# Service difficulty reports: N639JB

A list on [N639JB](https://openairdocs.org/aircraft/N639JB.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR YENA2026030600271](https://openairdocs.org/sdr/YENA2026030600271.md): Unknown · odor · Mar 4, 2026 · N639JB · Airbus A320232 · Air Distribution System
  > FLT # 321 BOS -PBI. "ODOR /FUMES BETWEEN 14000-8000 EXPERIENCED IN COCKPIT DURING APPROACH.; INSP ENG'S A/C BELLY, APU. NO FINDINGS, NO ODOR NOTED. C/W INFO NOTICE 2017-T015. STEPS 1+2. IDENTIFIED ODOR AS TYPE 10. ACCONPLISHED DECONTAMINATION LEVEL B. PER TSM
- [SDR YENA2025012700110](https://openairdocs.org/sdr/YENA2025012700110.md): Unknown · odor · Jan 26, 2025 · N639JB · Airbus A320232 · Air Distribution System
  > FLT#1471, LGA-FLL. 'BURNING RUBBER SMELL ON DESCENT ( PACKS) FA REPORTED AN ODOR OF RUBBER NEAR L2 OOR AT 1400' ON FINAL APPROACH ODOR DETECTED IN COCKPIT OPUN ENGINE SHUTDOWN AT GATE.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2024051600751](https://openairdocs.org/sdr/YENA2024051600751.md): Unknown · odor · May 15, 2024 · N639JB · Airbus A320232 · Air Distribution System
  > FLT#1255, SJO-FLL. 'BURNING SMELL IN THE CABIN AND FLIGHT DECK; PERFORMED TSM 05-50-00-810-831A. NO BURNING SMELL NOTED. A/C OK FOR SVC.'
- [SDR YENA2023100901201](https://openairdocs.org/sdr/YENA2023100901201.md): Unknown · unknown · Oct 7, 2023 · N639JB · Airbus A320232 · Air Distribution System
  > FLT#163, JFK-SRQ. 'FA COMPLAINS OF ODOR DIRTY SOCK (OILY SMELL). FIRST ON TAXI. THEN ON DESCENT; C/W INFO NOTICE.ISOLATED FAULT TO TYPE 10 (A/C) PER TSM 05-50-00-810-085.RAN ENGINES AND BLEED SYSTEM WITH NO SMELL DETECTED.A/C OK FOR CONT SVC.'
- [SDR YENA2023100301183](https://openairdocs.org/sdr/YENA2023100301183.md): Not Reported · not reported · Oct 2, 2023 · N639JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 833 IN FRAME SEGMENTS 1, CRACK L = 0.125 INCH APPROX IN PASSENGER CABIN; (RESOLVED ON W/O: 1265460 TASKCARD: NR-00002) REF AE W/O # 2023 274/1 N/R# 2023-526562. ACCOMPLISHED REINFORCEMENT DOOR S
- [SDR YENA2023100301182](https://openairdocs.org/sdr/YENA2023100301182.md): Not Reported · not reported · Oct 2, 2023 · N639JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 843 IN FRAME SEGMENTS 1, CRACK L = 0.110 INCH APPROX IN PASSENGER CABIN; (RESOLVED ON W/O: 1265460 TASKCARD: NR-00003) REF AE W/O# 2023 274/1 N/R# 2023-526563. ACCOMPLISHED REINFORCEMENT DOOR S
- [SDR YENA2023100301181](https://openairdocs.org/sdr/YENA2023100301181.md): Not Reported · not reported · Oct 2, 2023 · N639JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 834 IN FRAME SEGMENTS 1, CRACK L = 0.095 INCH APPROX IN PASSENGER CABIN; (RESOLVED ON W/O: 1265460 TASKCARD: NR-00004) REF AE W/O# 2023 274/1 N/R# 2023-526564. ACCOMPLISHED REINFORCEMENT DOOR S
- [SDR YENA2023100301180](https://openairdocs.org/sdr/YENA2023100301180.md): Not Reported · not reported · Oct 2, 2023 · N639JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHEILD CENTER POST LOWER ATTACHMENT INTERNAL AREA RH SIDE, UPPER TENSION BOLT, CRACK LENGTH IS 0.125 INCH APPROX IN COCKPIT (1 EA); (RESOLVED ON W/O: 1257978 TASKCARD: NR-00037) REFERENCE AEROMAN W.O. 2023 2
