# N919DE: 1993 Mcdonnell Douglas MD-88, registration cancelled 2019-08-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 22, 2019
- Status when cancelled: Valid registration
- 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: 53422
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 8, 1993
- Certificate issued: December 2, 1993
- Last registry action: February 21, 2019
- Mode S code: ACB86A
- 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/N919DE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=919DE
- Page: https://openairdocs.org/deregistered/N919DE-2019-08-22

From the FAA registry file of November 12, 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 (140, newest 50)

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

- [SDR DALA2018061904117](https://openairdocs.org/sdr/DALA2018061904117), Jun 19, 2018: DOOR. UNSECURE. CONDITIONED AIR GROUND CONNECT DOOR, FORWARD CONDITIONED AIR DOOR FELL OFF. DEFER FWD AC DOOR PER CDL 53-30-04A. DISP GRANTED. PLAC INSTALLED. (IN FWD CLOSET).
- [SDR DALA2018022601127](https://openairdocs.org/sdr/DALA2018022601127), Feb 24, 2018: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTS BETWEEN ROW 22-25 CEILING INOP. REPL BATTERY PACK PER AMM 33-53. OPS CHECK GOOD.
- [SDR DALA2018021500930](https://openairdocs.org/sdr/DALA2018021500930), Feb 15, 2018: BATTERY. DISCHARGED. FWD GALLEY EMERGENCY LIGHTS INOP. R&R BATTERIES IN FORWARD GALLEY LOC B5-23 PER AMM 33-53 OP CKS GOOD OK FOR SVC.
- [SDR DALA2017092107002](https://openairdocs.org/sdr/DALA2017092107002), Sep 12, 2017: TAB. DAMAGED. COMPOSITE EXPOSED ON RUDDER TAB. REMOVED THE TAB IAW AMDS 2720-4438 AND INSTALLED A NEW TAB IAW AMDS 2720-4321.
- [SDR DALA2017040502753](https://openairdocs.org/sdr/DALA2017040502753), Apr 4, 2017: BATTERY PACK. INOPERATIVE. FOUND OVERWING EXIT LIGHTS INOPERATIVE. REPLACED THE BATTERIES IAW AMM 33-53, LIGHTS CHECKED GOOD.
- [SDR DALA2017020200878](https://openairdocs.org/sdr/DALA2017020200878), Feb 1, 2017: FAN. FAILED. FLT LEVEL 340, FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL WITH A HAZE IN THE CABIN. AFTER THE SMELL REACHED THE COCKPIT, ELECTRICAL, WE DIVERTED TO CAE. FOUND R
- [SDR DALA2016110708340](https://openairdocs.org/sdr/DALA2016110708340), Nov 4, 2016: WIRE. CHAFED. AFT EMERGENCY LIGHT INOPERATIVE. FOUND CHAFED WIRE IN SERVICE LOOP. REMOVED THE PORTION OF WIRE AND SPLICED IAW AMM 20-50. LIGHTS OPERATE NORMAL.
- [SDR DALA2016102407529](https://openairdocs.org/sdr/DALA2016102407529), Oct 24, 2016: BATTERY PACK. DISCHARGED. EMERGENCY LIGHT INOP FROM ROW 31 TO TAIL. REPLACED BATTERY PACK. OPS CKS GOOD.
- [SDR DALA2016100307009](https://openairdocs.org/sdr/DALA2016100307009), Oct 1, 2016: FUSE. BLOWN. AFT SECTION EMERG LIGHTS INOP. REPLACED FUSE IN BATTERY PACK. OPS CK GOOD. REF WDM 33-51.
- [SDR DALA2016092606837](https://openairdocs.org/sdr/DALA2016092606837), Sep 24, 2016: FUSE. BLOWN. FOUND DURING SERVICE CHECK, AFT CABIN AND TAIL COMPARTMENT EMERGENCY LIGHTS WILL NOT TEST. REPLACED BLOWN FUSE AT POWER SUPPLY B5-212, POSITION 9, IAW WDM 33-51
- [SDR DALA2015092805843](https://openairdocs.org/sdr/DALA2015092805843), Sep 27, 2015: BATTERY PACK. INOPERATIVE. MAINTENANCE FOUND THE COCKPIT EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACKS WERE REPLACED.
