# Service difficulty reports: N805JB

A list on [N805JB](https://openairdocs.org/aircraft/N805JB.md).

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

- [SDR YENA2025093000981](https://openairdocs.org/sdr/YENA2025093000981.md): Hinge Fitting · corroded · Sep 25, 2025 · N805JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ3 VERTICAL STABILIZER; REMOVED AND REPLACED #3 VERTICAL STABILISER FITTING ALL WORK DONE BY O. FLORES 8621011 AND QC RII. C. PORTILLO # 230. ALL WORK EMBODIED ON AEROMAN
- [SDR YENA2025093000980](https://openairdocs.org/sdr/YENA2025093000980.md): Bearing · corroded · Sep 25, 2025 · N805JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ4 VERTICAL STABILIZER; REMOVED AND REPLACED HINGE ARM FITTING 4 AND FASTENERS ON VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008 STEP 2.A AND A320 SRM 51-72-11 AND DW
- [SDR YENA2025093000979](https://openairdocs.org/sdr/YENA2025093000979.md): Hinge Arm · corroded · Sep 25, 2025 · N805JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ1 VERTICAL STABILIZER; (RESOLVED ON W/O: 1401080 TASKCARD: NR-00014) REMOVED AND REPLACED HINGE ARM FITTING 1 AND FASTENERS ON VERTICAL STABILIZER I.A.W A320 SRM 55-36-42
- [SDR YENA2025081900851](https://openairdocs.org/sdr/YENA2025081900851.md): Computer · failed · Aug 14, 2025 · N805JB · Airbus A320232 · Flight Control System
  > FLT #2144, PBI-EWR. DURING CLIMBOUT 310KTS FL260 SHIMMY SHUDDER FELT LIGHT INTONSITY WITH MANUAL ROLL INPUTS VIBRATION STOPED RETURED WITH AP ON DIMINISHED CLIMBING THROUGH FL330 SURVEY FORM COMPLETED DFDR PUSHED; INSPECTED AILERON SERVO AND HINGE BEARINGS FOR
- [SDR YENA2025081900850](https://openairdocs.org/sdr/YENA2025081900850.md): Computer · failed · Aug 14, 2025 · N805JB · Airbus A320232 · Flight Control System
  > FLT #2144, PBI-EWR. DURING CLIMBOUT 310KTS FL260 SHIMMY SHUDDER FELT LIGHT INTONSITY WITH MANUAL ROLL INPUTS VIBRATION STOPED RETURED WITH AP ON DIMINISHED CLIMBING THROUGH FL330 SURVEY FORM COMPLETED DFDR PUSHED; INSPECTED AILERON SERVO AND HINGE BEARINGS FOR
- [SDR YENA2025021100147](https://openairdocs.org/sdr/YENA2025021100147.md): Unknown · odor · Feb 10, 2025 · N805JB · Airbus A320232 · Air Distribution System
  > FLT#1257, HPN-PBI. 'FA REPORTS FUME ODOR ON TOUCHDOWN AND AGAIN WHEN PARKING FLIGHT DECK NOTICED ODOR AT 5000 FT ON APPROACH; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B2 IDENTIFIED ODOR DECONTAMINATION LEVEL 1 WAS ACCOMPLISHED PER TSM 05-50-00-810-83
- [SDR YENA2024040800496](https://openairdocs.org/sdr/YENA2024040800496.md): Unknown · odor · Apr 3, 2024 · N805JB · Airbus A320232 · Air Distribution System
  > FLT#2593, JFK-MIA. 'OILY/DIRTY SOCK SMELL THROUGHOUT ENTIRE A/C ( APU BLEED AIR SUPPLY SYSTEM); C/W INFORMATION NOTICE SECTION 2017-T015 DECONTAMINATION LEVEL A PER TSM 05-50-0081D-085B A/C OK FOR CONT SVC MX-4 UPDATED PLACARD REMOVED MDDR CLEARED.'
