# N958DN: 1997 Mcdonnell Douglas MD-90-30, registration cancelled 2021-03-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 23, 2021 - 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: 53528 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: February 4, 2012 - Certificate issued: March 31, 2011 - Last registry action: November 6, 2019 - Mode S code: AD52B7 - 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/N958DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=958DN - Page: https://openairdocs.org/deregistered/N958DN-2021-03-23 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 (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2017081006138](https://openairdocs.org/sdr/DALA2017081006138), Aug 8, 2017: BATTERY PACK. NOT SEATED. REAR TEAILCONE EMERGENCY EXIT LIGHT CONTINUES TO FLASH OFF & ON. RESEATED THE BATTERY PACK. SYSTEM OPS NORMAL. - [SDR DALA2017053104413](https://openairdocs.org/sdr/DALA2017053104413), May 28, 2017: BATTERY PACK. DISCHARGED. FIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE, ROWS 1 THRU 5. REMOVED AND REPLACED BATTERY PACK AT ROW 4C. OPERATION CHECKS GOOD. - [SDR DALA2016112109252](https://openairdocs.org/sdr/DALA2016112109252), Nov 19, 2016: SUPPORT. DAMAGED. FORWARD CARGO COMPARTMENT AFT BULKHEAD DAMAGED AT STA 522, L29R. REMOVED WALL SUPPORT. INSTALLED NEW SUPPORT IAW SRM 51-30. - [SDR DALA2016100707139](https://openairdocs.org/sdr/DALA2016100707139), Oct 4, 2016: POWER SUPPLY. INOPERATIVE. CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATION CHECKED OK. - [SDR DALA2016080705949](https://openairdocs.org/sdr/DALA2016080705949), Aug 7, 2016: BATTERY PACK. INOPERATIVE. FOUND CATWALK EMERGENCY LIGHTS, LEFT SIDE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT FLIGHT ATTENDANT SEAT. OPS CHECKED GOOD. - [SDR DALA2016080405775](https://openairdocs.org/sdr/DALA2016080405775), Jul 30, 2016: SKIN. CORRODED. CORROSION ON RIGHT SIDE OF FUSELAGE AFT OF C3 DOOR. REPAIRED IAW ERA 549447-14. - [SDR DALA2016080305746](https://openairdocs.org/sdr/DALA2016080305746), Jul 29, 2016: PANEL. DAMAGED. FOUND RIGHT MAIN LANDING GEAR FLAP CLOSEOUT SPRING PANEL DAMAGED. REMOVED AND REPLACED INBOARD BUTE DOOR AND BEAM ASSEMBLY IAW DWG 5936844. - [SDR DALA2016062104887](https://openairdocs.org/sdr/DALA2016062104887), Jun 19, 2016: TRANSDUCER. MALFUNCTIONED. RIGHT INBD ANTISKID FAULT ON LANDING. CREW INFORMED BY TOWER THAT RT INBD TIRE WAS FLAT. MAINTENANCE R & R RT INBD TRANSDUCERS AND NR 3 AND NR 4 TIRES. FORWARD - [SDR DALA2016062004800](https://openairdocs.org/sdr/DALA2016062004800), Jun 17, 2016: TIRE. BLOWN. EXPERIENCED A RT INBD BLOWN TIRE EVENT UPON LANDING. MAINTENANCE REPLACED NR 3 AND NR 4 TIRES. AIRCRAFT OK FOR SERVICE. - [SDR DALA2016062004802](https://openairdocs.org/sdr/DALA2016062004802), Jun 12, 2016: TIRE. BLOWN. EXPERIENCED A BLOWN TIRE EVENT ON LANDING. RT OTBD ANTI-SKID EOAP CAUTION MESSAGE ON LANDING. PERFORMED AACU BITE. AACU FAULTS RT OTBD WHEEL NOT TURNING. REPLAC - [SDR DALA2016050203552](https://openairdocs.org/sdr/DALA2016050203552), Apr 29, 2016: ANTI-SKID SYS. MALFUNCTIONED. ON LANDING, AIRCRAFT DISPLAYED RT OTBD ANTI-SKID AND ANTI-SKID FAULT MESSAGES WITH A SUBSEQUENT BLOWN NR 4 MAIN TIRE ASSEMBLY. MAINTENANCE PERFORMED AN AACU BIT - [SDR DALA2016012600648](https://openairdocs.org/sdr/DALA2016012600648), Jan 25, 2016: FITTING. CORRODED. CORROSION ON INBD FORWARD FITTING FOR NR 2 GALLEY, BS 207. FOUND TO BE OUT OF LIMITS. REPAIRED IAW ERA 543268-14, REV O. - [SDR DALA2016012400647](https://openairdocs.org/sdr/DALA2016012400647), Jan 