# N912DN: 1996 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: 53392
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: April 19, 1996
- Certificate issued: July 26, 1996
- Last registry action: August 31, 2020
- Mode S code: AC9E71
- 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/N912DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=912DN
- Page: https://openairdocs.org/deregistered/N912DN-2022-11-29

From the FAA registry file of November 3, 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 (143, newest 50)

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

- [SDR DALA2019091005266](https://openairdocs.org/sdr/DALA2019091005266), Sep 9, 2019: FLOOR PANEL. DAMAGED. WHILE WORKING NEF 1255035 FOUND FWD GALLEY FLOOR PANELS CORRODED AND DAMAGED. REPLACED DAMAGED FLOOR PANEL PER AMM 53-21. REPLACED CORRODED FASTENERS WITH NEW H
- [SDR DALA2019070904118](https://openairdocs.org/sdr/DALA2019070904118), Jul 6, 2019: SLIDE. LOOSE. AT DEPARTURE 1R DOOR SLIDE PACK CAME LOOSE. RE-INSTALLED SLIDE PACK AND GIRT BAR PIN. OK FOR SERVICE. (LP# 5619230)
- [SDR DALA2019042902695](https://openairdocs.org/sdr/DALA2019042902695), Apr 26, 2019: LONGERON. CRACKED. LONGERON CRACKED AT STATION 1486 RT SIDE 12R. C/W PERMANENT REPAIR PER ERA 577544-14 REV A SECTION I PERMANENT REPAIR INSTRUCTIONS PRI C/W THROUGH NON ROUTINE O
- [SDR DALA2019042322583](https://openairdocs.org/sdr/DALA2019042322583), Apr 22, 2019: CONTROLLER. ODOR. FROM THE CAPT SIDE THERE IS FAINT HOT ELECTRICAL SMELL. APPEARS TO COME FROM UNDER THE CAPT GLAIRSHIELD. LT PACK TEMP CTRL VLVE WOULD DRIVE HOT WITH DUCT TEMP15
- [SDR DALA2018060403791](https://openairdocs.org/sdr/DALA2018060403791), Jun 2, 2018: LIGHT. INOPERATIVE. LEFT OVER WING EMERGENCY EVACUATION LIGHT INOP. R&R LEFT AND RIGHT EXTERIOR EMERGENCY LIGHT ASSEMBLIES PER AMM 33-51. R&R POWER SUPPLY B5-125 PER AMM 33-51. ALL
- [SDR DALA2018033102084](https://openairdocs.org/sdr/DALA2018033102084), Mar 30, 2018: ACCESS PANEL. DAMAGED. ELONGATE HOLES ON ACCESS PANEL 370TL ON THE VERTICAL STABILIZER. THE ACCESS PANEL WAS REPAIRED IAW ER/A 567293-14, REV ORIGINAL, AND ETI-90-18-022, REV 1.
- [SDR DALA2018032401861](https://openairdocs.org/sdr/DALA2018032401861), Mar 23, 2018: ANGLE. CRACKED. CRACKED RT ANGLE TO ATTACH VERTICAL STABILIZER P/N 5912188-50 IN REF 5530-01034-0102. REPLACED PER SRM VOL I 51-30-02 AND 51-30-05.
- [SDR DALA2018032301847](https://openairdocs.org/sdr/DALA2018032301847), Mar 22, 2018: FLOOR PANEL. NOT REPORTED. PERFORM PERMANET REPAIR PER ER/A 560348-14 REV ORIG FLOOR PANELS NBRS 221KF AND 221LF WERE FABRICATED, REPLACED AND IDENTIFIED PER VOL 1 SRM 53-20-03 PAR 5 AND 
- [SDR DALA2018031901802](https://openairdocs.org/sdr/DALA2018031901802), Mar 18, 2018: SUPPORT. CORRODED. AFTER REMOVE FLOOR PANELS IN REF LOG 3112788. CORROSION WAS FOUND ON AFT EVACUATION SLIDE LATCH SUPPORT X=-53 FROM STA Y=180 TO 200 AT FWD WET AREA. SLIDE LATCH
- [SDR DALA2017083106514](https://openairdocs.org/sdr/DALA2017083106514), Aug 31, 2017: POWER SUPPLY. DISCONNECTED. DURING A SERVICE CHECK, FOUND THE COCKPIT EMERGENCY LIGHT & AFT FACING EXIT SIGN OVER L1 JUMPSEAT INOPERATIVE. FOUND POWER SUPPLY B5-234 DISCONNECTED. CONNECTED
- [SDR DALA2017062705138](https://openairdocs.org/sdr/DALA2017062705138), Jun 26, 2017: RELEASE MECH. OUT OF ADJUST. OUT OF CLEARANCE , CLAMPS FOR LOCKING CABLES DURING PULL TEST. ADJUSTED EMERGENCY RELEASE MECHANISM FOR TAILCONE.
