# Service difficulty reports: N712JB

A list on [N712JB](https://openairdocs.org/aircraft/N712JB.md).

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

- [SDR YENA2026032500340](https://openairdocs.org/sdr/YENA2026032500340.md): Unknown · odor · Mar 23, 2026 · N712JB · Airbus A320232 · Air Distribution System
  > FLT # 727 FLL-FLL. BURNING SMELL IN FLT DECK AND FWD GALLEY. FYI JUST PRIOR TO SMELL, THE PUSHBACK TUG HAD A BRAKE FAILURE WITH SMOKE.; COMPLIED WITH INFORMATION NOTICE 2017-T015 STEP 1. ISOLATED FAULT TO BE TYPE 10 PUSHBACK TUG BRAKE FAILURE WITH SMOKE. ACCOM
- [SDR YENA2025081200823](https://openairdocs.org/sdr/YENA2025081200823.md): Ecs · odor · Aug 11, 2025 · N712JB · Airbus A320232 · Cabin Cooling System
  > FLT#1691, JFK-LIR. INFLIGHT REPORTED DIRTYSOCK SMELL AS AIRCRAFT DESCENDED BELOW 10000 ( PACKS); COMPLIED WITH INFORMATION NOTICE 2017-T015L, SECTION B1. DECONTAMINATION LEVEL A WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. NO FURTHER ODOR WHEN OPERATING BOT
- [SDR YENA2025080800820](https://openairdocs.org/sdr/YENA2025080800820.md): A/C Pack · odor · Aug 7, 2025 · N712JB · Airbus A320232 · Cabin Cooling System
  > FLT#2251, BOS-MCO. AFT FA'S REPORTING A STRONG DIRTY SOCK SMELL ON LANDING APU NOT RUNNING. IN COCKPIT A PAINT SMELL WAS NOTICED ON DESENT LANDING; COMPLIED WITH INFO NOTICE 2017-T015. IDENTIFIED ODOR AT PACK 1. INSPECTED APU & APU BLEED DUCT FOR OIL CONTAMINA
- [SDR YENA2024112601507](https://openairdocs.org/sdr/YENA2024112601507.md): Floor Support · corroded · Nov 23, 2024 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: AT R2 DOOR FR68 STA3257 1967, LONGITUDE FLOOR BEAM HAS CORROSION AROUND FASTENER HOLES; (RESOLVED ON W/O: 1314960 TASKCARD: NR-00002) REF HAECO-GSO SO 169002 NR 44343. REMOVED CORROSION IAW A320 SRM 51-74-00. REPAIRED DAMAGE AERA IAW
- [SDR YENA2024112601506](https://openairdocs.org/sdr/YENA2024112601506.md): Tie Down · corroded · Nov 23, 2024 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: AFT CARGO FR52+10 HAS CORROSION AT THE TIE DOWN MOUNT; (RESOLVED ON W/O: 1314960 TASKCARD: NR-00020) REF HAECO-GSO 169002 NR 44563. REPAIRED DAMAGE ON FR52A INNER FLANGE AT STR 39 RH IAW HAECO REO-G25255. WORK ACCOMPLISHED 5133 QC450.
- [SDR YENA2024112601505](https://openairdocs.org/sdr/YENA2024112601505.md): Gusset · cracked · Nov 23, 2024 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: FR 68 STR 10LH 1 EACH GUSSET HOLE HAS NDT INDICATION; "REF HAECO-GSO SO 169002 NR 44394. REMOVED GUSSET AT FRAME 68 STR 10LH IAW A320 SRM 51-42-11. REPAIRED FRAME IAW A320 SRM 53-41-12-300-018. INSTALLED NEW GUSSET P/N D5348002075802
- [SDR YENA2024112601504](https://openairdocs.org/sdr/YENA2024112601504.md): Gusset · cracked · Nov 23, 2024 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: FR 66 STR 10LH 1 EACH GUSSET HOLE HAS NDT INDICATION; "REF HAECO-GSO SO 169002 NR 44389. REMOVED GUSSET AT FRAME 66 STR 10LH IAW A320 SRM 51-42-11. REPAIRED FRAME IAW A320 SRM 53-41-12-300-018. INSTALLED NEW GUSSET P/N D5348002075802
