# N914DE: 1993 Mcdonnell Douglas MD-88, registration cancelled 2019-09-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 16, 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: 49957
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 30, 1993
- Certificate issued: March 1, 1993
- Last registry action: August 13, 2019
- Mode S code: ACA5D7
- 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/N914DE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=914DE
- Page: https://openairdocs.org/deregistered/N914DE-2019-09-16

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 (79, newest 50)

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

- [SDR DALA2017061804799](https://openairdocs.org/sdr/DALA2017061804799), Jun 17, 2017: LIGHT. INOPERATIVE. EMERGENCY LIGHTS ON CATWALK INOP. RELAMPED LIGHT ASSY 2EA. LOCATIONS, CATWALK PER AMM 33-52. CHECKS OK.
- [SDR DALA2017032802520](https://openairdocs.org/sdr/DALA2017032802520), Mar 26, 2017: FRAME. CRACKED. DURING A WALKAROUND, RAMP REPORTED MID CARGO DOOR HARD TO OPEN. FOUND MID CARGO DOOR LOWER FRAME CRACKED 4-6 INCHES ALONG RIVET ROW WHERE SKIN ATTACHES. REPAIRE
- [SDR DALA2016102707747](https://openairdocs.org/sdr/DALA2016102707747), Oct 26, 2016: COVER. UNSERVICEABLE. TAIL CONE SLIDE COVER IS NOT SERVICEABLE. REPLACED SLIDE COVER IAW AMDS WC 5350-4644.
- [SDR DALA2016102707746](https://openairdocs.org/sdr/DALA2016102707746), Oct 26, 2016: SLIDE. DETACHED. TAILCONE SLIDE IS DETACHED FROM PACKAGING. INSTALLED SLIDE ON AMDS 5350-4644.
- [SDR DALA2016102607733](https://openairdocs.org/sdr/DALA2016102607733), Oct 26, 2016: CABLE. CHAFED. TAILCONE CABLE HAS AREA OF WEAR AND CHAFING. REPLACED THE CABLE.
- [SDR DALA2016102607595](https://openairdocs.org/sdr/DALA2016102607595), Oct 25, 2016: SPAR. CRACKED. RT WING AT STATION XRS 164 IS CRACKED AT APPROX 6:00 POSITION AT LOWER LUG, CRACK IS APPROX .250" LONG. RT WING AFT SPAR AT STA XRS164 REPAIRED BY DOUBLER INSTA
- [SDR DALA2016102407545](https://openairdocs.org/sdr/DALA2016102407545), Oct 24, 2016: DOOR. OUT OF ADJUST. FIRST CLASS LAV, OXYGEN COMPARTMENT DOOR BINDING DOES NOT FREELY DROP. ADJUSTED DOOR PER CMM 35-10-11. OPS CHECK GOOD.
- [SDR DALA2016101907354](https://openairdocs.org/sdr/DALA2016101907354), Oct 18, 2016: HINGE FITTING. CORRODED. NR 2 RT FLAP HINGE UPPER INBD AND LOWER INBD MOUNTING STUDS CORRODED. REPLACED THE HINGE FITTING AND UPPER & LOWER MOUNTING STUDS IAW AMDS 5710-01110-05B.
- [SDR DALA2016082206138](https://openairdocs.org/sdr/DALA2016082206138), Aug 21, 2016: BATTERY. DISCHARGED. AFT OVERHEAD COCKPIT EMERGENCY LIGHTS INOPERATIVE. ATTEMPTED RELAMP. R & R BATTERY. OPS NORMAL, OK FOR SERVICE IAW AMM 33-53.
- [SDR DALA2016071805382](https://openairdocs.org/sdr/DALA2016071805382), Jul 18, 2016: WIRE HARNESS. DAMAGED. SEAT MOUNTED EMERGENCY LIGHT AT SEAT 20DE INOPERATIVE. REPLACED THE WIRE HARNESS AND PIG TAIL AT SEAT 20DE IAW AMM 33-50. OPS CHECKED GOOD.
- [SDR DALA2016061404686](https://openairdocs.org/sdr/DALA2016061404686), Jun 14, 2016: LIGHT. INOPERATIVE. RIGHT EXTERIOR OVERWING EXIT LIGHT INOPERATIVE. INSTALLED NEW BULB IN EXTERIOR OVERWING EXIT LIGHT. OPS CK OK. OK FOR SERVICE.
- [SDR DALA2016061404685](https://openairdocs.org/sdr/DALA2016061404685), Jun 14, 2016: BATTERY. DISCHARGED. LEFT AND RIGHT OVERWING EXIT DOORS AFT, OVERHEAD INTERIOR EXIT SIGN INOPERATIVE. INSTALLED NEW BATTERY IN BATTERY PACK FOR AFT OVERWING DOORS UPPER EXIT SIGNS. 
