# N311US: 1990 Airbus Industrie A320-211, registration cancelled 2018-09-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 27, 2018
- Status when cancelled: Valid registration
- Airframe: [Airbus Industrie A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (registry code 3930320)
- Engine: [GE CFM56 series](https://openairdocs.org/engine/ge-cfm56-series) (registry code 30016)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (OpenAirDocs)
- Serial number: 125
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 13, 1990
- Certificate issued: December 31, 2009
- Last registry action: April 7, 2016
- Mode S code: A34C5B
- 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/N311US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=311US
- Page: https://openairdocs.org/deregistered/N311US-2018-09-27

From the FAA registry file of October 29, 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 (130, newest 50)

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

- [SDR DALA14028663211](https://openairdocs.org/sdr/DALA14028663211), May 5, 2014: BATTERY PACK. INOPERATIVE. RT EMERGENCY LIGHT PACK BATTERY FAULTED. R & R BATTERY PACK IAW AMM 33-51. CHECKED NORMAL.
- [SDR DALA14021943211](https://openairdocs.org/sdr/DALA14021943211), Apr 9, 2014: LIGHT. DAMAGED. DURING NON-ROUTINE CHECK, FOUND 16 ABC SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT AND LAMP HOLDER AT SEAT 16 ABC AND FUNCTIO
- [SDR DALA13023993211](https://openairdocs.org/sdr/DALA13023993211), May 16, 2013: DOOR. OUT OF ADJUST. AFT RT EMERGENCY OVERWING EXIT AMBER CAUTION LIGHT CAME ON, ON UPPER ECAM DURING FCF. AFT RT EMERGENCY OVERWING EXIT COVER FLAP ADJUSTED IAW AMM 52-21-11-700-05
- [SDR DALA13022533211](https://openairdocs.org/sdr/DALA13022533211), May 14, 2013: EPSU. FAILED. DURING NON ROUTINE CHECK, FOUND POWER SUPPLY 13WL FAILED TEST. REMOVED EPSU 13WL IAW AMM 33-51-38-000-001-A. MX INSTALLED SERVICEABLE EPSU AT 13WL AND FUNCTIONA
- [SDR DALA13023973211](https://openairdocs.org/sdr/DALA13023973211), May 10, 2013: STRUT. WORN. LEFT FLAP INTERCONNECT STRUT HAS EXCESSIVE SIDE PLAY AND ACTUATING ROD WORN. REPLACED WITH NEW INTERCONNECTING STRUT ON LT FLAP IAW AMM 27-51-44, PB 401. ADJUST
- [SDR DALA13021713211](https://openairdocs.org/sdr/DALA13021713211), May 9, 2013: SKIN. DAMAGED. DURING INSPECTION, MX REPLACED FWD CENTER TITANIUM & RT FUSELAGE LATERAL SKIN PANEL BETWEEN FR1-FR 12 IAW ER/A 512316-14. REPLACED FWD CENTER TITANIUM SKIN IAW 
- [SDR DALA13021703211](https://openairdocs.org/sdr/DALA13021703211), May 8, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131GF HAS MULTIPLE DENTS AND SCRATCHES. FABRICATED FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.
- [SDR DALA13021693211](https://openairdocs.org/sdr/DALA13021693211), May 7, 2013: SKIN. DAMAGED. DURING INSPECTION, FOUND LT WING NR 3 SLAT TOP SKIN AT RIB OTBD OF TRACK NR 7 DENT IS OUT OF NEARNESS TO RIB & SPAR. NO ALLOWABLE LIMIT ON THIS AREA IAW SRM 57-
- [SDR DALA13021473211](https://openairdocs.org/sdr/DALA13021473211), May 7, 2013: WEB. GOUGED. DURING INSPECTION, FOUND FWD CARGO THRESHOLD WEB HAS DEEP GOUGE 7" AFT OF FR26. REPLACED DAMAGED THRESHOLD WEB IAW DWG 53230315 & SRM 51-42-11.
