# Service difficulty reports: N324US, cancelled Jan 14, 2026

A list on [N324US, cancelled Jan 14, 2026](https://openairdocs.org/deregistered/N324US-2026-01-14.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 4 · 189 reports

- [SDR DALA2025061904598](https://openairdocs.org/sdr/DALA2025061904598.md): Elec Connector · disconnected · Jun 13, 2025 · N324US · Airbus A320211 · Fire Protection System Wiring
  > SHIP 3224 DISC: CREW REPORTS ENG SQUIB NOT TESTING ON PREFLIGHT. C/A: RECONNECTED CONNECTOR PLUG FOR NBR AFT FIRE BOTTLE SQUIB TEST OK. REF A320 AMM 26-21-00. DURING CLOSE UP FOUND PANEL 415 BR WITH ONE MISSING FASTENER. OK TO DEFER FOR UP TO 10 CYCLES PER A32
- [SDR DALA2025052403992](https://openairdocs.org/sdr/DALA2025052403992.md): Light · inoperative · May 22, 2025 · N324US · Airbus A320211 · Emergency Lighting
  > SHIP 3224 DISC: DURING SVC CK FOUND ONE OF IN SEAT EMERGENCY PATH LIGHT BURN OUT. ON SEAT 3C. C/A: R/R SEAT MOUNTED EMERGENCY LIGHT AT 3C REF A320 AMM 33-51. OPS NORMAL. (LP: 7384264)
- [SDR DALA2025041102800](https://openairdocs.org/sdr/DALA2025041102800.md): Elec Connector · shorted · Apr 9, 2025 · N324US · Airbus A320211 · Fire Protection System Wiring
  > SHIP 3224 DISC: DURING CROSSBLEED START OF #1 ENG WHEN THRUST WAS BROUGHT UP ON ENG 2 APPROX 35% N1 ENG2 FIRE ECAM POPPED UP WITH FIRE WARNINGS. WHEN THE ENG THRUST WAS REDUCED TO IDLE ECAM DISSAPEARED. C/A: OPENED UP NBR 2 ENG FOR MTC. SHOOK WIRES. FOUND ENG
- [SDR DALA2025020700961](https://openairdocs.org/sdr/DALA2025020700961.md): Radome · damaged · Feb 3, 2025 · N324US · Airbus A320211 · Aerodynamic Fairings
  > SHIP 3224 DISC: DURING BIRD STRIKE INSPECTION, FOUND DAMAGE TO RADOME. C/A: REMOVED AND REPLACED RADOME PER A320 AMM 53-15. (LP: 6701447)
- [SDR DALA2024101310021](https://openairdocs.org/sdr/DALA2024101310021.md): Windshield · damaged · Oct 12, 2024 · N324US · Airbus A320211 · Flight Compartment Windows
  > SHIP 3224 DISC: BIRD STRIKE 6000' CA SIDE WINDSHIELD NO ABNORMAL ENGINE INDICATIONS. C/A: REMOVED CAPTAIN WINDOW AND WINDSHIELD PANE; PER A320 AMMM 56-11 (895623). INSTALLED CAPT WINDOW AND WINDSHIELD PANEL PER A320 AMM 56-11. (LP: 6658136)
- [SDR DALA2024071707217](https://openairdocs.org/sdr/DALA2024071707217.md): Clamp · loose · Jul 12, 2024 · N324US · Airbus A320211 · Pneumatic Distribution System
  > SHIP 3224- PRES/DIV - TO FSD DUE TO LOSS OF PRESSURIZATION (CAB PR EXCESS CAB ALT AND AIR ENG 2 BLEED LEAK ECAM MESSAGES). CORRECTIVE ACTION: FOUND MULTIPLE BLEED LEAKS. PRV CLAMP LOOSE, PRSOV CLAMP, OVER PRESSURE VALVE FLAPPER COVER LOOSE PER A320 AMM 36-11.
