# N318US: 1991 Airbus Industrie A320-211, registration cancelled 2018-09-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 28, 2018
- Status when cancelled: First renewal notice
- 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: 206
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 29, 1991
- Certificate issued: January 31, 2013
- Last registry action: October 7, 2015
- Mode S code: A3665C
- 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/N318US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=318US
- Page: https://openairdocs.org/deregistered/N318US-2018-09-28

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 (131, newest 50)

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

- [SDR DALA2017051403878](https://openairdocs.org/sdr/DALA2017051403878), May 13, 2017: COVER. MISSING. ROW 11 RIGHT EMERGENCY LIGHT COVER MISSING, REPLACED THE COVER.
- [SDR DALA2017010800181](https://openairdocs.org/sdr/DALA2017010800181), Jan 7, 2017: BOX BEAM. CRACKED. LEFT SIDE BOX BEAM UPPER FLANGE CRACKED. REPAIRED IAW AMDS 5310-01450-02.
- [SDR DALA2016102707849](https://openairdocs.org/sdr/DALA2016102707849), Oct 26, 2016: LIGHT. DAMAGED. SEAT MOUNTED EMERGENCY LIGHT SEAT 21C DAMAGED, EMERGENCY LIGHT REPAIRED.
- [SDR DALA2016111808969](https://openairdocs.org/sdr/DALA2016111808969), Jan 19, 2016: STRINGER. CORRODED. CORROSION ON STRINGER 44 BETWEEN FRAMES 56 AND 59, REMOVED CORROSION AND INSTALLED REPAIR IAW SRM.
- [SDR DALA2016012100723](https://openairdocs.org/sdr/DALA2016012100723), Jan 19, 2016: STRINGER. CORRODED. FOUND EVEDENCE OF CORROSION IN MULTIPLE LOCATIONS ON S42R BETWEEN FRAMES 54 & 58, REMOVED AREAS OF CORROSION REPAIR ON S42R BETWEEN FRAMES 54 & 58 IAW SRM 53-00
- [SDR DALA2016111808971](https://openairdocs.org/sdr/DALA2016111808971), Jan 16, 2016: FRAME. CORRODED. CORROSION ON FRAME 43L AT FRAME 55. REPAIR THE FRAME.
- [SDR DALA2016011900504](https://openairdocs.org/sdr/DALA2016011900504), Jan 16, 2016: STRINGER. CORRODED. CORROSION ON STRINGER 42L BETWEEN FRAMES 56 AND 57. REMOVED STR 42L BETWEEN FRAMES 55 AND 58. FABRICATED AND INSTALLED STRINGER SECTION AND COUPLING/SPLICE IAW 
- [SDR DALA2016011900483](https://openairdocs.org/sdr/DALA2016011900483), Jan 16, 2016: STRINGER. CORRODED. FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 56 AND 57. REMOVED STR 43L BETWEEN FRAME 55 TO 59. INSTALLED NEW STRINGER SECTION IAW SRM 53-00-13.
- [SDR DALA2015022701737](https://openairdocs.org/sdr/DALA2015022701737), Feb 25, 2015: WIRE. BROKEN. DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 9 IS INOPERATIVE. FOUND BROKEN GROUND WIRE AT SPLICE. REPLACED SPLICE AND FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA2015022601674](https://openairdocs.org/sdr/DALA2015022601674), Feb 25, 2015: WIRE. PULLED. DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 12 INOPERATIVE. FOUND POWER WIRE PULLED FROM SPLICE. REINSTALLED WIRE TO SPLICE AND FUNCTIONAL CHECK WAS
- [SDR DALA14011823218](https://openairdocs.org/sdr/DALA14011823218), Feb 21, 2014: POWER SUPPLY. INOPERATIVE. DURING NON-ROUTINE CHECK, FOUND SEVERAL SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED EPSU AND FUNCTIONAL CHECKED NORMAL.
- [SDR DALA13065943218](https://openairdocs.org/sdr/DALA13065943218), Dec 3, 2013: CONNECTOR. UNSECURE. DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT SYSTEM TEST FAILED. MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTING AT SEATS 9C, 16C, 17C, 21C, 22C, 23C, INOPE
- [SDR DALA13054143218](https://openairdocs.org/sdr/DALA13054143218), Oct 20, 2013: RELAY. MALFUNCTIONED. DOOR LIGHTS ON AFTER GEAR UP. CABIN LIGHT UNCONTROLLABLE FROM F/A PANEL. R & R RELAY 8WL IAW ASM 33-51. OPS TESTED GOOD, OK FOR CONTINUED SERVICE.
- [SDR DALA13032633218](https://openairdocs.org/sdr/DALA13032633218), Jun 28, 2013: PROFILE. CRACKED. DURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS CRACK. HFEC IAW NTM 51-10-08 PT6, CONFIRMED CRACK BY FASTENER HOLE. REPLACE
- [SDR DALA13032693218](https://openairdocs.org/sdr/DALA13032693218), Jun 28, 2013: PROFILE. CRACKED. DURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS SEVERAL CRACKS AROUND FASTENER HOLES. HFEC IAW NTM 51-10-08, PT6, CONFIRMED
