# N952DN: 1998 Boeing MD-90-30, registration cancelled 2020-08-25

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 25, 2020
- 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: 53560
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 17, 2013
- Certificate issued: November 19, 2012
- Last registry action: November 16, 2018
- Mode S code: AD3C6D
- 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/N952DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=952DN
- Page: https://openairdocs.org/deregistered/N952DN-2020-08-25

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 (38)

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

- [SDR DALA2019051002928](https://openairdocs.org/sdr/DALA2019051002928), May 9, 2019: ENGINE. FAILED. RT. ENGINE FAILED DURING CLIMB AT 5000 MSL. (0) OIL PRESSURE, EGT 980 AND RISING. SHUTDOWN NORMAL. REPLACED NUMBER 2 ENGINE ON LOG 1063040. (LP# 5691956)
- [SDR DALA2018102206190](https://openairdocs.org/sdr/DALA2018102206190), Oct 18, 2018: STARTER. DISINTEGRATED. LEFT ENG DURING START NO N2 ROTATION GROUND CREW REPORTED SPARKS AND FLAMES. COMPLIED WITH MANUAL ABORTED START PROCEDURE PER QRH. FOUND STARTER DISINTEGRATED. 
- [SDR DALA2019122407534](https://openairdocs.org/sdr/DALA2019122407534), Aug 25, 2018: SPAR. NOT REPORTED. ER/A 570845-14AD ISSUED FOR REPAIR TO LH HORIZONTAL STAB UPPER REAR SPAR BARREL NUT HOLE. FOLLOW ON ACTION IS REQUIRED. C/A ERA REVISED TO REV 'A'. SECTION II I
- [SDR DALA2018073104785](https://openairdocs.org/sdr/DALA2018073104785), Jul 29, 2018: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT EXIT SIGN AT SEAT 34 INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT SEAT 32C IAW AMM 33-51-03.
- [SDR DALA2018061103956](https://openairdocs.org/sdr/DALA2018061103956), Jun 7, 2018: COFFEEMAKER. SMOKE. AIRBORNE - SMOKE FROM COFFEE POT 102. WHET TO QRH, TURNED OFF GALLEY POWER, SMOKE DISSIPATED. R&R FWD GALLEY F102 COFFEE MAKER. FOUND C/B POPPED ON BACK OF C/M.
- [SDR DALA2018032902027](https://openairdocs.org/sdr/DALA2018032902027), Mar 29, 2018: SHUTOFF VALVE. FAILED. WHILE BOARDING, THE CREW REPORTED AN ANTI-SKID FAULT, FOLLOWED BY AN ELECTRICAL ODOR IN THE COCKPIT. REPLACED THE ANTI-SKID RETURN SHUTOFF VALVE. REPLACED THE A
- [SDR DALA2017122709019](https://openairdocs.org/sdr/DALA2017122709019), Dec 24, 2017: SCHRADER VALVE. LOOSE. PERFORMED AN AIR TURN BACK TO TPA DUE TO A NOSE LANDING GEAR UNSAFE INDICATION AND NOSE EAR DID NOT RETRACT. AN EMERGENCY WAS DECLARED. TPA MAINTENANCE FOUND TH
- [SDR DALA2017081706275](https://openairdocs.org/sdr/DALA2017081706275), Aug 11, 2017: POWER SUPPLY. INOPERATIVE. SERVICE DOOR VERTICAL EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY B5-241 IAW MM. OPERATION CHECKS GOOD.
- [SDR DALA2017072705814](https://openairdocs.org/sdr/DALA2017072705814), Jul 26, 2017: CONNECTOR. DISCONNECTED. CEILING EMERGENCY LIGHTS INOPERATIVE FROM SEAT 15 THRU 21. TROUBLESHOT. FOUND ELECTRICAL CONNECTOR FOR BATTERY PACK DISCONNECTED. RESECURED CONNECTOR AND OPERAT
- [SDR DALA2017070505259](https://openairdocs.org/sdr/DALA2017070505259), Jul 4, 2017: FRAME. CRACKED. CABIN LEFT HAND FRAME STA 902 FOUND TO HAVE CRACK. REPLACED ON TASK CARD 5310-01375-06-LT.
