# Service difficulty reports: N509JB

A list on [N509JB](https://openairdocs.org/aircraft/N509JB.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 · 79 reports

- [SDR YENA2026022300233](https://openairdocs.org/sdr/YENA2026022300233.md): Seal · leaking · Feb 21, 2026 · N509JB · Airbus A320232 · Cargo/Baggage Doors
  > FLT # 1044 PBI-PBI. CABIN PRESS CAUTION/WARNING CABIN CLIMBED TO 9800FT @ FLT270.;PERFORMED TSM TASK 21-31-00-810-809. PERFORMED GVI OF A/C NO DEFECTS NOTED. CHECKED CONDITION OF A/C DOOR SEALS, NO DEFECTS NOTED. PRESSURIZED A/C AND FOUND AFT CARGO DOOR LEAKI
- [SDR YENA2025090400909](https://openairdocs.org/sdr/YENA2025090400909.md): Skin · corroded · Sep 3, 2025 · N509JB · Airbus A320232 · Trailing Edge Flaps
  > DURING HEAVY MAINTENANCE: CORROSION ON TOP SKIN, TRAILING EDGE OVERHANG, LOWER SURFACE, BTW WX4013 AND WX4349 ( BTW RIB 8 7 RIB 9), ON RH WING; REFERENCE AEROMAN W.O. 2025 279 / 1- N.R. 481112 * PERFORMED PERMANENT REPAIR ON TOP SKIN PANEL #2, TRAILING EDGE O
- [SDR YENA2025090400908](https://openairdocs.org/sdr/YENA2025090400908.md): Skin · corroded · Sep 3, 2025 · N509JB · Airbus A320232 · Trailing Edge Flaps
  > DURING HEAVY MAINTENANCE: CORROSION ON TOP SKIN, TRAILING EDGE OVERHANG, LOWER SURFACE, BTW WX40 13 & WX4349 ( BTW RIB 8 AND 9) ON LT WING; REFERENCE SAL WO 2025 279/1 NR 2025-481126. EVALUATED BLENDED AREA LOCATED ON TOP SKIN, T/E OVERHANG, LOWER SURFACE, BTW
- [SDR YENA2025033100343](https://openairdocs.org/sdr/YENA2025033100343.md): Slat · damaged · Mar 29, 2025 · N509JB · Airbus A320232 · Leading Edge Devices
  > FLT#891, BOS-TPA.' BIRD STRIKE R WING LEADING EDGE OUTBOARD OF ENGINE; REMOVED AND REPLACED RH SLAT #2 REFERENCE AMM 27-84-64. OPS CHECK GOOD AT THIS TIME REFERENCE AMM 27-84-00.
- [SDR YENA2024080601093](https://openairdocs.org/sdr/YENA2024080601093.md): Floorbeam · corroded · Aug 5, 2024 · N509JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: PASSENGER CABIN, UPPER SURFACE FLOOR BEAM STRUCTURE, FR 16, BTW 'Y' 254 AND 'Y' 765, WITH CORROSION; (RESOLVED ON W/O: 1282422 TASKCARD: NR-00018) CORROSION WAS LOCATED ONLY IN FR16 Y254, IT WAS REMOVED IN FLOOR BEAM STRUCTURE BTW FR1
- [SDR YENA2024080601092](https://openairdocs.org/sdr/YENA2024080601092.md): Floor Support · corroded · Aug 5, 2024 · N509JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: PASSENGER CABIN, UPPER SURFACE FLOOR BEAM STRUCTURE, BTW FR 18 TO FR 20, 'Y' -1292 WITH CORROSION; UPPER SURFACE FLOOR BEAM STRUCTURE, BETWEEN FR 18 TO FR 20, 'Y' -1292 WAS REPAIRED, THIS REPAIR IS CATEGORY "A" NO FUTURE ACTIONS REQUI