- [SDR YENA2024112601503](https://openairdocs.org/sdr/YENA2024112601503.md): Gusset · cracked · Nov 23, 2024 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: FR 66 STR 12 LH 1 EACH GUSSET HOLE NDT INDICATION; "REF HAECO-GSO SO 169002 NR 44390. REMOVED GUSSET AT FRAME 66 STR 12L IAW A320 SRM 51-42-11. REPAIRED FRAME IAW A320 SRM 53-41-12-300-018. INSTALLED NEW GUSSET P/N D5348002075802. RE
- [SDR YENA2024112601502](https://openairdocs.org/sdr/YENA2024112601502.md): Floor Support · corroded · Nov 23, 2024 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE: UNDER MAIN CABIN FLOORBOARD, FLOORBOARD LONGITUDE SUPPORT AT FR 16 TO FRAME 21-1292 STA 7599 HAS CORROSION; "REF HAECO-GSO SO 169002 NR 44295. REMOVED AND REPLACED SEAT TRACK IAW A320 SRM 51-42-11 AND AIRBUS DRAWING D53112782.THIS REP
- [SDR YENA2024070800942](https://openairdocs.org/sdr/YENA2024070800942.md): None · none · Jul 5, 2024 · N712JB · Airbus A320232 · Standard Practices/Structures
  > FLT#170, FLL-BOS. 'F/A'S REPORTED BURNING RUBBER SMELL MID CABIN; ACCOMPLISHED AMM TASK 05-50-00-831-A; ODOR CLASSIFICATION IS TYPE 10 CABIN ODOR AND CENTERED AROUND ROWS 14-15 ABC/DEF.REPLACED LIGHT ASSEMBLY AT 14 ABC/DEF AS PRECAUTIONARY REF AMM 33-22-11-86
- [SDR YENA2023061600667](https://openairdocs.org/sdr/YENA2023061600667.md): Transducer · failed · Jun 13, 2023 · N712JB · Airbus A320232 · Pneumatic System
  > FLT#593, EWR-STI. (AIRCRAFT DIVERTED TO JFK) 'EPR / N1 / BLEED FLUCTUATION IN FLIGHT; REMOVED AND REPLACED PRU SENSE LINE IAW AMM 36-11-49. REMOVED AND REPLACED BLEED PRESSURE TRANSDUCER 7HAI IAW AMM 36-11-15. OPS CHECK GOOD ALL PARAMETERS NORMAL.'
- [SDR YENA2022122301292](https://openairdocs.org/sdr/YENA2022122301292.md): Apu · contaminated · Dec 26, 2022 · N712JB · Airbus A320232 · APU Core Engine
  > FLT#1433, MCO-SJU. SMELL FROM ROWS 5-20 A DIRTY SOCK & MUSTY DRY SMELL. PERFORMED CABIN ODOR INSPECTED BOTH ENGINES FOR EVIDENT OIL BLEED FOUND GOOD., CONTINUE INSPECTED APU FOUND OIL ON INTAKE. PROCEDURES TO PACK BURN BOTH AND REPLACEMENT EPA RECIRCULAT
- [SDR YENA2022112801158](https://openairdocs.org/sdr/YENA2022112801158.md): Cooling Fan · leaking · Nov 26, 2022 · N712JB · Airbus A320232 · APU Oil System
  > FLT#379, DCA-FLL. 'DIRTY SOCK SMELL REPORTED BY FLIGHT ATTENDANT; COMPLIED WITH INFO NOTICE 2017-T015-J. NO 30-DAY HISTORY. PER TSM 05-50-00-810-085-B ODOR TYPE 1 LEVEL A. FOUND THE SOURCE OF ODOR TO BE APU OIL COOLING FAN LEAKING. ACCOMPLISHED LEVEL 1 ECS DE
- [SDR YENA2022111601126](https://openairdocs.org/sdr/YENA2022111601126.md): Slide · unwanted deploy · Nov 13, 2022 · N712JB · Airbus A320232 · Escape Slide
  > FLT # 405, EWR-FLL. R1 DOOR SLIDE DEPLOYED; REMOVED & REPLACED R1 DOOR SLIDE PER AMM 25-62-44-400-803-A. CHECKS NORMAL.
