# N902DA: 1994 Mcdonnell Douglas MD-90-30, registration cancelled 2020-08-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 25, 2020
- 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: 53382
- Year built: 1994
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: February 10, 1995
- Certificate issued: April 26, 1995
- Last registry action: November 6, 2019
- Mode S code: AC76E6
- 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/N902DA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=902DA
- Page: https://openairdocs.org/deregistered/N902DA-2020-08-25

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 (98, newest 50)

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

- [SDR DALA2017020701019](https://openairdocs.org/sdr/DALA2017020701019), Feb 1, 2017: COALESCER BAG. NOT REPORTED. SMOKE IN COCKPIT AND CABIN DURING LANDING ROLLOUT. DISSIPATED RAPIDLY. REMOVED AND REPLACED COALESCER BAGS PERFORMED DUCT BURNOUT. AIRCRAFT OKAY FOR SERVICE.
- [SDR DALA2016110708349](https://openairdocs.org/sdr/DALA2016110708349), Nov 2, 2016: LIGHT. BROKEN. FOUND EMERGENCY LIGHT BROKEN AT AFT TAILCONE OVERHEAD CATWALK. REMOVED AND REPLACED POWER SUPPLY AND BATTERY. OPERATION CHECKS GOOD.
- [SDR DALA2016030401661](https://openairdocs.org/sdr/DALA2016030401661), Mar 3, 2016: UNKNOWN. SMOKE. LIGHT SMOKE AND ODOR IN CABIN AFTER LANDING. INSPECTED BOTH ENGINES AND APU FOR CONTAMINATE. NONE FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS. ALL
- [SDR DALA2016012000644](https://openairdocs.org/sdr/DALA2016012000644), Jan 13, 2016: BEAM. CORRODED. AFT CARGO DOOR SILL BEAM CORRODED. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-60-02, FIG 9.
- [SDR DALA2016011100268](https://openairdocs.org/sdr/DALA2016011100268), Jan 8, 2016: RECEPTACLE. WORN. TAILCONE RECEPTICLES WORN. REPLACED IAW SRM 51-30-02.
- [SDR DALA2016011100267](https://openairdocs.org/sdr/DALA2016011100267), Jan 8, 2016: DOOR SILL. CORRODED. LOWER FUSELAGE, AFT CARGO DOOR SILL BEAM CORRODED. REPAIRED.
- [SDR DALA2016011200230](https://openairdocs.org/sdr/DALA2016011200230), Jan 7, 2016: SUPPORT FITTING. CORRODED. LOWER FUSELAGE AFT CARGO DOOR CUTOUT FORWARD CORNER, SUPPORT FITTING CORRODED. NEW ANGLE INSTALLED IAW SRM 53-00-01.
- [SDR DALA2015113007341](https://openairdocs.org/sdr/DALA2015113007341), Nov 23, 2015: BATTERY PACK. INOPERATIVE. AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. R & R BATTERY PACK AND POWER SUPPLY AT ROW 27CDE. OPERATION CHECKS OK.
- [SDR DALA2015061203807](https://openairdocs.org/sdr/DALA2015061203807), Jun 12, 2015: SLIDE. MALFUNCTIONED. WHILE CLOSING THE L1 DOOR THE SLIDE DEPLOYED. R & R L1 DOOR SLIDE.
- [SDR DALA14014329202](https://openairdocs.org/sdr/DALA14014329202), Feb 28, 2014: WEB. CRACKED. TAIL INTERIOR VENTRAL STAIRS WEB CRACKED LT SIDE FORWARD OF SPRING LOCK MECHANISM. REPAIRED LT VENTRAL STAIRWAY SLANTED SIDE WEB IAW PRI AND ERA 523510-14, REV 
- [SDR DALA14014319202](https://openairdocs.org/sdr/DALA14014319202), Feb 28, 2014: WEB. CRACKED. TAIL INTERIOR VENTRAL STAIRS WEB CRACKED RT SIDE JUST FORWARD OF SPRING LOCK MECHANISM. REPAIRED RIGHT VENTRAL STAIRWAY SLANTED SIDE WEB IAW PRI AND ERA 523510-
- [SDR DALA14013549202](https://openairdocs.org/sdr/DALA14013549202), Feb 25, 2014: DOOR. CRACKED. CRACKS FOUND COMMON TO SLANTED SIDE WEB NEAR THE AFT END OF THE FIXED VENTRAL DOOR.