- [SDR YENA2024080601091](https://openairdocs.org/sdr/YENA2024080601091.md): Skin · corroded · Aug 5, 2024 · N509JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: RH WING UPPER SURFACE SKIN, WITH CORROSION NEXT TO PREVIOUS DOBLER REPAIR, BETWEEN RIBS 14, 15 AND REAR SPAR; CORROSION DAMAGE ON RH WING TOP SKIN PANEL 2, BETWEEN RIB 14/ RIB 15 AND REAR SPAR AT 0.750" FROM A REPAIR PLATE WAS EVALUAT
- [SDR YENA2024080601090](https://openairdocs.org/sdr/YENA2024080601090.md): Skin · punctured · Aug 5, 2024 · N509JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: UPPER FUSELAGE, ON FR80 BETWEEN STGR 2RH AND STGR 3RH WITH A PUNCTURE; UPPER FUSELAGE, ON FR80 BETWEEN STGR 2RH AND STGR 3RH PUNCTURE WAS REPAIRED, THIS REPAIR IS CAT A, NO REQUIRES FURTHER ACTION I.A.W SRM 53-51-- 11-300-002 REV 149
- [SDR YENA2024080601089](https://openairdocs.org/sdr/YENA2024080601089.md): Hinge Arm · damaged · Aug 5, 2024 · N509JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: REMOVAL OF VERTICAL STAB ARM OF HINGES FROM #1 THRU #7 TO PERFORM INSPECTION; REF AMERICANA WO# 131-2003 S/N 00579 FOR WORK PERFORMED. FITTING ASSEMBLY FORK END (BR2, BR 5 AND BR6) WERE REPLACED BY NEW FITTINGS IAW A320 SRM 55-36-42-3
- [SDR YENA2024080601088](https://openairdocs.org/sdr/YENA2024080601088.md): Light · no test · Aug 5, 2024 · N509JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: EMERGENCY LIGHTS OPERATIONAL TEST NOT SATISFACTORY IN L2 EMERGENCY ESCAPE SLIDE; ESCAPE SLIDE /RAFT AFT DOOR LH WAS REPLACED IAW AMM 25-62-44-00-012-A AND IAW AMM 25-62-44-400-007-A REV 101 DATE MAY 01/2024 WORK PERFORM BY MEXICANA WO
- [SDR YENA2024080601087](https://openairdocs.org/sdr/YENA2024080601087.md): Light · no test · Aug 5, 2024 · N509JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: EMERGENCY LIGHT OPERATIONAL TEST NOT SATISFACTORY IN L1 EMERGENCY ESCAPE SLIDE; ESCAPE SLID/RAFT FWD DOOR LH WAS REPLACED IAW AMM 25-62-44-000-012-A AND IAW AMM 25-62-44-400-007-A REV 101 DATE: MAY 01/2024 WORK PERFORMED BY MEXICANA
- [SDR YENA2024080601086](https://openairdocs.org/sdr/YENA2024080601086.md): Light · no test · Aug 5, 2024 · N509JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: EMERGENCY LIGHT OPERATIONAL TEST NOT SATISFACTORY IN R2 EMERGENCY ESCAPE SLIDE RAFT P/N D30665-709 S/N M19328; ESCAPE SLIDE/RAFT AFT DOOR RH WAS REPLACED IAW AMM 25-62-44-000-804-A REV 101 DATE 01 MAY 2024.