- [SDR DALA2015083105340](https://openairdocs.org/sdr/DALA2015083105340), Aug 30, 2015: DOOR. NO TEST. LEFT AFT OVERWING EMERGENCY EXIT DOOR FAILED EXTERIOR DOOR HANDLE RELEASE TEST IAW W/C 5200-2643. DOOR RELEASES AS SOON AS EXTERIOR HANDLE TAB PRESSED WHILE HAN
- [SDR DALA2015083105339](https://openairdocs.org/sdr/DALA2015083105339), Aug 30, 2015: CONTAINER. CRACKED. DURING INSPECTION, MAINTENANCE FOUND TAILCONE EVACUATION SLIDE BASE PLATE CRACKED AT COVER ATTACH POINTS. THE CONTAINER ASSY WAS REPLACED IAW AMDS WORKCARD 2561
- [SDR DALA2015082705259](https://openairdocs.org/sdr/DALA2015082705259), Aug 26, 2015: FRAME. CRACKED. AFT FUESLAGE TAIL CONE AREA FRAME BS 1463, S25R FOUND A THREE INCH CRACK ON FRAME. REPAIRED IAW SRM 53-03D, FIG 38A.
- [SDR DALA2016041402903](https://openairdocs.org/sdr/DALA2016041402903), Mar 21, 2015: SKIN. DAMAGED. REMOVED RT WINGTIP ASSY IAW AMM 57-20. REPLACED RT WING TIP ASSY IAW AMM 57-20-02. OPS CHECKED GOOD. COMPLIED WITH ER/A 534223-14, REV ORIGINAL.
- [SDR DALA2015030902031](https://openairdocs.org/sdr/DALA2015030902031), Mar 7, 2015: PIN. SEIZED. DURING TAILCONE RELEASE SYS FUNCTIONAL CHECK, MAINTENANCE FOUND THE INTERIOR TAILCONE RELEASE CABLE RELEASE PIN SEIZED. MAINTENANCE R & R THE RELEASE CABLE RELE
- [SDR DALA2015030902030](https://openairdocs.org/sdr/DALA2015030902030), Mar 7, 2015: CABLE. WORN. MAINTENANCE FOUND KEVLAR CABLE ASSY WORN FOR TAILCONE ASSY. MAINTENANCE REPLACED THE KEVLAR CABLE ASSY, CHECKS OK. LP1853081.
- [SDR DALA2014092205208](https://openairdocs.org/sdr/DALA2014092205208), Sep 20, 2014: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY OVERHEAD LIGHTING AT THE OVERWING EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-104 AND
- [SDR DALA14030359019](https://openairdocs.org/sdr/DALA14030359019), May 15, 2014: CABLE. DETACHED. THE CREW DISCOVERED THE 1L DOOR GIRT BAR WIRE CABLE WAS NOT ATTACHED TO THE GIRT BAR. MAINTENANCE REINSTALLED THE GIRT BAR CABLE AND THE AIRCRAFT WAS RETURNED T
- [SDR DALA13044299019](https://openairdocs.org/sdr/DALA13044299019), Sep 12, 2013: SKIN. DAMAGED. WINDOW BELT FRAME FOUND CRACKED AT PREVIOUS LIGHTNING STRIKE BLEND. BS 541 TO 560 AREA C. NDT CONFIRMED 06-10-01-001. WORK ACCOMPLISHED ON PRI 518567-14. REPAIR
- [SDR DALA13044279019](https://openairdocs.org/sdr/DALA13044279019), Sep 11, 2013: SKIN. CRACKED. DURING SCHEDULED MX, A .7500 INCH SKIN CRACK WAS FOUND AT BS 1310, APPROXIMATELY 2.5 INCHES ABOVE THE EDGE OF THE SKIN PANEL NEAR LONGERON 7R. REPAIRED IAW ER/A
- [SDR DALA13034489019](https://openairdocs.org/sdr/DALA13034489019), Jul 11, 2013: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT DOOR L1 AND THE FIRST CLASS CABIN WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND
- [SDR DALA13024039019](https://openairdocs.org/sdr/DALA13024039019), May 21, 2013: PIN. LOOSE. DURING ROUTINE INSPECTION, THE INSPECTOR NOTED THAT THE NR 1 LEFT DOOR SLIDE PACKING PIN WAS LOOSE. THE SLIDE WAS REPLACED IAW AMM 25-62 AND THE REQUIRED INSPEC
- [SDR DALA12012279019](https://openairdocs.org/sdr/DALA12012279019), Nov 4, 2012: CABIN PRESSURE. MULTIPLE FAIL. CREW REPORTED THAT THE ACFT COMPLETELY LOSS PRESSURIZATION NEAR THE TOP OF DESCENT. PASSENGER OXYGEN MASKS DID DEPLOYED AND AN EMERGENCY DESCENT TO 10K WAS DECL
- [SDR DALA12011019019](https://openairdocs.org/sdr/DALA12011019019), Oct 23, 2012: BATTERY PACK. INOPERATIVE. DURING SERVICE CHECK, MX FOUND EMERGENCY PATHWAY LIGHTS INOPERATIVE FROM ROW 1 THROUGH 11 AND LT AND RT FORWARD ENTRY DOOR EXIT SIGNS OUT. REMOVED AND REINSTALL
- [SDR DALA12009699019](https://openairdocs.org/sdr/DALA12009699019), Oct 9, 2012: LANYARD. LOOSE. PILOT FOUND CABLE HANGING FROM FORWAD FO SIDE GALLEY DOOR. MX SECURED R1 DOOR GIRT BAR LANYARD. ACFT OK FOR SERVICE.
