# N910DN: 1995 Mcdonnell Douglas MD-90-30, registration cancelled 2024-12-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 12, 2024 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas MD-90-30](https://openairdocs.org/model/mcdonnell-douglas-md-90-30) (registry code 3023690) - Engine: [IAE V2500SERIES](https://openairdocs.org/engine/iae-v2500series) (registry code 34601) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 53390 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: November 14, 1995 - Certificate issued: February 16, 1996 - Last registry action: September 2, 2023 - Mode S code: AC9703 - 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/N910DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=910DN - Page: https://openairdocs.org/deregistered/N910DN-2024-12-12 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 Mcdonnell Douglas MD-90-30: https://openairdocs.org/model/mcdonnell-douglas-md-90-30.md ## Service difficulty reports (132, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2019090305134](https://openairdocs.org/sdr/DALA2019090305134), Sep 2, 2019: LIGHT. INOPERATIVE. RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-51. (LP# 5833520) - [SDR DALA2019042402601](https://openairdocs.org/sdr/DALA2019042402601), Apr 23, 2019: ENGINE. MALFUNCTIONED. CLIMBING THROUGH 11000 FEET FELT STRONG YAW TO LEFT, N1 AND N2 ROLLED BACK, EGT HIGH ALL ON NBR 1 ENG. LOUD BANG. SHUT DOWN ENGINE PER QRH AND RETURNED TO PHL. - [SDR DALA20190402086](https://openairdocs.org/sdr/DALA20190402086), Apr 2, 2019: BATTERY PACK. INOPERATIVE. BOTH AFT OVERWING EMERG EXIT SIGNS INOP DURING EMERG LIGHT CHECK. REPLACED EMERG LIGHT BATTERY IAW MD90 AMM 33-51-03. OPS NORMAL. (LP# 4748966) - [SDR DALA2019012800614](https://openairdocs.org/sdr/DALA2019012800614), Jan 27, 2019: CONNECTOR. BROKEN. TAIL COMPT. OVERHEAD EMERGENCY LIGHT INOP. FOUND BROKEN CONNECTOR & REPLACED REF SWPM 20-20-01. OPS CHECK GOOD.(LP# 0920676) - [SDR DALA2018101005961](https://openairdocs.org/sdr/DALA2018101005961), Oct 10, 2018: CABLE. BROKEN. CABLE FOR TAILCONE NITROGEN CYLINDER BROKEN. REMOVED AND INSTALLED NEW CABLE FOR TAILCONE NITROGEN CYLINDER PER AMM 20-30. (LP# 0777925) - [SDR DALA2018030201321](https://openairdocs.org/sdr/DALA2018030201321), Mar 2, 2018: FIRE DETECTOR. MALFUNCTIONED. RECEIVED A LT ENGINE FIRE DETECTOR FAULT, THREE TIMES INTERMITTENTLY ON FINAL. OPENED ENGINE FAN COWLS AND THRUST REVERSER COWLS FOR MTC. REPLACED THE LEFT ENGI - [SDR DALA2018022801260](https://openairdocs.org/sdr/DALA2018022801260), Feb 24, 2018: WARNING SYSTEM. FALSE ACTIVATION. FIRE LOOP B ENG 01 ILLUMINATED PRIOR TO DEPARTURE. T/S PER FIM 26-11-00-810-802 BITE CHK PER AMM 26-11 AND OPS CHK AMM 26-11. ALL CHKS GOOD NO DISCREPANCIES NOT - [SDR DALA2018020900812](https://openairdocs.org/sdr/DALA2018020900812), Feb 9, 2018: RIB. DAMAGED. 13 OF THE LOWER ATTACHMENT HOLES IN THE CENTER RIB ASSEMBLY, WERE FOUND TO BE OUT OF TOLERANCE. MAINTENANCE OVERSIZE THE HOLES IN THE RIB AND INSTALLED REPAIR B - [SDR DALA2018020900788](https://openairdocs.org/sdr/DALA2018020900788), Feb 8, 2018: SKIN. CORRODED. DURING CLEAN SLANT PRESSURE PANEL SEVERAL CORROSION WAS FOUND ON WING BOX CENTER FUEL TANK UPPER SKIN BTW STA Y984 TO 1003 X40 TO X60. CENTER FUEL TANK UPPER SK - [SDR DALA2018020700720](https://openairdocs.org/sdr/DALA2018020700720), Feb 4, 2018: SLIDE. TORN. TORN TAIL CONE EVACUATION