# N923DN: Boeing 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: [Boeing MD-90-30](https://openairdocs.org/model/boeing-md-90-30) (registry code 13848ME)
- 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: 53585
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 24, 2011
- Certificate issued: May 26, 2010
- Last registry action: January 14, 2020
- Mode S code: ACC9A7
- 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/N923DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=923DN
- Page: https://openairdocs.org/deregistered/N923DN-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 Boeing MD-90-30: https://openairdocs.org/model/boeing-md-90-30.md

## Service difficulty reports (177, newest 50)

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

- [SDR DALA2019100605737](https://openairdocs.org/sdr/DALA2019100605737), Oct 6, 2019: FITTING. CRACKED. DUE VERIFICATION FLIGHT DUE TO LT MLG UNSAFE LIGHT. VERIFICATION OF LANDING GEAR OPERATION FAILS. WHEN GEAR HANDLE SELECTED DOWN GOT 3 GREEN AND AMBER DOOR LIGH
- [SDR DALA2019100605738](https://openairdocs.org/sdr/DALA2019100605738), Oct 5, 2019: ARM. LOOSE. LANDING GEAR UNSAFE. GEAR HANDLE UP. LEFT GEAR UNSAFE IN UP POSITION. RAN QRH GEAR DOOR LIGHT DID NOT EXTINGUISH UPON LOWERING GEAR. COMPLETED PROCEDURE AND LAN
- [SDR DALA2019062653867](https://openairdocs.org/sdr/DALA2019062653867), Jun 24, 2019: LINE. LEAKING. STRONG SMELL OF OIL POSSIBLY FUEL FROM START TO CLIMBING OUT OF 10000 (10 MINS). FA'S DID NOT NOTICE SMELL IN CABIN. FOUND APU FUEL NOZZLE HARD LINE LEAKING. RE
- [SDR DALA201906203673](https://openairdocs.org/sdr/DALA201906203673), Jun 19, 2019: FUEL CONTROL. LEAKING. FUEL ODOR IN CABIN AFTER STARTING APU ON TAXI IN. APU AIR SWITCH ON. CONFIRMED FUEL SMELL IN CABIN(AFT). FOUND APU FUEL CONTROL LEAKING FUEL AT LOWER FITTING. T
- [SDR DALA201904232580](https://openairdocs.org/sdr/DALA201904232580), Apr 19, 2019: DOOR FRAME. CORRODED. DURING REMOTION OF RETAINERS WAS FOUND CORROSION ON INTERNAL PRODUCTION DOUBLER AT LOWER DOOR JAMB OF AFT CARGO COMPARTMENT SUMMARY: OF NRC 00180 ON INTERNAL PR
- [SDR DALA201904232579](https://openairdocs.org/sdr/DALA201904232579), Apr 19, 2019: DOOR FRAME. CORRODED. INITIAL INSPECTION: CORROSION ON DOOR JAMB LOWER AREA. AT AFT CARGO COMPARTMENT. CORROSION ON DOOR JAMB LOWER AREA WAS REPAIRED (AS PERMANENT REPAIR) PER MD90 V
- [SDR DALA2019042392577](https://openairdocs.org/sdr/DALA2019042392577), Apr 18, 2019: SKIN. CRACKED. INITIAL INSPECTION: CRACK ON FUSELAGE SKIN ON AFT NLG DOOR AFT HINGE RH SIDE. FUSELAGE SKIN ON AFT RH NLG DOOR AFT HINGE, WAS REPAIRED (AS PERMANENT REPAIR) PER
- [SDR DALA2019042392576](https://openairdocs.org/sdr/DALA2019042392576), Apr 18, 2019: SKIN. CRACKED. INITIAL INSPECTION: CRACK ON FUSELAGE SKIN STA. Y=1437 AND BTW LONGERONS 12RH AND 13RH. SUMMARY OF NRC 00058 FUSELAGE SKIN STA Y=1437 AND BTW LONGERONS 12RH AND
- [SDR DALA2019041702500](https://openairdocs.org/sdr/DALA2019041702500), Apr 16, 2019: SKIN. CRACKED. CRACK ON FUSELAGE SKIN STA. 1494 BTW LONGERONS 3 AND 4 LH SIDE. PERMANENT REPAIR SCTION I WAS PERFORMED ON FUSELAGE SKIN STA. 1494 BTW LONGERONS 3 AND 4 LH SIDE
- [SDR DALA20190402084](https://openairdocs.org/sdr/DALA20190402084), Mar 6, 2019: SPAR. CORRODED. REAR SPAR LOWER CHORD / BS 161 / LEFT WING / CORROSION REMOVAL PSE 57.11.02.2 - PERMANENT REPAIR ACCOMPLISHMENT. CURRENT REVISION OF ER/A 525623-14AD IS REV. C.