- [SDR YENA2024080601085](https://openairdocs.org/sdr/YENA2024080601085.md): Floor Support · corroded · Aug 5, 2024 · N509JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: PASSENGER CABIN, UPPER SURFACE FLOOR BEAM STRUCTURE, BTW FR 16 AND FR 18, 'Y' - 254, WITH CORROSION; PASSENGER CABIN, UPPER SURFACE FLOOR BEAM STRUCTURE, BTW FR 16 AND FR 18, 'Y' - 254. DAMAGE WAS REPAIRED I.A.W. SRM 53-11-14-300-004,
- [SDR YENA2024080601084](https://openairdocs.org/sdr/YENA2024080601084.md): Floor Support · corroded · Aug 5, 2024 · N509JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON FLOOR STRUCTURE BTW 1732 AND FR-20; "FUSELAGE FLOOR STRUCTURE, WEB AT Y 1732 BETWEEN FR 20/FR 24 WAS REPLACED I.A.W. A320 S.R.M. 51-72-11-911-001 MAY 01/24 REV.149 AND SRM 51-42-11 MAY 01/- 24 REV.149. ALL WORK ACCOMPLISH
- [SDR YENA2024080601083](https://openairdocs.org/sdr/YENA2024080601083.md): Floorbeam · corroded · Aug 5, 2024 · N509JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: "PASSENGER CABIN, UPPER SURFACE FLOOR BEAM STRUCTURE, FR 16, BTW 'Y' - 254 AND 'Y' 254, WITH CORROSIONS (3); RAIL DUMMY PN: D5311283020200 WAS REPLACED IN FR12 TO FR16 Y81 I.A.W A320 SRM 51-72-11-911-001 / 51-72-11-911-00 REV.: 149 DA
- [SDR YENA2024080601082](https://openairdocs.org/sdr/YENA2024080601082.md): Floorbeam · corroded · Aug 5, 2024 · N509JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE: "PASSENGER CABIN, UPPER SURFACE FLOOR BEAM STRUCTURE, FR 16, BTW 'Y' - 254 AND 'Y' 254, WITH CORROSIONS (3); "RAIL DUMMY PN: D5311283020200 WAS REPLACED IN FR12 TO FR16 Y81 I.A.W A320 SRM 51-72-11-911-001 / 51-72-11-911-00 REV.: 149 D
- [SDR YENA2023122001602](https://openairdocs.org/sdr/YENA2023122001602.md): None · none · Dec 10, 2023 · N509JB · Airbus A320232 · Standard Practices/Structures
  > DURING HEAVY MAINTEANACE: AIRCRAFT REQUIRES MOD AND WEEKLY WO# 1266397 AND 1293881. ENCOMPASSED WITHIN CAS WO# 509-1266397; RETURN TO SERVICE IN ACCORDANCE WITH FAR 43.9. AS AUTHORIZED BY THIS REPAIR STATION MANUAL. THE FOLLOWING PERSON CERTIFIES THAT THE W
- [SDR YENA2023083001004](https://openairdocs.org/sdr/YENA2023083001004.md): Terminal · failed · Aug 28, 2023 · N509JB · Airbus A320232 · Electrical Power System Wiring
  > FLT#268, PUJ-JFK. 'ELECTRICAL BURNING SMELL EMENATING FROM OVERHEAD FWD GALLEY LIGHT FIXTURE (S) TURNED LIGHTS OFF SMELL DISAPATED ( THALES-AVANT IFE (ENTIRE SYSTEM)); REMOVED AND REPLACED ICMT IAW AMM 44-21-11 AND PSB IAW AMM 44-22-44 DUE TO BURNING SMELL FR
- [SDR YENA2023005010462](https://openairdocs.org/sdr/YENA2023005010462.md): Unknown · unknown · Apr 29, 2023 · N509JB · Airbus A320232 · Air Conditioning System
  > FLT#6, PTP-JFK. 'SIGNIFICANT ODOR IN CABIN DURING FINAL APPROACH REPORTED BY INFLIGHT; ACCOMPLISH WITH INFORMATION NOTICE 2017-T015, SECTION A, 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 YENA2023041100339](https://openairdocs.org/sdr/YENA2023041100339.md): Ptu · failed · Apr 9, 2023 · N509JB · Airbus A320232 · Hydraulic Power System
  > FLT#1270, CHS-LGA. (AIRCRAFT DIVERTED TO JFK) 'Y HYD RSVR LO LVL; FOUND PTU MANIFOLD TO BE AT CAUSE FOR THE LEAK. REMOVED AND REPLACED PTU MANIFOLD IAW AMM 29-13-51. OPS CHECK & LEAK CHECK ARE GOOD. A/C OK TO CONTINUE FOR SERVICE.'