- [SDR DALA2024071307098](https://openairdocs.org/sdr/DALA2024071307098.md): Clamp · loose · Jul 12, 2024 · N324US · Airbus A320211 · Air Distribution System
  > SHIP 3224 - PRES/DIV - TO FSD DUE TO LOSS OF PRESSURIZATION (CAB PR EXCESS CAB ALT AND AIR ENG 2 BLEED LEAK ECAM MESSAGES). CORRECTIVE ACTION: PERFORMED SUCCESSFUL CABIN PRESSURE CONTROL TEST AND REFERENCE LOG 5092640 FOR CAUSE. FOUND MULTIPLE BLEED LEAKS. PRV
- [SDR DALA2024052105390](https://openairdocs.org/sdr/DALA2024052105390.md): Door · no test · May 17, 2024 · N324US · Airbus A320211 · Passenger Oxygen System
  > SHIP 3224 DISC: PSU OXY PANEL DIDN'T OPEN ON TEST LOCATION 14ABC. C/A: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 067-0001:2527-01041-02 /001 00003 REPACKED AND TROUBLESHOT OXY PSU REF AMDS 2527-01041- 02. OPS CHECK GOOD. (LP: 0347564)
- [SDR DALA2024032303700](https://openairdocs.org/sdr/DALA2024032303700.md): Test Panel · inoperative · Mar 20, 2024 · N324US · Airbus A320211 · Emergency Equipment
  > SHIP 3224 DISC: DURING SLIDE CHANGE FOUND PROGRAMMING AND TEST PANEL INOP. C/A: R/R PTP TEST PANEL IAW A320 AMM 23-73. ALL CHECKS GOOD. PLACARD AND DECALE REMOVED. (LP: 4392886)
- [SDR DALA2024032303699](https://openairdocs.org/sdr/DALA2024032303699.md): Light · no test · Mar 20, 2024 · N324US · Airbus A320211 · Emergency Lighting
  > SHIP 3224 DISC: SYS EMER LIGHT TEST INOP. C/A: SIGNED OFF WITH LOG #4392886 PLACARD AND DECALE REMOVED. (LP: 4392887)
- [SDR DALA2024010800209](https://openairdocs.org/sdr/DALA2024010800209.md): Unknown · unknown · Jan 5, 2024 · N324US · Airbus A320211 · Hydraulic Indicating System
  > ATB DUE TO FALSE HYDRAULIC OVERHEAT MESSAGES ON ECAM ONLY. YELLOW HYD SYSTEM RESERVOIR OVERHEAT MESSAGE FIRST. THEN REMAINING SYSTEMS AFTER QRH PROCEDURE. CORRECTIVE ACTION: REPLACED SDAC 1 AND 2.
- [SDR DALA2023121810357](https://openairdocs.org/sdr/DALA2023121810357.md): None · none · Dec 17, 2023 · N324US · Airbus A320211 · Standard Practices/Structures
  > SHIP 3224 - ATO - AT 100KTS DUE TO A FLOCK OF SPARROWS IN THE FLIGHT PATH. CORRECTIVE ACTION: NO DAMAGE FOUND. AIRCRAFT RTS.
