# N911DE: 1992 Mcdonnell Douglas MD-88, registration cancelled 2022-06-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 13, 2022
- Status when cancelled: Second renewal notice
- Airframe: [Mcdonnell Douglas MD-88](https://openairdocs.org/model/mcdonnell-douglas-md-88) (registry code 3023688)
- 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: 49967
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: December 15, 1992
- Certificate issued: January 26, 1993
- Last registry action: February 22, 2019
- Mode S code: AC9AB2
- 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/N911DE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=911DE
- Page: https://openairdocs.org/deregistered/N911DE-2022-06-13

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 (159, newest 50)

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

- [SDR DALA2020030701695](https://openairdocs.org/sdr/DALA2020030701695), Mar 7, 2020: FRAME. CRACKED. REAR FRAME CRACK AT 0300 POSITION - TAILLCONE MOUNTING FRAME. DRILLED UP NEW FRME P/N 59667694501, READY FOR INSTALLATION. STARTED INSTALLATION OF FRAME IAW MD8
- [SDR DALA2020030701694](https://openairdocs.org/sdr/DALA2020030701694), Mar 7, 2020: FRAME. CRACKED. REAR FRAME CRACKED AT 0700 POSITION - TAILCONE MOUNT FRAME. DRILLED UP NEW FRAME P/N 59667691. INSTALLED NEW FRAME PER MD 88 SRM 51-30-02. (LP1519795)
- [SDR DALA2020030701692](https://openairdocs.org/sdr/DALA2020030701692), Mar 7, 2020: LATCH. OUT OF ADJUST. TAILCONE RELEASE TEST FAILED USING AFT BULKHEAD DOOR. ADJUSTED RIGHT UPPER AND LEFT LOWER TAILCONE LATCHES PER MD88 AMM 5353 OPS CHK NML. (LP1519691)
- [SDR DALA2020030701693](https://openairdocs.org/sdr/DALA2020030701693), Mar 4, 2020: LATCH. WORN. TAILCONE ATTACH LATCH @0800 POSITION LOOSE AND WORN. REPLACED TAILCONE ATTACH LATCH AT 0800 POSITION PER MD88 AMM 53-53 NEEDS ADJUSTMENT AT TAILCONE INST.(48175
- [SDR DALA2020022501396](https://openairdocs.org/sdr/DALA2020022501396), Feb 25, 2020: BATTERY PACK. INOPERATIVE. OVERHEAD EMER LIGHTS OUT FROM SEATS 11-15. R/R EMER BATT PACK BATTERIES PER MD88 AMM 33-53. (LP6465677)
- [SDR DALA2019042502628](https://openairdocs.org/sdr/DALA2019042502628), Apr 24, 2019: CONNECTOR. DISCONNECTED. FOUND EMERGENCY LIGHTS OUT ON SEAT 35 DE AND 25 DE. RECONNECTED THE QUICK DISCONNECTS ON THE EMERGENCY LIGHTS FOR SEATS 25 AND 35 DE. OPS CHECK GOOD. (LP4893432
- [SDR DALA2019040202076](https://openairdocs.org/sdr/DALA2019040202076), Apr 2, 2019: CABLE. TORN. AWR IN REFERENCE AMDS 5350-4287 STEP 4 TORN ON TAILCONE KEVLAR CABLE WAS FOUND. KEVLAR CABLE WAS REPLACED PER MD-88 AMM 20-30-01 AND MD-88 AMM 20-10-17-201. (LP
- [SDR DALA2019040202075](https://openairdocs.org/sdr/DALA2019040202075), Apr 1, 2019: DOUBLER. CORRODED. CORROSION ON PRODUCTION DOUBLER AT AFT LAVATORY PANEL. DUE TO CORROSION OUT OF LIMITS PRODUCTION DOUBLER AT AFT LAVATORY PANEL WAS REPAIRED AS A TIME LIMITED RE
