# Service difficulty reports: N657JB

A list on [N657JB](https://openairdocs.org/aircraft/N657JB.md).

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

- [SDR YENA2026092500906](https://openairdocs.org/sdr/YENA2026092500906.md): Unknown · odor · Sep 25, 2026 · N657JB · Airbus A320232 · Air Distribution System
  > FLT 1923, DCA-MCO, DURING FINAL DESCENT ON APPROACH DIRTY SOCK ODOR, STRONG IN COCKPIT, TURNED PACK 1 OFF AND ODOR SEEMED TO GO AWAY.
- [SDR YENA2026092500905](https://openairdocs.org/sdr/YENA2026092500905.md): Check Valve · failed · Sep 24, 2026 · N657JB · Airbus A320232 · Hydraulic System, Main
  > FLT 1077, MCO-PUJ, RETURN TO FIELD. Y HYD RSVR OVHT. ECAM AFTER T/O. Y HYD ENG2 PUMP LOW PRESSURE, FOLLOWING QRH / ECAM BELOW 10,000 OVHT CLEARED. T/S IAW TSM 29-13-00-810-802-A. FOUND UNUSUAL NOISE WHEN E-PUMP OPERATED. REMOVED CHK VALVE 3083GM, FOUND CHK
- [SDR YENA2025122201246](https://openairdocs.org/sdr/YENA2025122201246.md): Unknown · vibration · Dec 20, 2025 · N657JB · Airbus A320232 · Fuselage Structure (General)
  > FLT#147, EWR-SJU. "DURING CRUISE #1 FA CALLED STATING LOUD HUMMING NOISE AND VIBRATION IN CABIN FLOOR NEAR ROW 13. CA INVESTIGATED AS WELL. NO OTHER INDICATIONS ON SYSTEMS. PAGE POSSIBLE LOOSE PANEL OR FAIRING SEAL" (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2025061000577](https://openairdocs.org/sdr/YENA2025061000577.md): A/C Pack · odor · Jun 9, 2025 · N657JB · Airbus A320232 · Cabin Cooling System
  > FLT#1248, TPA-LGA. ' OIL SMELL 15 SECONDS AT 12000 FT. DID ODOR RECOGNITION CHECKLIST. ODOR WENT AWAY AFTER WE ISOLATED THE PACK; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A. ISOLATED FAULT TO TYPE 10 AMBIENT AIR PER TSM 05-50-00-810-831-A. A/C IS OK
- [SDR YENA2025042300423](https://openairdocs.org/sdr/YENA2025042300423.md): Ecs · contaminated · Apr 22, 2025 · N657JB · Airbus A320232 · Air Conditioning System
  > FLT#637, BDL-MCO. 'CABIN AIR QUALITY EVENT ON APPROACH INTO ORLANDO FLIGHT ATTENDANTS IN THE AFT CABIN COULD SMELL FUEL/OIL SMELL VERY STRONG. ONE FLIGHT ATTENDANT REPORTS AND HEADACHE STARTED AROUND 2000 FULL CONFIGURATION FOR LANDING FLAPS FULL GEAR DOWN; C
- [SDR YENA2025042300417](https://openairdocs.org/sdr/YENA2025042300417.md): Unknown · odor · Apr 20, 2025 · N657JB · Airbus A320232 · Air Distribution System
  > FLT#495, BOS-PUJ, 'FLT ATTENDANTS REPORT SMELLING FUEL OR OIL DURING DURING FLT AROUND ROW 14; C/W INFO NOTICE 2017-T015J & TSM 05-50-00-810-831-A, ECS DECONTAMINATION C/W, NO ODOR PRESENT, A/C OK FOR SERVICE, MCC BOB.'