- [SDR YENA2022062400620](https://openairdocs.org/sdr/YENA2022062400620.md): Cabin Air Sys · fumes · Jun 22, 2022 · N712JB · Airbus A320232 · Air Distribution Fan
  > FLT#38, SJO-FLL. 'AIRCRAFT FUMES EVENT LEVEL 1 (ONE). TAXI OUT AND DESCENT IN VISIBLE MOISTURE OUTSIDE; POST MX ON LOG PAGE 3408366 ITEMS 1 (INSPECTED APU & APU BAY AREA FOR OIL LEAKS AS PER AMM49-95-00. NO EVIDENCE OF LEAKAGE DETECTED. PERFORMED APU START AND
- [SDR YENA2022041800379](https://openairdocs.org/sdr/YENA2022041800379.md): Egt Indication · false indication · Apr 17, 2022 · N712JB · Airbus A320232 · Cylinder Head Temperature (CHT) Indicating System
  > FLT#6116, SMF-LAX. ' AFTER ENG 1 START DURING ENG 2 START ENG 2 EGT CONTINUED TO CLIMB. AFTER 750 DEC C. ENG 1 EGT ECAM 999 C ON ENG 1, THEN EGT RAPID RESET TO 170 C; PER TSM 77-00-00-810-817B, INSPECTED # 1 ENG EGT JUNCTION BOX AND HARNESS ALL GOOD. NO CLM ME
- [SDR YENA2021082700547](https://openairdocs.org/sdr/YENA2021082700547.md): Unknown · odor · Aug 24, 2021 · N712JB · Airbus A320232 · Air Distribution System
  > FLT # 1558, BOG-FLL. MILD MUSTY ODOR STARTED FROM TOP OF CRUISE LAST FOR THE ENTIRLY OF THE FLIGHT FROM COCKPIT TO ROW 5; BASED ON ODOR REPORT INPUT AND WITH MCC CONCURRANCE, EVENT IS CONSIDERED A LEVEL 1 EVENT CITING INFO NOTICE 2017-7015H, SECTION A, ISLOAT
- [SDR YENA2020021060161](https://openairdocs.org/sdr/YENA2020021060161.md): Connector · unsecure · Feb 6, 2020 · N712JB · Airbus A320232 · Light System Wiring
  > FT # 1348, SJU-DCA. ROW 18 CEILING EMERGENCY LIGHT INOP; T/S AND FOUND LOOSE CONNECTION ON EMERGENCY CEILING LIGHT, RESECURED CONNECTOR OPCK OF EMERGENCY LIGHT SYSTEM OK. REF AMM 33-51-00.
- [SDR YENA201908310496](https://openairdocs.org/sdr/YENA201908310496.md): Cap · defective · Aug 31, 2019 · N712JB · Airbus A320232 · Turbine Section
  > FLT 72, SLC-JFK. DIRTY SOCKS ODOR EVENT ON DESCENT. APPROX. 6000 FEET. PACK 1 TURNED OFF ODOR DISSIPATED. ODOR WAS COCKPIT ONLY; REMOVED AND REPLACED # 1 ENG L/P TURBINE SHAFT BLIND CAP IAW AMM 72-51-41-000-012B. OIL LEAK CK REQD PER AMM 71-00-00-710-012 IAW
- [SDR YENA201906300381](https://openairdocs.org/sdr/YENA201906300381.md): Unknown · odor · Jun 30, 2019 · N712JB · Airbus A320232 · Air Distribution System
  > FLT 531, SLC-LGB. NOTICEABLE "DIRTY SOCK" ODOR DETECTED BY FLIGHT ATTENDANTS ON FINAL DECENT DURING LAST 15 MINUTES ODOR DETECTED BY FLIGHT CREW; C/W INFO NOTICE 2017-T015E SECTION A. A/C IS OK FOR CONT SVC.
- [SDR YENA201811030953](https://openairdocs.org/sdr/YENA201811030953.md): Structure · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > AT CURRENT (10/2018) C6 CHECK (SAL), CORROSION WAS FOUND ON CENTER WING BOX TOP SKIN UPPER SURFACE BETWEEN FR41-42 & +Y1292. SEE THE REF /1/ EA FOR MORE DETAILS. THE SRM DOES NOT PROVIDE ALLOWABLE DAMAGE LIMITS NOR REPAIR GUIDELINES FOR THE DAMAGE LOCATION. RE
- [SDR YENA201811030952](https://openairdocs.org/sdr/YENA201811030952.md): Stringer · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING C6 CHECK AT (SAL), CORROSION WAS FOUND ON STRINGER 38L BTWN FR 53-64 AND STRINGER 37L BTWN FR 60-64 AT THE AFT FUSELAGE. SEE THE REF /1/ EA FOR MORE DETAILS. EVALUATED THE DAMAGE AGAINST SRM 53-41-13 AND THERE IS NO ALLOWABLE NOR APPLICABLE REPAIR FOR T
- [SDR YENA2018110530740](https://openairdocs.org/sdr/YENA2018110530740.md): Skin · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON EXTERNAL SKIN AT FRAME 42, +Y1292. REPAIRED THE SKIN IAW EC A18-886-01, AND EA 57-0294--18.