- [SDR DALA2016112109257](https://openairdocs.org/sdr/DALA2016112109257), Nov 20, 2016: WEB. CRACKED. AFT SIDE OF WEB, STA 1520 PULLEY CUT OUT CRACKED. REPAIRED IAW ERA 552963-14, REV O.
- [SDR DALA2016112109256](https://openairdocs.org/sdr/DALA2016112109256), Nov 19, 2016: ANGLE. CRACKED. RIGHT HAND SIDE AFT LOUVER , STA 1520, L10R CRACKED. REPLACED ANGLE IAW DWG 9911839.
- [SDR DALA2016050503781](https://openairdocs.org/sdr/DALA2016050503781), May 5, 2016: SKIN. CRACKED. EMPENNAGE FUSELAGE SKIN IS CRACKED IN 3 AREAS BETWEEN, BS 1494, S2 LT-S4 LT. REPAIRED IAW ERA 546459-14, REV O.
- [SDR DALA2016050503780](https://openairdocs.org/sdr/DALA2016050503780), May 4, 2016: JACKSCREW. WORN. HORIZONTAL STABILIZER JACKSCREW THREADS WORN AT CENTER AREA. REMOVED AND INSTALLED JACKSCREW IAW AMDS 27-41-4591.
- [SDR DALA2014121006513](https://openairdocs.org/sdr/DALA2014121006513), Dec 7, 2014: DOOR FRAME. GOUGED. GOUGE ON FORWARD LOWER FRAME OF CARGO BIN DOOR. ACCOMPLISHED PRI 531222-14, REV 1.
- [SDR DALA14025849212](https://openairdocs.org/sdr/DALA14025849212), Apr 21, 2014: SUPPORT ANGLE. BROKEN. AFT VENTRAL STAIRS HAS A STEP SUPPORT ANGLE THAT IS BROKEN AND A NUT STRIP ANGLE THAT IS DAMAGED, LT SIDE OF STEP. CUT OUT DAMAGE SECTION. FABRICATED AND INSTAL
- [SDR DALA14025869212](https://openairdocs.org/sdr/DALA14025869212), Apr 19, 2014: WEB. CORRODED. AFT CARGO BAY BS 1390, SUPPORT WEB HAS CORROSION ON FORWARD AND AFT FACE. CUTOUT DAMAGED WEBS. FABRICATED AND INSTALLED REPAIR SPLICES IAW ERA 523972-14, REV O.
- [SDR DALA14025299212](https://openairdocs.org/sdr/DALA14025299212), Apr 19, 2014: LONGERON. CORRODED. AFT CARGO, UNDER WASTE WATER TANK, BS 1344-1364, LONGERON 27R, CORRODED. CUT OUT DAMAGE. FABRICATED AND INSTALLED SPLICE IAW SRM 51-30-05 AND 51-30-02.
- [SDR DALA14025289212](https://openairdocs.org/sdr/DALA14025289212), Apr 18, 2014: FRAME. CORRODED. AFT CARGO BILGE AREA, BS 1379 LONGERON 30, CORROSION ON FRAME, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLLED FORMER SECTION IAW SRM 53-10-02.
- [SDR DALA14025279212](https://openairdocs.org/sdr/DALA14025279212), Apr 17, 2014: LONGERON. CORRODED. AFT CARGO BAY LONGERON 30 CORRODED BS 1324-1355. FOUND CORROSION TO BE OUT OF LIMITS. FABRICATED AND INSTALLED LONGERON AND SPLICE IAW SRM 53-10-01 AND DWG 5936
- [SDR DALA14025269212](https://openairdocs.org/sdr/DALA14025269212), Apr 17, 2014: FRAME. CORRODED. AFT CARGO BAY FRAME CORRODED AT BS 1231, BETWEEN LONGERON 29 AND 30R. FOUND TO BE OUT OF LIMITS AFTER REWORK. FABRICATED AND INSTALLED FRAME AND SPLICE REPAIR I
- [SDR DALA14025859212](https://openairdocs.org/sdr/DALA14025859212), Apr 16, 2014: ANGLE. CRACKED. EMPENNAGE TOP RT ANGLE VERTICAL SKIN HAS CRACK BETWEEN 2 EA RIVETS JUST TOP SIDE OF RT AC GRILL. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ANGLE AND 
- [SDR DALA14025259212](https://openairdocs.org/sdr/DALA14025259212), Apr 16, 2014: FRAME. MISREPAIRED. REPAIR AT FRAME BS 1344, LONGERON 29L TO 29R NOT INSTALLED IAW SRM REFERENCE. REMOVED, FABRICATED AND INSTALLED NEW ANGLES IAW SRM 53-10-02, FIG 2.
- [SDR DALA14025249212](https://openairdocs.org/sdr/DALA14025249212), Apr 16, 2014: DOUBLER. CORRODED. AFT PRESSURE BULKHEAD DOUBLER CORRODED, BS 1395, LONGERON 29R-29L, REMOVED DAMAGE. LOCATED, DRILLED AND INSTALLED NEW DOUBLER IAW SRM 51-30-05 AND DWG 9915561.
