# N313US: 1990 Airbus Industrie A320-211, registration cancelled 2018-09-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 27, 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: 153
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 27, 1991
- Certificate issued: February 22, 2013
- Last registry action: December 5, 2015
- Mode S code: A353C9
- 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/N313US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=313US
- Page: https://openairdocs.org/deregistered/N313US-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 (115, newest 50)

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

- [SDR DALA2018060403785](https://openairdocs.org/sdr/DALA2018060403785), Jan 24, 2018: STRUCTURE. CRACKED. OVERSIZED HOLES AND CRACKS WERE FOUND DURING SHOP ACCOMPLISHMENT OF EM 5230-01163 (AD 2017-22-07) TO FWD CARGO DOOR, P/N D52371000012 S/N UH-1153, REPAIRED PER 
- [SDR DALA2017080906065](https://openairdocs.org/sdr/DALA2017080906065), Aug 8, 2017: CONNECTOR. MALFUNCTIONED. WHILE PERFORMING EMERGENCY LIGHT TEST DURING SERVICE CHECK, HAD MULTIPLE MESSAGES INTERNAL LIGHT FAULT. DISCONNECTED & RECONNECTED R MIN CABIN EPSU CONNECTOR. T
- [SDR DALA2017070205105](https://openairdocs.org/sdr/DALA2017070205105), Jun 30, 2017: LAMP. INOPERATIVE. EMERGENCY LIGHT SEAT 5 LT INOPERATIVE, REPLACED THE LAMPS.
- [SDR DALA2017020601038](https://openairdocs.org/sdr/DALA2017020601038), Feb 5, 2017: BATTERY PACK. NO TEST. SERVICE CHECK FOUND EMERGENCY LIGHTS TEST FAILED, REPLACED THE BATTERY.
- [SDR DALA2016120709694](https://openairdocs.org/sdr/DALA2016120709694), Dec 6, 2016: FRAME. CRACKED. FRAME 16 WAS FOUND CRACKED, PERFORMED TEMPORARY REPAIR IAW ER/A 551555-14AD REVISION ORIGINAL.
- [SDR DALA2016120509631](https://openairdocs.org/sdr/DALA2016120509631), Dec 4, 2016: STRINGER. CORRODED. CORROSION ON STRINGER 31R IN AFT CARGO COMPARTMENT BETWEEN FRAME 65 TO FRAME 66. REPLACED STRINGER 31R IN AFT CARGO COMPARTMENT FROM FRAME 64 TO FRAME 67 AS PER
- [SDR DALA2016120409627](https://openairdocs.org/sdr/DALA2016120409627), Dec 3, 2016: STRINGER. CORRODED. CORROSION ON STRINGER 25R IN AFT CARGO COMPARTMENT BETWEEN FRAME 65 TO FRAME 66. REPLACED STRINGER 25R IN AFT CARGO COMPARTMENT BETWEEN FR 64 TO FR 67 AS PER SR
- [SDR DALA2016112909407](https://openairdocs.org/sdr/DALA2016112909407), Nov 28, 2016: FRAME. CRACKED. CRACK ON LATERAL FWD SEGMENT FRAME ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN, REPLACED LATERAL FWD SEGMENT FRAME IAW SRM 51-72-11 AND DRAWING D52279010
- [SDR DALA2015092905867](https://openairdocs.org/sdr/DALA2015092905867), Sep 28, 2015: LIGHT. DAMAGED. EMERGENCY SEAT MOUNTED LIGHT DAMAGED. REPLACED LIGHT ASSY.
- [SDR DALA2014090404911](https://openairdocs.org/sdr/DALA2014090404911), Sep 1, 2014: LIGHT. MISSING. DURING NON-ROUTINE CHECK, FOUND SEAT 20A MISSING AISLE EMERGENCY LIGHT. MAINTENANCE REPLACED EMERGENCY LIGHT AND FUNCTIONAL CHECKED NORMAL.
- [SDR DALA2014070703901](https://openairdocs.org/sdr/DALA2014070703901), Jul 4, 2014: WIRE. PULLED. DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS AT SEATS 08C-23C INOPERATIVE. MAINTENANCE FOUND WIRE PULLED FROM SPLICE AT EACH LOCATION. SPLICED WIRES BACK TO
- [SDR DALA13035083213](https://openairdocs.org/sdr/DALA13035083213), Jul 12, 2013: BATTERY PACK. FAILED. DURING CRUISE EMERGENCY EXIT LIGHTS AND THE EMERGENCY AISLE LIGHTING WERE FLASHING ERRATICALLY ON AND OFF WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION. MX REPL