- [SDR YENA2023100301179](https://openairdocs.org/sdr/YENA2023100301179.md): Not Reported · not reported · Oct 2, 2023 · N639JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHEILD CENTER POST LOWER ATTACHMENT INTERNAL AREA LH SIDE UPPER TENSION BOLT, CRACK LENGTH IS 0.125 APPROX IN COCKPIT; (RESOLVED ON W/O: 1257978 TASKCARD: NR-00038) REFERENCE AEROMAN W.O. 2023 274/1 NR 2023-
- [SDR YENA2023100301178](https://openairdocs.org/sdr/YENA2023100301178.md): Not Reported · not reported · Oct 2, 2023 · N639JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST UPPER FASTENERS LH-RH AREA / CRACK - TEMPORARY REPAIR. (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2023072000843](https://openairdocs.org/sdr/YENA2023072000843.md): Unknown · unknown · Jul 19, 2023 · N639JB · Airbus A320232 · Air Conditioning System
  > FLT#2701, JFK-FLL. 'DIRTY SOCK ODOR SMELL WAS PRESENT FROM TOP OF DECENT AT FL 360 ALL THE WAY TO TAXI AT GATE; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2, DECONTAMINATION LEVEL 2 WAS ACCOMPLISHED PER TSM 05-50-00-710-080-A. THE AIRCRAFT IS OK FOR S
- [SDR YENA2022052000502](https://openairdocs.org/sdr/YENA2022052000502.md): Bleed Valve · fault message · May 17, 2022 · N639JB · Airbus A320232 · Compressor Bleed Control
  > FLT#1018, FLL-JAX. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL). ' ENG 1 COMPRESSOR VANE, AVOID THRUST CHANGES ECAM; SEE L/P 3327939 ITEM 2 (ACCOMPLISHED VISUAL CHECK OF ELEC CONNECTORS ON 2.5 BLEED ACTUATOR. NO DAMAGE OR MISALIGNMENT WAS FOUND. PERFORMED LUBR
- [SDR YENA2022050200432](https://openairdocs.org/sdr/YENA2022050200432.md): None · none · Apr 30, 2022 · N639JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#1589, EWR-SJU. ' ON DESCENT PASSING THROUGH CLOUDS ODOR LIKE SWEATY SOCKS LASTING FOR 5MINUTES WAS DETECTED IN THE COCKPIT ONLY. ON GATE ARRIVAL AFTER STARTING APU AND SELECTING APU BLEED, ODOR WAS IMMEDIATELY DETECTED IN THE COCKPIT ONLY AGAIN. ODOR IN BO
- [SDR YENA2021083100550](https://openairdocs.org/sdr/YENA2021083100550.md): Skin · corroded · Aug 25, 2021 · N639JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSSION LOCATED RIB 10 LOWER SURFACE TE RH WING OVERHANG, RIB14 LOWER SURFACE TE RH WINGWING OVERHANG, RIB14 +16"" LOWER SURFACE TE RH WING OVERHANG; REF AEROMAN NR 2021-339164, 2021-339165, 2021-339167 WO 2021 199/1. REF JB EC A21
- [SDR YENA2020040730277](https://openairdocs.org/sdr/YENA2020040730277.md): Light · failed · Apr 3, 2020 · N639JB · Airbus A320232 · Emergency Lighting
  > FT # 6140, EWR-JFK. AS PER TC A320-25-62-44-400-007 OPERATIONAL TEST OF EMERGENCY LTS FAILED ( EPSU EXT LOAD EMERG L); R & R LH AFT EMERGENCY LIGHT ASSY IAW AMM 33-51-00 OPS TEST OK
- [SDR YENA202001100009](https://openairdocs.org/sdr/YENA202001100009.md): Lens · defective · Jan 6, 2020 · N639JB · Airbus A320232 · Emergency Lighting
  > FT # 319, FLL-SLC. EMERGENCY EXIT LIGHT/LENS INOP AT SEAT 1C; REMOVED & REPLACED EMERGENCY LIGHT LENS AS REQUIRED. MX-4 UPDATED. PLACARD REMOVED. MDDR CLOSED.
