# Service difficulty reports: N621JB

A list on [N621JB](https://openairdocs.org/aircraft/N621JB.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 YENA2026081400677](https://openairdocs.org/sdr/YENA2026081400677.md): Relay · failed · Aug 12, 2026 · N621JB · Airbus A320232 · Manifold Pressure (MP) Indicating
  > FLT 1439, BOS-AUS (AIRTURN BACK TO BOS). NR 2 ENG EPR MODE FAULT ON CLIMB OUT AT APPROX FL 230. REPLACED P2/T2 PROBE NO HELP IAW 73-22-11. R & R RELAY BOX OPS CHECKED OK IAW 71-51-49-400-010-A.
- [SDR YENA2025092300960](https://openairdocs.org/sdr/YENA2025092300960.md): Door Frame · cracked · Sep 20, 2025 · N621JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB HOLE OF FR 68 LH DOOR STOP FITTING Ñ1. CRACK DIRECTION 5 AND 11 OCLOCK. CRACK D= 0.160 INCH; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00036) PERFORMED PERMANENT REPAIR ON FR68 LH AT LOWER INBOARD HOLE
- [SDR YENA2025092300959](https://openairdocs.org/sdr/YENA2025092300959.md): Door Frame · cracked · Sep 20, 2025 · N621JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING Ñ1. CRACK DIRECTION 5 OCLOCK. CRACK D= 0.160 INCH; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00037) PERFORMED PERMANENT REPAIR ON LOC. ON LOWER INB HOLE OF FR 68 RH D
- [SDR YEN2025F00008](https://openairdocs.org/sdr/YEN2025F00008.md): Door Frame · cracked · Sep 20, 2025 · N621JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING Ñ1. CRACK DIRECTION 5 OCLOCK. CRACK D= 0.160 INCH; PERFORMED PERMANENT REPAIR ON LOC. ON LOWER INB HOLE OF FR 68 RH DOOR STOP FITTING #1 IAW A320 SRM 53-41-12-300
- [SDR YENA2025092300958](https://openairdocs.org/sdr/YENA2025092300958.md): Beam · corroded · Sep 20, 2025 · N621JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: CORROSION ON LONGITUDINAL BEAM LOCATED BTW FR. 40 TO FR.41 AND AT LEVEL STR 20A. R/H SIDE EMERGENCY EXIT DOOR AREA IN PASSENGER CABIN; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00038) REMOVED AND REPLACED LONGITUDINAL BEAM LOC. BTW FR40
- [SDR YENA2025092300957](https://openairdocs.org/sdr/YENA2025092300957.md): Hinge Arm · corroded · Sep 20, 2025 · N621JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: AFTER REMOVED BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ5 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00040) REMOVED AND REPLACED HINGE FITTING #5 LOC. VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008 ALL
- [SDR YENA2025092300956](https://openairdocs.org/sdr/YENA2025092300956.md): Bearing · corroded · Sep 20, 2025 · N621JB · Airbus A320232 · Vertical Stabilizer
  > DURING HEAVY MAINTENANCE: AFTER REMOVE BEARING CORROSION WAS FOUND ON HINGE ARM FITTING Ñ4 ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1404606 TASKCARD: NR-00041) REMOVED AND REPLACED HINGE FITTING #4 LOC. VERTICAL STABILIZER I.A.W A320 SRM 55-36-42-300-008. ALL
- [SDR YENA2025081800844](https://openairdocs.org/sdr/YENA2025081800844.md): Computer · failed · Aug 15, 2025 · N621JB · Airbus A320232 · Flight Control System
  > FLT # 2427 FLL-MBJ, AIR RETURN BACK INTO FLL. DUAL INPUT CALL AT ABOUT 2500FT, WHEN THERE WAS NO DUAL INPUT ECAM FOR ELAC 2 PERFORMED THE RESET PROCEDURE BUT THE ECAM CAME BACK THE AIRCRAFT DID TWO SHARP JERKS AFTER TAKEOFF TO THE RIGHT;TWO AIRCRAFT MOVEMENTS
- [SDR YENA2025081800843](https://openairdocs.org/sdr/YENA2025081800843.md): Computer · failed · Aug 15, 2025 · N621JB · Airbus A320232 · Flight Control System
  > FLT # 2427 FLL-MBJ, AIR RETURN BACK INTO FLL. DUAL INPUT CALL AT ABOUT 2500FT, WHEN THERE WAS NO DUAL INPUT ECAM FOR ELAC 2 PERFORMED THE RESET PROCEDURE BUT THE ECAM CAME BACK THE AIRCRAFT DID TWO SHARP JERKS AFTER TAKEOFF TO THE RIGHT;TWO AIRCRAFT MOVEMENTS
- [SDR YENA2025050700466](https://openairdocs.org/sdr/YENA2025050700466.md): Battery · no test · May 7, 2025 · N621JB · Airbus A320232 · Emergency Lighting
  > FLT#591, BOS-TPA. 'EPSU 10WL BATTERY FAILS OPERATIONAL TEST; REMOVED AND REPLACED EPSU 10WL BATTERY IAW AMM 33-51-38 OPS CHECKS GOOD.'
