# Service difficulty reports: N641JB

A list on [N641JB](https://openairdocs.org/aircraft/N641JB.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 · 61 reports

- [SDR YENA2025121501202](https://openairdocs.org/sdr/YENA2025121501202.md): Filter · odor · Dec 14, 2025 · N641JB · Airbus A320232 · Air Distribution System
  > FLT#1437, BDL-MCO. FUME EVENT FROM 10000FT TO AFTER LANDING AND TO GATE. PACK 1 ONLY THE BACK OF CABIN WAS FINE VERY STRONG AT 3000FT AND RIGHT AFTER LANDING; C/W WITH INFO NOTICE 2017-T015L TROUBLESHOOT APU ODOR R/R RECIRCULATION FILTERS IAW AMM 21-21-41 PER
- [SDR YENA2025091700944](https://openairdocs.org/sdr/YENA2025091700944.md): Ecs · contaminated · Sep 15, 2025 · N641JB · Airbus A320232 · Air Conditioning System
  > FLT#172, FLL-LGA. CABIN CREW REPORTED FUMES DURING DESCENT IN ROWS 10-15. SMELL OF CHEMICALS OR DIRTY SOCKS; COMPLIED WITH INO NOTICE 2017-T015, ACCOMPLISHED ECS DECONTAMINATION AND REPLACED HEPA FILTERS AND OZONE FILTERS, REF PAGE 4527976 AND 4527977. A/C OK
- [SDR YENA2025091500931](https://openairdocs.org/sdr/YENA2025091500931.md): Oil System · leaking · Sep 14, 2025 · N641JB · Airbus A320232 · APU Oil System
  > FLT#1383, GUA-FLL. "FUMES EVENT ON DECENT THROUGHT 10,000 FEET STUNK IN BACK LESS UP FRONT DIRTY SOCKS OIL; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2 TYPE 1 APU AND PERFORMED DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. AIRC
- [SDR YENA2025091500930](https://openairdocs.org/sdr/YENA2025091500930.md): Unknown · fumes · Sep 13, 2025 · N641JB · Airbus A320232 · Air Distribution System
  > FLT#1380, FLL-GUA. "INFLIGHT COMPLAINED ABOUT FUMES AFTER LANDING BOTH ENGINES OFF APU ON WITH APU BLEED NO NOTIFICATION DURING FLIGHT ( APU SYSTEM).
- [SDR YENA2025082800892](https://openairdocs.org/sdr/YENA2025082800892.md): Oil Cooler · leaking · Aug 27, 2025 · N641JB · Airbus A320232 · APU Oil System
  > FLT#1406, SDQ-MCO. "AFTER LANDING WE CHANGED OVER TO APU BLEED ON TAXIWAY. WE NOTICED A BURNING OIL SMELL UPON DOOR, INFLIGHT MONITORED THE SMELL WAS STRONG IN THE CABIN AS WELL; COMPLIED WITH INFO NOTICE 2017-T015-L SECTION B2. IDENTIFY ODOR SOURCE TO BE THE
- [SDR YENA2025081300832](https://openairdocs.org/sdr/YENA2025081300832.md): Intake · contaminated · Aug 11, 2025 · N641JB · Airbus A320232 · APU Core Engine
  > FLT#525, PVD-SJU. "FUMES NOTICIED IN AFT CABIN BY FA'S VERY STRONG SMELL OF BURNT FUEL OR HYDRAULICS THE SMELL IS REDUCED AFTER PACK 2 0FF; DURING THE PROCEDURES FOLLOWED TO HANDLE THIS ODOR EVENT, THE SOURCE OF THE ODOR WAS FOUND TO BE APU, ALSO FOUND THE AIR
- [SDR YENA2024011200038](https://openairdocs.org/sdr/YENA2024011200038.md): Unknown · unknown · Jan 10, 2024 · N641JB · Airbus A320232 · Standard Practices/Structures
  > FLT#1468, PBI-HPN. (AIRCRAFT DIVERTED TO SYR) 'MODERTAE TO SEVER TURBULANCE ON APPROACH TO HPN FLAP OVERSPEED REQUIRES INSPECTION; PERFORMED FLAP OVERSPEED INSP IAW AMM 05-51-13. NO DEFECTS FOUND PER MCC LOUIS.'