- [SDR YENA2022050200431](https://openairdocs.org/sdr/YENA2022050200431.md): None · none · Apr 29, 2022 · N509JB · Airbus A320232 · Air Conditioning System
  > FLT#1677, JFK-JAX. 'PACK 1 PLACED ON MEL DUE TO ODOR EVENT ( PACKS); REF WO #1176652 PERFORMED PACK 1 AND 2 BURNED REF AMM 21-00-00-615-802A. NO ODOR WAS NOTICED. MDDR CLEARED. MX-4 UPDATED.'
- [SDR YENA2022022400086](https://openairdocs.org/sdr/YENA2022022400086.md): None · failed · Feb 18, 2022 · N509JB · Airbus A320232 · Rudder Control System
  > FLT # 2092, MIA-JFK. A/C FLYING UNCOORDINATED IN CRUISE ON APPROACH RUDDER TRIM WAS TRIMMING IN THE OPPOSITE DIRECTION AND CREATED A SIGNIFICANT MISS TRIM AT A/P DISCONNECT; REF LOG PG 3322673 ITEM #2 R/R #5 LEFT WING SPOILER ACTUATOR AND PERFORMED RUDDER RIGG
- [SDR YENA2021041600247](https://openairdocs.org/sdr/YENA2021041600247.md): Skin · corroded · Apr 11, 2021 · N509JB · Airbus A320232 · Wing, Center Box
  > DURING HMV, EA A21-330-01 WINGS / CENTER WING BOX / UPPER SKIN PANEL / UPPER SURFACE / Y1468 & STIFF 16-17 / CORROSION DAMAGE - PERMANENT REPAIR (THIS IS CONSIDERED A MAJOR REPAIR)
- [SDR YENA2021041600246](https://openairdocs.org/sdr/YENA2021041600246.md): Ball Lock · out of alignment · Apr 11, 2021 · N509JB · Airbus A320232 · Escape Slide
  > DURING HMV, MISALIGNED SLIDE WING 193AT FLUSH BALL LOCK; REF AEROMAN NR 2021-113247 WO 2021-116/1 R & R SLIDE WING 193AT IAW AMM 25-63-42-000-001-A
- [SDR YENA2021041600245](https://openairdocs.org/sdr/YENA2021041600245.md): Epsu · failed insp · Apr 11, 2021 · N509JB · Airbus A320232 · Emergency Lighting
  > DURING HMV, FAULT MESSAGE EPSU UNIT AFT L 13WL; REF AEROMAN NR 2021-113115 WO 2021 116/1 REMOVED AND REPLACED EPSU FIN POSITION 13WL ASPER AMM 33-51-38-000-001-A, AMM 33-51-38-400-001-A AND TSM 33-51-00-810-801-A AND PERFORMED OPERATIONAL CHECK OF THE EPSU AS
- [SDR YENA2021041600244](https://openairdocs.org/sdr/YENA2021041600244.md): Skin · corroded · Apr 11, 2021 · N509JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HMV, CORROSION UPPER SURFACE BTW RIB6 TO RIB7 AT LEVEL STR1 AND STR2 LEADING EDGE ON LH WING; REF AEROMAN NR REMOVED CORROSION ON UPPER SURFACE BTW RIB 6 TO RIB 7 AT LEVEL STR 1 AND STR 2 LEADING EDGE ON LH WING IAW A320 SRM 51-74-00, THEN EVALUATED RE
- [SDR YENA2021041600243](https://openairdocs.org/sdr/YENA2021041600243.md): Power Supply · faulted · Apr 11, 2021 · N509JB · Airbus A320232 · Emergency Lighting
  > DURING HMV, FAULT MESSAGE EPSU UNIT EMER L FIN 11WL; REF AEROMAN NR 2021-113451 WO 2021 115/1 REMOVED AND REPLACED EPSU FIN POSITION 11WL I.A.W A.M.M. 33-51-38-000-001-A, A.M.M. 33-51-38-400-001-A AND TSM 33-51-00-810-801-A AND PERFORMED OPERATIONAL CHECK OF T