- [SDR DALA2023070505399](https://openairdocs.org/sdr/DALA2023070505399.md): Unknown · unknown · Jul 4, 2023 · N324US · Airbus A320211 · Passenger Oxygen System
  > SHIP 3224 DURING COMPLETION OF W/C 2527-01041-02, FOUND DMG CONNECTOR AT ROW 26 L/H PSU. CORRECTIVE ACTION: REPLACED HARNESS. OPS CHECK GOOD. (9887956)
- [SDR DALA2023070505398](https://openairdocs.org/sdr/DALA2023070505398.md): Unknown · unknown · Jul 4, 2023 · N324US · Airbus A320211 · Passenger Oxygen System
  > SHIP 3224 DURING TEST PSU AT ROW 26 L/H FAILED TO OPEN. CORRECTIVE ACTION: R/R PSU AT ROW 26 L/H PER A320 AMM 25-25-41. OPS CHK GOOD. (9887955)
- [SDR DALA2023070505397](https://openairdocs.org/sdr/DALA2023070505397.md): Unknown · unknown · Jul 4, 2023 · N324US · Airbus A320211 · Passenger Oxygen System
  > SHIP 3224 DURING TEST PSU AT ROW 25 R/H FAILED TO OPEN. CORRECTIVE ACTION: R/R PSU AT ROW 25 R/H PER A320 AMM 25-25-41. OPS CHK GOOD. (9887954)
- [SDR DALA2023021301103](https://openairdocs.org/sdr/DALA2023021301103.md): None · none · Feb 12, 2023 · N324US · Airbus A320211 · Door Warning System
  > SHIP 3224 DOOR R FWD EMER EXIT ECAM MSG DISPLAYED ON DEPARTURE. CORRECTIVE ACTION: FOUND DOOR PANEL OVER DOOR OPEN HANDLE PULLED OUT CAUSING MSG, RE-SECURED PNL MSG CLEARED. (4192226)
- [SDR DALA2023010400051](https://openairdocs.org/sdr/DALA2023010400051.md): Proximity Sensor · faulted · Dec 31, 2022 · N324US · Airbus A320211 · Door Warning System
  > R2 DOOR SHOWS ARMED ON DOOR PAGE DOOR IS PROPERLY DISARMED AND PINNED. IT STILL SHOWS ARMED. R & R 17WV2 PROXIMITY SENSOR IAW AMM 52-71. OPS CHECK GOOD.
- [SDR DALA2023010900112](https://openairdocs.org/sdr/DALA2023010900112.md): Spar · corroded · Dec 21, 2022 · N324US · Airbus A320211 · Wing Spar
  > SHIP 3224 CORROSION IN FASTENER HOLE #55 COMMON TO LH WING AFT SPAR. CORRECTIVE ACTION: COMPLIED WITH ERA 604693-14AD SECTION I.
- [SDR DALA2022121308030](https://openairdocs.org/sdr/DALA2022121308030.md): Bulkhead · cracked · Dec 11, 2022 · N324US · Airbus A320211 · Fuselage Main, Bulkhead
  > SHIP 3224 FUSELAGE / BULKHEADS / FR35 AT STGR30LH / CRACKS- SECTION IV INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ER/A 599118-14 REV A SECTION IV. (2534907)
- [SDR DALA2022121308029](https://openairdocs.org/sdr/DALA2022121308029.md): Bulkhead · cracked · Dec 11, 2022 · N324US · Airbus A320211 · Fuselage Main, Bulkhead
  > SHIP 3224 FUSELAGE / BULKHEADS / FR35 AT STGR30LH / CRACKS SECTION III INSPECTION. CORRECTIVE ACTION: ACCOMPLISHED ERA ER/A 599118-14 REV A SECTION III. (2534904)
- [SDR DALA2022121308028](https://openairdocs.org/sdr/DALA2022121308028.md): None · none · Dec 11, 2022 · N324US · Airbus A320211 · Fuselage Main, Bulkhead
  > SHIP 3224 NEED TO COMPLY WITH ER/A 599118-14 SECTION II CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH. (2534891)
- [SDR DALA2022120907947](https://openairdocs.org/sdr/DALA2022120907947.md): Unknown · none · Dec 8, 2022 · N324US · Airbus A320211 · Fuselage Main, Bulkhead
  > SHIP 3224 NEED TO COMPLY WITH CRACK INSPECTION ER/A 599120-14 REV A. CORRECTIVE ACTION: COMPLIED WITH ERA. (2530520)
- [SDR DALA2022120907946](https://openairdocs.org/sdr/DALA2022120907946.md): Frame · none · Dec 8, 2022 · N324US · Airbus A320211 · Fuselage Main, Bulkhead
