# N949DN: 1997 Mcdonnell Douglas MD-90-30, registration cancelled 2022-12-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 17, 2022 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas MD-90-30](https://openairdocs.org/model/mcdonnell-douglas-md-90-30) (registry code 302369A) - Engine: [IAE V2528-D5](https://openairdocs.org/engine/iae-v2528-d5) (registry code 34609) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E40NE](https://openairdocs.org/tcds/E40NE) (OpenAirDocs) - Serial number: 53358 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 26, 2013 - Certificate issued: February 26, 2013 - Last registry action: November 15, 2021 - Mode S code: AD2EEF - 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/N949DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=949DN - Page: https://openairdocs.org/deregistered/N949DN-2022-12-17 From the FAA registry file of November 3, 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 Mcdonnell Douglas MD-90-30: https://openairdocs.org/model/mcdonnell-douglas-md-90-30.md ## Service difficulty reports (48) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2018052103506](https://openairdocs.org/sdr/DALA2018052103506), May 19, 2018: GROUND WIRE. BROKEN. ONE CEILING EMERGNECY LIGHT WAS FOUND INOPERATIVE. FOUND A BROKEN GROUND WIRE. TERMINATED THE GROUND WIRE IAW SWPM 20-20. OPS CHECKED GOOD. - [SDR DALA2017121408614](https://openairdocs.org/sdr/DALA2017121408614), Dec 12, 2017: DOOR. DAMAGED. DAMAGE FOUND ON DOOR AT ARRIVAL. INSPECTED, EVALUATED AND PERFORMED TEMPORARY REPAIR IAW ERA 564228-14. PERMANENT REPAIR PERFORMED ON L1 DOOR IAW ERA 564228-14, - [SDR DALA2017062204921](https://openairdocs.org/sdr/DALA2017062204921), Jun 20, 2017: SKIN. CRACKED. RIGHT SKIN CRACKED VERTICAL STABILIZER. REPAIRED IAW ERA 556419-14. - [SDR DALA2017061304810](https://openairdocs.org/sdr/DALA2017061304810), Jun 12, 2017: SKIN. CRACKED. CRACK AT LEFT FUSELAGE SKIN, NOSE LANDING GEAR STRUT DOOR FORWARD AND AFT HINGE CUTOUTS. REPAIRED IAW SRM 53-30-01. - [SDR DALA2017061304809](https://openairdocs.org/sdr/DALA2017061304809), Jun 12, 2017: DOUBLER. CRACKED. CRACK AT BS 1460, DOUBLER, LONGERON 2R. REPLACED IAW SRM 51-30-02. - [SDR DALA2017061004662](https://openairdocs.org/sdr/DALA2017061004662), Jun 9, 2017: FRAME. CRACKED. FRAME BS 902 CRACKED. REPLACED THE FRAME. - [SDR DALA2017061504738](https://openairdocs.org/sdr/DALA2017061504738), Jun 8, 2017: BRACKET. CRACKED. RIGHT AIR BOX WEB ANGLE BRACKET CRACKED, BS 1520. REPLACED THE BRACKET. - [SDR DALA2017061504737](https://openairdocs.org/sdr/DALA2017061504737), Jun 8, 2017: BRACKET. CRACKED. RIGHT AIR BOX WEB ANGLE BRACKET CRACKED, BS 1520. REPLACED THE BRAKET. - [SDR DALA2017061504736](https://openairdocs.org/sdr/DALA2017061504736), Jun 6, 2017: BRACKET. CRACKED. HANDRAIL BRACKET CRACKED, BS 1520 BULKHEAD FORWARD SIDE. REPLACED THE BRACKET. - [SDR DALA2017041002922](https://openairdocs.org/sdr/DALA2017041002922), Apr 5, 2017: UNKNOWN. ODOR. FLIGHT ATTENDANT REPORTED AND ELECTRICAL ODOR DURING