# N322US: 1991 Airbus Industrie A320-211, registration cancelled 2023-03-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 2, 2023
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (registry code 3930320)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 263
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 24, 1992
- Certificate issued: July 14, 2015
- Last registry action: February 14, 2022
- Mode S code: A37791
- Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N322US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=322US
- Page: https://openairdocs.org/deregistered/N322US-2023-03-02

From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Airbus Industrie A320-211: https://openairdocs.org/model/airbus-industrie-a320-211.md

## Service difficulty reports (101, newest 50)

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

- [SDR DALA2019121007214](https://openairdocs.org/sdr/DALA2019121007214), Dec 10, 2019: LIGHT. DAMAGED. EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATION 1C, REPLACED LIGHT FIXTURE AT SEAT 1C
- [SDR DALA2018081095007](https://openairdocs.org/sdr/DALA2018081095007), Aug 9, 2018: CONTROL VALVE. FAILED. 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), Jul 17, 2018: SKIN. DAMAGED. 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), Jul 14, 2018: DAMPER. UNSERVICEABLE. 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), Jul 14, 2018: ROD END. CORRODED. CORROSION ON TRAILING EDGE ROD END OF YAW DAMPER. REMOVED, REPLACED AND FUNCTIONAL CHECK.
- [SDR DALA2018071604501](https://openairdocs.org/sdr/DALA2018071604501), Jul 14, 2018: SLIDE. DEFORMED. SLIDE DEFORMATION PASSENGER CREW DOOR 832, AFT GALLEY AREA. REMOVED AND REPLACED SLIDE. CHECKS GOOD.
- [SDR DALA2018060903916](https://openairdocs.org/sdr/DALA2018060903916), Jun 8, 2018: WIRE. CUT. FOUND L2 SLIDE WIRES CUT. REMOVED AND REPLACED L2 DOOR SLIDE ASSEMBLY.
- [SDR DALA2017091106815](https://openairdocs.org/sdr/DALA2017091106815), Sep 9, 2017: POWER SUPPLY. INOPERATIVE. 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), May 24, 2017: BATTERY PACK. INOPERATIVE. 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), Mar 7, 2017: SKIN. NOT REPORTED. 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), Feb 3, 2017: VENT. CORRODED. 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 PA
- [SDR DALA2016072805619](https://openairdocs.org/sdr/DALA2016072805619), Jul 27, 2016: FITTING. DAMAGED. DAMAGE ON RIGHT CRUCIFORM, REPAIRED IAW ER/A 548323-14AD REV A FOR WING CENTER CRUCIFORM FITTING.
- [SDR DALA2016072105469](https://openairdocs.org/sdr/DALA2016072105469), Jul 20, 2016: FRAME. DAMAGED. 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), Jul 20, 2016: FRAME. CRACKED. CRACK INDICATIONS AT FRAME 16. COMPLIED WITH FINAL ERA 548219-14AD REV ORIGINAL.
- [SDR DALA2016072105467](https://openairdocs.org/sdr/DALA2016072105467), Jul 20, 2016: BOX BEAM. NOT REPORTED. CENTER FUSELAGE RT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548164-14AD.
- [SDR DALA2016072105466](https://openairdocs.org/sdr/DALA2016072105466), Jul 20, 2016: BOX BEAM. NOT REPORTED. CENTER FUSELAGE LT SIDE BOX BEAM AT FRAME 43 AND Y1650. COMPLY WITH ERA 548129-14AD.
- [SDR DALA2016111808959](https://openairdocs.org/sdr/DALA2016111808959), Jul 18, 2016: STRINGER. CORRODED. 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), Jul 18, 2016: STRINGER. CORRODED. 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), Jul 10, 2016: SKIN. DAMAGED. 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
- [SDR DALA2015091005572](https://openairdocs.org/sdr/DALA2015091005572), Sep 9, 2015: SKIN. DAMAGED. 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
- [SDR DALA2015011200226](https://openairdocs.org/sdr/DALA2015011200226), Jan 1, 2015: WIRE. BROKEN. 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 