- [SDR YENA2024022900304](https://openairdocs.org/sdr/YENA2024022900304.md): Unknown · odor · Feb 29, 2024 · N621JB · Airbus A320232 · Air Distribution System
  > FLT#613, HPN-FLL. 'AFT FLIGHT ATT SAID HE SMELLED SMOKE OR BURNING WHEN WE LOWERED THE GEAR; PERFORMED INSPECT FOR SMOKE OR BURN SMELL PER TSM 05-50-00-810-8310A. NO HISTORY OR SIGNS OF ODOR. CLASSIFIED AS A TYPE 10. A/C OK FOR SERVICE.'
- [SDR YENA2023120401523](https://openairdocs.org/sdr/YENA2023120401523.md): Unknown · unknown · Dec 4, 2023 · N621JB · Airbus A320232 · Air Conditioning System
  > FLT#36, PHX-JFK. '#1 FA REPORTS CHEMICAL ODOR IN FWD CABIN ONLY ON FINAL APPROACH LASTED 1 MIN; COMPLIED WITH INFO NOTICE 2017-T015 SECTION B2 DECONTAMINATION LEVEL A WAS ACCOMPLISHED PER TSM 05-50-00-810-085 AC OK FOR SVC.'
- [SDR YENA2023111501389](https://openairdocs.org/sdr/YENA2023111501389.md): Unknown · unknown · Nov 13, 2023 · N621JB · Airbus A320232 · Hydraulic Power System
  > FLT#261, BOS-SJU. (AIRCRAFT DECLARED AN EMERGENCY INTO SJU) 'HYD G RSVR LO LVL HYD G RSVR LO PR.' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023052600552](https://openairdocs.org/sdr/YENA2023052600552.md): Unknown · unknown · May 23, 2023 · N621JB · Airbus A320232 · Air Conditioning System
  > FLT#2613, ATL-LGA. 'DIRTY SOCK SMELL THROUGHOUT THE AIRCRAFT; COMPLIED WIITH INFO NOTICE 2017-T015J SECTION B2 DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER AMM 25-00-00-615-803A VERIFIED SOURCE OF ODOR TO BE APU. FOUND OIL TRACES IN APU COMPARTMENT APU PLACED
- [SDR YENA2023005020493](https://openairdocs.org/sdr/YENA2023005020493.md): Unknown · unknown · May 1, 2023 · N621JB · Airbus A320232 · Air Conditioning System
  > FLT#2433, DCA-PBI. 'FLIGHT ATTENDANTS (ALL) GOT THE DIRTY SOCK (OLD DEICING FLUID) SMELL IN THE CABIN ON DESCENT (APU DEFERRED); COMPLIED W/ INFO NOTICE 2017-T015, SECTION B2, DECONTAMINATION LEVEL 1 WAS ACCOMPLISHED PER TSM 05-50-00-810-085-B. A/C IS OK FOR S
- [SDR YENA2023005010464](https://openairdocs.org/sdr/YENA2023005010464.md): Unknown · unknown · May 1, 2023 · N621JB · Airbus A320232 · Air Conditioning System
  > FLT#1799, LGA-MCO. 'DIRTY SOCK ODOR FROM COCKPIT TO AFT AIRCRAFT ON DESCENT THROUGH 8000; COMPLIED WITH INFORMATIONAL NOTICE 2017-T015, SECTION B2 DECONTAMINATION LEVEL A WAS ACCOMPLISHED PER TSM 05-50-00-810-831-A. A/C IS OK FOR CONTINUED SERVICE. ODOR COMING
- [SDR YENA2023041100344](https://openairdocs.org/sdr/YENA2023041100344.md): Unknown · unknown · Apr 7, 2023 · N621JB · Airbus A320232 · Standard Practices/Structures
  > FLT#1529, JFK-RSW. 'UPON ARRIVAL AT GATE INFLIGHT NOTIFIED ME OF A 'FUME EVENT ' ON DESCENT PASSING THRU 10,000 AND LASTING 5-7 MINUTES. NO ODOR WAS DETECTED IN THE FLIGHT DECK ( APU SYSTEM).' (SUPPLEMENTAL INFORMATION TO FOLLOW)
- [SDR YENA2023032700279](https://openairdocs.org/sdr/YENA2023032700279.md): Unknown · unknown · Mar 24, 2023 · N621JB · Airbus A320232 · Air Conditioning System
