# N910DE: 1992 Mcdonnell Douglas MD-88, registration cancelled 2022-11-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 23, 2022
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas MD-88](https://openairdocs.org/model/mcdonnell-douglas-md-88) (registry code 3023689)
- Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 53419
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: November 18, 1992
- Certificate issued: December 28, 1992
- Last registry action: May 18, 2022
- Mode S code: AC96FB
- 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/N910DE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=910DE
- Page: https://openairdocs.org/deregistered/N910DE-2022-11-23

From the FAA registry file of November 5, 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-88: https://openairdocs.org/model/mcdonnell-douglas-md-88.md

## Service difficulty reports (182, newest 50)

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

- [SDR DALA2020033002059](https://openairdocs.org/sdr/DALA2020033002059), Mar 30, 2020: LANYARD. BROKEN. THE L1 DOOR SLIDE LANYARD WAS FOUND BROKEN. MAINTENANCE REPLACED THE SLIDE LANYARD FOR THE L1 DOOR PER MD88 AMM 25-62. (LP #7179212)
- [SDR DALA2020031601856](https://openairdocs.org/sdr/DALA2020031601856), Mar 15, 2020: FRAME. CRACKED. CANTED FRAME CRACKED AT 2 O'CLOCK POSITION AND 7 O'CLOCK. REMOVED L/H LWR FRAME + UPPER FRAME, DRILLED UP THE NEW L/H LWR FRAME + BEGAN DRILLING NEW UPPER FRAME
- [SDR DALA2019122907587](https://openairdocs.org/sdr/DALA2019122907587), Dec 28, 2019: SKIN. CORRODED. CORROSION FOUND JUST AFT OF LAV SVC PANEL. CORROSION ALSO NOTED FURTHER AFT AT PRESSURE DOME AREA. SKIN IS BULGED AND SEPARATED AT SEAM. AREA MARKED. BLENDED CO
- [SDR DALA2019071104157](https://openairdocs.org/sdr/DALA2019071104157), Jul 11, 2019: INLET. CONTAMINATED. WHILE BOARDING FLIGHT LEADER AND CAPT SMELLED BURNING OIL ORDER IN COCKPIT AND FWD CABIN FOUND OIL AROUND APU NON REM DOORS. T/S PER NO GO ODI FOUND APU INLET C
- [SDR DALA2019061293522](https://openairdocs.org/sdr/DALA2019061293522), Jun 7, 2019: DOOR FRAME. CRACKED. R/H FWD MAIN LANDING GEAR WHEEL FRAME IS CRACKED. ACCOMPLISHED SEC I TIME LIMITED REPAIR PER ER/A 578803-14 REV ORIGINAL. ASSOCIATED ER/A 14-578803. REPLACED R/
- [SDR DALA2019050902912](https://openairdocs.org/sdr/DALA2019050902912), May 9, 2019: LIGHT. DAMAGED. EMERGENCY LIGHT ASSY DAMAGED AT 32D. REPLACED LIGHT ASSY AT 32D OPS NL REF AMM 33-52. (LP5800382)
- [SDR DALA2019032301882](https://openairdocs.org/sdr/DALA2019032301882), Mar 22, 2019: CONNECTOR. DAMAGED. SEAT 13DE AND 21DE EMERGENCY PATH LIGHTS INOP. REPAIRED CONNECTORS, REF SWPM 20-90. NOW CHECKS GOOD. (LP5845377)