- [SDR YENA2021041600241](https://openairdocs.org/sdr/YENA2021041600241.md): Skin · corroded · Apr 11, 2021 · N509JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HMV, CORROSION UPPER SURFACE OF UPPER SKIN CENTER WING BOX AT LEVEL FRAME 41 AND FR 42 BTW Y1292 AND Y1732 IN PASSENGER CABIN CPCP RELATED 571157-01; REF AEROMAN NR 2021-113286 WO 2021 116/1 PERFORMED PERMANENT REPAIR ON UPPER SURFACE OF CENTER WING B
- [SDR YENA2021041600240](https://openairdocs.org/sdr/YENA2021041600240.md): Floor Support · corroded · Apr 11, 2021 · N509JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HMV, CORROSION FLOOR BEAM + Y765 LOCATED BTW FR18 & FR19 AT FORWRD GALLEY AREA;REF AEROMAN NR 2021-113244 -REMOVED & REPLACED FLOOR BEAM +Y765 LOCATED BTW FR12-FR24 IAW A320 SRM 51-72-11-911-001 AND DRAWING D53111225 WORK ACCOMPLISHED BT R.CASTRO 8653
- [SDR YENA2021041600239](https://openairdocs.org/sdr/YENA2021041600239.md): Support · corroded · Apr 11, 2021 · N509JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HMV, COROSION LOWER SILL LOC. FR66 & FR68 STR 23R AFT GALLEY AREA; "REF AEROMAN NR W/O# 2021-116/1 WCC# 2021-113261 REMOVED AND REPLACED LOWER SILL LOC. FR66 & FR68 STR 23R AFT GALLEY AREA. IAW A320 SRM 51-72-11-911-001 & DWG# D53480020 (THIS IS CONSID
- [SDR YENA2021041600238](https://openairdocs.org/sdr/YENA2021041600238.md): Skin · corroded · Apr 11, 2021 · N509JB · Airbus A320232 · Wing, Center Box
  > DURING HMV, RER AEROMAN NR 2021-113286 CORROSION UPPER SURFACE OF UPPER SKIN CENTER WING BOX AT LEVEL FR41 AND FR42 BTW Y1292 AND Y1732 IN PASSENGER CABIN; "PERFORMED PERMANENT REPAIR ON UPPER SURFACE OF UPPER SKIN CENTER WING BOX AT FR41 TO FR42 BTW Y1292 AND
- [SDR YENA2021041600237](https://openairdocs.org/sdr/YENA2021041600237.md): Floorbeam · corroded · Apr 11, 2021 · N509JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HMV, CORROSION FLOOR BEAM + Y765 LOCATED BTW FR18 & FR19 AT FORWRD GALLEY AREA; REF AEROMAN NR 2021-113244 -REMOVED & REPLACED FLOOR BEAM +Y765 LOCATED BTW FR12-FR24 IAW A320 SRM 51-72-11-911-001 AND DRAWING D53111225 (THIS IS CONSIDERED A MAJOR REPAI
- [SDR YENA202006030363](https://openairdocs.org/sdr/YENA202006030363.md): Epsu · faulty · Jun 3, 2020 · N509JB · Airbus A320232 · Emergency Lighting
  > FLT 284, MCO-JFK. EPSU EXTERNAL LOAD FAULT/INTERNAL LOAD FAULT DURING OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM. PERFORMED TROUBLE SHOOTING IAW TSM 33-51-00-810-807-A FOR ESPU 13WL STOPPED AT STEP 7B. REQUIRES FURTHER TROUBLE SHOOTING. REF LOG PAGE 285
