# N315US: 1991 Airbus Industrie A320-211, registration cancelled 2018-01-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 24, 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: 171
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 18, 1991
- Certificate issued: January 31, 2013
- Last registry action: October 7, 2015
- Mode S code: A35B37
- 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/N315US
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=315US
- Page: https://openairdocs.org/deregistered/N315US-2018-01-24

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 (105, newest 50)

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

- [SDR DALA2017031302068](https://openairdocs.org/sdr/DALA2017031302068), Mar 12, 2017: LENS. MISSING. FLOOR EMERGENCY LIGHT AT SEAT 11C RED LENS MISSING, REPLACED THE BULB AND LENS.
- [SDR DALA2017031001941](https://openairdocs.org/sdr/DALA2017031001941), Mar 9, 2017: WIRE. BROKEN. ROW 9 EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN WIRE.
- [SDR DALA2017020801180](https://openairdocs.org/sdr/DALA2017020801180), Feb 8, 2017: BULB. INOPERATIVE. R2 DOOR EMERGENCY LIGHT SIGN ABOVE DOOR, ONE BULB INOPERATIVE, REPLACED THE BULB.
- [SDR DALA2016122210072](https://openairdocs.org/sdr/DALA2016122210072), Dec 20, 2016: COMPRESSOR. SEIZED. HAD AN ACRID ELECTRICAL ODOR IN THE COCKPIT. REPLACED THE WATER SYSTEM AIR COMPRESSOR. FOUND SEIZED. AIRCRAFT RETURNED TO SERVICE.
- [SDR DALA2016102807847](https://openairdocs.org/sdr/DALA2016102807847), Oct 28, 2016: WIRE. BROKEN. BROKEN EMERGENCY LIGHT WIRE, REPAIRED THE WIRE.
- [SDR DALA2015111206952](https://openairdocs.org/sdr/DALA2015111206952), Nov 11, 2015: SKIN. CORRODED. CORROSION ON INSIDE SURFACE OF SKIN OTBD OF STR 42L BETWEEN FRAMES 56-57. PRI 541258-14AD, REV O,1,2. C/W PRI 541258-14AD, REV 2, STEP 9.
- [SDR DALA2015111206951](https://openairdocs.org/sdr/DALA2015111206951), Nov 11, 2015: SKIN. CORRODED. CORROSION ON SKIN UNDER STR 43L BETWEEN FRAME 56 & 57, PRI 541258-14AD, REV 0, 1, 2 AND ER/A 541258-14AD. BLENDED OUT CORROSION UNDER SKIN IAW 51-74-00, MININUM
- [SDR DALA2015111206950](https://openairdocs.org/sdr/DALA2015111206950), Nov 11, 2015: STRINGER. CORRODED. CORROSION ON STR 42L BETWEEN 56-57. EXISTING REPAIR BETWEEN FRAMES 57-58 AND A SPLICE UNDER FRAME 53. FABRICATED STR 42L BETWEEN FRAMES 55 & 58 AND COUPLER IAW 
- [SDR DALA2015111206949](https://openairdocs.org/sdr/DALA2015111206949), Nov 11, 2015: STRINGER. CORRODED. CORROSION ON STR 43L BETWEEN FRAMES 56-57. EXISTING SPLICE BETWEEN FRAMES 56-57 AND A SPLICE UNDER FRAME 54. FABRCATED STR 43L BETWEEN FRAMES 55 & 58 AND COUPLE
- [SDR DALA13017723215](https://openairdocs.org/sdr/DALA13017723215), Apr 15, 2013: SKIN. CORRODED. DURING INSPECTION, FOUND CORROSION ON SKIN, AFT CARGO BAY S38R+1.5 AND FR 64+20. PERFORMED PERMANENT REPAIR ON SKIN IAW ERA 513499-14, REV ORIGINAL AND PR I N. 
- [SDR DALA13017703215](https://openairdocs.org/sdr/DALA13017703215), Apr 15, 2013: WEB. CORRODED. DURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY S38L BETWEEN FR 56 AND FR 57 LOWER SURFACE. PERFORMED REPAIR ON WEB IAW ERA 513503-14, REV ORIGINAL P
- [SDR DALA13017373215](https://openairdocs.org/sdr/DALA13017373215), Apr 15, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 41R LOCATED BETWEEN FR 28 TO FR 29 IN FORWARD CARGO COMPARTMENT; MEASURES APROX L=0.250" W=0.100" D= 0.002" PERFO
- [SDR DALA13017793215](https://openairdocs.org/sdr/DALA13017793215), Apr 14, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION STRINGER 43L, AFT CARGO BETWEEN FR 58 AND FR 59. PERFORMED PERMANENT REPAIR IAW SRM 53-00-13, PARA 4.A FIG 201, PAGES 202 TO 
- [SDR DALA13016873215](https://openairdocs.org/sdr/DALA13016873215), Apr 13, 2013: TRUNNION. WORN. DURING INSPECTION, FOUND SEVERE WEAR ON LOWER SURFACE OF LT INBD FLAP DRIVE TRUNNION, MEASURE THE OUTSIDE DIAMETER OF THE TRUNNION SHAFT IS:2.864". REPLACED LT 
- [SDR DALA13016853215](https://openairdocs.org/sdr/DALA13016853215), Apr 13, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 35R AFT CARGO COMP FR 64+20". REPLACED STRINGER 35R IAW SRM 51-72-11.