- [SDR YENA201909210539](https://openairdocs.org/sdr/YENA201909210539.md): Wire Harness · broken · Sep 21, 2019 · N639JB · Airbus A320232 · Light System Wiring
  > FLT 2989, JFK-MCO. SEAT ROW 17C EMERGENCY LIGHT INOP; FOUND HARNESS FROM SEAT TO WALL BROKEN. R & R HARNESS & OPS NORMAL IAW AMM 33-51-18.
- [SDR YENA201905150273](https://openairdocs.org/sdr/YENA201905150273.md): Actuator · failed · May 15, 2019 · N639JB · Airbus A320232 · Compressor Bleed Valve
  > FLT 1479, DCA-FLL. DIVERTED TO IAD. AT 1500 FT APPROX WE HEARD A VERY LOUD BANG GOT AN INDICATION OF AN ENGINE STALL AND A/C SLOWED. WE DECLARED AN EMERGENCY AND LANDED AT IAD 800 LBS OVERWEIGHT; PREFORM TSM FOR ENG STALL. R & R VSV ACT. OVERWEIGHT LANDING INS
- [SDR YENA201903250160](https://openairdocs.org/sdr/YENA201903250160.md): Unknown · odor · Mar 25, 2019 · N639JB · Airbus A320232 · Air Distribution System
  > FLT 131, MCO-LAX. DIRTY SOCK ODOR DURING TAKEOFF AND LANDING WAS NOTIFIED BY IN-FLIGHT AFTER LANDING ( PACKS - BOTH); REACTIVATED AND PERFORMED OPS CK OF PACK 1 AND 2. ALL NORMAL. MDDR CLEARED. MX 4 UPDATED. PLACARD REMOVED.
- [SDR YENA201903160138](https://openairdocs.org/sdr/YENA201903160138.md): Terminal · disconnected · Mar 16, 2019 · N639JB · Airbus A320232 · Emergency Lighting
  > FLT 27, EWR-MCO. EMERGENCY LGT INSIDE ABOVE EXIT ROW INOP; T/S EMERG EXIT SIGN LT FOUND TERMINAL NOT CONNECTED. RECONNECTED TERMINAL. OPS CHECK NORMAL. OK FOR SVC.
- [SDR YENA2019021510066](https://openairdocs.org/sdr/YENA2019021510066.md): Actuator · failed · Feb 11, 2019 · N639JB · Airbus A320232 · Engine Thrust Reverser
  > FT # 975, AIRCRAFT HAD A MUSTY ODOR AFTER #1 ENG START. NO ISSUES DURING EXT AIR START AND ONE ENTIRE TAXI WITH WITH #2 ENGINE. SMELL WAS WORSE ON DESCENT. PILOTS AND FLT ATT NOTICED; PERFORMED INSPECTION OF #1 ENG DUE TO SMELL PERFORMED BORO REF LOG PAGE 254
- [SDR YENA201902100065](https://openairdocs.org/sdr/YENA201902100065.md): Unknown · odor · Feb 10, 2019 · N639JB · Airbus A320232 · Air Distribution System
  > FLT 7, FLL-LAS. F1 FA INFORMED FLT CREW AT GATE THAT DIRTY SOCK SMELL WAS QUITE STRONG ON DESCENT BELOW FL180 SEAT ROW 24 AND AFT; C/W INFO NOTED 2017-T015D SECTION A. AIRCRAFT IS OK FOR SERVICE.
