# N925DN: 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: 53587
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 20, 2011
- Certificate issued: July 7, 2010
- Last registry action: August 31, 2020
- Mode S code: ACD115
- Owner when cancelled: [Delta Air Lines](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES)
- 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/N925DN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=925DN
- Page: https://openairdocs.org/deregistered/N925DN-2022-11-29

From the FAA registry file of October 29, 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 (99, newest 50)

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

- [SDR DALA2019070304114](https://openairdocs.org/sdr/DALA2019070304114), Jul 3, 2019: FITTING. OUT OF ADJUST. CAPTAIN EXIT WINDOW WILL NOT OPEN, HANDLE JAMMED. FOUND LOWER AFT WINDOW HOOK DIFFICULT TO DISENGAGE. ADJUSTED LOWER AFT HOOK FITTING REF AMM 56-12, OPS CHECKS 
- [SDR DALA2019050602859](https://openairdocs.org/sdr/DALA2019050602859), May 5, 2019: FRAME. CRACKED. CRACK WAS FOUND OF 0.375" IN DEPTH ON LH FRAME TAB UPPER RADIUS OF OVERWING FRAME, STA.Y= 962. (SM).SUMMARY OF NR 00091:FRAME ON STA Y=962 LT WAS REPLACE PER DW
- [SDR DALA2019040982322](https://openairdocs.org/sdr/DALA2019040982322), Apr 7, 2019: BATTERY PACK. FAILED. TAILCONE EXIT LIGHT ILLUMINATED. REPLACED AFT EXIT EMERGENCY LIGHT BATTERY PACK PER MD90 AMM 33-51. OPS CHECK NORMAL. (LP# 5836934)
- [SDR DALA20190402085](https://openairdocs.org/sdr/DALA20190402085), Mar 29, 2019: LANYARD. MISSING. R1 DOOR GIRTBAR MISSING LANYARD. INSTALLED SERVICEABLE BISTLE AND GIRT LANYARD REF MD90 AMM 25-61. NO RII REQUIRED. OK FOR SVC. (LP# 5836906)
- [SDR DALA2019012000397](https://openairdocs.org/sdr/DALA2019012000397), Jan 19, 2019: SKIN. DAMAGED. VERTICAL STABILIZER LEADING EDGE AT SPLICE 52.267 SEVERAL COUNTERSINKS BAD (FASTENER BELOW SKIN SURFACE) IN LOWER ROW OF FASTENERS. REAMED 24 EA HOLES ON 1/4" F
- [SDR DALA2018111606646](https://openairdocs.org/sdr/DALA2018111606646), Nov 16, 2018: UNKNOWN. ODOR. F/A'S REPORTED LIGHT HAZE AND FUMES IN CABIN ON TAXI IN TO ORD. AS PRECAUTIONARY MEASURE ABORTED APU START. SHORTLY AFTER F/A'S REPORTED THE HAZE AND FUMES WERE
- [SDR DALA2017102707891](https://openairdocs.org/sdr/DALA2017102707891), Oct 26, 2017: CABLE. DISCONNECTED. DOOR 2R GIRT BAR CABLE FOUND LOOSE DISCONNECTED. REINSTALLED GIRT BAR SLIDE PINS.
- [SDR DALA2017051003832](https://openairdocs.org/sdr/DALA2017051003832), May 9, 2017: DOUBLER. CRACKED. AFT ACCESSORY COMPARTMENT CRACKED INNER FUSELAGE PRODUCTION DOUBLER, BS 1520 BETWEEN LONGERON 3R TO 2R. REPAIRED IAW SRM 53-10-03, ETI 90-17-030 AND ERA 558299-
- [SDR DALA2017051003829](https://openairdocs.org/sdr/DALA2017051003829), May 9, 2017: DOUBLER. CRACKED. AFT ACCESSORY COMPARTMENT CRACKED INNER FUSELAGE PRODUCTION DOUBLER, BS 1520, BETWEEN LONGERONS 3R TO 2R. REPAIRED IAW ETI 90-17-030 AND ERA 558099-14 REV O.
- [SDR DALA2017050903827](https://openairdocs.org/sdr/DALA2017050903827), May 8, 2017: BULKHEAD WEB. CORRODED. CORROSION ON AFT PRESSURE BULKHEAD WEB, BS 1395 LONGERONS 24L-24R. CORROSION WAS REMOVED IAW ETI 90-17-021 AND ERA 556396-14, REV O.