- [SDR DALA13032683218](https://openairdocs.org/sdr/DALA13032683218), Jun 28, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR LWR AFT LATCH HOOK ATTACH FITTING HAS CORROSION. REMOVED OLD FITTING IAW SRM 51-42-11. LOCATED AND DRILLED N
- [SDR DALA13032673218](https://openairdocs.org/sdr/DALA13032673218), Jun 28, 2013: PLATE. CHAFED. DURING INSPECTION, FOUND LT NR 3 SLAT TRACK COVER PLATE CHAFING W/ SLAT T/E LWR SKIN. ACCOMPLISHED REPAIR IAW ER/A 494603-14MA, SECTION 1, PERMANENT REPAIR IDEN
- [SDR DALA13032653218](https://openairdocs.org/sdr/DALA13032653218), Jun 27, 2013: FLOOR SUPPORT. CRACKED. DURING INSPECTION, FOUND COCKPIT FLOOR SUPPORT RT SIDE FWD FR8 Y-1292, AROUND NUTPLATE SHEETMETAL CRACKED. ACCOMPLISHED REPAIR IAW ER/A 515379-14, REV ORIGINAL 
- [SDR DALA13031533218](https://openairdocs.org/sdr/DALA13031533218), Jun 24, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND AFT CARGO BETWEEN FR 58-59, STR 44, FLOOR SUPPORT HAS SURFACE CORROSION. BLENDED CORROSION. BLENDED CORROSION IAW SRM 51-74-00. NO ESTA
- [SDR DALA13031523218](https://openairdocs.org/sdr/DALA13031523218), Jun 24, 2013: FLOOR PANEL. DAMAGED. MID CABIN, FLOOR PANEL 241AF FOUND ONE ELONGATED HOLE AND CRACKED. FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007-A.
- [SDR DALA13031513218](https://openairdocs.org/sdr/DALA13031513218), Jun 24, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162CF DELAMINATED 21" X 15". AFT CARGO COMPARTMENT SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209.
- [SDR DALA13031503218](https://openairdocs.org/sdr/DALA13031503218), Jun 24, 2013: FLOORBEAM. CORRODED. DURING INSPECTION, FOUND AFT CARGO FLOORBEAM AT FR58, LT SIDE, FWD FACE HAS 2EA AREAS OF CORROSION. REMOVED FLOORBEAM AT FR 58 IAW SRM 51-42-11. NO ALLOWABLE LI
- [SDR DALA13033173218](https://openairdocs.org/sdr/DALA13033173218), Jun 23, 2013: SKIN. DAMAGED. DURING INSPECTION, FOUND AFT LT PASSENGER DOOR EXTERNAL FROM LOWER EDGE TO ABOVE 16 INCHES SKIN HAS DENT. FOUND OUT OF LIMITS IAW SRM 52-10-00, DIAGRAM 103. CUT
- [SDR DALA13030913218](https://openairdocs.org/sdr/DALA13030913218), Jun 22, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND AFT CARGO COMPARTMENT BETWEEN FR56-FR57, STR 43L CORRODED. CLEANED AREA IAW AMM 12-21-12. CORROSION FOUND. NO LIMITS ESTABLISHED IAW SR
- [SDR DALA13032663218](https://openairdocs.org/sdr/DALA13032663218), Jun 21, 2013: STRINGER. DAMAGED. DURING INSPECTION, FOUND AFT CARGO AT FR 65, STR 43L HAS CORROSION. REMOVED CORROSION IAW SRM A320 51-74-00. NO ALLOWABLE DAMAGE FOUND ON SRM. PERFORMED STRINGE
- [SDR DALA13030903218](https://openairdocs.org/sdr/DALA13030903218), Jun 21, 2013: SHEAR TIE. CORRODED. DURING INSPECTION, FOUND FWD CARGO COMPT BILGE AREA AT FR 28 STGR 41R -42R CLIP HAS CORROSION. REMOVED SHEAR CLIP IAW SRM 51-42-11. NO ALLOWABLE DAMAGE LIMITS F
- [SDR DALA13030153218](https://openairdocs.org/sdr/DALA13030153218), Jun 19, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND FWD CARGO BAY, FR 33-34, S41L CORRODED. BLENDED CORROSION IAW SRM 51-74-00 CHECKED LIMITS, WITH NO ALLOWABLE DAMAGE FOUND ON SRM. CUT O
- [SDR DALA13030143218](https://openairdocs.org/sdr/DALA13030143218), Jun 19, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND AFT CARGO BAY FR58 - 59 S42L CORRODED. CLEANED AREA IAW AMM 12-21-12. NO LIMITS ON CORROSION ESTABLISHED IAW SRM 53-41-13, FIG 101. REM
- [SDR DALA13032643218](https://openairdocs.org/sdr/DALA13032643218), Jun 17, 2013: ANGLE. CRACKED. DURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE HAS SEVERAL CRACKS AROUND FASTENER. HFEC IAW NTM 51-10-08, PT6 CONFIRMED CRACKS
- [SDR DALA13029903218](https://openairdocs.org/sdr/DALA13029903218), Jun 17, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152EF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029893218](https://openairdocs.org/sdr/DALA13029893218), Jun 17, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151DF HAS SEVERAL BROKEN EDGES & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029873218](https://openairdocs.org/sdr/DALA13029873218), Jun 17, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151LF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37705.
- [SDR DALA13029863218](https://openairdocs.org/sdr/DALA13029863218), Jun 17, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151AF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00 FIG 209 & DWG 3D25-37705.
