# N310NW: 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: [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: 121
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 14, 1990
- Certificate issued: December 31, 2009
- Last registry action: March 7, 2016
- Mode S code: A34812
- 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/N310NW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=310NW
- Page: https://openairdocs.org/deregistered/N310NW-2018-09-27

From the FAA registry file of October 31, 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 (135, newest 50)

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

- [SDR DALA2018080583210](https://openairdocs.org/sdr/DALA2018080583210), Jan 17, 2018: DOOR FRAME. CRACKED. FWD CARGO DOOR FRAME FORKS HAD OVERSIZED AND CRACKED HOLES AT FRAMES 54 - 54A. REPAIRED IAW ER/A 570292-14AD SECTION 1.
- [SDR DALA2017011100269](https://openairdocs.org/sdr/DALA2017011100269), Jan 10, 2017: POWER SUPPLY. INOPERATIVE. DURING EMERGENCY LIGHT SYSTEM TEST, FOUND RIGHT POWER SUPPLY UNIT INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY.
- [SDR DALA2016122610070](https://openairdocs.org/sdr/DALA2016122610070), Dec 24, 2016: LAMP. INOPERATIVE. RT AFT OVERWING HANDLE EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.
- [SDR DALA2016122610069](https://openairdocs.org/sdr/DALA2016122610069), Dec 24, 2016: LAMP. INOPERATIVE. RT FWD EMERGENCY OVERWING HANDLE EMERGENCY LIGHT INOPERATIVE, REPLACED THE LAMP.
- [SDR DALA2016121209829](https://openairdocs.org/sdr/DALA2016121209829), Dec 11, 2016: SKIN. DAMAGED. EVIDENCE REWORK PASSENGER CREW DOOR 832 EXTERNAL SKIN LOCATED 15" FROM LOWER EDGE AND 30.5" FROM FWD EDGE AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON PASS
- [SDR DALA2016120509633](https://openairdocs.org/sdr/DALA2016120509633), Dec 4, 2016: ACCESS PANEL. CORRODED. CORROSION ON ACCESS PANEL 640JB ON RT WING. REPLACED ACCESS PANEL 640JB ON RT WING
- [SDR DALA2016120509632](https://openairdocs.org/sdr/DALA2016120509632), Dec 4, 2016: ACCESS PANEL. CORRODED. CORROSION ON ACCESS PANEL 540PB FUEL TANK ON LT WING. REPLACED ACCESS PANEL 540PB ON LT WING.
- [SDR DALA2016120209623](https://openairdocs.org/sdr/DALA2016120209623), Dec 2, 2016: SKIN. DAMAGED. EXISTING REWORK ON EXTERNAL SKIN AT LOWER FUSELAGE TO FRAME 31+17" BETWEEN STRINGER 42R TO STRINGER 43R, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BTW FR31TO 
- [SDR DALA2016063005103](https://openairdocs.org/sdr/DALA2016063005103), Jun 28, 2016: LIGHT. BROKEN. ROW 7ABC EMERGENCY SEAT LIGHT INOPERATIVE, REPAIRED BROKEN .
- [SDR DALA2015050703116](https://openairdocs.org/sdr/DALA2015050703116), May 5, 2015: WIRE. BROKEN. DURING NON-ROUTINE CHECK, FOUND CABIN EMERGENCY LIGHTS INOPERATIVE AT SEAT ROW 7AB. T/S AND FOUND BROKEN WIRE AT CABIN SEAT ROW 7 A/B. SPLICED WIRE AND FUNCTION
- [SDR DALA14003343210](https://openairdocs.org/sdr/DALA14003343210), Jan 15, 2014: WIRE. BROKEN. DURING CHECK, FOUND SEAT 7ABC EMERGENCY SEAT LIGHT INOPERATIVE. REPAIRED A BROKEN WIRE UNDER SEAT. FUNCTIONAL CHECKED NORMAL.
- [SDR DALA13022183210](https://openairdocs.org/sdr/DALA13022183210), May 11, 2013: WIRE. BROKEN. DURING IINSPECTION, FOUND EMERGENCY PATH LIGHT AT SEAT 6 WIRE BROKEN UNDER 6A. MX RECONNECTED WIRE AT 6A AND FUNCTIONAL CHECK WAS NORMAL.
- [SDR DALA12016903210](https://openairdocs.org/sdr/DALA12016903210), Dec 18, 2012: SILL. CORRODED. DURING INSPECTION, FOUND FWD CARGO PIT DOOR SILL HAS CORROSION IN SEVERAL PLACES AS MARK NR 130/54. REMOVED CORROSION IAW SRM 51-74-00, NO ESTABLISH LIMITS. REM