- [SDR DALA2017070505238](https://openairdocs.org/sdr/DALA2017070505238), Jul 1, 2017: ATTACH ANGLE. CRACKED. CRACKED ANGLE SUPPORT AT AFT FACE OF FRAME, BS 1520, LONGERON 3L. REMOVED AND REPLACED IAW SRM 51-30-05, AND DWG 9911839.
- [SDR DALA2017070505237](https://openairdocs.org/sdr/DALA2017070505237), Jul 1, 2017: ATTACH ANGLE. CRACKED. AFT LOWER ATTACH ANGLE FOR LOUVER BOX FOUND CRACK AT FRAME, BS 1520, LONGERON 4L. REMOVED AND REPLACED IAW SRM 51-30-05, AND DWG 9911839.
- [SDR DALA2017070205194](https://openairdocs.org/sdr/DALA2017070205194), Jun 30, 2017: FRAME. CRACKED. CRACK ON FRAME ANGLE AT BS 1542 BELOW LOWER BOX. REPAIRED IAW SRM 53-10-03.
- [SDR DALA2017070205197](https://openairdocs.org/sdr/DALA2017070205197), Jun 29, 2017: DOUBLER. CORRODED. VERTICAL STABILIZER INTERNAL DOUBLER HAS FRETTING. REMOVED AND REPLACED DOUBLER IAW SRM 51-30-02 AND DWG 5910242.
- [SDR DALA2017070205147](https://openairdocs.org/sdr/DALA2017070205147), Jun 28, 2017: ATTACH ANGLE. CRACKED. VERTICAL STABILIZER RIGHT HAND INTERNAL ATTACH ANGLE CRACKED. REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 5912188.
- [SDR DALA2017070205146](https://openairdocs.org/sdr/DALA2017070205146), Jun 28, 2017: ATTACH ANGLE. CRACKED. VERTICAL STABILIZER LEFT HAND INTERNAL ATTACH CRACKED. REMOVED AND REPLACED VERTICAL STABILIZER LEFT HAND INTERNAL ATTACH ANGLE IAW SRM 51-30-02, 51-30-05 AND D
- [SDR DALA2017070205141](https://openairdocs.org/sdr/DALA2017070205141), Jun 28, 2017: FRAME. CRACKED. NOSE LANDING GEAR WHEEL WELL STATION 45R FRAME CRACKED. REMOVED AND REPLACED NOSE LANDING GEAR WHEEL WELL IAW 51-30-02, 51-30-05 AND DWG 9910088.
- [SDR DALA2017070605261](https://openairdocs.org/sdr/DALA2017070605261), Jun 27, 2017: HINGE. CRACKED. NOSE LANDING GEAR AT LEFT AFT DOOR AFT HINGE HAS A CRACK IN THE RADIUS. REPAIRED IAW SRM 53-30-01.
- [SDR DALA2017070205145](https://openairdocs.org/sdr/DALA2017070205145), Jun 27, 2017: ATTACH FITTING. CRACKED. LONGERON 2L TO FRAME STA 1475 FORWARD ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED ATTACHMENT CLIP ATL2L STA 1475 IAW SRM 51-30-05 AND DWG 5911432.
- [SDR DALA2017070205144](https://openairdocs.org/sdr/DALA2017070205144), Jun 27, 2017: ATTACH FITTING. CRACKED. LONGERON 2R TO FRAME STA 1475 FORWARD ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED ATTACHMENT CLIP STA 1475 L2R IAW SRM 51-30-05 AND DWG 5911432.
- [SDR DALA2017070205143](https://openairdocs.org/sdr/DALA2017070205143), Jun 27, 2017: ATTACH FITTING. CRACKED. LONGERON 2L TO FRAME STA 1475 AFT ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED ATTACHMENT CLIP IAW SRM 51-30-05 AND DWG 9964460.
- [SDR DALA2017070205142](https://openairdocs.org/sdr/DALA2017070205142), Jun 27, 2017: ATTACH FITTING. CRACKED. LONGERON 2R TO FRAME STA 1475 AFT ATTACHMENT CLIP CRACKED. REMOVED AND REPLACED ATTACHMENT CLIP AT L2R, STA 1475 IAW SRM 51-30-05 AND DWG 9964460.
- [SDR DALA2017062104910](https://openairdocs.org/sdr/DALA2017062104910), Jun 20, 2017: DOUBLER. GOUGED. MID CARGO DOOR PAN DEEPLY GOUGED. ONLY DOUBLER DAMAGED. REPAIRED IAW SRM 52-30-02.
- [SDR DALA2017031302004](https://openairdocs.org/sdr/DALA2017031302004), Mar 8, 2017: LAMP. INOPERATIVE. TWO EMERGENCY LIGHTS INOPERATIVE IN THE TAIL COMPARTMENT. REPLACED THE LAMPS. OPERATION CHECKED GOOD.