- [SDR DALA2019033002043](https://openairdocs.org/sdr/DALA2019033002043), Mar 30, 2019: SKIN. DAMAGED. INITIAL INSPECTION: CREASE ON FUSELAGE SKIN BTW STA Y=1265 AND Y =1277 BTW LONG 27L AND 28R. FUSELAGE SKIN BTW STA Y=1265 AND Y=1277 BTW LONG 27L AND 28R WAS RE
- [SDR DALA2019032901991](https://openairdocs.org/sdr/DALA2019032901991), Mar 28, 2019: PAINT. DAMAGED. INITIAL INSPECTION: MISSING AND DAMGE PAINT ON RUDDER CONTROL TAB. TAB WAS REMOVED/INSTALLED PER AMM 27-20-02-401. PAINTED PER P.S. 900-3-6-NO36 AND BALANCED PE
- [SDR DALA2019033102056](https://openairdocs.org/sdr/DALA2019033102056), Mar 27, 2019: SKIN. DENTED. FUSELAGE SKIN STA Y=1250-1287 & L27L TO L28R DENTS & SCRATCHES. ACCOMPLISH ER/A 576844-14 SECTION II INSPECTION WITHIN EVERY 8000 CYCLES AFTER ACCOMPLISHMENT OF
- [SDR DALA2019033102055](https://openairdocs.org/sdr/DALA2019033102055), Mar 26, 2019: SKIN. DAMAGED. FUSELAGE SKIN AFT LAV SERVICE DOOR CUTOUT STA Y=1307-1322, L-22L SKIN & INTERNAL DOUBLER/ CORROSION. ACCOMPLISH ER/A 576847-14 SECTION II INSPECTION WITHIN EVER
- [SDR DALA2019010200014](https://openairdocs.org/sdr/DALA2019010200014), Jan 1, 2019: COALESCER BAG. DIRTY. AFTER T/O AND GEAR RETRACTION STRONG SMELL FROM NOSE TIRES NOTICED IN FLT DECK AND MAIN CABIN. C/W ODI SMOKE /ODOR T/S WC 2120-2367 PERFORMED ALTERNATE DUCT BUR
- [SDR DALA2018051603379](https://openairdocs.org/sdr/DALA2018051603379), May 14, 2018: WARNING SYSTEM. FALSE ACTIVATION. DUE TO EMERGENCY DECLARED BECAUSE OF TOO LOW GEAR AURAL WARNING FOR GEAR WARNING DURING APPROACH. T/S THE EGPWS AND RADIO ALTIMETER SYSTEMS PER AMM 34-45 AND 34
- [SDR DALA2018043002896](https://openairdocs.org/sdr/DALA2018043002896), Apr 29, 2018: SLIDE. TORN. SERVICE DOOR SLIDE NOTED TO BE TORN. REPLACED R1 SLIDE PACK.
- [SDR DALA2018040402179](https://openairdocs.org/sdr/DALA2018040402179), Apr 4, 2018: DOOR FRAME. DIRTY. FORCE REQUIRED TO OPEN THE DOOR AND DROP THE TAILCONE. AFT PASSENGER DOOR OUT OF LIMITS IAW AMDS 88- 0553-8-0066, AMDS 5350-01077-0101 STEP 7. CLEANED DEBRIS FR
- [SDR DALA2018010300035](https://openairdocs.org/sdr/DALA2018010300035), Jan 2, 2018: BATTERY. DISCHARGED. EMERGENCY CEILING LIGHTS IN TAIL INOP. BATTERIES WOULD NOT HOLD CHARGE. CHANGED 'D' CELL BATTERIES OPERATIONAL CHECK OF TAIL PATH CEILING LIGHTS GOOD IAW AMM 33
- [SDR DALA2017081506259](https://openairdocs.org/sdr/DALA2017081506259), Aug 13, 2017: UNKNOWN. ODOR. DIVERTED DUE TO A REPORTED SWEET BURNING ODOR FROM OVERHEAD BINS AT SEAT ROWS 12 TO 20. NO ODOR WAS PRESENT IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT I
- [SDR DALA2017052704330](https://openairdocs.org/sdr/DALA2017052704330), May 27, 2017: WIRE. BROKEN. EMERGENCY LIGHTING INOPERATIVE AT 24DE. FOUND WIRE BROKEN ON HARNESS. REPAIRED THE WIRE HARNESS IAW SWPM 20. ALL LIGHTS OPS CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017052704329](https://openairdocs.org/sdr/DALA2017052704329), May 27, 2017: BATTERY PACK. INOPERATIVE. EMERGENCY CEILING LIGHTS INOPERATIVE BETWEEN ROWS 26 AND 30. REPLACED THE BATTERIES AT ROW 28. OPS CHECKED GOOD IAW AMM 33-53.