- [SDR DALA2016052504224](https://openairdocs.org/sdr/DALA2016052504224), May 25, 2016: APU. SMOKE. PERFORMED ATB DUE TO REPORTED SMOKE IN CABIN ON CLIMB OUT. AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE APU AND PERFORMED PACK SYSTEM INSPECTION/CLEANING
- [SDR DALA2016032502383](https://openairdocs.org/sdr/DALA2016032502383), Mar 24, 2016: BOTTLE. LOW PRESSURE. THE CREW REPORTED THAT THE L1 EMERGENCY ESCAPE SLIDE PRESSURE WAS LOW. MAINTENANCE R & R THE L1 EMERGENCY EXCAPE SLIDE.
- [SDR DALA2016020800927](https://openairdocs.org/sdr/DALA2016020800927), Feb 5, 2016: DOOR FRAME. CRACKED. RIGHT WHEEL WELL FWD FRAME MLG DOOR JAMB HAS CRACK IN OTBD RADIUS 3" LONG. R & R FWD FRAME IAW DWG 5930584. COMPLETED INSTALLING FWD FRAME IAW DWG 5930584. INST
- [SDR DALA2016020800926](https://openairdocs.org/sdr/DALA2016020800926), Feb 5, 2016: DOOR FRAME. CRACKED. LEFT WHEEL WELL FWD FRAME MLG DOOR JAMB HAS CRACK IN OTBD RADIUS 3.5" LONG. REMOVED AND DRILLED NEW FWD FRAME IAW DWG 5930584. BEGAN INSTALLING FRAME IAW DWG 59
- [SDR DALA2016010800107](https://openairdocs.org/sdr/DALA2016010800107), Jan 8, 2016: WIRE. DAMAGED. MAINTENANCE FOUND AFT EXIT SIGN IN TAIL SECTION INOPERATIVE. A WIRE WAS REPAIRED AND SIGN CHECKED OK.
- [SDR DALA2017061604775](https://openairdocs.org/sdr/DALA2017061604775), Aug 28, 2014: CHANNEL. DAMAGED. LEFT WING OTBD FLAP AFT HINGE FAIRING CHANNEL HAS AN ELONGATED HOLE, REPAIRED IAW ERA 525967-14, REV ORIG
- [SDR DALA2014082704847](https://openairdocs.org/sdr/DALA2014082704847), Aug 26, 2014: SCUFF PLATE. CRACKED. CENTER CARGO DOOR CUTOUT SCUFF PLATE IS CRACKED IN TWO PLACES AT INSIDE CORNERS. CARGO DOOR SCUFF PLATE WELDED IAW EA 491023-14MA AND PS 900-7-2-1.
- [SDR DALA2014082404811](https://openairdocs.org/sdr/DALA2014082404811), Aug 23, 2014: ANGLE. CORRODED. CENTER CARGO DOOR CUTOUT, LOWER DOOR SILL ZEE ANGLE HAS NUMEROUS SPOTS OF CORROSION BS 645 - 683. REMOVED CORROSION IAW SRM 53-01, FIG 101. TRIMMED OUT 2 EA, OU
- [SDR DALA2014082104741](https://openairdocs.org/sdr/DALA2014082104741), Aug 20, 2014: SKIN. DAMAGED. UNIDENTIFIED PREVIOUS DEEP BLEND OUT ON FUSELAGE SKIN AT STA 186, BETWEEN LONGERON 27R AND 28R. REMOVED PAINT ON PREVIOUS BLEND AT STA 186 BETWEEN LONGERON 27R 
- [SDR DALA2017061604776](https://openairdocs.org/sdr/DALA2017061604776), Jul 23, 2013: TIRE. FAILED. MAJOR TIRE SEPARATION ON NR 4 TIRE.
- [SDR DALA2017101007400](https://openairdocs.org/sdr/DALA2017101007400), May 20, 2013: LAMP. INOPERATIVE. L4 ENTRY DOOR SLIDE LIGHT ARMING INDICATOR INOPERATIVE. REPLACED THE LAMP. CHECKED GIRT BAR ENGAGEMENT. LAMP AND GIRT BAR FUNCTION OK. OK FOR SERVICE.
- [SDR DALA13008489014](https://openairdocs.org/sdr/DALA13008489014), Feb 19, 2013: CONDUIT. OUT OF RIG. DURING TAILCONE FUNCTIONAL CHECK, LOWER CONDUITS FOR PULL CABLES IAW STEP 4D5, FOUND OUT OF RIG. REPOSITIONED CONDUIT IAW AMM.
