# N904DA: 1995 Mcdonnell Douglas MD-90-30, registration cancelled 2020-10-08 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 8, 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: 53384 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 1, 1999 - Certificate issued: May 15, 1995 - Last registry action: February 20, 2020 - Mode S code: AC7E54 - 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/N904DA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=904DA - Page: https://openairdocs.org/deregistered/N904DA-2020-10-08 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 (93, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2018022101052](https://openairdocs.org/sdr/DALA2018022101052), Feb 20, 2018: POWER SUPPLY. INOPERATIVE. MULTIPLE EMER LIGHTS IN F/C INOP. REMOVED & REPLACED APPLICABLE BATTERY POWER SUPPLY. OPS CHECK GOOD. - [SDR DALA2018022101051](https://openairdocs.org/sdr/DALA2018022101051), Feb 20, 2018: WIRE. DISCONNECTED. TAIL COMP CATWALK ONE EMER LIGHT INOP. RECONNECTED WIRES & OPS CHECK GOOD. - [SDR DALA2017111508150](https://openairdocs.org/sdr/DALA2017111508150), Nov 13, 2017: HANDLE. LACK OF LUBE. TAILCONE EMERGENCY RELEASE HANDLE EXCEEDS OPENING FORCE DURING TEST. ADJUSTED AND LUBED THE DOOR IAW MM. OPS CHECKED GOOD. - [SDR DALA2017101607531](https://openairdocs.org/sdr/DALA2017101607531), Oct 16, 2017: FIRE LOOP. BROKEN. DURING CLIMBOUT, RT ENGINE FIRE DETECTION FAULT ILLUMINATED. AIR RETURN DUE TO QRH GUIDANCE. C/W ODI EVENT, WORKCARD 2611-2002 R ENG FIRE DETECTION INT CHECK FO - [SDR DALA2018020600712](https://openairdocs.org/sdr/DALA2018020600712), Oct 5, 2017: LEVER. BINDING. AT FLARE FOR LANDING, ELEV CONTROL MAN ILLUMINATED AND YOKE CONTROL OF ELEVATOR FELT FROZEN OR JAMMED. DID NOT FEEL MERELY UN BOOSTED AND HYDRAULIC ELEVATOR CON - [SDR DALA2017101107441](https://openairdocs.org/sdr/DALA2017101107441), Oct 2, 2017: CONNECTOR. DISCONNECTED. THREE CEILING EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 32A, 39C, & 1 IN THE CATWALK. EMERGENCY LIGHT IN TAIL, FOUND FIXTURE ASSY WIRED WRONG, MOVED WIRE TO PRO - [SDR DALA2017071005301](https://openairdocs.org/sdr/DALA2017071005301), Jul 6, 2017: WIRE. DISCONNECTED. CATWALK FIRST SIDEWALL EMERGENCY LIGHT INOPERATIVE. FOUND WIRE DISCONNECTED. INSTALLED NEW PIN AND SOCKET. OPERATION CHECKED GOOD. - [SDR DALA2017032702456](https://openairdocs.org/sdr/DALA2017032702456), Mar 24, 2017: LENS. UNSECURE. EMERGENCY EXIT SIGN COVER LOOSE. SECURED. - [SDR DALA2017031502081](https://openairdocs.org/sdr/DALA2017031502081), Mar 11, 2017: LIGHT. MISSING. EMERGENCY LIGHT MISSING AT ROW 26 ABC. REPLACED THE EMERGENCY LIGHT IAW MM. OPS CHECKED GOOD. - [SDR DALA2017011200298](https://openairdocs.org/sdr/DALA2017011200298), Jan 11, 2017: SUPPORT FRAME. CRACKED. FOUND 2 CRACKS IN RIGHT NOSE LANDING GEAR SUPPORT FRAME BETWEEN BS 40 AND 60. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW ERA 55383 - [SDR DALA2017011300301](https://openairdocs.org/sdr/DALA2017011300301), Jan 9, 2017: PANEL. CRACKED. EMPENNAGE VENTRAL STAIRWAY AFT CUT OUT HAS 8 INCH CRACK IN LIGHT PANEL. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW WEB SECTION IAW PRI/ERA 553835-14 AND DWG 9 - [SDR DALA2017011000297](https://openairdocs.org/sdr/DALA2017011000297), Jan 9, 2017: VANE. GOUGED. RIGHT WING OUTBOARD FLAP VANE LEADING EDGE GOUGED. REPAIRED IAW ERA 553839-14, REV O. AND SRM 51-10-02. - [SDR DALA2017011000296](https://openairdocs.org/sdr/DALA2017011000296), Jan 9, 2017: SKIN. CRACKED. RIGHT WING FIXED LEADING EDGE BELOW SLAT TRACK NR 8 SKIN CRACKED. REPAIRED IAW SRM 57-20-01. - [SDR DALA2017011000295](https://openairdocs.org/sdr/DALA2017011000295), Jan 9, 2017: FITTING. CRACKED. CRACK IN THE RIGHT FITTING AT AUX SPAR TO EMPENNAGE ATTACH POINT. REMOVED AND REPLACED FITTING IAW SRM 51-30-02, 51-30-05, AND 51-10-05. - [SDR DALA2017011000293](https://openairdocs.org/sdr/DALA2017011000293), Jan 9, 2017: NOT REPORTED. CRACKED. CRACK FOUND AT THE AFT EMERGENCY WALK WAY. REPAIRED IAW SRM 51-70-01. - [SDR DALA2017010900250](https://openairdocs.org/sdr/DALA2017010900250), Jan 7, 2017: ATTACH FITTING. CRACKED. CRACK IN LEFT HAND FITTING AT AUXILIARY SPAR ATTACH TO EMPENNAGE. REMOVED AND REPLACED LEFT HAND AUX SPAR ATTACH FITTING IAW SRM 51-30-05, 51-30-01 AND DWG 9917 - [SDR DALA2017010600163](https://openairdocs.org/sdr/DALA2017010600163), Jan 5, 2017: SKIN. DELAMINATED. LEFT AILERON LOWER SURFACE HAS SMALL AREA OF DELAMINATION. HOT BONDED PERMANENT REPAIR INTO LEFT AILERON LOWER SURFACE IAW SRM 57-50-02 AND 51-10-04. - [SDR DALA2017010500162](https://openairdocs.org/sdr/DALA2017010500162), Jan 3, 2017: CUSP WEB. CORRODED. FOUND CUSP MEMBRANE CRACKED AT BS 955, LBL 64. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER, FILLER AND RING DOUBLER IAW SRM 53-20-02. - [SDR DALA2017010400059](https://openairdocs.org/sdr/DALA2017010400059), Jan 3, 2017: SKIN. CRACKED. CRACK VERIFICATION. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER ON RIGHT AFT NLG DOOR AFT HINGE CUTOUT IAW SRM 53-30-01. - [SDR DALA2017010400058](https://openairdocs.org/sdr/DALA2017010400058), Jan 3, 2017: SKIN. CRACKED. EXTERIOR FUSELAGE, AFT HINGE CUTOUT IS CRACKED AT AFT NLG DOOR. STOPPED DRILLED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-01. - [SDR DALA2016091906729](https://openairdocs.org/sdr/DALA2016091906729), Sep 18, 2016: BAYONET. WORN. DURING TAIL CONE EMERGENCY RELEASE, FOUND LT SIDE UPPER AND LOWER TAIL CONE BAYONETS WORN. REPLACED IAW CMM. - [SDR DALA2016081706062](https://openairdocs.org/sdr/DALA2016081706062), Aug 8, 2016: BULB. WRONG PART. EMERGENCY LIGHT NEAR L1 DOOR IS DIM. FOUND INCORRECT BULB INSTALLED AND EMERGENCY LIGHT ASSEMBLY AND STANDBY LIGHT ASSEMBLY CORRECTED. OPS CHECKED OK. - [SDR DALA2016051203955](https://openairdocs.org/sdr/DALA2016051203955), May 9, 2016: BOTTLE. LOW PRESSURE. R1 DOOR SLIDE PRESSURE LOW. R & R DOOR SLIDE IAW AMDS 2561-4641. - [SDR DALA2015020200840](https://openairdocs.org/sdr/DALA2015020200840), Jan 30, 2015: TRANSMITTER. LEAKING. ON GROUND, WITH EXTERNAL AIR CONNECTED, STRONG ODOR OF FUEL AND EXHAUST FUMES FROM MID TO AFT OF ACFT. ODOR WAS PRESENT THROUGH MID CLIMB. MAINTENANCE FOUND FUE - [SDR DALA2014121306576](https://openairdocs.org/sdr/DALA2014121306576), Dec 12, 2014: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT FASTENER, RT SIDE, BS 1437, 12 INCHES ABOVE RT PYLON. REPAIRED IAW PRI 531221-14, REV O. - [SDR DALA2014120906510](https://openairdocs.org/sdr/DALA2014120906510), Dec 9, 2014: FASTENER. LOOSE. LOOSE FASTENERS AT STA ZFS = 52.267 VERTICAL STABILIZER L/E. FOUND FIVE TOTAL HOLES OUT OF LIMITS AND REQUIRED BUSHING REPAIR IAW SG09550004-7003. INSTALLED DOU - [SDR DALA2014120906512](https://openairdocs.org/sdr/DALA2014120906512), Dec 7, 2014: SKATE ANGLE. CRACKED. INTERNAL STABILIZER ATTACH ANGLE CRACKED, LT SIDE BS 1458 - 1486. R & R THE SKATE ANGLE IAW DWG 5912188. - [SDR DALA2014120906511](https://openairdocs.org/sdr/DALA2014120906511), Dec 7, 2014: SKATE ANGLE. CRACKED. INTERNAL STABILIZER ATTACH ANGLE RT SIDE, BS 1458-1486 CRACKED. R & R SKATE ANGLE IAW DWG 5912188. - [SDR DALA2014090304894](https://openairdocs.org/sdr/DALA2014090304894), Aug 31, 2014: WIRE. DISCONNECTED. ALL AFT AIRSTAIRS LIGHTS INOPERATIVE. FOUND WIRES DISCONNECTED, CONNECTED THE WIRES AND OPERATES NORMAL. - [SDR DALA13066079204](https://openairdocs.org/sdr/DALA13066079204), Dec 2, 2013: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS FOR TAIL SECTION CATWALK INOPERATIVE. MAINTENANCE R & R BATTERY PACK, B5-212. OPERATION CHECKS GOOD. - [SDR DALA13066069204](https://openairdocs.org/sdr/DALA13066069204), Dec 2, 2013: WIRE. LOOSE. DURING SERVICE CHECK, TWO EMERGENCY LIGHTS INOPERATIVE AROUND ROW 35 AND 38. MAINTENANCE FOUND CONNECTOR WIRES J2-38B AND J2-48A LOOSE. RESEATED. OPS CHECKED GO - [SDR DALA13050419204](https://openairdocs.org/sdr/DALA13050419204), Oct 4, 2013: LAMP. INOPERATIVE. DURING SERVICE CHECK, MX FOUND EMERGENCY CEILING LIGHT ROW 38R INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD. - [SDR DALA13050409204](https://openairdocs.org/sdr/DALA13050409204), Oct 4, 2013: LAMP. INOPERATIVE. DURING SERVICE CHECK, MX FOUND EMERGENCY LIGHT ROW 36L, INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD. - [SDR DALA13048009204](https://openairdocs.org/sdr/DALA13048009204), Sep 29, 2013: WIRE. DISCONNECTED. DURING SERVICE CHECK, OVERWING EMERGENCY EXIT SIGN INOPERATIVE. FOUND WIRES DISCONNECTED IN CEILING PANEL. RECONNECTED WIRES. OPERATION CHECKS GOOD. - [SDR DALA13014499204](https://openairdocs.org/sdr/DALA13014499204), Mar 31, 2013: BULB. BURNED OUT. L1 DOOR EMERGENCY EXIT SIGN OVER DOOR INOPERATIVE. REPLACED LAMP. OPERATION CHECKED GOOD. OK FOR SERVICE. - [SDR DALA13008459204](https://openairdocs.org/sdr/DALA13008459204), Feb 19, 2013: SLIDE. DAMAGED. L1 DOOR SLIDE, CANNOT SEE HORIZONTAL LINE ON THE GIRT BOTTOM EDGE IAW MM 25-61-01-420-801, PG 3. R & R L1 DOOR SLIDE IAW AMM. - [SDR DALA13008439204](https://openairdocs.org/sdr/DALA13008439204), Feb 17, 2013: CUSP WEB. CRACKED. MAIN CABIN CUSP WEB AT STRINGER 18 IS CRACKED AT THE LIGHTNING HOLE LOCATED AT STA 1355R. REPAIRED MAIN CABIN CUSP WEB IAW SRM 51-10-03, 53-20-02 AND 53-10-03. - [SDR DALA13008109204](https://openairdocs.org/sdr/DALA13008109204), Feb 17, 2013: RIB. CRACKED. RT WING FIXED L/E RIB AT OTBD EDGE OF SLAT IS CRACKED AT LOWER END. REJECTED, EDGE DISTANCE WAS NOT MAINTAINED ON REPAIR. REPAIRED CRACK AND MISDRILLED HOLES IA - [SDR DALA13008089204](https://openairdocs.org/sdr/DALA13008089204), Feb 16, 2013: STRINGER. CRACKED. AFT AIRSTAIR AREA SKIN AT BS 1520 CANTED BULKHEAD STRINGER 4R IS CRACKED. REPAIRED STRINGER IAW ER/A 510924-14 REV O. - [SDR DALA13008079204](https://openairdocs.org/sdr/DALA13008079204), Feb 16, 2013: BULKHEAD