- [SDR DALA14012099202](https://openairdocs.org/sdr/DALA14012099202), Feb 23, 2014: STIFFENER. CRACKED. TAIL INTERIOR, STAIR WAY INTERCOSTAL, FWD DIAGONAL SUPPORT STIFFENER CRACKED, RT SIDE AT CANTED FRAME BS 1549. VERIFIED CRACK, R & R STIFFENER IAW DWG 9911946.
- [SDR DALA14012089202](https://openairdocs.org/sdr/DALA14012089202), Feb 23, 2014: STIFFENER. SEVERED. TAIL INTERIOR, LOWER SUPPORT CHANNEL SEVERED, RT SIDE AT CANTED FRAME, BS 1549 AT AND BELOW STAIRWAY INTERCOSTAL ATTACH POINT. R & R SUPPORT STIFFENER IAW DWG 9
- [SDR DALA14012069202](https://openairdocs.org/sdr/DALA14012069202), Feb 22, 2014: FRAME. CRACKED. TAIL INTERIOR, FORWARD SIDE OF CANTED FRAME WEB CRACKED BS 1531, FROM UPPER ANGLE BETWEEN L8-9R. REPAIRS COMPLETE IAW PRI 52348-14, REV O.
- [SDR DALA14012079202](https://openairdocs.org/sdr/DALA14012079202), Feb 19, 2014: SKIN. CRACKED. FUSELAGE EXTERIOR SKIN CRACKED AT CANTED FRAME, BS 1531 LT SIDE. REPAIRED IAW SRM 53-00-01, FIG 6.
- [SDR DALA13023039202](https://openairdocs.org/sdr/DALA13023039202), May 15, 2013: LIGHT. MISSING. DURING SERVICE CHECK, FOUND EMERGENCY PATHWAY LIGHTS MISSING SECTION BETWEEN ROW 27 AND 28 EDF. INSTALLED EMERGENCY LIGHT SECTION IAW EA 02-477506-03 REV A. ACF
- [SDR DALA13009619202](https://openairdocs.org/sdr/DALA13009619202), Feb 27, 2013: BULB. INOPERATIVE. DURING SERVICE CHECK, FOUND SEVERAL INOPERATIVE BULBS IN TAIL COMPARTMENT EMERGENCY LIGHT SIGNS. REPLACED LAMPS AS REQUIRED. OPS CHECKED GOOD.
- [SDR DALA13003349202](https://openairdocs.org/sdr/DALA13003349202), Jan 18, 2013: CLAMP. SEPARATED. DIVERTED, DUE TO PRESSURIZATION ISSUES AT FL140. STARTED DESCENT TO 10,000. THE LT PACK SHOWED ZERO FLOW AND THE RT PACK WAS OPERATING NORMALLY AND SHOWING GOOD
- [SDR DALA1252809202](https://openairdocs.org/sdr/DALA1252809202), Oct 25, 2012: STRUCTURE. CRACKED. F/A REPORTED STRANGE NOISES FROM TAIL COMPARTMENT UPON ROTATION. SUSPECTED CATWALK DOES NOT RAISE PROPERLY WHEN AFT AIRSTAIRS ARE DOWN AND FELL TO THE DOWN POSI
- [SDR DALA1249089202](https://openairdocs.org/sdr/DALA1249089202), Sep 19, 2012: STRUCTURE. OUT OF POSITION. FLIGHT CREW REPORTED THAT AFT AIRSTAIR WILL NOT RAISE WITH STAIRS DOWN. MX FOUND CATWALK SIDES CATCHING ON CEILING CUTOUT. AFT VENTRAL STAIRS FORWARD TO MCO/PLA
- [SDR DALA1240339202](https://openairdocs.org/sdr/DALA1240339202), Jun 29, 2012: TIRE. FAILED. NUMBER 2 MAIN LANDING GEAR TIRE BLEW ON ROTATION. INNER LOWER LEFT WING BUTT DOOR WAS RIPPED OFF LEFT WING. LEFT MAIN LANDING GEAR ANTI-SKID AND GROUND PROXIMIT