- [SDR DALA2019030401404](https://openairdocs.org/sdr/DALA2019030401404), Mar 1, 2019: GROMMET. DEFECTIVE. CAPT PFD INOP CB POPPED. ELECTRICAL BURN SMELL EVIDENT. REPOSITIONED CAPTS INSTRUMENT PANEL AND INSP AREA NO LEAKS NOTED. APPLIED WATER TO CAPT WINDSHIELD AND W
- [SDR DALA2019022601214](https://openairdocs.org/sdr/DALA2019022601214), Feb 25, 2019: TERMINAL. LOOSE. SMOKE STARTED COMING FROM FWD WINDOW RIGHT SIDE OF COCKPIT STOPPED WHEN WINDSHIELD ANTI ICE SWITCH ON RT WAS TURNED OFF. WINDSHIELD DEACTIVATED PER MEL 30-41-01
- [SDR DALA2019011700308](https://openairdocs.org/sdr/DALA2019011700308), Jan 17, 2019: CABLE. SEVERED. TAILCONE JETTISON BOTLLE TRIGGER CABLE SEVERED IN HALF ONE HANGING. REMOVED AND REPLACED TAILCONE DISPLACEMENT SYST BALL VALVE CABLE. OK FOR SERVICE. (LP#531030
- [SDR DALA2018082805306](https://openairdocs.org/sdr/DALA2018082805306), Aug 24, 2018: DOOR FRAME. CRACKED. RIGHT MAIN LANDING GEAR FORWARD DOOR FRAME CHANNEL WAS CRACKED. REMOVED, DRILLED THE REPLACEMENT FRAME IAW DWG 5930584-503. INSTALLED THE DOOR FRAME IAW DWG 593
- [SDR DALA2018070204343](https://openairdocs.org/sdr/DALA2018070204343), Jul 2, 2018: WIRE. BROKEN. AFT ACCESSORY COMPARTMENT LT SIDE OF CATWALK HAS INOP EMERGENCY LIGHT. IDENTIFIED FIXTURE AS L2-845. RANG FROM P1-1211 TO R5-3803, R5-3804. FOUND R5-3803 OPEN, 
- [SDR DALA2018060873895](https://openairdocs.org/sdr/DALA2018060873895), Jun 6, 2018: ACTUATOR. LEAKING. LOW HYD QTY LT SYSTEM. RAN QRH & TURNED OFF LT HYD PUMP. SYSTEM DID NOT REPRESSURIZE ON LANDING. FOUND THE LT LOWER INBOARD SLEEVE ACTUATOR LEAKING FROM THE SHA
- [SDR DALA2018060403792](https://openairdocs.org/sdr/DALA2018060403792), Jun 3, 2018: CABLE. FRAYED. TAIL CONE DISPLACEMENT SYSTEM ACTUATION PULL CABLE WORN/FRAYED. TAIL CONE DISPLACEMENT SYSTEM ACTUATION PULL CABLE REMOVED AND REPLACED IAW AMM 53-52.
- [SDR DALA201805153105](https://openairdocs.org/sdr/DALA201805153105), May 6, 2018: BOTTLE. LOW PRESSURE. DURING A SERVICE CHECK, FOUND THE TAILCONE NITROGEN BOTTLE OUT OF RANGE FOR TEMP. SERVICED THE TAILCONE BOTTLE IAW AMM 12-18-01.
- [SDR DALA2017111508149](https://openairdocs.org/sdr/DALA2017111508149), Nov 14, 2017: CONNECTOR. DAMAGED. CATWALK EMERGENCY LIGHT INOPERATIVE. RESET A PIN IN THE CONNECTOR IAW SWPM. OPS CHECKED GOOD. (LP# 4020528)
- [SDR DALA2017111308086](https://openairdocs.org/sdr/DALA2017111308086), Nov 11, 2017: POWER SUPPLY. INOPERATIVE. FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY.
