# N957DN: 1997 Mcdonnell Douglas MD-90-30, registration cancelled 2020-05-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 4, 2020
- 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: 53527
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 5, 2012
- Certificate issued: April 28, 2011
- Last registry action: January 14, 2020
- Mode S code: AD4F00
- 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/N957DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=957DN
- Page: https://openairdocs.org/deregistered/N957DN-2020-05-04

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 (49)

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

- [SDR DALA2016102707789](https://openairdocs.org/sdr/DALA2016102707789), Oct 26, 2016: LENS. DAMAGED. EMERGENCY LIGHT LENS DAMAGED. REPAIRED.
- [SDR DALA2016062905131](https://openairdocs.org/sdr/DALA2016062905131), Jun 26, 2016: SLIDE. DAMAGED. L1 DOOR SLIDE UNLACED. REMOVED AND REPLACED L1 DOOR SLIDE.
- [SDR DALA2016060604495](https://openairdocs.org/sdr/DALA2016060604495), Jun 3, 2016: OUTFLOW VALVE. MALFUNCTIONED. AUTO 1 AND 2 PRESSURIZATION FAILED IN FLIGHT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND AUTO 1 AND 2 INOPERATIVE. R & R OUTFLOW ACTUATOR IAW MM. OPERATION CHECKS
- [SDR DALA2016041803161](https://openairdocs.org/sdr/DALA2016041803161), Apr 16, 2016: TURBINE CASE. CRACKED. LEFT ENGINE AFT VIBRATOR ISOLATOR THERMAL OVERHEATING FROM CRACK IN TURBINE CASE. R & R AFT VIBRATIONS ISOLATOR IAW MM.
- [SDR DALA2016041402922](https://openairdocs.org/sdr/DALA2016041402922), Apr 13, 2016: FRAME. WORN. OVERWING FRAME, BS 883 RT HAS WEAR ON UPPER RADIUS OF THE FRAME TAB FROM THE CUSP WEB. REPAIRED IAW ERA 545329-14AD, REV O.
- [SDR DALA2016041402921](https://openairdocs.org/sdr/DALA2016041402921), Apr 13, 2016: FRAME. WORN. OVERWING FRAME, BS 883 LT HAS WEAR ON UPPER RADIUS OF THE FRAME TAB FROM THE CUSP WEB. REPAIRED IAW ERA 545329-14AD.
- [SDR DALA2016041002846](https://openairdocs.org/sdr/DALA2016041002846), Apr 9, 2016: MOUNT. CRACKED. FORWARD LAV AFT MOUNT FLOOR FITTING CORRODED AND CRACKED. FABRICATED AND INSTALLED FITTING IAW DWG.
- [SDR DALA2016041102847](https://openairdocs.org/sdr/DALA2016041102847), Apr 8, 2016: LONGERON. CRACKED. TAIL INTERIOR LONGERON L3R CRACKED, BS 1494. REPAIRED IAW SRM 53-10-01.
- [SDR DALA2016040902845](https://openairdocs.org/sdr/DALA2016040902845), Apr 8, 2016: LONGERON. CRACKED. LONGERON 2L CRACKED AT BS 1475. REPAIRED IAW PRI/ERA 545446-14, REV O.
- [SDR DALA2016040802844](https://openairdocs.org/sdr/DALA2016040802844), Apr 8, 2016: SKIN. CRACKED. FUSELAGE EXTERIOR SKIN CRACKED AT 3 LOCATIONS, BS 1483 AND BS 1481 BETWEEN L2R AND L4R RT SIDE. COMPLIED WITH ERA 545389-14, REV O.
- [SDR DALA2016040802843](https://openairdocs.org/sdr/DALA2016040802843), Apr 7, 2016: FITTING. CORRODED. G2 AFT INBD FITTING CORRODED. REPAIRED IAW DWG C712071.
