# N945DN: 1998 Boeing MD-90-30, registration cancelled 2023-06-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 26, 2023 - Status when cancelled: Sale reported, canceled - 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: 53559 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 14, 2013 - Last registry action: September 20, 2022 - Mode S code: AD2013 - Location: [Blytheville, AR](https://openairdocs.org/faa-place/AR/Blytheville) - Owner type: Individual - Owner's area on the map: 35.8994° N, 89.8993° W: Placed by OpenAirDocs at the center of ZIP code 72315, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N945DN - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=945DN - Page: https://openairdocs.org/deregistered/N945DN-2023-06-26 From the FAA registry file of October 31, 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA2018091405597](https://openairdocs.org/sdr/DALA2018091405597), Sep 12, 2018: GENERATOR. FAILED. ATB, LT VSCF FAILURE IN CRUISE WITH LT GEN OFF AND AC PWR FAULT. UNABLE TO START APU. EPCU FAULTED 'LEFT CONV EU FAIL' WITH LT CHANNEL NBPT AND LT CHANNEL UF TR - [SDR DALA2018053003674](https://openairdocs.org/sdr/DALA2018053003674), May 30, 2018: SKIN. DENTED. A TWO INCH DENT WAS FOUND NEAR BS 579 LONGERONS 15-16R. PERFORMED AN HFEC OF DAMAGED SKIN PANEL AND INTERNAL HFEC OF EXPOSED SKIN PANEL AND INTERNAL HFEC OF EXP - [SDR DALA2018052983619](https://openairdocs.org/sdr/DALA2018052983619), May 25, 2018: INTERCOSTAL. CRACKED. TAILCONE BAY BS 1567, INTERCOSTAL CRACKED, 2 INCHES RIGHT OF TOP CENTER LINE. REMOVED AND REPLACED THE INTERCOSTAL. - [SDR DALA2018052980618](https://openairdocs.org/sdr/DALA2018052980618), May 25, 2018: INTERCOSTAL. CRACKED. TAILCONE BAY FRAME BS 1567, INTERCOSTAL WAS CRACKED. TWO INCHES LEFT OF TOP CENTER LINE. REMOVED AND DRILLED A NEW INTERCOSTAL. - [SDR DALA2018050803144](https://openairdocs.org/sdr/DALA2018050803144), May 7, 2018: SKIN. DENTED. FOUND A DENT FORWARD OF FORWARD CARGO DOOR, BS 370, LONGERON 24R. REPAIRED THE SKIN IAW ERA 568404-14, REV 0, SEC 1. - [SDR DALA2017111508148](https://openairdocs.org/sdr/DALA2017111508148), Nov 14, 2017: BATTERY PACK. INOPERATIVE. EMERGENCY CEILING LIGHTS INOPERATIVE ROW 24. REPLACED THE BATTERY PACK. OPS CHECKED GOOD. - [SDR DALA2017040502834](https://openairdocs.org/sdr/DALA2017040502834), Apr 4, 2017: SKIN. CRACKED. FUSELAGE SKIN HAS A CRACK, BS 1474, LONGERON 2R. REPAIRED IAW SRM 53-30-01. - [SDR DALA2017040502833](https://openairdocs.org/sdr/DALA2017040502833), Apr 4, 2017: ATTACH ANGLE. CRACKED. LONGERON TO FRAME ATTACH ANGLE IS CRACKED AT BS 1475, LONGERON 2L. REMOVED AND REPLACED IAW SRM 51-30-05 AND DWG 9964460, REV AB AND AA. - [SDR DALA2017040402831](https://openairdocs.org/sdr/DALA2017040402831), Apr 3, 2017: STIFFENER. CRACKED. STIFFENER