23, 2016: SEAT TRACK. CORRODED. GALLEY 2 SEAT TRACK CORRODED AT BS 200 -- 236, RBL 24. FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 53-40-01. - [SDR DALA2015091805717](https://openairdocs.org/sdr/DALA2015091805717), Sep 17, 2015: INTERCOSTAL. CRACKED. INTERCOSTAL ATTACH WEB CRACKED AT LT VENTRAL STAIR STIFFENER. REMOVED, FABRICATED AND INSTALLED REPAIR PARTS IAW ERA 539471-14. - [SDR DALA2015062203895](https://openairdocs.org/sdr/DALA2015062203895), Jun 22, 2015: CATWALK. MALFUNCTIONED. VENTRAL STAIR CATWALK WILL NOT STOW IN THE UP POSITION. R & R CLEVIS TO VENTRAL STAIR CATWALK IAW MM. OPS CHECKS OK. - [SDR DALA2015032602403](https://openairdocs.org/sdr/DALA2015032602403), Mar 24, 2015: DISPLAY. ODOR. F/O PFD DISCOLORED AND FLICKERED WITH A FAINT ELECTRICAL ODOR. TURNED OFF AND THE ODOR WENT AWAY. VERIFIED ODOR IN REMOVED PFD. R & R PFD IAW AMM. OPS CHECKS NO - [SDR DALA2014102905828](https://openairdocs.org/sdr/DALA2014102905828), Oct 28, 2014: SKIN. DAMAGED. FUSELAGE SKIN REPAIR AT STA 1212, BETWEEN L24R AND L25R DAMAGED. REPAIRED IAW ERA 530255-14, SECTION I. - [SDR DALA14028409258](https://openairdocs.org/sdr/DALA14028409258), Apr 30, 2014: CONTROLLER. MALFUNCTIONED. RED CABIN ALT ANNUNCIATOR ACCOMPANIED BY AURAL WARNING AT FL280 WITH NO WARNING CABIN AT ALT FL100. INITIATED DESCENT. FOLLOWED QRH AND CABIN ALT NEVER EXCEEDED - [SDR DALA14004299258](https://openairdocs.org/sdr/DALA14004299258), Jan 15, 2014: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT BS 1475, 3 INCHES RT OF VERTICAL STABILIZER/TAIL. CUTOUT DAMAGE, INSTALLED DOUBLER, TRIPLER AND LONGERON SPLICE IAW PRI 522196, REV O A - [SDR DALA14003199258](https://openairdocs.org/sdr/DALA14003199258), Jan 14, 2014: FRAME. CRACKED. CRACKED WEB AT CANTED FRAME BS 953, LBL 23. REPAIRED. - [SDR DALA13035059258](https://openairdocs.org/sdr/DALA13035059258), Jul 16, 2013: UNKNOWN. ODOR. FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR COMING FROM FORWARD GALLEY. ODOR DISSIPATED WITH ACFT IN SAME CONFIGURATION. NO ODOR EVIDENT. INSPECTED FORWARD GAL - [SDR DALA13035069258](https://openairdocs.org/sdr/DALA13035069258), Jul 9, 2013: LIGHT. OVERHEATED. FLIGHT CREW REPORTED READING LIGHT AT 28A OVERHEATING AND STRONG BURNING PLASTIC ODOR. MX R & R LIGHT ASSY 28A IAW AMM. OPS CHECKS OK. - [SDR DALA13033009258](https://openairdocs.org/sdr/DALA13033009258), Jun 28, 2013: DOUBLER. CRACKED. VERTICAL STABILIZER, LT SIDE RAM AIR INLET ACCESS PANEL INNER DOUBLER CRACKED AT LOWER AFT CORNER. REMOVED INNER DOUBLER AND CRACKED INNER DOUBLER IAW ERA 51633 - [SDR DALA13032999258](https://openairdocs.org/sdr/DALA13032999258), Jun 28, 2013: SKIN. CRACKED. VERTICAL STABILIZER, LT SIDE AT RAM AIR INLET ACCESS PANEL LOWER AFT CORNER SKIN CRACKED. REMOVED CRACKED SKIN ERA 516334-4. DAMAGE CONTAINED. REPAIRS COMPLETED - [SDR DALA13033069258](https://openairdocs.org/sdr/DALA13033069258), Jun 27, 2013: SKIN. CRACKED. REMOVED SECTION OF DORSAL ATTACHMENT SKATE ANGLE LT, BS 1494 FOR ACCESS TO DORSAL SKIN CRACK. REMOVED SECTION OF ANGLE FOR ACCESS. ACCOMPLISHED ERA 516367-14 RE - [SDR DALA13033139258](https://openairdocs.org/sdr/DALA13033139258), Jun 26, 2013: SCOOP. CRACKED. DURING SPECIAL VISIT, ATTEMPTS TO WELD CRACKS IN RAM AIR SCOOP WERE UNSUCCESSFUL, ERA 516402-14 ISSUED. ACCOMPLISHED SECTION I OF ERA 516402-14, REV O. - [SDR DALA13033029258](https://openairdocs.org/sdr/DALA13033029258), Jun 26, 2013: SKATE ANGLE. DAMAGED. RIGHT INBD SKATE ANGLE WAS FOUND DAMAGED DURING DVI OF SURROUNDING STRUCTURE OF DORSAL FIN. REMOVED RIGHT INNER