# Service difficulty reports: N184US

A list on [N184US](https://openairdocs.org/aircraft/N184US.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 8 · 386 reports

- [SDR AALA202610054320](https://openairdocs.org/sdr/AALA202610054320.md): Warning Light · false indication · Oct 2, 2026 · N184US · Airbus A321211 · Door Warning System
  > AIRCRAFT WAS NOT GROUNDED: AFT LEFT SIDE PASSENGER DOOR SHOWING OPEN INDICATION WITH DOOR CLOSED AND LOCKED. MAINTENANCE REPLACED PANEL, WARNING LIGHT PER AMM 52-73-21. THIS CLEARS MEL 52-10A.
- [SDR AALA202609166520](https://openairdocs.org/sdr/AALA202609166520.md): Bottle · low pressure · Sep 14, 2026 · N184US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR ASSIST BOTTLE NEEDS SERVICING. MAINTENANCE SERVICED ASSIST BOTTLE.
- [SDR AALA202609070956](https://openairdocs.org/sdr/AALA202609070956.md): Flashlight · no test · Sep 5, 2026 · N184US · Airbus A321211 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHT AT JUMP SEAT 1L DOES NOT SHOW THAT IT IS CHARGING - MAINTENACE REPLACED FLASHLIGHT PER AMM 25-63-00
- [SDR AALA202608188620](https://openairdocs.org/sdr/AALA202608188620.md): Bypass Valve · overheated · Aug 15, 2026 · N184US · Airbus A321211 · Cabin Cooling System
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO THE FLIGHT CREW REPORTING WITH THE RIGHT PACK ON MEL THAT DURING CLIMBOUT THE LEFT PACK OVERHEATED RESULTING IN THE LOSS OF THE REMAING PACK LEADING TO A LACK OF PRESSURIZ
- [SDR AALA202607301104](https://openairdocs.org/sdr/AALA202607301104.md): Seal · broken · Jul 28, 2026 · N184US · Airbus A321211 · Emergency Equipment
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS LEFT BACK FLASHLIGHT SEAL BROKEN ON 4L. MAINTENANCE REPLACED FLASHLIGHT AND INSTALLED A NEW TAMPER PROOF SEAL ON 4L POSITION PER AMM 25-65-00.
- [SDR AALA202607098564](https://openairdocs.org/sdr/AALA202607098564.md): Engine · stalled · Jul 5, 2026 · N184US · Airbus A321211 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT DUE TO THE FLIGHT CREW REPORTING THAT ON ROTATION THE RIGHT ENGINE EXCEEDED EGT FOR APPROX 1 MINUTE AFTER 3 LOUD BANGS WERE HEARD. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO
- [SDR AALA202604274909](https://openairdocs.org/sdr/AALA202604274909.md): Filter · dirty · Apr 26, 2026 · N184US · Airbus A321211 · Air Distribution System
  > AIRCRAFT WAS GROUNDED: 2 MINUTES FROM LANDING THERE WAS A MUSTY SOCK SMELL ON THE FLIGHT DECK. FLIGHT ATTENDANTS SAID THEY DIDN'T SMELL IT BUT THERE WAS A VERY STRONG SMELL OF MARIJUANA IN THE CABIN THAT MASKED ANY OTHER ODORS. MAINTENANCE ACCOMPLISHED JOB CAR
- [SDR AALA202604202137](https://openairdocs.org/sdr/AALA202604202137.md): Bottle · low pressure · Apr 14, 2026 · N184US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.
- [SDR AALA202602183563](https://openairdocs.org/sdr/AALA202602183563.md): Battery · no test · Feb 17, 2026 · N184US · Airbus A321211 · Emergency Lighting
  > AIRCRAFT WAS NOT GROUNDED: L1 DOOR EMERGENCY LIGHT POWER SUPPLY UNIT BATTERY FAILED TEST. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38.
