# Service difficulty reports: N322US, cancelled Mar 2, 2023

A list on [N322US, cancelled Mar 2, 2023](https://openairdocs.org/deregistered/N322US-2023-03-02.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 3 · 101 reports

- [SDR DALA2019121007214](https://openairdocs.org/sdr/DALA2019121007214.md): Light · damaged · Dec 10, 2019 · N322US · Airbus A320211 · Emergency Lighting
  > EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATION 1C, REPLACED LIGHT FIXTURE AT SEAT 1C
- [SDR DALA2018081095007](https://openairdocs.org/sdr/DALA2018081095007.md): Control Valve · failed · Aug 9, 2018 · N322US · Airbus A320211 · Steering Unit
  > EMERGENCY DECLARED FOR A NOSE WHEEL STEERING FAULT. REPLACED THE NOSE WHEEL STEERING SERVO CONTROL VALVE AND CONNECTOR 6GC IAW AMM. OPS AND LEAK CHECKED GOOD.
- [SDR DALA2018071904574](https://openairdocs.org/sdr/DALA2018071904574.md): Skin · damaged · Jul 17, 2018 · N322US · Airbus A320211 · Fuselage Main, Plate/Skin
  > PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOWER FUSELAGE FRAME 72 TO FRAME 73, STR 24L TO 25L PER PRI 570056-14. COMPLIED WITH PRI/ERA 5700556-14 REV O.
- [SDR DALA2018071604504](https://openairdocs.org/sdr/DALA2018071604504.md): Damper · unserviceable · Jul 14, 2018 · N322US · Airbus A320211 · Passenger/Crew Doors
  > CREW DOOR DAMPER 842, AFT GALLEY AREA, DOESN'T PASS CHECK. REMOVED AND REPLACED DOOR DAMPER AND EMERGENCY CYLINDER. CHECKS GOOD.
- [SDR DALA2018071604502](https://openairdocs.org/sdr/DALA2018071604502.md): Rod End · corroded · Jul 14, 2018 · N322US · Airbus A320211 · Autopilot System
  > CORROSION ON TRAILING EDGE ROD END OF YAW DAMPER. REMOVED, REPLACED AND FUNCTIONAL CHECK.
- [SDR DALA2018071604501](https://openairdocs.org/sdr/DALA2018071604501.md): Slide · deformed · Jul 14, 2018 · N322US · Airbus A320211 · Escape Slide
  > SLIDE DEFORMATION PASSENGER CREW DOOR 832, AFT GALLEY AREA. REMOVED AND REPLACED SLIDE. CHECKS GOOD.
- [SDR DALA2018060903916](https://openairdocs.org/sdr/DALA2018060903916.md): Wire · cut · Jun 8, 2018 · N322US · Airbus A320211 · Escape Slide
  > FOUND L2 SLIDE WIRES CUT. REMOVED AND REPLACED L2 DOOR SLIDE ASSEMBLY.
- [SDR DALA2017091106815](https://openairdocs.org/sdr/DALA2017091106815.md): Power Supply · inoperative · Sep 9, 2017 · N322US · Airbus A320211 · Emergency Lighting
  > EMERGENCY LIGHT FAILED, INT LOADS AFTL, EXT LOADS AFTL & BATTERY AFTL ILLUMINATED. REPLACED THE EPSU 13WL AND SLIDE.
- [SDR DALA2017052404232](https://openairdocs.org/sdr/DALA2017052404232.md): Battery Pack · inoperative · May 24, 2017 · N322US · Airbus A320211 · Emergency Lighting
  > DURING A SERVICE CHECK, FOUND THE AFT LT BATTERY PACK FOR EMERGENCY LIGHTS INOPERATIVE, REPLACED THE BATTERY PACK.
- [SDR DALA2019070704066](https://openairdocs.org/sdr/DALA2019070704066.md): Skin · not reported · Mar 7, 2017 · N322US · Airbus A320211 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT GOGO WI-FI FWD ATG4 ANTENNA, FR 25 TO FR 26, S-43L TO S-42R; SECTION II PERMANENT REPAIR II PER ER/A 539169-14AD REV.B.
- [SDR DALA2017020301036](https://openairdocs.org/sdr/DALA2017020301036.md): Vent · corroded · Feb 3, 2017 · N322US · Airbus A320211 · Fuselage Main, Plate/Skin
  > LAVATORY VENT HAS CORROSION AND CRACK ON SKIN BETWEEN FR69 AND FR70, S31R AND S32R. SEE NR FOR ADDITIONAL INFORMATION 001-0001:2000-2001/001 00008 SEALED AND PAINTED AND CLOSED RT AFT BULKHEAD PANEL. REPAIRED IAW SRM 53-41-11.