  > FLT#1971, LGA-FLL. 'VERY STRONG ODOR/FUME ON DESCENT AND FINAL. SMELLED ACRID OIL COMING OUT OF BLEEED SYS WITH AND WITHOUT APU; ACCOMPLISHED TSM 05-50-00-810-831-A, FOUND TO BE THE APU. PERFORMED SUBTASK 05-50-00-810-085B. COMPLIED WITH INFO NOTICE 2017-T015
- [SDR YENA2022111001104](https://openairdocs.org/sdr/YENA2022111001104.md): None · none · Nov 9, 2022 · N621JB · Airbus A320232 · Emergency Lighting
  > DURING HEAVY MAINTENANCE: DON'T PAST TEST EMERGENCY LIGHT PTP SHOWS EPSU EXT LOAD AFT L BATTERY; REF AEROMAN WO 2022-283/1 NR2022-558321. REMOVED AND REPLACED THE BATTERY OF THE EMERGENCY POWER SUPPLY UNIT FIN 13WL IAW AMM 33-51-38-000-002-A AND 33-51-38-400-
- [SDR YENA2022111001103](https://openairdocs.org/sdr/YENA2022111001103.md): None · none · Nov 9, 2022 · N621JB · Airbus A320232 · Emergency Equipment
  > DURING HEAVY MAINTENANCE: DONT PASS TEST EMERGENCY LIGHT TEST THROUGH PTP AT THE FWD GALLEY AREA; REF AEROMAN WO 2022-283/1 NR 2022-558319 REMOVED AND REPLACED EMERGENCY EVACUATION DOOR SLIDE RAFT 831 IAW AMM 25-62-44-000-012-A. AND AMM 25-62-44-400-007-A. AN
- [SDR YENA2022111001102](https://openairdocs.org/sdr/YENA2022111001102.md): None · none · Nov 9, 2022 · N621JB · Airbus A320232 · Fuselage, Stabilizer Attach Fittings
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 INSIDE INNER FRAME SEGMENT FORWARD POSITIONS. THE LONGEST CRACK IS 2.23 INCHES APPROX. PASSENGER CABIN; REF AEROMAN W/O 2022-283/1 NR 2022-557954. PERFORMED PERMANENT REPAIR ON EMERGENCY E
- [SDR YENA2022111001101](https://openairdocs.org/sdr/YENA2022111001101.md): None · none · Nov 9, 2022 · N621JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: REF AEROMAN W/O 2022-283/1 NR 2022-557900. CRACK INDICATION ON FRAME 16 LH SIDE OPEN FASTENER HOLE H3 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 2 AND 3 O'CLOCK ON INTERCOSTAL FITTING LAYER AT FWD GALLEY; REF AEROMAN W/O 2
- [SDR YENA2022111001100](https://openairdocs.org/sdr/YENA2022111001100.md): None · none · Nov 9, 2022 · N621JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: REF AEROMAN W/O 2022-283/1 NR 2022-557867. CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APPROX. IN COCKPIT (1EA); REF AEREOMAN W/0 2022-283/1 NR 2022-5
- [SDR YENA2022111001099](https://openairdocs.org/sdr/YENA2022111001099.md): None · none · Nov 9, 2022 · N621JB · Airbus A320232 · Fuselage Internal Mounting Structure
  > DURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT(1EA); REF AEROMAN W/O 2022-283/1 NR 2022-557868. REMOVED AND REPLACED CONTINUITY FITTIN
- [SDR YENA2022012400019](https://openairdocs.org/sdr/YENA2022012400019.md): Apu · coked · Jan 21, 2022 · N621JB · Airbus A320232 · Air Conditioning System
  > FLT # 1557, FLL-BOG. STRONG ODOR DIRTY SOCK SMELL PASSING 17,000 INTO BOGOTA. FOLLOWED ISOLATION PROCEDURE. SUSPECT PACK #1 SMELL DISSIPATED. SMELT BY BOTH FLIGHT CREW AND #1 F/A SMELT LEVEL 2 ( PACKS); REF L/P 3253928 FOR CORRECTIVE ACTION. MX-4 UPDATED, PL
- [SDR YENA2021122000865](https://openairdocs.org/sdr/YENA2021122000865.md): Unknown · odor · Dec 19, 2021 · N621JB · Airbus A320232 · Air Distribution System