SLIDE AT AFT ACCESSORY COMPARTMENT. EVACUATION SLIDE AT AFT ACCESSORY COMPARTMENT P/N 100506-201 S/N D9T009 WAS REPLACED PER SERVICEAB - [SDR DALA2018020200707](https://openairdocs.org/sdr/DALA2018020200707), Feb 1, 2018: BUSHING. CRACKED. CRACKED BUSHING OF UPPER AND MID ATTACH POINTS ON RUDDER. REPLACED. - [SDR DALA2017120408407](https://openairdocs.org/sdr/DALA2017120408407), Nov 29, 2017: WIRE. BROKEN. ONE CEILING EMER LIGHT INOP IN F/C. FOUND WIRE BROKEN LEADING TO ROW 4 LIGHT. RE-TERMINATED WIRE AND CHECKS OK. - [SDR DALA2017032102273](https://openairdocs.org/sdr/DALA2017032102273), Mar 17, 2017: POWER SUPPLY. INOPERATIVE. 5 OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW MM. OPERATION CHECKS OKAY. - [SDR DALA2016120209476](https://openairdocs.org/sdr/DALA2016120209476), Dec 1, 2016: CYLINDER. LEAKING. TAILCONE JETTISON BOTTLE BALL VALVE LEAKING. WON'T HOLD PRESSURE. REMOVED AND REPLACED TAILCONE NITROGEN CYLINDER IAW MM. - [SDR DALA2016111108729](https://openairdocs.org/sdr/DALA2016111108729), Nov 10, 2016: ANGLE. CRACKED. LEFT SIDE INSIDE LOUVER OPENING, FORWARD SIDE OF BS 1542 ANGLE CRACKED. REPLACED THE ANGLE IAW DWG 9911842. - [SDR DALA2016111108728](https://openairdocs.org/sdr/DALA2016111108728), Nov 10, 2016: ANGLE. CRACKED. LEFT SIDE LOUVER OPENING, AFT SIDE OF BS 1520 ANGLE BETWEEN LONGERONS 5 - 7L CRACKED. REPLACED ANGEL IAW DWG 9911839. - [SDR DALA2016041803155](https://openairdocs.org/sdr/DALA2016041803155), Apr 15, 2016: BATTERY PACK. INOPERATIVE. L2 DOOR AND AFT EMERGENCY EXIT SIGNS INOPERATIVE. R & R BATTER PACK B5-212 IAW MM. FOUND FUSE BLOWN ON POWER SUPPLY. R & R FUSE. OPS CHECKS OK. - [SDR DALA2016041202833](https://openairdocs.org/sdr/DALA2016041202833), Apr 5, 2016: CONTROLLER. MALFUNCTIONED. WHILE CRUISING AT FL 300 THE AUTO INOPERATIVE LIGHT ILLUMINATED ON THE CABIN PRESSURE CONTROLLER. NEITHER SYSTEM 1 OR 2 WERE OPERABLE. IAW QRH PROCEDURE CABIN H - [SDR DALA2016032902454](https://openairdocs.org/sdr/DALA2016032902454), Mar 27, 2016: CONTROL UNIT. FAILED. ABORTED TAKEOFF AT APPROXIMATELY 5 KNOTS DUE TO AN ACS FAULT ON EOAP. MESSAGE EXTINGUISHED WHEN THROTTLES WERE RETURNED TO IDLE AND ENGINE SPOOLED DOWN. MAINTEN - [SDR DALA2016032102289](https://openairdocs.org/sdr/DALA2016032102289), Mar 19, 2016: CABLE. MISSING. TAILCONE JETTISON BOTTLE CABLE MISSING ON VALVE HEAD. R & R BOTTLE IAW MM. - [SDR DALA2016031401934](https://openairdocs.org/sdr/DALA2016031401934), Mar 13, 2016: FRAME. NOT REPORTED. FOUND ATTACH FLANGE ON FRAME STA 1328 FROM L24 TO R27. REPAIRED IAW ERA 412247-14, REV D AND ERA 544762-14, REV O. - [SDR DALA2016022101383](https://openairdocs.org/sdr/DALA2016022101383), Feb 19, 2016: POWER SUPPLY. INOPERATIVE. EMERGENCY CEILING LIGHTS AT ROW 35-37, RT SIDE INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY. - [SDR DALA2015051903352](https://openairdocs.org/sdr/DALA2015051903352), May 12, 2015: SKIN. CRACKED. CRACK ON HORIZONTAL STABILIZER UPPER FT SKIN PANEL. REPAIRED IAW ERA 535905-14AD, REV O. - [SDR DALA2015032202271](https://openairdocs.org/sdr/DALA2015032202271), Mar 20, 2015: FAN. SEIZED. STRONG ELECTRICAL ODOR IN COCKPIT AFTER LANDING. FOUND RADIO RACK FAN CIRCUIT BREAKER TRIPPED AND RADIO RACK FAN SEIZED. R & R IAW MM. OPS CHECKED OK. - [SDR DALA2014091405038](https://openairdocs.org/sdr/DALA2014091405038), Sep 10, 2014: POWER SUPPLY. INOPERATIVE. AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R POWER SUPPLY. OPS CHECKED GOOD. - [SDR DALA2014072104171](https://openairdocs.org/sdr/DALA2014072104171), Jul 20, 2014: SKIN. DAMAGED. FUSELAGE SKIN AND UNDERLYING DOUBLER DAMAGED. REPAIRED IAW ERA 527710-14. - [SDR DALA2014072104168](https://openairdocs.org/sdr/DALA2014072104168), Jul 20, 2014: SKIN. DAMAGED. MID CARGO DOOR FUSELAGE CUT OUT SKIN TORN AND DAMAGED, FORWARD SIDE, IN THE MIDDLE OF THE CUTOUT. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER AND TRIPLER I - [SDR DALA14013469210](https://openairdocs.org/sdr/DALA14013469210), Feb 25, 2014: CONNECTOR. INOPERATIVE. L2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. R & R LIGHT ASSEMBLY L2-846 AND CONNECTORS. OPS CHECKED GOOD. - [SDR DALA14010219210](https://openairdocs.org/sdr/DALA14010219210), Feb 14, 2014: LONGERON. CORRODED. AFT CARGO, LONGERON 23L BETWEEN BS 1136-1155, CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW LONGEORN SPLICE IAW SRM 51-10 - [SDR DALA14010179210](https://openairdocs.org/sdr/DALA14010179210), Feb 14, 2014: SPACER. CORRODED. CORROSION FOUND ON AFT CARGO DOOR FRAME. REMOVED CORROSION. FABRICATED AND INSTALLED NEW SPACER IAW 53-60-02 AND 51-10-03. - [SDR DALA14010149210](https://openairdocs.org/sdr/DALA14010149210), Feb 14, 2014: LONGERON SPLICE. CORRODED. AFT CARGO, LONGERON SPLICE 24L AT BS 1259 HAS HEAVY CORROSION. REMOVED LONGERON SPLICE. FABRICATED AND INSTALLED NEW LONGERON SPLICE IAW SRM 51-10-03 AND DWG 59 - [SDR DALA14010139210](https://openairdocs.org/sdr/DALA14010139210), Feb 14, 2014: LONGERON SPLICE. CORRODED. AFT CARGO LONGERON SPLICE 23L AT BS 1259 HAS HEAVY CORROSION. REMOVED LONGERON SPLICE. FABRICATED AND INSTALLED NEW LONGERON SPLICE IAW SRM 51-10-03 AND DWG 591 - [SDR DALA14010249210](https://openairdocs.org/sdr/DALA14010249210), Feb 13, 2014: FRAME. CORRODED. AFT CARGO BAY FRAME BS 1344, BETWEEN L29L AND 29R CORRODED. CUT OUT DAMAGE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FRAME IAW SRM 53-00-01, 53-10-02 - [SDR DALA14010169210](https://openairdocs.org/sdr/DALA14010169210), Feb 13, 2014: FRAME. CORRODED. AFT CARGO BAY FRAME, BS 1344, CORRODED BETWEEN L29L AND L29R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FRAME IAW SRM 51-10-01, - [SDR DALA14010159210](https://openairdocs.org/sdr/DALA14010159210), Feb 13, 2014: LONGERON SPLICE. CORRODED. AFT CARGO LONGERON SPLICE 22L, BS 1259 CORRODED. REMOVED LONGERON SPLICE. FABRICATED AND INSTALLED NEW LONGERON SPLICE IAW SRM 51-30-05. 51-10-05 AND 51-10-03 A - [SDR DALA14011079210](https://openairdocs.org/sdr/DALA14011079210), Feb 12, 2014: CUSP WEB. CRACKED. CUSP WEB AT BS 902 IS CRACKED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER IAW SRM 53-20-02, FIG 6. - [SDR DALA14010259210](https://openairdocs.org/sdr/DALA14010259210), Feb 12, 2014: FRAME. CORRODED. AFT CARGO BAY FRAME, BS 1328, BETWEEN L29L-29R, CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-00-01, - [SDR DALA14010209210](https://openairdocs.org/sdr/DALA14010209210), Feb 10, 2014: SKIN. DAMAGED. LEFT FUSELAGE SKIN AT LOWER LAP SEAM, APPROXIMATELY BS 456, L26L HAS PREVIOUS DEEP BLEND OUT WITH TWO FASTENERS INSTALLED IMPROPERLY. REMOVED DAMAGE. FOUND TO B - [SDR DALA14009519210](https://openairdocs.org/sdr/DALA14009519210), Feb 10, 2014: CUSP WEB. CORRODED. RIGHT CUSP WEB BS 200, CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-30-02, 51-10-03, AND ERA 522800. - [SDR