- [SDR DALA2016072805619](https://openairdocs.org/sdr/DALA2016072805619.md): Fitting · damaged · Jul 27, 2016 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DAMAGE ON RIGHT CRUCIFORM, REPAIRED IAW ER/A 548323-14AD REV A FOR WING CENTER CRUCIFORM FITTING.
- [SDR DALA2016072105469](https://openairdocs.org/sdr/DALA2016072105469.md): Frame · damaged · Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, Frame
  > DAMAGE ON FRAME 24, STRINGER 6R ON THE AFT SIDE OF THE FRAME. CUTOUT DAMAGE AND REPAIRED IAW ERA 548700-14.
- [SDR DALA2016072105468](https://openairdocs.org/sdr/DALA2016072105468.md): Frame · cracked · Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, Frame
  > CRACK INDICATIONS AT FRAME 16. COMPLIED WITH FINAL ERA 548219-14AD REV ORIGINAL.
- [SDR DALA2016072105467](https://openairdocs.org/sdr/DALA2016072105467.md): Box Beam · not reported · Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, Structure
  > CENTER FUSELAGE RT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548164-14AD.
- [SDR DALA2016072105466](https://openairdocs.org/sdr/DALA2016072105466.md): Box Beam · not reported · Jul 20, 2016 · N322US · Airbus A320211 · Fuselage Main, Frame
  > CENTER FUSELAGE LT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548129-14AD.
- [SDR DALA2016111808959](https://openairdocs.org/sdr/DALA2016111808959.md): Stringer · corroded · Jul 18, 2016 · N322US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 33 AND 34. CORROSION WAS CUTOUT AND REPAIRED IAW SRM.
- [SDR DALA2016111808958](https://openairdocs.org/sdr/DALA2016111808958.md): Stringer · corroded · Jul 18, 2016 · N322US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON STRINGER 43L BETWEEN FRAMES 33 AND 34. CORROSION WAS CUTOUT AND REPAIRED IAW SRM.
- [SDR DALA2016071205309](https://openairdocs.org/sdr/DALA2016071205309.md): Skin · damaged · Jul 10, 2016 · N322US · Airbus A320211 · Fuselage Main, Plate/Skin
  > SKIN MISDRILLED THRU STRINGER FRAME 64 STRINGER 10L. REPAIRED THE SKIN IAW SRM 53-00-11 FIG. 239, PARA 4.W. AND REPAIRED STRINGER IAW SRM 53-00-13 FIG 203 PAR 4.A
- [SDR DALA2015091005572](https://openairdocs.org/sdr/DALA2015091005572.md): Skin · damaged · Sep 9, 2015 · N322US · Airbus A320211 · Fuselage Main, Plate/Skin
  > EVIDENCE OF DAMAGE TO LOWER FWD SKIN BETWEEN FRAMES 25-26 AND STRINGERS 44-43R PRI/ERA ISSUED 539169-14 REV 0 REV 1 REV 2 REV 3. C/W PRI/ERA 539169-14 REV 0,1,2 AND 3.
- [SDR DALA2015011200226](https://openairdocs.org/sdr/DALA2015011200226.md): Wire · broken · Jan 1, 2015 · N322US · Airbus A320211 · Light System Wiring
  > DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 6C INOPERATIVE. FOUND BOTH WIRES PULLED OUT OF LIGHT ASSY IN SEAT. REPAIRED BROKEN WIRES AND FUNCTIONAL CHECKED NORMAL.
- [SDR DALA2014092105120](https://openairdocs.org/sdr/DALA2014092105120.md): Light · missing · Sep 20, 2014 · N322US · Airbus A320211 · Emergency Lighting
  > DURING INSPECTION, FOUND EMERGENCY EXIT ROW LIGHT AT 20 RT MISSING AT SEAT. MAINTENANCE REPLACED SEAT EMEGENCY LIGHT ASSY AND REPAIRED WIRING. FUNCTIONAL CHECKED NORMAL.
- [SDR DALA2014082004662](https://openairdocs.org/sdr/DALA2014082004662.md): Stringer Splice · corroded · Aug 19, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER SPLICE 42R IN FWD CARGO BAY BETWEEN FRAMES 28 - 31. REPLACED STRINGER SPLICE IAW SRM 51-42-11, 51-72-11, DWG D53231248200, ERA 528125-14, ORIGINAL REVISION AND PRI 528125-14 REV 0.