- [SDR AALA202601062470](https://openairdocs.org/sdr/AALA202601062470.md): Wire · disconnected · Jan 5, 2026 · N184US · Airbus A321211 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: WALL MOUNTED EMERGENCY EXIT MARKER (90WL8) INOPERATIVE AT THE R4 DOOR. MAINTENANCE FOUND THE WIRES NOT CONNECTED TO THE LED, CONNECTED THE WIRE ANDAND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
- [SDR AALA202601063780](https://openairdocs.org/sdr/AALA202601063780.md): Wire · misinstalled · Jan 5, 2026 · N184US · Airbus A321211 · Light System Wiring
  > AIRCRAFT WAS NOT GROUNDED: WALL MOUNTED EMERGENCY EXIT MARKER (90WL7) INOPERTIVE AT THE L4 DOOR. MAINTENANCE FOUND WIRES INCORRECTLY CONNECTED TO THE LED, CONNECTED THE WIRES CORRECTLY AND ACCOMPLISHED AA SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.
- [SDR AALA202512090062](https://openairdocs.org/sdr/AALA202512090062.md): Bottle · leaking · Dec 8, 2025 · N184US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT WAS GROUNDED: R1 DOOR WILL NOT FULLY OPEN TO GUST LOCK POSITION. MAINTENANCE FOUND THE R1 DOOR R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW, REPLACED THE R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-01. A SATISFACTORY
- [SDR AALA202512087650](https://openairdocs.org/sdr/AALA202512087650.md): Life Line · misinstalled · Dec 4, 2025 · N184US · Airbus A321211 · Emergency Equipment
  > AIRCRAFT IN BASE MAINTENANCE: R1 SLIDE ARM INTERMITTENT. MAINTENANCE FOUND THE MOORING LINE INCORRECTLY INSTALLED ON THE GIRT BAR, REINSTALLED MOORING LINE ON GIRT BAR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-62-44.
- [SDR AALA202512059766](https://openairdocs.org/sdr/AALA202512059766.md): Speaker · no test · Dec 4, 2025 · N184US · Airbus A321211 · Emergency Equipment
  > AIRCRAFT IN BASE MAINTENANCE: STATION 3 HAS NO ALARM NOISE, THE VISIONAL ALERT WORKS BUT NO AURAL WARNING. MAINTENANCE REPLACED THE LOUDSPEAKER PER AMM 23-73-51 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY EVACUATION SIGNALING SYSTEM PER
- [SDR AALA202512055598](https://openairdocs.org/sdr/AALA202512055598.md): Speaker · no test · Dec 4, 2025 · N184US · Airbus A321211 · Emergency Equipment
  > AIRCRAFT IN BASE MAINTENANCE: STATION 2 HAS NO ALARM NOISE, THE VISIONAL ALERT WORKS BUT NO AURAL WARNING. MAINTENANCE REPLACED THE LOUDSPEAKER PER AMM 23-73-51 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY EVACUATION SIGNALING SYSTEM PER
- [SDR AALA202512043918](https://openairdocs.org/sdr/AALA202512043918.md): Diaphragm · leaking · Dec 2, 2025 · N184US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER DIAPHRAGM PER AMM 52-10-00.
- [SDR AALA202511254342](https://openairdocs.org/sdr/AALA202511254342.md): Boss · low pressure · Nov 24, 2025 · N184US · Airbus A321211 · Service Doors
  > AIRCRAFT IN BASE MAINTENANCE: FORWAQRD RIGHT PASSENGER / CREW DOOR 841 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
- [SDR AALA202511202545](https://openairdocs.org/sdr/AALA202511202545.md): Skin Panel · corroded · Nov 19, 2025 · N184US · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL OVERHANG LOWER SURFACE BETWEEN RIB 7A AND RIB 9. REPAIRED SKIN PANEL PER EA 368796.
- [SDR AALA202511195066](https://openairdocs.org/sdr/AALA202511195066.md): Skin Panel · corroded · Nov 18, 2025 · N184US · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL OVERHANG LOWER SURFACE AT LEVEL RIB 15. REPAIRED SKIN PANEL PER EA 368796.
- [SDR AALA202511175049](https://openairdocs.org/sdr/AALA202511175049.md): Fitting · cracked · Nov 14, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK CORNER FITTING OPEN HOLE L6 AT FR 36 AND +Y1292. REPLACED CORNER FITTING PER EA 367961
- [SDR AALA202511135613](https://openairdocs.org/sdr/AALA202511135613.md): Skin Panel · corroded · Nov 12, 2025 · N184US · Airbus A321211 · Wing, Plate/Skin
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT RIB 5 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 368796.
- [SDR AALA202511130896](https://openairdocs.org/sdr/AALA202511130896.md): Shear Plate · cracked · Nov 10, 2025 · N184US · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.