- [SDR DALA13008499014](https://openairdocs.org/sdr/DALA13008499014), Feb 18, 2013: STRAP. SATURATED. DURING TAILCONE FUNCTIONAL, FOUND AFT AND FORWARD HOLD DOWN STRAPS SOAKED IN HYD FLUID, IN POOR CONDITION. R & R NEW STRAPS ON WC 2500-4484.
- [SDR DALA13008479014](https://openairdocs.org/sdr/DALA13008479014), Feb 18, 2013: BUSHING. WORN. DURING TAILCONE FUNCTIONAL TEST, FOUND TEE PIN BUSHINGS WORN. REPLACED TEE PIN BUSHINGS IAW AMM.
- [SDR DALA13008469014](https://openairdocs.org/sdr/DALA13008469014), Feb 18, 2013: CABLE. FRAYED. FOUND TAILCONE KEVLAR CABLE FRAYED. R & R KEVLAR INTERIOR CABLE IAW AMM. OPS CHECKS GOOD.
- [SDR DALA13008129014](https://openairdocs.org/sdr/DALA13008129014), Feb 14, 2013: DOOR FRAME. CORRODED. CORROSION ON DOOR FRAME OF AFT BAG BIN LOWER EDGE AT APPROX BS 1165 STR 28R. REPAIRED IAW SRM 53-05 FIG 123, OPTION 2.
- [SDR DALA1218599014](https://openairdocs.org/sdr/DALA1218599014), Mar 23, 2012: LANYARD. BROKEN. DURING SERVICE CHECK, MAINTENANCE FOUND L1 DOOR SLIDE LANYARD CABLE BROKEN. MAINTENANCE REMOVED AND REPLACED SLIDE LANYARD PER AMM. OPERATION CHECKS GOOD.
- [SDR DALA1151939014](https://openairdocs.org/sdr/DALA1151939014), Sep 7, 2011: WINDOW FRAME. DAMAGED. LIGHTNING STRIKE ON FWD/AFT SECTION OF WINDOW FRAME NR 32 BETWEEN STA Y=503 TO 522 AT FUSELAGE EXTERNAL SKIN. REWORKED PER ERA 495214-14 REV ORG.
- [SDR DALA1151929014](https://openairdocs.org/sdr/DALA1151929014), Sep 7, 2011: BELTFRAME. DAMAGED. LIGHTNING STRIKE ON AFT LOWER CORNER OF LT WINDOW BELT FRAME STA 7=712 AT FUS EXTERNAL SKIN. REWORKED PER ERA 495214-14 REV ORG.
- [SDR DALA1151919014](https://openairdocs.org/sdr/DALA1151919014), Sep 7, 2011: WINDOW FRAME. DAMAGED. SCRIBE LINES AROUND WINDOW FRAME NR 64 BETWEEN STA Y=807-826 AT FUSELAGE SKIN. REWORKED PER ERA 495214-14 REV ORG.
- [SDR DALA1151429014](https://openairdocs.org/sdr/DALA1151429014), Sep 6, 2011: FRAME. CORRODED. CORROSION ON LOWER CAP OF FRAME AT STA 1380 BETWEEN LONGERONS 27LT AND 27RT. "T" CAP WAS REPAIRED IAW ERA 495215-4 REV ORIG.
- [SDR DALA1151489014](https://openairdocs.org/sdr/DALA1151489014), Sep 6, 2011: SKIN. DAMAGED. TRANSFERED FROM ADF CTL NUM:037166001-ON WALK AROUND FOUND FWD ENTRY OUTER SKIN DAMAGED AT LOWER FWD CORNER DOOR SKIN WAS REPAIRED IAW SRM 52-05D FIG 55.
- [SDR DALA1149479014](https://openairdocs.org/sdr/DALA1149479014), Aug 24, 2011: FITTING. CORRODED. EA 09-093855-03AD REV B ME 02 CORROSION ON RT MLG SUPPORT FITTING BUSHING BORE SURFACE. REPAIRED PER AMR 0957393 REV 1.
- [SDR DALA1149469014](https://openairdocs.org/sdr/DALA1149469014), Aug 24, 2011: FITTING. CORRODED. EA 09-093855-03AD REV B ME 02 CORROSION ON RT MLG SUPPORT FITTING SUPPORT. REPAIRED PER AMR 0957393 REV 1.
- [SDR DALA1149459014](https://openairdocs.org/sdr/DALA1149459014), Aug 24, 2011: FITTING. CORRODED. EA 09-093855-03AD REV B ME 01 CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE. REPAIRED PER AMR 0957393 REV 1.
