# N901DA: 1995 Mcdonnell Douglas MD-90-30, registration cancelled 2021-02-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 12, 2021
- 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: 53381
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 27, 1995
- Certificate issued: July 13, 1995
- Last registry action: August 31, 2020
- Mode S code: AC732F
- 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/N901DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=901DA
- Page: https://openairdocs.org/deregistered/N901DA-2021-02-12

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 (153, newest 50)

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

- [SDR DALA2018053103719](https://openairdocs.org/sdr/DALA2018053103719), May 31, 2018: BATTERY PACK. INOPERATIVE. AFT EMERGENCY LIGHTS WERE INOPERATIVE. R & R THE BATTERY PACK AND POWER SUPPLY IAW AMM 33-51-03-401. OPS CHECKED GOOD.
- [SDR DALA2018011800354](https://openairdocs.org/sdr/DALA2018011800354), Jan 18, 2018: CONNECTOR. LOOSE. EMERGENCY EXIT LIGHTS IN CEILING PANEL 1 AND 2 INOPERATIVE. FOUND BATTERY PACK CONNECTOR LOOSE AT B2-236. SECURED. OPERATION CHECKS GOOD.
- [SDR DALA2017120808483](https://openairdocs.org/sdr/DALA2017120808483), Dec 6, 2017: COVER. BROKEN. EMERGENCY EXIT SIGN ROW 26 BROKEN. INSTALLED NEW LIGHT COVER.
- [SDR DALA2017061504828](https://openairdocs.org/sdr/DALA2017061504828), Jun 13, 2017: POWER SUPPLY. FAILED. DURING CRUISE, FL310, FLIGHT ATTENDANTS AND PASSENGERS IN MID CABIN NOTICED A BURNING ELECTRICAL ODOR. FIRST OFFICER NOTED A RISE IN CABIN TEMP. SUPPLY BETWEEN 
- [SDR DALA2017041002924](https://openairdocs.org/sdr/DALA2017041002924), Apr 6, 2017: RELEASE MECH. OUT OF ADJUST. TAIL CONE FAILED INTERNAL RELEASE MECHANISM TEST. ADJUSTED TAIL CONE JETTISON. PULL WAS WITHIN LIMITS.
- [SDR DALA2017040102678](https://openairdocs.org/sdr/DALA2017040102678), Mar 31, 2017: STRUCTURE. DAMAGED. VERTICAL STABILIZER LEADING EDGE IS DAMAGED BEYOND REPAIR LIMITS. COMPLIED WITH ERA 556744-14, REV O.
- [SDR DALA2017032902580](https://openairdocs.org/sdr/DALA2017032902580), Mar 29, 2017: FRAME. CRACKED. CANTED FRAME HAS A CRACK AT BS 1542. COMPLIED WITH ERA 556775-14, REV O.
- [SDR DALA2017032902579](https://openairdocs.org/sdr/DALA2017032902579), Mar 29, 2017: TEE FITTING. DAMAGED. AFT PRESSURE BULKHEAD TEE SPLICE BS 1395 BETWEEN LONGERONS 26 AND 27R DAMAGED. REPAIRED IAW PRI/ERA 556133-14, REV O.
- [SDR DALA2017032902578](https://openairdocs.org/sdr/DALA2017032902578), Mar 29, 2017: FRAME SPLICE. DAMAGED. BS 1395 AFT PRESSURE BULKHEAD TEE SPLICE BETWEEN LONGERONS 26 AND 27L DAMAGED. REPAIRED THE BULKHEAD FRAME SPLICE IAW PRI/ERA 556133-14, REV O.
- [SDR DALA2017032902577](https://openairdocs.org/sdr/DALA2017032902577), Mar 29, 2017: SPAR CAP. DAMAGED. VERTICAL STABILIZER LEFT LEADING EDGE FRONT SPAR CAP FORWARD FLANGE HAS DAMAGED FASTENER HOLES . REPAIRED.
- [SDR DALA2017032902576](https://openairdocs.org/sdr/DALA2017032902576), Mar 29, 2017: FRAME. CRACKED. CRACK ON CANTED FRAME, BS 1542. COMPLIED WITH PRI/ERA 556789-14, REV O.
- [SDR DALA2017032102392](https://openairdocs.org/sdr/DALA2017032102392), Mar 18, 2017: PIN. WORN. TAIL INTERIOR EMERGENCY EXIT PULL TEE PIN IS WORN AT BS 1554. REPLACED IAW MM.