- [SDR AALA202511131574](https://openairdocs.org/sdr/AALA202511131574.md): Shear Plate · cracked · Nov 10, 2025 · N184US · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKD AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.
- [SDR AALA202511144818](https://openairdocs.org/sdr/AALA202511144818.md): Support Frame · excess play · Nov 9, 2025 · N184US · Airbus A321211 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #2 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.
- [SDR AALA202511148531](https://openairdocs.org/sdr/AALA202511148531.md): Support Frame · excess play · Nov 9, 2025 · N184US · Airbus A321211 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #1 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.
- [SDR AALA202511142844](https://openairdocs.org/sdr/AALA202511142844.md): Support Frame · excess play · Nov 9, 2025 · N184US · Airbus A321211 · Ailerons
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #3 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.
- [SDR AALA202511070202](https://openairdocs.org/sdr/AALA202511070202.md): Pressure Deck · cracked · Nov 6, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE AT FR 36 AND +Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 367961
- [SDR AALA202511073472](https://openairdocs.org/sdr/AALA202511073472.md): Pressure Deck · cracked · Nov 6, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED CENTER FUSELAGE PRESSURE DECK MEMEBRANE AT FR 36 AND -Y1292. REPAIRED PRESSURE DECK MEMBRANE PER EA 367961
- [SDR AALA202511074270](https://openairdocs.org/sdr/AALA202511074270.md): Fitting · cracked · Nov 6, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.
- [SDR AALA202511063672](https://openairdocs.org/sdr/AALA202511063672.md): Door Frame · cracked · Nov 5, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT FR 16 LEFT AND #7 DOORSTOP FITTING. REPAIRED FRAME PER EA 367767.
- [SDR AALA202511067238](https://openairdocs.org/sdr/AALA202511067238.md): Door Frame · cracked · Nov 5, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT FR 16 RIGHT AND #5 DOORSTOP FITTING. REPAIRED FRAME PER EA 367781.
- [SDR AALA202511066482](https://openairdocs.org/sdr/AALA202511066482.md): Support Frame · excess play · Oct 31, 2025 · N184US · Airbus A321211 · Wing Main, Frame Structure
  > AIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #3 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.
- [SDR AALA202510214204](https://openairdocs.org/sdr/AALA202510214204.md): Window Frame · cracked · Oct 20, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0 LEFT. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.
- [SDR AALA202510218031](https://openairdocs.org/sdr/AALA202510218031.md): Window Frame · cracked · Oct 20, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING RIGH HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0 RIGHT. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.
- [SDR AALA202510206400](https://openairdocs.org/sdr/AALA202510206400.md): Fitting · corroded · Oct 18, 2025 · N184US · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23L. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.
- [SDR AALA202510203245](https://openairdocs.org/sdr/AALA202510203245.md): Floorbeam · corroded · Oct 18, 2025 · N184US · Airbus A321211 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM INBOARD UPPER SECTION CONNECTING SPLICE AT FR 66 AND +Y1292. REPLACED SECTION CONNECTING SPLICE PER SRM 51-72-11.
- [SDR AALA202510202957](https://openairdocs.org/sdr/AALA202510202957.md): Door Sill · corroded · Oct 18, 2025 · N184US · Airbus A321211 · Fuselage Main, Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 66 AND FR 68 AT S23L. REPLACED SILL PER SRM 51-72-11.
- [SDR AALA202510207877](https://openairdocs.org/sdr/AALA202510207877.md): Seat Track · corroded · Oct 18, 2025 · N184US · Airbus A321211 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SEAT RAIL BETWEEN FR 64 AND FR 66 AT +Y1292. REPLACED SEAT RAIL PER SRM 51-72-11.
- [SDR AALA202510158950](https://openairdocs.org/sdr/AALA202510158950.md): Plate · loose · Oct 12, 2025 · N184US · Airbus A321211 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT DOOR 843 GRIP PLATE IS LOOSE. MAINTENANCE TIGHTENED GRIP PLATE PER AMM 52-22-22.
- [SDR AALA202510104705](https://openairdocs.org/sdr/AALA202510104705.md): Floor Support · corroded · Oct 8, 2025 · N184US · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION TO PASSENGER CABIN FLOOR SUPPORT BETWEEN FR 12 AND FR 24 AT -Y254. REPLACED FLOOR SUPPORT PER SRM 51-72-11.