- [SDR DALA13016843215](https://openairdocs.org/sdr/DALA13016843215), Apr 13, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 44 BETWEEN FR 31 TO FR 32 AND Y 0 FWD CARGO COMPARTMENT. PERFORMED REPAIR ON STRINGER 44 IAW ER/A NR 512769-14. R
- [SDR DALA13016833215](https://openairdocs.org/sdr/DALA13016833215), Apr 13, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 41R BETWEEN FR 32 TO FR 33 FORWARD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER 41R IAW ER/A NR 512764-14, R
- [SDR DALA13016813215](https://openairdocs.org/sdr/DALA13016813215), Apr 12, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 43L, AFT CARGO BAY BETWEEN FR 64 AND STR 65. PERFORMED PERMANENT REPAIR ON STRINGER 43L IAW SRM A320 53-00-13, FI
- [SDR DALA13016803215](https://openairdocs.org/sdr/DALA13016803215), Apr 12, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 35R, AFT CARGO BAY FR 64+15". REPLACED STRINGER 35R, IAW SRM 51-72-11.
- [SDR DALA13016793215](https://openairdocs.org/sdr/DALA13016793215), Apr 12, 2013: SKIN. CORRODED. DURING INSPECTION, FOUND SEVERE CORROSION ON INTERNAL SURFACE SKIN LOCATED BETWEEN FR 33 TO FR 34 AND STRINGERS 39R TO 41L IN FWD CARGO COMPARTMENT. PERFORMED P
- [SDR DALA13016783215](https://openairdocs.org/sdr/DALA13016783215), Apr 12, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 41R LOCATED BETWEEN FR 31 TO FR 32 IN FORWARD CARGO COMPARTMENT. PEFORMED REPAIR ON STRINGER 41R IAW ER/A NR 5127
- [SDR DALA13016773215](https://openairdocs.org/sdr/DALA13016773215), Apr 12, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 44 LOCATED BTW FR 24 TO FR 24A IN FORWARD CARGO COMPARTMENT. PERFORMED REPAIR ON STRINGER 44 IAW ER/A 512766-14 R
- [SDR DALA13015943215](https://openairdocs.org/sdr/DALA13015943215), Apr 10, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 43R LOCATED BTW FR 32 TO FR 33 IN FORWARD CARGO COMPARTMENT; MEASURES APROX. POINT 1 L=0.100" W=0.098" D=0.001"; 
- [SDR DALA13015933215](https://openairdocs.org/sdr/DALA13015933215), Apr 10, 2013: WEB. CORRODED. DURING INSPECTION, FOUND CORROSION ON WEB LOCATED BETWEEN FR 51 TO FR 52 STR 38R IN AFT CARGO COMPARTMENT (AFTER REMOVED PROFILE LOC BETWEEN FR 48 AND FR 52A ST
- [SDR DALA13016193215](https://openairdocs.org/sdr/DALA13016193215), Apr 9, 2013: CARGO TRACK. CORRODED. DURING INSP, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=3.5" W=0.300" D=0.003" REPLA
- [SDR DALA13016183215](https://openairdocs.org/sdr/DALA13016183215), Apr 9, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 34 AND BETWEEN STR 42R TO STR 43R IN FWD CARGO COMPARTMENT. MEASURES APROX. L=2.00" W=0.300" D=0.003" REPLACED
- [SDR DALA13016173215](https://openairdocs.org/sdr/DALA13016173215), Apr 9, 2013: COVER. CORRODED. DURING INSPECTION, FOUND CORROSION ON COVER SHEET, AFT CARGO COMP. DOOR (L=1.900"; W=0.155" AND DEPT=0.001") REPLACED COVER SHEET, AFT CARGO COMPT. DOOR IAW SRM
- [SDR DALA13015893215](https://openairdocs.org/sdr/DALA13015893215), Apr 9, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 40R LOCATED AT LEVEL FR 34 IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.175" W=0.120"D=0.001" PERFORM
- [SDR DALA13015833215](https://openairdocs.org/sdr/DALA13015833215), Apr 9, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT. MEASURES APROX. L=0.800" W=0.300" D=0.002". RE
- [SDR DALA13015823215](https://openairdocs.org/sdr/DALA13015823215), Apr 9, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 43L TO STR 43R IN FORWARD CARGO COMPARTMENT. MEASURES APROX. L=3.00" W=0.350" D=0.002". REP
- [SDR DALA13015903215](https://openairdocs.org/sdr/DALA13015903215), Apr 8, 2013: STRINGER. WORN. DURING INSPECTION, FOUND WEAR ON STRINGER 42L, AFT COMP BETWEEN FR 57 AND FR 58. PERFORMED PERMANENT REPAIR ON STRINGER 42L BETWEEN FR 57 TO FR58 AFT CARGO COMP
- [SDR DALA13015073215](https://openairdocs.org/sdr/DALA13015073215), Apr 7, 2013: STRINGER SPLICE. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE, AFT CARGO BAY STR 38R, FR 51 (L=0.026", W=0.017" AND D=0.003") WC 5320-5010. REPLACED STRINGER SPLICE LOC
- [SDR DALA13015063215](https://openairdocs.org/sdr/DALA13015063215), Apr 7, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 29 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT; MEASURES APROX L=1.700" W=0.300" D=0.002".