- [SDR DALA2017050803634](https://openairdocs.org/sdr/DALA2017050803634), May 6, 2017: CONNECTOR. BROKEN. DURING SERVICE CHECK, FOUND SEAT 22 EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR BROKEN. INSTALLED A NEW CONNECTOR IAW SWPM 20. OPS CHECKED OK. OK FOR SERVICE.
- [SDR DALA2017050803633](https://openairdocs.org/sdr/DALA2017050803633), May 6, 2017: WIRE. BROKEN. DURING SERVICE CHECK, FOUND AFT CATWALK MIDDLE EMERGENCY LIGHT INOPERATIVE. WIRE BROKEN FROM CONNECTOR. INSTALLED NEW TERMINAL PIN IAW SWPM 20. OPS CHECKED OK. 
- [SDR DALA2017050203523](https://openairdocs.org/sdr/DALA2017050203523), May 1, 2017: COFFEEMAKER. MALFUNCTIONED. ON ENTERING THE ACFT, A STRONG ELECTRICAL BURNING ODOR. TROUBLESHOT IAW IAW 2120-2367. FOUND F/C FWD NR 1 COFFEEMAKER HEATING WITH SWITCH IN OFF POSITION CREATI
- [SDR DALA2017030201713](https://openairdocs.org/sdr/DALA2017030201713), Mar 1, 2017: RELEASE CABLE. BROKEN. AFT ACCESSORIES COMPARTMENT: BROKEN RELEASE TAILCONE CONTROL CABLE WIRES AT 10 HRS POSITION. RELEASE TAILCONE CONTROL CABLE AT 10 HRS POSITION WAS REPLACED AND 
- [SDR DALA2017030101644](https://openairdocs.org/sdr/DALA2017030101644), Feb 26, 2017: OUTFLOW VALVE. CRACKED. CRACK ON OUTFLOW VALVE BUTTERFLY. DAMAGED OUTFLOW BUTTERFLY VALVE WAS REMOVED IAW AMM 21-32-05 401.
- [SDR DALA2017022701583](https://openairdocs.org/sdr/DALA2017022701583), Feb 26, 2017: RIB. CRACKED. LEFT WING HAD A CRACKED RIB ON SLAT PANEL NR 3 AT XOS 332. THE SLAT PANEL WAS REPLACED, INSTALLED AND ADJUSTED IAW AMM 27-80-01.
- [SDR DALA2017022701580](https://openairdocs.org/sdr/DALA2017022701580), Feb 26, 2017: SKIN. CRACKED. DAMAGE TEE FITTING DURING PERFORMING OF AMDS CARD 5200-2503 STEP 2 (F), ONE CRACK WAS FOUND TO THE LT AFT EMERGENCY EXIT DOOR INNER SKIN. REPAIRED IAW ETI-88-17
- [SDR DALA2017022701579](https://openairdocs.org/sdr/DALA2017022701579), Feb 25, 2017: PAN. CRACKED. CRACK ON RT EMERGENCY EXIT DOOR FRAME PAN UPPER AREA BS 864 TO 880. DAMAGE AREA WAS REPAIRED IAW ETI-88-17-063 REV 5, ER/A 554155-14 REV. ORIG. AND SRM 53-05 FI
- [SDR DALA2017022601577](https://openairdocs.org/sdr/DALA2017022601577), Feb 25, 2017: FRAME. CRACKED. AFT ACCESORIES COMPARTMENT HAD A CRACKED FRAME BS 1485. THE FRAME WAS REPAIRED IAW SRM 53-03D, FIG 43.