FLIGHT. TURNED OFF GALLEY POWER AND THE ODOR DISSIPATED. ODOR WAS LIMITED TOE FORWARD GALLEY. MAINTENANCE I - [SDR DALA2017020701016](https://openairdocs.org/sdr/DALA2017020701016), Feb 3, 2017: SLIDE. UNSERVICEABLE. L1 DOOR SLIDE HAS GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE IAW MM. - [SDR DALA2016113009478](https://openairdocs.org/sdr/DALA2016113009478), Nov 30, 2016: DOOR. DAMAGED. DAMAGE TO FORWARD AFT LOWER CORNERS OF L1 DOOR. EDGE FLANGE. REPAIRED IAW SRM 52-01-01. - [SDR DALA2016101007217](https://openairdocs.org/sdr/DALA2016101007217), Oct 6, 2016: JACKSCREW. DAMAGED. GROOVE WEAR ON JACKSCREW THREAD. COMPLIED WITH PRI/ERA 551394-14AD. - [SDR DALA2016101007213](https://openairdocs.org/sdr/DALA2016101007213), Oct 6, 2016: SPAR. CRACKED. LEFT HORIZONTAL STABILIZER UPPER REAR SPAR AFT BARREL NUT HOLE CRACK. REMOVED AND REPLACED STABILIZER ASSEMBLY IAW AMDS 5510-4001. - [SDR DALA2016101307218](https://openairdocs.org/sdr/DALA2016101307218), Oct 3, 2016: LUG. CORRODED. AFT SUPPORT RIGHT FITTING ON HORIZONTAL SUPPORT OUTBOARD LUG CORRODED. COMPLIED WITH PRI/ERA 551207-14. (LP# 270936) - [SDR DALA2017061504739](https://openairdocs.org/sdr/DALA2017061504739), Aug 8, 2016: SKIN. PUNCTURED. FUSELAGE SKIN LEFT BS 240, STRINGER 18L PUNCTURED. REPAIR ACCOMPLISHED. - [SDR DALA2016080905952](https://openairdocs.org/sdr/DALA2016080905952), Aug 6, 2016: POWER SUPPLY. MALFUNCTIONED. EMERGENCY LIGHT ABOVE AFT CABIN DOOR RIGHT SIDE, FLICKERS ON AND OFF. REMOVED AND REPLACED POWER SUPPLY AND BATTERY ASSEMBLY. OPERATION CHECKS NORMAL. (LP# 8720 - [SDR DALA2016010703041](https://openairdocs.org/sdr/DALA2016010703041), Apr 20, 2016: SKIN. DAMAGED. DAMAGE TO NOSE FUSELAGE UPPER SKIN PANEL. REPAIRED IAW ERA 534440-14, SECTION I . - [SDR DALA2016010703040](https://openairdocs.org/sdr/DALA2016010703040), Apr 20, 2016: SKIN. DAMAGED. DAMAGE TO RT SERVICE DOORS SURROUNDING SKIN PANEL. REPAIRED IAW ERA 534439-14, SECTION I. - [SDR DALA2016010703039](https://openairdocs.org/sdr/DALA2016010703039), Apr 20, 2016: SKIN. DENTED. DENT AND CREASE ON UPPER SKIN PANEL. REPAIRED IAW ERA 534431, SECTION I. - [SDR DALA2016010500032](https://openairdocs.org/sdr/DALA2016010500032), Jan 4, 2016: DOUBLER. DAMAGED. DEFORMED INTERNAL PRODUCTION DOUBLER BETWEEN BS 180-200, LONGERON 9-11R AT RT SERVICE DOOR SURROUNDING SKIN PANEL. REPAIRED IAW ERA 541592-14, REV O. - [SDR DALA2015121107560](https://openairdocs.org/sdr/DALA2015121107560), Dec 6, 2015: STRUCTURE. DAMAGED. ON ARRIVAL, REPORTED DAMAGE TO LOWER LT CORNER OF L1 DOOR. REPAIRED IAW SRM 52-01-01. - [SDR DALA2015070604125](https://openairdocs.org/sdr/DALA2015070604125), Jul 5, 2015: SKATE ANGLE. CRACKED. VERTICAL STABILIZER LT SKATE ANGLE CRACKED. DOUBLER REPAIRED IAW SRM 55-30-05. - [SDR DALA2015070704276](https://openairdocs.org/sdr/DALA2015070704276), Jul 4, 2015: SKIN. CRACKED. SKIN CRACKED, AFT SIDE OF BS 1475 BETWEEN STRINGERS 1 - 2R. REPAIRED IAW SRM 53-30-01, FIG 16 AND PRI/ERA 537342-14, REV O. - [SDR DALA2015070504124](https://openairdocs.org/sdr/DALA2015070504124), Jul 