- [SDR DALA2017070305200](https://openairdocs.org/sdr/DALA2017070305200), Jun 19, 2017: LINE. LEAKING. WHILE LOADING PASSENGERS, THE FLIGHT CREW REPORTED AN ODOR IN THE CABIN. ALSO NOTED ODOR IN COCKPIT. THE APU HAD INGESTED HYDRAULIC FLUID INTO THE APU INLET. IS
- [SDR DALA2017050103527](https://openairdocs.org/sdr/DALA2017050103527), Apr 28, 2017: RETAINER. DAMAGED. BRACKET THAT HOLDS GIRT BAR AT R1 DOOR HAS A SPLIT IN IT AND GIRT BAR DROPS DOWN. INSTALLED NEW RETAINER ASSEMBLY. OPERATION CHECKED OK.
- [SDR DALA2017040302675](https://openairdocs.org/sdr/DALA2017040302675), Mar 31, 2017: BUSHING. SCRATCHED. HORIZONTAL STABILIZER SCRATCHED ON RIGHT BUSHINGS,XE49, XE103, AN XE157. REPLACED THE BUSHINGS IAW ERA 549239-14, REV O.
- [SDR DALA2017040302677](https://openairdocs.org/sdr/DALA2017040302677), Mar 30, 2017: BUSHING. SCRATCHED. SCRATCHES ON HINGE BUSHINGS. NEW BUSHINGS INSTALLED IAW ERA 556356-14, REV O.
- [SDR DALA2017040302674](https://openairdocs.org/sdr/DALA2017040302674), Mar 30, 2017: BUSHING. SCRATCHED. HORIZONTAL STABILIZER SCRATCHED ON RIGHT BUSHINGS. NEW BUSHINGS INSTALLED IAW ERA 549239-14, REV O.
- [SDR DALA2017033102669](https://openairdocs.org/sdr/DALA2017033102669), Mar 30, 2017: INTERCOSTAL. CORRODED. AFT CARGO BAY CORRODED ON THE INTERCOSTAL, BS 1269 - 1288, LONGERON 29L. REPLACED THE INTERCOSTAL IAW SRM 51-30-05.
- [SDR DALA2017033002571](https://openairdocs.org/sdr/DALA2017033002571), Mar 29, 2017: FRAME. CRACKED. CRACKED ON OVERWING FRAME, BS 962, LEFT. REPLACED THE FRAME IAW SRM 51-30-02 AND 51-30-05.
- [SDR DALA2017032802569](https://openairdocs.org/sdr/DALA2017032802569), Mar 27, 2017: SPAR. DAMAGED. BENT DIAPHRAGM AND ELONGATED RIVET HOLE ON LEFT WING REAR SPAR, XRS 457. REPAIRED IAW SRM 51-10-05 AND 57-00-01.
- [SDR DALA2017032402454](https://openairdocs.org/sdr/DALA2017032402454), Mar 23, 2017: SKIN. CORRODED. CORROSION ON HORIZONTAL STABILIZER SKIN. REPAIRED IAW ERA 556326-14, REV O.
- [SDR DALA2017032402453](https://openairdocs.org/sdr/DALA2017032402453), Mar 23, 2017: FUEL TANK. CORRODED. CORROSION ON CENTER FUEL TANK, BETWEEN BS 898 AND 902, LBL 56. REPAIRED IAW ERA 555641-14AD.
- [SDR DALA2017032402452](https://openairdocs.org/sdr/DALA2017032402452), Mar 23, 2017: FUEL TANK. CORRODED. CORROSION ON CENTER FUEL TANK BS 926, LBL 56. REPAIRED IAW ERA 555641-14AD.
- [SDR DALA2017032302451](https://openairdocs.org/sdr/DALA2017032302451), Mar 23, 2017: LONGERON. CORRODED. CORROSION ON LONGERON 30 BETWEEN BS 168 AND 218 E/E COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 51-30-02, 53-10-01 AND 51-30-05.
- [SDR DALA2017032402390](https://openairdocs.org/sdr/DALA2017032402390), Mar 23, 2017: STRUCTURE. CORRODED. CORROSION ON BARREL NUT HOLES NR 10, 12, AND 13 LEFT SIDE, XH=7 HORIZONTAL STABILIZER. COMPLIED WITH ERA 556327-14.
- [SDR DALA2017032302389](https://openairdocs.org/sdr/DALA2017032302389), Mar 22, 2017: FRAME. CRACKED. CRACKED FRAME ANGLE, BS 1508 BETWEEN LONGERON 4R - 4L AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-30-02 AND DWG 9911860.
- [SDR DALA2017032302388](https://openairdocs.org/sdr/DALA2017032302388), Mar 22, 2017: FRAME. CRACKED. CRACKED FRAME BS 1508. REPLACED IAW SRM 51-10-05 AND DWG 9911860-3.