- [SDR DALA12016693210](https://openairdocs.org/sdr/DALA12016693210), Dec 18, 2012: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152RF DAMAGED AND DAMAGE DIM L=3" X W=2". FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007.
- [SDR DALA12016683210](https://openairdocs.org/sdr/DALA12016683210), Dec 18, 2012: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152QF DAMAGED WITH DIM OF DAMAGED L=2" X W=1.5". FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007.
- [SDR DALA12016423210](https://openairdocs.org/sdr/DALA12016423210), Dec 16, 2012: BEAM. CORRODED. DURING INSPECTION, FOUND FWD LT OVERWING EMERGENCY EXIT DOOR CURVED BEAM HAS CORROSION. REMOVED CORROSION FROM CURVED BEAM IAW SRM 51-74-00 AND CHECK LIMITS ORI
- [SDR DALA12016413210](https://openairdocs.org/sdr/DALA12016413210), Dec 16, 2012: SUPPORT ANGLE. CORRODED. DURING INSPECTION, FOUND LT FWD OVERWING EMERGENCY EXIT DOOR AFT VERTICAL FRAME ANGLE SUPPORT CORRODED. REMOVED VERTICAL FRAME ANGLE SUPPORT IAW SRM 51-42-11. R
- [SDR DALA12016243210](https://openairdocs.org/sdr/DALA12016243210), Dec 13, 2012: FRAME. CORRODED. DURING INSPECTION, FOUND RT AFT PASSENGER DOOR SILL AFT FRAME 66, UPPER SURFACE AROUND NUT PLATE HOLES HAS CORROSION. BLENDED OUT CORROSION IAW SRM 51-74-00. DI
- [SDR DALA12016233210](https://openairdocs.org/sdr/DALA12016233210), Dec 13, 2012: ATTACH FITTING. CHAFED. DURING INSPECTION, FOUND CHAFED MARK ON LT AFT PAX DOOR ASSIST CYLINDER ATTACHMENT FITTING. BLENDED OUT DAMAGE IAW SRM 51-73-00. DIM OF REWORK L=.4", W=.2", D=.
- [SDR DALA12016223210](https://openairdocs.org/sdr/DALA12016223210), Dec 13, 2012: PLATE. DAMAGED. DURING INSPECTION, FOUND LT WING SLAT TRACK NR 6, CLOSING PLATE CHAFING WITH SLAT LOWER T/E. BLENDED OUT CHAFE DAMAGE IAW SRM 51-73-00. DIM OF REWORK L=3.2", W=
- [SDR DALA12016283210](https://openairdocs.org/sdr/DALA12016283210), Dec 13, 2012: RIB. CORRODED. DURING INSPECTION, FOUND LT OTBD FLAP, INBD RIB L/E HAS 2 AREAS OF PITTING AFTER RUB STRIP REMOVAL. BLENDED CORROSION IAW SRM 51-74-00, AREA L 1 =1.5" W=1.0 "D 
- [SDR DALA12016013210](https://openairdocs.org/sdr/DALA12016013210), Dec 12, 2012: PANEL. CRACKED. DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151CF CRACKED 6.0 INCHES LONG. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 L=6.0, W=.100 OUT OF LIMITS IAW 5
- [SDR DALA12016003210](https://openairdocs.org/sdr/DALA12016003210), Dec 12, 2012: PANEL. PUNCTURED. DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 162EF MULTIPLE PUNCTURES. SLOPE PANEL FABRICATED IAW FIG 209, DIAMETER OF PUNCTURE .350 AREA (1) .400 AREA (2) FO
- [SDR DALA12015993210](https://openairdocs.org/sdr/DALA12015993210), Dec 12, 2012: PANEL. DAMAGED. DURING INSPECTION, FOUND AFT CARGO SLOPE PANEL 151HF HAS EDGE DAMAGE BEYOND ALLOWABLE LIMITS. SLOPE PANEL FABRICATED IAW 53-02-00. DAMAGE LOCATED AT EDGE OF CUT
- [SDR DALA12015983210](https://openairdocs.org/sdr/DALA12015983210), Dec 12, 2012: FLOOR PANEL. DAMAGED. DURING INSPECTION, FOUND FLOOR PANEL 241AF IS SOFT AND SPONGY. REMOVED CABIN FLOOR PANEL IAW MM 53-12-12-000-001-A. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG
- [SDR DALA12015913210](https://openairdocs.org/sdr/DALA12015913210), Dec 11, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, FOUND AFT CARGO BAY AT FRAME 58, STR 44 BEAM HAS CORROSION. REMOVED CORROSION IAW 51-74-00. AREA MEASURES L=1.0"X W=.80"X D=.012" ORG MAT .07