  > SHIP 3224 FUSELAGE / BULKHEADS / FR35 AT STGR30RH / CRACKS / #6 HOLE INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 599120-14 REV A. (2530500)
- [SDR DALA2022120707861](https://openairdocs.org/sdr/DALA2022120707861.md): Floorbeam · cracked · Dec 6, 2022 · N324US · Airbus A320211 · Fuselage Main, Floor Beam
  > FRONT SPAR AT FRAME 36 FLOORBEAM & VERTICAL STIFFENER CRACKED. COMPLIED WITH ERA 599001-14 REV A SECTION II. (2527658)
- [SDR DALA2022062104318](https://openairdocs.org/sdr/DALA2022062104318.md): Support Bracket · cracked · Jun 20, 2022 · N324US · Airbus A320211 · Fuselage Main, Keel
  > SHIP 3224 CRACK SUPPORT BRACKET LOCATED BETWEEN FR45 TO FR46 LH SIDE KEEL BEAM AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-35-11. (2286173)
- [SDR DALA2022062004282](https://openairdocs.org/sdr/DALA2022062004282.md): Skin · corroded · Jun 19, 2022 · N324US · Airbus A320211 · Wing Spar
  > SHIP 3224 CORROSION UPPER SURFACE EXTERNAL SKIN REAR SPAR AREA FR24 TO FR26 ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 599270-14 REV ORIGINAL. (2284870)
- [SDR DALA2022062004281](https://openairdocs.org/sdr/DALA2022062004281.md): Skin · corroded · Jun 19, 2022 · N324US · Airbus A320211 · Wing Spar
  > SHIP 3224 CORROSION TRAILING EDGE REAR SPAR UPPER SKIN LOC. BTW RIB 24 TO RIB26 ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 599270-14 REV. ORIGINAL. (2284205)
- [SDR DALA2022062004280](https://openairdocs.org/sdr/DALA2022062004280.md): Frame · cracked · Jun 19, 2022 · N324US · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3224 CRACK INDICATION ON FRAME 35 RH AT LEVEL STRINGER 30 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 599120-14AD REV ORIGINAL. (2284931)
- [SDR DALA2022062004279](https://openairdocs.org/sdr/DALA2022062004279.md): Frame · cracked · Jun 19, 2022 · N324US · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3224 CRACK INDICATION ON EXTERNAL SKIN FRAME 35 RH AT LEVEL STRINGER 30 AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 599120-14AD REV ORIGINAL. (2284925)
- [SDR DALA2022062004278](https://openairdocs.org/sdr/DALA2022062004278.md): Frame · cracked · Jun 19, 2022 · N324US · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3224 CRACK INDICATION ON FRAME 35 LH AT LEVEL STRINGER 30 HOLE 6 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 599118-14AD REV ORIGINAL. (2284917)
- [SDR DALA2022062004277](https://openairdocs.org/sdr/DALA2022062004277.md): Frame · cracked · Jun 19, 2022 · N324US · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3224 CRACK INDICATION ON EXTERNAL SKIN FRAME 35 LH AT LEVEL STRINGER 30 HOLE 16 AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 599118-14AD REV ORIGINAL. (2284894)
- [SDR DALA2022062004287](https://openairdocs.org/sdr/DALA2022062004287.md): Attach Fitting · corroded · Jun 18, 2022 · N324US · Airbus A320211 · Elevator, Spar/Rib
  > SHIP 3224 CORROSION BUSHING ATTACH FITTING ELEVATOR HINGE 4 ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED LUGS END INSTALLED BUSHINGS OF HINGE FITTING #4 OF L/H ELEVATOR PER A320 SRM 55-26-41 AND 55-26-41. (2283881)
- [SDR DALA2022062004286](https://openairdocs.org/sdr/DALA2022062004286.md): Attach Fitting · corroded · Jun 18, 2022 · N324US · Airbus A320211 · Elevator, Spar/Rib
