# N919DN: 1997 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: 53576
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: August 10, 2010
- Certificate issued: February 8, 2010
- Last registry action: November 29, 2022
- Mode S code: ACB872
- 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/N919DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=919DN
- Page: https://openairdocs.org/deregistered/N919DN-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 (85, newest 50)

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

- [SDR DALA2020030601662](https://openairdocs.org/sdr/DALA2020030601662), Mar 5, 2020: BATTERY PACK. DISCHARGED. FOUND LWR EMERGENCY PATH LIGHTS ON BOTH FWD DOORS INOP. R/R EMERGENCY LIGHT SLID AND BATTERY PACK B5-211 PER MD90 AM;33 -51. OPS CHECK GOOD . A/C OK FOR SVC. (6
- [SDR DALA2019121607317](https://openairdocs.org/sdr/DALA2019121607317), Dec 16, 2019: BATTERY. INOPERATIVE. ROW 25 EMERGENCY LIGHT OUT C/A R/R BATTERY ASSY PER MD90 AMM 33-51. OPS CHECK IS GOOD AT THIS TIME. (6615064)
- [SDR DALA2019112106793](https://openairdocs.org/sdr/DALA2019112106793), Nov 21, 2019: UNKNOWN. ODOR. WHILE PULLING INTO THE GATE. AFTER LANDING IN SYRACUSE WE ACTIVATED APU AIR. THE FA IN THE AFT CABIN CHIMED THE COCKPIT TO REPORT FUMES THAT SMELLED LIKE RUBBER
- [SDR DALA2019090405135](https://openairdocs.org/sdr/DALA2019090405135), Sep 4, 2019: CABLE. FRAYED. AFT TAILCONE DISPLACEMENT NITROGEN CYLINDER PULL CABLE FRAYED THROUGH. REMOVED AND REPLACED CABLE PER AS REQUIRED PER AMM 53-52. SERVICED NITROGEN CYL PER AMM 1
- [SDR DALA2019013000625](https://openairdocs.org/sdr/DALA2019013000625), Jan 29, 2019: BATTERY. THERMAL RUNAWAY. FOUND BOTH SHIP BATTERIES THERMAL RUNAWAY & BATT CABLES INSULATION MELTED. BATTERIES REMOVED FROM A/C. ROUTED BATT WIRES P48B2 AND P49B2. TERMINATED AND INSTALL
- [SDR DALA2019012300489](https://openairdocs.org/sdr/DALA2019012300489), Jan 22, 2019: SKIN. CRACKED. DURING REPLACEMENT OF RH ATTACH ANGLE WAS FOUND A CRACK ON VERTICAL STABILIZER SKIN STA ZFS= -26.8. VERTICAL STABILIZER SKIN STA ZFS= -26.8 WAS REPAIRED (PERMAN
- [SDR DALA2019012200398](https://openairdocs.org/sdr/DALA2019012200398), Jan 21, 2019: PUSHROD. CORRODED. CORROSION ON RUDDER LIMITER PUSHROD P/N NAS354-4-270. RUDDER LIMITER PUSHROD P/N NAS354-4-270 WAS REPLACED PER AMM 27-23-02-420-801 AND WAS ADJUSTED PER AMM 27-
- [SDR DALA2019012100401](https://openairdocs.org/sdr/DALA2019012100401), Jan 20, 2019: SEAL. MISSING. APPROX 15 IN OF SPANWISE SLAT LOWER TRAILING EDGE SEAL MISSING FROM RT WING. NEW SEAL WAS INSTALLED PER VOL.II SRM 51-30-05 AND VOL.II SRM 51-30-02. (LP# 389713
- [SDR DALA2019011800370](https://openairdocs.org/sdr/DALA2019011800370), Jan 17, 2019: ATTACH ANGLE. CRACKED. CRACKED RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475. RT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475 WAS REPLACED PER SRM 51-30-02
- [SDR DALA2019011800369](https://openairdocs.org/sdr/DALA2019011800369), Jan 17, 2019: ATTACH ANGLE. CRACKED. CRACKED LT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475. LT INTERNAL VERTICAL STABILIZER ATTACH ANGLE ON STA. Y= 1475 WAS REPLACED PER SRM 51-30-02
- [SDR DALA2019011700306](https://openairdocs.org/sdr/DALA2019011700306), Jan 17, 2019: SKIN. CRACKED. CRACK ON EXTERNAL FUSELAGE SKIN AT STA Y=1494 BTW LONGERONS 3R AND 4R. PERMANENT REPAIR WAS PERFORMED SECTION I ON EXTERNAL FUSELAGE SKIN AT STA Y=1494 BTW LONG
- [SDR DALA2019011500305](https://openairdocs.org/sdr/DALA2019011500305), Jan 14, 2019: DOOR FRAME. CRACKED. CRACK ON FWD DOOR JAMB STA Y=1012 X=57. FWD DOOR JAMB STA Y=1012 X=57 WAS REPLACED. (LP# 0904201)
- [SDR DALA2019011300251](https://openairdocs.org/sdr/DALA2019011300251), Jan 12, 2019: FITTING. CORRODED. AWR HIDDEN DAMAGE IN REF MON/9219/045-MON, 92 L/L, 0566067 INSP. CORROSION ON FWD AND AFT LATCH FITTINGS OVER X=-54 WAS FOUND DURING REMOTION FLOOR PANEL 221KF 
- [SDR DALA2018021901001](https://openairdocs.org/sdr/DALA2018021901001), Feb 19, 2018: BATTERY PACK. DISCHARGED. EXIT LIGHTS ABOVE WING EXIT DOORS AT ROW 27 INOP. R&R BATTERY PACK AT ROW 27 PER AMM 33-51 CKS GOOD.
