# N937DN: Mcdonnell Douglas MD-90-30, registration cancelled 2020-10-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 8, 2020 - Status when cancelled: First renewal notice - 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: 53352 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 5, 2012 - Certificate issued: January 25, 2012 - Last registry action: January 16, 2018 - Mode S code: AD0002 - 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/N937DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=937DN - Page: https://openairdocs.org/deregistered/N937DN-2020-10-08 From the FAA registry file of November 7, 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 (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2018061504033](https://openairdocs.org/sdr/DALA2018061504033), Jun 14, 2018: SPLICE. CORRODED. CORROSION ON LEADING EDGE INBOARD AND OUTBOARD SECTION OF LEADING EDGE SPLICE BELT ON HORIZONTAL STABILIZER LT. CORROSION ON LEADING EDGE INBOARD AND OUTBOARD S - [SDR DALA2018061404006](https://openairdocs.org/sdr/DALA2018061404006), Jun 13, 2018: STRUCTURE. CRACKED. CRACKS FOUND ON RT SIDE OF STRUCTURE SURROUNDING JACKSCREW ASSEMBLY. THE CRACKS WERE ATTENDED IAW ETI-90-18-035, REV 2, AND ER/A 569425-14, REV ORIGINAL. - [SDR DALA2018061203966](https://openairdocs.org/sdr/DALA2018061203966), Jun 11, 2018: FLOOR PANEL. CORRODED. CORROSION FOUND ON FLOOR PANEL 211EG IN THE COCKPIT. THE FLOOR PANEL WAS REMOVED IAW SRM VOL II, 51-30-01. - [SDR DALA2018060803894](https://openairdocs.org/sdr/DALA2018060803894), Jun 7, 2018: SEAT TRACK. CORRODED. CORROSION FOUND ON THE SEAT TRACK, LBL 22, BS 200 - 237. THE SEAT TRACK WAS REPAIRED IAW SRM 53-40-01. - [SDR DALA2018030701460](https://openairdocs.org/sdr/DALA2018030701460), Mar 6, 2018: EXTINGUISHER. EMPTY. ON WAKEUP, A DISCHARGE LIGHT ILLUMINATED FOR THE NR 1 CARGO FIRE BOTTLE. REMOVED & REPLACED THE FIRE BOTTLE IAW AMM 26-22-01. - [SDR DALA2017081806289](https://openairdocs.org/sdr/DALA2017081806289), Jul 13, 2017: ACCESS PANEL. CRACKED. CRACK AT LEADING EDGE OF FUEL ACCESS PANEL. REPAIRED PER ERA 560110-14. - [SDR DALA2017062204918](https://openairdocs.org/sdr/DALA2017062204918), Jun 20, 2017: PIN. DISCONNECTED. EMERGENCY LIGHT INOPERATIVE ROW 32. TROUBLESHOT. FOUND PIN DISCONNECTED FROM SPLICE. CONNECTED PIN. OPERATION CHECKED GOOD. - [SDR DALA2017052304137](https://openairdocs.org/sdr/DALA2017052304137), May 21, 2017: BOTTLE. OUT OF LIMITS. L1 DOOR SLIDE BOTTLE PRESSURE IS OUT OF LIMITS. REMOVED AND REPLACED THE SLIDE. - [SDR DALA2017091206837](https://openairdocs.org/sdr/DALA2017091206837), Dec 6, 2016: SPAR. CORRODED. LEFT HORIZONTAL STABILIZER UPPER, AFT SPAR NR 1 AND 2 BARREL NUT BORES WERE FOUND WITH CORROSION. REPAIRED IAW ER/A 549961. - [SDR DALA2016082306232](https://openairdocs.org/sdr/DALA2016082306232), Aug 21, 2016: AMPLIFIER. MALFUNCTIONED. PERFORMED A DIVERSION DUE TO AN RT ENG FIRE, T-HANDLE RED LIGHT WITH AURAL WARNING "FIRE RIGHT ENGINE" AND RT ENG FIRE DET FAULT EOAP MESSAGE IN CRUISE. MAINTEN - [SDR DALA2016061504640](https://openairdocs.org/sdr/DALA2016061504640), Jun 15, 2016: FRAME. DAMAGED. UPPER RADIUS OF THE FRAME TAB IS DAMAGED BS 962, RT OF THE OVERWING FRAME. REPAIRED IAW ERA 547722-14, REV O. - [SDR DALA2016061604801](https://openairdocs.org/sdr/DALA2016061604801), Jun 12, 2016: STRAP. MISROUTED. TAILCONE SLIDE CONNECTION STRAP ROUTED INCORRECTLY. ROUTED STRAP CORRECTLY. - [SDR DALA2016022401387](https://openairdocs.org/sdr/DALA2016022401387), Feb 19, 2016: BATTERY PACK. INOPERATIVE. BOTH FORWARD CABIN OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK IAW MM. OPS CHECKS OK. - [SDR DALA2015061003715](https://openairdocs.org/sdr/DALA2015061003715), Jun 