- [SDR DALA2014092105120](https://openairdocs.org/sdr/DALA2014092105120), Sep 20, 2014: LIGHT. MISSING. DURING INSPECTION, FOUND EMERGENCY EXIT ROW LIGHT AT 20 RT MISSING AT SEAT. MAINTENANCE REPLACED SEAT EMEGENCY LIGHT ASSY AND REPAIRED WIRING. FUNCTIONAL CHECKE
- [SDR DALA2014082004662](https://openairdocs.org/sdr/DALA2014082004662), Aug 19, 2014: STRINGER SPLICE. CORRODED. 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, 
- [SDR DALA2014081704625](https://openairdocs.org/sdr/DALA2014081704625), Aug 16, 2014: DOOR SILL. CORRODED. 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), Aug 16, 2014: STRINGER. CORRODED. 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), Aug 15, 2014: WINDOW FRAME. CRACKED. 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), Aug 15, 2014: PLATE. CORRODED. AFTER REMOVING LOWER CORNER FITTING PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON REINFORCEMENT PLATE FRAME 20 STRINGER 23L. REPLACED LOWER REINFORCEMENT P
- [SDR DALA2014081804586](https://openairdocs.org/sdr/DALA2014081804586), Aug 14, 2014: FRAME. CORRODED. 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
- [SDR DALA2014081504585](https://openairdocs.org/sdr/DALA2014081504585), Aug 14, 2014: FLOOR SUPPORT. CORRODED. 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: ORIGI
- [SDR DALA2014081504583](https://openairdocs.org/sdr/DALA2014081504583), Aug 14, 2014: FLOOR SUPPORT. CORRODED. 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 L
- [SDR DALA2014081404578](https://openairdocs.org/sdr/DALA2014081404578), Aug 13, 2014: FITTING. CORRODED. 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), Aug 13, 2014: FITTING. CORRODED. 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
- [SDR DALA2014081404576](https://openairdocs.org/sdr/DALA2014081404576), Aug 13, 2014: STRUCTURE. CORRODED. 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 5
- [SDR DALA2014081304566](https://openairdocs.org/sdr/DALA2014081304566), Aug 12, 2014: FLOOR SUPPORT. CORRODED. 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), Aug 12, 2014: FLOOR SUPPORT. CORRODED. 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), Aug 12, 2014: SEAT TRACK. CORRODED. 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), Aug 11, 2014: FLOOR SUPPORT. CORRODED. 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), Aug 11, 2014: STRINGER. CORRODED. 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), Aug 11, 2014: ANGLE. CRACKED. 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), Aug 11, 2014: ANGLE. CRACKED. 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), Aug 11, 2014: ANGLE. CRACKED. 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), Aug 11, 2014: ANGLE. CRACKED. 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), Aug 11, 2014: ANGLE. CRACKED. 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), Aug 11, 2014: ANGLE. CRACKED. 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), Aug 11, 2014: STRUCTURE. CRACKED. DURING INSPECTION, FOUND CRACK ON AFT LOAD TRANSMITTING PROFILE LOCATED INTERNAL AREA EMERGENCY DOOR 833. REPLACED SEGMENT ANGLE LOCATED ON INTERNAL AREA EMERGE
- [SDR DALA2014081104386](https://openairdocs.org/sdr/DALA2014081104386), Aug 11, 2014: FLOOR SUPPORT. CORRODED. 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), Aug 11, 2014: STRINGER. CORRODED. 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), Aug 11, 2014: FLOOR SUPPORT. CORRODED. 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), Aug 10, 2014: CLEAT. CORRODED. 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=0.0
- [SDR DALA2014081004382](https://openairdocs.org/sdr/DALA2014081004382), Aug 9, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765 BETWEEN FRAMES 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DG D53472000.

All 101: https://openairdocs.org/deregistered/N322US-2023-03-02/reports.md

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