- [SDR YENA2024042300659](https://openairdocs.org/sdr/YENA2024042300659.md): Sign · inoperative · Apr 21, 2024 · N657JB · Airbus A320232 · Emergency Lighting
  > FLT#380, MBJ-JFK. 'EMR EXIT SIGN AIRCRAFT LEFT NOT ILLUMINATED; REF L/P'S 4010079 (UPON REMOVAL OF ROW #10 & #11 DATO PANEL (LOWER) & UPPER SIDEWALL PANEL FOUND GROUNDING WIRE DISCONNECTED FROM TERMINAL BLOCK 6811WN (REF AWM 33-51-03). RECONNECTED GROUND WIRE
- [SDR YENA2023081500940](https://openairdocs.org/sdr/YENA2023081500940.md): Unknown · unknown · Aug 14, 2023 · N657JB · Airbus A320232 · Emergency Lighting
  > FLT#2583, JFK-MCO. 'OVERWING EMER LIGHT RIGHT SIDE (MID CABIN) INOP; FOUND LOOSE GROUND AT 6531VN, TIGHTENED & OPS CHECK GOOD IAW AMM 33-51-00.'
- [SDR YENA2023081500939](https://openairdocs.org/sdr/YENA2023081500939.md): Unknown · unknown · Aug 14, 2023 · N657JB · Airbus A320232 · Exterior Lighting
  > FLT#2392, MIA-JFK. 'NOSE LANDING LIGHT INOP ( TAXI AND TAKEOFF LIGHT SYSTEMS) (TAKEOFF LIGHT FOUND TO BE INOP); RELAMPED T/O LIGHT IAW AMM 33-46-11. MX-4 UPDATED PLACARD REMOVED. MCC NOTIFIED.'
- [SDR YENA2023080800927](https://openairdocs.org/sdr/YENA2023080800927.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE: CORROSION FRAME 32 SHEAR TIE BTW STR43R AND STR44 IN FWD CARGO COMPARTMENT REF AEROMSAN WO1222982-NR2023-403471; (RESOLVED ON W/O: 1222982 TASKCARD: NR-00014) REMOVED AND REPLACED SHEAR TIE LOC. FR 34 BTW STR 41R AND STR 42R IN FWD C
- [SDR YENA2023080800926](https://openairdocs.org/sdr/YENA2023080800926.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION FRAME 34 SHEAR TIE BTW STR 43R AND STR 44 IN FWD CARGO COMPARTMENT;(RESOLVED ON W/O: 1222982 TASKCARD: NR-00015) REF WO 1222982 NR2023-403476 -: REMOVED AND REPLACED SHEAR TIE LOC. FR 32 BTW STR 43R AND STR 44 IN FWD CARGO
- [SDR YENA2023080800925](https://openairdocs.org/sdr/YENA2023080800925.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION FRAME 34 SHEAR TIE BTW STR 42R AND STR 43R IN FWD CARGO COMPARTMENT; REF AEROAN WO1222982 NR2023-403475 REMOVED AND REPLACED SHEAR TIE LOC. FR 34 BTW STR 42R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11, SRM 51-72-11, AND
- [SDR YENA2023080800924](https://openairdocs.org/sdr/YENA2023080800924.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION FRAME34 SHEAR TIE BTW STR41R AND STR42R IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE LOC. FR34 BTW STR 41R AND STR 42R IN FWD C.C IAW A320 SRM 51-72-11 AND DWG D53231375.
- [SDR YENA2023080800923](https://openairdocs.org/sdr/YENA2023080800923.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION FRAME 34 SHEAR TIE BTW STR 43R & STR 44 IN FED CARGO COMPARTMENT; REMOVED AND REPLACED SHEAR TIE LOC FR34 BTW STR 43RSTR44 INFWD CARGO COMPARTMENT IAW A320- SRM 51-42-11 & 51-71-11 DWG D53231375.
