# N935DN: 1996 Mcdonnell Douglas MD-90-30, registration cancelled 2022-11-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 29, 2022 - 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: 53460 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 19, 2012 - Certificate issued: March 31, 2016 - Last registry action: December 2, 2021 - Mode S code: ACF894 - 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/N935DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=935DN - Page: https://openairdocs.org/deregistered/N935DN-2022-11-29 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 (136, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2019030401403](https://openairdocs.org/sdr/DALA2019030401403), Feb 28, 2019: AMPLIFIER. DEFECTIVE. SHIP 9235 - DIV - DUE TO L ENG FIRE DET FAULT EOAP MESSAGE ACCOMPANIED BY A B LOOP LIGHT ON THE OVERHEAD FIRE PANEL. SELECTED A LOOP AND LIGHT EXTINGUISHED. COR - [SDR DALA2019022101086](https://openairdocs.org/sdr/DALA2019022101086), Feb 20, 2019: BOTTLE. LOW PRESSURE. LOW PRESSURE INDICATED ON GAUGE (RED BAND) ON FWD ENTRY DOOR SLIDE S/N 2858. DOOR SLIDE REPLACED. (LP# 0952769) - [SDR DALA2019021961029](https://openairdocs.org/sdr/DALA2019021961029), Feb 15, 2019: SPACER. CORRODED. SPACER ON BEAM AT AFT CARGO DOOR CUT OUT LWR AREA WAS CORRODED. REPLACED PER MD90 SRM VOL I 53-60-02 FIG 9. (LP# 0946458) - [SDR DALA2019011400253](https://openairdocs.org/sdr/DALA2019011400253), Jan 11, 2019: STARTER. DAMAGED. AT GATE ARRIVAL DURING DEPLANING WE NOTICED A SLIGHT ELECTRICAL SMELL IN COCKPIT AND FOUND CABIN, TURNED OFF PACK AND SMELL DISCIPATED, SHUT DOWN APU- TRIED TO - [SDR DALA2018083005368](https://openairdocs.org/sdr/DALA2018083005368), Aug 28, 2018: WIRE. SHORTED. EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. FOUND WIRES L1594J18 AND L1598B18 SHORTING TO GROUND WITH EACH OTHER AT PRESSURE SEAL. REPAIRED THE WIRING IAW WDM 3 - [SDR DALA2018062654222](https://openairdocs.org/sdr/DALA2018062654222), Jun 23, 2018: POWER SUPPLY. INOPERATIVE. L1 DOOR UPPER EXIT EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE POWER SUPPLY. - [SDR DALA2018052903626](https://openairdocs.org/sdr/DALA2018052903626), May 25, 2018: DUCT. CRACKED. STRONG ACRID FUMES STARTED DURING TAKEOFF. CABIN TEMP WAS IN MANUAL IAW MEL BUT TEMP INDICATED COOL. FUMES SEEMED TO DISSIPATE AFTER TURNING OFF RIGHT PACK. CHA - [SDR DALA201805153335](https://openairdocs.org/sdr/DALA201805153335), May 12, 2018: SKIN. CRACKED. WHILE PERFORMING AMDS CARD 5510-01073-02, FOUND A DAMAGED UPPER BOLT OF THE RIGHT SIDE INBOARD ELEVATOR HINGE. ATTEMPTING TO REMOVE BOLT FOR INSPECTION. DUE TO - [SDR DALA2018041202383](https://openairdocs.org/sdr/DALA2018041202383), Apr 11, 2018: POWER SUPPLY. INOPERATIVE. DURING A SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT EXTERNAL LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY B5-125 IAW AMM 33-51-03. LIGHTS OPS CHECKED NORMAL. - [SDR DALA2017122008845](https://openairdocs.org/sdr/DALA2017122008845), Dec 19, 2017: ELECTRICAL SYS. FAILED. EXPERIENCED A TOTAL LOSS OF ELECTRICAL POWER WHILE BEING VECTORED FOR APPROACH. MAINTENANCE TROUBLESHOT AND FOUND OHMS FROM GENERATOR TO CEU T-1 270 M OHMS, T-2 - [SDR DALA2017111008056](https://openairdocs.org/sdr/DALA2017111008056), Nov 9, 2017: LAMP. INOPERATIVE. ONE EMERGENCY LIGHT FAILED TO ILLUMINATE AT ROW 17. REPLACED THE LAMPS IAW AMM 33-51. OPS CHECKED GOOD. OK FOR SERVICE. - [SDR DALA2017072805815](https://openairdocs.org/sdr/DALA2017072805815), Jul 25, 2017: BRAKE. DAMAGED. AFTER UNEVENTFUL LANDING AND RUNWAY CROSSING, FLIGHT CREW FELT A BUMP AND SHORT LIVED DECELERATION THEN RELEASE. BRAKE INDICATIONS APPEARED NORMAL. THE CREW WAS - [SDR DALA2017070605266](https://openairdocs.org/sdr/DALA2017070605266), Jul 3, 2017: LANYARD. DETACHED. LANYARD ON R1 DOOR FELL OUT OF ACCESS DOOR. REATTACHED. OPERATION CHECKS GOOD. - [SDR DALA2017060504554](https://openairdocs.org/sdr/DALA2017060504554), May 25, 2017: CABLE. FRAYED. TAIL CONE LATCH RELEASE CABLE RUN 547 HAS SEVERAL BROKEN STRANDS . REMOVED & REPLACED, OPS CHECKED GOOD. - [SDR DALA2017052504368](https://openairdocs.org/sdr/DALA2017052504368), May 23, 2017: FRAME. CRACKED. AFT ACCESSORY COMPARTMENT FRAME BS 1520 LEFT SIDE OF STRINGER 2R CRACKED. INSTALLED A NEW FRAME IAW SRM 51-30-02, AND 51-30-05. - [SDR DALA2017052404158](https://openairdocs.org/sdr/DALA2017052404158), May 23, 2017: FRAME. CRACKED. CRACKS ON CANTED FRAME, BS 1520 DOUBLER AT FASTENER HOLE. REMOVED AND REPLACED THE DOUBLER IAW DWG 9953015, AND SRM 51-3.0-02, AND 51-30-05. - [SDR DALA2017060504553](https://openairdocs.org/sdr/DALA2017060504553), May 22, 2017: BATTERY PACK. INOPERATIVE. OVER WING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD. - [SDR DALA2017052404161](https://openairdocs.org/sdr/DALA2017052404161), May 22, 2017: PANEL. CRACKED. VERTICAL STABILIZER LOWER AFT CORNER IS CRACKED AT PANEL 370BL. REPAIRED IAW ERA 555250-14, REV O. - [SDR DALA2017051704001](https://openairdocs.org/sdr/DALA2017051704001), May 16, 2017: FRAME. CRACKED. CRACK ON RIGHT FRAME BS 45, IN THE NOSE WHEEL WELL. REMOVED AND REPLACED THE FRAME IAW DWG 9910088, REV CJ, SRM 51-30-02, AND 51-30-05. - [SDR DALA2017051704000](https://openairdocs.org/sdr/DALA2017051704000), May 16, 2017: FRAME. CRACKED. NOSE WHEEL WELL, BS 45 LEFT FRAME CRACKED. REPAIRED IAW SRM 53-90-01. - [SDR DALA2017051603936](https://openairdocs.org/sdr/DALA2017051603936), May 15, 2017: STRAP. CRACKED. STRAP AT FRAME, BS 1520 INBOARD OF LONGERON 3R IS CRACKED. FABRICATED AND INSTALLED NEW STRAP IAW DWG 9911839, REV DP. - [SDR DALA2017050903746](https://openairdocs.org/sdr/DALA2017050903746), May 8, 2017: SKIN. CRACKED. FUSELAGE SKIN CRACK AT NOSE STRUT DOOR AFT HINGE RIGHT HAND SIDE. IN WORK/FIXED. - [SDR DALA2017050603712](https://openairdocs.org/sdr/DALA2017050603712), May 5, 2017: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT NOSE STRUT DOOR AFT HINGE LEFT HAND SIDE. FIXED/IN WORK. - [SDR DALA2017010900251](https://openairdocs.org/sdr/DALA2017010900251), Jan 8, 