- [SDR DALA2017022401544](https://openairdocs.org/sdr/DALA2017022401544), Feb 18, 2017: GROUND WIRE. BROKEN. AFT RIGHT OVER WING EMERGENCY EXIT SIGN INOPERATIVE. FOUND GROUND TERMINAL BROKEN AT GROUND 5232. RETERMINATED WIRE. OPERATION CHECKS GOOD.
- [SDR DALA2017011700387](https://openairdocs.org/sdr/DALA2017011700387), Jan 13, 2017: LAMP. INOPERATIVE. TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD.
- [SDR DALA2016120809737](https://openairdocs.org/sdr/DALA2016120809737), Dec 6, 2016: DUCT. DAMAGED. FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING ODOR. CIRCUIT BREAKER 1-12 AND 1-13, CARGO HEATER TRIPPED. ODOR DISSIPATED. FOUND ELEMENTS SHORTED ON THE HEATER DU
- [SDR DALA2016101007215](https://openairdocs.org/sdr/DALA2016101007215), Oct 9, 2016: BATTERY PACK. INOPERATIVE. EMERGENCY EXIT SIGH INOPERATIVE ABOVE DOOR L2 DOOR. REMOVED AND REPLACED BATTERY PACK. OPERATION CHECKED GOOD.
- [SDR DALA2016020400948](https://openairdocs.org/sdr/DALA2016020400948), Feb 1, 2016: SKIN. DAMAGED. SEVERAL HOLES DAMAGED AT FS 1174, LONGERON 30L AND 29L. COMPLIED WITH PRI/ERA 543071-14, REV C.
- [SDR DALA2015070704277](https://openairdocs.org/sdr/DALA2015070704277), Jul 4, 2015: SUPPORT CHANNEL. CRACKED. VENTRAL STABILIZER ACTUATOR SUPPORT CHANNEL CRACKED. REPAIRED IAW PRI ERA 537315-14.
- [SDR DALA2015041302787](https://openairdocs.org/sdr/DALA2015041302787), Apr 2, 2015: LINE. DISCONNECTED. REPORTED NR 4 BRAKE FIRE DURING TAXI AFTER LANDING. NR 4 BRAKE OVERHEATED TO APPROXIMATELY 700C. ACFT WAS STOPPED AND TOWED INTO GATE. MAINTENANCE FOUND THE NR 
- [SDR DALA2015031702279](https://openairdocs.org/sdr/DALA2015031702279), Mar 16, 2015: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT STA 1475, INBD OF L1R . CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR IAW SRM 53-30-01, FIG 16.
- [SDR DALA2015031502205](https://openairdocs.org/sdr/DALA2015031502205), Mar 14, 2015: SKIN. CRACKED. LEFT HORIZONTAL CENTER SKIN HAS LFEC INDICATION. COMPLY WITH PRI 533591-14AD, REV 1. REPAIR IAW ERA 533591-14AD, REV O.
- [SDR DALA2015022301653](https://openairdocs.org/sdr/DALA2015022301653), Feb 19, 2015: LANYARD. FRAYED. FORWARD ENTRY DOOR GIRT BAR LANYARD FRAYED. R & R LANYARD IAW AMM 25-61.
- [SDR DALA2015021801438](https://openairdocs.org/sdr/DALA2015021801438), Feb 16, 2015: UNKNOWN. SMOKE. HAZE AND SMOKE APPEARED DURING LANDING IN THE CABIN. ODOR WAS MUSTY AND NOTHING APPEARED TO BE BURNING. HAZE DISAPPEARED IN LESS THAN 5 MINUTES. APU WAS NOT RUN
- [SDR DALA2014121706582](https://openairdocs.org/sdr/DALA2014121706582), Dec 14, 2014: OIL SYSTEM. OVERSERVICED. AT 30000 FEET, CRANKED APU AND ELECTRICAL BACKUP, F/A CALLED AND REPORTED ODOR IN CABIN. SHUTDOWN APU IMMEDIATELY. ODOR DISSAPATED. MAINTENANCE TROUBLESHOT AND 
- [SDR DALA2014120206384](https://openairdocs.org/sdr/DALA2014120206384), Nov 23, 2014: SOCKET. BROKEN. EMERGENCY LIGHT IN TAIL INTERIOR SOCKET BROKEN, LOOSE AND LENSE MISSING ABOVE CATWALK. R & R AND CHECKED EMERGENCY LIGHT ASSEMBLY IAW AMM. CHECKS GOOD.
- [SDR DALA14004319201](https://openairdocs.org/sdr/DALA14004319201), Jan 18, 2014: STRUCTURE. DENTED. SMALL DENT ON BOTTOM OF L1 DOOR AT FORWARD LOWER CORNER. REPAIRED IAW SRM 52-01-01. AIRCRAFT OK FOR SERVICE.