- [SDR YENA2023080800922](https://openairdocs.org/sdr/YENA2023080800922.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION BELLY FAIRING KEEL BEAM STRUCTURE LOCATED AT LEVEL STR 42L AN D BTW FR.35 AND FR 36 AT LOWER FUSELAGE; ACCOMPLISHED REPAIR OF CORROSION AFFECTING STRINGER 42L AT THE KEEL BEAM BOX STRUCTURE AREA BETWEEN FR35 TO FR36 IN ACCOR
- [SDR YENA2023080800921](https://openairdocs.org/sdr/YENA2023080800921.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION FRAME 34 SHEAR TIE BTW STR 41R AND STR 42R IN FWD CARGO COMPARTMENT ( CPCP RELATED REFER TO MPD TASK 532180-01); REF AEROMAN N/R 2023-403474, R&R SHEAR TIE LOC FR 34 BTW STR 41R AND 42R IN FWD CARGO COMPARTMENT IAW A320 SRM
- [SDR YENA2023080800920](https://openairdocs.org/sdr/YENA2023080800920.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Wing Structure
  > DURING HEAVY MAINTENANCE: DEBONDED UPPER EXTERNAL SKIN I/B FLAP LOCATED AT 6.5 INCHES FROM INBOARD EDGE ON R/H WING; REF AEROMAN N/R 2023- 403383, REPAIRED UPPER SKIN I/B FLAP ON RH WING IAW EC# A23-652-01, EA# 57-0258-23, REV O, AND EA # 57-0258-23 PART 1. MA
- [SDR YENA2023080800919](https://openairdocs.org/sdr/YENA2023080800919.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION FRAME 32 SHEAR TIE BTW STR43R AND STR44 IN FWD CARGO COMPARTMENT REF AEROMSAN WO1222982-NR2023-403471; REMOVED AND REPLACED SHEAR TIE LOC. FR 34 BTW STR 41R AND STR 42R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11, SRM 51-
- [SDR YENA2023080800918](https://openairdocs.org/sdr/YENA2023080800918.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Wing Structure
  > DURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG RIB 18 TO RIB 19 ON RH WING; REF AEROMAN WO2023 132/1 NR2023-403107 -- REF JB NR 00013 FOR THE FUR CREATION.--REMOVED CORROSION LOCATED RIB 18 PLUS 15.163 INCHES TRAILING EDGE T
- [SDR YENA2023080800917](https://openairdocs.org/sdr/YENA2023080800917.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION BELLY FAIRING KEE BEAM STRUCTURE LOCATED AT LEVEL STR 42L AN D BTW FR.35 AND FR 36 AT LOWER FUSELAGE; REF AEROMAN WO 2023 132/1 NR 2023-403355 -- ACCOMPLISHED REPAIR OF CORROSION AFFECTING STRINGER 42L AT THE KEEL BEAM BOX S
- [SDR YENA2023080800916](https://openairdocs.org/sdr/YENA2023080800916.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Structure (General)
  > DURING HEAVY MAINTENANCE: CORROSION FRAME 34 SHEAR TIE BTW STR 43R & STR 44 IN FWD CARGO COMPARTMENT; REF AEROMAN WO 2023-132/1 NR 2023-403476 - REMOVED AND REPLACED SHEAR TIE LOC. FR34 BTW STR 43R AND 44 IN FWD CARGO COMPARTMENT IAW WITH A320 SRM 51-42-11, SR
- [SDR YENA2023080800915](https://openairdocs.org/sdr/YENA2023080800915.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: REF AEROMAN WO1222982 NR2023-403475 -- CORROSION FRAME 34 SHEAR TIE BTW STR 42R AND STR 43R IN FWD CARGO COMP ARTMENT; REMOVED AND REPLACED SHEAR TIE LOC. FR 34 BTW STR 42R IN FWD CARGO COMPARTMENT IAW A320 SRM 51-42-11, SRM 51-72-11,
- [SDR YENA2023080800914](https://openairdocs.org/sdr/YENA2023080800914.md): Unknown · unknown · Aug 5, 2023 · N657JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CORROSION FRAME34 SHEAR TIE BTW STR41R AND STR42R IN FWD CARGO COMPARTMENT; REF AEM WO 2023-132-1, NR 2023-403474 REMOVED AND REPLACED SHEAR TIE LOC. FR34 BTW STR 41R AND STR 42R IN FWD C.C IAW A320 SRM 51-72-11 AND DWG D53231375. (
- [SDR YENA2023060500576](https://openairdocs.org/sdr/YENA2023060500576.md): Unknown · unknown · Jun 1, 2023 · N657JB · Airbus A320232 · Engine Indicating System
  > FLT#1219, JFK-ATL. (AIRCRAFT PERFORMED ANA IR TURN BACK AND DECLARED AN EMERGENCY) ' PASSING 10,000FT ENG 1 STALL AND OVERTEMP FELT LOUD BANG AND YAW; REF WO # 1258201 FOR REMOVAL AND REPLACEMENT OF ENG # 1.