  > FLT 2295, EWR-MIA. BURNING OL SMELL IN AFT PORTION OF AIRCRAFT REPORTED BY ACFT F/A'S DURING CLIMB OUT SMELL WAS REPORTED AROUND 12,000FT SMELL DISAPPEARED SEVERAL MINUTES LATER DURING ARRIVAL SMELL REPORTED AROUND 11,000FT AND DISSIPATED PRIOR TO LANDING FLIG
- [SDR YENA2021102700727](https://openairdocs.org/sdr/YENA2021102700727.md): Unknown · odor · Oct 26, 2021 · N621JB · Airbus A320232 · Air Distribution System
  > FLT 939, JFK-SJD. ON FINAL DES ENTIRE CABIN CREW REPORTED DIRTY SOCK ODOR IN CABIN; COMPLIED WITH INFORMATION NOTICE ON SB. 2017-T015 SECTION B 1 OK A/C OK FOR SERVICE MCC MARIO NOTIFIED
- [SDR YENA2020121100591](https://openairdocs.org/sdr/YENA2020121100591.md): Battery · failed · Dec 7, 2020 · N621JB · Airbus A320232 · Emergency Lighting
  > FLT 1391, BOS-TPA. EMERGENCY LIGHT BATTERY 10 WL FAILED BATTERY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY, IAW AMM 33-51-38.
- [SDR YENA2020121100590](https://openairdocs.org/sdr/YENA2020121100590.md): Battery · failed · Dec 7, 2020 · N621JB · Airbus A320232 · Emergency Lighting
  > FLT 1391, BOS-TPA. EMERGENCY LIGHT BATTERY 10WL FAILED BATTERY TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY 10WL, IAW AMM 33-51-38.
- [SDR YENA201902250101](https://openairdocs.org/sdr/YENA201902250101.md): Battery · failed · Feb 25, 2019 · N621JB · Airbus A320232 · Emergency Lighting
  > FLT 391, BOS-TPA. EPSU BATTERY 11WL FAILS EMERG LIGHT SYSTEM TEST; R & R BATTERY AT EPSU 11WL IAW AMM 33-51-38, SYSTEM OPS CHECKS GOOD.
- [SDR YENA201810220705](https://openairdocs.org/sdr/YENA201810220705.md): Seat Track · corroded · Oct 22, 2018 · N621JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR STRUCTURE, SEAT TRACK Y765, FR 62 +8.00", STR 23L. CORROSION MEAS. 3.90"L X.772"W X.063" D. MATERIAL LOSS = 29%; CORROSION THAT IS BEYOND ALLOWABLE LIMITS, PER SRM 53-41-15-283-001 ON SEAT TRACK Y76
- [SDR YENA201708260696](https://openairdocs.org/sdr/YENA201708260696.md): Flap · locked · Aug 26, 2017 · N621JB · Airbus A320232 · Trailing Edge Flap Control System
  > FT 1522, LGB-PDX. F/CTL FLAPS LOCKED ALIGNMENT FAULT" ECAM DURING APPROACH. FLAPS LOCKED BETWEEN 0 AND 1; RESET FLAP C/B OPS CHECK GOOD PER AMM 27-51-00. A/C OK FOR SERVICE.
- [SDR YENA201707150576](https://openairdocs.org/sdr/YENA201707150576.md): Flap System · malfunctioned · Jul 15, 2017 · N621JB · Airbus A320232 · Trailing Edge Flap Control System
  > EMERGENCY DECLARED. F/CTL FLAP LOCKED. ALIGNMENT FAULT ECAM ON APPROACH; PERFORMED TSM 27-51-00-810-849-A. RESET FAULT, NO FAULT NOTED. ACC BITE TEST OF SFCC-1 AND SFCC-2 IAW AMM 27-51-00-740-002, NO FAULT NOTED. PERFORMED FLAPS OPERATIONAL TEST IAW AMM 27-
- [SDR YENA201706240519](https://openairdocs.org/sdr/YENA201706240519.md): Proximity Sensor · faulted · Jun 24, 2017 · N621JB · Airbus A320232 · Trailing Flap Position Indicating System
  > DURING FINAL APPROACH, FLAPS LOCKED, ALIGNMENT FAULT SLATS 2 FLAPS <1. R & R 37CV PROXIMITY SENSOR IAW AMM 27-51-44-000-002A, OPS CHECKED NORMAL.