- [SDR DALA2017081506273](https://openairdocs.org/sdr/DALA2017081506273), Aug 12, 2017: SIGN. MISSING. L2 DOOR EXIT SIGN MISSING. INSTALLED. OPERATION CHECKS GOOD.
- [SDR DALA2017061904829](https://openairdocs.org/sdr/DALA2017061904829), Jun 14, 2017: OUTFLOW VALVE. OBSTRUCTED. AT FL280, AUTO PRESSURIZATION ERRATIC. THE AUTO - MANUAL CONTROL SWITCH WAS UNABLE TO SELECT THE MANUAL MODE. CABIN ALTITUDE BEGAN TO RAPIDLY CLIMB. THE OXYGEN 
- [SDR DALA2017061504817](https://openairdocs.org/sdr/DALA2017061504817), Jun 14, 2017: RECEPTACLE. WORN. SEVERAL TAIL CONE GUIDE PIN RECEPTACLES FOUND WORN. REPLACED IAW SRM 51-30-00.
- [SDR DALA2017012000585](https://openairdocs.org/sdr/DALA2017012000585), Jan 19, 2017: SCREW. SHEARED. CENTER CARGO DOOR JAMB HAS 1 SHEARED DOOR STOP ADJUSTMENT SCREW AFT EDGE. REMOVED AND REPLACED CENTER CARGO DOOR JAMB DOOR STOP AND SET SCREW IAW MM 52-31-01.
- [SDR DALA2017012000584](https://openairdocs.org/sdr/DALA2017012000584), Jan 19, 2017: SCREW. SHEARED. AFT CARGO DOOR JAM HAS SHEARED DOOR STOP ADJUSTMENT SCREW AT EDGE. REMOVED AND REPLACED AFT CARGO DOOR JAMB IAW MM 52-31-01.
- [SDR DALA2017011300300](https://openairdocs.org/sdr/DALA2017011300300), Jan 12, 2017: FLOOR SUPPORT. NOT REPORTED. MAIN CABIN FLOOR SUPPORT CRACKED, BS 180, LBL 2 IN E/E COMPARTMENT. REPAIRED IAW SRM 53-00-01.
- [SDR DALA2017011300299](https://openairdocs.org/sdr/DALA2017011300299), Jan 12, 2017: FRAME. CRACKED. CRACKED FRAME ANGLE, BS 180, RBL 0. REMOVED AND REPLACED ANGLE IAW SRM 51-30-02 AND DWG 9936534 AND 9923484.
- [SDR DALA2016051203956](https://openairdocs.org/sdr/DALA2016051203956), May 11, 2016: BATTERY PACK. INOPERATIVE. BOTH AFT OVERWIND EXIT SIGNS BY FLOOR INOPERATIVE, LT AND RT OVERWING HATCHES. REMOVED AND INSTALLED NEW BATTERY IAW MM. OPS CHECKS GOOD.
- [SDR DALA2016040602716](https://openairdocs.org/sdr/DALA2016040602716), Apr 1, 2016: CABLE. BROKEN. TAILCONE JETTISON BOTTLE CABLE BROKEN. INSTALLED NEW CABLE ASSEMBLY.
- [SDR DALA2016012900863](https://openairdocs.org/sdr/DALA2016012900863), Jan 20, 2016: CHARGER. MALFUNCTIONED. BATTERY CHARGER FAIL MESSAGE ON OAP. FOUND ALL 3 BATTERIES VERY HOT. R & R BATTERIES, CHARGER, BATTERY RECEPTACLE PLUGS, AND STARTER RELAY IAW AMM.