- [SDR DALA2017032202387](https://openairdocs.org/sdr/DALA2017032202387), Mar 22, 2017: DOUBLER. CORRODED. CORROSION ON PRODUCTION DOUBLER AT AFT PRESSURE BULKHEAD BETWEEN LONBERONS 28L AND 28R, BS 1395. REPLACED IAW SRM 51-10-03 AND 51-30-05.
- [SDR DALA2017032002215](https://openairdocs.org/sdr/DALA2017032002215), Mar 19, 2017: CUSP WEB. CORRODED. CORROSION ON RIGHT CUSP WEB BETWEEN BS 1212 AND 1269, RBL 54 AND 60. REPAIRED IAW SRM 53-20-02, 51-30-01, 51-30-02, AND 51-30-05.
- [SDR DALA2017032002214](https://openairdocs.org/sdr/DALA2017032002214), Mar 19, 2017: WEB. CRACKED. CRACK ON WEB AFT FACE, BS 1520 AT THE 10 O'CLOCK POSITION. REPLACED WEB AND STIFFENERS IAW SRM 53-10-04 AND 51-30-05.
- [SDR DALA2017032002213](https://openairdocs.org/sdr/DALA2017032002213), Mar 19, 2017: FRAME. CRACKED. CRACK ON FRAME BS 1443.. REPAIRED IAW SRM 53-10-02. (LP# 2937224)
- [SDR DALA2017032102386](https://openairdocs.org/sdr/DALA2017032102386), Mar 18, 2017: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM, BS 1364, RBL 16 TO LBL 16. FOUND TO BE OUT OF LIMITS. REPLACED SUPPORT IAW SRM 53-10-03, 51-30-05, AND 51-10-03.
- [SDR DALA2017032102385](https://openairdocs.org/sdr/DALA2017032102385), Mar 18, 2017: FLOOR SUPPORT. CORRODED. CORRODED FLOOR SUPPORT BS 1364 - 1404 RBL 18. REPLACED IAW SRM 51-30-01 AND DWG 9936656.
- [SDR DALA2017032102275](https://openairdocs.org/sdr/DALA2017032102275), Mar 18, 2017: LONGERON. CRACKED. AFT ACCESSORY COMPARTMENT CRACK ON LONGERON 12 L STA 1494. REPAIRED IAW SRM 53-10-01.
- [SDR DALA2017031702153](https://openairdocs.org/sdr/DALA2017031702153), Mar 17, 2017: CUSP WEB. CORRODED. CORROSION ON CUSP WEB, BS 1227-1238, RBL 54 TO 60. REMOVED AND INSTALLED IAW SRM 53-20-02 AND 51-30-01.
- [SDR DALA2017031602150](https://openairdocs.org/sdr/DALA2017031602150), Mar 15, 2017: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL, BS 984, RBL 44, Z=-6. REPAIRED IAW SRM 51-70-01.
- [SDR DALA2017031502146](https://openairdocs.org/sdr/DALA2017031502146), Mar 14, 2017: WEB. CORRODED. CORROSION ON DIAPHRAGM FROM BS 180-200, RBL 9 TO 44 AND LBL 9 TO 44. REPAIRED IAW SRM 51-11-01.
- [SDR DALA2017031502142](https://openairdocs.org/sdr/DALA2017031502142), Mar 14, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BS 160 - 196, LBL 54. REPLACED IAW SRM 51-30-01 AND 51-30-05.
- [SDR DALA2017031502136](https://openairdocs.org/sdr/DALA2017031502136), Mar 14, 2017: CUSP WEB. CORRODED. CORRODED ON RIGHT CUSP WEB, BS 386 - 430 AND 589, RBL 54 - 60. REPAIRED IAW SRM 53-20-02.
- [SDR DALA2017031502135](https://openairdocs.org/sdr/DALA2017031502135), Mar 14, 2017: CUSP WEB. CORRODED. CORROSION ON CUSP WEB, BS 385-394, RBL 54 - -60. REPAIRED IAW SRM 53-20-02.
- [SDR DALA2017031502134](https://openairdocs.org/sdr/DALA2017031502134), Mar 14, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BS 200 - 256, LBL 16. REPLACED THE FLOOR SUPPORT IAW SRM 53-10-01, 51-10-05, 51-30-02, AND 51-30-05.
- [SDR DALA2017031402132](https://openairdocs.org/sdr/DALA2017031402132), Mar 14, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT BS 200 - 256, LBL 16. FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 53-10-01, 51-10-05, AND 51-30-02.

All 177: https://openairdocs.org/deregistered/N923DN-2022-11-29/reports.md

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