- [SDR DALA13021463211](https://openairdocs.org/sdr/DALA13021463211), May 7, 2013: STRUCTURE. CORRODED. DURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LOWER CURVE EDGE FWD TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMO
- [SDR DALA13021453211](https://openairdocs.org/sdr/DALA13021453211), May 7, 2013: STRUCTURE. CORRODED. DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR LOWER AFT TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMOVED CORROSI
- [SDR DALA13021443211](https://openairdocs.org/sdr/DALA13021443211), May 7, 2013: STRUCTURE. CORRODED. DURING INSPECTION, FOUND LEFT FWD EMERGENCY EXIT DOOR LOWER CURVE EDGE AFT TEE SECTION CORRODED. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM A32 0 51-44-11. R
- [SDR DALA13021433211](https://openairdocs.org/sdr/DALA13021433211), May 7, 2013: STRUCTURE. CORRODED. DURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR TEE SECTION HAS CORROSION. REPLACED TEE SECTION IAW SRM 51-42-11 AND SRM 51-44-11. REMOVED CORROSION IAW SRM
- [SDR DALA13021683211](https://openairdocs.org/sdr/DALA13021683211), May 6, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131HF HAS MULTIPLE DENTS & SCRATCHES. FABRICTATED FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.
- [SDR DALA13020903211](https://openairdocs.org/sdr/DALA13020903211), May 4, 2013: HINGE FITTING. DAMAGED. DURING INSPECTION, FOUND LT MLG DOOR FWD HINGE AFT LUG, INBD SIDE IS CHAFED. NO ESTABLISHED LIMITS IAW SRM 53-36-11, PAGE 101. REPLACED FITTING IAW DWG R5337050
- [SDR DALA13020913211](https://openairdocs.org/sdr/DALA13020913211), May 3, 2013: HINGE FITTING. DAMAGED. DURING INSPECTION, FOUND LT MLG DOOR FWD HINGE, FWD LUG, FWD FACE HAS CHAFE DAMAGE, FITTING R & R IAW REPAIR DWG R53370500C & SRM 51-42-11.
- [SDR DALA13020893211](https://openairdocs.org/sdr/DALA13020893211), May 3, 2013: FITTING. OUT OF ADJUST. DURING INSPECTION, FOUND RT SIDE OF FWD FUSELAGE BETWEEN FR3 - FR4 STATIC PORT FITTING REQUIRES REPLACEMENT. REMOVED STATIC FITTING IAW SRM 51-42-11. LOCATED AN
- [SDR DALA13020613211](https://openairdocs.org/sdr/DALA13020613211), May 1, 2013: PLATE. CORRODED. DURING INSPECTION, FOUND AFT CARGO BAY CENTER SEALING PLATE CRACKED AROUND SCREW HOLE AND FITTING ATTACHMENT CORRODED. REMOVED SEALING PLATE AND TIE DOWN FITTIN
- [SDR DALA13020253211](https://openairdocs.org/sdr/DALA13020253211), Apr 29, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 132DF CORRODED AND GOUGED. REPLACED FLOOR PANEL IAW SRM 51-72-11.
- [SDR DALA13019423211](https://openairdocs.org/sdr/DALA13019423211), Apr 27, 2013: FLOOR SUPPORT. BENT. DURING INSPECTION, FOUND AFT CARGO BAY FR 58-59 FLOOR SUPPORT BENT AT FWD CORNER & CORRODED AROUND SCREW HOLE. REMOVED CORROSION IAW 51-74-00. FOUND TO BE OUT O
- [SDR DALA13019413211](https://openairdocs.org/sdr/DALA13019413211), Apr 27, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 231AF HAS CORROSION ON HINGE AND PANEL. REPLACED FLOOR PANEL.
