# N913DN: 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: 53393 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: October 12, 1996 - Certificate issued: January 17, 1997 - Last registry action: June 9, 2022 - Mode S code: ACA228 - 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/N913DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=913DN - Page: https://openairdocs.org/deregistered/N913DN-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 (154, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2020021301108](https://openairdocs.org/sdr/DALA2020021301108), Feb 12, 2020: HYDRAULIC SYSTEM. LEAKING. UPON LANDING RIGHT HYDRAULIC QUANTITY RAPIDLY DROPPED TO 4 QTS. F/A NOTIFIED US DURING TAXI A SMELL OF HYDRAULIC FLUID BURNING C/A VERIFIED LEAK FROM TAIL DRAIN - [SDR DALA2019103106309](https://openairdocs.org/sdr/DALA2019103106309), Oct 29, 2019: UNKNOWN. ODOR. ON DESCENT, PASSING THROUGH 15000; NOTED A BURNING OIL ODOR IN COCKPIT. IT CAME ON SUDDENLY AND IT WAS STRONG ENOUGH TO CONSIDER PUTTING ON OUR O2 MASKS. IT THE - [SDR DALA2019102906229](https://openairdocs.org/sdr/DALA2019102906229), Oct 25, 2019: DOOR FRAME. CRACKED. SHIP 9213 RIGHT WHEEL WELL FWD DOOR JAMB CRACKED. REMOVED AND REPLACED RT FWD WHEEL WELL FRAME PER BOEING DWG 5930584 (6612127) - [SDR DALA2019020540755](https://openairdocs.org/sdr/DALA2019020540755), Jan 17, 2019: DOOR. MISSING. LEFT WING #7 LEADING EDGE SLAT TRACK CUTOUT DOOR MISSING. DEFERRED AS PER MD90 CDL 57-30-01 CDL/PLACARD INSTALLED DISPATCH APPROVED. (LP# 3788178) - [SDR DALA2018101005960](https://openairdocs.org/sdr/DALA2018101005960), Oct 10, 2018: BATTERY PACK. DISCHARGED. EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK B5-232 IAW AMM 33-51-03 OPS CK GOOD. (LP#4253574) - [SDR DALA2018081305048](https://openairdocs.org/sdr/DALA2018081305048), Aug 11, 2018: WEB. DAMAGED. STEERING ACTUATOR MADE CONTACT WITH LEFT NOSE GEAR SUPPORT WEB. REMOVED DAMAGE ON NLG SUPPORT WEB IAW SRM 53-90-01. PERFORMED DVI OF REPAIR AREA PER MD-90 SRM 5 - [SDR DALA2018061203968](https://openairdocs.org/sdr/DALA2018061203968), Jun 7, 2018: CABLE. BURNED. DURING INSPECTION OF BATTERY CABLE CONNECTORS, BURNED BATTERY CABLE TERMINAL AND BURNED CONNECTOR WERE FOUND IAW AMDS 4944-4001, STEP 2. THE CONNECTOR ASSEMBLY - [SDR DALA2018060873893](https://openairdocs.org/sdr/DALA2018060873893), Jun 6, 2018: SKIN. CRACKED. CRACK FOUND IN THE VERTICAL STABILIZER SKIN NEAR THE RAM AIR INLET AREA, LT SIDE, ZFS 9. THE SKIN WAS REPAIRED IAW ERA 569140-14, REV ORIGINAL, AND ETI-90-18-02 - [SDR DALA2018060603846](https://openairdocs.org/sdr/DALA2018060603846), Jun 5, 2018: ATTACH ANGLE. CRACKED. CRACK IN THE LT & RT INTERNAL VERTICAL STABILIZER ATTACH ANGLES BS 1458 TO 1486. REPLACED THE ATTACH ANGLES IAW SRM 51-30-02, VOL II, AND 51-30-05. - [SDR DALA2018060603845](https://openairdocs.org/sdr/DALA2018060603845), Jun 5, 2018: FORMER. CRACKED. A CRACK WAS FOUND ON THE VERTICAL STABILIZER FORMER AT ZFS 26.812. REPLACED THE FORMER IAW SRM 51-30-02, VOL. II, AND 51-30-05. - [SDR DALA2018060603844](https://openairdocs.org/sdr/DALA2018060603844), Jun 5, 2018: SKIN. DAMAGED. DAMAGE FOUND