- [SDR DALA1149439014](https://openairdocs.org/sdr/DALA1149439014), Aug 24, 2011: FITTING. SCRATCHED. EA 09-093855-03AD REV B ME01 SCRATCHES ON LT MLG SUPPORT FITTING BEARING BORE. REPAIRED PER AMR 0957393 REV ORIG.
- [SDR DALA1149399014](https://openairdocs.org/sdr/DALA1149399014), Aug 24, 2011: SKIN. CORRODED. DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN BTW STA Y=1086-1087 LONGERON 29RT-30 AND BTW STA Y=1099-1100 LONGERON 28RT-29RT.
- [SDR DALA1149449014](https://openairdocs.org/sdr/DALA1149449014), Aug 23, 2011: FITTING. CORRODED. EA 09-093855-03AD REV B ME 01 CORROSION ON LT MLG SUPPORT FITTING BUSHING BORE BOTTOM SURFACE. REPAIRED PER AMR 0957393 REV 1.
- [SDR DALA1149289014](https://openairdocs.org/sdr/DALA1149289014), Aug 23, 2011: SKIN. CORRODED. DURING HMV CORROSION WAS FOUND ON INNER SKIN STA Y=788-793 BTW LONGERON 30 AND 29L AT MID CARGO COMPARTMENT INNER SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.
- [SDR DALA1149109014](https://openairdocs.org/sdr/DALA1149109014), Aug 22, 2011: PANEL. DAMAGED. MAINTENANCE REPAIRED PER SRM 53-04D. DUE ERA 466086-14 REV C LT WINDOW BELT PANEL FS 408-522 ACCOMPLISH PERM REPAIR PER RESTRICTION 4 PRIOR TO 40500 AC CYCLES (
- [SDR DALA1149099014](https://openairdocs.org/sdr/DALA1149099014), Aug 22, 2011: PANEL. DAMAGED. MAINTENANCE REPAIRED PER ERA 466085-14 REV E DUE ERA 466085-14 REV C LT WINDOW BELT PANEL FS 408-522 WINDOW NBR 31 ACCOMPLISH PERM REPAIR PRIOR TO 52630 AC CYCL
- [SDR DALA1149119014](https://openairdocs.org/sdr/DALA1149119014), Aug 22, 2011: SKIN. CORRODED. DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN FROM STA 1081-1130 BETWEEN LONG 30-35RT FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 53.
- [SDR DALA1149089014](https://openairdocs.org/sdr/DALA1149089014), Aug 22, 2011: PAN. CRACKED. DURING HMV A CRACK WAS FOUND ON AFT EDGE OF CARGO COMPARTMENT DOOR PAN BELOW STOP NR 5. DOOR PAN WAS REPAIRED IAW SRM 52-05 FIG 50.
- [SDR DALA1149009014](https://openairdocs.org/sdr/DALA1149009014), Aug 21, 2011: SKIN. CORRODED. DURING HMV CORROSION WAS FOUND ON INNER FUSELAGE SKIN IN STA Y=1099 TO 1105 BETWEEN LONGERON 29RT AND 29LT AT AFT CARGO COMPARTMENT. FUSELAGE SKIN WAS REPAIRED 
- [SDR DALA1149419014](https://openairdocs.org/sdr/DALA1149419014), Aug 20, 2011: PAN. CRACKED. CRACKED PAN BELOW FITTING STOP NR 5 OF ADT CARGO COMPT FWD SECTION. REPAIRED PER SRM 52-05.
- [SDR DALA1148789014](https://openairdocs.org/sdr/DALA1148789014), Aug 19, 2011: FRAME. CRACKED. DURING HMV A BROKEN FRAME WAS FOUND AT STA Y=1451 AND LONGERON 1. FRAME WAS REPAIRED IAW SRM 53-03D FIG 4.
- [SDR DALA1148749014](https://openairdocs.org/sdr/DALA1148749014), Aug 19, 2011: DOUBLER. CORRODED. DURING HMV CORROSION WAS FOUND ON PREVIOUS REPAIR DOUBLER AT LOWER BEAM FROM STA Y=668-680 OF MID CARGO COMPARTMENT DOOR JAMB. REPAIR DOUBLER WAS REPLACED IAW S
- [SDR DALA1132189014](https://openairdocs.org/sdr/DALA1132189014), May 6, 2011: BATTERY. DISCHARGED. DURING LINE CHECK MAINTENANCE FOUND LEFT AND RIGHT OVERWING EXIT UPPER SIGNS INOP. MAINTENANCE REPLACED BATTERIES AT BATTERY PACK 135-105. OPERATION OF EXIT SIG

All 79: https://openairdocs.org/deregistered/N914DE-2019-09-16/reports.md

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