- [SDR DALA2016040602842](https://openairdocs.org/sdr/DALA2016040602842), Apr 6, 2016: FLOORBEAM. CORRODED. CORROSION ON CABIL FLOORBEAM , BS 160, BETWEEN RBL 10-20. REPLACED SUPPORT IN NRC 367.
- [SDR DALA2016040602841](https://openairdocs.org/sdr/DALA2016040602841), Apr 6, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, BS 177 TO 181. REPLACED IAW DWG 9936534.
- [SDR DALA2016040602840](https://openairdocs.org/sdr/DALA2016040602840), Apr 6, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, BS 160. REPLACED IAW DWG 9936534.
- [SDR DALA2016040602839](https://openairdocs.org/sdr/DALA2016040602839), Apr 6, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, BS 180. REPLACED IAW DWG 9936534.
- [SDR DALA2016040602838](https://openairdocs.org/sdr/DALA2016040602838), Apr 6, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, BS 200. REPLACED IAW DWG 9936534.
- [SDR DALA2016040602837](https://openairdocs.org/sdr/DALA2016040602837), Apr 6, 2016: CUSP WEB. CORRODED. CORROSION ON CUSP WEB, BS 180-190, RBL 46. REMOVED CORROSION. REPAIRED IAW SRM 53-00-01.
- [SDR DALA2016040602836](https://openairdocs.org/sdr/DALA2016040602836), Apr 6, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, BS 200. REPLACED IAW DWG 9936534.
- [SDR DALA2016040602835](https://openairdocs.org/sdr/DALA2016040602835), Apr 6, 2016: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, BS 200. OUT OF LIMITS. REPLACED IAW DWG 9936534.
- [SDR DALA2016040602834](https://openairdocs.org/sdr/DALA2016040602834), Apr 6, 2016: FLOORBOARD. CORRODED. CORROSION ON FLOORBOARD WEB AT BS 195. REPAIRED IAW SRM 51-11-01.
- [SDR DALA2016040602723](https://openairdocs.org/sdr/DALA2016040602723), Apr 6, 2016: WEB. CORRODED. CORROSION ON FLOOR WEB, BS 196-200. REPAIRED IAW SRM 51-11-01.
- [SDR DALA2016040602722](https://openairdocs.org/sdr/DALA2016040602722), Apr 6, 2016: WEB. CORRODED. CORROSION ON FLOOR WEB, BS 192. REPAIRED IAW SRM 53-20-02 AND 51-11-01.
- [SDR DALA2016040602721](https://openairdocs.org/sdr/DALA2016040602721), Apr 6, 2016: WEB. CORRODED. CORROSION ON FLOOR WEB, BS 200.5. REPAIRED IAW SRM 51-11-01.
- [SDR DALA2016040602720](https://openairdocs.org/sdr/DALA2016040602720), Apr 6, 2016: FITTING. CORRODED. CORROSION ON R1 DOOR AFT GIRT BAR FITTING. R & R FITTING IAW SRM 51-00-01.
- [SDR DALA2016040602719](https://openairdocs.org/sdr/DALA2016040602719), Apr 6, 2016: FLOOR SUPPORT. CORRODED. CORROSION UNDER G7 GALLEY AND FORWARD LAVATORY FLOOR SUPPORTS, BS 200-BS 218, LBL 18. REPAIRED IAW SRM 53-00-01 AND DWG 9936534 AND 9936535.
- [SDR DALA2016040602718](https://openairdocs.org/sdr/DALA2016040602718), Apr 5, 2016: FRAME. CRACKED. CRACK FOUND ON FORWARD SIDE OF FRAME TAB, VERIFIED WITH HFEC. REPAIRED FRAME, STA 902.
- [SDR DALA2016033002636](https://openairdocs.org/sdr/DALA2016033002636), Mar 29, 2016: STRUCTURE. CRACKED. RIGHT WING LOWER L/E CRACKED AT OTBD FWD CORNER OF FUELING BAY. REPAIRED IAW SRM 57-20-01.