- [SDR DALA14025239212](https://openairdocs.org/sdr/DALA14025239212), Apr 16, 2014: DOOR FRAME. DAMAGED. MID CARGO BAY CUTOUT LOWER PLATE HAS NUMEROUS LOCATIONS OF CORROSION, GOUGES AND TOOL DAMAGE. REMOVED DAMAGED MID CARGO DOOR JAMB BEAM, LOCATED, DRILLED AND INS
- [SDR DALA14022819212](https://openairdocs.org/sdr/DALA14022819212), Apr 12, 2014: FRAME. CORRODED. AFT CARGO BILGE AREA, BS 164, LONGERONS 26-27R FRAME CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FRAME SECTION IAW SRM 53-2
- [SDR DALA14021939212](https://openairdocs.org/sdr/DALA14021939212), Apr 9, 2014: FLOORBEAM. CORRODED. FLOORBEAM BS 200 RBL 5-LBL 5 CORRODED. REMOVED CORROSION IAW SRM 51-30-02, VOL 2, AND FOUND OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I. REMOVED AND REPLACED FLOO
- [SDR DALA14021929212](https://openairdocs.org/sdr/DALA14021929212), Apr 9, 2014: FLOORBEAM. CORRODED. FLOORBEAM CORRODED BS 180, RBL 12-44, REMOVED CORROSION AND FOUND OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-30-02, SR
- [SDR DALA14021919212](https://openairdocs.org/sdr/DALA14021919212), Apr 9, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BS 160 LBL 12. FOUND OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02, VOL 2, DWG 9936534, 
- [SDR DALA14021909212](https://openairdocs.org/sdr/DALA14021909212), Apr 9, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BS 160 BL 0. FOUND OUT LIMITS IAW SRM 53-00-01, FIG 3, VOL I, REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02, DWG 9936534, SRM 51-10
- [SDR DALA14022849212](https://openairdocs.org/sdr/DALA14022849212), Apr 9, 2014: FRAME. CORRODED. CORROSION ON FRAME BS 1344, LONGERON 29L-27R. BOTH SIDES OF FRAME, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FORMER SECTION IAW 53-10-02, FIG 2.
- [SDR DALA14022809212](https://openairdocs.org/sdr/DALA14022809212), Apr 9, 2014: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT MAIN CABIN, BS 180 XCW 35 LT. REMOVED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-30-02.
- [SDR DALA14021899212](https://openairdocs.org/sdr/DALA14021899212), Apr 8, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT AT L-1 DOOR, BS 160-200, LBL 58 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-02, VOL 2, DWG 9936534, SRM 51-10-03, AMM 51-10-00, 
- [SDR DALA14021889212](https://openairdocs.org/sdr/DALA14021889212), Apr 8, 2014: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED AT SEVERAL AREAS BETWEEN BS 160-200, LBL 56. REMOVED CORROSION IAW SRM 51-10-03, VOL 2. FOUND TO BE OUT LIMITS IAW SRM 53-00-01, FIG 3, V
- [SDR DALA14021639212](https://openairdocs.org/sdr/DALA14021639212), Apr 7, 2014: LONGERON FITTING. CORRODED. AFT CARGO BAY BS 1395, L29R END FITTING CORRODED. R & R LONGERON END FITTING IAW SRM 51-30-05, FIG 1.
- [SDR DALA14021629212](https://openairdocs.org/sdr/DALA14021629212), Apr 7, 2014: LONGERON FITTING. CORRODED. AFT CARGO BAY BS 1395, L29L END FITTING CORRODED. R & R IAW SRM 51-30-05, FIG 12.
- [SDR DALA14020659212](https://openairdocs.org/sdr/DALA14020659212), Apr 3, 2014: SHEAR PLATE. CORRODED. BILGE AREA IN AFT CARGO BAY BS 1269-1276 BETWEEN L29-30R CORROSION ON SHEAR TIE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE IAW SRM 51-30
- [SDR DALA14020679212](https://openairdocs.org/sdr/DALA14020679212), Mar 31, 2014: SHEAR TIE. CORRODED. AFT CARGO BAY BS 1307, BETWEEN L27-28R HAD CORROSION ON SHEAR TIE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SHEAR TIE AND STRA