  > SHIP 3224 CORROSION BUSHING ATTACH FITTING ELEVATOR HINGE 6 ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED LUGS AND REPLACED BUSHINGS OF HINGE FITTING #6 OF ELEVATOR RH AS PER A320 SRM 55-26-41. (2283878)
- [SDR DALA2022062004285](https://openairdocs.org/sdr/DALA2022062004285.md): Attach Fitting · corroded · Jun 18, 2022 · N324US · Airbus A320211 · Elevator, Spar/Rib
  > SHIP 3224 CORROSION BUSHING ATTACH FITTING ELEVATOR HINGE 1 ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPAIRED LUGS OF HINGE FITTING #1 OF ELEVATOR RH PER A320 SRM 55-26-41. (2283871)
- [SDR DALA2022062004284](https://openairdocs.org/sdr/DALA2022062004284.md): Anchor Fitting · corroded · Jun 18, 2022 · N324US · Airbus A320211 · Wing, Attach Fittings
  > SHIP 3224 CORROSION RETRACTION ACTUATOR ATTACHMENT FITTINGS BUSHING ON RH MAIN LANDING GEAR. CORRECTIVE ACTION: PERFORMED TIME LIMITED REPAIR ON MLG RETRACTION JACK ANCHORAGE FITTING RH WING PER A320 SRM 57-26-13. (2283929)
- [SDR DALA2022061704236](https://openairdocs.org/sdr/DALA2022061704236.md): Anchor Fitting · corroded · Jun 17, 2022 · N324US · Airbus A320211 · Wing, Attach Fittings
  > SHIP 3224 CORROSION RETRACTION ACTUATOR ATTACHMENT FITTINGS BUSHING AT LH MAIN LANDING GEAR. CORRECTIVE ACTION: PERFORMED TIME LIMITS REPAIR ON MLG RETRACTION JACK ANCHORAGE FITTING LH WING, AS PER A320 SRM 57-26-13. (2281405)
- [SDR DALA2022061704238](https://openairdocs.org/sdr/DALA2022061704238.md): Bulkhead · none · Jun 16, 2022 · N324US · Airbus A320211 · Fuselage Main, Bulkhead
  > SHIP 3224 NEED TO COMPLY WITH DTA MONITOR INSPECTION LOG REFERENCE ER/A 519920-14 SECTION II CRACKS IN BULKHEAD. CORRECTIVE ACTION: COMPLIED WITH ERA 519920-14 SECTION II. (2281105)
- [SDR DALA2022061704232](https://openairdocs.org/sdr/DALA2022061704232.md): Skin · corroded · Jun 16, 2022 · N324US · Airbus A320211 · Fuselage Floor Panel
  > SHIP 3224 CORROSION INTERNAL SKIN LOCATED FR 67 AND STR 30L TO STR 31L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 599306-14 REV. ORIGINAL. (2280627)
- [SDR DALA2022061704239](https://openairdocs.org/sdr/DALA2022061704239.md): Bulkhead · none · Jun 14, 2022 · N324US · Airbus A320211 · Fuselage Main, Bulkhead
  > SHIP 3224 NEED TO COMPLY WITH ER/A 599118-14 SECTION II CRACK ON BULKHEAD. CORRECTIVE ACTION: COMPLIED WITH ER/A 599118-14 SECTION II. (2281234)
- [SDR DALA2022061504187](https://openairdocs.org/sdr/DALA2022061504187.md): Spar · cracked · Jun 14, 2022 · N324US · Airbus A320211 · Wing, Center Box
  > SHIP 3224 CRACK INDICATION FOUND ON OPEN HOLE 1 POSITION 2 OF THE FRONT SPAR VERTICAL STR AND THE FLOOR BEAM FR 36. (Y765). CORRECTIVE ACTION: COMPLIED WITH ERA 599001-14AD REV ORIGINAL. (2277784)
- [SDR DALA2022061504186](https://openairdocs.org/sdr/DALA2022061504186.md): Spar · cracked · Jun 14, 2022 · N324US · Airbus A320211 · Wing, Center Box
  > SHIP 3224 CRACK INDICATION ON DOOR IN FWD CARGO COMPARTMENT (1 EA) (CRACK INDICATION FOUND ON OPEN HOLE 1 POSITION 4 OF THE FRONT SPAR VERTICAL STR AND THE FLOOR BEAM FR 36. (-Y254). CORRECTIVE ACTION: COMPLIED WITH ER/A 599001-14AD REV. ORIGINAL. (2277782)