- [SDR DALA2017050803741](https://openairdocs.org/sdr/DALA2017050803741), May 7, 2017: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PANEL 520FT, 520AT, 620FT AND 141AL. REPLACED.
- [SDR DALA2017050803717](https://openairdocs.org/sdr/DALA2017050803717), May 6, 2017: FITTING. BROKEN. DURING OPERATIONAL CHECK OF THE INTERNAL EMERGENCY TAIL CONE RELEASE MECHANISM, HANDLE CLIPS WERE BROKEN. REPLACED IAW SRM 51-30-02.
- [SDR DALA2017050803715](https://openairdocs.org/sdr/DALA2017050803715), May 5, 2017: SUPPORT. CORRODED. CORROSION ON FITTING GIRT BAR LATCH SUPPORT RIGHT HAND, STA 120, X=-54. FOUND TO BE OUT OF LIMITS. FABRICATED FITTING IAW DWG 3936190, REV O.
- [SDR DALA2017050603713](https://openairdocs.org/sdr/DALA2017050603713), May 5, 2017: SKIN. CRACKED. CRACK ON HOLE OF FUSELAGE SKIN AND LONGERON AT STA 775, L10L. REPAIRED IAW ERA 566400-14, REVA.
- [SDR DALA2017050303659](https://openairdocs.org/sdr/DALA2017050303659), May 2, 2017: FRAME. CRACKED. CRACK ON FRAME LIGHTNING HOLE AT BS 1567 BETWEEN 6 AND 9 HOURS POSITIONS. REPLACED IAW SRM 51-30-02, AND 51-30-05.
- [SDR DALA2017043003471](https://openairdocs.org/sdr/DALA2017043003471), Apr 29, 2017: STEP. CORRODED. CORROSION ON WEB STEP NR 11 AT AFT VENTRAL STAIR. REPLACED IAW SRM 51-30-02 AND 51-30-05.
- [SDR DALA2017043003470](https://openairdocs.org/sdr/DALA2017043003470), Apr 29, 2017: ANGLE. CORRODED. CORROSION ON ANGLE OF INTERCOSTAL STA 1269 - 1277 BETWEEN LONGERON 30-29R. REPLACED IAW SRM 53-10-03 AND 51-10-01.
- [SDR DALA2017043003469](https://openairdocs.org/sdr/DALA2017043003469), Apr 29, 2017: FRAME. CORRODED. CORROSION ON FRAME STA 1364 BETWEEN LONGERON 28R AND 28L. FOUND TO BE OUT OF LIMITS. REPLACED FRAME IAW SRM 53-10-02 AND 51-30-05.
- [SDR DALA2017043003467](https://openairdocs.org/sdr/DALA2017043003467), Apr 29, 2017: STRUCTURE. CRACKED. FUSELAGE CRACK STA 1041 TO 1060 LONGERON 20R. REPAIRED IAW SRM 53-10-01.
- [SDR DALA2017043003472](https://openairdocs.org/sdr/DALA2017043003472), Apr 28, 2017: SUPPORT. CRACKED. AFT CARGO COMPARTMENT CRACKED AT SLANT PANEL SUPPORT STA 1117L, 1136L/R, 1155L, 1328L AND 193R. FABRICATED AND INSTALLED NEW SUPPORTS IAW SRM 51-10-03 AND ERA 4
- [SDR DALA2017042903466](https://openairdocs.org/sdr/DALA2017042903466), Apr 28, 2017: ATTACH ANGLE. CRACKED. WHEEL WELL CRACK ON ATTACH ANGLE STA 1051 PROJECTION LONGERON 20L. REPAIRED IAW SRM 51-30-05 AND 53-10-01.
- [SDR DALA2017042803465](https://openairdocs.org/sdr/DALA2017042803465), Apr 27, 2017: ANGLE. CORRODED. CORROSION ON AFT ACCESSORY COMPARTMENT FRAME ANGLE STA 1437 BETWEEN PROTECTION LONGERON 25L AND 25R. REPLACED IAW DWG 9912246, REV CE AND SRM 51-30-02 AND 51-30
- [SDR DALA2017043003504](https://openairdocs.org/sdr/DALA2017043003504), Apr 26, 2017: BULKHEAD. CORRODED. CORROSION ON ANGLE ON AFT BULKHEAD AFT FACE BS 1395, PROTECTION LONGERON 29R. REPLACED IAW SRM 51-30-05, 51-30-02 AND DWG 9915561, REV CG.