ON THE FUSELAGE SKIN, BETWEEN BS 465 - 522. PERFORMED A PERMANENT REPAIR IAW ERA 569135-14, REV ORIGINAL, AND ETI-90-17-023, REV 4. - [SDR DALA2018060303790](https://openairdocs.org/sdr/DALA2018060303790), Jun 2, 2018: SKIN. CRACKED. CRACK ON FUSELAGE SKIN AROUND AFT HINGE OF LT/AFT NLG DOOR. FUSELAGE SKIN AROUND AFT HINGE OF LT NLG DOOR WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-30-01 VOLUM - [SDR DALA2018052903625](https://openairdocs.org/sdr/DALA2018052903625), May 28, 2018: SKIN. DAMAGED. CORROSION ON PRODUCTION DOUBLER CUT-OUT ON DRAIN BS 1328-1344 BETWEEN LONGERONS 26 - 27R. REPLACED IAW DWG:5936667, REV CD, AND SRM 51-30-02, VOL II. - [SDR DALA2018041802594](https://openairdocs.org/sdr/DALA2018041802594), Apr 17, 2018: SLIDE. DAMAGED. AFT TAILCONE SLIDE WAS FOUND TO BE UNWRAPPING. REMOVED AND INSTALLED SLIDE IAW 2561-4643. - [SDR DALA2017041903229](https://openairdocs.org/sdr/DALA2017041903229), Apr 18, 2017: STRUCTURE. NOT REPORTED. MAJOR REPAIR, R1 DOOR FINAL DRAWING REPAIR. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-20-02. - [SDR DALA2017040402832](https://openairdocs.org/sdr/DALA2017040402832), Apr 3, 2017: LIGHT. BROKEN. TAIL COMPARTMENT EMERGENCY LIGHT LENS AND BASE BROKEN. INSTALLED A NEW LIGHT. OPERATION CHECKED GOOD. - [SDR DALA2016080505808](https://openairdocs.org/sdr/DALA2016080505808), Jul 28, 2016: WINDSHIELD. ARCED. ARCING OBSERVED ON CAPTAINS FORWARD WINDSHIELD. CIRCUIT BREAKER X24 PULLED PER QRH. CRACKS NOTED. REMOVED AND REPLACED WINDOW IAW MM. OPS CHECKED OK. - [SDR DALA2016062004884](https://openairdocs.org/sdr/DALA2016062004884), Jun 14, 2016: CABLE. MISSING. TAILCONE NITROGEN CYLINDER PULL CABLE MISSING. REPLACED CABLE IAW MM. AIRCRAFT OK FOR SERVICE. - [SDR DALA2016061104637](https://openairdocs.org/sdr/DALA2016061104637), Jun 10, 2016: FRAME. CRACKED. CRACKED UPPER CAP OF FRAME, BS 1520 CANT AT 11 O'CLOCK POSITION ON AFT ACCESSORY COMPARTMENT. REPAIRED IAW ERA 546490-14, REV O AND ETI 90-16-018, REV 4. - [SDR DALA2016061104636](https://openairdocs.org/sdr/DALA2016061104636), Jun 10, 2016: FRAME. CRACKED. SEVERAL CRACKS ON FRAME BS 1520 CANT BETWEEN LONGERON 1-11L, AFT ACCESSORY COMPARTMENT. REPLACED IAW SRM 51-30-02 AND 51-30-0. CRACK 11" IN LENGTH. - [SDR DALA2016061104635](https://openairdocs.org/sdr/DALA2016061104635), Jun 10, 2016: SPAR. CRACKED. CRACK WAS FOUND ON RT HORIZONTAL STABILIZER, REAR SPAR, AFT BARREL NUT HOLE. REPLACED IAW SRM 51-30-02 AND 51-30-05 AND DWG 90550002, REV B. - [SDR DALA2016061104634](https://openairdocs.org/sdr/DALA2016061104634), Jun 10, 2016: HOUSING. WORN. WEAR ON MID CARGO COMPARTMENT DOOR HANDLE HOUSING. REPLACED IAW SRM 51-10-03. - [SDR DALA2016061004609](https://openairdocs.org/sdr/DALA2016061004609), Jun 9, 2016: STIFFENER. CRACKED. SEVERAL STIFFENERS CRACKED AT FRAME 1520 CANT AFT ACCESSORY COMPARTMENT. REPLACED FRAME IAW SRM 51-30-02 AND DWG 9953015. - [SDR DALA2016061004608](https://openairdocs.org/sdr/DALA2016061004608), Jun 9, 2016: SPAR CAP. DAMAGED. BORE ON CAP, BS X= 5.93 AND X= 13.21 HORIZONTAL STABILIZER OUT OF TOLERANCE. REPAIRED IAW ERA 546508-14AD, REV O. - [SDR