- [SDR DALA13034043213](https://openairdocs.org/sdr/DALA13034043213), Jul 8, 2013: EPSU. FAILED. DURING NON ROUTINE CHECK, FOUND EPSU INTERNAL LOAD EMERGENCY LIGHT FAILED. MX REPLACED EPSU 10WL AND FUNCTIONAL CHECKED NORMAL.
- [SDR DALA13007133213](https://openairdocs.org/sdr/DALA13007133213), Feb 11, 2013: SHEAR TIE. CORRODED. DURING INSPECTION, FOUND FWD CARGO AT FR 31 BET CENTERLINE AND STR 43R, SHEAR TIE HAS CORROSION. CHECKED LIMITS L=1.00" W=1.00" D=0.010". NO ALLOWABLE DAMAGE IA
- [SDR DALA13006653213](https://openairdocs.org/sdr/DALA13006653213), Feb 7, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF IS CORRODED. REMOVED CORROSION IAW SRM 51-74-00, L=1.0" W=0.70" D=0.050 NO ESTABLISHED SRM LIMITS.
- [SDR DALA13006643213](https://openairdocs.org/sdr/DALA13006643213), Feb 7, 2013: WEB. CORRODED. DURING INSPECTION, FOUND AFT CARGO BAY FRAME 55-56, STR 39-40R WEB PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW ER/A 4
- [SDR DALA13006633213](https://openairdocs.org/sdr/DALA13006633213), Feb 7, 2013: STRUCTURE. CRACKED. DURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FASTENER HOLES (5EA) HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED 
- [SDR DALA13006623213](https://openairdocs.org/sdr/DALA13006623213), Feb 7, 2013: STRUCTURE. CRACKED. DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FOUR FASTENER HOLES HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .
- [SDR DALA13006353213](https://openairdocs.org/sdr/DALA13006353213), Feb 6, 2013: STRUCTURE. CORRODED. DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR FWD LOWER T SECTION HAS CORROSION. REMOVED OLD "T" SECTION IAW SRM 51-42-11. TREATED AND PRIMED HOLES IAW SR
- [SDR DALA13006483213](https://openairdocs.org/sdr/DALA13006483213), Feb 6, 2013: PROFILE. CRACKED. DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE (4EA) FASTENER HOLES HAS CRACK. CRACK INDICATION NOTED .025" LENGTH OF DAMAGE
- [SDR DALA13006433213](https://openairdocs.org/sdr/DALA13006433213), Feb 6, 2013: STRUCTURE. CRACKED. DURING INSP, FOUND RT FWD EMERGENCY EXIT DOOR, FWD LOAD TRANSMITTING PROFILE (9EA) FASTENER HOLE HAS CRACKED. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025"
- [SDR DALA13006423213](https://openairdocs.org/sdr/DALA13006423213), Feb 6, 2013: STRUCTURE. CRACKED. DURING INSPECTION, RT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FASTENER HOLE HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .027" LENGTH 
- [SDR DALA13006413213](https://openairdocs.org/sdr/DALA13006413213), Feb 6, 2013: STRUCTURE. CORRODED. DURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR LOWER AFT TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=.90" W=.80" D=.010" NO ALLOWABLE D
- [SDR DALA13006403213](https://openairdocs.org/sdr/DALA13006403213), Feb 6, 2013: STRUCTURE. CORRODED. DURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR, FWD LOWER TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=1.0" W=.70" D=.012" NO ALLOWABLE 
- [SDR DALA13006393213](https://openairdocs.org/sdr/DALA13006393213), Feb 6, 2013: STRUCTURE. CORRODED. DURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR, FWD LOWER TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=2.0" W=1.5" D=.040" NO ALLOWABLE 