- [SDR DALA13019323211](https://openairdocs.org/sdr/DALA13019323211), Apr 25, 2013: SKIN. DAMAGED. DURING INSPECTION, FOUND LOWER FWD FUSELAGE EXTERNAL SKIN BETWEEN FR 26-27 S40R HAS TWO LIGHTNING STRIKES. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORM
- [SDR DALA13019433211](https://openairdocs.org/sdr/DALA13019433211), Apr 25, 2013: WEB. DAMAGED. DURING INSPECTION, FOUND FWD FUSELAGE RT UPPER SPLICE SUPPORT WEB APPROX STR 4R BETWEEN FR 1 & FR 3 HAS SEVERAL TOOL MARKS. REPLACED RT UPPER SPLICE SUPPORT WEB
- [SDR DALA13019403211](https://openairdocs.org/sdr/DALA13019403211), Apr 25, 2013: SKIN. DAMAGED. LOWER FWD FUSELAGE EXTERNAL SKIN BETWEEN FR26-27 STRGR 40R HAS 2EA LIGHTNING STRIKE. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PERFORMED HFEC ROTARY PROBE I
- [SDR DALA13019393211](https://openairdocs.org/sdr/DALA13019393211), Apr 25, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222FF HAS CORROSION. REPLACED FLOOR PANEL IAW SRM 51-72-11.
- [SDR DALA13019383211](https://openairdocs.org/sdr/DALA13019383211), Apr 25, 2013: SKIN. DAMAGED. DURING INSPECTION, FOUND LOWER FORWARD FUSELAGE RT SIDE AT FR 30, STGR 39R EXTERNAL SKIN HAS LIGHTNING STRIKE. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, PER
- [SDR DALA13019373211](https://openairdocs.org/sdr/DALA13019373211), Apr 25, 2013: SKIN. DAMAGED. DURING INSPECTION, FOUND LOWER FWD FUSELAGE RT SIDE AT FR 30, S39R EXTERNAL SKIN HAS LIGHTNING STRIKE AS MARKED. DRILLED OUT DAMAGE FASTENER IAW SRM 51-42-11, P
- [SDR DALA13019363211](https://openairdocs.org/sdr/DALA13019363211), Apr 25, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 232DF HAS TWO BAD INSERTS. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13019353211](https://openairdocs.org/sdr/DALA13019353211), Apr 25, 2013: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221AF HAS PUNCTURED 1" X 1". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13019343211](https://openairdocs.org/sdr/DALA13019343211), Apr 25, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND FLOOR PANEL 261FF HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-74-00, REPLACED FLOOR PANEL, IAW SRM 51-72-11.
- [SDR DALA13019333211](https://openairdocs.org/sdr/DALA13019333211), Apr 25, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF CORROSION ON LOWER SIDE. DAMAGE DIA L=6" X W=18" NO ALLOWABLE LIMIT ON SRM, REPLACED AFT CARGO FLOOR PANEL 
- [SDR DALA13018973211](https://openairdocs.org/sdr/DALA13018973211), Apr 24, 2013: SKIN. GOUGED. DURING INSPECTION, FOUND LOWER FUSELAGE 3IN FWD OF FR51 AND ONE INCH BELOW STRG 41L HAS SKIN GOUGE. BLENDED AREA IAW 51-73-00, FOUND TO BE OUT OF LIMITS IAW SRM
- [SDR DALA13017803211](https://openairdocs.org/sdr/DALA13017803211), Apr 18, 2013: SKIN. CRACKED. DURING INSPECTION, FOUND LWR AFT FUSELAGE LAV VENT, FUSELAGE SKIN BETWEEN STGR 29R AND STG R 30R, BETWEEN FR69 AND FR70 HAS CRACK ON SKIN NEXT TO VENT. CUT OUT 
- [SDR DALA13017763211](https://openairdocs.org/sdr/DALA13017763211), Apr 17, 2013: SKIN. CRACKED. DURING INSPECTION, FOUND LWR AFT FUSELAGE LAV BENT, FUSELAGE SKIN BETWEEN STGR 29R AND STGR 30R, BETWEEN FR69 AND FR70 HAS CRACK ON SKIN NEXT TO BENT. CUT OUT D
- [SDR DALA13017753211](https://openairdocs.org/sdr/DALA13017753211), Apr 16, 2013: SKIN. DENTED. DURING INSPECTION, FOUND LT SIDE OF FWD FUSELAGE AT FR15 WHERE DOOR STOP TOUCHES ACFT SKIN DENT IS OUT OF NEARNESS TO FRAME. DENT FOUND FWD OF FRAME 15 BETWEEN 
- [SDR DALA13017743211](https://openairdocs.org/sdr/DALA13017743211), Apr 15, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 222CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.