- [SDR YENA201706040463](https://openairdocs.org/sdr/YENA201706040463.md): Battery · failed · Jun 4, 2017 · N621JB · Airbus A320232 · Emergency Lighting
  > AFT LEFT EPSU BATTERY FAULTED. R & R THE BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR YENA201705180374](https://openairdocs.org/sdr/YENA201705180374.md): Epsu · inoperative · May 18, 2017 · N621JB · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS AT ROWS 15, 19, 23 INOPERATIVE. R & R 11WL EPSU IAW AMM 33-51-38-000-002. OPS CHECKED GOOD IAW AMM 33-51-00-710-007.
- [SDR YENA201704180289](https://openairdocs.org/sdr/YENA201704180289.md): Power Supply · failed · Apr 18, 2017 · N621JB · Airbus A320232 · Emergency Lighting
  > FOUND NO COMM BETWEEN CID'S & EPSU. R & R THE EPSU (10WL) IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR YENA201612031080](https://openairdocs.org/sdr/YENA201612031080.md): Seat Track · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AT L2 DOOR FWD LOWER CORNER, SMALL AFT PIECE OF INBD SEAT TRACK Y1732, FRAME 66. R & R THE SEAT TRACK IAW SRM 51-72-11.
- [SDR YENA201612031079](https://openairdocs.org/sdr/YENA201612031079.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED FLOOR SUPPORT AT FRAME 68, -Y1292. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201612031078](https://openairdocs.org/sdr/YENA201612031078.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AROUND SCREW HOLE ON THE FLOOR SUPPORT AT -Y1292, FR 66+8. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201612031077](https://openairdocs.org/sdr/YENA201612031077.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON TWO SCREW HOLES ON FLOOR SUPPORT AT -Y1292, FRAME 66. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201612031076](https://openairdocs.org/sdr/YENA201612031076.md): Door Sill · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FRAME 67 + 19 R2 DOOR SILL. R & R DOOR SILL IAW SRM 53-41-14-300-001.
- [SDR YENA201612031075](https://openairdocs.org/sdr/YENA201612031075.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AROUND SCREW HOLE ON THE FLOOR SUPPORT AT Y1292 FROM FRAME 64 TO 66. R & R FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201612031074](https://openairdocs.org/sdr/YENA201612031074.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED AT SCREW HOLES FR 68+11ON FLOOR SUPPORT AT Y1292. R & R FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201612031073](https://openairdocs.org/sdr/YENA201612031073.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVEREDS ON FLOOR SUPPORT AT Y1292 FRAMES 67 - 68. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201612031072](https://openairdocs.org/sdr/YENA201612031072.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y1732 FR 65+10. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201612031071](https://openairdocs.org/sdr/YENA201612031071.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT -Y1292 +8 INCHES FROM FR 16. R & R FLOOR SUPPORT IAW SRM 51-72-11.
- [SDR YENA201612031070](https://openairdocs.org/sdr/YENA201612031070.md): Floor Support · corroded · Dec 3, 2016 · N621JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON AT BARREL NUT HOLES ON FR 66 FLOOR SUPPORT Y464. R & R FLOOR BEAM Y464 IAW A302 SRM 51-72-11.
- [SDR YENA20160707639](https://openairdocs.org/sdr/YENA20160707639.md): Battery Pack · failed · Jul 7, 2016 · N621JB · Airbus A320232 · Emergency Lighting
  > DURING INSPECTION, FOUR OVERWING RED EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK PASSED.
- [SDR YENA20150130012](https://openairdocs.org/sdr/YENA20150130012.md): Power Supply · faulted · Jan 30, 2015 · N621JB · Airbus A320232 · Emergency Lighting
  > DURING MAINTENANCE, EPSU EMERGENCY EXIT AT LT POSITION FAULTED. R & R EPSU AT LT EMERGENCY EXIT, IAW AMM 33-51-38. OPS CHECK AND TEST OK.

Next page: https://openairdocs.org/aircraft/N621JB/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 = 'N621JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N621JB/reports

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