- [SDR YENA201902100064](https://openairdocs.org/sdr/YENA201902100064.md): Ecs · contaminated · Feb 10, 2019 · N639JB · Airbus A320232 · Air Distribution System
  > FLT 8, LAS-FLL. VERY OUT-LEASH ODOR FROM 14,000 FT TO GATE ON DESCENT. CABIN ODOR FILED OUT. ODOR WAS VERY STRONG AT 14,000 FT. SMELLED LIKE CHEMICALS AT 8000. IT SMELL LIKE DIRTY SOCKS; COMPLIED WITH INFORMATION NOTICE 2017-T015D SECTION TABLE 1. AIRCRAFT IS
- [SDR YENA201901310051](https://openairdocs.org/sdr/YENA201901310051.md): Apu · odor · Jan 31, 2019 · N639JB · Airbus A320232 · APU Core Engine
  > FT 855, JFK-PLS. LIGHT DIRTY SOCK SMELL ON DESCENT OUT OF 10000 FT, SMELL SEEMED TO DISSIPATE BY 8000 FT. SMELL CAME BACK ONCE APU BLEED WAS TURNED ON. MULTIPLE COMPLAINTS FROM CABIN CREW THROUGHOUT THE ENTIRE CABIN SMELL WASN'T AS STRONG IN THE COCKPIT AS IT
- [SDR YENA201709190775](https://openairdocs.org/sdr/YENA201709190775.md): Coffeemaker · failed · Sep 19, 2017 · N639JB · Airbus A320232 · Buffet/Galleys
  > FUMES DETECTED IN CABIN DURING CRUISE WITH MINOR MOUNTAIN WAVE PRESENT THE ODOR WAS DESCRIBED AS ACRYLIC. NO FUMES DETECTED IN COCKPIT AFTER TEN MINUTES. IFE AND COFFEE POTS WERE DEACTIVATED. ODOR WAS NO LONGER PRESENT. PERFORMED ALL MAINTENANC
- [SDR YENA201708170674](https://openairdocs.org/sdr/YENA201708170674.md): Proximity Switch · out of adjust · Aug 17, 2017 · N639JB · Airbus A320232 · Escape Slide
  > R2 DOOR SLIDE DOES NOT INDICATE ARMED WHEN PRESSURIZED. PERFORMED TSM 52-13-00-810-805-A AND ADJUST PROXIMITY SWITCH 7WN2 IAW AMM 52-71-00-820-002-A, OK. PERFORMED OPERATIONAL TEST TO MEASURE STRUCTURE LEAKAGE IAW AMM 05-53-00-780-003-A01. R2 DOOR SLIDE SHOW
- [SDR YENA201708170673](https://openairdocs.org/sdr/YENA201708170673.md): Floor Support · corroded · Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT -Y1292 BETWEEN FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND SRM 51-42-11.
- [SDR YENA201708170672](https://openairdocs.org/sdr/YENA201708170672.md): Floor Support · corroded · Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > CORROSION WAS DISCOVERED ON FLOOR SUPPORT + Y1292 BETWEEN FRAMES 66 AND 68. R & R THE FLOOR SUPORT IAW SRM 51-72-11.
- [SDR YENA201708170671](https://openairdocs.org/sdr/YENA201708170671.md): Splice · corroded · Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > CORROSION WAS DISCOVERED ON THE SPLICE LOCATED BETWEEN FRAMES 68 - 69, -Y 1162.5. R & R THE SPLICE IAW SRM 51-42-11.
- [SDR YENA201708170670](https://openairdocs.org/sdr/YENA201708170670.md): Floor Support · corroded · Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT +Y 1292 AT FWD GALLEY AREA BETWEEN FRAMES 12 - 24. R & R THE FLOOR SUPPORT IAW SRM 51-42-11.
- [SDR YENA201708170669](https://openairdocs.org/sdr/YENA201708170669.md): Dummy Rail · corroded · Aug 17, 2017 · N639JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE DUMMY RAIL Y 503.2, AT FWD GALLEY AREA BETWEEN FRAMES 12 - 16. R & R THE DUMMY RAIL IAW SRM 51-42-11, AND 51-72-11.
- [SDR YENA201707190591](https://openairdocs.org/sdr/YENA201707190591.md): Servo · failed · Jul 19, 2017 · N639JB · Airbus A320232 · Elevator Control System
  > FLT 36, RETURN TO FIELD. CLIMBING OUT OF FL 180, FELT INCREASING VIBRATIONS FROM THE REAR OF THE PLANE. THE INFLIGHT CREW CONFIRMED MAJOR VIBRATIONS MORE APPARENT AT THE REAR, COMING FROM THE FLOOR OR BENEATH THE FLOOR. WE STOPPED CLIMB FL 220 & SLOWED TO 220
- [SDR YENA201704060248](https://openairdocs.org/sdr/YENA201704060248.md): Battery Pack · failed · Apr 6, 2017 · N639JB · Airbus A320232 · Emergency Lighting
  > DURING PRE DEPARTURE CHECKLIST, FOUND EMERGENCY LIGHTS INOPERATIVE AT OVERWING EXIT ROW SEATS. REMOVED & REPLACED ESPU & BATTERY AT 13WL.