- [SDR DALA2016033002635](https://openairdocs.org/sdr/DALA2016033002635), Mar 29, 2016: BULKHEAD. CRACKED. TAIL INTERIOR CANTED BULKHEAD STA 1520, FORWARD AND AFT WEB IS CRACKED RT SIDE. REPAIRED IAW SRM 53-10-03, PARA 10A.
- [SDR DALA2016032602419](https://openairdocs.org/sdr/DALA2016032602419), Mar 25, 2016: BULKHEAD. CRACKED. CANTED BULKHEAD, BS 1520, AFT WEB IS CRACKED LT SIDE. ACCESS INSIDE LT VENT BOX. REPAIRED BULKHEAD IAW SRM 51-10-03, FIG 9C.
- [SDR DALA2014102905827](https://openairdocs.org/sdr/DALA2014102905827), Oct 28, 2014: LATCH. WORN. LEFT UPPER TAILCONE LATCH WORN. R & R LATCH ASSEMBLY.
- [SDR DALA14032699257](https://openairdocs.org/sdr/DALA14032699257), May 22, 2014: FRAME. CHAFED. FOUND CHAFING DAMAGE ON FRAME WEB AT BS 1437, L4L. COMPLIED WITH ERA 526153-14, REV O.
- [SDR DALA14032689257](https://openairdocs.org/sdr/DALA14032689257), May 21, 2014: SKIN. CRACKED. LEFT LOWER AFT FUSELAGE, BS 1531, SKIN CRACKED, AT RIVET ABOVE VENTRAL STAIR CUTOUT. REMOVED DAMAGE. COMPLETED REPAIR IAW SRM 53-00-01, FIG 6.
- [SDR DALA14032679257](https://openairdocs.org/sdr/DALA14032679257), May 21, 2014: SKIN. CRACKED. SKIN HAS A CRACK THROUGH 2 SIDE OF FASTENER HOLE, BS 1475, L2R. REPAIRED FUSELAGE AND INSTALLED DOUBLER IAW ERA 526106-14, REV O.
- [SDR DALA12014079257](https://openairdocs.org/sdr/DALA12014079257), Nov 18, 2012: COFFEEMAKER. CONTAMINATED. FLIGHT CREW REPORTED A BURNING ODOR FROM COFFEEMAKERS BY THE L1 DOOR. COFFEEMAKERS TURNED OFF. ODOR DISSIPATED. MX FOUND PLASTIC CUP RESIDUE ON LOWER COFFEE DIS
- [SDR DALA13037239257](https://openairdocs.org/sdr/DALA13037239257), Sep 21, 2012: CABLE. WORN. VENTRAL STAIRWAY MOVEABLE CEILING CABLE AND SPRINGS WORN. R & R LEFT LIFT CABLE AND SPRING IAW MM. OPS CHECKED GOOD.
- [SDR DALA1235989257](https://openairdocs.org/sdr/DALA1235989257), Apr 23, 2012: LONGERON. CORRODED. AFT CARGO COMPARTMENT AREA, LONGERON 30 HAS EXFOLIATED CORROSION AT STA 1259 LT AND RT. REPAIRED PER ERA 502682-14 REV O.
- [SDR DALA1235959257](https://openairdocs.org/sdr/DALA1235959257), Apr 12, 2012: SKIN. CRACKED. R1 DOOR CUT OUT LOWER CORNER EXTERNAL SKIN HAS EDGE CRACKED. REPAIRED PER ERA 501348-14 REV O.
- [SDR DALA1222869257](https://openairdocs.org/sdr/DALA1222869257), Apr 12, 2012: FLOORBEAM. CORRODED. MID CARGO FLOORBEAM HAS CORROSION STA 693 L28R TO L28L. REPLACED PER SRM 51-30-05.