- [SDR DALA2017022601576](https://openairdocs.org/sdr/DALA2017022601576), Feb 25, 2017: SHEAR TIE. CRACKED. AFT ACCESORIES COMPARTMENT HAD A CRACKED SHEAR TIE BS 1380 BETWEEN LONGERONS 17 & 18R. THE SHEAR TIE WAS REPLACED IAW SRM 53-14-4, 51-30-2, AND 51-30-5.
- [SDR DALA2017022601575](https://openairdocs.org/sdr/DALA2017022601575), Feb 25, 2017: RIB. CRACKED. LEFT WING RIB CRACKED ON FIXED LEADING EDGE APROX XRS 295. THE RIB WAS REPLACED IAW SRM 51-30-2, 51-30-5.
- [SDR DALA2017022301488](https://openairdocs.org/sdr/DALA2017022301488), Feb 22, 2017: ANGLE. CRACKED. L1 DOOR HAS A CRACKED ANGLE ON FWD INTERCOSTAL BETWEEN BEAMS 4 AND 5. THE ANGLE WAS REPLACED IAW SRM 51-30-2 AND DWG 9955763 REV. M.
- [SDR DALA2017022301486](https://openairdocs.org/sdr/DALA2017022301486), Feb 22, 2017: ACCESS PANEL. DAMAGED. ELONGATED HOLES ON FUEL TANK ACCESS PANEL1365C. REPAIRED IAW SRM 51-22-2A PAR. 6.
- [SDR DALA2017022201453](https://openairdocs.org/sdr/DALA2017022201453), Feb 21, 2017: FRAME. CRACKED. AFT ACCESSORIES COMPARTMENT, CRACKED FRAME ON STA Y=1485 CANT. DAMAGE AREA WAS REPAIRED PER ETI-88-17-065 REV 1 AND ER/A 555626-14 RE ORIG.
- [SDR DALA2017022201451](https://openairdocs.org/sdr/DALA2017022201451), Feb 21, 2017: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORTS BTW STA Y=1145 AND Y= 1222 BTW LONG 28 RT AND 29 RT. DUE TO EXCESSIVE CORROSION UPPER FLOOR SUPPORT WAS REPLACED PER SRM 51-30-1, 51
- [SDR DALA2017022201448](https://openairdocs.org/sdr/DALA2017022201448), Feb 21, 2017: CARGO TRACK. CORRODED. CORROSION ON LT TIE DOWN TRACK FROM STA Y=1117 TO STA Y=1122 IN AFT CARGO COMPARTMENT. TIE TRACK WAS REPLACED PER DRAWING 5936660 REV BZ AND SRM 51-30-1, 51-30-
- [SDR DALA2017022201447](https://openairdocs.org/sdr/DALA2017022201447), Feb 21, 2017: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT, CORROSION ON FLOOR SUPPORT STA Y= 1117 BTW LONG 28LH AND 28 RT. FLOOR SUPPORT WAS REPLACED PER , SRM.51-30-5. (LP2900754)
- [SDR DALA2017021901353](https://openairdocs.org/sdr/DALA2017021901353), Feb 18, 2017: FINGER DOUBLER. CORRODED. AFT CARGO BAY HAS CORROSION ON A FINGER DOUBLER BETWEEN LONGERONS 28L AND 28R, BS 1231 - 1271. THE FINGER DOUBLERS WERE REPLACED IAW SRM 53-04-3, FIG. 12.
- [SDR DALA2017021801352](https://openairdocs.org/sdr/DALA2017021801352), Feb 17, 2017: DOUBLER. CORRODED. AFT CARGO BAY CORROSION ON PREVIOUS REPAIR DOUBLER OF LOWER DOOR FRAME BEAM. THE REPAIR WAS REPLACED IAW SRM 53-05, FIG 123, ETI-88-17-048 REV. ORIGINAL AND ERA
- [SDR DALA2017021701317](https://openairdocs.org/sdr/DALA2017021701317), Feb 16, 2017: ACCESS PANEL. CORRODED. CORROSION ON FUEL TANK ACCESS PANELS 1410C AND 1303C. THE ACCESS PANELS WERE REPLACED.