- [SDR DALA2019020420697](https://openairdocs.org/sdr/DALA2019020420697), Feb 1, 2019: DOOR FRAME. CORRODED. AWR. CORROSION ON LWR DOOR JAMB BTW STA 399 TO 415 AT FWD CARGO COMPARTMENT. REPAIR ON LWR DOOR JAMB BTW STA 399 TO 415 AT FWD CARGO COMPARTMENT WAS PERMORMED P
- [SDR DALA2019012900611](https://openairdocs.org/sdr/DALA2019012900611), Jan 28, 2019: SPACER. CORRODED. AWR. INITIAL INSPECTION. CORROSION ON SPACER IN LWR BEAM PREVIOUS REPAIR AT AFT CARGO DOOR CUT OUT LWR AREA. CORROSION LEVEL 2. SPACER ON BEAM PREVIOUS REPAIR A
- [SDR DALA2019010500062](https://openairdocs.org/sdr/DALA2019010500062), Jan 4, 2019: COOLING FAN. ODOR. BURNING SMELL WHEN INSTR COOLING FAN RUNNING PULL C/B ODOR GOES AWAY. C/W NO GO ODI PREV 2172 PER AMDS W/C 2120-2367. VERIFIED INST COOLING FAN IS BAD CAUSING T
- [SDR DALA2018072504672](https://openairdocs.org/sdr/DALA2018072504672), Jul 25, 2018: BATTERY. DISCHARGED. EMERGENCY LIGHTS DOOR 2 LEFT INOP. REMOVED AND REPLACED TWO EMERGENCY 'D' CELL BATTERIES FOR THE OVER EMERGENCY LIGHTS AT DOOR 2L. OPERATIONAL CHECK GOOD IAW AM
- [SDR DALA2018033002038](https://openairdocs.org/sdr/DALA2018033002038), Mar 30, 2018: ACTUATOR. FAILED. DURING CLIMB OUT, A NOISE AND VIBRATION FROM NOSE GEAR AREA INCREASED WITH AIRSPEED. RETURNED TO DEPARTURE. RIGHT NOSE GEAR DOOR FOUND OPEN. REPLACED RIGHT DOOR
- [SDR DALA2018030801468](https://openairdocs.org/sdr/DALA2018030801468), Mar 6, 2018: WIRE. SHORTED. ACARS PRINTER WIRE BUNDLE SHORTING ON AIRCRAFT STRUCTURE. PULLED & COLLARED ACARS PRINTER C/B F18. REMOVED ACARS PRINTER. FOUND 4 WIRES SHORTING TO GROUND. REPA
- [SDR DALA2017042503376](https://openairdocs.org/sdr/DALA2017042503376), Apr 25, 2017: CABLE. FRAYED. DURING TAILCONE INSPECTION FOUND CABLE FRAYED. R & R TAILCONE CABLE IAW AMM 53-53-0.
- [SDR DALA2016123010145](https://openairdocs.org/sdr/DALA2016123010145), Dec 30, 2016: SHAFT. WORN. WEAR ON L1 MECHANISM DOOR SHAFT ASSY P/N4915850-1. REPLACED SHAFT ASSY PER MD 88 AMM 26-62-00-201 , 52-11-01-201 (LP# 2828265)
- [SDR DALA2016123010142](https://openairdocs.org/sdr/DALA2016123010142), Dec 29, 2016: LONGERON. CRACKED. AFT ACCESORIES COMPARTMENT CRACK LONGERON 12R, BS 1431 BULKHEAD. REPAIRED IAW ETI-88-16-462 REV. 1 AND ER/A 552834-14.
- [SDR DALA2016122910128](https://openairdocs.org/sdr/DALA2016122910128), Dec 28, 2016: HOUSING. WORN. WEAR ON AFT CARGO DOOR HANDLE HOUSING. HOUSING WAS REMPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2016122710084](https://openairdocs.org/sdr/DALA2016122710084), Dec 26, 2016: PAN. CRACKED. CRACKED PAN BELOW STOP FITTING NR 2 ON FWD CARGO DOOR FWD EDGE. REPAIRED IAW ETI-88-16-480 REV. 2 AND ER/A 552866-14.
- [SDR DALA2016122410060](https://openairdocs.org/sdr/DALA2016122410060), Dec 23, 2016: DOOR FRAME. CRACKED. CRACKED FWD DOOR JAMB CHANNEL BS 937 AND RBL 5. RH MLG JAMB CHANNEL WAS REPAIRED IAW ERA 552882-14.