- [SDR DALA13058059201](https://openairdocs.org/sdr/DALA13058059201), Oct 30, 2013: WIRE. DAMAGED. DURING SERVICE CHECK, FOUND TWO EMERGENCY LIGHTS AT ROW 5-7 INOPERATIVE. MAINTENANCE FOUND LOOSE WIRE SPLICE FOR CEILING EMERGENCY LIGHTING. WIRE TERMINAL RESEA
- [SDR DALA13034969201](https://openairdocs.org/sdr/DALA13034969201), Jul 11, 2013: WIRE. BROKEN. F/A REPORTS STRONG ELECTRICAL BURNING ODOR IN AFT OF ACFT. RETURN TO BLOCKS. MX FOUND SIDEWALL LIGHT DIMMER SWITCH WITH BROKEN TERMINAL AND WIRE. MX SECURED BRO
- [SDR DALA13033169201](https://openairdocs.org/sdr/DALA13033169201), Jun 27, 2013: STRUCTURE. DENTED. LOWER EDGE OF L1 DOOR DENTED. RESHAPED LOWER EDGE OF L1 DOOR IAW SRM 52-01-01. OK FOR SERVICE.
- [SDR DALA13031399201](https://openairdocs.org/sdr/DALA13031399201), Jun 20, 2013: LIGHT. MISSING. RT OVERWING EMERGENCY PATHWAY LIGHT, AFT DOOR LIGHT MISSING. INSTALLED EMERGENCY EXIT SIGN AND LIGHT ASSY. OPS CHECKS GOOD.
- [SDR DALA13027519201](https://openairdocs.org/sdr/DALA13027519201), Jun 3, 2013: LIGHT. DAMAGED. EMERGENCY FLOOR PATHWAY LIGHTS DAMAGED/INOPERATIVE. MX REINSTALLED LIGHT. OPS CHECKED GOOD.
- [SDR DALA13027509201](https://openairdocs.org/sdr/DALA13027509201), Jun 3, 2013: LIGHT. DAMAGED. EMERGENCY FLOOR PATHWAY LIGHTS WAS DAMAGED/INOPERATIVE. MX REINSTALLED STALLED. OPS CHECKED GOOD.
- [SDR DALA13025239201](https://openairdocs.org/sdr/DALA13025239201), May 24, 2013: LONGERON SPLICE. CORRODED. AFT CARGO COMPARTMENT BILGE, BS 1348 - 1359, LONGERON 30, SPLICE IS CORRODED SEVERAL PLACES. TASK 53-302-07. REMOVED OLD SPLICE. FOUND TO BE OUT OF LIMITS. FABR
- [SDR DALA13025229201](https://openairdocs.org/sdr/DALA13025229201), May 24, 2013: FRAME. CORRODED. AFT CARGO COMPARTMENT BILGE, BS 1364, LONGERON 26R - 26L, FRAME IS CORRODED IN SEVERAL PLACES. TASK 53-302-07. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. REP
- [SDR DALA13024489201](https://openairdocs.org/sdr/DALA13024489201), May 23, 2013: WEB. CORRODED. AFT CARGO COMPARTMENT STA 1271, RBL14-16 WEB HAS CORROSION AROUND NUTPLATE TASK 53-302-07. R & R WEB IAW SRM 51-30-05 AND 51-30-02.
- [SDR DALA13024469201](https://openairdocs.org/sdr/DALA13024469201), May 23, 2013: LONGERON SPLICE. CORRODED. AFT CARGO COMPARTMENT BILGE, STA 1348-1359, LONGERON 29R SPLICE CORRODED IN SEVERAL PLACES. 100 PERCENT MATERIAL LOSS. OUT OF LIMITS. WORK COMPLETED ON WO 26896
- [SDR DALA13024459201](https://openairdocs.org/sdr/DALA13024459201), May 23, 2013: LONGERON. CORRODED. AFT CARGO COMPARTMENT BILGE, STA 1359, LONGERON 29R IS CORRODED AT AFT END OF SPLICE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. WORK COMPLETED ON WO 26896-1
- [SDR DALA13024449201](https://openairdocs.org/sdr/DALA13024449201), May 23, 2013: FRAME. CORRODED. AFT CARGO COMPARTMENT BS 1379, LONGERON 27R FRAME HAS CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW SRM 53-10-02, SRM 51-10-03.