- [SDR YENA2023112201444](https://openairdocs.org/sdr/YENA2023112201444.md): Control Valve · failed · Nov 21, 2023 · N641JB · Airbus A320232 · Airfoil Anti/De-ice System
  > FLT#2439, LGA-JFK. 'WING A.ICE SYS FAULT ECAM IT WOULD APPEAR VALVE NEVER OPEN BECAUSE FAULT LIGHT IN WING ANTI-ICE BUTTON REMAINED ILLUMINATED AFTER INITIAL BUTTON PRESS AND NEVER EXTINGUISHED, SYSTEM FAULT IMMEDIATELY AFTER BEING TURNED ON. INCREASE POWER DI
- [SDR YENA2023103001332](https://openairdocs.org/sdr/YENA2023103001332.md): Unknown · unknown · Oct 26, 2023 · N641JB · Airbus A320232 · Air Distribution System
  > FLT#2510, SDQ-JFK. 'FUME EVENT - ON TAKEOFF ROLL- OIL FUMES (DIRTY SOCKS) IN COCKPIT; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10,(A), 1C PER TSM 05-50-00-810-085-B / TSM 05-50-00-810-085-D. REMOVED AND REPLACED RECIRCULATI
- [SDR YENA2023101001212](https://openairdocs.org/sdr/YENA2023101001212.md): Unknown · unknown · Oct 6, 2023 · N641JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN SLAT 2 ON RH WING; REF AEROMAN W/O 2023 277/1 WCC 2023 - 533561. PERFORMED REPAIR LOC. EXTERNAL SKIN SLAT 2 ON RH WING IAW A320 SRM 57-40-00-300-023 THIS REPAIR IS CATEGORY A. NO REQUIRED FURTHER INSPECTION.
- [SDR YENA2023101001211](https://openairdocs.org/sdr/YENA2023101001211.md): Unknown · unknown · Oct 6, 2023 · N641JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOC. BTW FR 24 TO FR 25 AT LEVEL STRINGER 41R TO ST RINGER 42R AT LOWER FUSELAGE; (RESOLVED ON W/O: 1240686 TASKCARD: NR-00004) REF AEROMAN W/O 277/1 WCC 2023-533495 EVALUATED DENT ON EXTERNAL SKIN LOC. BTW FR 24 T
- [SDR YENA2023101001210](https://openairdocs.org/sdr/YENA2023101001210.md): Unknown · unknown · Oct 6, 2023 · N641JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN FASTENER HOLE H1 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION ARE 8, 9 AND 10 OCLOCK, CRACK DEPT H IS 0.197 INCH APPROX; REF AEROMAN WO 2023-277/1 WCC 2023 - 533689 REMOVED AND REPLACED INTE
- [SDR YENA2023101001209](https://openairdocs.org/sdr/YENA2023101001209.md): Unknown · unknown · Oct 6, 2023 · N641JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN FASTENER HOLE H3 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION ARE 7, 9, 11 AND 12 OCLOCK, CRACK DEPTH IS 0.213 INCH APPROX; REF AEROMAN WO 2023-277/1 WCC 2023-533690 REMOVED AND REPLACED INT
- [SDR YENA2023101001208](https://openairdocs.org/sdr/YENA2023101001208.md): Unknown · unknown · Oct 6, 2023 · N641JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON LOWER SILL LOCATED BTW FR 61 TO FR 62 AT LEVEL OF STR 38R BULK CARGO COMPARTMENT; (RESOLVED ON W/O: 1240686 TASKCARD: NR-00005) REF AEROMAN WO 2023-277/1 WCC 2023 - 533702 PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED
- [SDR YENA2023101001207](https://openairdocs.org/sdr/YENA2023101001207.md): Unknown · unknown · Oct 6, 2023 · N641JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT IN TERNAL AREA RH SIDE, LOWER TENSION BOLT, CRACK LENGTH IS 0.110 INCH AP PROXIMATELY. IN COCKPIT (1 EA) REF AEROMAN W/O 2023 277/1 WCC 2023-533624; REF AEROMAN W/O 2
- [SDR YENA2022091900930](https://openairdocs.org/sdr/YENA2022091900930.md): None · none · Sep 17, 2022 · N641JB · Airbus A320232 · Air Conditioning System
  > FLT#76, MSY-JFK. 'STRONG MUSTY ODOR DESCENDING THROUGH 6,000 SOURCES WAS THE AIR VENTS IN THE FLIGHT DECK. PERFORMED ODOR ISOLATION PROCEDURE. THE ODOR STOPPED AFTER TURNING OFF PACK #1 (ABOUT 3,000 FEET); COMPLIED WITH INFO NOTICED 2017-T015, SECTION A, ISOL
- [SDR YENA2022072200673](https://openairdocs.org/sdr/YENA2022072200673.md): None · none · Jul 21, 2022 · N641JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#276, SJU-BDL. (AIRCRAFT PERFORMED AN AIR TURN BACK TO SJU) ' PASSING 9'000 FEET FAS REPORTED BURNING RUBBER SMELL THEY REPORTED THE SMELL STARTED AFTER T/O FUMES CHECKLIST COMPLETED SMELL D15 REDUCED SMELL NOTICED FROM ROW 3 FWD; PERFORMED FIM 05-50-00-81
- [SDR YENA2022050500444](https://openairdocs.org/sdr/YENA2022050500444.md): None · none · Apr 27, 2022 · N641JB · Airbus A320232 · Fuselage, Stabilizer Attach Fittings
  > DURING HEAVY MAINTENANCE: A CRACK INDICATION WAS FOUND INSIDE OF THE INNER EMERGENCY EXIT HATCH FRAME SEGMENT (1) OF THE FWD RH SIDE DOOR 843; REF AEROMAN WO # 2022 71/1, NR 2022-205389; PERFORMED FRAME / RE-ENFORCE DOOR STRUCTURE MODIFICATION ON EEH DOOR 843
- [SDR YENA2022050500443](https://openairdocs.org/sdr/YENA2022050500443.md): None · none · Apr 27, 2022 · N641JB · Airbus A320232 · Fuselage, Stabilizer Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND INSIDE OF THE INNER EEH FRAME SEGMENT (), OF THE AFT LH SIDE DOOR 834 AT AFT AND FWD SIDE POSITION; REF AEROMAN WO 2022 71/1, NR 2022-205390, PERFORMED FRAME / REINFORCEMENT DOOR STRUCTURE MODIFICATION ON EEH DO
- [SDR YENA2022050500442](https://openairdocs.org/sdr/YENA2022050500442.md): Nonskid · none · Apr 27, 2022 · N641JB · Airbus A320232 · Fuselage, Stabilizer Attach Fittings
  > DURING HEAVY MAINTENANCE: A CRACK INDICATION WAS FOUND INSIDE OF THE INNER EEH FRAME SEGMENT (1), OF THE FWD LH SIDE DOOR 833 AT AFT SIDE POSITION; REF AEROMAN WO 2022 71/1, NR 2022-205388; PERFORMED FRAMED FRAME / REINFORCEMENT DOOR STRUCTURE MODIFICATION ON