- [SDR YENA201704060247](https://openairdocs.org/sdr/YENA201704060247.md): Power Supply · failed · Apr 6, 2017 · N639JB · Airbus A320232 · Emergency Lighting
  > PRE DEPARTURE CHECKLIST FOUND EMERGENCY LIGHTS INOPERATIVE AT THE OVERWING EXIT ROWS, & SEATS. REMOVED & REPLACED THE ESPU & BATTERY AT 13WL & 12WL.
- [SDR YENA20160830773](https://openairdocs.org/sdr/YENA20160830773.md): Fdu · failed · Aug 30, 2016 · N639JB · Airbus A320232 · Fire Detection
  > FLIGHT CREW REPORTED ENGINE 2 FIRE LOOP-A INTERMITTENT DURING FLIGHT, ENGINE FIRE DETECTION SYSTEMS. R & R FDU2 IAW AMM 26-12-34. PERFORMED OPS CHECK. OPS CHECKED NORMAL.
- [SDR YENA20160612550](https://openairdocs.org/sdr/YENA20160612550.md): Switch · failed · Jun 12, 2016 · N639JB · Airbus A320232 · Emergency Lighting
  > PILOT NOTICED EMERGENCY LIGHTS DID NOT TURN OFF WITH SWITCH IN ARM POSITION. REPLACED EMERGENCY LIGHT, COCKPIT SWITCH IAW AMM 33-51-00. OPS CHECK PERFORMED AND PASSED.
- [SDR YENA20160326267](https://openairdocs.org/sdr/YENA20160326267.md): Seat Track · corroded · Mar 26, 2016 · N639JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN, LT SEAT TRACK Y1292 CORRODED ON 2 SPOTS, FWD OF FRAME 68. SEAT TRACK R & R IAW SRM 51-72-11.
- [SDR YENA20140609107](https://openairdocs.org/sdr/YENA20140609107.md): Battery Pack · no test · Jun 9, 2014 · N639JB · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE, EPSU BATTERY FAILED SYS TEST. R & R BATTERY IAW AMM 33-51-38-020-051A. OPS CHECKED GOOD.
- [SDR YENA20130817177](https://openairdocs.org/sdr/YENA20130817177.md): Computer · failed · Aug 17, 2013 · N639JB · Airbus A320232 · Flight Control System
  > AIR RETURN TO DEPARTURE CAPT LEG, AFTER ROTATION NOTICED NEEDED FWD PRESSURE ON STICK TO KEEP ACFT FROM PITCHING UP. AT 1,000' ACCELERATED AND CLEANED UP ON SCHED. CONTINUED TO CLIMB, STILL HAD TO HOLD FWD PRESSURE ON STICK TO STOP ACFT FROM FURTHER PITCHING
- [SDR YENA20111221401](https://openairdocs.org/sdr/YENA20111221401.md): Mechanism · out of adjust · Dec 21, 2011 · N639JB · Airbus A320232 · Passenger/Crew Doors
  > FLT 616 JAX-JFK, CREW REPORTED AFT L2 DOOR AROUND HANDLE CREEPS OUT OF IT'S ARMED DETENT AS AIRCRAFT CLIMBS AND PRESSURIZES. ACCOMPLISHED VISUAL INSPECTION AND FOUND PEN JAMMED BETWEEN GIRT LOCKS AND GIRT BAR. REMOVED FOD AND PEN. PERFORMED OPS CHECK OF L2
- [SDR YENA200812020122](https://openairdocs.org/sdr/YENA200812020122.md): Battery · discharged · Nov 28, 2008 · N639JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED. "LEFT EPSU" ON WEEKLY CHECK. REMOVED AND REPLACED LEFT EPSU BATTERY (11W) IAW TSM 33-51-00-810-808. OPS TEST OF EMERGENCY LIGHT SYS OK.

## 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 = 'N639JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N639JB/reports

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