- [SDR YENA2023011300036](https://openairdocs.org/sdr/YENA2023011300036.md): Controller · failed · Jan 10, 2023 · N657JB · Airbus A320232 · Cabin Pressure Controller
  > FLT#1476, SJU- STT. (AIRCRAFT PERFORMED AN AIR TURN BACK TO SJU) ' AFTER DEPARTURE IN CLIMB THRU ABOUT 3000' CAB PR SYSTEM 1 FAULT. AT ABOUT 7000' MASTER WARNING CAB PR EXCESS CAB ALT; REMOVED AND REPLACED CPC #1 FIN #11HL IAW AMM 21-31-34. OPS CHECK OK.'
- [SDR YENA2022012800032](https://openairdocs.org/sdr/YENA2022012800032.md): None · none · Jan 27, 2022 · N657JB · Airbus A320232 · Doors
  > FLT # 172, FLL-LGA (AIR TURNBACK TO FLL). R1 DOOR LOUD HUMMING NOISE AND VIBRATION ABOVE FL100 AND VERY BAD ABOVE FL250 - FLOOR VIBRATING, SMOOTH LANDING, NORMAL @ LANDING NOT OVERWEIGHT; INSPECTED R1 DOOR IAW AMM 52-11-00. CONDITION OF DOOR SEALS AND DOOR OP
- [SDR YENA2020072700402](https://openairdocs.org/sdr/YENA2020072700402.md): Battery · failed · Jul 22, 2020 · N657JB · Airbus A320232 · Emergency Lighting
  > FLT 6250,REF TASK CARD 335100-03-1 (BATTERY CAPACITY); R & R FWD ESPU BATTERY PER AMM 33-51-00. OPS CHK.
- [SDR YENA2020072700401](https://openairdocs.org/sdr/YENA2020072700401.md): Battery · failed · Jul 22, 2020 · N657JB · Airbus A320232 · Emergency Lighting
  > FT # 6250, MZJ-JFK. REF TASK CARD 335100-03-01 (BATTERY CAPACITY CH); R & R AFT ESPU BATTERY PER AMM 33-51-00. OPS CHK OK
- [SDR YENA2020072700400](https://openairdocs.org/sdr/YENA2020072700400.md): Power Supply · failed · Jul 21, 2020 · N657JB · Airbus A320232 · Emergency Lighting
  > FLT 6250, AFTER REPLACEMENT OF L2 DOOR SLIDE EMERGENCY LIGHT, OPERATIONAL CHECK FAILED. R & R LT & RT ESPU BATTERIES IAW AMM 33-51-00. OPS TESTED OK. R & R R ESPU IAW AMM 33-51-11. OPS CHECKED OK.
- [SDR YENA2020072700399](https://openairdocs.org/sdr/YENA2020072700399.md): Battery · failed · Jul 21, 2020 · N657JB · Airbus A320232 · Emergency Lighting
  > FLT 6250, AFTER REPLACEMENT OF L2 DOOR SLIDE EMERGENCY LIGHT, OPERATIONAL CHECK FAILED. R & R L & R ESPU BATTERIES IAW AMM 33-51-00. OPS TEST OK. R & R R ESPU IAW AMM 33-51-11. OPS CHECKED OK.