- [SDR YENA2022050500441](https://openairdocs.org/sdr/YENA2022050500441.md): Nonskid · none · Apr 27, 2022 · N641JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: DENT EXTERNAL SKIN LOC BTW FR81 AND FR 82 AT STR 2RH AND 3RH ON UPPER FUSELAGE; REF AEROMAN WO 2022 71/1, NR 2022-205434, PERFORMED PERMANENT REPAIR LOC EXTERNAL SKIN BTW FR81 AND FR82 AT STR 2RH AND 3RH ON UPPER FUSELAGE IAW SRM 53-5
- [SDR YENA2021021800101](https://openairdocs.org/sdr/YENA2021021800101.md): Power Supply · inoperative · Feb 5, 2021 · N641JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, INOP EPSU 13WL; (REF AEROMAN NR 2021-71/1-2021-59122) R & R EPSU 13WL IAW A320 AMM 33-51-38-000-001-A. OPS CHECK GOOD
- [SDR YENA2020022060191](https://openairdocs.org/sdr/YENA2020022060191.md): Light · failed · Feb 16, 2020 · N641JB · Airbus A320232 · Emergency Lighting
  > FT # EWR-TPA. L2 DOOR ESCAPE SLIDE LIGHTING FAILED EMERGENCY LIGHT TEST ( ESCAPE SLIDE LIGHTING); R & R L2 DOOR SLIDE IAW AMM 25-62-44-400-007-A DOOR OPS CHECK OK, EMERGENCY LIGHT SYSTEM TEST OK, THIS CLEARS MDDR#415365, MX-4 UPDATED, PLCARD REMOVED.
- [SDR YENA2020022060189](https://openairdocs.org/sdr/YENA2020022060189.md): Battery · no test · Feb 16, 2020 · N641JB · Airbus A320232 · Emergency Lighting
  > FT # 273, EWR-TPA. EMERGENCY LIGHT TEST FAILED; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES 12WL & 13WL PER AMM 33-51-38
- [SDR YENA2020022060188](https://openairdocs.org/sdr/YENA2020022060188.md): Battery · failed · Feb 16, 2020 · N641JB · Airbus A320232 · Emergency Lighting
  > FT # 273, EWR-TPA. EMERGENCY LIGHT TEST FAILED; REMOVED & REPLACED EMERGENCY LIGHT BATTERIES 12WL & 13WL PER AMM 33-51-38
- [SDR YENA2019061730324](https://openairdocs.org/sdr/YENA2019061730324.md): Slide · no test · Jun 13, 2019 · N641JB · Airbus A320232 · Escape Slide
  > R2 DOOR SLIDE FAILED EMERGENCY LIGHT TEST ( ESCAPE SLIDE LIGHTING); T/S PER TSM 33-51-00-810-808-A. FOUND ELECTRICAL CONNECTOR ON R2 SLIDE NOT FULLY SECURED. SECURED CONNECTOR AND PERFORMED OPS CHECK IAW AMM 33-51-00. OPS CHECK GOOD. MDDR CLEARED.
- [SDR YENA201906139321](https://openairdocs.org/sdr/YENA201906139321.md): Battery · failed · Jun 9, 2019 · N641JB · Airbus A320232 · Emergency Lighting
  > FT # 391, MCO-TPA. EMERGENCY LIGHT TEST FAILED EPSU AT FIN 10WL BATTERY; REMOVED & REPLACED EPSU BATTERY AT FIN 10WL PER AMM 33-51038.
- [SDR YENA201808270329](https://openairdocs.org/sdr/YENA201808270329.md): Unknown · odor · Aug 27, 2018 · N641JB · Airbus A320232 · Air Distribution System
  > FLT 6106, MBJ-JFK. " FOUL SMELL" CLIMB FROM 300 TO 360; COMPLIED WITH INFORMATION NOTICE 2017-T015C SECTION A. AIRCRAFT IS OKAY FOR SERVICE.