- [SDR DALA12015973210](https://openairdocs.org/sdr/DALA12015973210), Dec 11, 2012: ATTACH BRACKET. CORRODED. DURING INSPECTION, FOUND AFT CARGO COMPT FRAME 58, STR 36-38L, SEAL PLATE ATTACHMENT BRACKET HAS CORROSION. FOUND AFTER SEAL PLATE REMOVAL. REMOVED CORROSION IA
- [SDR DALA12016293210](https://openairdocs.org/sdr/DALA12016293210), Dec 10, 2012: CARRIAGE. GOUGED. DURING INSPECTION, FOUND RT WING NR 1 FLAP TRACK, FLAP CARRIAGE FWD LOWER TRACK HAS GOUGE (2 EA). ACCOMPLISHED RT WING NR 1 FLAP TRACK, FLAP CARRIAGE FWD LWR TR
- [SDR DALA12015713210](https://openairdocs.org/sdr/DALA12015713210), Dec 10, 2012: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 221FF CORRODED ON LWR SURFACE 3.5" X 2.0". REPLACED FLOOR PANEL IAW SRM 51-72-00.
- [SDR DALA12015503210](https://openairdocs.org/sdr/DALA12015503210), Dec 8, 2012: WEB. CORRODED. DURING INSPECTION, FOUND FORWARD CABIN RT SIDE AT FR 16 STRINGER 23 UPPER SURFACE WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1", W=
- [SDR DALA12015493210](https://openairdocs.org/sdr/DALA12015493210), Dec 8, 2012: SKIN. DAMAGED. DURING INSPECTION, FOUND RT SIDE LOWER AFT FUSELAGE FR 69,S28-29R EXTERNAL SKIN SURFACE HAS PRE-EXISTING TOOL MARK (APPEARS TO BE FROM FASTENER REPLACEMENT). RE
- [SDR DALA12015433210](https://openairdocs.org/sdr/DALA12015433210), Dec 6, 2012: FLOOR PANEL. CRACKED. DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 221EF CRACKED 4.0" X 1.0". AND FWD UTILITY PANEL 221EF. REPLACED IAW SRM 51-72-00.
- [SDR DALA12015703210](https://openairdocs.org/sdr/DALA12015703210), Dec 4, 2012: SKIN. DAMAGED. DURING INSPECTION, FOUND LOWER FUSELAGE HAS LIGHTNING STRIKE ON THIRD FASTENER ON STRINGER 42R FWD OF FR 31. REMOVED FASTENER & REAMED HOLE IAW SRM 53-21-11, FI
- [SDR DALA12015483210](https://openairdocs.org/sdr/DALA12015483210), Dec 4, 2012: HINGE PIN. CORRODED. DURING INSPECTION, FOUND LT WING SPOILER NR 4 CENTER HINGE INBD PIN CORRODED. RECEIVED NEW CTR PIN TO BE INSTALLED ON JIC 5770-1010S-LT.
- [SDR DALA12015033210](https://openairdocs.org/sdr/DALA12015033210), Dec 4, 2012: HINGE PIN. CORRODED. DURING INSPECTION, FOUND RT WING NR 5 SPOILER BOTH INBD AND OTBD CTR HINGE PIN HAS CORROSION AND THREAD DAMAGED. RECEIVED NEW CTR PINS INSTALLED ON JIC 5770-101
- [SDR DALA12015023210](https://openairdocs.org/sdr/DALA12015023210), Dec 4, 2012: HINGE PIN. CORRODED. DURING INSPECTION, FOUND LT WING SPOILER NR 5 CENTER HINGE INBD PIN CORROD PIN INSTALLED ON JIC 5770-1010S-LT.
- [SDR DALA12015013210](https://openairdocs.org/sdr/DALA12015013210), Dec 4, 2012: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262FF CORRODED 3.0" X 3.0". REPLACED FLOOR PANEL IAW SRM 51-72-00.
- [SDR DALA12015003210](https://openairdocs.org/sdr/DALA12015003210), Dec 4, 2012: THRESHOLD. CORRODED. DURING INSPECTION, FOUND AFT CARGO THRESHOLD PANEL 152KF CORRODED.3.5 X 3.5. REPLACED AFT CARGO THRESHOLD PANEL IAW SRM 51-72-00.
- [SDR DALA12014993210](https://openairdocs.org/sdr/DALA12014993210), Dec 3, 2012: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262EF WITH MULTIPLE CORRODED INSERTS. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.
- [SDR DALA12014983210](https://openairdocs.org/sdr/DALA12014983210), Dec 3, 2012: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL PUNCTURED 261DF 4.0" X 4.0". FABRICATED FLOOR PANEL IAW DWG.
- [SDR DALA12014973210](https://openairdocs.org/sdr/DALA12014973210), Dec 3, 2012: FLOOR PANEL. PUNCTURED. DURING INSPECTION, FOUND FWD UTILITY FLOOR PANEL 222CF PUNCTURED "2.5 X 3.0". FABRICATED FLOOR PANEL IAW DWG 3D25-37498.