CRACKED AT BSW 1520, BULKHEAD FRAME BETWEEN LONGERONS 7 AND 8L. REMOVED AND REPLACED IAW DWG 9911839 AND SRM 51-30-05. - [SDR DALA2017040402830](https://openairdocs.org/sdr/DALA2017040402830), Apr 2, 2017: ATTACH FITTING. CRACKED. RIGHT VERTICAL STABILIZER ATTACH ANGLE CRACKED. BS 1458-1486. REMOVED AND REPLACED IAW SRM 51-30-02 AND DWG 5912188, REV BD. - [SDR DALA2017040202673](https://openairdocs.org/sdr/DALA2017040202673), Apr 1, 2017: ATTACH ANGLE. CRACKED. LEFT VERTICAL STABILIZER ATTACH ANGLE, BS 1458 - 1486 CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-30-02, 51-30-05, AND DWG 5912188, REV BD. - [SDR DALA2017040202672](https://openairdocs.org/sdr/DALA2017040202672), Apr 1, 2017: LONGERON CLIP. CRACKED. LONGERON CLIP FOUND TO HAVE A CRACK AT BS 1475, LONGERON 2R. FABRICATED A NEW LONGERON CLIP IAW SRM 51-10-05, 51-10-03, AND DW 5911432, REV CE, AND CF. - [SDR DALA2017040202671](https://openairdocs.org/sdr/DALA2017040202671), Apr 1, 2017: SEAT TRACK. CORRODED. RIGHT OUTBOARD RBL 54 SEAT TRACK BS 932 - 937.5 HAS SIGNS OF LIGHT SURFACE CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51- - [SDR DALA2017040102670](https://openairdocs.org/sdr/DALA2017040102670), Mar 31, 2017: FRAME. CRACKED. NOSE LANDING GEAR WHEEL WELL CUTOUT FRAME CRACKED, BS 45, RIGHT SIDE. REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05 AND DWG 9910088, REV CJ. - [SDR DALA2017040302676](https://openairdocs.org/sdr/DALA2017040302676), Mar 30, 2017: SKIN. CRACKED. CRACK ON EXTERNAL SKIN, BS 1530, LONGERON 25L. REPAIRED THE SKIN IAW ERA 2953999. - [SDR DALA2017033002570](https://openairdocs.org/sdr/DALA2017033002570), Mar 29, 2017: ATTACH FITTING. CRACKED. FRAME ATTACHMENT IS CRACKED AT BS 1475 LONGERON 2R. REMOVED AND REPLACED IAW SRM 53-30-01. - [SDR DALA2017013100856](https://openairdocs.org/sdr/DALA2017013100856), Jan 28, 2017: SWITCH. FAILED. ON APPROACH, AFTER LANDING GEAR LOWERED, THE PARKING BRAKE ILLUMINATED, QRH PROCEDURE COMPLIED WITH. TROUBLESHOT. REMOVED AND REPLACED SWITCH S1-130 AND AACU IA - [SDR DALA2016120809740](https://openairdocs.org/sdr/DALA2016120809740), Dec 6, 2016: BATTERY PACK. INOPERATIVE. TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY IN AFT RIGHT LAVATORY. OPERATION CHECKED GOOD. - [SDR DALA2016050603779](https://openairdocs.org/sdr/DALA2016050603779), May 5, 2016: OXYGEN MASK. UNWANTED DEPLOY. THE CREW PERFOMED AN AIR TURN BACK TO ATL. AFTER TAKEOFF, CLIMBING THROUGH 1000 GL, THE LEFT CAPTAINS SIDE OF ACFT, O2 MASKS DROPPED. PRESSURIZATION NORMAL. MAI - [SDR DALA2016050603778](https://openairdocs.org/sdr/DALA2016050603778), May 4, 2016: OXYGEN MASK. UNWANTED DEPLOY. THE CREW PERFORMED AN AIR TURN BACK. ALL LT SIDE PASSENGER O2 MASKS DROPPED. CABIN PRESSURIZATION NORMAL. MAINTENANCE REPLACED R2-315 