SKATE ANGLE. DRILLED NEW ANGLE. INSTALLED ANGLE - [SDR DALA13032989258](https://openairdocs.org/sdr/DALA13032989258), Jun 23, 2013: STRUCTURE. CRACKED. RAM AIR INLET UPPER AFT EDGE CRACKED. PERFORMED WELD REPAIR IAW SRM 55-30-05. FPI AND HFEC IAW PS 900-6-3, NR 2 AND 06-10-01.001, NO CRACKS. - [SDR DALA13031759258](https://openairdocs.org/sdr/DALA13031759258), Jun 23, 2013: SHEAR TIE. CRACKED. BS 1486, LONGERON 2R CRACKED SHEAR TIE. REMOVED AND INSTALLED SHEAR TIE IAW SRM 51-10. - [SDR DALA13000109258](https://openairdocs.org/sdr/DALA13000109258), Dec 31, 2012: CABLE. LOOSE. DURING SERVICE CHECK, MX FOUND L1 DOOR SLIDE DEPLOY CABLE HANGING LOOSE. R & R SLIDE IAW AMDS CARD DECK 2500-4332. ACFT OK FOR SERVICE. - [SDR DALA1248049258](https://openairdocs.org/sdr/DALA1248049258), Sep 5, 2012: LAMP. WEAK. DURING SERVICE CHECK, MAINTENANCE FOUND AFT LEFT OVERWING EMERGENCY EXIT LIGHTED SIGN OVER DOOR VERY DIM. MAINTENANCE FOUND ONLY THREE BULBS WORKING. REPLACED L - [SDR DALA1243309258](https://openairdocs.org/sdr/DALA1243309258), Jul 25, 2012: POWER SUPPLY. INOPERATIVE. DURING SERVICE CHECK, MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER PACK PER AMM OPERATION CHECKS GOOD. - [SDR DALA1240379258](https://openairdocs.org/sdr/DALA1240379258), Jul 4, 2012: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS REMAIN ILLUMINATED WITH SWITCH TURNED OFF. REMOVED AND REPLACED OVERWING BATTERY PACK PER AMM. - [SDR DALA1202889258](https://openairdocs.org/sdr/DALA1202889258), Jan 22, 2012: FASTENER. UNKNOWN. AS PER EA 02-476701-12AD REV E ME0301 STEP 20 SDR REQUIRED. REPLACED UPPER ROW OF ENGINE AFT MOUNT SUPPORT FITTING FASTENERS (ROW A) INSPECTED ROW B, NO DEFECTS - [SDR DALA1202879258](https://openairdocs.org/sdr/DALA1202879258), Jan 22, 2012: FASTENER. UNKNOWN. AS PER EA 02-476701-12AD ME0101 STEP 20 SDR REQUIRED. REPLACED UPPER ROW OF ENGINE AFT MOUNT SUPPORT FASTENERS (ROW A) INSPECTED ROW B, NO DEFECTS NOTICED. - [SDR DALA1154299258](https://openairdocs.org/sdr/DALA1154299258), Dec 20, 2006: SKIN. DENTED. REPAIR OF DENT ON THE SKIN AT STA 273 OD2010-SR-008 NRC HRB20101206-01-01 BOEING APPROVAL SHY-SHY-10-0084-02B. - [SDR DALA1154289258](https://openairdocs.org/sdr/DALA1154289258), Dec 20, 2006: FITTING. CORRODED. VERTICAL STABILIZER FITTING CORROSION REPAIR OD2006-SR-044 NRC B55-061119-344 BOEING APPROVAL 1-259780511-3. - [SDR DALA1154279258](https://openairdocs.org/sdr/DALA1154279258), Dec 14, 2006: ATTACH ANGLE. DAMAGED. FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE REPAIR OD2006- SR-043 NRC B55-061119-328 BOEING APPROVAL 1-257893345-5. - [SDR DALA1154269258](https://openairdocs.org/sdr/DALA1154269258), Dec 14, 2006: STRUCTURE. DAMAGED. REPAIR OF WING LEADING EDGE WORN DAMAGE OD2006-SR-042 NRC B55-061119-228 BOEING APPROVAL 1-255950271-5. - [SDR DALA1154259258](https://openairdocs.org/sdr/DALA1154259258), Dec 12, 2006: SKIN PANEL. CRACKED. SLAT SKIN PANEL CRACK REPAIR IAW OD2006-SR-041 NRC B55-061119-230 BAC APPROVAL 1-257893301-2. - [SDR DALA1154249258](https://openairdocs.org/sdr/DALA1154249258), Nov 30, 2006: PAN. CORRODED. FWD CARGO DOOR JAMB PAN CORROSION REPAIR IAW SRM 53-05 NRC B55-061119-047 AND BAC APPROVAL 1-253499901-2 - [SDR DALA1154309258](https://openairdocs.org/sdr/DALA1154309258), Nov 22, 2006: DOOR FRAME. CORRODED. MID CARGO DOOR JAMB CORROSION REPAIR NRC 48 SRM 53-05. - [SDR DALA1154319258](https://openairdocs.org/sdr/DALA1154319258), Nov 21, 2006: DOOR FRAME. CORRODED. MID CARGO DOOR JAMB CORROSION NRC 25. --- 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.