# Service difficulty reports: N580JB

A list on [N580JB](https://openairdocs.org/aircraft/N580JB.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 · 91 reports

- [SDR YENA2025120101133](https://openairdocs.org/sdr/YENA2025120101133.md): Computer · malfunctioned · Nov 29, 2025 · N580JB · Airbus A320232 · Flight Control System
  > FLT#1970, BOS-PHX. WHILE DESCENDING AND SLOWING TO 210 KTS AT 9000 FEET, SELECTED FLAPS 1 AND RECEIVED ELAC 1 FAULT. PLANE ROLLED APPROX 15 DEGREES RIGHT. DISCONNECTED A/P AND HAND FLEW PLANE TO NORMAL LANDING; REF LG # 4520823 ITEM #2, # 4520824 ITEM #1 FO
- [SDR YEN2025F00010](https://openairdocs.org/sdr/YEN2025F00010.md): Pump · failed · Nov 29, 2025 · N580JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > FLT#1970, BOS-PHX. "WHILE DESCENDING AND SLOWING TO 210 KTS AT 9000 FEET, SELECTED FLAPS 1 AND RECEIVED ELAC 1 FAULT. PLANE ROLLED APPROX 15 DEGREES RIGHT. I DISCONNECTED A/P AND HAND FLEW PLANE TO NORMAL LANDING; REF LG # 4520823 ITEM #2, # 4520824 ITEM #1 FO
- [SDR YENA2025021700155](https://openairdocs.org/sdr/YENA2025021700155.md): Battery · failed · Feb 13, 2025 · N580JB · Airbus A320232 · Emergency Lighting
  > FLT#2126, MBJ-FLL. 'EMERGENCY LIGHT INOP; REMOVED AND REPLACED ALL 4 EPSU BATTERIES REF AMM 33-51-38-000-001-A SEE SUBSEQUENT ITEMS FOR PART TRANSACTIONS THIS ITEM CLEARED FWD EPSU BATTERY.'
- [SDR YENA2024081301137](https://openairdocs.org/sdr/YENA2024081301137.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 31 BTW STR 40L AND STR 41L IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00019) REF AEROMAN WO 2024 51/1 NR 2024-370753. REMOVED AND REPLACED CLEAT (SHEAR TIE) LOCAT
- [SDR YENA2024081301136](https://openairdocs.org/sdr/YENA2024081301136.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 31 AND BTW STR 40R AND STR 41R IN FW D CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00020) REF AEROMAN WO 2024- 51/1 NR 2024-370766. REMOVED AND REPLACED CLEAT (SHEAR TIE)
- [SDR YENA2024081301135](https://openairdocs.org/sdr/YENA2024081301135.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR 41R AND STR 42R IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00021) REF AEROMAN WO 2024-51/1 NR 2024-370812. REMOVED AND REPLACED CLEAT (SHEAR TIE) LOCAT
- [SDR YENA2024081301134](https://openairdocs.org/sdr/YENA2024081301134.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR 42R AND STR 43R IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00022) REF AEROMAN WO 2024 51/1 NR 2024-370813. REMOVED AND REPLACED CLEAT (SHEAR TIE) LOCAT
- [SDR YENA2024081301133](https://openairdocs.org/sdr/YENA2024081301133.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR 42L AND STR 43L IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00023) REF AEROMAN WO 2024 51/1 NR 2024 370814 REMOVED AND REPLACED CLEAT (SHEAR TIE) LOCATE
- [SDR YENA2024081301132](https://openairdocs.org/sdr/YENA2024081301132.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 34 BTW STR 41L AND STR 42L IN FWD CA RGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00024) REF AEROMAN WO 2024- 51/1 NR 2024- 370815. REMOVED AND REPLACED SHEAR TIE LOCATED AT
- [SDR YENA2024081301131](https://openairdocs.org/sdr/YENA2024081301131.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 33 AND BTW STR 40R AND STR 41R IN FW D CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00025) REF AEROMAN WO 2024 51/1 NR 2024-370827. REMOVED AND REPLACED SHEAR TIE LOCATED A