- [SDR DALA2017042703464](https://openairdocs.org/sdr/DALA2017042703464), Apr 26, 2017: FRAME. CORRODED. AFT CARGO COMPARTMENT CORROSION ON FRAME STA 1344 BETWEEN LONGERON 25L AND 25R. REPAIRED IAW SRM 53-10-02.
- [SDR DALA2017042703463](https://openairdocs.org/sdr/DALA2017042703463), Apr 26, 2017: SKIN. CRACKED. CRACK ON HOLE ON FUSELAGE SKIN AND LONGERON AT STA 775 AND 10L. REPAIRED IAW ERA 566400-14 REV O.
- [SDR DALA2017043003473](https://openairdocs.org/sdr/DALA2017043003473), Apr 25, 2017: BULKHEAD. CORRODED. CORROSION ON AFT BULKHEAD WEB AFT CARGO COMPARTMENT, STA 1395, PROJECTION LONGERON 24L TO 24R. REPLACED IAW DWG 9915561 AND SRM 51-30-02, 51-30-05.
- [SDR DALA2017042603461](https://openairdocs.org/sdr/DALA2017042603461), Apr 25, 2017: LONGERON. CRACKED. LONGERON CRACKED 5L, STA 1364. REPAIRED IAW SRM 53-10-01.
- [SDR DALA2017042503459](https://openairdocs.org/sdr/DALA2017042503459), Apr 24, 2017: FRAME. CORRODED. CORROSION ON FRAME STA 1328 BETWEEN LONGERONS 28R AND 26L. REPAIRED IAW SRM 53-10-02.
- [SDR DALA2017042503411](https://openairdocs.org/sdr/DALA2017042503411), Apr 24, 2017: LONGERON. CRACKED. CRACK ON LONGERON 17R AND BS 408. REPAIRED IAW SRM 53-10-11.
- [SDR DALA2017042403410](https://openairdocs.org/sdr/DALA2017042403410), Apr 23, 2017: FORMER. WORN. WEAR ON LEFT AND RIGHT FORMER BS 1460, REPAIRED IAW ERA 511165-14, REV D.
- [SDR DALA2017042403409](https://openairdocs.org/sdr/DALA2017042403409), Apr 22, 2017: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM BS 160 BETWEEN LBL 7 AND 54. REPLACED IAW SRM 51-30-02, AND 51-30-05.
- [SDR DALA2017042403407](https://openairdocs.org/sdr/DALA2017042403407), Apr 22, 2017: INTERCOSTAL. CORRODED. CORROSION ON INTERCOSTAL BS 1437, RBL 15. REPAIRED IAW SRM 51-70-01. (LP# 2987151)
- [SDR DALA2017042303406](https://openairdocs.org/sdr/DALA2017042303406), Apr 22, 2017: DOUBLER. WORN. WEAR ON FORWARD & AFT LOWER DOUBLERS ON MID CARGO DOOR. REPLACED IAW SRM 51-30-02.
- [SDR DALA2017042303405](https://openairdocs.org/sdr/DALA2017042303405), Apr 22, 2017: PAN. WORN. WEAR ON MID CARGO DOOR INNER & OUTER PAN LOWER SECTIONS. DAMAGE OUT OF LIMITS. REPAIRED IAW ERA 413163-14, REV B.
- [SDR DALA2017042303404](https://openairdocs.org/sdr/DALA2017042303404), Apr 22, 2017: ANGLE. CORRODED. CORROSION ON ANGLE, BS 160, BETWEEN LBL 7 AND 54. REPLACED THE ANGLE IAW DWG 9955780, REV LA.
- [SDR DALA2017042403408](https://openairdocs.org/sdr/DALA2017042403408), Apr 21, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, BS 160 - 200, LBL 54. REPLACED IAW SRM 51-30-02, 51-30-05, AND 51-10-05.