RELAY. RESTOWED MASKS AND - [SDR DALA2016033002453](https://openairdocs.org/sdr/DALA2016033002453), Mar 24, 2016: LINE. FAILED. CREW EXPERIENCED A LOSS OF RT HYDRAULIC SYS FLUID DURING FLIGHT. AN EMERGENCY WAS DECLARED AND THE CREW PERFORMED AN ALTERNATE GEAR EXTENSION FOR LANDING. MAINT - [SDR DALA2015102306506](https://openairdocs.org/sdr/DALA2015102306506), Oct 21, 2015: SKIN. DAMAGED. DAMAGE AFT OF R1 DOOR, JUST FORWARD OF WINDOW PLUG. - [SDR DALA2015092405829](https://openairdocs.org/sdr/DALA2015092405829), Sep 21, 2015: POWER SUPPLY. INOPERATIVE. L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY POWER SUPPLY IAW AMM. OPS CHECKS OK. - [SDR DALA2015042402947](https://openairdocs.org/sdr/DALA2015042402947), Apr 23, 2015: SLIDE. UNSECURE. TAILCONE SLIDE OUT OF PACK. R & R TAILCONE EVACUATION SLIDE IAW AMDS 2461-4643. LP 1917510. - [SDR DALA2015041302754](https://openairdocs.org/sdr/DALA2015041302754), Apr 11, 2015: SLIDE. INOPERATIVE. L1 DOOR SLIDE INOPERATIVE. R & R L1 DOOR SLIDE IAW JIC 2561-4641. LP 7291306. - [SDR DALA2014121706581](https://openairdocs.org/sdr/DALA2014121706581), Dec 14, 2014: WIRE. BURNED. SMOKE FROM CAPTAINS WING & NOSE LIGHT PANEL DURING SHORT FINAL. THE LIGHTS WERE TURNED OFF AND SMOKE CEASED. INSPECTED AND FOUND WIRE END BURNED ON NGL LIGHT SW - [SDR DALA13034769245](https://openairdocs.org/sdr/DALA13034769245), Jul 14, 2013: LANYARD. INOPERATIVE. ON SERVICE CHECK, FOUND SLIDE LANYARD HANGING OUTSIDE BUSSLE AT L1 DOOR. REMOVED AND INSTALLED SLIDE IAW AMM. RII COMPLIED WITH. OK FOR SERVICE. - [SDR DALA13033729245](https://openairdocs.org/sdr/DALA13033729245), Jun 30, 2013: LIGHT. MISSING. FLIGHT CREW REPORTED EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. MX REPLACED 20" OF MISSING LIGHT IAW MM. - [SDR DALA13016009245](https://openairdocs.org/sdr/DALA13016009245), Apr 10, 2013: LANYARD. FRAYED. DOOR SLIDE COVER LOCK LANYARDS ARE FRAYED, R & R LANYARDS IAW W/C 2500-4332. - [SDR DALA13013459245](https://openairdocs.org/sdr/DALA13013459245), Mar 25, 2013: ANGLE. CORRODED. AFT VENTRAL STAIRS, LOWER SEGMENT IS CORRODED IN INTERNAL SKIN UNDER STEPS IN SEVERAL PLACE. REMOVED ANGLE FOUND 100 PERCENT OUT OF LIMITS, AND AREAS ON STRINGE - [SDR DALA13010909245](https://openairdocs.org/sdr/DALA13010909245), Mar 6, 2013: CUSP WEB. CHAFED. RT MAIN CUSP WEB, STA 218, RBL 46 FORWARD OF LIGHTNING HOLE HAS CHAFE MARKS. FOUND CRACKED AREA, CUT OUT DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED DOUB - [SDR DALA13010879245](https://openairdocs.org/sdr/DALA13010879245), Mar 6, 2013: STRUCTURE. CRACKED. MAIN CABIN CENTER WING BOX UPPER SURFACE LT SIDE UPPER CHORD CRACKED AT FORWARD FASTENER GOING VERTICAL APPROX STA 913, LBL 48. CUT OUT DAMAGED AREA, FABRICATED --- 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.