- [SDR YENA2024081301130](https://openairdocs.org/sdr/YENA2024081301130.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 32 AND BTW STR 41R AND STR 42R IN FW D CARGO COMPARTMENT; (RESOLVED ON W/O: 1301446 TASKCARD: NR-00028) REF AEROMAN WO 2024 51/1 NR 2024 370834. REMOVED AND REPLACED SHEAR TIE LOCATED AT LEVEL OF FR 3
- [SDR YENA2024081301129](https://openairdocs.org/sdr/YENA2024081301129.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 30 AND BTW STR 41R AND STR 42R IN F WD CARGO COMPARTMENT; (RESOLVED ON W/O: 1301446 TASKCARD: NR-00029) REF AEROMAN WO 2024 51/1 NR 2024 370848. REMOVED AND REPLACED SHEAR TIE LOCATED AT LEVEL OF FR 3
- [SDR YENA2024081301128](https://openairdocs.org/sdr/YENA2024081301128.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION SHEAR TIE LOCATED AT FR 30 AND BTW STR 41R AND STR 42R IN F WD CARGO COMPARTMENT; (RESOLVED ON W/O: 1301446 TASKCARD: NR-00029) REF AEROMAN WO 2024 51/1 NR 2024 370848. REMOVED AND REPLACED SHEAR TIE LOCATED AT LEVEL OF FR 3
- [SDR YENA2024081301127](https://openairdocs.org/sdr/YENA2024081301127.md): Shear Tie · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK SHEAR TIE IN AFT CARGO COMPARTMENT (CRACK SHEAR TIE LOC ON FRAME 61 BTW STR 41 TO 42L ON AFT CARGO COMPARTMENT); REF AEROMAN WO # 2024-51/1 NR # 2024-371091REMOVED AND REPLACED SHEAR TIE (CLIP) LOC. ON FR 61 BTW STR 41L TO STR
- [SDR YENA2024081301126](https://openairdocs.org/sdr/YENA2024081301126.md): Stringer · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: CORROSION STRINGER 42L AND FR61 IN AFT CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00044) REF AEROMAN WO # 2024-51/1 NR- 2024-370795 PERFORMED PERMANENT REPAIR LOC. FR 60 STRINGER 42L IN AFT CARGO COMPARTM
- [SDR YENA2024081301125](https://openairdocs.org/sdr/YENA2024081301125.md): Frame · cracked · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE 8, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.098 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/
- [SDR YENA2024081301124](https://openairdocs.org/sdr/YENA2024081301124.md): Frame · cracked · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE A, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.096 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/
- [SDR YENA2024081301123](https://openairdocs.org/sdr/YENA2024081301123.md): Frame · cracked · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE B, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.094 INCHES. CRACK DIR ECTION: 9 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/
- [SDR YENA2024081301122](https://openairdocs.org/sdr/YENA2024081301122.md): Frame · cracked · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE C, LOCATED AT FR 16 LH ON DOUB LE JOGGLE AREA, PASSENGER CABIN. CRACK DEPTH = 0.075 INCHES. CRACK DIR ECTION: 1 OCLOCK. CONFIRM INDICATION USING BOROSCOPE VIEW IAW NTM 51-9 0-00; (RESOLVED ON W/
- [SDR YENA2024081301121](https://openairdocs.org/sdr/YENA2024081301121.md): Fitting · corroded · Aug 12, 2024 · N580JB · Airbus A320232 · Nacelle/Pylon, Main Frame
  > DURING HEAVY MAINTENANCE: CORROSION SPIGOT FITTING ON RH PYLON (1 EA); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00051) REF AEROMAN WO # 2024-51/1 NR # 2024-371044 REPLACED LOWER SPIGOT FITTING IAW A320 SRM 54-51-12-300-002 STEP 2.A(3) TO (9).