- [SDR DALA1214769202](https://openairdocs.org/sdr/DALA1214769202), Mar 8, 2012: FRAME. CORRODED. CORROSION ON FRAME IN AFT CARGO COMP AT STA 1379 LNGR 28R TO LNGR 25L. CORROSION OF FRAME WAS FOUND OUT OF LIMITS. CORROSION ON SHEAR TIE FOUND OUT OF LIMITS. I
- [SDR DALA1215859202](https://openairdocs.org/sdr/DALA1215859202), Mar 5, 2012: FLOORBEAM. CORRODED. CORROSION FOUND ON SUPPORT BEAM UPPER CORD AT STA 1364 LBL 10 TO LBL 20. REMOVED CORRODED AFT FLOOR SUPPORT BEAM SECTION AND COMPLIED WITH ERA 498694-14 REV 0 F
- [SDR DALA1212599202](https://openairdocs.org/sdr/DALA1212599202), Mar 3, 2012: SUPPORT FITTING. UNKNOWN. INSPECT LT MLG RETRACT ACTUATOR SUPPORT FITTING. REMOVED ACTUATOR, SUPPORT FITTING, BUSHING, AND BEARING. INSPECT (GVI) GEAR SUPPORT FITTING BEARING AND BUSHING
- [SDR DALA1212589202](https://openairdocs.org/sdr/DALA1212589202), Mar 3, 2012: SUPPORT FITTING. UNKNOWN. INSPECT RT MLG ACTUATOR SUPPORT FITTING. REMOVED ACTUATOR, SUPPORT FITTING, BUSHING, AND BEARING. INSPECT (GVI) GEAR SUPPORT FITTING BEARING BORE AND BUSHING BO
- [SDR DALA1214649202](https://openairdocs.org/sdr/DALA1214649202), Mar 1, 2012: SUPPORT BRACKET. DAMAGED. FWD ENTRY DOOR L-1 HOLD OPEN HOOK SHAFT SUPPORT BRACKET DAMAGED & EXTERNAL PREVIOUS REPAIR CHAFED. REMOVED & REPLACED HOLD HOOK SHAFT BRACKET, REMOVED & REPLACE
- [SDR DALA1212609202](https://openairdocs.org/sdr/DALA1212609202), Mar 1, 2012: DOOR FRAME. CORRODED. AFT PRESSURE BULKHEAD DOOR JAMB AT LT AND RT LWR SIDE WITH CORROSION. REMOVED LT AND RT LOWER DOOR JAMB CHANNELS AND LOWER DOOR JAMB FOUND WITH TOTAL MATERIAL L
- [SDR DALA1212189202](https://openairdocs.org/sdr/DALA1212189202), Feb 27, 2012: FLOOR SUPPORT. CORRODED. LEFT SIDE FLOOR SUPPORT FROM STA 1364 TO 1402 LBL 24 WAS FOUND CORRODED AND OUT OF LIMITS. REPLACED WITH NEW FLOOR SUPPORT SRM 51-10-05 FIG 1 PG 2 VOL 2 (AAR NR
- [SDR DALA1212159202](https://openairdocs.org/sdr/DALA1212159202), Feb 27, 2012: FLOOR SUPPORT. CORRODED. RIGHT SIDE FLOOR SUPPORT FROM STA 1364 TO 1402 RBL 24 WAS FOUND OUT OF LIMITS. REPLACED FLOOR SUPPORT PER MD 90 SRM 51-10-05 FIG 1 (NR 862386).
- [SDR DALA1211469202](https://openairdocs.org/sdr/DALA1211469202), Feb 27, 2012: SKIN. CRACKED. DUE AT HMV/PSV CHECK, ERA 487631-14 REV A CODE 53-31. PERMANENT REPAIR TO FUSELAGE SKIN STA 1475 BTW 2L-3L CRACK. ACTL LN 2151. COMPLIED WITH ON N/R 862522.
