# N316US: 1991 Airbus Industrie A320-211, registration cancelled 2018-07-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 12, 2018 - 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: 192 - Year built: 1991 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 24, 1991 - Certificate issued: January 31, 2013 - Last registry action: October 7, 2015 - Mode S code: A35EEE - 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/N316US - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=316US - Page: https://openairdocs.org/deregistered/N316US-2018-07-12 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 (78, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2018080304854](https://openairdocs.org/sdr/DALA2018080304854), Jul 11, 2017: DOOR FRAME. DAMAGED. FOUND DURING SHOP VISIT AND ACCOMPLISHMENT OF EM 5230-01163 (AD 2017-22-07) FWD CARGO DOOR PN: D5237100001000 SN: UH1192 / FRAME FORKS / OVERSIZED HOLES AT FR26 - [SDR DALA2017031001940](https://openairdocs.org/sdr/DALA2017031001940), Mar 9, 2017: LIGHT. INOPERATIVE. LAV "A" AUXILIARY EMERGENCY LIGHT IS INOP, RELAMPED. - [SDR DALA2017031001939](https://openairdocs.org/sdr/DALA2017031001939), Mar 9, 2017: LIGHT. INOPERATIVE. LAV "D" AUXILIARY EMERGENCY LIGHT IS INOP, RELAMPED. - [SDR DALA2017031001938](https://openairdocs.org/sdr/DALA2017031001938), Mar 9, 2017: LIGHT. INOPERATIVE. AFT RIGHT OVERWING DOOR HANDLE EMERGENCY LIGHT IS INOP. RELAMPED BOTH BULBS. - [SDR DALA2017031001937](https://openairdocs.org/sdr/DALA2017031001937), Mar 9, 2017: LIGHT. INOPERATIVE. FWD RIGHT OVERWING DOOR HANDLE EMERGENCY LIGHT IS INOP. RELAMPED BOTH BULBS. - [SDR DALA2016111408765](https://openairdocs.org/sdr/DALA2016111408765), Nov 14, 2016: LIGHT. INOPERATIVE. MULTIPLE BULBS INOP IN MOST LARGE EMERGENCY EXIT SIGNS, RE-LAMP. - [SDR DALA2016070605180](https://openairdocs.org/sdr/DALA2016070605180), Jul 2, 2016: LIGHT. INOPERATIVE. EMERGENCY EXIT PATH LIGHT AT SEAT ROW 23 ABC INOPERATIVE, INSTALLED NEW LIGHT ASSY. - [SDR DALA2016011300262](https://openairdocs.org/sdr/DALA2016011300262), Jan 12, 2016: CONNECTOR. DISCONNECTED. SEAT ROW 24 EMERGENCY LIGHT INOPERATIVE. RECONNECTED LIGHT ASSY. - [SDR DALA2016011200260](https://openairdocs.org/sdr/DALA2016011200260), Jan 11, 2016: STRINGER SPLICE. CORRODED. CORROSION ON STR 43L SPLICE REPAIR COUPLING BETWEEN FRAMES 56 AND 57. REPLACED STR 43L SPLICE IAW SRM 53-00-13, FIG 201. - [SDR DALA2016011200259](https://openairdocs.org/sdr/DALA2016011200259), Jan 11, 2016: STRINGER. CORRODED. CORROSION ON STR 42L BETWEEN FRAMES 56 AND 57. REPLACED STR SPLICE 42L IAW SRM 53-00-13, FIG 201. - [SDR DALA2015092205775](https://openairdocs.org/sdr/DALA2015092205775), Sep 19, 2015: LIGHT. INOPERATIVE. DURING SERVICE CHECK, INTERNAL LOADS EMERGENCY LIGHT FAULTED ON CIDS PANEL ON EMERGENCY LIGHT SYSTEM CHECK. REPAIRED LIGHT AND ALL TESTS OK. - [SDR DALA2015012700652](https://openairdocs.org/sdr/DALA2015012700652), Jan 23, 2015: WIRE. DAMAGED. DURING NON ROUTINE CHECK, FOUND SEAT ROW 9 LT EMERGENCY LIGHT INOPERATIVE. REPLACED SPLICE AT SEAT 9D EMERGENCY LIGHT AND FUNCTIONAL CHECK WAS NORMAL. - [SDR DALA2014122406702](https://openairdocs.org/sdr/DALA2014122406702), Dec 23, 2014: CONNECTOR. UNSECURE. DURING