- [SDR YENA2024081301120](https://openairdocs.org/sdr/YENA2024081301120.md): Stringer · damaged · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE: ELONGATED HOLE (2EA) ON STRINGER 2RH BETWEEN FR80 TO FR81 UPPER FUSELAGE; (RESOLVED ON W/O: 1301446 TASKCARD: NR-00057) REF AE W/O# 2024-51/1. N/R# 2024 - 371123. ACCOMPLISHED REPAIR OF ELONGATED HOLES ON EXISTING REPAIR LOCATION ON R
- [SDR YENA2024081301119](https://openairdocs.org/sdr/YENA2024081301119.md): Skin · damaged · Aug 12, 2024 · N580JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / SKIN PANEL BETWEEN FR80-81 & STGR 1R-3R / ELONGATED HOLES & EXISTING REPAIR - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9033-24 COVER & P1-P2 /2/ AIRBUS RDAF 81440328/004/2024 ISSUE B /3/ AIRBUS TD/814
- [SDR YENA2024051600750](https://openairdocs.org/sdr/YENA2024051600750.md): Warning Light · false activation · May 15, 2024 · N580JB · Airbus A320232 · Fire Bottle, Fixed
  > FLT#1795, JFK-AUS. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'AFTER T/O RECEIVED ENG 1 AGENT 1 DISCH LIGHT. ILLUMINATED AND REMAINED ON NO OVERWEIGHT LANDING ON RETURN TO JFK; REF TSM 26-21-00-810-815-A. FOUND FAULTY ENG 1/ AGENT 1 P/BSW. R/R ENG 1/ AGENT 1
- [SDR YENA2022120201196](https://openairdocs.org/sdr/YENA2022120201196.md): Unknown · odor · Dec 1, 2022 · N580JB · Airbus A320232 · Air Distribution System
  > FLT#688, BNA-LGA. 'ODOR EVENT COMING THROUGH 10000FT; PERFORMED DECONTAMINATION OF AIRCRAFT IAW AMM 36-12-00. NO ODOR IS PRESENT. COMPLETED WITH INFORMATION NOTICE 2017-TO15, SECTION B2. DECONTAMINATION LEVEL 2 WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. AIRC
- [SDR YENA2022030100103](https://openairdocs.org/sdr/YENA2022030100103.md): Fan · failed · Feb 26, 2022 · N580JB · Airbus A320232 · Air Conditioning System
  > FLT # 669, JFK-SJC. VENT BLOWER FAULT ECAM IN CRUIZE SLIGHT VIBRATION AND ELECTRICAL SMELL COMING FROM VENT IN COCKPIT PRIOR TO ECAM. ( EXTRACT FAN - NO AVNCS SYS FAULT ECAM CAUTION); REMOVED AND REPLACED AVX VENT EXTRACT FAN REF AMM 21-26-51. OPS CK GOOD. M
- [SDR YENA2021091700611](https://openairdocs.org/sdr/YENA2021091700611.md): Skin · corroded · Sep 12, 2021 · N580JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, CORROSION AROUND FASTENER ROW TOP RIGHT WING SURFACE STR 11 BETWEEN RIB 2/3 DOT 88-017; REMOVED CORROSION FROM AREA IAW A320 SRM 51-74-00 PERFORMED NDT INSPECTION ON AREA WITH ORIGINAL MATERIAL.210 MATERIAL LOSS OF.040 AND FOUND OUT OF LIMITS IA
- [SDR YENA2021091700610](https://openairdocs.org/sdr/YENA2021091700610.md): Skin · corroded · Sep 12, 2021 · N580JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, CORROSION AROUND FASTENER ROW TOP RIGHT WING SURFACE STR 11 BETWEEN RIB 3/4; REMOVED CORROSION IAW A320 SRM 51-74-00 PERFORMED NDT INSPECTION ON AREA WITH ORIGINAL THICKNESS.210 MATERIAL REMAIN.173 WITH A LOSS OF.037 AND FOUND OUT OF LIMITS IAW
- [SDR YENA2021091700609](https://openairdocs.org/sdr/YENA2021091700609.md): Skin · corroded · Sep 12, 2021 · N580JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, CORROSION AROUND FASTENER TOP RIGHT-WING SURFACE STR 11 HEAR SLAT #3 DOT 88-023; REMOVED CORROSION FROM AREA IAW A320 SRM 57-21-11 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL THICKNESS.166 MATERIAL REMAIN.155 WITH A LOSS OF.011AND FOUND OUT OF LI