- [SDR DALA1242629019](https://openairdocs.org/sdr/DALA1242629019), Jul 22, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKES WERE FOUND ON FWD AND AFT EDGES OF LT WINDOW BELT FRAME BS 617-636. WINDOW BELT FRAME WAS BLENDED OUT AFT EDGES AND WITHIN LIMITS 
- [SDR DALA1242619019](https://openairdocs.org/sdr/DALA1242619019), Jul 22, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKES WERE FOUND ON AFT UPPER CORNER OF LT WINDOW BELT FRAME BS 617-636. WINDOW BELT FRAME AFT UPPER CORNER LOWER OUT OF CRITICAL ZONE 1
- [SDR DALA1243019019](https://openairdocs.org/sdr/DALA1243019019), Jul 21, 2012: SKIN. DENTED. FOUND DENT TO FUSELAGE, APPROXIMATELY 2 FEET AFT OF L1 DOOR COMPLIED WITH PERMANENT REPAIR TO FUSELAGE DENT PER SRM 53-04-5.
- [SDR DALA1242489019](https://openairdocs.org/sdr/DALA1242489019), Jul 20, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKE WAS FOUND ON WINDOW BELT FWD EDGE BS 788-807. WINDOW BELT WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504370-14 REV ORIG.
- [SDR DALA1242479019](https://openairdocs.org/sdr/DALA1242479019), Jul 20, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKE WAS FOUND ON LT WINDOW BELT FWD EDGE BS 826-845. WINDOW BELT WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW ERA 504370-14 REV ORI
- [SDR DALA1242469019](https://openairdocs.org/sdr/DALA1242469019), Jul 20, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKE WAS FOUND ON WINDOW BELT FRAME AFT LOWER CORNER BTW BS 693-674 RT SIDE. WINDOW BELT FRAME WAS BLENDED OUT AND REPAIR DOUBLER INSTAL
- [SDR DALA1242459019](https://openairdocs.org/sdr/DALA1242459019), Jul 20, 2012: BEAM. CORRODED. DURING HMV, CORROSION WAS FOUND ON MID CARGO COMPARTMENT LOWER BEAM BS 636-693 (C2). BEAM WAS BLENDED OUT AND BS 655 AND 674 WAS OUT OF LIMITS. THE AREA WAS CUT
- [SDR DALA1242439019](https://openairdocs.org/sdr/DALA1242439019), Jul 20, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKES WERE FOUND ON LT WINDOW BELT FRAME FWD UPPER CORNER. ALSO, AFT UPPER CORNER BS 655-674. WINDOW BELT FRAME WAS BLENDED OUT AND REPA
- [SDR DALA1242429019](https://openairdocs.org/sdr/DALA1242429019), Jul 20, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKE WAS FOUND ON LT WINDOW BELT FRAME AFT LOWER CORNER BS 807-826. WINDOW BELT FRAME WAS BLENDED OUT AND REPAIR DOUBLER WAS INSTALLED B
- [SDR DALA1242419019](https://openairdocs.org/sdr/DALA1242419019), Jul 20, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKES WERE FOUND ON LT WINDOW BELT FRAME LOWER AFT CORNER. ALSO LOWER FORWARD CORNER BS 541-560 WINDOW BELT FRAME WAS BLENDED OUT IAW ER
- [SDR DALA1242409019](https://openairdocs.org/sdr/DALA1242409019), Jul 20, 2012: SKIN. DAMAGED. DURING HMV, LIGHTNING STRIKES WERE FOUND ON WINDOW BELT FRAME ON FWD LOWER CORNER. ALSO ON AFT UPPER CORNER BTW BS 1193 AND 1212. WINDOW BELT FRAME WAS BLENDED 
- [SDR DALA1242399019](https://openairdocs.org/sdr/DALA1242399019), Jul 20, 2012: SKIN. CORRODED. DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN IN BS 782 BETWEEN LONGERON 28R-29R. FUSELAGE SKIN WAS BLENDED OUT AND REPAIR DOUBLER INSTALLED IAW 53-04 PARA 5
- [SDR DALA1242389019](https://openairdocs.org/sdr/DALA1242389019), Jul 20, 2012: SKIN. CORRODED. DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN BS 803 AND LONGERON 29R. FUSELAGE SKIN WAS BLENDED OUT AND DOUBLER REPAIR INSTALLED IAW MD88 SRM 53-04 PARA 57.