- [SDR YENA201803150965](https://openairdocs.org/sdr/YENA201803150965.md): Skin · warped · Mar 15, 2018 · N641JB · Airbus A320232 · Landing Gear Doors
  > THE RT MLG DOOR (P/N D5288016500500, SN AR5146) WAS FOUND WITH THE OUTER CONTOUR DISTORTED/WARPED. THE DOOR WAS SENT TO FOR REPAIR AND COULD NOT SUPPORT. SUBSEQUENTLY THE MLG DOOR WAS SENT FOR REPAIR UNDER RO2060419 (WO: W13079). ASSESSED THE DAMAGE AND DEVE
- [SDR YENA201803140964](https://openairdocs.org/sdr/YENA201803140964.md): Skin · warped · Mar 14, 2018 · N641JB · Airbus A320232 · Landing Gear Doors
  > THE LT MLG DOOR (P/N D5288016500400 SN AR5146) WAS FOUND WITH THE OUTER CONTOUR DISTORTED/WARPED. THE DOOR WAS SENT FOR REPAIR AND COULD NOT SUPPORT. SUBSEQUENTLY THE MLG DOOR WAS SENT FOR REPAIR UNDER RO2060412 (WO: 13080). ASSESSED THE DAMAGE AND DEVELOPED
- [SDR YENA201708200685](https://openairdocs.org/sdr/YENA201708200685.md): Seat Track · corroded · Aug 20, 2017 · N641JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON TOP FACE MAIN CABIN RT SEAT TRACK -Y1292. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-11-15.
- [SDR YENA201708200684](https://openairdocs.org/sdr/YENA201708200684.md): Seat Track · corroded · Aug 20, 2017 · N641JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN LT SEAT TRACK Y1292 AT FRAME 16; REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-11-15, AND 51-42-11.
- [SDR YENA201708200683](https://openairdocs.org/sdr/YENA201708200683.md): Floorbeam · corroded · Aug 20, 2017 · N641JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN FLOORBEAM -Y765; REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-41-14 FIG 001.
- [SDR YENA201707030553](https://openairdocs.org/sdr/YENA201707030553.md): Battery · discharged · Jul 3, 2017 · N641JB · Airbus A320232 · Emergency Lighting
  > FT 225, JFK-TPA. EMERGENCY LIGHT FAILS TEST. R&R EMERGENCY LIGHT BATTERY AT 12WL AND 13WL IAW AMM 33-51-38. EMER LIGHT TEST OK. SUPPLEMENTAL INFORMATION TO FOLLOW.
- [SDR YENA201707030552](https://openairdocs.org/sdr/YENA201707030552.md): Battery · discharged · Jul 3, 2017 · N641JB · Airbus A320232 · Emergency Lighting
  > FT 225, JFK-TPA. EMERGENCY LIGHT FAILS TEST. R&R EMERGENCY LIGHT BATTERY AT 12WL AND 13WL IAW AMM 33-51-38. EMER LIGHT TEST OK. SUPPLEMENTAL INFORMATION TO FOLLOW.
- [SDR YENA201706130485](https://openairdocs.org/sdr/YENA201706130485.md): Sign · malfunctioned · Jun 13, 2017 · N641JB · Airbus A320232 · Emergency Lighting
  > AIRCRAFT'S LEFT EXIT SIGN INOPERATIVE. RESET EXIT SIGN.