DALA2016061004633](https://openairdocs.org/sdr/DALA2016061004633), Jun 9, 2016: FRAME SPLICE. DAMAGED. DAMAGED SPLICE ON FRAME, BS 1520. FABRICATED AND INSTALLED NEW SPLICE IAW DWG 9953015. - [SDR DALA2016061004632](https://openairdocs.org/sdr/DALA2016061004632), Jun 9, 2016: FRAME. CRACKED. CRACKED WEB FRAME, BS 1520 CANT. CANT WAS REPLACED IAW SRM 51-30-02, DWG 9953015 AND 51-30-05. - [SDR DALA2016060904607](https://openairdocs.org/sdr/DALA2016060904607), Jun 8, 2016: ATTACH FITTING. CORRODED. HORIZONTAL STABILIZER HARDWARE ATTACH POINTS CORRODED. REPLACED IAW AMM 55-10-00. - [SDR DALA2016060904606](https://openairdocs.org/sdr/DALA2016060904606), Jun 8, 2016: SKIN. DAMAGED. LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 206 BETWEEN LONGERON 1R AND 2R. REPAIRED IAW SRM 53-31-02, 51-30-03 AND 51-10-05. - [SDR DALA2016060604490](https://openairdocs.org/sdr/DALA2016060604490), Jun 5, 2016: SKIN. CRACKED. CRACK ON FUSELAGE SKIN , BS 1542 CANT BETWEEN LONGERONS 3 TO 5L. REPAIRED IAW SRM 53-00-01. - [SDR DALA2016060404489](https://openairdocs.org/sdr/DALA2016060404489), Jun 3, 2016: INTERCOSTAL. WORN. WORN INTERCOSTALS MID CARGO COMPARTMENT, BETWEEN BERM 1 AND 2. REPLACED IAW SRM 51-30-05, 51-10-01, 51-10-02, AND DWG 9957664, REV N. - [SDR DALA2016053104292](https://openairdocs.org/sdr/DALA2016053104292), May 29, 2016: DOUBLER. WORN. WEAR ON REPAIR DOUBLER OF GUST LOCK CUTOUT AT L1 DOOR. DOUBLER WAS REPLACED IAW ERA 413167-14, REV O. - [SDR DALA2016052804290](https://openairdocs.org/sdr/DALA2016052804290), May 27, 2016: SKIN. DENTED. EXCESSIVE DENTS ON EXTERNAL SKIN BETWEEN BEAMS 4 AND 5 AT FORWARD CARGO COMPARTMENT. REPAIRED IAW SRM 53-31-02. - [SDR DALA2016052804289](https://openairdocs.org/sdr/DALA2016052804289), May 26, 2016: INTERCOSTAL. CRACKED. CRACK ON INTERCOSTAL ON FORWARD DOOR JAMB AT LT MLG WHEEL WELL AREA, JUST BELOW HYDRAULIC GROUND SERVICE. REPAIRED IAW SRM 51-30-02 AND 51-30-005 AND DWG 593058 - [SDR DALA2016052704288](https://openairdocs.org/sdr/DALA2016052704288), May 26, 2016: HINGE. SCRATCHED. SCRATCHES ON RT ELEVATOR ATTACH POINT BUSHING HINGE, NR 2, 3, 4 AND 5. REPLACED IAW MM AND PS 900-1-2-1. - [SDR DALA2016052604286](https://openairdocs.org/sdr/DALA2016052604286), May 25, 2016: ANGLE. WORN. WEAR ON ANGLE CLIP ON RT FORWARD OVERWING, EMERGENCY EXIT DOOR JAMB, BS 902. R & R IAW SRM 51-30-08. - [SDR DALA2016031401932](https://openairdocs.org/sdr/DALA2016031401932), Mar 11, 2016: BRAKE. FIRE. AFTER LANDING THE NR 3 MLG BRAKE WAS SHOWING HOT. MLG NR 1, LOW BRAKE 250 DEGREES. NR 2, LT BRAKE 270, NR 3, RT BRAKE 510 DEGREES. NR 4, RO BRAKE 360 DEGREES. U - [SDR DALA2015111707003](https://openairdocs.org/sdr/DALA2015111707003), Nov 16, 2015: PUMP. ODOR. AT ARRIVAL TO GATE, REPORT OF STRONG CHEMICAL BURNING ODOR. MAINTENANCE CONFIRMED ELECTRICAL ODOR IN FORWARD HALF OF CABIN. R & R RELAYS R2-528 AND R2-529 DUE T - [SDR DALA2015020400913](https://openairdocs.org/sdr/DALA2015020400913), Feb 1, 2015: LAMP. INOPERATIVE. MID CABIN CEILING EMERGENCY EXIT SIGN IS INOPERATIVE. REPLACED THE LAMPS. OPS CHECKED GOOD. - [SDR DALA14032429213](https://openairdocs.org/sdr/DALA14032429213), May 25, 2014: RELEASE CABLE. CORRODED. TAILCONE