- [SDR DALA1242319019](https://openairdocs.org/sdr/DALA1242319019), Jul 19, 2012: ANGLE. DAMAGED. DURING HMV, TOOLING MARKS WERE FOUND ON PRESSURE DOME LOWER TEE ANGLE AT BS 1338 BETWEEN LONGERON 26 LT AND 26 RT. REMOVED DAMAGE TEE ANGLE BETWEEN LONGERON 25 
- [SDR DALA1242309019](https://openairdocs.org/sdr/DALA1242309019), Jul 19, 2012: STRUCTURE. CORRODED. DURING HMV, CORROSION WAS FOUND ON REPAIR SPLICE OF LONGERON 28 LT AND 29 LT BTW STA Y=1250-1271 AT AFT CARGO COMPARTMENT LONGERON 28L WAS ATTENDED ON NRC 25417
- [SDR DALA1242299019](https://openairdocs.org/sdr/DALA1242299019), Jul 19, 2012: SKIN. CRACKED. DURING HMV, CRACKED FUSELAGE SKIN WAS FOUND BTW BS 1497 - 1501 LONGERONS 17-18L. DAMAGE AREA WAS CUT OUT AND SHIM DOUBLER REPAIR INSTALLED IAW SRM 53-04-3 FIG 2
- [SDR DALA1242089019](https://openairdocs.org/sdr/DALA1242089019), Jul 18, 2012: LONGERON. CORRODED. DURING HMV, CORROSION WAS FOUND ON LONGERON 24 LT STA Y=1290, LONGERON WAS REMOVED FROM BS 1275-1328. REPAIR LONGERONS AND SPLICES INSTALLED IAW SRM 53-02 FIG 1
- [SDR DALA1242079019](https://openairdocs.org/sdr/DALA1242079019), Jul 18, 2012: LONGERON. CORRODED. DURING HMV, CORROSION WAS FOUND ON LONGERON 27 LT FROM BS 1257-1330 AND LONGERON 28 LT. DAMAGE SECTION WAS REMOVED BS 1204-1330 AND REPAIRED IAW SRM 53-02 FIG 1
- [SDR DALA1242069019](https://openairdocs.org/sdr/DALA1242069019), Jul 18, 2012: SKIN. CORRODED. DURING HMV, CORROSION WAS FOUND ON FUSELAGE SKIN BELOW WING TO FUSELAGE FILLET PANEL RUBSTRIPS ON BS 727-826 BETWEEN LONGERONS 16-30L AND BS 826-864 BETWEEN LON
- [SDR DALA1242059019](https://openairdocs.org/sdr/DALA1242059019), Jul 18, 2012: LONGERON. CORRODED. DURING HMV, CORROSION WAS FOUND ON LONGERON 22 LT BTW BS 1277 TO 1335. DAMAGE LONGERON WAS REMOVED AND REPAIR LONGERON AND SPLICE INSTALLED IAW SRM 53-02 FIG 18
- [SDR DALA1242049019](https://openairdocs.org/sdr/DALA1242049019), Jul 18, 2012: LONGERON. CORRODED. DURING HMV, CORROSION WAS FOUND ON LONGERON 23L IN BS 1287 AT AFT CARGO COMPARTMENT. DAMAGE LONGERON WAS REMOVED7 AND REPAIR SPLICE INSTALLED IAW SRM 53-02 FIG 
- [SDR DALA1240879019](https://openairdocs.org/sdr/DALA1240879019), Jul 9, 2012: LONGERON. DAMAGED. DURING HMV, WEAR WAS FOUND ON STRAP AND LONGERON 8 RT AT BS 1401-1418. DAMAGED LONGERON 8 RT STA Y=1406-1429 AND SPLICE WAS REMOVED AND REPAIRED. PARTS INSTALLE
- [SDR DALA1240489019](https://openairdocs.org/sdr/DALA1240489019), Jul 8, 2012: SKIN. DENTED. DENT ON FUSELAGE AFT OF L1 DOOR APPROXIMATELY 2 FT AFT OF DOOR AT STA Y=239. REPAIRED FUSELAGE SKIN IAW WITH SRM 53-04-5 AND ERA 483596-14 REV ORIG.
- [SDR DALA1159329019](https://openairdocs.org/sdr/DALA1159329019), Oct 21, 2011: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT ANGLE CORRODED RBL 44 AT STA 148 AND 160. INSTALLED FLOOR SUPPORT ANGLE AT RBL 44 AT STA 148 - 160 IAW DC9/MD80 SRM 51-10-4 PG 1 MD80 SRM 51-30-5 

All 140: https://openairdocs.org/deregistered/N919DE-2019-08-22/reports.md

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