- [SDR YENA201706020462](https://openairdocs.org/sdr/YENA201706020462.md): Hydraulic Line · loose · Jun 2, 2017 · N641JB · Airbus A320232 · Hydraulic System, Main
  > FT 573, EWR-TPA. STEADY DECREASE IN HYD FLUID TO THE GREEN SYSTEM ENROUTE UNTIL WE RECEIVED GREEN QUALITY LO ECAM COMPLIED WITH ECAM AND LANDED UNEVENLY. FOUND HYDRAULIC LINE LEAKING TIGHTENED LINE IAW AMM 29-11-00. ACCOMPLISHED FUNCTIONAL CHECK OF ALL FLIGHT
- [SDR YENA201706010461](https://openairdocs.org/sdr/YENA201706010461.md): Valve · malfunctioned · Jun 1, 2017 · N641JB · Airbus A320232 · Trailing Edge Flap Control System
  > FT # 1075, PVD-MCO. EMERGENCY DECLARED. F/CTL FLAP FAULT ON GLIDE SLOPE WHEN SELECTING FLAP POSITION 2; R & R SYSTEM 2 FLAP PCU PRESSURE OFF BRAKE, HYDRAULIC MOTOR AND VALVE BLOCK IAW AMM 27-54-52, 27-54-53, 27-54-54 ALSO R & R SFCC 2 AS PRECAUTIONARY IAW AMM
- [SDR YENA201706010460](https://openairdocs.org/sdr/YENA201706010460.md): Sensor · malfunctioned · Jun 1, 2017 · N641JB · Airbus A320232 · Trailing Edge Flap Control System
  > EMERGENCY DECLARED. F/CTL FLAP FAULT ON GLIDE SLOPE WHEN SELECTING FLAP POSITION 2; R & R SYSTEM 2 FLAP PCU PRESSURE OFF BRAKE, HYDRAULIC MOTOR AND VALVE BLOCK IAW AMM 27-54-52, 27-54-53, 27-54-54. R & R SFCC 2 AS PRECAUTIONARY IAW AMM 27-51-34. SYSTEM OPS CHE
- [SDR YENA201706010459](https://openairdocs.org/sdr/YENA201706010459.md): Motor · malfunctioned · Jun 1, 2017 · N641JB · Airbus A320232 · Hydraulic System, Main
  > EMERGENCY DECLARED. F/CTL FLAP FAULT ON GLIDE SLOPE WHEN SELECTING FLAP POSITION 2; R & R SYSTEM 2 FLAP PCU PRESSURE OFF BRAKE, HYDRAULIC MOTOR AND VALVE BLOCK IAW AMM 27-54-52, 27-54-53, 27-54-54. R & R SFCC 2 AS PRECAUTIONARY IAW AMM 27-51-34. SYSTEM OPS CH
- [SDR YENA201706010458](https://openairdocs.org/sdr/YENA201706010458.md): Valve · unknown · Jun 1, 2017 · N641JB · Airbus A320232 · Trailing Edge Flap Control System
  > FLAP FAULT ON GLIDE SLOPE WHEN SELECTING FLAP POSITION 2. R & R THE NR 2 SYSTEM FLAP PCU PRESSURE OFF BRAKE, HYDRAULIC MOTOR AND VALVE BLOCK IAW AMM 27-54-52, 27-54-53, 27-54-54. R & R SFCC 2 AS PRECAUTIONARY IAW AMM 27-51-34. SYSTEM OPS CHECKED NORMAL.
- [SDR YENA201705160381](https://openairdocs.org/sdr/YENA201705160381.md): Filter · odor · May 16, 2017 · N641JB · Airbus A320232 · Air Distribution System
  > DIRTY SOCK ODOR WHILE PASSING THROUGH 7500 - 5000 FT DURING DESCENT. ODOR SEEMED STRONGEST IN THE COCKPIT. NR 1 ENGINE CHANGE ACCOMPLISHED IAW W/O 847556. R & R THE OZONE FILTERS 1 & 2. NO LEAKS NOTED IAW MM 21-51-41. ACCOMPLISHED A PACK BURNOUT IAW MM 2
- [SDR YENA201705160380](https://openairdocs.org/sdr/YENA201705160380.md): Filter · odor · May 16, 2017 · N641JB · Airbus A320232 · Air Distribution System
  > DIRTY SOCK ODOR WHILE PASSING THROUGH 7500 - 5000FT DURING DESCENT. ODOR SEEMED STRONGEST IN THE COCKPIT NR 1 ENGINE CHANGE ACCOMPLISHED IAW W/O 847556. R & R THE OZONE FILTERS 1 & 2. NO LEAKS NOTED IAW MM 21-51-41. ACCOMPLISHED A PACK BURNOUT IAW MM 21-00-