4, 2015: LONGERON. CRACKED. LONGERON 2L CRACKED AT BS 1475. REPAIRED IAW SRM 53-30-01, FIG 14. - [SDR DALA2015070504121](https://openairdocs.org/sdr/DALA2015070504121), Jul 4, 2015: SKIN. CRACKED. SKIN CRACKED AFT SIDE OF BS 1475 BETWEEN STRINGERS 1 - 2R. REPAIRED IAW SRM 53-30-01, RIG 16 AND ERA 537336-14, REV O. - [SDR DALA2015070704281](https://openairdocs.org/sdr/DALA2015070704281), Jul 3, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED, BS 1494, BETWEEN STRINGERS 3 - 4R. REPAIRED IAW SRM 53-00-01. - [SDR DALA2015070604123](https://openairdocs.org/sdr/DALA2015070604123), Jul 1, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED, BS 1475, L2R. REPAIRED IAW ERA 537336. - [SDR DALA2015070604126](https://openairdocs.org/sdr/DALA2015070604126), Jun 30, 2015: SHEAR TIE. CRACKED. SHEAR TIE CRACKED BS 1475, STR 2R. SHEAR TIE REPLACED. - [SDR DALA2015041302753](https://openairdocs.org/sdr/DALA2015041302753), Apr 11, 2015: SKIN. DAMAGED. DAMAGED AREA ON FUSELAGE SKIN AT BS 148-218, L8R AND L12R. DISCREPANCY ADDRESSED ON NONROUTINES IAW ERA 534431-14, REV O. LP 1900490. - [SDR DALA2015041002740](https://openairdocs.org/sdr/DALA2015041002740), Mar 9, 2015: SKIN. DAMAGED. FORWARD SERVICE DOOR EXTERNAL SKIN HAS DENT WITH GOUGE ON UPPER SIDE. ACCOMPLISHED PERMANENT REPAIR ON FORWARD SERVICE DOOR EXTERNAL SKIN UPPER IAW ERA 534435-1 - [SDR DALA2015041002739](https://openairdocs.org/sdr/DALA2015041002739), Mar 9, 2015: DOOR FRAME. DENTED. RIGHT FORWARD SERVICE DOOR JAMB IS DENTED AT AFT UPPER CORNER. ACCOMPLISHED PERMANENT REPAIR IAW ERA 534438-14, REV O. LP 1897335. - [SDR DALA2015041002738](https://openairdocs.org/sdr/DALA2015041002738), Mar 9, 2015: DEPRESSOR. BENT. SEAL DEPRESSOR IS BENT, RT FORWARD SERVICE DOOR FUSELAGE CUTOUT, AFT UPPER CORNER. ACCOMPLISHED PERMANENT REPAIR IAW ERA 534438-14, REV O. LP 1897337. - [SDR DALA14020609249](https://openairdocs.org/sdr/DALA14020609249), Apr 2, 2014: PIN. DISLODGED. BOTTOM PARACHUTE PIN ON L1 DOOR SLIDE PACK DISCOVERED TO BE DISLODGED. TOP PIN ALMOST DISLODGED. MAINTENANCE R & R L1 DOOR SLIDE ASSEMBLY. - [SDR DALA13064899249](https://openairdocs.org/sdr/DALA13064899249), Nov 25, 2013: SHEAR TIE. DAMAGED. SHEAR TIE DAMAGED, BS 240, BETWEEN L17-18L. R & R DAMAGED SHEAR TIE IAW SRM 51-30-00. - [SDR DALA13047999249](https://openairdocs.org/sdr/DALA13047999249), Sep 26, 2013: ACM. OVERSERVICED. EXPERIENCED A PLASTIC ODOR COMING FROM THE AIR CONDITIONING SYS ON CLIMBOUT THROUGH 15000 FT. ODOR DISSIPATED AND THEN REOCCURRED ON DESCENT BELOW 10000 FT. PER - [SDR DALA13039519249](https://openairdocs.org/sdr/DALA13039519249), Aug 13, 2013: SKIN. DENTED. SMALL DENT ON FORWARD CABIN DOOR EDGE DISCOVERED BY GATE CREW. MADE REPAIRS IAW SRM 52-01-01. OK FOR SERVICE. - [SDR DALA13036839249](https://openairdocs.org/sdr/DALA13036839249), Jul 24, 2013: RELEASE CABLE. CORRODED. TAILCONE RELEASE CABLE HAS CORROSION ON ALL CLEVIS COMMON TO YOKE, Y1567-895. R & R TAILCONE RELEASE CABLE NR 547 IAW AMM. RII COMPLIED