- [SDR AALA202510148583](https://openairdocs.org/sdr/AALA202510148583.md): Floorbeam · elongated · Oct 7, 2025 · N184US · Airbus A321211 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES LOCATED ON FR24 INBOARD SPLICE FLOOR BEAM -Y254 FWD GALLEY AREA (0.222 IN). MAINTENANCE REPLACED SPLICE LOCAED ON FR24 INBOARD FLOOR BEAM -Y254 FWD GALLEY AREA IAW A321 51-42-11-801, SRM 51-72-11-911-001 AND DWG D5
- [SDR AALA202510131809](https://openairdocs.org/sdr/AALA202510131809.md): Floorbeam · worn · Oct 7, 2025 · N184US · Airbus A321211 · Fuselage Main, Floor Beam
  > AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR BEAM OUTBOARD SPLICE HAS WORN / ELONGATED HOLES AT FR 24 AND -Y254. REPLACED SPLICE PER SRM 51-72-11.
- [SDR AALA202510132947](https://openairdocs.org/sdr/AALA202510132947.md): Shackle · worn · Oct 7, 2025 · N184US · Airbus A321211 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON AFT ATTACH FITTING SHACKLE WORN AT PYLON RIB 10. REPLACED SHACKLE PER AMM 54-51-17.
- [SDR AALA202510135698](https://openairdocs.org/sdr/AALA202510135698.md): Shackle · worn · Oct 7, 2025 · N184US · Airbus A321211 · Nacelle/Pylon, Main Frame
  > AIRCRAFT IN BASE MAINTENANCE: LEFT PYLON FORWARD INBOARD ATTACH FITTING SHACKLE WORN AT PYLON RIB 4. REPLACED SHACKLE PER AMM 54-51-17.
- [SDR AALA202510088165](https://openairdocs.org/sdr/AALA202510088165.md): Attach Fitting · corroded · Oct 7, 2025 · N184US · Airbus A321211 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) RIGHT HAND POSITION AT RIB 4. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-400-001-A
- [SDR AALA202510083234](https://openairdocs.org/sdr/AALA202510083234.md): Fitting · cracked · Oct 7, 2025 · N184US · Airbus A321211 · Fuselage Miscellaneous Structure
  > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FITTING AT FR 2 AND -Y 330. REPLACED FITTING PER SRM 51-42-11.
- [SDR AALA202510109137](https://openairdocs.org/sdr/AALA202510109137.md): Bottle · no test · Oct 5, 2025 · N184US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION ON DOOR DAMPER AND EMERGENCY OPERATION CYLINDER INPASSENGER CREW DOOR 831 AT FWD GALLEY AREA. MAINTENANCE REMOVED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IN PASSENGER CREW DOOR 841 P/N: FE240-0
- [SDR AALA202510100653](https://openairdocs.org/sdr/AALA202510100653.md): Bottle · no test · Oct 5, 2025 · N184US · Airbus A321211 · Passenger/Crew Doors
  > AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION ON DOOR DAMPER AND EMERGENCY OPERATION CYLINDER INPASSENGER CREW DOOR 841 AT FWD GALLEY AREA. MAINTENANCE REMOVED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IN PASSENGER CREW DOOR 841 P/N: FE240-0
- [SDR AALA202510064841](https://openairdocs.org/sdr/AALA202510064841.md): Attach Fitting · corroded · Oct 4, 2025 · N184US · Airbus A321211 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) OUTBOARD ON PYLON OUTBOARD SIDE. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-000-001-A AND AMM 54-51-17-400-001-A.
- [SDR AALA202510065770](https://openairdocs.org/sdr/AALA202510065770.md): Attach Fitting · corroded · Oct 4, 2025 · N184US · Airbus A321211 · Nacelle/Pylon, Attach Fittings
  > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON FORWARD ATTACH FITTING (SHACKLE) OUTBOARD ON PYLON INBOARD SIDE. REPLACED PYLON ATTACH FITTING PER AMM 54-51-17-000-001-A AND AMM 54-51-17-400-001-A.

Next page: https://openairdocs.org/aircraft/N184US/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 = 'N184US' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N184US/reports

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