2017: FIRE WARNING. FALSE ACTIVATION. RIGHT FUEL SWITCH RED FIRE WARNING ON FUEL SWITCH, ILLUMINATED AFTER PLACING SWITCH TO ON DURING ENGINE START. REMAINED ILLUMINATED. MAINTENANCE RESET RIGHT ENG - [SDR DALA2017010900165](https://openairdocs.org/sdr/DALA2017010900165), Jan 6, 2017: DOOR FRAME. CRACKED. RIGHT MAIN LANDING GEAR DOOR FRAME CRACKED. REMOVED, FABRICATED AND INSTALLED NEW DOOR FRAME IAW DWG 5930584. - [SDR DALA2016081706066](https://openairdocs.org/sdr/DALA2016081706066), Aug 8, 2016: ENGINE. FAULTED. ON SHORT FINAL, NR 1 EGT GAUGE BEGAN FLASHING AND INDICATED 699. EPR GAUGES DID NOT MATCH. LANDING WAS NORMAL. AFTER SHUTDOWN, EGT=708 WITH LT ENG SYS FAIL MESS - [SDR DALA2016051603983](https://openairdocs.org/sdr/DALA2016051603983), May 15, 2016: BATTERY PACK. INOPERATIVE. L2 DOOR EMERGENCY EXIT LIGHT FORWARD OF DOOR IS INOPERATIVE. R & R BATTERY POWER SUPPLY. NO HELP. CHANGED BATTERY. OPERATION CHECKS OK. - [SDR DALA2016040602713](https://openairdocs.org/sdr/DALA2016040602713), Apr 4, 2016: PIN. DISLODGED. L1 DOOR SLIDE PINS DISLODGED. R & R SLIDE. - [SDR DALA2016030801876](https://openairdocs.org/sdr/DALA2016030801876), Mar 5, 2016: HARNESS. DAMAGED. AFT TAIL CONE SLIDE HARNESS DAMAGED. INSTALLED NEW TAIL CONE SLIDE HARNESS IAW AMDS. - [SDR DALA2016020901185](https://openairdocs.org/sdr/DALA2016020901185), Feb 7, 2016: WIRE. DAMAGED. AFT STAIRS EMERGENCY SIDEWALL LIGHT INOPERATIVE. FOUND WIRE BROKEN AT QUICK DISCONNECT. REPAIRED IAW SWPM. OPERATION CHECKS OK. - [SDR DALA2015060903806](https://openairdocs.org/sdr/DALA2015060903806), Jun 8, 2015: ANGLE. CORRODED. CORROSION ON ANGLES LOCATED ON RT WING OTBD FLAP INNER STRUCTURE, XRS 164. FLAP AND VANES WERE R & R . - [SDR DALA2015060403599](https://openairdocs.org/sdr/DALA2015060403599), Jun 3, 2015: SKIN. CORRODED. CORROSION ON RT WING UPPER SKIN STA XRS=240. REPAIRED IAW ERA 534378-14 AD, REV O. LP 1976805. - [SDR DALA2015060103598](https://openairdocs.org/sdr/DALA2015060103598), May 29, 2015: STRUCTURE. CORRODED. CORROSION ON FIXED L/E AFT LOWER EDGE STA XRS=240. REPAIRED IAW ETI90-15052, REV 1 AND ERA 534406-14, REV O. - [SDR DALA2015052703515](https://openairdocs.org/sdr/DALA2015052703515), May 26, 2015: CLEVIS. CORRODED. THREE RUSTED CLEVIS`S, ON CABLE SUPPORT AT TAILCONE RELEASE SYSTEM. R & R AND ADJUSTED CLEVIS ON CABLE SUPPORT AT TAILCONE RELEASE IAW AMM. LP 1965257. - [SDR DALA2015052703519](https://openairdocs.org/sdr/DALA2015052703519), May 25, 2015: SKIN. CRACKED. CRACKED OUTER SKIN, BS 1484, BETWEEN LONGERON 2R-3R. REPAIRED IAW SRM 51-10-3, 51-30-02, 51-30-05, AND ERA 534366-14, REV O. - [SDR DALA2015052703521](https://openairdocs.org/sdr/DALA2015052703521), May 24, 2015: SPAR CAP. CORRODED. CORROSION ON LOWER CAP, BS XRS 531 AND 544 AT RT WING FRONT SPAR. REPAIRED IAW ETI 90-15-044 R1 AND ERA 534381-14, REV O. - [SDR DALA2015052703520](https://openairdocs.org/sdr/DALA2015052703520), May 24, 2015: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK, BS 235-238, X=-44. FOUND TO BE OUT OF LIMITS. R & R THE SEAT TRACK IAW SRM 53-40-01. - [SDR DALA2015052703517](https://openairdocs.org/sdr/DALA2015052703517), May 24, 2015: FRAME. CRACKED. CRACKED FRAME, BS 294, LONGERON 6L AT INNER FUSELAGE STRUCTURE. REPAIRED IAW ERA 534382-14, REV O. - [SDR DALA2015052503513](https://openairdocs.org/sdr/DALA2015052503513), May 24, 2015: DOOR FRAME. CRACKED. CRACKED FORMER ON RT FORWARD MLG DOOR JAMB, BS 1006, X=-56. R & R FORMER IAW SRM 51-30-02, 51-30-05, AND 51-10-05. LP 1961928. - [SDR DALA2015052503512](https://openairdocs.org/sdr/DALA2015052503512), May 24, 2015: SUPPORT. CRACKED. CRACK ON KEEL BEAM AFT SUPPORT BETWEEN BS 1079 - 1098, LONGERON 30. SUPPORT WAS REPLACED IAW SRM 51-30-05. LP 1961920. - [SDR DALA2015052203444](https://openairdocs.org/sdr/DALA2015052203444), May 21, 2015: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK, BS 856-874 AND 883-902, X=54. TASK 53-211-02. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01 AND 51-10-03. - [SDR DALA2015052103441](https://openairdocs.org/sdr/DALA2015052103441), May 21, 2015: FORMER. CRACKED. CRACKED FORMER ON LT MLG FORWARD DOOR JAMB, BS 997 X=7. R & R FORMER IAW SRM 51-30-02, 51-30-01, 51-30-05, 51-10-03. - [SDR DALA2015052203443](https://openairdocs.org/sdr/DALA2015052203443), May 20, 2015: SKIN. DAMAGED. METALLIZED COVER ON RUDDER TAB DAMAGED. REPAIRED IAW SRM 55-41-01. - [SDR DALA2015052003439](https://openairdocs.org/sdr/DALA2015052003439), May 19, 2015: STRUCTURE. CORRODED. CORROSION ON HORIZONTAL STABILIZER BARREL NUT NR 10. REMOVED BARREL NUT AND NEW BUSHING FABRICATED AND INSTALLED IAW SRM 55-10-03. - [SDR DALA2015052103445](https://openairdocs.org/sdr/DALA2015052103445), May 19, 2015: PIN. OUT OF POSITION. THE SECURITY PIN FOR L1 DOOR SLIDE WAS OUT OF POSITION. R & R SLIDE. - [SDR DALA2015052003438](https://openairdocs.org/sdr/DALA2015052003438), May 18, 2015: FORMER. CRACKED. CRACKED FORMER, BS 994, C=7, KEEL BEAM FORWARD EDGE. REMOVED, FABRICATED AND INSTALLED NEW FORMER IAW SRM 51-30-02, 51-30-05, 51-10-05, AND 51-10-03. - [SDR DALA2015051803344](https://openairdocs.org/sdr/DALA2015051803344), May 17, 2015: BEAM. CRACKED. CRACK ON FORWARD EDGE BEAM NR 4 AT FORWARD SERVICE DOOR R1. R & R BEAM IAW SRM 51-10-05, 51-10-03, 51-30-01, 51-30-02, 51-30-04, 51-30-05 AND DWG 9911582, REV T - [SDR DALA2015051803343](https://openairdocs.org/sdr/DALA2015051803343), May 17, 2015: CUSP WEB. CORRODED. CORROSION ON LT CUSP WEB, BS 935-947, X= 54 - 60. REPAIRED IAW SRM 53-20-02, FIG 26. - [SDR DALA2015051903350](https://openairdocs.org/sdr/DALA2015051903350), May 15, 2015: SUPPORT. BROKEN. RT SLANT SUPPORTS BROKEN, BS 561, 655 AND 674. REPLACED IAW SRM 412241-14MA, REV C. - [SDR DALA2015051603342](https://openairdocs.org/sdr/DALA2015051603342), May 15, 2015: SEAT TRACK. CORRODED. CORROSION ON RIGHT SEAT TRACK BS 470-526, X=54. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 53-40-01. All 136: https://openairdocs.org/deregistered/N935DN-2022-11-29/reports.md --- 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.