- [SDR DALA1222849257](https://openairdocs.org/sdr/DALA1222849257), Apr 9, 2012: FLOORBEAM. CORRODED. CORROSION ON TOP OF FLOORBEAM STA 1307 LBL 4.5 AND LBL 9.5. FABRICATED FLOORBEAM PER DWG S2929169 AND INSTALLED PER SRM 51-30-05.
- [SDR DALA1222019257](https://openairdocs.org/sdr/DALA1222019257), Apr 8, 2012: DOUBLER. CORRODED. AFT PRESSURE DOME LOWER BL 0 TRIANGLE SHAPED DOUBLER CORRODED. REMOVED TEE ANGLE AND DOUBLER. DOUBLER CORRODED OUT OF LIMITS. INSTALLED NEW DOUBLER AND INSTALLE
- [SDR DALA1222839257](https://openairdocs.org/sdr/DALA1222839257), Apr 7, 2012: SEAT TRACK. CORRODED. SEAT TRACK GOUGED AND CORRODED STA 1156 LBL 22. REPLACE SEAT TRACK AND INSTALLED SPLICE REPAIR PER SRM 53-40-01.
- [SDR DALA1235979257](https://openairdocs.org/sdr/DALA1235979257), Mar 28, 2012: SEAT TRACK. CORRODED. FOUND CORROSION ON SEAT TRACK RBL 44.5 BS 234. REMOVED AND REPLACED SEAT TRACK PER SRM 51-40-01 FIG 4 AND FIG 6.
- [SDR DALA1233709257](https://openairdocs.org/sdr/DALA1233709257), Mar 28, 2012: SEAT TRACK. DAMAGED. FOUND CABIN SEAT TRACK SCRATCHED LBL44.5 STA 1231 TO 1146. REPLACED TRACK PER SRM 53-40-01.
- [SDR DALA1220319257](https://openairdocs.org/sdr/DALA1220319257), Mar 28, 2012: CUSP WEB. CORRODED. RT CUSP WEB FROM BS 674 TO 750 SEVERAL AREAS WITH SURFACE CORROSION. REMOVED CORROSION, OIL CANNING AND OUT OF LIMITS. REPAIRED AREAS PER SRM 53-20-02 VOL I AND
- [SDR DALA1235949257](https://openairdocs.org/sdr/DALA1235949257), Mar 25, 2012: ANGLE. CRACKED. EMPENNAGE RT SIDE AT STRINGER 16 ON CANTED 1520.225 THERE IS A CRACK IN THE RADIUS. REMOVED ANGLE AND REPLACED PER MD90 SRM 51-30-05 VOL II, 51-30-02 VOL II, AN
- [SDR DALA1233699257](https://openairdocs.org/sdr/DALA1233699257), Mar 25, 2012: SUPPORT FITTING. UNKNOWN. INSPECTED RT MLG RETRACT ACTUATOR SUPPORT FITTING. REPLACED FITTING, BUSHING, AND BEARING.
- [SDR DALA1222829257](https://openairdocs.org/sdr/DALA1222829257), Mar 24, 2012: LONGERON. CORRODED. MID CARGO HAS CORROSION SPOT ON 4EA. STRAPS LONGERON 28R AND 30 STA 758-769. FABRICATED STRAPS PER DWG 9936578 AND 5936071. INSTALLED PER MD 90 SRM 51-10-05 AND
- [SDR DALA1235939257](https://openairdocs.org/sdr/DALA1235939257), Mar 23, 2012: FLOOR SUPPORT. CORRODED. AFT CARGO COMPT BETWEEN STA 1212 AND 1269 FLOOR SUPPORT WITH CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER MD90 SRM 51-10-05 VOL. II.
- [SDR DALA1235929257](https://openairdocs.org/sdr/DALA1235929257), Mar 22, 2012: LONGERON. CORRODED. MIS CARGO COMPARTMENT DOOR JAMB BETWEEN STA 693-750 WITH HEAVY CORROSION. REMOVED AND REPLACED LONGERON 28R FROM STA 655 - 788 PER SRM 51-30-05 AND DRAWING 5930

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