- [SDR YENA2024010900020](https://openairdocs.org/sdr/YENA2024010900020.md): Unknown · unknown · Jan 7, 2024 · N805JB · Airbus A320232 · Air Distribution System
  > FLT#1903, JFK-SJU. 'PASSING 5000 FA CALLED TO REPORT DIRTY SOCKS SMELL SAID THEY WERE LIGHT HEADED AND DIZZY FWD AND AFT GALLEY;COMPLY WITH INFO NOTICE 2017-T015 SECTION A, ISOLATED FAULT TO TYPE 10, (A) 1C PER TSM 05-50-00-810-085-B1 TSM 05-50-00-810-085-D. A
- [SDR YENA2023081500942](https://openairdocs.org/sdr/YENA2023081500942.md): Unknown · unknown · Aug 11, 2023 · N805JB · Airbus A320232 · Landing Gear System
  > FLT#1347, DCA-SJU. 'DURING APPROACH TO LAND, 1ST ATTENT TO LOWER GEAR WAS UNSUCCESSFUL. THE ONLY INDICATION WAS LANDING GEAR DOORS PARTIALLY OPEN IN AMBER (WIND NOISE CONFIRMED) RECYCLED GEAR HANDLE AND LANDING GEAR EXTENDED NORMALLY, ALL INDICATIONS NORMAL. (
- [SDR YENA2022022100083](https://openairdocs.org/sdr/YENA2022022100083.md): None · none · Feb 20, 2022 · N805JB · Airbus A320232 · Weather Radar System
  > FLT # 471, LGA-FLL. NAV RA 2 FAULT ON APPROACH; COMPLIED WITH INFO NOTICE 2022-T001B, O DEFECTS NOTED.BITE TEST OK PER 34-42-00-740-002-A.SUSPECT 5G INTERFERENCE.NO 30 DAY HISTORY.MCC BOB NOTIFIED..
- [SDR YENA2021112300778](https://openairdocs.org/sdr/YENA2021112300778.md): Unknown · odor · Nov 21, 2021 · N805JB · Airbus A320232 · Air Distribution System
  > FLT 132, LAX-MCO. INFLIGHT CREW REPORTED "DUSTY" ODOR DURING DESCENT FLIGHT CREW DID NOT NOTICE SMELL; COMPLIED WITH INFO NOTICE 2017-T015 SECTION A(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 S
- [SDR YENA2021102700726](https://openairdocs.org/sdr/YENA2021102700726.md): Apu · odor · Oct 26, 2021 · N805JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > FLT 1099, LGA-MCO. DIRTY SOCKS SMELL ON DESCENT INTO MCO, BETWEEN 4000' AND 2000'; VERIFIED SOURCE OF ODOR COMING FROM APU, SEE ITEM 2 FOR APU DEFERRAL. COMPLIED WITH INFO NOTICE 2017-T015I SECTION A. PERFORMED LEVEL A TYPE 1 DECONTAMINATION OF THE ECS REF AMM
- [SDR YENA2021052800342](https://openairdocs.org/sdr/YENA2021052800342.md): A/C Pack · odor · May 25, 2021 · N805JB · Airbus A320232 · Cabin Cooling System
  > FLT 1517, LGA-TPA. FUMES IN THE COCKPIT DURING DESCENT. TURNED OFF PACK 1 AND SMELL DISSAPATED; COMPLIED WITH INFORMATION NOTICE 2017-T015F SECTION A. AIRCRAFT IS OK FOR SERVICE.
- [SDR YENA2021031200171](https://openairdocs.org/sdr/YENA2021031200171.md): Mask · failed · Mar 11, 2021 · N805JB · Airbus A320232 · Crew Oxygen System
  > FLT 1532, CTG-JFK. FO'S OXY MASK HAS BROKEN FACESHIELD CLIP AT BRIDGE OF NOSE; FO'S OXY MASK HAS BROKEN FACESHIELD CLIP AT BRIDGE OF NOSE.