- [SDR DALA2016122310040](https://openairdocs.org/sdr/DALA2016122310040), Dec 22, 2016: DOUBLER. CORRODED. CORROSION ON AFT LAVATORY SERVICE PANEL INNER DOUBLER. THE DOUBLER WAS REPLACED IAW ER/A 552849-14 REV: ORIGINAL.
- [SDR DALA2016122210028](https://openairdocs.org/sdr/DALA2016122210028), Dec 21, 2016: PAN. CRACKED. CRACKED PAN BELOW STOP FITTING NR 2 ON FWD CARGO COMPARTMENT DOOR FWD EDGE. CRACKED PAN WAS REPAIRED IAW ER/A 552873-14 REV: ORIGINAL, MESSAGE 16-0778-08B AND E
- [SDR DALA2016122210027](https://openairdocs.org/sdr/DALA2016122210027), Dec 21, 2016: PAN. CRACKED. CRACK ON INNER PAN FWD LOWER CORNER AT FWD SERVICE DOOR. INNER PAN FWD LOWER CORNER AT FWD SERVICE DOOR WAS REPAIRED IAW ETI 88-16-483 REV.3 AND ER/A 552873-14 
- [SDR DALA2016122110002](https://openairdocs.org/sdr/DALA2016122110002), Dec 20, 2016: FRAME. CRACKED. AFT ACCESORIES COMPARTMENT, CRACK ON FRAME BS 1485 BETWEEN LONGERONS 15 - 16L. THE FRAME WAS REPAIRED IAW ER/A 552836-14 REV. ORIGINAL. MESSAGE 16-0739-04B AND 
- [SDR DALA2016122109995](https://openairdocs.org/sdr/DALA2016122109995), Dec 20, 2016: FLOOR PANEL. CRACKED. CRACKED CHANNEL ON CABIN FLOOR PANEL 769G. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05 PAR. 145 FIG.
- [SDR DALA2016122009971](https://openairdocs.org/sdr/DALA2016122009971), Dec 19, 2016: FORMER. CRACKED. FUSELAGE, CRACKED FORMER STA Y=907 AND X=-60 AT RT FILLET PANEL. FORMER WAS REPAIRED PER SRM 53-01 FIG 2.
- [SDR DALA2016121909968](https://openairdocs.org/sdr/DALA2016121909968), Dec 18, 2016: HINGE. DAMAGED. C2 CARGO DOOR, ELONGATED HOLES ON CARGO DOOR HINGES C2. HOLES WERE REWORKED PER ERA 497387-14MA REV B AND DOORS HINGES WAS REMOVED /INSTALLED PER AMM 52-31-02-2
- [SDR DALA2016121909939](https://openairdocs.org/sdr/DALA2016121909939), Dec 18, 2016: FRAME. CRACKED. AFT ACCESSORIES COMPARTMENT: CRACK ON FRAME STA Y=1485 CANT LONG 7R TO 9R. AREA WAS REPAIRED PER SRM 53-03 FIG. 49 AND SRM 51-30-2, 51-30-5 AND 51-30-1.