- [SDR YENA2020072700398](https://openairdocs.org/sdr/YENA2020072700398.md): Battery · failed · Jul 21, 2020 · N657JB · Airbus A320232 · Emergency Lighting
  > FLT 6250, AFTER REPLACEMENT OF L2 DOOR SLIDE EMERGENCY LIGHT, OPERATIONAL CHECK FAILED. R & R THE LT & RT ESPU BATTERIES IAW AMM 33-51-00. OPS TEST OK. R & R R ESPU IAW AMM 33-51-11. OPS CHECKED OK.
- [SDR YENA201902280108](https://openairdocs.org/sdr/YENA201902280108.md): Battery Pack · failed · Feb 28, 2019 · N657JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, (REF: NR# 440562-34367) EMERGENCY LIGHTS TEST FAILS, FWD LT BATTERY PACK AND FT LT BATTERY PACK; REMOVED TWO BATTERY PACKS, 10WL AND 13WL IAW AMM 33-51-38-000-002-A. REPLACED TWO BATTERY PACKS 10WL AND 13WL IAW AMM 33-51-38-400-002-A.
- [SDR YENA201902280107](https://openairdocs.org/sdr/YENA201902280107.md): Battery Pack · failed · Feb 28, 2019 · N657JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE, (REF: NR# 440562-34367) EMERGENCY LIGHTS TEST FAILS, FWD LT BATTERY PACK AND FT LT BATTERY PACK; REMOVED TWO BATTERY PACKS, 10WL AND 13WL IAW AMM 33-51-38-000-002-A. REPLACED TWO BATTERY PACKS 10WL AND 13WL IAW AMM 33-51-38-400-002-A.
- [SDR YENA201706260541](https://openairdocs.org/sdr/YENA201706260541.md): Shear Tie · corroded · Jun 26, 2017 · N657JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENNANCE, CORROSION WAS DISCOVERED ON THE SHEAR TIE FRAME 33 BETWEEN 43R AND 43L. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DRAWING D53232617.
- [SDR YENA201706260540](https://openairdocs.org/sdr/YENA201706260540.md): Shear Tie · corroded · Jun 26, 2017 · N657JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENNANCE, CORROSION WAS DISCOVERED ON SHEAR TIE FR30 BTW STRINGERS 42 & 43R. REPLACED THE SHEAR TIE IAW SRM 51-72-11, AND DWGS D53232589, D5322318.
- [SDR YENA201706260539](https://openairdocs.org/sdr/YENA201706260539.md): Shear Tie · corroded · Jun 26, 2017 · N657JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENNANCE, CORROSION WAS DISCOVERED ON SHEAR TIE FRAME 28 BETWEEN STRINGERS 43L TO 43R. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D 53232977.
- [SDR YENA201706260538](https://openairdocs.org/sdr/YENA201706260538.md): Floor Support · corroded · Jun 26, 2017 · N657JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENNANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT Y+919, FRAMES 65 AND 67. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472812.
- [SDR YENA201706260537](https://openairdocs.org/sdr/YENA201706260537.md): Seat Track · corroded · Jun 26, 2017 · N657JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENNANCE, CORROSION WAS DISCOVERED ON THE SEAT TRACK, FRAMES 64 TO 66. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING D53472231.
- [SDR YENA201706260536](https://openairdocs.org/sdr/YENA201706260536.md): Door Sill · corroded · Jun 26, 2017 · N657JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENNANCE, CORROSION WAS DISCOVERED ON LOWER DOOR SILL FRAME 66 AT STRINGER 23L AFT GALLEY AREA. REPLACED LWR DOOR SILL IAW SRM 51-72-11 AND DRAWING D53480505.