- [SDR DALA13006383213](https://openairdocs.org/sdr/DALA13006383213), Feb 6, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND AFT CARGO BAY FRAME 59 STR 44 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION NO LIMITS IN SRM 53-41-14 L=.5" W=.5" D=.020". REMOVED COR
- [SDR DALA13006673213](https://openairdocs.org/sdr/DALA13006673213), Feb 5, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND AFT CARGO FRAME 58-59, STR 44, FLOOR SUPPORT CORRODED. REMOVED AFT CARGO FLOOR SUPPORT IAW A320 SRM 51-42-11 FR 58-59 STR 44. REMOVED C
- [SDR DALA13006363213](https://openairdocs.org/sdr/DALA13006363213), Feb 4, 2013: DOOR. CORRODED. DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR FWD LOWER T SECTION HAS CORROSION. REMOVED OLD "T" SECTION IAW SRM 51-42-11. TREATED AND PRIMED HOLE S IAW S
- [SDR DALA13006323213](https://openairdocs.org/sdr/DALA13006323213), Feb 4, 2013: STRUCTURE. GOUGED. DURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE AFT GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW A320 TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.284" W=0.062"
- [SDR DALA13006313213](https://openairdocs.org/sdr/DALA13006313213), Feb 4, 2013: STRUCTURE. GOUGED. DURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE MID GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.446" W=0.022" D=0.
- [SDR DALA13006303213](https://openairdocs.org/sdr/DALA13006303213), Feb 4, 2013: FRAME. GOUGED. DURING INSPECTION, FOUND FWD CARGO COMPT FR28 FRAME SPLICE AFT FACE IS GOUGED STR 35L. BLENDED FISH PLATE IAW SRM 51-73-00, MEASUREMENTS ARE L=1.5" W=.5" D=. 01
- [SDR DALA13006293213](https://openairdocs.org/sdr/DALA13006293213), Feb 4, 2013: FRAME SPLICE. GOUGED. DURING INSPECTION, FOUND FWD CARGO COMPT FR26 FRAME SPLICE AFT FACE IS GOUGED STR 35L. REPLACED FISH PLATE IAW SRM 51-42-11 DWG NR C2.D53230405. BLENDED FISH PL
- [SDR DALA13006663213](https://openairdocs.org/sdr/DALA13006663213), Feb 3, 2013: FRAME. CORRODED. DURING INSPECTION, FOUND AFT CARGO FRAME 55-58, STR 43L HAS CORROSION. REMOVED CORROSION IAW 51-74-00 FROM STRINGER 43L BET FRAME 55-58 AND FOUND NO ESTABLISHED
- [SDR DALA13006283213](https://openairdocs.org/sdr/DALA13006283213), Feb 3, 2013: STOP FITTING. CHAFED. DURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE FRAME 68 ROLLER STOP FITTING ON MID OUTER SURFACE HAS CHAFED. REPLACED ROLLER STOP FITTING AT LT AFT PAX ENTR
- [SDR DALA13005903213](https://openairdocs.org/sdr/DALA13005903213), Feb 2, 2013: SKIN. GOUGED. DURING INSPECTION, FOUND RT NR 4 SLAT LWR T/E SKIN HAS GOUGE 10" INBD OF SLAT TRACK NR 10. ACCOMPLISHED REPAIR IAW ER/A 509275-14 REV ORIGINAL AS PERMANENT REPA
- [SDR DALA13005893213](https://openairdocs.org/sdr/DALA13005893213), Feb 2, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND AFT CARGO FRAME 56-57, STR 41L HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DAMAGE DIMENSION S L=5.0" W=1.0"D=0.012". NO 
- [SDR DALA13006373213](https://openairdocs.org/sdr/DALA13006373213), Jan 31, 2013: FLOORBOARD. CRACKED. DURING INSPECTION, FOUND MID CABIN FLOORBOARD 232MF CORNER EDGE IS CRACKED. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209.
- [SDR DALA13005583213](https://openairdocs.org/sdr/DALA13005583213), Jan 30, 2013: FLOORBOARD. DELAMINATED. DURING INSPECTION, FOUND MID CABIN BETWEEN FR35 TO 36 MOST CENTER FLOORBOARD 241AF HAS DELAMINATION. REPLACED FLOORBOARDIAW AMM 53-12-12-400-001-A. FABRICATED F