- [SDR YENA202006030362](https://openairdocs.org/sdr/YENA202006030362.md): Epsu · faulted · Jun 3, 2020 · N509JB · Airbus A320232 · Emergency Lighting
  > FLT 284, MCO-JFK. EPSU EXTERNAL LOAD FAULT/INTERNAL LOAD FAULT DURING OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM. PERFORMED TROUBLE SHOOTING IAW TSM 33-51-00-810-807-A FOR ESPU 13WL STOPPED AT STEP 7B. REQUIRES FURTHER TROUBLE SHOOTING. REF LOG PAGE 285
- [SDR YENA202001221831](https://openairdocs.org/sdr/YENA202001221831.md): Battery · failed · Jan 18, 2020 · N509JB · Airbus A320232 · Emergency Lighting
  > AS PER T/C: A320-33-51-00710-003 FOUND EPSU AND BATTERY EMERGENCY LIGHT TO BE AT FAULT AT LOCATION 13WL; R & R EPSU AND BATTERY EMERGENCY LIGHT IAW AMM 33-51-38.
- [SDR YENA202001221830](https://openairdocs.org/sdr/YENA202001221830.md): Epsu · failed · Jan 18, 2020 · N509JB · Airbus A320232 · Emergency Lighting
  > AS PER T/C: A320-33-51-00710-003 FOUND EPSU AND BATTERY EMERGENCY LIGHT TO BE AT FAULT AT LOCATION 13WL; R & R EPSU AND BATTERY EMERGENCY LIGHT IAW AMM 33-51-38.
- [SDR YENA2019110170629](https://openairdocs.org/sdr/YENA2019110170629.md): Wire Harness · damaged · Oct 27, 2019 · N509JB · Airbus A320232 · Light System Wiring
  > FT # 2922, PBI-BOS. LAST ROW LEFT HAND ESCAPE PATH LIGHT INOP. ( FLOOR PROX EMERG ESCAPE PATH MARK SYS - INCANDESCENT LIGHTING SYS - NOT APPLICABLE TO (N703 AND UP)); R & R LIGHT ASSY & HARNESS ASSY TO SIDEWALL PER A320 AMM 33-51-19. OPS CHECK SATISFACTORY.
- [SDR YENA2019082620474](https://openairdocs.org/sdr/YENA2019082620474.md): Wire Harness · inoperative · Aug 22, 2019 · N509JB · Airbus A320232 · Light System Wiring
  > 9ABC SEAT EMERGENCY PATH LIGHTING INOP. R & R 19 ABC PATH WHITE LIGHT HARNESS 7261VCA. OPS CHECKED GOOD IAW WMM 33-51-08.
- [SDR YENA2019040840179](https://openairdocs.org/sdr/YENA2019040840179.md): Slide · failed · Apr 4, 2019 · N509JB · Airbus A320232 · Escape Slide
  > FT # 391, DURING EMERGENCY LIGHT BITE AFT EPSU FAULT LIGHT FLASHING; T/S TO R2 SLIDE (POSSIBLE INTERNAL LIGHT SHORT). REMOVED AND REPLACED R2 DOOR SLIDE IAW AMM 25-62-44-400-803A.
- [SDR YENA2019040840178](https://openairdocs.org/sdr/YENA2019040840178.md): Power Supply · failed · Apr 4, 2019 · N509JB · Airbus A320232 · Emergency Lighting
  > FT # 391, 3 ROWS OF LOW LEVEL LIGHTING INOP; REMOVED AND REPLACED AFT EPSU (13WL) IAE AMM 33-51-38. OPS CKD GOOD
- [SDR YENA2019040840177](https://openairdocs.org/sdr/YENA2019040840177.md): Battery Pack · no test · Apr 4, 2019 · N509JB · Airbus A320232 · Emergency Lighting
  > FT # 391, EMERGENCY LIGHT TEST FAILED EPSU BATTERY 11WL; REMOVED AND REPLACED EPSU BATTERY AT FIN 11WL IAW AMM 33-51-38.