- [SDR DALA13024509201](https://openairdocs.org/sdr/DALA13024509201), May 21, 2013: SHEAR TIE. CORRODED. SHEAR TIE CORRODED, AFT CARGO BAY BS 1379 L26 - 27L. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED IAW SRM 53-10-03 AND 51-30-00 VOL II
- [SDR DALA13024479201](https://openairdocs.org/sdr/DALA13024479201), May 21, 2013: STRUCTURE. DAMAGED. FORWARD CABIN ENTRYWAY FLOOR, JUST INBD OF L1 DOOR CUTOUT, PREVIOUS WEB REPAIR HAS 3EA MISDRILLED HOLES JUST UNDER FLOOR PANEL SUPPORT ANGLE, STATION 170-180. R
- [SDR DALA13024439201](https://openairdocs.org/sdr/DALA13024439201), May 21, 2013: STOP FITTING. CRACKED. FORWARD CARGO DOOR FORWARD STOP PAD FITTING, 4TH FROM TOP, CRACKED. R & R IAW DWG 5910141 AND SRM 51-10-05.
- [SDR DALA13024519201](https://openairdocs.org/sdr/DALA13024519201), May 20, 2013: SHEAR TIE. CORRODED. AFT CARGO SHEAR TIE BS 1269 L28-29R CORRODED ON FWD SIDE. R & R SHEAR TIE IAW SRM 51-30-05 AND DWG 9936073.
- [SDR DALA13024429201](https://openairdocs.org/sdr/DALA13024429201), May 19, 2013: STOP FITTING. CRACKED. FORWARD CARGO DOOR, AFT STOP PAD FITTING, 3RD FROM TOP CRACKED. R & R DOOR STOP FITTING IAW DWG 5910141 AND SRM 51-10-05.
- [SDR DALA13023559201](https://openairdocs.org/sdr/DALA13023559201), May 19, 2013: LONGERON SPLICE. CORRODED. AFT CARGO COMPARTMENT BILGE, BS 1359, LONGERNON 28L IS CORRODED IN AFT END OF SPLICE. REMOVED CORROSION. LONGERON 28L, WITHIN LIMITS. SPLICE FOUND TO BE OUT OF 
- [SDR DALA13023349201](https://openairdocs.org/sdr/DALA13023349201), May 17, 2013: CARGO TRACK. CORRODED. CARGO TRACK FROM FS 1307 AND FS 2169 LONGERON 27R HAS MULTIPLE AREAS OF CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, ALODINED, PRIMED AN
- [SDR DALA13023339201](https://openairdocs.org/sdr/DALA13023339201), May 16, 2013: STOP FITTING. CRACKED. FORWARD CARGO DOOR, FORWARD STOP PAD FITTING CRACKED. R & R IAW DWG 591014.
- [SDR DALA13023009201](https://openairdocs.org/sdr/DALA13023009201), May 16, 2013: FRAME. CORRODED. VERTICAL STABLILIZER UPPER FORWARD FRAME HAS CORROSION. R & R FWD FRAME IAW DWG 5957208 AND SRM 51-10-05 VOLII, PG 1.
- [SDR DALA13022999201](https://openairdocs.org/sdr/DALA13022999201), May 16, 2013: STOP FITTING. CRACKED. FORWARD CARGO DOOR, FORWARD STOP PAD FITTING CRACKED. R & R STOP PAD FITTING IAW DWG 5910141.
- [SDR DALA13022989201](https://openairdocs.org/sdr/DALA13022989201), May 16, 2013: SEAT TRACK. DAMAGED. SEAT TRACK GOUGED AND CORRODED RBL 54.5, BS 1020 -1041. FOUND TO BE OUT OF LIMITS. REMOVED AND REPAIRED SEAT TRACK IAW SRM 53-40-01, FIG 6 AND 51-30-01, PG 1.
- [SDR DALA13022979201](https://openairdocs.org/sdr/DALA13022979201), May 16, 2013: CUSP WEB. CRACKED. BS 1352 CUSP WEB IS CRACKED. REPAIRED IAW SRM 53-20-02, FIG.

All 153: https://openairdocs.org/deregistered/N901DA-2021-02-12/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 20090330002659I](https://openairdocs.org/incident/20090330002659I), Mar 30, 2009: Doug MD9030 (N901DA), Salt Lake City, UT, Minor damage. (-23) Delta airlines MD-90 aircraft, registration number N901DA, flight number 1220 scheduled to operate from Salt Lake City, Utah, (slc) to santa ana,…
- [Incident 19950806031559I](https://openairdocs.org/incident/19950806031559I), Aug 6, 1995: Doug MD9030 (N901DA), Newark, NJ, Minor damage. After landing flames smoke left wing. Evacuated. Faulty strake fin strip and burned heater element replaced.

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