NON-ROUTINE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 18ABC. SECURED ELECTRICAL CONNECTOR AT 18ABC AND FUNCTIONAL CHECKED NORMAL. - [SDR DALA14029133216](https://openairdocs.org/sdr/DALA14029133216), May 10, 2014: WIRE. UNSECURE. DURING NON-ROUTINE CHECK, FOUND EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT SEAT 4C. MAINTENANCE SECURED WIRE AND FUNCTIONAL CHECKED NORMAL. - [SDR DALA13042633216](https://openairdocs.org/sdr/DALA13042633216), Sep 2, 2013: WIRE HARNESS. DAMAGED. DURING NON-ROUTINE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 18 ABC INOPERATIVE. MX FOUND SEAT HARNESS WIRE PULLED FROM CONNECTOR. INSTALLED NEW CONNECTO - [SDR DALA13038903216](https://openairdocs.org/sdr/DALA13038903216), Aug 11, 2013: LIGHT. DAMAGED. DURING NON ROUTINE CHECK, FOUND EMERGENCY SEAT MOUNTED LIGHT DAMAGED AND INOPERATIVE. MX REPLACED LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL. - [SDR DALA13031543216](https://openairdocs.org/sdr/DALA13031543216), Jun 25, 2013: PROFILE. CRACKED. DURING INSPECTION, FOUND CRACK ON LT AND RT LOAD TRANSMITING PROFILE LOCATED AT INTERNAL STRUCTURE OF RT FWD EMERGENCY EXIT. REPLACED LT AND RT LOAD TRANSMITTIN - [SDR DALA13031493216](https://openairdocs.org/sdr/DALA13031493216), Jun 23, 2013: PROFILE. CRACKED. DURING INSPECTION, FOUND CRACK ON LT AND RT LOAD TRANSMITTING PROFILE LOCATED INTERNAL STRUCTURE OF RT AFT EMERGENCY EXIT 844 MEASURES ARE LT L=1" RT L=3" APPRO - [SDR DALA13030893216](https://openairdocs.org/sdr/DALA13030893216), Jun 22, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 44 IN BULK CARGO COMPARTMENT BETWEEN FR 66 AND FR 67. REPAIRED IAW SRM 53-00-13. - [SDR DALA13030883216](https://openairdocs.org/sdr/DALA13030883216), Jun 22, 2013: SEAL BRACKET. CORRODED. DURING INSPECTION, FOUND CORROSION ON SEAL LOCATED UNDER INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA FWD CARGO. REPLACED SEAL LOCATED UNDER INTERNAL - [SDR DALA13030873216](https://openairdocs.org/sdr/DALA13030873216), Jun 21, 2013: CROSSBEAM. BENT. DURING INSPECTION, FOUND BEND ON CROSSBEAM LOCATED IN FWD CARGO BAY FR 32 BETWEEN STR 37L TO STR 37R. REPLACED CROSSBEAM IAW SRM 51-72-11 AND DWG. - [SDR DALA13030863216](https://openairdocs.org/sdr/DALA13030863216), Jun 21, 2013: CLEAT. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STGR 40-41R AT FR 31. REPLACED CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWE - [SDR DALA13029963216](https://openairdocs.org/sdr/DALA13029963216), Jun 19, 2013: CLEAT. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT LOCATED BETWEEN STGR 43L AND STGR 44 AT FR 32. REPLACED CLEAT IAW 51-72-11. - [SDR DALA13030133216](https://openairdocs.org/sdr/DALA13030133216), Jun 19, 2013: CLEAT. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT STR 41-42R FR 32 FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DRAWING D53231582. - [SDR DALA13030123216](https://openairdocs.org/sdr/DALA13030123216), Jun 19, 2013: CLEAT. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO BAY BETWEEN STRINGER 43 - 44L FR 32. REPLACED CLEAT AND FASTENER FWD CARGO COMPARTMENT IAW SRM 51-72-11 - [SDR DALA13029953216](https://openairdocs.org/sdr/DALA13029953216), Jun 18, 2013: CLEAT. CORRODED. DURING INSPECTION FOUND CORROSION ON CLEAT LOCATED BETWEEN STR 41R AND STR 42R AT LEVEL FR 31 FWD CARGO COMP. L=0.50", W=0.20", D=0.001" APROX. REPLACED CLEAT L - [SDR DALA13029943216](https://openairdocs.org/sdr/DALA13029943216), Jun 18, 2013: CLEAT. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 32 BETWEEN STGR 40L AND STGR 41LIN FWD CARGO COMPARTMENT L=0.800", W=0.500", D=0.001" APPROX. REPLACED - [SDR DALA13029933216](https://openairdocs.org/sdr/DALA13029933216), Jun 18, 2013: FLOORBEAM. BROKEN. DURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM FR32+4" AND Y254 FWD PAX CABIN. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00- - [SDR DALA13029923216](https://openairdocs.org/sdr/DALA13029923216), Jun 18, 2013: FLOORBEAM. BROKEN. DURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM FR.32+13" AND -Y254 FWD PAX CABIN. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53- - [SDR DALA13029913216](https://openairdocs.org/sdr/DALA13029913216), Jun 18, 2013: FLOORBEAM. BROKEN. DURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM FR 33+16" AND -Y254. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14, PARA 4. - [SDR DALA13029883216](https://openairdocs.org/sdr/DALA13029883216), Jun 18, 2013: FLOORBEAM. BROKEN. DURING INSPECTION, FOUND BROKEN UPPER FLANGE OF FLOORBEAM. PERFORMED PERMANENT REPAIR ON UPPER FLANGE OF FLOORBEAM IAW SRM 53-00-14, PARA 4.D FIG 204 (SHEET 1) - [SDR DALA13029833216](https://openairdocs.org/sdr/DALA13029833216), Jun 17, 2013: THRESHOLD. CORRODED. DURING INSPECTION, FOUND CORROSION ON THRESHOLD SHEET LOCATED BETWEEN FR 52A AND FR 56 AND BETWEEN STR 38R AND STR 39R INTERNAL STRUCTURE OF AFT CARGO COMPARTME - [SDR DALA13029203216](https://openairdocs.org/sdr/DALA13029203216), Jun 15, 2013: SPLICE. CORRODED. DURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT STR 29L AND AT LEVEL FR 67. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT STR 2 - [SDR DALA13029193216](https://openairdocs.org/sdr/DALA13029193216), Jun 15, 2013: SPLICE. CORRODED. DURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT STR 30L AND AT LEVEL FR 67. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT STR 3 - [SDR DALA13029183216](https://openairdocs.org/sdr/DALA13029183216), Jun 15, 2013: SPLICE. CORRODED. DURING INSPECTION, FOUND CORROSION ON SPLICE IN BULK CARGO COMPARTMENT AT FR 67 AT LEVEL STR 30R. REPLACED SPLICE LOCATED IN BULK CARGO COMPARTMENT AT FR.67 AT - [SDR DALA13029173216](https://openairdocs.org/sdr/DALA13029173216), Jun 15, 2013: SEAT TRACK. CORRODED. DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, FWD PAX CABIN BETWEEN FR 20 TO FR 24 AND -Y1292 L=3.00", W=0.500",D=0.005" APPROX, REPLACED SEAT TRACK FWD PAX - [SDR DALA13029163216](https://openairdocs.org/sdr/DALA13029163216), Jun 15, 2013: SKIN. CORRODED. DURING INSPECTION, FOUND CORROSION ON UPPER SHEET METAL LOCATED BETWEEN FR 24A AND FR 28, S39-41R IN FWD CARGO COMPARTMENT. MEASURES L=1.5" W=0.300", D=0.002 AP - [SDR DALA13029133216](https://openairdocs.org/sdr/DALA13029133216), Jun 14, 2013: FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 16 AND FR 20 AT LEVEL STR 23 RT L=0.500" W=0.250" D=0.001" APPROX. REPLACED CENTER FITTI - [SDR DALA13029123216](https://openairdocs.org/sdr/DALA13029123216), Jun 14, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 RT SIDE L=0.500", W=0.250", D=0.001" APPROX. REPLACED LOWER SILL LOCATED BETWEE - [SDR DALA13029113216](https://openairdocs.org/sdr/DALA13029113216), Jun 14, 2013: FLOORBEAM. CORRODED. DURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE, FR 66 LEVEL Y-1292. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472230. - [SDR DALA13029103216](https://openairdocs.org/sdr/DALA13029103216), Jun 14, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT STRUCTURE, LOCATED AFT PAX CABIN, AT FR 68 LEVEL Y-1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11. - [SDR DALA13029093216](https://openairdocs.org/sdr/DALA13029093216), Jun 14, 2013: FLOORBEAM. CORRODED. DURING INSPECTION, FOUND CORROSION ON FLOORBEAM STRUCTURE, LOCATED AFT PAX CABIN AT FR 67+13", LEVEL Y-1162. REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG NR D534 - [SDR DALA13029073216](https://openairdocs.org/sdr/DALA13029073216), Jun 14, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FR 66 AND FR 68 LT SIDE L=1", W=0.500", D=0.002" APROX. REPLACED LOWER SILL AND FASTENERS LOCAT - [SDR DALA13029013216](https://openairdocs.org/sdr/DALA13029013216), Jun 13, 2013: FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CORNER FITTING LOCATED FR 68 AT LEVEL STR 23 RT L=0.500" W=0.250" D=0.001" APPROX. REPLACED CORNER FITTING LOCATED FR 68 A - [SDR DALA13028993216](https://openairdocs.org/sdr/DALA13028993216), Jun 13, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND CORROSION ON SUPPORT LOCATED AT FR.68 AT LEVEL OF S24R IN AFT PAX CABIN. REPLACED SUPPORT SECTION IAW SRM 51-72-11 AND DWG D53470150. - [SDR DALA13028953216](https://openairdocs.org/sdr/DALA13028953216), Jun 13, 2013: FLOORBOARD. CORRODED. DURING INSPECTION, FOUND CORROSION ON OTBD UPPER FLOORBOARD SPLICE LOCATED AFT PAX CABIN AT FR.64, LEVEL Y-765, SSI 534147. L=1", W=0.5", D=0.003" APPROX. REPLA - [SDR DALA13029493216](https://openairdocs.org/sdr/DALA13029493216), Jun 12, 2013: FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CORNER FITTING AND FASTENERS LOCATED FR 68 AT STR 23. REPLACED CORNER FITTING AND FASTENERS IAW SRM 51-72-11 AND DWG NR D5 - [SDR DALA13029483216](https://openairdocs.org/sdr/DALA13029483216), Jun 12, 2013: WEB. CORRODED. DURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FR20 TO FR21 AND AT LEVEL -Y1680 FWD PAX CABIN. REPLACED WEB IAW SRM 51-72-11 AND DWG D53112783. - [SDR DALA13028873216](https://openairdocs.org/sdr/DALA13028873216), Jun 12, 2013: FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON FITTING LOCATED INTERNAL STRUCTURE OF CUT OUT DOOR LOCKING FITTING AREA AND BETWEEN FR 26 AND FR 27 FWD CARGO. REPLACED FI - [SDR DALA13028563216](https://openairdocs.org/sdr/DALA13028563216), Jun 11, 2013: SKIN. DENTED. DURING INSPECTION, FOUND DENT ON EXTERNAL FUSELAGE SKIN LOCATED FR 24+7" AND BETWEEN STR 41L AND STR 42L. PERFORMED PERMANENT REPAIR ON EXTERNAL FUSELAGE SKIN B All 78: https://openairdocs.org/deregistered/N316US-2018-07-12/reports.md ## Other aircraft with N316US - [Registered now](https://openairdocs.org/aircraft/N316US): Costruzioni Aeronautiche Tecna P2010 TDI, S/N 316/US, built 2025 --- 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.