- [SDR DALA1211939202](https://openairdocs.org/sdr/DALA1211939202), Feb 25, 2012: SLAT. GOUGED. DURING INSTALLATION OF #0 RT SLAT NR 2 TRACK FOUND I/B FWD RIB FWD/LWR EDGE GOUGED. BLENDED GOUGE AT #0 RT SLAT NR 2 TRACK INBD RIB FWD LOWER EDGE AS PER MD-90 
- [SDR DALA1212179202](https://openairdocs.org/sdr/DALA1212179202), Feb 24, 2012: SKIN. DAMAGED. REMOVED CORRODED SKIN DOUBLER AT STA 826 LNGR 28R. FABRICATED NEW DOUBLER OF 7075-T6 .063 AND .071 7075-T6 TRIPLER PER MD90 SRM 53-30-01 PG 70 VOL 1. PERFORM HF
- [SDR DALA1214809202](https://openairdocs.org/sdr/DALA1214809202), Feb 23, 2012: SKIN. CRACKED. FWD GALLEY DOOR R-1 OUTER SKIN LOWER FWD CORNER BENT. CRACKED STOP DRILLED CRACK IN REF MD90 SRM 52-10-01 FABRICATED REPAIR DOUBLER IN REF WITH MD90 SRM 52-10-0
- [SDR DALA1212149202](https://openairdocs.org/sdr/DALA1212149202), Feb 22, 2012: FITTING. CORRODED. AFT CARGO TIE FITTING HAS CORROSION AT STA 1376 LNGR23L. REMOVED FASTENERS AND CORROSION FROM TIE FITTING AND OUT OF LIMITS. DRILLED NEW FITTING P/N 3936440 AND
- [SDR DALA1212139202](https://openairdocs.org/sdr/DALA1212139202), Feb 22, 2012: SHEAR TIE. CORRODED. AFT CARGO FRAME STA 1344 FROM LNGR 27R TO 22L CORRODED. REMOVED SHEAR TIE FROM FRAME FROM LNGR 26L TO 26R. FABRICATED NEW SHEAR TIE REF DWG 9957739. INSTALLED N
- [SDR DALA1212129202](https://openairdocs.org/sdr/DALA1212129202), Feb 22, 2012: STRINGER. CORRODED. AFT CARGO HAS CORRSION ON LSTR 30 STA 1300-1388. REMOVED CORROSION ON LSTR 30 BETWEEN STA 1300-1388. OUT OF LIMITS FROM STA 1379-1388 REF MD90 SRM 53-00-01. REM
- [SDR DALA1210519202](https://openairdocs.org/sdr/DALA1210519202), Feb 22, 2012: LONGERON. CORRODED. AFT CARGO COMP HAS CORROSION SPOT ON LNGR 30 FS 1300/1388. REMOVED CORROSION AT AFT CARGO COMP LNGR 30 BETWEEN 1300/1388 REF MD90 SRM 51-10-03. FOUND WITH IN LI
- [SDR DALA1214679202](https://openairdocs.org/sdr/DALA1214679202), Feb 19, 2012: CUSP WEB. CRACKED. CABIN LT CUSP WEB BETWEEN STA 1334 & 1364 CRACKED AT LIGHTNING HOLE OUTBD SIDE. REMOVED DAMAGED SECTION OF CUSP WEB BTWN STA 1334 & 1364 IN REF MD90 SRM 51-30-0
- [SDR DALA1211959202](https://openairdocs.org/sdr/DALA1211959202), Feb 19, 2012: CUSP WEB. CRACKED. CABIN LT CUSP WEB BETWEEN STA 1334 & 1364 CRACKED AT LIGHTENING HOLE OUTBD SIDE. REMOVED DAMAGE SECTION OF CUSP WEB BETWEEN STA 1334 & 1364 IN REF MD-90 SRM 51-
- [SDR DALA1216089202](https://openairdocs.org/sdr/DALA1216089202), Feb 17, 2012: CUSP WEB. CRACKED. CABIN RT CUSP WEB BETWEEN STA 1344 AND STA 1364 AT LIGHTENING HOLE EDGE CRACKED. REMOVED DAMAGE AND FASTENERS. FABRICATED DOUBLER, FILLER, AND INSTALLED REPAIR 
- [SDR DALA1212169202](https://openairdocs.org/sdr/DALA1212169202), Feb 16, 2012: FLOORBEAM. DAMAGED. REMOVED EXISTING REPAIR BEAM STA 712 TO 731 AS PER MD90 SRM 51-30-04. FOUND TO BE OUT OF LIMITS AT STA 699 AND 744 AS PER MD90 SRM 53-00-01. AFTER FURTHER INSP,
- [SDR DALA1212119202](https://openairdocs.org/sdr/DALA1212119202), Feb 16, 2012: FLOORBEAM. DAMAGED. REMOVED EXISTING REPAIR BEAM STA 712 TO 731 AS PER 51-30-04. FOUND TO BE OUT OF LIMITS STA 699 AND STA 744 AS PER MD90 SRM 53-00-01. AFTER FURTHER INSP, HOLE OF