- [SDR YENA2020030950225](https://openairdocs.org/sdr/YENA2020030950225.md): Servo Control · failed · Mar 5, 2020 · N805JB · Airbus A320232 · Rudder Control System
  > "FT # 391, BOS-TPA. DURING PHASE 2 COCKPIT JOB CARD A320-27-24-00-710-002 OPS TEST OF RUDDER SERVOCTL WITH INDIVIDUAL HYD SYSTEM; FOUND RUDDER WOULD KICK OVER TO THE RIGHT WITH OUT PEDAL INPUT ON ""Y"" HYD SYSTEM PWR; FOUND ""Y"" SYSTEM SERVOCONTROL (3025GM) I
- [SDR YENA2020030950224](https://openairdocs.org/sdr/YENA2020030950224.md): Servo Control · failed · Mar 5, 2020 · N805JB · Airbus A320232 · Rudder Control System
  > "FT # 391, BOS-TPA. DURING PHASE 2 COCKPIT JOB CARD A320-27-24-00-710-002 OPS TEST OF RUDDER SERVOCTL WITH INDIVIDUAL HYD SYSTEM; FOUND RUDDER WOULD KICK OVER TO THE RIGHT WITH OUT PEDAL INPUT ON ""Y"" HYD SYSTEM PWR; FOUND ""Y"" SYSTEM SERVOCONTROL (3025GM) I
- [SDR YENA2020021280168](https://openairdocs.org/sdr/YENA2020021280168.md): Skin · dented · Feb 8, 2020 · N805JB · Airbus A320232 · Aerodynamic Fairings
  > DURING HEAVY MAINTENANCE, DENT EXTERNAL SKIN UPPER SURFACE TAIL CONE ON THE (1 EACH) AT LEVEL FR81 STR 1R TO STR 1L; REPAIRED EXTERNAL SKIN UPPER SURFACE TAIL CONE ON TAIL AT LEVEL FR81 BTW STR 1R TO 1L IAW A320 SRM 53-51-11-300-002 ITEM 2A (STEP 24 TO 28) AND
- [SDR YENA2019062400341](https://openairdocs.org/sdr/YENA2019062400341.md): Battery Pack · failed · Jun 20, 2019 · N805JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAIL BATTERY AT 11WL; REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT FIN 11WL PER AMM 33-51-38.
- [SDR YENA2019041620197](https://openairdocs.org/sdr/YENA2019041620197.md): Battery Pack · failed · Apr 12, 2019 · N805JB · Airbus A320232 · Emergency Lighting
  > FT # 225, EMERGENCY LIGHT TEST FAILED; REMOVED AND REPLACED BATTERIES AT 12WL AND 13WL BITE AND OPS TEST OK IAW AMM 33-51-38.
- [SDR YENA2019041620196](https://openairdocs.org/sdr/YENA2019041620196.md): Battery Pack · failed · Apr 12, 2019 · N805JB · Airbus A320232 · Emergency Lighting
  > FT # 225, EMER. LIGHT TEST FAILED; REMOVED AND REPLACED BATTERIES AT 12WL AND 13WL BITE AND OPS TEST OK IAW AMM 33-51-38.