- [SDR YENA2018110530739](https://openairdocs.org/sdr/YENA2018110530739.md): Stringer · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON STRINGER 37L, FRAMES 60 AND 64 IN THE AFT CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE STRINGER IAW EC A18-880-01, AND EA 53-0296-18,
- [SDR YENA2018110530738](https://openairdocs.org/sdr/YENA2018110530738.md): Web · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT WEB LEVEL STR 23R AND BETWEEN FR 69 AND FR 70 AT AFT GALLEY AREA; REF AEROMAN WO 934679, NR 2018-343796, REPLACED SUPPORT WEB LEVEL STR 23R AND BETWEEN FR 69 AND FR 70 AT AFT GALLEY AREA I.A.W.SRM
- [SDR YENA2018110530737](https://openairdocs.org/sdr/YENA2018110530737.md): Web · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON SUPPORT WEB LEVEL STR 23L AND BETWEEN FR 69 TO FR 70 AT AFT GALLEY AREA; REF AEROMAN WO 934679, NR 2018-343797, REPLACED SUPPORT WEB LEVEL STR 23L AND BETWEEN FR 70 AT AFT GALLEY AREA I.A.W. SRM A320 51-72
- [SDR YENA2018110530736](https://openairdocs.org/sdr/YENA2018110530736.md): Structure · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL BETWEEN FR 66 TO FR 67 AT LEVEL STR 23L AT AFT GALLEY AREA; REF AEROMAN WO 934679, NRC 2018-343822,REPLACED LOWER SILL BTW FR 66 TO FR 68 AT LEVEL STR 23L AT AFT GALLEY AREA I.A.W. SRM A320 51-7
- [SDR YENA201811053735](https://openairdocs.org/sdr/YENA201811053735.md): Dummy Rail · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE DUMMY RAIL, Y503.2, BETWEEN FRAMES 12 TO 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11, AND DRAWING D53112825.
- [SDR YENA201811053734](https://openairdocs.org/sdr/YENA201811053734.md): Floor Support · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT, +Y1292, BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT.
- [SDR YENA201811053733](https://openairdocs.org/sdr/YENA201811053733.md): Structure · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER CORNER, STRINGER 23L AND FRAME 68. REPLACED THE CORNER IAW SRM 51-72-11, AND DRAWING D53480505.
- [SDR YENA201811053732](https://openairdocs.org/sdr/YENA201811053732.md): Skin · corroded · Nov 3, 2018 · N712JB · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON THE CENTER WING BOX TOP SKIN UPPER SURFACE BETWEEN FRAMES 41 - 42, +Y1292. REPAIRED.
- [SDR YENA201808280939](https://openairdocs.org/sdr/YENA201808280939.md): Plate · broken · Aug 28, 2018 · N712JB · Airbus A320232 · Wing Miscellaneous Structure
  > FLT 236, STI-JFK. ON 08/28/2018 AT JFK, WHILE TROUBLESHOOTING A HYDRAULIC LEAK COMING FROM THE LT WING TRAILING EDGE AFT OF THE PYLON, THE GREEN MAIN HYDRAULIC POWER PIPE INSTALLATION BULKHEAD CONNECTOR (REF. IPC 29-11-05-3D ITEM) WAS FOUND SEPARATED FROM THE
- [SDR YENA201808142312](https://openairdocs.org/sdr/YENA201808142312.md): Unknown · odor · Aug 12, 2018 · N712JB · Airbus A320232 · Air Distribution System
  > FWD GALLEY COFFEE POTS 1 & 2, FA REPORTED A BAD ELECTRIC ODOR, AND LIGHT SMOKE. WITH BOTH TURNED OFF AND NO FURTHER ISSUE. REACTIVATED THE FWD COFFEEMAKERS 1 AND 2 AND PERFORMED OPS CHECK IAW AMM 25-35-00. BREWED 5 POTS WITH WARMER PLATES ON EACH, NO UNUSU
- [SDR YENA201801040004](https://openairdocs.org/sdr/YENA201801040004.md): Idg · failed · Jan 4, 2018 · N712JB · Airbus A320232 · AC Generation System
  > RETURNED TO FIELD AFTER TAKE OFF DUE TO THE NR 1 GENERATOR WENT INOPERATIVE. RESET UNSUCCESSFUL. PERFORMED TSM 24-26-00-810-868-A. R & R THE NR 1 GCU IAW 24-22-34. R & R THE NR 1 IDG IAW AMM 24-21-51. PERFORMED ENGINE RUNS. NO FAULTS NOTED.
- [SDR YENA201801040003](https://openairdocs.org/sdr/YENA201801040003.md): Gcu · failed · Jan 4, 2018 · N712JB · Airbus A320232 · AC Generation System
  > RETURNED TO FIELD AFTER TAKE OFF FOR THE NR 1 GENERATOR WENT INOPERATIVE. RESET UNSUCCESSFUL. PERFORMED TSM 24-26-00-810-868-A. R & R THE NR 1 GCU IAW 24-22-34. R & R THE NR 1 IDG IAW AMM 24-21-51. PERFORMED ENGINE RUNS. NO FAULTS NOTED.
- [SDR YENA20150420073](https://openairdocs.org/sdr/YENA20150420073.md): Pump · leaking · Apr 20, 2015 · N712JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > FLIGHT DIVERTED DUE TO ECAM MESSAGE HYD GRSVR LO LVL. FOUND GREEN HYDRAULIC SYSTEM EDP LEAKING ON NR 1 ENGINE. R & R EDP ASSEMBLY IAW AMM. NO LEAKS NOTED, OPS CHECK NORMAL.

## 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 = 'N712JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N712JB/reports

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