- [SDR YENA2021091700608](https://openairdocs.org/sdr/YENA2021091700608.md): Skin · corroded · Sep 12, 2021 · N580JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, L/H WING UPPER SURFACE HAS AREAS OF CORROSION AT STA 1957 RIB 4 AND UPPER SKIN BUTT SPLICE11 DOT 008; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL.213 MATERIAL REMAIN.185 WITH A LOSS OF.028
- [SDR YENA2021091700607](https://openairdocs.org/sdr/YENA2021091700607.md): Skin · corroded · Sep 12, 2021 · N580JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, LH WING UPPER SURFACE HAS AREA OF CORROSION AT RIB 1 3"FWD OF UPPER SKIN BUTT SPLICE 11.7 INCHES O/B OF FUSELAGE; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL.210 MATERIAL REMAIN.168 WITH LOS
- [SDR YENA2021091700606](https://openairdocs.org/sdr/YENA2021091700606.md): Skin · corroded · Sep 12, 2021 · N580JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION AT WING WALK AREA STA 700/RIB2 32" AFT OF FRONT SPAR; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL.200 MATERIAL REMAIN.155 WITH LOSS OF.045 AND F
- [SDR YENA2021091700605](https://openairdocs.org/sdr/YENA2021091700605.md): Skin · corroded · Sep 12, 2021 · N580JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION ABOVE FRONT SPAR AT STA 1957/RIB4; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL.260 MATERIAL REMAIN.152 WITH LOSS OF.108AND FOUND TO BE OUT OF LI
- [SDR YENA2021091700604](https://openairdocs.org/sdr/YENA2021091700604.md): Skin · corroded · Sep 12, 2021 · N580JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION AT RIB 8 ABOVE REAR SPAR; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL.311 MATERIAL REMAIN.240 WITH A LOSS OF.071 AND TO BE OUT OF LIMITS IAW A32
- [SDR YENA2021081700522](https://openairdocs.org/sdr/YENA2021081700522.md): Unknown · odor · Aug 13, 2021 · N580JB · Airbus A320232 · Air Distribution System
  > FLT 2085, BDL-MIA. CABIN ODOR REPORTED BY INBOUND FLIGHT ATTENDANTS DIRTY SOCK SMELL; INFLIGHT CREW DEBRIEFED DURING GATE OPERATION AND DEPLANING WITH DOOR OPEN. ODOR EVENT OCCURED AFT AND MID CABIN. COMPLIED WITH INFORMATION NOTICE 2017-T015G SECTION A ( A)
- [SDR YENA2021040600207](https://openairdocs.org/sdr/YENA2021040600207.md): Unknown · odor · Mar 31, 2021 · N580JB · Airbus A320232 · Air Distribution System
  > FLT 1533, JFK-CTG. ODOR EVENT ON TAKEOFF/CLIMBOUT. SPECIFICALLY NOTICEABLE IN THE COCKPIT. MX-270 FORM COMPLETED; COMPLIED INFO NOTICE 2017-1015F SECTION A. A/C OK FOR SERVICE
- [SDR YENA201907200414](https://openairdocs.org/sdr/YENA201907200414.md): Epsu · failed · Jul 20, 2019 · N580JB · Airbus A320232 · Emergency Lighting
  > FLT 430, SMF-BOS. AFT EXIT LIGHT INOP; R & R AFT EPSU IAW AMM 33-51-00 OPS CHECK AND TEST GOOD. A/C OK FOR CONT. SERVICED.
- [SDR YENA2019060325294](https://openairdocs.org/sdr/YENA2019060325294.md): Line · ruptured · May 25, 2019 · N580JB · Airbus A320232 · Hydraulic System, Main
  > FT # 80, AIRCRAFT WAS FOUND WITH A HYDRAULIC LEAK ON THE #1 ENGINE AFT PYLON AREA. AFTER GAINING ACCESS TO THE SUBJECT AREA, IT WAS FOUND THAT A HYDRAULIC LINE HAS RUPTURED AND CAUSED DAMAGE TO THE PYLON BOX STRUCTURE P/N D54541005000000. AFTER CLEANUP AND
- [SDR YENA201812310892](https://openairdocs.org/sdr/YENA201812310892.md): Battery · discharged · Dec 31, 2018 · N580JB · Airbus A320232 · Emergency Lighting
  > FLT 2991, BOS-TPA. EPSU 10WL BATTERY FAILS EMERGENCY LIGHT SYSTEM TEST; R & R EPSU 10WL BATTERY IAW AMM 33-51-38, EMERGENCY LIGHT SYSTEM CHECKS OK.