- [SDR YENA2019040520175](https://openairdocs.org/sdr/YENA2019040520175.md): Unknown · odor · Apr 2, 2019 · N805JB · Airbus A320232 · Air Distribution System
  > FT # 386, LEVEL 2 CABIN ODOR INFLIGHT FL360 ELECTRICAL/RUBBER SMELL BETWEEN ROWS 16-18. ANTI-ICE OFF, PACKS NORMAL; ACCOMPLISHED ELECTRICAL ODOR SYSTEM INTEGRITY CHECK PER AMM 44-20-000-803 PROCEDURE 4B 1-15,18. ROWS 18-20 LEFT AND RIGHT SIDE INSPECTION SHOW
- [SDR YENA2018022280107](https://openairdocs.org/sdr/YENA2018022280107.md): Unknown · odor · Feb 18, 2018 · N805JB · Airbus A320232 · Air Distribution System
  > FLT 493, BOS-DEN. INFLIGHT CREW REPORTED TO FLIGHT CREW A SLIGHT WIRE ELECTRICAL SMELL AROUND SEAT 14,15,16. LTV SYSTEM WAS SWITCHED OFF AND SMELL DISSIPATED; PERFORMED TSM 05-50-00-810-831-A CABIN ODOR IDENTIFIED AS LIVE TV. LIVE TV PLACED ON MEL. PERFORMED T
- [SDR YENA20161108976](https://openairdocs.org/sdr/YENA20161108976.md): Door Sill · corroded · Nov 8, 2016 · N805JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON DOOR SILL FRAME 66. THE CORROSION WAS REMOVED IAW SRM TASK 53-41-14-300-001.
- [SDR YENA20161108975](https://openairdocs.org/sdr/YENA20161108975.md): Door Sill · corroded · Nov 8, 2016 · N805JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON DOOR SILL AT FRAME 68. REMOVED THE CORROSION IAW SRM TASK 53-41-14-300-001.
- [SDR YENA20161108974](https://openairdocs.org/sdr/YENA20161108974.md): Shear Tie · corroded · Nov 8, 2016 · N805JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON FRAME SUPPORT BTW FRAMES 69-70 23L. R & R THE FRAME SUPPORT IAW SRM 51-72-11.
- [SDR YENA20161108973](https://openairdocs.org/sdr/YENA20161108973.md): Shear Tie · corroded · Nov 8, 2016 · N805JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON FRAME SUPPORT BETWEEN FRAMES 69-70 STRINGER 23R. R & R THE FRAME SUPPORT IAW SRM 51-72-11.
- [SDR YENA20151016470](https://openairdocs.org/sdr/YENA20151016470.md): Fan · failed · Oct 16, 2015 · N805JB · Airbus A320232 · Air Distribution Fan
  > AMBER FAN ON CONDITION PAGE, C/B 18X PANEL 122 VU POPPED AND FOUND ELECTRICAL ODOR ON C/B. R & R CABIN RECIRCULATION FAN IAW AMM 21-21-51. OPS CHECK GOOD.
- [SDR YENA20150921427](https://openairdocs.org/sdr/YENA20150921427.md): Servo Valve · faulty · Sep 21, 2015 · N805JB · Airbus A320232 · Steering Unit
  > AIR RETURNED, AFTER TAKEOFF RECEIVED ECAM MESSAGE NOSE WHEEL STEERING FAULT. TROUBLESHOOT TO STEERING SERVO VALVE. R & R SERVO VALVE, 6GC, IAW AMM 32-51-51. LEAK AND OPS CHECK GOOD.
- [SDR YENA20141117253](https://openairdocs.org/sdr/YENA20141117253.md): Windshield · cracked · Nov 17, 2014 · N805JB · Airbus A320232 · Flight Compartment Windows
  > CREW REPORTED AT FL 370, A LOUD POP AND ELECTRICAL ARCING ON FRONT RT WINDSHIELD. ECAM ANTI-ICE RT WINDSHIELD. FOUR LONG CRACKS ON WINDSHIELD OUTER FLY. R & R F/O FRONT WINDSHIELD. GROUND OPS CHECK OK. AIR LEAK CHECKED. NO LEAKS FOUND IAW 56-11-11.
- [SDR YENA20130210039](https://openairdocs.org/sdr/YENA20130210039.md): Slide · low pressure · Feb 10, 2013 · N805JB · Airbus A320232 · Escape Slide
  > FLT 493 BOS-DEN, R2 DOOR SLIDE PRESS IN THE RED. REMOVED AND REPLACED R2 DOOR SLIDE PER AMM 25-62-44-04. PRESSURE CHECK GOOD. 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 = 'N805JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N805JB/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.