- [SDR DALA2017042203403](https://openairdocs.org/sdr/DALA2017042203403), Apr 21, 2017: FLOORBEAM. CORRODED. CORROSION ON THE FLOORBEAM BS 200 BETWEEN RBL 44 - 54. REPLACED IAW SRM 51-30-05, AND 51-30-02.
- [SDR DALA2017042203402](https://openairdocs.org/sdr/DALA2017042203402), Apr 21, 2017: STRUCTURE. CRACKED. L1 DOOR CRACKED ON CUT OUT OF OPEN LOCK. REPAIRED IAW SRM 52-10-01.
- [SDR DALA2017042403340](https://openairdocs.org/sdr/DALA2017042403340), Apr 20, 2017: RUB STRIP. CORRODED. CORROSION ON RUBSTRIP OF FUEL PANEL. REPLACED THE RUB STRIP IAW SRM 57-10-05.
- [SDR DALA2017042403338](https://openairdocs.org/sdr/DALA2017042403338), Apr 20, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT, STA 1442, X=15. REPAIRED IAW SRM 51-70-01.
- [SDR DALA2017042103337](https://openairdocs.org/sdr/DALA2017042103337), Apr 20, 2017: ANGLE. CRACKED. CRACKED CLIP AND FRAME STA 1508, LONGERON 2L. REPLACED IAW SRM 51-30-05 AND DWG 9911860. (LP# 2984205)
- [SDR DALA2017042103336](https://openairdocs.org/sdr/DALA2017042103336), Apr 20, 2017: LONGERON. CORRODED. AFT CARGO COMPARTMENT CORROSION ON LONGERON 27R, RIGHT HAND SIDE FROM Y= 1395 TO Y=1340. FOUND TO BEE OUT OF LIMITS. LONGERON WAS REPLACED STA Y=1307 TO Y+ 1395
- [SDR DALA2017043003474](https://openairdocs.org/sdr/DALA2017043003474), Apr 19, 2017: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK STA 200 -240 X-44. REPLACED IAW SRM 53-40-01, 51-30-01 AND 51-30-05.
- [SDR DALA2017042403339](https://openairdocs.org/sdr/DALA2017042403339), Apr 19, 2017: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM BS 256 BETWEEN X=-22 AND -44 AT FLOOR STRUCTURE. REPLACED IAW SRM 51-10-05 AND 51-30-05. (LP# 2982733)
- [SDR DALA2017042003335](https://openairdocs.org/sdr/DALA2017042003335), Apr 19, 2017: WEB. CORRODED. CORROSION ON FLOOR MEMBRANE BETWEEN STA 157 AND 160, X=22. REPAIRED IAW SRM 53-00-01. (LP# 2981932)
- [SDR DALA2017041903230](https://openairdocs.org/sdr/DALA2017041903230), Apr 18, 2017: SKIN. CORRODED. CORROSION ON FUSELAGE SKIN STA 827 BETWEEN LONGERON 27R TO 28R. REPAIRED IAW SRM 53-30-01.
- [SDR DALA2017041803227](https://openairdocs.org/sdr/DALA2017041803227), Apr 17, 2017: SKIN. CORRODED. FUSELAGE SKIN CORROSION, STA 827 BETWEEN L27R - 28R. REPAIRED IAW SRM 53-30-01.
- [SDR DALA2017041803226](https://openairdocs.org/sdr/DALA2017041803226), Apr 17, 2017: PAN. CRACKED. CRACK ON INNER PAN AT BEAM FORWARD EDGE OF FORWARD CARGO DOOR. REPAIRED IAW SRM 52-30-02.
- [SDR DALA2017041803225](https://openairdocs.org/sdr/DALA2017041803225), Apr 17, 2017: PANEL. CORRODED. CORROSION ON COUNTERSINK HOLE AT FUEL PLATE 620AT. REWORKED PER SRM 57-00-04.
- [SDR DALA2017041803224](https://openairdocs.org/sdr/DALA2017041803224), Apr 17, 2017: CUSP WEB. CORRODED. CORROSION ON RIGHT HAND CUSP WEB BETWEEN STA 1260 - 1264, X=-54 AND X=60. REPAIRED IAW SRM 53-20-02, 51-10-03 AND 51-30-01.

All 99: https://openairdocs.org/deregistered/N925DN-2022-11-29/reports.md

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