- [SDR DALA2022061504185](https://openairdocs.org/sdr/DALA2022061504185.md): Spar · cracked · Jun 14, 2022 · N324US · Airbus A320211 · Wing, Center Box
  > SHIP 3224 CRACK INDICATION FOUND ON OPEN HOLE 2 POSITION 5 OF THE FRONT SPAR VERTICAL STR AND THE FLOOR BEAM FR 36. (-Y765). CORRECTIVE ACTION: COMPLIED WITH ERA 599001-14AD REV ORIGINAL. (2277776)
- [SDR DALA2022061504184](https://openairdocs.org/sdr/DALA2022061504184.md): Spar · cracked · Jun 14, 2022 · N324US · Airbus A320211 · Wing, Center Box
  > SHIP 3224 CRACK INDICATION FOUND ON OPEN HOLE 2 POSITION 4 OF THE FRONT SPAR VERTICAL STR AND THE FLOOR BEAM FR 36. (-Y254). CORRECTIVE ACTION: COMPLIED WITH ERA 599001-14AD REV.ORIGINAL. (2277774)
- [SDR DALA2022061504183](https://openairdocs.org/sdr/DALA2022061504183.md): Spar · cracked · Jun 14, 2022 · N324US · Airbus A320211 · Wing, Center Box
  > SHIP 3224 CRACK INDICATION FOUND ON OPEN HOLE 1 POSITION 3 OF THE FRONT SPAR VERTICAL STR AND THE FLOOR BEAM FR 36. (Y254). CORRECTIVE ACTION: COMPLIED WITH ERA 599001-14AD REV. ORIGINAL. (2277766)
- [SDR DALA2022061504182](https://openairdocs.org/sdr/DALA2022061504182.md): Spar · cracked · Jun 14, 2022 · N324US · Airbus A320211 · Wing, Center Box
  > SHIP 3224 CRACK INDICATION FOUND ON OPEN HOLE 2 POSITION 1 OF THE FRONT SPAR VERTICAL STR AND THE FLOOR BEAM FR 36. (Y1292). CORRECTIVE ACTION: COMPLIED WITH ERA 599001-14AD REV. ORIGINAL. (2277762)
- [SDR DALA2022061504181](https://openairdocs.org/sdr/DALA2022061504181.md): Spar · cracked · Jun 14, 2022 · N324US · Airbus A320211 · Wing, Center Box
  > SHIP 3224 CRACK INDICATION FOUND ON OPEN HOLE 2 POSITION 2 OF THE FRONT SPAR VERTICAL STR AND THE FLOOR BEAM FR 36. (Y765). CORRECTIVE ACTION: COMPLIED WITH ERA 599001-14AD REV ORIGINAL. (2277757)
- [SDR DALA2022061504180](https://openairdocs.org/sdr/DALA2022061504180.md): Spar · cracked · Jun 14, 2022 · N324US · Airbus A320211 · Wing, Center Box
  > SHIP 3224 CRACK INDICATION FOUND ON OPEN HOLE 1 POSITION 5 OF THE FRONT SPAR VERTICAL STR AND THE FLOORBEAM FR 36. (-Y765). CORRECTIVE ACTION: COMPLIED WITH ERA 599001-14AD REV.ORIGINAL. (2277753)
- [SDR DALA2022061304116](https://openairdocs.org/sdr/DALA2022061304116.md): Stringer · corroded · Jun 10, 2022 · N324US · Airbus A320211 · Fuselage Floor Panel
  > SHIP 3224 CORROSION STRINGER 39R BETWEEN FR 64 TO FR 66 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11. (2272277)
- [SDR DALA2022120707860](https://openairdocs.org/sdr/DALA2022120707860.md): None · none · Jun 9, 2022 · N324US · Airbus A320211 · Standard Practices/Structures
  > SHIP 3224 PLEASE COMPLY WITH ER/A 599001-14 SECTION II (CRACK). CORRECTIVE ACTION: COMPLIED WITH. (2271247)
- [SDR DALA2022060904045](https://openairdocs.org/sdr/DALA2022060904045.md): Damper · failed insp · Jun 8, 2022 · N324US · Airbus A320211 · Passenger/Crew Doors
  > SHIP 3224 PASSENGER CREW DOOR 832 DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DOOR DAMPER. OPS TEST GOOD. (2269801)

Next page: https://openairdocs.org/deregistered/N324US-2026-01-14/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 = 'N324US' AND deregistration_id = 'N324US-2026-01-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N324US-2026-01-14/reports

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