WITH. - [SDR DALA13036849249](https://openairdocs.org/sdr/DALA13036849249), Jul 23, 2013: RELEASE CABLE. BROKEN. DURING SERVICE CHECK, TAILCONE RELEASE CABLE ASSY RUN HAS A BROKEN WIRE. MX R & R TAILCONE CABLE ASSY RUN IAW MM. OPS CHECKED GOOD. - [SDR DALA13033049249](https://openairdocs.org/sdr/DALA13033049249), Jun 28, 2013: SKIN. CORRODED. LEFT HORIZONTAL STAB CENTER BOX JOINT, ON THE UPPER INBD SKIN SURFACE, STA XH24234 HAS DETERIORATING, FASTENER INSTALLATION (14EA). CLEANED ALL LEFT BARRELL NUT - [SDR DALA13032969249](https://openairdocs.org/sdr/DALA13032969249), Jun 27, 2013: SKIN. DAMAGED. RT HORIZONTAL STAB CENTER BOX JOINT, ON THE UPPER INBD SKIN SURFACE AT STA XH24.234 HAS DETERIORIATING SURFACE FASTENER, SURFACE SEALING (12 EA). FOUND HOLES NR - [SDR DALA13033059249](https://openairdocs.org/sdr/DALA13033059249), Jun 26, 2013: SUPPORT ANGLE. DAMAGED. RIGHT HORIZONTAL STAB SUPPORT ANGLE AT REAR SPAR STA XE 167.953 HAS HEAVY EXFOLIATION. REMOVED DAMAGED SUPPORT ANGLE FROM RT HORIZONTAL STAB, T/E ANGLE STA XE16 - [SDR DALA13032959249](https://openairdocs.org/sdr/DALA13032959249), Jun 26, 2013: STRUCTURE. CORRODED. HORIZONTAL STABILIZER, RT LOWER SURFACE FOURTH FROM AFT END HAS BARREL NUT PLUG PROTRUDING. INSPECTED AND FOUND CORROSION AT BARREL NUT HOLE, NR 32. REAMED HOLE - [SDR DALA13032949249](https://openairdocs.org/sdr/DALA13032949249), Jun 26, 2013: SUPPORT ANGLE. DAMAGED. HORIZONTAL STAB LEFT SUPPORT ANGLE AT REAR SPAR XE 167.953 HAS HEAVY EXFOLIATION. REMOVED DAMAGE SUPPORT ANGLE FROM LT HORIZONTAL STAB STA XE169.953. FABRICATED - [SDR DALA13031219249](https://openairdocs.org/sdr/DALA13031219249), Jun 22, 2013: SKIN. DAMAGED. HORIZONTAL STABILIZER LT LOWER SURFACE HAS SEVERAL BARREL NUT PLUGS THAT ARE DETERIORATED. CLEANED ALL BARREL NUT HOLES IAW SRM 51-20-00. FOUND 2 EA CORRODED. R - [SDR DALA13033159249](https://openairdocs.org/sdr/DALA13033159249), Jun 13, 2013: STIFFENER. DAMAGED. CRACKED STIFFENER ABOVE CENTER WING BOX STA 883, LBL 44.5. CUT OUT DAMAGED FLANGE ON STIFFENER ERA 498192-14, MA REV A. NO DEFECTS NOTED. FABRICATED, ALODINED, - [SDR DALA13030429249](https://openairdocs.org/sdr/DALA13030429249), Jun 13, 2013: BEAM. CORRODED. MID CARGO DOOR FRAME HEADER BEAM STA 730-750 HAS CORROSION AROUND RIV-NUTS TASK 53-122-02. REMOVED CORROSION, OUT OF LIMITS. FABRICATED, ALODINED, PRIMED, TOP C - [SDR DALA13029309249](https://openairdocs.org/sdr/DALA13029309249), Jun 12, 2013: SKIN. CORRODED. RIGHT FUSELAGE SKIN AT BS 750, 10 INCHES BELOW L27R IS CORRODED. REMOVED CORRODED BUTT SPLICE. FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF SKIN. FABRI ## 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 20150325004379I](https://openairdocs.org/incident/20150325004379I), Mar 25, 2015: Mcdonnell Douglas MD-90-30 (N949DN), Denver, CO, Minor damage. On 03/25/2015 at approximately 1000 hrs MDT, N949DN a mcdonald Douglas MD-90-30 had just started to be deiced by swiss port. The deice truck rolled into the… --- 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.