- [SDR YENA20160806681](https://openairdocs.org/sdr/YENA20160806681.md): Trim System · out of rig · Aug 6, 2016 · N657JB · Airbus A320232 · Rudder Tab Control System
  > FT 1091, AIR RETURN BACK. DURING CLIMBOUT AND CRUISE ACFT REQUIRED 2.7 DEGREES LEFT RUDDER TRIM IN ORDER TO FLY STRAIGHT. CREW REPORTED THIS GETTING WORSE WITH THE CLIMB WITH OR WITHOUT A/P ON OR OFF. PERFORMED RIGGING AND TESTS OF THE RUDDER TRIM ACTUATO
- [SDR YENA20160802679](https://openairdocs.org/sdr/YENA20160802679.md): Bleed Valve · failed · Aug 2, 2016 · N657JB · Airbus A320232 · Compressor Bleed Valve
  > AIR TURN BACK. CREW REPORTED RECEIVING THE FOLLOWING ECAM MESSAGE, ENGINE 1 EGT OVERLIMIT, DURING TAKEOFF CLIMB, EGT WAS AT APPROXIMATELY 660 DEGREES FOR 2 MINUTES. FOUND FAULTY 10TH STAGE BLEED VALVE. R & R 10TH STAGE BLEED VALVE AND 10TH STAGE HPC SOLENOID
- [SDR YENA20160802678](https://openairdocs.org/sdr/YENA20160802678.md): Solenoid Valve · failed · Aug 2, 2016 · N657JB · Airbus A320232 · Compressor Bleed Valve
  > AIR TURN BACK. CREW REPORTED RECEIVING THE FOLLOWING ECAM MESSAGE, ENGINE 1 EGT OVERLIMIT, DURING TAKEOFF CLIMB. EGT WAS AT APPROXIMATELY 660 DEGREES FOR 2 MINUTES. FOUND FAULTY 10TH STAGE BLEED VALVE. R & R 10TH STAGE BLEED VALVE AND 10TH STAGE HPC SOLENOI
- [SDR YENA20160323252](https://openairdocs.org/sdr/YENA20160323252.md): Battery Pack · failed · Mar 23, 2016 · N657JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT FAILS TEST. R & R EMERGENCY LIGHT BATTERY AT EPSU 10 WL LIGHT CKS GOOD IAW AMM 33-51-00.
- [SDR YENA20120925609](https://openairdocs.org/sdr/YENA20120925609.md): Ground Wire · damaged · Sep 25, 2012 · N657JB · Airbus A320232 · Light System Wiring
  > FLT 75 JFK-TPA, ON GROUND MAINTENANCE CHECK FOUND CEILING EMERGENCY LIGHT AT ROW 23 INOP. REPAIRED GROUNDING WIRE TO DC 1 IAW ESPM 20-53-21. OPS CHECK GOOD.
- [SDR YENA20120925608](https://openairdocs.org/sdr/YENA20120925608.md): Wire · damaged · Sep 25, 2012 · N657JB · Airbus A320232 · Light System Wiring
  > FLT 75 JFK-TPA, ON GROUND MAINTENANCE CHECK FOUND EMERGENCY LIGHT 361WL2 LAV D INOP. REPAIRED POWER WIRE SUPPLY SPLICE CONNECTION IAW ESPM 20-43-13. OPS CHECK GOOD.
- [SDR YENA20110705289](https://openairdocs.org/sdr/YENA20110705289.md): Epsu · failed · Jul 5, 2011 · N657JB · Airbus A320232 · Emergency Lighting
  > FLT 6403 MCO-TPA, ON GROUND MAINTENANCE CHECK FOUND BOTH LT/RT WING EXIT LIGHTS INOP. THE TECHNICIAN REMOVED AND REPLACED EPSU 12WL IAW AMM 33-51-38. OPS CHECK GOOD.

## 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 = 'N657JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N657JB/reports

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