdr/YENA2021011400058.md): Battery · failed · Jan 10, 2021 · N564JB · Airbus A320232 · Emergency Lighting
  > FLT 1922, PBI-BOS. FOUND EMERGENCY LIGHT BATTERY (LOCATION/FIN 12WL) FAILED DURING CAPACITY TEST, REF TASK CARD A320-33-51-00-710-003. R & R EMERGENCY POWER SUPPLY UNIT, IAW AMM 33-51-38. OPERATIONS CHECK GOOD.
- [SDR YENA2020081600423](https://openairdocs.org/sdr/YENA2020081600423.md): Smoke Detector · false indication · Aug 12, 2020 · N564JB · Airbus A320232 · Smoke Detection
  > FLT 1334, SJU-MCO. EMRGENCY DECLARED. AFT CARGO SMOKE WARNING ILLUMINATED IN FLIGHT FOR APPRX 5 SECONDS AND SELF EXTINGUISHED.DISCHARGE 1 LIGHT ILLUMINATED ON CARGO SMOKE PANEL W/NO PILOT ACTION. STS DISPLAYS.WHEN ON GROUND BEFORE OPEN CRG DOORS. PAX DISEMBA
- [SDR YENA2019081520453](https://openairdocs.org/sdr/YENA2019081520453.md): Battery · failed · Aug 12, 2019 · N564JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU BATTERY ON THE FOLLOWING POSITIONS FAILED TEST 10WL, 11WL, 12WL. REMOVED AND REPLACED EPSU BATTERIES AT 10WL, 11WL AND 12WL IAW AMM 33-51-38. SYS OPS CHECKS NORMAL. R/R EPSU AT 11WL POSITION IAW AMM 33-51-38.
- [SDR YENA201908152452](https://openairdocs.org/sdr/YENA201908152452.md): Battery · failed · Aug 12, 2019 · N564JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU BATTERY ON THE FOLLOWING POSITIONS FAILED TEST 10WL, 11WL, 12WL. REMOVED AND REPLACED EPSU BATTERIES AT 10WL, 11WL AND 12WL IAW AMM 33-51-38. SYS OPS CHECKS NORMAL. R/R EPSU AT 11WL POSITION IAW AMM 33-51-38.
- [SDR YENA2019081520451](https://openairdocs.org/sdr/YENA2019081520451.md): Battery · failed · Aug 12, 2019 · N564JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EPSU BATTERY ON THE FOLLOWING POSITIONS FAILED TEST 10WL, 11WL, 12WL. REMOVED AND REPLACED EPSU BATTERIES AT 10WL, 11WL AND 12WL IAW AMM 33-51-38. SYS OPS CHECKS NORMAL. R/R EPSU AT 11WL POSITION IAW AMM 33-51-38.
- [SDR YENA201901180031](https://openairdocs.org/sdr/YENA201901180031.md): Battery · failed · Jan 18, 2019 · N564JB · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EPSU 12WL BATTERY FAILED EMER. LIGHTS SYS. TEST; REPLACED BATTERY AT EPSU 12WL. EMER. LIGHTS SYS TEST GOOD.
- [SDR YENA201711110924](https://openairdocs.org/sdr/YENA201711110924.md): Epsu · failed · Nov 11, 2017 · N564JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, EMERGENCY LIGHTS INOPERATIVE IN LAVATORY D. TROUBLESHOT, FOUND 13WL EPSU BAD. REPLACED 13WL IAW AMM 33-51-38. OPS CHECK GOOD.
- [SDR YENA201711110923](https://openairdocs.org/sdr/YENA201711110923.md): Epsu · failed · Nov 11, 2017 · N564JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, FORWARD CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING AN OPERATIONAL TEST, WHEN CIRCUIT BREAKERS 1WL (H5) AND 2WL (H6) ARE OPENED. REPLACED THE EPSU 10WL IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR YENA201711110922](https://openairdocs.org/sdr/YENA201711110922.md): Battery Pack · no test · Nov 11, 2017 · N564JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, FORWARD CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING EMERGENCY LIGHT OPERATIONAL TEST WHEN CIRCUIT BREAKERS 1WL (H5) AND 2WL (H6) ARE OPENED; REPLACED EPSU 10WL IAW A320 AMM 33-51-38. OPS CHECKED GOOD.