- [SDR DALA13029853218](https://openairdocs.org/sdr/DALA13029853218), Jun 17, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152BF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-37705.
- [SDR DALA13029843218](https://openairdocs.org/sdr/DALA13029843218), Jun 17, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151QF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029823218](https://openairdocs.org/sdr/DALA13029823218), Jun 16, 2013: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151NF HAS SEVERAL PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029813218](https://openairdocs.org/sdr/DALA13029813218), Jun 16, 2013: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151HF HAS SEVERAL PUNCTURES & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029803218](https://openairdocs.org/sdr/DALA13029803218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151JF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029643218](https://openairdocs.org/sdr/DALA13029643218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029633218](https://openairdocs.org/sdr/DALA13029633218), Jun 16, 2013: PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152MF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029623218](https://openairdocs.org/sdr/DALA13029623218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152RF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029613218](https://openairdocs.org/sdr/DALA13029613218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161BF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029603218](https://openairdocs.org/sdr/DALA13029603218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151EF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029593218](https://openairdocs.org/sdr/DALA13029593218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161FF DELAMINATED. FABRICATED FLOOR PANEL IAW BFM 53-02-00, FIG 209.
- [SDR DALA13029583218](https://openairdocs.org/sdr/DALA13029583218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161EF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029573218](https://openairdocs.org/sdr/DALA13029573218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161CF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029563218](https://openairdocs.org/sdr/DALA13029563218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151FF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029553218](https://openairdocs.org/sdr/DALA13029553218), Jun 16, 2013: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 162FF HAS PUNCTURED & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029543218](https://openairdocs.org/sdr/DALA13029543218), Jun 16, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151GF HAS SEVERAL BROKEN INSERTS & DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13029533218](https://openairdocs.org/sdr/DALA13029533218), Jun 16, 2013: FLOOR PANEL. DELAMINATED. DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF DELAMINATED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.

All 131: https://openairdocs.org/deregistered/N318US-2018-09-28/reports.md

## FAA accident and incident reports (3)

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 19970821030219I](https://openairdocs.org/incident/19970821030219I), Aug 21, 1997: Airbus A320211 (N318US), Minneapolis, MN. Narrative: #2 engine failed on take-off roll. Take-off was rejected. Inspection of engine revealed metal debris in tailpipe. Failure cause yet to be determined.
- [Incident 19950525015489I](https://openairdocs.org/incident/19950525015489I), May 25, 1995: Airbus A320211 (N318US), Chicago, IL. Narrative: during climb the flight crew experienced several aileron deflections. After a few deflections elac 1 faulted. Elac 1 was reset and the flight…
- [Incident 19920222005899I](https://openairdocs.org/incident/19920222005899I), Feb 22, 1992: Airbus A320211 (N318US), New York, NY. Smoke in cabin while taxiing to gate. Shut down engines. Fired bottles. Evacuated on taxiway. No fire.

## Other aircraft with N318US

- [Registered now](https://openairdocs.org/aircraft/N318US): Costruzioni Aeronautiche Tecna P2010 TDI, S/N 318/US, built 2025

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