DALA14009479210](https://openairdocs.org/sdr/DALA14009479210), Feb 10, 2014: LONGERON. CORRODED. AFT CARGO BAY LONGERON 29R, BS 1374 CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED LONGEORN SPLICE IAW SRM 53-10-01 AND 51-10- - [SDR DALA14008449210](https://openairdocs.org/sdr/DALA14008449210), Feb 8, 2014: FRAME. CRACKED. BS 902, OVERWING FRAME, UPPER RADIUS OF FRAME TAB CRACKED. REMOVED, LOCATED, DRILLED AND INSTALLED FRAME IAW 51-30-02, 51-30-05, DWG SR90530027. - [SDR DALA14011069210](https://openairdocs.org/sdr/DALA14011069210), Feb 7, 2014: INTERCOSTAL. CORRODED. AFT CARGO BAU INTERCOSTAL, BS 1204 BETWEEN LONGERON 29 AND 30R CORRODED. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-10-03 AND DW - [SDR DALA14008439210](https://openairdocs.org/sdr/DALA14008439210), Feb 7, 2014: FRAME. CORRODED. AFT CARGO BAY FRAME, BS 1379, CORRODED. REMOVED CORRODED FRAME, L26L-L26R. LOCATED, DRILLED AND INSTALLED FRAME IAW SRM 51-10-05, 51-10-03 AND 51-10-00. - [SDR DALA14007669210](https://openairdocs.org/sdr/DALA14007669210), Feb 3, 2014: CUSP WEB. CORRODED. RT CUSP WEB BS 1136-1155 CORRODED. REMOVED RT CUSP WEB. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-30-02, 51-10-03 AND DWG 9940443, REV A. - [SDR DALA14007659210](https://openairdocs.org/sdr/DALA14007659210), Feb 2, 2014: FITTING. CORRODED. AFT CARGO BAY LONGERON 29L END FITTING, BS 1395 IS CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED NEW FITTING IAW SRM 51 - [SDR DALA14007649210](https://openairdocs.org/sdr/DALA14007649210), Feb 2, 2014: FITTING. CORRODED. AFT CARGO BAY LONGERON 28L END FITTING, BS 1395 CORRODED. REMOVED FITTING. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FITTING IAW SRM 51-10-05, 51- - [SDR DALA14007639210](https://openairdocs.org/sdr/DALA14007639210), Feb 2, 2014: FITTING. CORRODED. AFT CARGO BAY STRINGER 27 END FITTING BS 1395 IS CORRODED. REMOVED FITTING. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FITTING IAW SRM 51-10-05, 51 - [SDR DALA14007629210](https://openairdocs.org/sdr/DALA14007629210), Feb 2, 2014: FITTING. CORRODED. AFT CARGO BAY JACK POINT FITTING HAS DEEP CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED NEW FITTING IAW SRM 51-10-0 - [SDR DALA14007739210](https://openairdocs.org/sdr/DALA14007739210), Jan 31, 2014: FLOORBEAM. CORRODED. FORWARD WET AREA, BS 180, LBL 8 - 40 FLOORBEAM CORRODED. R & R FLOORBEAM IAW SRM 51-10-05 AND 51-30-02. - [SDR DALA14010999210](https://openairdocs.org/sdr/DALA14010999210), Jan 30, 2014: CUSP WEB. CORRODED. LEFT CUSP WEB, BS 668, CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-20-02, FIG 19 AND 5 All 132: https://openairdocs.org/deregistered/N910DN-2024-12-12/reports.md ## 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 20191105020839I](https://openairdocs.org/incident/20191105020839I), Nov 5, 2019: Mcdonnell Douglas MD-90-30 (N910DN), Houston, TX, Substantial damage. This office responded to a aircraft incident bird strike, assigned by the communication center, at kiah. The aircraft experienced a bird strike during takeoff… - [Incident 20050524008679I](https://openairdocs.org/incident/20050524008679I), May 24, 2005: Doug MD9030 (N910DN), Salt Lake City, UT, Minor damage. (-23) On may 24, 2005, at 1105 MDT, delta flt #589, a MD-90-30, N910DN, enroute from Salt Lake City, (slc) to new orleans (msy) returned to slc due to an… --- 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.