- [SDR DALA2016121909938](https://openairdocs.org/sdr/DALA2016121909938), Dec 18, 2016: HINGE. DAMAGED. ELONGATED HOLES ON HINGES AT AFT UPPER INBOARD SIDE OF THE FUSELAGE DOOR CARGO JAM. HINGES AT AFT UPPER INBOARD SIDE OF THE FUSELAGE DOOR CARGO JAMB WERE REPLAC
- [SDR DALA2016121809937](https://openairdocs.org/sdr/DALA2016121809937), Dec 17, 2016: SKIN. CORRODED. CORROSION ON TWO HOLES ON LWR ACCESS CUTOUT ADJACENT TO STRINGER 12 AT XRS=210 AT LT WING. LWR ACCESS CUT OUT WAS REPAIRED PER ER/A 552851-14AD REV ORIGINAL AND
- [SDR DALA2016121809936](https://openairdocs.org/sdr/DALA2016121809936), Dec 17, 2016: FLOOR PANEL. CRACKED. CRACKED CABIN FLOOR PANEL NR: 389A, 693A, 617G, 1079E, 256E AND 389G. FLOOR PANELS 256E, 389G AND 1079E WERE REPAIRED PER SRM 53-05 PAR 145 FIG 131C. FLOOR PANE
- [SDR DALA2016121809934](https://openairdocs.org/sdr/DALA2016121809934), Dec 17, 2016: FLOOR PANEL. CRACKED. CRACK ON GENERATION FLOOR PANEL NR: 541F, 927E, 1079A, 389A, 769A AND 256A. FLOOR PANELS 541F, 927E AND 256A WERE REPAIRED PER SRM 53-05 PAR 145 FIG 131B AND 13
- [SDR DALA2016121909969](https://openairdocs.org/sdr/DALA2016121909969), Dec 16, 2016: SKIN. PUNCTURED. PUNCTURE ON FWD CARGO COMPARTMENT DOOR INNER SKIN. FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER. ERA 094625-14.
- [SDR DALA2016121909941](https://openairdocs.org/sdr/DALA2016121909941), Dec 16, 2016: BULKHEAD. CORRODED. AFT ACCESSORY COMPARTMENT: CORROSION ON BULKHEAD, INTERCOSTALS, RT/LT CAP AND RT/LT BEAM AT AFT STAIRWAY WALKING BRIDGE. DUE EXCESSIVE CORROSION BULKHEAD NR 2 W
- [SDR DALA2016121709926](https://openairdocs.org/sdr/DALA2016121709926), Dec 16, 2016: INTERCOSTAL. CRACKED. AFT ACCESSORIES COMPARTMENT: CRACK ON INTERCOSTAL BTW STA Y=1485 CANT TO Y=1497 CANT BTW LONG PROJECTION 18L TO 22L. INTERCOSTAL WAS REPLACED PER DWG 9917701 RE
- [SDR DALA2016121609909](https://openairdocs.org/sdr/DALA2016121609909), Dec 16, 2016: CARGO TRACK. CORRODED. AFT CARGO BAY HAS CORROSION ON THE RT CARGO TRACK BETWEEN BS 1007 - 1155, AND BS 1212 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND DWG 5936660 REV. 
- [SDR DALA2016121609896](https://openairdocs.org/sdr/DALA2016121609896), Dec 15, 2016: SUPPORT. CORRODED. AFT CARGO COMPARTMENT: CORROSION ON ZEE SUPPORT ABOVE RT CARGO TRACK BETWEEN BS 1117 TO 1155. THE SUPPORT WAS REPLACED IAW SRM 51-30-1 , 51-30-5 AND DWG 5936660
- [SDR DALA2016121609900](https://openairdocs.org/sdr/DALA2016121609900), Dec 15, 2016: ACCESS PANEL. CORRODED. CORROSION ON SECONDARY ACCESS PANEL 1410C. THE ACCESS PANELS WAS REPLACED IAW 51-10-3.
- [SDR DALA2016121609899](https://openairdocs.org/sdr/DALA2016121609899), Dec 15, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PANEL 1333C . INSTALLED A NEW ACCESS PANEL IAW AMM 28-00-00.
- [SDR DALA2016121609898](https://openairdocs.org/sdr/DALA2016121609898), Dec 15, 2016: FRAME. CRACKED. AFT ACCESORIES COMPARTMENT HAD A CRACK ON FRAME BS 1510. THE FRAME WAS REPLACED IAW SRM 51-30-02.