RELEASE CABLE TERMINAL CORRODED. R & R TAIL CONE RELEASE CABLE. OPERATION CHECKED IAW AMDS 53-52-7116. - [SDR DALA14032389213](https://openairdocs.org/sdr/DALA14032389213), May 24, 2014: VANE. DAMAGED. RIGHT FIXED VANE INBD HAS PUNCTURE AND A GOUGE. SANDED, CLEANED, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-10-02 AND 59-20-05. - [SDR DALA14032399213](https://openairdocs.org/sdr/DALA14032399213), May 22, 2014: SKIN. CRACKED. AFT ACCESSORY COMPARTMENT AT BS 1520 INBD SIDE OF LONGERON 2R SKIN DOUBLER CRACKED. CUT OUT DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10 - [SDR DALA14032439213](https://openairdocs.org/sdr/DALA14032439213), May 21, 2014: WEB. CRACKED. AFT ACCESSORY COMPARTMENT AT BS 1520 WEB CRACKED. CUTOUT DAMAGE. FABRICATED AND INSTALLED REPAIR IAW ERA 524972-14. - [SDR DALA14032379213](https://openairdocs.org/sdr/DALA14032379213), May 21, 2014: STOP FITTING. WORN. AFT CARGO DOOR LOWER AFT STOP FITTING IS WORN AND HAS BARE METAL. R & R LOWER STOP FITTING ON AFT CARGO DOOR IAW SRM 51-30-02. - [SDR DALA14032369213](https://openairdocs.org/sdr/DALA14032369213), May 20, 2014: FRAME. DAMAGED. AFT CARGO FRAME BS 1344, LONGERON 28L IS OUT OF LIMITS. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-02. - [SDR DALA14031659213](https://openairdocs.org/sdr/DALA14031659213), May 20, 2014: STRUCTURE. CORRODED. BS 1364, LONERON 29R CORRODED WHERE FRAME ATTACH ANGLES AND SKIN JOINT. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FORMER IAW SRM 51-10-03. - [SDR DALA14031649213](https://openairdocs.org/sdr/DALA14031649213), May 20, 2014: FORMER. CORRODED. FORMER CORRODED FROM LONGERON 29L-29R. REMOVED CORROSION FROM L28L - 29R. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FORMER IAW SRM 53-00-01, 51-30 - [SDR DALA14031639213](https://openairdocs.org/sdr/DALA14031639213), May 19, 2014: DOOR FRAME. CORRODED. AFT LOWER CARGO DOOR FRAME DOUBLER HAS SURFACE CORROSION, REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. R & R HEADER BEAM IAW DWG 5930483, REV AR. - [SDR DALA14031629213](https://openairdocs.org/sdr/DALA14031629213), May 19, 2014: FINGER DOUBLER. CRACKED. FINGER DOUBLER LONGERON 26L BS 1288 IN AFT CARGO CRACKED. REMOVED, FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DWG 5936667, REV CD. - [SDR DALA14031619213](https://openairdocs.org/sdr/DALA14031619213), May 19, 2014: LONGERON. CORRODED. CORROSION ON LONGERON 28L BETWEEN BS 1344-1364. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW LONGERON IAW DWG 5936667, REV CD. - [SDR DALA14031319213](https://openairdocs.org/sdr/DALA14031319213), May 18, 2014: FRAME. CRACKED. AFT ACCESSORY COMPARTMENT, RIGHT HAND SIDE, AT CANT FRAME 1542 LOWER END CRACKED. All 154: https://openairdocs.org/deregistered/N913DN-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 20030226003329I](https://openairdocs.org/incident/20030226003329I), Feb 26, 2003: Doug MD9030 (N913DN), Dallas-Ft Worth, TX. (-23) On 2/26/03 at 1738Z, delta airlines, acft N913DN, a MD-90, enroute ont to dfw, landed on runway 36L. Aircraft locked up both l/h MLG wheels and skidded… --- 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.