- [SDR DALA13017733211](https://openairdocs.org/sdr/DALA13017733211), Apr 15, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FLOOR PANEL 261PF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.
- [SDR DALA13017713211](https://openairdocs.org/sdr/DALA13017713211), Apr 15, 2013: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND FLOOR PANEL 262AB HAS NUMEROUS PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.
- [SDR DALA13017693211](https://openairdocs.org/sdr/DALA13017693211), Apr 15, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND FLOOR PANEL 261DF IS DELAMINATED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209, & DWG 3D25-37498.
- [SDR DALA13017683211](https://openairdocs.org/sdr/DALA13017683211), Apr 15, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND FLOOR PANEL 262EF HAS CORROSION. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.
- [SDR DALA13017673211](https://openairdocs.org/sdr/DALA13017673211), Apr 15, 2013: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 232FF HAS PUNCTURE. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.
- [SDR DALA13017663211](https://openairdocs.org/sdr/DALA13017663211), Apr 15, 2013: FLOOR PANEL. CRACKED. DURING INSPECTION, FOUND FWD UTILITY AREA FLOOR PANEL 232MF IS CRACKED 12 INCHES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 DWG 3D25-37498.
- [SDR DALA13017653211](https://openairdocs.org/sdr/DALA13017653211), Apr 15, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND FLOOR PANEL 261EF CORRODED IN SEVERAL PLACES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209, DWG 3D25-37498.
- [SDR DALA13017643211](https://openairdocs.org/sdr/DALA13017643211), Apr 15, 2013: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND FWD CABIN FLOOR PANEL 221AB HAS TWO PUNCTURES. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 DWG 3D25-37498 .
- [SDR DALA13017203211](https://openairdocs.org/sdr/DALA13017203211), Apr 14, 2013: SEAT TRACK. CORRODED. DURING INSPECTION, FOUND FORWARD CABIN SEAT TRACK BETWEEN FR 20-24, Y-1292. SEAT TRACK CROWN AND UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION AND FOUND
- [SDR DALA13017783211](https://openairdocs.org/sdr/DALA13017783211), Apr 13, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131CF PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.
- [SDR DALA13017543211](https://openairdocs.org/sdr/DALA13017543211), Apr 13, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131BF CRACKED AND DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.
- [SDR DALA13017533211](https://openairdocs.org/sdr/DALA13017533211), Apr 13, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131KF HAS MULTIPLE DENTED & CRACKED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.
- [SDR DALA13017523211](https://openairdocs.org/sdr/DALA13017523211), Apr 13, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF HAS MULTIPLE DENTS & DELAMINATED. FABRICATED FLOOR PANEL IAW DWG 3D25-37705.
- [SDR DALA13017513211](https://openairdocs.org/sdr/DALA13017513211), Apr 13, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162BF DAMAGED. FABRICATED SLOPE PANEL IAW DWG 3D25-37705.

All 130: https://openairdocs.org/deregistered/N311US-2018-09-27/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA09FA047](https://openairdocs.org/ntsb/DCA09FA047), May 4, 2009: Airbus A320 (N311US), Denver, CO, substantial damage. Probable cause: The first officer’s excessive pitch-up of the airplane while landing with a tailwind, which resulted in a tailstrike following a bounced landing. Contributing to the bounced landing were a high…

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19910102002359I](https://openairdocs.org/incident/19910102002359I), Jan 2, 1991: Airbus A320211 (N311US), Las Vegas, NV, Minor damage. Captains windshield shattered at altitude. Precautionary landing at Las Vegas.

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