- [SDR DALA2016121609897](https://openairdocs.org/sdr/DALA2016121609897), Dec 15, 2016: FLOOR PANEL. CORRODED. CORROSION ON FLOOR PANEL. REPAIRED IAW ER/A 504469-14MA.
- [SDR DALA2016121509885](https://openairdocs.org/sdr/DALA2016121509885), Dec 14, 2016: SPLICE. CRACKED. CRACKED SPLICE BS 988 AND LBL 7. REPAIRED IAW ER/A 413026-14MA.
- [SDR DALA2016121509880](https://openairdocs.org/sdr/DALA2016121509880), Dec 14, 2016: SKIN. BULGED. PROTUBERANCE ON LOWER SKIN OF RT WING OUTBD FLAP OUTBD GUIDE VANE AT XV2=321. REPAIRED IAW SRM 57-03 D PAR. 11 (LP#2808044)
- [SDR DALA2016121509879](https://openairdocs.org/sdr/DALA2016121509879), Dec 14, 2016: FINGER DOUBLER. CORRODED. CORROSION ON THE FINGER DOUBLER BETWEEN BS 1193 - 1309, LONGERONS 25 - 26L. FINGER DOUBLER WAS REPLACED IAW SRM 53-34-0 FIG, 3 AND 51-10-1 FIG 36.
- [SDR DALA2016121409850](https://openairdocs.org/sdr/DALA2016121409850), Dec 14, 2016: DOOR. CRACKED. RT WING HAS A CRACKED INBD FLIGHT SPOILER BUTTE DOOR XRS 184. REPAIR THE DOOR IAW SRM 51-70-4 FIG.1 (SHEET 1).
- [SDR DALA2016121409849](https://openairdocs.org/sdr/DALA2016121409849), Dec 13, 2016: FRAME. CRACKED. AFT ACCESORIES BAY HAS A CRACK ON THE FRAME LOWER CAP BS 1431 LONGERONS 11 & 12R. THE FRAME WAS REPAIRED IAW ER/A 552832-14 REV. ORIGINAL AND ETI-88-16-460 REV.
- [SDR DALA2016121409847](https://openairdocs.org/sdr/DALA2016121409847), Dec 13, 2016: CARGO TRACK. CORRODED. AFT CARGO BAY HAS CORROSION ON THE LT CARGO TRACK BS 1007 - 1322. REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2016121409845](https://openairdocs.org/sdr/DALA2016121409845), Dec 13, 2016: DOUBLER. CORRODED. FWD CARGO BAY HAS CORROSION ON A PREVIOUS REPAIR DOUBLER AT LOWER DOOR FRAME PAN BS 370 TO 427. THE REPAIR DOUBLERS WAS REPLACED IAW ER/A 526949-14 REV.ORIG. AN
- [SDR DALA2016121309794](https://openairdocs.org/sdr/DALA2016121309794), Dec 12, 2016: FRAME. CORRODED. AFT ACCESORIES COMPARTMENT, CORROSION ON FRAME BS 1393 LBL 3 TO LBL 10, BETWEEN LONGERONS 25 - 28L. AREA WAS REPAIRED IAW SRM 51-70-5 FIG 1.
- [SDR DALA2016121209787](https://openairdocs.org/sdr/DALA2016121209787), Dec 10, 2016: SKIN. NOT REPORTED. DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE) ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT LT WING. ATTENDED WITH ER/A 
- [SDR DALA2016121209786](https://openairdocs.org/sdr/DALA2016121209786), Dec 10, 2016: SKIN. NOT REPORTED. DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE) ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT RT WING. ATTENDED WITH ER/A 

All 182: https://openairdocs.org/deregistered/N910DE-2022-11-23/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 19930326008679I](https://openairdocs.org/incident/19930326008679I), Mar 26, 1993: Doug MD88 (N910DE), Lexington, KY, Minor damage. Spongy feeling of landing gear. Aborted. Found seam tar had been picked up by gear and thrown into NR2 engine.

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