- [SDR DALA13015053215](https://openairdocs.org/sdr/DALA13015053215), Apr 6, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND AFT CABIN UTILITY ARE FLOOR SUPPORT BETWEEN FR 64-66,Y765 UPPER SURFACE FLANGE HAS CORROSION. BLENDED AREA L=1.8",W=1.8"D=.034", MAX AL
- [SDR DALA13015043215](https://openairdocs.org/sdr/DALA13015043215), Apr 5, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT; MEASURES APROX. L=0.750",W=0.250", D=0.002". REPLA
- [SDR DALA13015033215](https://openairdocs.org/sdr/DALA13015033215), Apr 5, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 38R TO STR 39R IN FORWARD CARGO COMPARTMENT L=0.800", W=0.250", D=0.002" MEASURES APPROX SS
- [SDR DALA13015023215](https://openairdocs.org/sdr/DALA13015023215), Apr 5, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT; MEASURES APROX L=2.00", W=0.310", D=0.002". RE
- [SDR DALA13014993215](https://openairdocs.org/sdr/DALA13014993215), Apr 4, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 43R TO STR 43L IN FORWARD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=3.5" W=0.375" D=0.
- [SDR DALA13014703215](https://openairdocs.org/sdr/DALA13014703215), Apr 4, 2013: FITTING. CORRODED. CORROSION ON CORNER FITTING LOCATED FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE. L=4" W=1.25" D=0.003" APPROX. REPLACED CORNER FITTING LOCATED FR 68 RT SIDE AFT CAB
- [SDR DALA13014693215](https://openairdocs.org/sdr/DALA13014693215), Apr 4, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BTW FR 66 AND FR 68 RT SIDE AFT CABIN FLOOR STRUCTURE L=2" W=1.5" D=0.003" APPROX. SSI 534147. REPLACED
- [SDR DALA13014683215](https://openairdocs.org/sdr/DALA13014683215), Apr 4, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=1.300" W=0.350" D=0.0
- [SDR DALA13014713215](https://openairdocs.org/sdr/DALA13014713215), Apr 3, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.500" =0.800" D=0.002". REP
- [SDR DALA13014673215](https://openairdocs.org/sdr/DALA13014673215), Apr 3, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 34 AND BETWEEN STR 41R TO STR 42R IN FWD CARGO COMPARTMENT SSI 532180; MEASURES APROX L=2.100" W=0.300" D=0.00
- [SDR DALA13014663215](https://openairdocs.org/sdr/DALA13014663215), Apr 3, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 43L TO STR 43R IN FWD CARGO COMPARTMENT; MEASURES APROX. L=3.00" W=0.375" D=0.003". REPLACE
- [SDR DALA13014653215](https://openairdocs.org/sdr/DALA13014653215), Apr 3, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 31 AND BETWEEN STR 43R TO STR 44 IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=0.750" W=0.210" D=0.002". REP
- [SDR DALA13014643215](https://openairdocs.org/sdr/DALA13014643215), Apr 3, 2013: STRINGER. CORRODED. DURING INSPECTION, FOUND CORROSION ON STRINGER 25R, BULK CARGO COMP BETWEEN FR 64 AND FR 65. REPLACED STRINGER 25R LOCATED BULK CARGO COMPARTMENT BETWEEN FR 64 
- [SDR DALA13014633215](https://openairdocs.org/sdr/DALA13014633215), Apr 3, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 40R TO STR 41R IN FWD CARGO COMPARTMENT; MEASURES APPROX. L=0.800" W=0.300" D=0.002". REPLA
- [SDR DALA13014623215](https://openairdocs.org/sdr/DALA13014623215), Apr 3, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 30 AND BETWEEN STR 41R TO STR 42R IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.500" W=0.300" D=0.002". RE
- [SDR DALA13014613215](https://openairdocs.org/sdr/DALA13014613215), Apr 3, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 32 AND BETWEEN STR 42L TO STR 43L IN FORWARD CARGO COMPARTMENT; MEASURES APROX. L=1.00" W=0.310" D=0.002". REP
- [SDR DALA13014603215](https://openairdocs.org/sdr/DALA13014603215), Apr 3, 2013: ATTACH FITTING. CORRODED. DURING INSPECTION, FOUND CORROSION ON CLEAT AT FR 33 AND BETWEEN STR 42R TO STR 43R IN FORWARD CARGO COMPARTMENT SSI 532180; MEASURES APROX. L=0.750" W=0.210 " 

All 105: https://openairdocs.org/deregistered/N315US-2018-01-24/reports.md

## Other aircraft with N315US

- [Registered now](https://openairdocs.org/aircraft/N315US): DJI AGRAS T50, S/N 1581F6BUB236S0010094

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