- [SDR DALA12014963210](https://openairdocs.org/sdr/DALA12014963210), Dec 3, 2012: FLOOR PANEL. CRACKED. DURING INSPECTION, FOUND MAIN CABIN FLOOR PANEL 231YF CRACKED 7.0" LONG. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.
- [SDR DALA12014943210](https://openairdocs.org/sdr/DALA12014943210), Dec 3, 2012: FLOOR PANEL. CORRODED. DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF WITH CORRODED INSERTS. FABRICATED FLOOR PANEL IAW DWG 3D25-37498.
- [SDR DALA12014773210](https://openairdocs.org/sdr/DALA12014773210), Dec 3, 2012: FLOOR SUPPORT. CRACKED. DURING NON ROUTINE CHECK, FOUND COCKPIT FLOOR SUPPORT BETWEEN FR 8-11 Y-765 WEB CRACKED. REMOVED WEB FROM FR8 TO FR11 Y-765 IAW SRM 51-42-11. RECEIVED NEW WEB P
- [SDR DALA12014763210](https://openairdocs.org/sdr/DALA12014763210), Dec 3, 2012: FLOOR PANEL. PUNCTURED. DURING NON ROUTINE CHECK, FOUND AFT UTILITY FLOOR PANEL 262AB PUNCTURED 2.0" X 2.0". FABRICATED FLOOR PANEL IAW DWG.
- [SDR DALA12014433210](https://openairdocs.org/sdr/DALA12014433210), Dec 1, 2012: PANEL. DAMAGED. DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 151BF DAMAGED 4.0" X 4.0". FABRICATED SLOPE PANEL 151BF ON STAM TRAVELER T12/971271 IAW DWG 3D25-37705.
- [SDR DALA12014423210](https://openairdocs.org/sdr/DALA12014423210), Dec 1, 2012: PANEL. DAMAGED. DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152BF DAMAGED 6.5" X 6.5". FABRICATED SLOPE PANEL 152BF ON STAM TRAVELER T12/971269 IAW DWG 3D25-37705.
- [SDR DALA12014413210](https://openairdocs.org/sdr/DALA12014413210), Dec 1, 2012: PANEL. DAMAGED. DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152CF DAMAGED 4.0" X 5.0". FABRICATED SLOPE PANEL 152CF ON STAM TRAVELER T12/971268 IAW DWG 3D25-37705.
- [SDR DALA12014403210](https://openairdocs.org/sdr/DALA12014403210), Dec 1, 2012: PANEL. DAMAGED. DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152EF DAMAGED 3.0" X 3.0". FABRICATED SLOPE PANEL 152EF ON STAM TRAVELER T12/971263 IAW DWG 3D25-37705.
- [SDR DALA12014393210](https://openairdocs.org/sdr/DALA12014393210), Dec 1, 2012: PANEL. DAMAGED. DURING NON ROUTINE CHECK, FOUND AFT CARGO SLOPE PANEL 152FF DAMAGED 5.0" X 5.0". FABRICATED SLOPE PANEL 152FF ON STAM TRAVELER T12/971261 IAW DWG 3D25-37705.

All 135: https://openairdocs.org/deregistered/N310NW-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 CHI97IA034](https://openairdocs.org/ntsb/CHI97IA034), Nov 24, 1996: Airbus Industrie A-320-211 (N310NW), Romulus, MI, incident, no damage. Probable cause: restricted movement of the autopilot mode engagement/disengagement lever bearing in the rudder artificial feel and trim unit. A factor relating to this incident was: company management not…

## FAA accident and incident reports (2)

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 19961124042649I](https://openairdocs.org/incident/19961124042649I), Nov 24, 1996: Airbus A320211 (N310NW), Detroit, MI. Narrative: on November 24, 1996, while on approach into Detroit Wayne county airport, northwest airlines flight 211'S captain reported "after approach in light…
- [Incident 19940227007009I](https://openairdocs.org/incident/19940227007009I), Feb 27, 1994: Airbus A320211 (N310NW), Detroit, MI, Minor damage. Aircrafts left winglet struck a parked B727 while taxiing.

## Other aircraft with N310NW

- [Registered now](https://openairdocs.org/aircraft/N310NW): DJI AGRAS T50, S/N 1581F6BUB235H0010027

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