- [SDR YENA201903120128](https://openairdocs.org/sdr/YENA201903120128.md): Fan · failed · Mar 12, 2019 · N509JB · Airbus A320232 · Air Distribution Fan
  > FLT 1992, TPA-BOS. FL 330 VENT EXTRACT FAULT LOUD BUZZ FOLLOWED BY SLIGHT ELECTRICAL BURNING SMELL AVIONICS VENT EXTR CIRCUIT BREAKER POPPED (EXTRACT FAN - NO AVNCS SYS FAULT ECAM CAUTION); R & R EXTRACT FAN IAW AMM 21-26-51. OPS CHECK GOOD. MX4 UPDATED, PLACA
- [SDR YENA201903120123](https://openairdocs.org/sdr/YENA201903120123.md): Battery · failed · Mar 12, 2019 · N509JB · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EPSU BATTERY 10WL FAILS EMERG. LIGHT SYSTEM TEST; R & R BATTERY AT EPSU 10WL IAW AMM 33-51-38 SYSTEM CHECKS OK.
- [SDR YENA2018120730817](https://openairdocs.org/sdr/YENA2018120730817.md): Skin · corroded · Dec 3, 2018 · N509JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE BTWN RIB 4-5 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 4-5 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. THIS JOB M
- [SDR YENA2018120730816](https://openairdocs.org/sdr/YENA2018120730816.md): Skin · corroded · Dec 3, 2018 · N509JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE BTWN RIB1-2 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 1-2 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. THIS JOB MU
- [SDR YENA2018120730815](https://openairdocs.org/sdr/YENA2018120730815.md): Skin · corroded · Dec 3, 2018 · N509JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED UPPER SURFACE AT LEVEL RIB 7 ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BETWEEN RIB 7 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. REF. AE
- [SDR YENA2018120730814](https://openairdocs.org/sdr/YENA2018120730814.md): Skin · corroded · Dec 3, 2018 · N509JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN LOCATED BTWN RIB 8-9 UPPER SURFACE ON LH WING; PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTWN RIB 8-9 UPPER SURFACE ON LH WING IAW EA 57-0384-18 REV.0 PART 1 & 2 / EC A18-990-01. REF. AEROM
- [SDR YENA2018120730813](https://openairdocs.org/sdr/YENA2018120730813.md): Floor Support · corroded · Dec 3, 2018 · N509JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR BEAM -Y1162 LOCATED BTW FR 68 TO FR 70 AT AFT GALLEY AREA; REF BP NR # 2018-395184 REPLACED FLOOR BEAM -Y1162 LOCATED BTW FR 68 TO FR 70 AFT GALLEY AREA IAW SRM A320 51-42-11 & 51-72-11 AND DRAWING D5
- [SDR YENA201802070062](https://openairdocs.org/sdr/YENA201802070062.md): Battery · failed · Feb 7, 2018 · N509JB · Airbus A320232 · Emergency Lighting
  > FLT 225, JFK-TPA. EMERGENCY LIGHT BATTERY 12WL FAILED CAP TEST. R & R BATTERY IAW AMM 33-51-01, OPS CKS OK.
- [SDR YENA201802070061](https://openairdocs.org/sdr/YENA201802070061.md): Battery · failed · Feb 7, 2018 · N509JB · Airbus A320232 · Emergency Lighting
  > FLT 225, JFK-TPA. EMERGENCY LIGHT BATTERY 11WL FAILED CAP TEST. R & R BATTERY IAW AMM 33-51-01, OPS CKS OK.

Next page: https://openairdocs.org/aircraft/N509JB/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 = 'N509JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N509JB/reports

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