- [SDR DALA14020669212](https://openairdocs.org/sdr/DALA14020669212), Mar 31, 2014: SHEAR TIE. CORRODED. AFT CARGO BAY BILGE AREA, BS 1328, BETWEEN L28 -29R SHEAR TIE CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SECTION OF SHEAR TIE IAW DWG 9919605 AND SRM 53-10
- [SDR DALA14020649212](https://openairdocs.org/sdr/DALA14020649212), Mar 31, 2014: SEAT TRACK. CORRODED. CABIN SEAT TRACK HAD SEVERAL AREAS WITH CORROSION AT RBL 46 BETWEEN BS 200-579. FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-40-01, 51-10-03 AND 51-10
- [SDR DALA14020619212](https://openairdocs.org/sdr/DALA14020619212), Mar 31, 2014: FRAME. CORRODED. AFT CARGO BAY, CORROSION ON FRAME BS 1250, BETWEEN L29-30L. FOUND OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW FRAME IAW SRM 53-10-02, 51-30-01 AND 51-1
- [SDR DALA14020579212](https://openairdocs.org/sdr/DALA14020579212), Mar 31, 2014: SEAT TRACK. CORRODED. CABIN FLOOR SEAT TRACK, LBL 56 FROM BS 902-983 HAS AREAS OF CORROSION, BARE METAL AND WORN. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALL
- [SDR DALA14020589212](https://openairdocs.org/sdr/DALA14020589212), Mar 28, 2014: STRUCTURE. CORRODED. UPPER FUSELAGE AT MAIN PASSENGER CABIN, RIGHT SIDE FUEL CENTER TANK CORRODED AT BS 954, RBL 55-46. REMOVED CORROSION, TREATED, PRIMED AND FILLED VOIDS IAW ERA 5
- [SDR DALA14020049212](https://openairdocs.org/sdr/DALA14020049212), Mar 28, 2014: STRUCTURE. CRACKED. CRACK FOUND JUST AFT L1 DOOR, BS 210, L15L ON DOOR SURROUNDING STRUCTURE. CUTOUT DAMAGE. FABRICATED AND INSTALLED FILLER AND STRAP IAW SRM 51-30-02 ADN 53-60-02
- [SDR DALA14024889212](https://openairdocs.org/sdr/DALA14024889212), Mar 26, 2014: FRAME. CORRODED. FRAME BS 168 BETWEEN LONGERONS 17-19R, HAS CORROSION. REMOVED CORROSION. FABRICATED AND INSTALLED NEW FRAME STRAP IAW ERA 523963-14, REV O AND DWG 3921387.
- [SDR DALA14019659212](https://openairdocs.org/sdr/DALA14019659212), Mar 26, 2014: SEAT TRACK. DAMAGED. CABIN SEAT TRACK, LBL 46, BETWEEN BS 200-488, AREAS CORRODED, SCRATCHED AND BARE METAL. FOUND OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK, SPLICE AND
- [SDR DALA14019649212](https://openairdocs.org/sdr/DALA14019649212), Mar 26, 2014: SEAT TRACK. DAMAGED. CABIN SEAT TRACK LBL 56, FROM BS 218 - 430, SEVERAL AREAS CORRODED, BARE METAL AND WORN. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED 
- [SDR DALA14019629212](https://openairdocs.org/sdr/DALA14019629212), Mar 26, 2014: CUSP WEB. CORRODED. CUSP WEB CORRODED AT LT AREA BETWEEN BS 840-864. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-20-02.
- [SDR DALA14019669212](https://openairdocs.org/sdr/DALA14019669212), Mar 25, 2014: SEAT TRACK. DAMAGED. CABIN SEAT TRACK, LBL 46, BS 1258 - 1363 CORRODED, SCRATCHED AND HAS BARE METAL IN SEVERAL AREAS. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW SEAT T

All 143: https://openairdocs.org/deregistered/N912DN-2022-11-29/reports.md

## FAA accident and incident reports (1)

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 20061126025289I](https://openairdocs.org/incident/20061126025289I), Nov 26, 2006: Doug MD9030 (N912DN), Nashville, TN. (-23) On November 26, 2006, delta flight 1523, a/c N912DN, MD-90, departed bna for slc. At FL 135 the flight crew reported a loss of all electrical power…

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