- [SDR DALA2015012300588](https://openairdocs.org/sdr/DALA2015012300588), Jan 22, 2015: ATTACH BRACKET. CORRODED. CORROSION AROUND RIVETS OF D-RING ATTACH BRACKETS, TWO ON TAILCONES SLIDE VALISE. R & R THE ATTACH BRACKETS IAW SRM 51-30-02.
- [SDR DALA2015012300587](https://openairdocs.org/sdr/DALA2015012300587), Jan 21, 2015: FRAME. CORRODED. AFT ACCESSORY COMPARTMENT, FRAME BS 1520 BETWEEN LONGERONS 1 - 24L, LOWER END OF FRAME HAS SEVERAL SPOTS WITH CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF L
- [SDR DALA2015012500679](https://openairdocs.org/sdr/DALA2015012500679), Jan 19, 2015: CARGO TRACK. CORRODED. AFT CARGO BAY CARGO TRACK BETWEEN BS 1160-1307 CORRODED. FOUND TO BE OUT OF LIMITS. R & R THE CARGO TRACK IAW SRM 53-40-01, FIG 5. AND FIG 7.
- [SDR DALA2015012200585](https://openairdocs.org/sdr/DALA2015012200585), Jan 19, 2015: ANGLE. CORRODED. CORROSION ON ANGLE AND INTERNAL FUSELAGE SKIN AT LT SIDE OF VENTRAL STAIRS CUTOUT BS 1463-1480. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INS
- [SDR DALA2015012000418](https://openairdocs.org/sdr/DALA2015012000418), Jan 17, 2015: BAR. CORRODED. LEFT FLAP FLEX JOINT LOWER BAR HAS CORRODED. SEVERAL COUNTER SUNK HOLES. REMOVED CORROSION. REPAIRED IAW ERA 531458-14.
- [SDR DALA2015011800415](https://openairdocs.org/sdr/DALA2015011800415), Jan 17, 2015: SKIN. CORRODED. CORROSION ON ANGLE AND INTERNAL FUSELAGE SKIN ON RT SIDE OF VENTRAL STAIR CUTOUT, BS 1463 - 1480. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND I
- [SDR DALA2015012100426](https://openairdocs.org/sdr/DALA2015012100426), Jan 15, 2015: LANYARD. TORN. L1 DOOR EVACUATION SLIDE LANYARD TORN. REMOVED AND INSTALLED NEW LANYARD IAW AMDS 2561-4641.
- [SDR DALA2015011800416](https://openairdocs.org/sdr/DALA2015011800416), Jan 15, 2015: CARGO TRACK. CORRODED. CENTER CARGO BAY LT SIDE CARGO TRACK BETWEEN BS 522-845 HAS CORROSION AROUND FASTENERS, NUT PLATES AND FLANGES. REMOVED THE CORROSION AND FOUND THE FLANGES TO B
- [SDR DALA2015011700414](https://openairdocs.org/sdr/DALA2015011700414), Jan 15, 2015: FRAME. CRACKED. AFT ACCESSORY COMPARTMENT FRAME CRACKED AT LONGERON 2R, BS 1494. REMOVED CRACKED FRAME. FABRICATED AND INSTALLED NEW FRAME IAW DWG 9911860, REV L AND SRM 51-30-
- [SDR DALA2015011700413](https://openairdocs.org/sdr/DALA2015011700413), Jan 15, 2015: FRAME. CRACKED. AFT ACCESSORY COMPARTMENT BS 1494, LONGERON 2R FRAME CRACKED. REMOVED CRACKED FRAME ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-10-05, FIG 1 AND DWG 99
- [SDR DALA2015011600591](https://openairdocs.org/sdr/DALA2015011600591), Jan 14, 2015: FINGER DOUBLER. DAMAGED. AFT ACCESSORY COMPARTMENT CANTED FRAME FINGER DOUBLER AT BS 1542 DAMAGED. REMOVED DAMAGED FRAME SECTION. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DWG 991
- [SDR DALA2015011400305](https://openairdocs.org/sdr/DALA2015011400305), Jan 13, 2015: FITTING. CORRODED. TWO TAILCONE SLIDE HOLD DOWN STRAP FITTINGS CORRODED. REMOVED AND INSTALLED TAILCONE SLIDE FORWARD HOLD DOWN STRAPS.