- [SDR DALA2014081704625](https://openairdocs.org/sdr/DALA2014081704625.md): Door Sill · corroded · Aug 16, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER L1 DOOR SILL BETWEEN FRAMES 16 - 20. REPLACED LOWER L1 DOOR SILL IAW SRM 51-72-11 AND DWG D53110339.
- [SDR DALA2014081604597](https://openairdocs.org/sdr/DALA2014081604597.md): Stringer · corroded · Aug 16, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 33L BETWEEN FRAMES 65 - 66. REPAIRED STRINGER IAW SRM 53-00-13 PARAGRAPH 4A, FIG 201, SHEET 2, 3, 4 AND 5, PAGES 202-218.
- [SDR DALA2014082004663](https://openairdocs.org/sdr/DALA2014082004663.md): Window Frame · cracked · Aug 15, 2014 · N322US · Airbus A320211 · Fuselage Main, Structure
  > DURING M2-CHECK, A CRACK WAS FOUND ON THE FRAME SECTION AT LT SLIDING WINDOW IAW ALI 53-11-35-PB6. REPAIRED IAW ER/A 527498-14AD, REV ORIGINAL.
- [SDR DALA2014081504598](https://openairdocs.org/sdr/DALA2014081504598.md): Plate · corroded · Aug 15, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > AFTER REMOVING LOWER CORNER FITTING PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON REINFORCEMENT PLATE FRAME 20 STRINGER 23L. REPLACED LOWER REINFORCEMENT PLATE AND FASTENER IAW SRM 51-72-11 AND ENGINEERING REPAIR AUTHORIZATION, 527501-14, REV ORIGINAL AN
- [SDR DALA2014081804586](https://openairdocs.org/sdr/DALA2014081804586.md): Frame · corroded · Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Main, Frame
  > CORROSION ON FWD FACE LATERAL FRAME 20 STRINGER 23R. PERFORMED TIME LIMITED REPAIR ON FWD FACE LATERAL FRAME 20 LOCATED FWD PASSENGER ENTRY DOOR LEVEL STR 23 RT INTERNAL STRUCTURE IAW ER/A 527494-14, REVISION ORIGINAL AND PRELIMINARY REPAIR INSTRUCTIONS 52749
- [SDR DALA2014081504585](https://openairdocs.org/sdr/DALA2014081504585.md): Floor Support · corroded · Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BETWEEN FRAME 16 AND 20 Y-254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND ENGINEERING REPAIR, AUTHORIZATION N 527502-14, REV: ORIGINAL.
- [SDR DALA2014081504583](https://openairdocs.org/sdr/DALA2014081504583.md): Floor Support · corroded · Aug 14, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SILL IN AFT PAX CABIN LOCATED BETWEEN FRAMES 66 AND 68 AT STRINGER 23R. REPLACED LOWER SILL IN AFT PAX CABIN LOCATED BETWEEN FR 66-FR 68 AT LEVEL STR 23R IAW SRM 51-72-11 AND DWG D53480019; JOB COMPLETE.
- [SDR DALA2014081404578](https://openairdocs.org/sdr/DALA2014081404578.md): Fitting · corroded · Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, Structure
  > DURING INSPECTION, FOUND CORROSION ON LOWER CORNER ON FWD LEFT PASSENGER DOOR AT FRAME 16, STINGER 23. REPLACED LOWER CORNER IAW SRM 51-72-11 AND DWG D53112109;
- [SDR DALA2014081404577](https://openairdocs.org/sdr/DALA2014081404577.md): Fitting · corroded · Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, Structure
  > DURING INSPECTION, FOUND CORROSION ON CENTER FITTING, FWD OF LEFT PASSENGER ENTRY DOOR, BETWEEN FRAMES 16 - 20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53112109.
- [SDR DALA2014081404576](https://openairdocs.org/sdr/DALA2014081404576.md): Structure · corroded · Aug 13, 2014 · N322US · Airbus A320211 · Fuselage Main, Structure
  > DURING INSPECTION, FOUND CORROSION ON LOWER CORNER LOCATED FWD OF LEFT PASSENGER ENTRY DOOR AT FRAME 20, STRINGER 23L. REPLACED LOWER CORNER STRUCTURE IAW SRM 51-72-11 AND DWG 53112109.