- [SDR DALA13005383213](https://openairdocs.org/sdr/DALA13005383213), Jan 29, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161 BF IS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-5019 AND DWG 3D25-37705
- [SDR DALA13005373213](https://openairdocs.org/sdr/DALA13005373213), Jan 28, 2013: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF INSERTS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-6602.
- [SDR DALA13005053213](https://openairdocs.org/sdr/DALA13005053213), Jan 28, 2013: FLOOR SUPPORT. DAMAGED. DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOORBEAM BETWEEN FR 16-20 Y-254 UPPER FLANGE HOLES HAS CORROSION. REMOVED DAMAGE IAW SRM 51-74-00. DAMAGE M
- [SDR DALA13005063213](https://openairdocs.org/sdr/DALA13005063213), Jan 23, 2013: SKIN. GOUGED. DURING INSPECTION, FOUND LOWER FUSELAGE JUST AFT OF FR 65 BETWEEN STR 28L - 29L SKIN APPEARS TO BE GOUGED UNDER PAINT. N/R 100/4. CUTOUT DAMAGED SKIN IAW SRM 53
- [SDR DALA13004233213](https://openairdocs.org/sdr/DALA13004233213), Jan 23, 2013: SILL. CORRODED. DURING INSPECTION, FOUND RT AFT PASSENGER ENTRANCE LOWER DOOR SILL AT FWD FR68 GIRT BAR & INBD HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. BLENDED 
- [SDR DALA13004203213](https://openairdocs.org/sdr/DALA13004203213), Jan 23, 2013: FITTING. CORRODED. DURING INSPECTION, FOUND NR 1 ENGINE SPIGOT RECEPTACLE FITTING BORE AT UPPER SPAR HAS FITTING CORROSION. REMOVED CORROSION IAW SRM 51-74-00 FINAL DIAMETER FOUND
- [SDR DALA13003753213](https://openairdocs.org/sdr/DALA13003753213), Jan 22, 2013: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261FF HAS CORROSION 4" X 6". REPLACED FLOOR PANEL IAW SRM 51-72-00.
- [SDR DALA13003743213](https://openairdocs.org/sdr/DALA13003743213), Jan 22, 2013: FLOOR PANEL. GOUGED. DURING INSPECTION, FOUND MAIN CABIN FWD AREA FLOOR PANEL 231CF HAS GOUGE 3" X 2". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13003733213](https://openairdocs.org/sdr/DALA13003733213), Jan 22, 2013: FLOORBOARD. DAMAGED. DURING INSPECTION, FOUND MAIN CABIN, FWD AREA FLOORBOARD 232DF HAS A HOLE .300" X .500". FABRICATED FLOORBOARD IAW SRM 53-02-00, FIG 209.
- [SDR DALA13003623213](https://openairdocs.org/sdr/DALA13003623213), Jan 21, 2013: WEB. CORRODED. DURING INSPECTION, FOUND FORWARD CABIN RT SIDE STRINGER 23 BETWEEN FR 20 TO 21 UPPER SURFACE WEB CORRODED. REMOVED CORROSION IAW SRM 51-74-00. REPLACED WEB IAW 
- [SDR DALA13003563213](https://openairdocs.org/sdr/DALA13003563213), Jan 20, 2013: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241LF HAS PUNCTURE. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.
- [SDR DALA13003553213](https://openairdocs.org/sdr/DALA13003553213), Jan 20, 2013: FLOOR PANEL. DENTED. DURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241DF HAS INDENTION ON BOTTOM. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

All 115: https://openairdocs.org/deregistered/N313US-2018-09-27/reports.md

## 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 19920115005359I](https://openairdocs.org/incident/19920115005359I), Jan 15, 1992: Airbus A320211 (N313US), Seattle, WA. Pilot aborted takeoff due to loud noise in galley. Liquor kit fell to floor. Resumed flight.

## Other aircraft with N313US

- [Registered now](https://openairdocs.org/aircraft/N313US): Costruzioni Aeronautiche Tecna P2010 TDI, S/N 313/US, built 2025

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