WEB. CRACKED. AFT AIRSTAIR AREA AT BS 1520 STRINGER 4L BULKHEAD WEB IS CRACKED. REPAIRED BULKHEAD IAW ER/A 510925-14 REV O. - [SDR DALA13008399204](https://openairdocs.org/sdr/DALA13008399204), Feb 15, 2013: SUPPORT BRACKET. DAMAGED. LEFT WHEEL WELL PANEL SUPPORT BRACKET DAMAGED. R & R SUPPORT BRACKET IAW ER/A 510934-14, REV O. - [SDR DALA13007949204](https://openairdocs.org/sdr/DALA13007949204), Feb 15, 2013: ANGLE. CORRODED. AFT LAVATORY BS 1364, LBL 20 ANGLE CORRODED. REMOVED CORROSION. 100 PERCENT MATERIAL LOSS. OUT OF LIMITS. REPAIRED IAW ER/A 510933-14, REV O. - [SDR DALA13008269204](https://openairdocs.org/sdr/DALA13008269204), Feb 13, 2013: STRUCTURE. CORRODED. DURING HMV, FOUND AFT CARGO BS 1344, BETWEEN STR 25 AND 26L EVIDENCE OF CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED FILLER, TREATED, PRI - [SDR DALA13006789204](https://openairdocs.org/sdr/DALA13006789204), Feb 9, 2013: SEAT TRACK. CORRODED. AFT LAVATORY, BS 1364 LBL 22 SEAT TRACK UPPER END CORRODED. REMOVED CORROSION. OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, FIG 6. - [SDR DALA13006889204](https://openairdocs.org/sdr/DALA13006889204), Feb 8, 2013: SKIN. CORRODED. VERTICAL TIP FORWARD END, RT SIDE FRAME FOR SKIN PANEL CORRODED. WORK ACCOMPLISHED ON ER/A 510927-14, REV O. - [SDR DALA13006879204](https://openairdocs.org/sdr/DALA13006879204), Feb 8, 2013: FRAME. CORRODED. VERTICAL STABILIZER UPPER FORWARD END, LT SIDE FRAME FOR SKIN PANEL, CORRODED. WORK ACCOMPLISHED ON ER/A 510927-14, REV O. - [SDR DALA13006779204](https://openairdocs.org/sdr/DALA13006779204), Feb 8, 2013: FLOORBEAM. CORRODED. AFT CABIN BS 1364, LBL 20 FLOORBEAM CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW ERA 510933-14, REV. - [SDR DALA13006849204](https://openairdocs.org/sdr/DALA13006849204), Feb 7, 2013: WEB. CORRODED. FORWARD GALLEY RT SIDE BS 160 SUPPORT WEB CORRODED. REMOVED CORROSION, OUT OF LIMITS IAW 53-00-01. OK FOR SERVICE IAW ERA 510923-14, REV O. - [SDR DALA13006829204](https://openairdocs.org/sdr/DALA13006829204), Feb 6, 2013: CARGO TRACK. DAMAGED. AFT CARGO COMPARTMENT BS 1212-1250 LT CARGO TRACK HAS SEVERAL PREVIOUS MISDRILLED HOLES. INSTALLED CARGO TRACK LT, STA 1174-1250 IAW SRM 53-40-01, PG 40. - [SDR DALA13006729204](https://openairdocs.org/sdr/DALA13006729204), Feb 6, 2013: CARGO TRACK. CORRODED. AFT CARGO COMPARTMENT BS 1174 TO 1212 LT CARGO TRACK SUPPORT HAS LIGHT CORROSION AT SCREW HOLES. FABRICATED NEW CARGO TRACK SECTION IAW 53-40-01, FIG 7 FOUND AD All 93: https://openairdocs.org/deregistered/N904DA-2020-10-08/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 20081025851249I](https://openairdocs.org/incident/20081025851249I), Oct 25, 2008: Doug MD9030 (N904DA), Salt Lake City, UT, Minor damage. (-23) Delta flight 1147 aborted takeoff on runway 17 abeam taxiway kilo 5. The pilot reported ingesting a large white bird in the right engine at v 1 speed.… - [Incident 19990325016639I](https://openairdocs.org/incident/19990325016639I), Mar 25, 1999: Doug MD9030 (N904DA), Santa Ana, CA, Minor damage. (-5)During landing phase on a wet runway at John Wayne airport, the left side anti-skid apparently failed, causing the left inboard tire to blow out from the… --- 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.