- [SDR DALA2014081304566](https://openairdocs.org/sdr/DALA2014081304566.md): Floor Support · corroded · Aug 12, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
- [SDR DALA2014081304565](https://openairdocs.org/sdr/DALA2014081304565.md): Floor Support · corroded · Aug 12, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
- [SDR DALA2014081304563](https://openairdocs.org/sdr/DALA2014081304563.md): Seat Track · corroded · Aug 12, 2014 · N322US · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y-1292, BETWEEN FRAMES 64 - 66+5". REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.
- [SDR DALA2014081204420](https://openairdocs.org/sdr/DALA2014081204420.md): Floor Support · corroded · Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y512 BETWEEN FRAMES 64 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
- [SDR DALA2014081204419](https://openairdocs.org/sdr/DALA2014081204419.md): Stringer · corroded · Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, FOUND CORROSION ON STRINGER 42L IN FWD CARGO BAY BETWEEN FRAMES 33 - 34. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53231212.
- [SDR DALA2014081104394](https://openairdocs.org/sdr/DALA2014081104394.md): Angle · cracked · Aug 11, 2014 · N322US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE INTERNAL AREA EMERGENCY DOOR 843. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522 79010.
- [SDR DALA2014081104393](https://openairdocs.org/sdr/DALA2014081104393.md): Angle · cracked · Aug 11, 2014 · N322US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING ANGLE INTERNAL AREA EMERGENCY DOOR 843. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.
- [SDR DALA2014081104392](https://openairdocs.org/sdr/DALA2014081104392.md): Angle · cracked · Aug 11, 2014 · N322US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING ANGLE LOCATED INTERNAL AREA EMERGENCY DOOR 844. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.
- [SDR DALA2014081104391](https://openairdocs.org/sdr/DALA2014081104391.md): Angle · cracked · Aug 11, 2014 · N322US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATED INTERNAL AREA EMERGENCY EXIT DOOR 833. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522-79010.
- [SDR DALA2014081104390](https://openairdocs.org/sdr/DALA2014081104390.md): Angle · cracked · Aug 11, 2014 · N322US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATION INTERNAL AREA EMERGENCY DOOR 834. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D52279010.
- [SDR DALA2014081104389](https://openairdocs.org/sdr/DALA2014081104389.md): Angle · cracked · Aug 11, 2014 · N322US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND CRACK ON FWD LOAD TRANSMITTING ANGLE LOCATION INTERNAL AREA EMERGENCY DOOR 844. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D522 79010.
- [SDR DALA2014081104388](https://openairdocs.org/sdr/DALA2014081104388.md): Structure · cracked · Aug 11, 2014 · N322US · Airbus A320211 · Emergency Exits
  > DURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE LOCATED INTERNAL AREA EMERGENCY DOOR 833. REPLACED SEGMENT ANGLE LOCATED ON INTERNAL AREA EMERGENCY DOOR AFT POSITION IAW SRM 51-72-11 AND DWG D522 79010.
- [SDR DALA2014081104386](https://openairdocs.org/sdr/DALA2014081104386.md): Floor Support · corroded · Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.
- [SDR DALA2014081104385](https://openairdocs.org/sdr/DALA2014081104385.md): Stringer · corroded · Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN FWD CARGO BAY BETWEEN FRAMES 32 - 34. REPLACED THE STRINGER IAW SRM 51-72-11 AND DWG D53231626.
- [SDR DALA2014081104384](https://openairdocs.org/sdr/DALA2014081104384.md): Floor Support · corroded · Aug 11, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-464.5 LOCATED BETWEEN FRAMES 64 - 67+10. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72305.
- [SDR DALA2014081004383](https://openairdocs.org/sdr/DALA2014081004383.md): Cleat · corroded · Aug 10, 2014 · N322US · Airbus A320211 · Fuselage Main, Attach Fittings
  > DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT AT FRAME 33 AND BETWEEN STR 40L TO STR 41L MEASURES APPROXIMATELY L=0.110", W=0.105", D=0.002" SSI 532180. REPLACED CLEAT AND FASTENERS LOCATED IN FWD CARGO COMPARTMENT AT FR 33 AND BETWEEN
- [SDR DALA2014081004382](https://openairdocs.org/sdr/DALA2014081004382.md): Floor Support · corroded · Aug 9, 2014 · N322US · Airbus A320211 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DG D53472000.

Next page: https://openairdocs.org/deregistered/N322US-2023-03-02/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 = 'N322US' AND deregistration_id = 'N322US-2023-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N322US-2023-03-02/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.