- [SDR DALA1214699202](https://openairdocs.org/sdr/DALA1214699202), Feb 14, 2012: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK AT RBL 54.50 STA 452 TO 845 FOUND CORREDED & OUT OF LIMITS IN REF WITH MD90 SRM 53-40-01. FABRICATED SEAT TRACKS AT RBL 54.5 STA 452-845IN
- [SDR DALA1211969202](https://openairdocs.org/sdr/DALA1211969202), Feb 14, 2012: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACKS AT RBL 54.50, STA 452 TO STA 845 FOUND CORRODED & OUT OF LIMITS IN REF WITH MD 90 SRM 53-40-01. FABRICATED SEAT TRACKS AT RBL 54.50 STA 4
- [SDR DALA1216229202](https://openairdocs.org/sdr/DALA1216229202), Feb 10, 2012: CUSP WEB. CORRODED. CORROSION FROM STA 160 TO STA 200 LBL 10 ON CUSP WEB. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED WEB FROM 7075 T6 .020 AND DOUBLER FROM 7075 T6 .025.
- [SDR DALA1214669202](https://openairdocs.org/sdr/DALA1214669202), Feb 7, 2012: CUSP WEB. CRACKED. CABIN LT CUSP WEB CRACKED AT STA 1136. REMOVED DAMAGE CUSP WEB. FABRICATED CUSP WEB IN REF DWG 9910151 SHEET 8. INSTALLED CUSP WEB IN REF MD90 SRM 53-20-02.
- [SDR DALA1211999202](https://openairdocs.org/sdr/DALA1211999202), Feb 7, 2012: CUSP WEB. CRACKED. CABIN LT CUSP WEB CRACKED AT STA 1136. REMOVED DAMAGED CUSP WEB FABRICATED CUSP WEB IN REF DWG 9910151 SHT 8. INSTALLED CUSP WEB IN REF MD90 SRM 53-20-02 REF N/
- [SDR DALA1210489202](https://openairdocs.org/sdr/DALA1210489202), Feb 7, 2012: DOOR FRAME. CORRODED. FWD LWR CARGO COMPT DOOR JAMB FROM STA 389 - 427 FOUND AREAS CORRODED. CORROSION FOUND OUT OF LIMITS OF MD 90 SRM 53-00-01. CUT OUT DAMAGED LWR DOOR JAMB PER SR
- [SDR DALA1214759202](https://openairdocs.org/sdr/DALA1214759202), Feb 6, 2012: SKIN. CORRODED. FWD CARGO COMPT CORRODED AT INNER SKIN O/B OF L26L, FWD OF STA 237. REMOVED CORROSION ON INNER SKIN & LONGERON L26L & FOUND WEAR. REMOVED CORROSION OF FINGER DO

All 98: https://openairdocs.org/deregistered/N902DA-2020-08-25/reports.md

## FAA accident and incident reports (3)

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 20120417007029I](https://openairdocs.org/incident/20120417007029I), Apr 17, 2012: Mcdonnell Douglas MD-90-30 (N902DA), Spokane, WA, No damage. After takeoff below 15 thousand feet, pilot reported that the left red unsafe light and orange door open light came on. Fuel consumption was reported as being…
- [Incident 20051218028649I](https://openairdocs.org/incident/20051218028649I), Dec 18, 2005: Doug MD9030 (N902DA), Salt Lake City, UT, Minor damage. (-23) On December 18, 2005 at 1655 MST delta airlines (dala) flt #1711, N902DA, MD-90 landed at Salt Lake City, (slc). Rwy 34, and during rollout the #1 LH…
- [Incident 20010119000139I](https://openairdocs.org/incident/20010119000139I), Jan 19, 2001: Doug MD9030 (N902DA), Santa Ana, CA, Minor damage. (-23)Pilot reported that a/c was set up for "fast landing" on rwy 19R at sna and upon touchdown, anti-skid fail light illuminated. A/c braking caused left…

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