- [SDR DALA2015011400303](https://openairdocs.org/sdr/DALA2015011400303), Jan 12, 2015: DOOR FRAME. CORRODED. AFT CARGO DOOR FRAME CORRODED. FOUND CORROSION ON REPAIR SPACER. FABRICATED AND INSTALLED NEW SPACER IAW SRM 53-60-02, FIG 9A.
- [SDR DALA2015011200290](https://openairdocs.org/sdr/DALA2015011200290), Jan 10, 2015: LANYARD. TORN. L2 DOOR EVACUATION SLIDE LANYARD CABLE ASSEMBLY IS TORN. REMOVED AND INSTALLED NEW SLIDE LANYARD IAW AMDS 2561-4642.
- [SDR DALA2015011200287](https://openairdocs.org/sdr/DALA2015011200287), Jan 9, 2015: ANGLE. CRACKED. ANGLE CRACKED AT BS 1475, LONGERON 2L, AFT SIDE. REMOVED AND REPLACED IAW DWG 9964461, REV W.
- [SDR DALA2015011200286](https://openairdocs.org/sdr/DALA2015011200286), Jan 9, 2015: ANGLE. CRACKED. CRACKED ANGLE AT BS 1475, LONGERON 2R. REMOVED AND REPLACED IAW DWG 9964461, REV W.
- [SDR DALA2015011200285](https://openairdocs.org/sdr/DALA2015011200285), Jan 9, 2015: ANGLE. CRACKED. CRACKED ANGLE AT FRAME 1475, LONGERON 2R, REMOVED AND REPLACED IAW DWG 5911432, REV CE AND SRM 51-30-05.
- [SDR DALA2015011200284](https://openairdocs.org/sdr/DALA2015011200284), Jan 9, 2015: ANGLE. CRACKED. CRACKED ANGLE AT FRAME 1475, LONGERON 2L, REMOVED AND REPLACED IAW DWG 5911432.
- [SDR DALA2016102607686](https://openairdocs.org/sdr/DALA2016102607686), Jan 7, 2015: RUB STRIP. CORRODED. FUEL PANEL 520DT RUBSTRIP CORRODED. REMOVED AND REPLACED RUBSTRIP IAW SRM 57-00-04.
- [SDR DALA2016102607685](https://openairdocs.org/sdr/DALA2016102607685), Jan 7, 2015: RUB STRIP. CORRODED. FUEL PANEL 620CT RUBSTRIP CORRODED. REMOVED AND REPLACED RUBSTRIP IAW SRM 57-00-04.
- [SDR DALA2016102607684](https://openairdocs.org/sdr/DALA2016102607684), Jan 7, 2015: RUB STRIP. CORRODED. FUEL PANEL RUBSTRIP CORRODED. REMOVED AND REPLACED RUBSTRIP IAW SRM 57-00-04.
- [SDR DALA2015010700138](https://openairdocs.org/sdr/DALA2015010700138), Jan 5, 2015: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT IN FORWARD WET AREA, BS 148-200 HAS CORROSION, LBL 10. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IA
- [SDR DALA2015010700137](https://openairdocs.org/sdr/DALA2015010700137), Jan 5, 2015: FRAME. DAMAGED. BS 1003 FRAME LBL 50 HAS TWO .2500" HOLES DRILLED WITHOUT APPROPRIATE SPACING. FABRICATED A STANDARD REPAIR IAW SRM 51-31-01 AND ERA 504723-14, REV O. (LP 17718
- [SDR DALA2016102607683](https://openairdocs.org/sdr/DALA2016102607683), Jan 3, 2015: STRAP. CORRODED. CORROSION ON TAILCONE STRAPS. REMOVED AND REPLACED STRAP IAW AMM.
- [SDR DALA2015010600134](https://openairdocs.org/sdr/DALA2015010600134), Jan 2, 2015: INTERCOSTAL. CRACKED. MAIN CABIN, INTERCOSTAL BETWEEN BS 826-845 AT BL 0 HAS TWO CRACKS ON TOP ISDE. R & R INTERCOSTAL IAW SRM 51-30-02, 51-30-05 AND DWG 9936580, REV BW.
- [SDR DALA2015010100011](https://openairdocs.org/sdr/DALA2015010100011), Dec 31, 2014: CUSP WEB. CORRODED. RIGHT SIDE CUSP WEB BETWEEN BS 731-712 SHOWS EVIDENCE OF CORROSION. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. INSTALLED A NEW CUSP WEB IAW DWG 9940443, REV 

All 85: https://openairdocs.org/deregistered/N919DN-2022-11-29/reports.md

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