7, 2015: PANEL. CRACKED. DURING A TAILCONE DROP, TAILCONE LOWER T/E PANEL WAS CRACKED AND DENTED. COMPLIED WITH ERA 463180-14MA PERMANENT REPAIR. - [SDR DALA2015022401705](https://openairdocs.org/sdr/DALA2015022401705), Feb 23, 2015: UNKNOWN. SMOKE. AFTER LANDING, WHITE/GREY SMOKE FIRST CLASS BACK TO MID CABIN. DIMINSHED VISABILITY. TROUBLESHOT. NO TROUBLE FOUND. R & R COALESCER BAGS AND PERFORMED DUCT BURN - [SDR DALA2014122206646](https://openairdocs.org/sdr/DALA2014122206646), Dec 21, 2014: LAMP. INOPERATIVE. AFT TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS . OPS CHECKED GOOD. - [SDR DALA14014939237](https://openairdocs.org/sdr/DALA14014939237), Mar 4, 2014: SKIN. CRACKED. HORIZONTAL STAB SKIN CRACKED. REPAIRED IAW ERA 523708-14AD, SECTION I. - [SDR DALA14014339237](https://openairdocs.org/sdr/DALA14014339237), Feb 28, 2014: BATTERY PACK. DISCONNECTED. DURING SERVICE CHECK, FOUND TAIL COMPARTMENT UPPER EMERGENCY LIGHTS INOPERATIVE. MX FOUND BATTERY PACK B5-239 DISCONNECTED. RECONNECTED. OPS CHECKED GOOD. - [SDR DALA12007349237](https://openairdocs.org/sdr/DALA12007349237), Sep 14, 2012: DOOR FRAME. CORRODED. MID CARGO BAY DOOR LOWER FRAME HAS SEVERAL SPOTS OF CORROSION, BS 693-750. REMOVED DAMAGED AREA. DRILLED AND INSTALLED NEW FRAME IAW SRM 51-30-05, 51-10-05, 51- - [SDR DALA12006599237](https://openairdocs.org/sdr/DALA12006599237), Sep 7, 2012: SKIN. DAMAGED. LIGHTNING STRIKE ON SKIN AT BS 256, L5-6L. REPAIR ACCOMPLISHED PER DWG SG09530001. - [SDR DALA12006589237](https://openairdocs.org/sdr/DALA12006589237), Sep 7, 2012: SKIN. DAMAGED. LIGHTNING STRIKE ON SKIN AT BS 294, L4L. REPAIR ACCOMPLISHED PER DWG SG0953000. - [SDR DALA12006579237](https://openairdocs.org/sdr/DALA12006579237), Sep 7, 2012: SKIN. DAMAGED. LIGHTNING STRIKE ON SKIN AT BS 313 L4L. REPAIR ACCOMPLISHED PER DWG SG09530001. - [SDR DALA12006199237](https://openairdocs.org/sdr/DALA12006199237), Aug 23, 2012: CHANNEL. DAMAGED. RIGHT WHEEL WELL CUTOUT FORWARD FRAME CHANNEL INBOARD END HAS PIECE BROKEN OFF STA 1003 LBL 10. FABRICATED REPAIR ANGLES AND INSTALLED REPAIR AT RIGHT WHEEL WEL - [SDR DALA12006189237](https://openairdocs.org/sdr/DALA12006189237), Aug 23, 2012: CHANNEL. DAMAGED. LEFT WHEEL WELL CUTOUT, FORWARD FRAME CHANNEL INBOARD END HAS PREVIOUS STOP DRILL BUT AREA IS KNIFED EDGED STA 1003 RBL 10. REMOVED PREVIOUS REPAIR ANGLE (CRACK - [SDR DALA12006179237](https://openairdocs.org/sdr/DALA12006179237), Aug 20, 2012: SEAT TRACK. DAMAGED. SEAT TRACK LBL 54.5 FROM BS 856 TO 1080 SPLICE HAS SEVERAL GOUGES AND EXPOSED BARE METAL IN SEVERAL PLACES. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 53-4 - [SDR DALA12006169237](https://openairdocs.org/sdr/DALA12006169237), Aug 16, 2012: SKIN. CORRODED. RIGHT FUSELAGE AT BS 826, L28R SKIN HAS CORROSION. CUTOUT DAMAGED AREA PER SRM 53-31-03 VOL 1. FABRICATED DOUBLER, FILLER AND FOUR FINGER DOUBLERS. INSTALLED FI - [SDR DALA12006099237](https://openairdocs.org/sdr/DALA12006099237), Aug 15, 2012: SEAT TRACK. DAMAGED. SEAT TRACK AT LBL 22, FROM STA 588 TO FR STA 856 SPLICE HAS SEVERAL GOUGES AND EXPOSED BARE METAL, SEVERAL LOCATIONS. BLENDED GOUGES AT LBL 22 STA 588 TO 856 FR - [SDR DALA12006219237](https://openairdocs.org/sdr/DALA12006219237), Jul 11, 2012: BOTTLE. DISCHARGED. TAILCONE DISCHARGE BOTTLE PRESSURE LOW. SERVICED TAILCONE DISCHARGE BOTTLE PER AMM. CHECKED GOOD. - [SDR DALA12006209237](https://openairdocs.org/sdr/DALA12006209237), Jul 11, 2012: SLIDE. NO TEST. TAILCONE SLIDE FAILED TO DEPLOY DURING TEST. FOUND SNAP ON SLIDE COVER STRAP WORN. INSTALLED NEW STUD MFG MS 27983-3N. TAILCONE DEPLOYMENT SUCCESSFUL. SLIDE DEP --- 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.