- [SDR YENA201705160379](https://openairdocs.org/sdr/YENA201705160379.md): Engine · odor · May 16, 2017 · N641JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > PILOTS DETECTED A DIRTY SOCK ODOR WHILE PASSING THROUGH 7500 - 5000 FT DURING DESCENT. ODOR SEEMED STRONGEST IN THE COCKPIT. NR 1 ENGINE CHANGE ACCOMPLISHED IAW W/O 847556. R & R THE OZONE FILTERS 1 & 2. NO LEAKS NOTED IAW MM 21-51-41. ACCOMPLISHED A PAC
- [SDR YENA201705140363](https://openairdocs.org/sdr/YENA201705140363.md): Filter · odor · May 14, 2017 · N641JB · Airbus A320232 · Air Distribution System
  > DIRTY SOCK ODOR ON DESCENT AROUND 5000 FEET, WITH ENGINE BLEEDS ON AND, NO APU, AND BOTH PACKS ON. PERFORMED TROUBLESHOOTING IAW TSM 05-50-00-810-831-A. PERFORMED AN ENGINE WASH IAW EMM 72-00-00-100-001-B00. R & R THE RT & LT OZONE FILTERS IAW AMM 21-51-4
- [SDR YENA201705140362](https://openairdocs.org/sdr/YENA201705140362.md): Filter · odor · May 14, 2017 · N641JB · Airbus A320232 · Air Distribution System
  > DIRTY SOCK ODOR DURING DESCENT, AROUND 5000 FEET, WITH ENGINE BLEEDS ON, NO APU, AND BOTH PACKS ON. PERFORMED TROUBLESHOOTING IAW TSM 05-50-00-810-831-A. PERFORMED AN ENGINE WASH IAW EMM 72-00-00-100-001-B00. R & R THE RT & LT OZONE FILTERS IAW AMM 21-51-41
- [SDR YENA201704040243](https://openairdocs.org/sdr/YENA201704040243.md): Filter · odor · Apr 4, 2017 · N641JB · Airbus A320232 · Air Distribution System
  > ODOR DURING DESCENT FROM PACKS, STRONGER ODOR WITH APU BLEED. R & R THE NR 1 & 2 PACKS OZONE FILTERS IAW AMM 21-51-41. PERFORMED HIGH POWER RUN ASSURANCE CHECK, ISOLATED PACKS, NO ODOR PRESENT. OK FOR SERVICE.
- [SDR YENA201704040242](https://openairdocs.org/sdr/YENA201704040242.md): Filter · odor · Apr 4, 2017 · N641JB · Airbus A320232 · Air Distribution System
  > ODOR DURING DESCENT FROM PACKS, STRONGER ODOR WITH APU BLEED. R & R THE NR 1 & 2 PACKS OZONE FILTERS IAW AMM 21-51-41. PERFORMED HIGH POWER RUN ASSURANCE CHECK, ISOLATED PACKS, NO ODOR PRESENT. OK FOR SERVICE.
- [SDR YENA20161111977](https://openairdocs.org/sdr/YENA20161111977.md): Epsu · failed · Nov 11, 2016 · N641JB · Airbus A320232 · Emergency Lighting
  > FWD EXIT LIGHTS OVER BOTH PASSENGER DOORS WERE INOPERATIVE. R & R EPSU (10WL) IAW AMM 33-51-38. PERFORMED OPS CHECKS. OPS CHECKD PASSED.
- [SDR YENA20160413289](https://openairdocs.org/sdr/YENA20160413289.md): Sensor · failed · Apr 13, 2016 · N641JB · Airbus A320232 · Landing Gear Position and Warning
  > EMERGENCY DECLARED. NLG UNLOCK INDICATION ON LANDING GEAR PANEL UPON LOWERING GEAR; PERFORMED VISUAL INSPECTION OF NLG UPLOCK ACTUATOR AND FOUND 12GA SENSOR DISCONNECTED. CLEANED CONNECTOR PLUG AND PERFORMED DETAILED INSPECTION OF CONNECTOR PLUG CONNECTIONS

Next page: https://openairdocs.org/aircraft/N641JB/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 = 'N641JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N641JB/reports

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