- [SDR DALA2017021701312](https://openairdocs.org/sdr/DALA2017021701312), Feb 16, 2017: INTERCOSTAL. CRACKED. RIGHT MLG WHEEL WELL HAS A CRACKED INTERCOSTAL BELOW THE HYD HAND PUMP. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01, FIG 2.
- [SDR DALA2017021701310](https://openairdocs.org/sdr/DALA2017021701310), Feb 16, 2017: WEB. CRACKED. AFT ACCESORIES COMPARTMENT HAS A CRACKED WEB BS 1437, LONGERIN 8 - 9L. THE WEB WAS REPAIRED IAW ETI-88-17-058 REV 1, AND ER/A 554147-14 REV. ORIG.
- [SDR DALA2017021701308](https://openairdocs.org/sdr/DALA2017021701308), Feb 16, 2017: SKIN. CRACKED. LEFT WING CRACKED ON LOWER SKIN BUTE DOOR, XCW 104. THE BUTE DOOR WAS REPAIRED IAW SRM 51-70-4, FIG 1, 51-30-2 AND 51-30-1.
- [SDR DALA2017021701307](https://openairdocs.org/sdr/DALA2017021701307), Feb 16, 2017: FLOOR PANEL. CORRODED. METALLIC FLOOR PANEL UNDER FIRST OFICCER SEAT CORRODED. A NEW FLOOR PANEL WAS DRILLED IAW SRM 51-10-4 AND A NEW FLOOR PANEL WAS INSTALLED.
- [SDR DALA2017021601279](https://openairdocs.org/sdr/DALA2017021601279), Feb 15, 2017: ACCESS PANEL. CORRODED. CORROSION ON FUEL TANK ACCESS NR 1414C RT. FUEL TANK ACCESS NR 1414C WAS REPLACED PER SRM 51-22-2A PAR 6.
- [SDR DALA2017021501238](https://openairdocs.org/sdr/DALA2017021501238), Feb 14, 2017: WEB. CORRODED. ELONGATED HOLE ON WEB ON AFT SERVICE DOOR INNER STRUCTURE. REPAIRED IAW ETI-88-17-060 REV 1 AND ERA 554151-14 REV ORIG.
- [SDR DALA2017021501234](https://openairdocs.org/sdr/DALA2017021501234), Feb 14, 2017: WEB. CRACKED. CRACKED WEB BS 1463, LONGERONS 7 - 8L. THE WEB SECTION WAS REPLACED IAW SRM 53-14-4 FIG 3, AND 51-30-5.
- [SDR DALA2017021401193](https://openairdocs.org/sdr/DALA2017021401193), Feb 13, 2017: FLOOR PANEL. CRACKED. CRACK ON FLOOR PANEL. THE FLOOR PANEL WAS REPAIRED IAW AMM 25-00-00-801 AND SRM 53-01 FIG. 2.
- [SDR DALA2017021401192](https://openairdocs.org/sdr/DALA2017021401192), Feb 13, 2017: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB FROM BS 1117 - 1174, RBL 44 - 60. THE CUSP WEB WAS REPLACED IAW SRM 51-30-2, AND 51-30-5.
- [SDR DALA2017021201165](https://openairdocs.org/sdr/DALA2017021201165), Feb 11, 2017: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB FROM STA Y=663 TO STA Y=665U AND BTW X=-54 TO X=-60 PER AND LOWER SURFACE. DAMAGE AREA WAS REPAIRED SRM 53-05 FIG 131 A.

All 159: https://openairdocs.org/deregistered/N911DE-2022-06-13/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 20000503033649I](https://openairdocs.org/incident/20000503033649I), May 3, 2000: Doug MD88 (N911DE), Shreveport, LA, Minor damage. (-23)Delta flight 555, MD-80, landed at Shreveport Regional, taxing in after landing, turned too sharp off taxiway to ramp and the nose gear and left main…

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