- [SDR YENA2018120490803](https://openairdocs.org/sdr/YENA2018120490803.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM -Y450.8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AND DRAWING # D53472816
- [SDR YENA2018120490802](https://openairdocs.org/sdr/YENA2018120490802.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM -Y464.8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AND DRAWING # D53472816.
- [SDR YENA2018120490801](https://openairdocs.org/sdr/YENA2018120490801.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM - Y450 AT AFT GALLEY AREA ON FRAME 65 (1 E/A); REF BP NR # 2018-374657 REPLACED FLOOR BEAM - Y464.8 BTW FR 64 TO FR 67 AT AFT GALLEY AREA AS PER SRM A320 51-72-11 AN DRAWING # D53472816
- [SDR YENA2018120490800](https://openairdocs.org/sdr/YENA2018120490800.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1162.5 BTW FR 66 TO FR 68 AT AFT GALLEY AREA; REF BP NR # 2018-374614 REPLACED FLOOR BEAM + Y1162.5 BTW FR 66 TO FR 68 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780
- [SDR YENA2018120490799](https://openairdocs.org/sdr/YENA2018120490799.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA; REF BP NR # 2018-374616 REPLACED FLOOR BEAM +Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780
- [SDR YENA2018120490798](https://openairdocs.org/sdr/YENA2018120490798.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM - Y 1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA; REF BP NR # 2018-374620 REPLACED FLOOR BEAM - Y1162.5 BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM A320 51-72-11 AND DRAWING D53472780
- [SDR YENA2018120490797](https://openairdocs.org/sdr/YENA2018120490797.md): Web · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT WEB AT STR 23R AT AFT GALLEY AREA; REF BP NR # 2018-374680 REPLACED SUPPORT WEB AT STR 23R BTW FR 69 TO FR 70 AT AFT GALLEY AREA AS PER SRM A320-51-72-11 AND DRAWING # D53474180.
- [SDR YENA2018120490796](https://openairdocs.org/sdr/YENA2018120490796.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y1162.5 BETWEEN FR 66-FR 68 AT AFT GALLEY AREA; REPLACED FLOOR BEAM-Y1162.5 BETWEEN FR 66-FR 68 AY AFT GALLEY AREA IAW SRM A320-51-72-11 AND DRWG D53472780. REF AEROMAN NR 2018-374619.
- [SDR YENA2018120490795](https://openairdocs.org/sdr/YENA2018120490795.md): Stringer · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON STRINGER 43L LOCATED BTW FR 62 TO FR 63 IN AFT CARGO COMPARTMENT; REF BP NR # 2018-374610 REPLACED STRINGER 43L BTW FR 60 60 FR 64 IN AFT CARGO COMPARTMENT AS PER SRM A320 51-72-11 AND DRAWING # E 53470342.
- [SDR YENA2018120490794](https://openairdocs.org/sdr/YENA2018120490794.md): Dummy Rail · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RAIL DUMMY Y503.2 LOC BTW FR 12 TO FR 16 AT FWD GALLEY AREA; REF BP NR # 2018-374621 REPLACED RAIL DUMMY Y503.2 LOC BTW FR 12 TO FR 16 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DRAWING # 53112825
- [SDR YENA2018120490793](https://openairdocs.org/sdr/YENA2018120490793.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM +Y1292 LOC. BTW FR 12 TO FR 24 IN PASSENGER CABIN; REF BP NR # 2018-374613 REPLACED FLOOR BEAM LOC +Y1292 BTW FR 12 TO FR 24 IN PASSENGER CABIN AS PER SRM A32051-72-11 AND DRAWING # D53112812.
- [SDR YENA2018120490792](https://openairdocs.org/sdr/YENA2018120490792.md): Floor Support · corroded · Nov 29, 2018 · N580JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y 1292 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA; REPLACED FLOOR BEAM LOCATION -Y1292 BTW FR 12 TO 24 AT FWD GALLEY AREA AS PER SRM A320-51-72-11 AND DWG D53112812. ALL WORK ACCOMPLISHED ON AERO

Next page: https://openairdocs.org/aircraft/N580JB/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 = 'N580JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N580JB/reports

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