- [SDR DALA2016121909956](https://openairdocs.org/sdr/DALA2016121909956), Dec 16, 2016: SIGN. UNSECURE. EMERGENCY EXIT SIGN CENTER AISLE L2 DOOR NEEDS TO BE SECURED. SECURED THE SIGN. OPERATION CHECKED GOOD.
- [SDR DALA2016012000478](https://openairdocs.org/sdr/DALA2016012000478), Jan 19, 2016: BOTTLE. EMPTY. L1 DOOR SLIDE INFLATION PRESSURE AT ZERO. REPLACED L1 DOOR SLIDE JIC 2561-4641.
- [SDR DALA2016012000477](https://openairdocs.org/sdr/DALA2016012000477), Jan 19, 2016: PIN. PULLED. L1 DOOR SLIDE PINS PULLED. R & R SLIDE ASSEMBLY.
- [SDR DALA2015072904745](https://openairdocs.org/sdr/DALA2015072904745), Jul 27, 2015: STRUCTURE. LEAKING. DIVERTED DUE TO OIL FUME ODOR IN CABIN. RT GENERATOR OFF AND RT AC POWER FAULT WITH CORRESPONDING LOSS OF AC POWER. RT GENERATOR OVERHEAT STATUS MESSAGE ON EOAP
- [SDR DALA2015062603977](https://openairdocs.org/sdr/DALA2015062603977), Jun 25, 2015: FRAME. CRACKED. LEFT FUSELAGE OVERWING FRAME AT BS 924 CRACKED AT CUSP WEB. R & R OVERWING FRAME AT BS 924 IAW AMDS 5310-01375-07-LT AND DWG SR90530027, CONFIG -7009.
- [SDR DALA2015013000841](https://openairdocs.org/sdr/DALA2015013000841), Jan 29, 2015: SKIN. CRACKED. THE UPPER AFT SKIN PANEL ON THE RT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED DURING INSPECTION. REPAIRED IAW ERA 531274-14, REV O.
- [SDR DALA2015020200838](https://openairdocs.org/sdr/DALA2015020200838), Jan 29, 2015: SKIN. CRACKED. UPPER AFT SKIN PANEL ON THE RT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND CRACKED. PERFORMED A BONDED REPAIR IAW ERA 531274-14AD.
- [SDR DALA2014071104055](https://openairdocs.org/sdr/DALA2014071104055), Jul 10, 2014: POWER SUPPLY. MALFUNCTIONED. EMERGENCY EXIT SIGN INOPERATIVE. R & R POWER SUPPLY. OPS CHECKED OK.
- [SDR DALA13029329252](https://openairdocs.org/sdr/DALA13029329252), Jun 16, 2013: LANYARD. UNKNOWN. TAILCONE SLIDE RELEASE LANYARD CLEVIS PINS NOT TAKED WITH AND "X" IAW DWG 8370024. R & R TAILCONE SLIDE RELEASE LANYARD IAW AMM.
- [SDR DALA13028039252](https://openairdocs.org/sdr/DALA13028039252), Jun 9, 2013: FRAME. CRACKED. BS 1542, CANTED FRAME LOWER END IS CRACKED. REMOVED DAMAGED SECTION BS 1542. FABRICATED NEW FRAME, REPAIR SPLICE DOUBLER AND SHIMS. INSTALLED REPAIR PARTS IAW E
- [SDR DALA13028029252](https://openairdocs.org/sdr/DALA13028029252), Jun 9, 2013: DOOR FRAME. DAMAGED. BLEND OUTS ON AFT CARGO DOOR FRAME. FABRICATED DOUBLER, STRAP AND BUSHINGS IAW ERA 513348-14. INSTALLED REPAIR PARTS IAW 51-30-05, 51-30-02 AND ERA 513398-14.
- [SDR DALA13023379252](https://openairdocs.org/sdr/DALA13023379252), May 15, 2013: LONGERON. CRACKED. LONGERON 20L, FS 1379, UNDER LT LAV FLOOR, FASTENER IS TOO CLOSE TO RADIUS AND POSSIBLE CRACK. REMOVED, FABRICATED, DRILLED AND INSTALLED SHEAR TIE IAW SRM 51-1
- [SDR DALA13022219252](https://openairdocs.org/sdr/DALA13022219252), May 12, 2013: LONGERON. CORRODED. AFT ACCESSORY BAY, CANTED FRAME 1488, AFT FACE FROM LONGERON R7 TO L11 SEVERAL STIFFENERS HAVE LIGHT SURFACE CORROSION. REMOVED CORROSION. STIFFENERS WITHIN LIM
- [SDR DALA13021509252](https://openairdocs.org/sdr/DALA13021509252), May 8, 2013: BEAM. CORRODED. MID CARGO DOOR FRAME LOWER BEAM IS CORRODED AROUND FASTENER HOLES. DRILLED REPAIR AND FABRICATED SPACER. INSTALLED REPAIR IAW SRM 53-60-02, FIG 9 AND 53-30-02, 

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