- [SDR YENA201711110921](https://openairdocs.org/sdr/YENA201711110921.md): Shear Plate · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE LEFT CABIN SHEAR PLATE BETWEEN FRAMES 69 AND 70, STRINGER 23L. REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 53-00-14-232-002, AND 53-41-14, FIGURE 2.
- [SDR YENA201711110920](https://openairdocs.org/sdr/YENA201711110920.md): Shear Plate · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN RIGHT SHEAR PLATE BETWEEN FRAMES 69 - 70, STRINGER 23R. REMOVED AND REPLACED THE SHEAR PLATE IAW SRM 51-72-11, AND 53-41-14, FIG 002.
- [SDR YENA201711110919](https://openairdocs.org/sdr/YENA201711110919.md): Stringer · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE AFT CARGO STRINGER 43L, 8 INCHES AFT OF FRAME 56. REPAIRED THE STRINGER IAW SRM 53-00-13-300-001, 51-73-11, 51-74-00, 51-21-11, 51,42-11, 53-00-17, 53-00-13-300-010, AND GMM5-169.
- [SDR YENA201711110918](https://openairdocs.org/sdr/YENA201711110918.md): Stringer · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CARGO BAY STRINGER 39L, FRAME 56. REPAIRED THE STRINGER IAW SRM 53-0013-300-001, 51-73-11, 51-74-00, 51-21-11, 51-42-11, 53-00-13-300-010, AND GMM -5-169.
- [SDR YENA201711110917](https://openairdocs.org/sdr/YENA201711110917.md): Floor Support · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON CABIN FLOOR SUPPORT Y765 AFT OF FRAME 66. REMOVED THE CORROSION AND VERIFIED CORROSION WAS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-14-283-002. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-41-14, FIG
- [SDR YENA201711110916](https://openairdocs.org/sdr/YENA201711110916.md): Door Sill · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE L2 DOOR SILL, FRAME FRAME 66. REMOVED THE CORROSION AND VERIFIED BEYOND 25% ALLOWABLE LIMITS IAW SRM 53-41-14-283-002. REMOVED AND REPLACED THE DOOR SILL IAW SRM 53-41-14, FIG 021.
- [SDR YENA201711110915](https://openairdocs.org/sdr/YENA201711110915.md): Door Sill · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE R2 DOOR SILL AT FRAME 66. REMOVED THE CORROSION VERIFIED BEYOND 25% ALLOWABLE LIMITS IAW SRM 51-41-14-283-002. REMOVED AND REPLACED THE DOOR SILL IAW SRM 53-41-14, FIG 021.
- [SDR YENA201711110914](https://openairdocs.org/sdr/YENA201711110914.md): Floor Support · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT BETWEEN FRAMES 14 TO 15, Y765. R & R THE FLOOR SUPPORT IAW SRM 53-11-14-283-001.
- [SDR YENA201711110913](https://openairdocs.org/sdr/YENA201711110913.md): Floor Support · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FWD CABIN FLOOR SUPPORT Y-254, FRAMES 18 - 20. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 53-11-15-283-002.
- [SDR YENA201711110912](https://openairdocs.org/sdr/YENA201711110912.md): Shear Web · corroded · Nov 11, 2017 · N564JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN RT SHEAR WEB BETWEEN FRAMES 69 - 70. R & R THE SHEAR WEB IAW SRM 53-41-14, FIG 002.

Next page: https://openairdocs.org/aircraft/N564JB/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 = 'N564JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N564JB/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.