# N995DL: 1991 Mcdonnell Douglas MD-88, registration cancelled 2022-10-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 26, 2022
- Status when cancelled: First 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: 53362
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: January 9, 1992
- Certificate issued: March 6, 1992
- Last registry action: August 13, 2019
- Mode S code: ADE58C
- 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/N995DL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=995DL
- Page: https://openairdocs.org/deregistered/N995DL-2022-10-26

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 Mcdonnell Douglas MD-88: https://openairdocs.org/model/mcdonnell-douglas-md-88.md

## Service difficulty reports (225, newest 50)

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

- [SDR DALA2020052202417](https://openairdocs.org/sdr/DALA2020052202417), May 22, 2020: PANEL. OUT OF ADJUST. THE SPRING RETRACT DOOR PANEL RIGHT SIDE ON THE AFT ESCAPE RAMP IS INOPERATIVE. MAINTENANCE ADJUSTED THE DOOR PANEL IAW MD-88 AMM 52-00. OPERATION NOW CHECKS GO
- [SDR DALA2020042002277](https://openairdocs.org/sdr/DALA2020042002277), Apr 20, 2020: BATTERY. DISCHARGED. THE CEILING EMERGENCY LIGHTS FROM SEAT ROW 22 TO 26 ARE INOPERABLE. MAINTENANCE REPLACED THE BATTERIES ON THE EMERGENCY LIGHT CHARGER ASSEMBLY PER MD88 AMM 33-5
- [SDR DALA2019111506705](https://openairdocs.org/sdr/DALA2019111506705), Nov 15, 2019: BATTERY PACK. INOPERATIVE. DURING SVC FOUND FWD CABIN EMERGENCY LIGHT INOP. T/S PER MD88 AMM:33-50 AND ROBBED EMERGENCY BATTERY FROM A/C 963 . OPS CHECK OK A/C OK FOR SVC. (LP6658249)
- [SDR DALA2019082104890](https://openairdocs.org/sdr/DALA2019082104890), Aug 21, 2019: FUSE. FAILED. EXIT ROW LIGHTS OUT FROM ROW 31 AFT. TROUBLE SHOOT TO BAD FUSE IN POWER PACK. REPLACED FUSE IAW CMM 33-21-70. OPS CHECK GOOD. (LP5158525)
- [SDR DALA2019021871017](https://openairdocs.org/sdr/DALA2019021871017), Feb 16, 2019: DUCT. BLOWN. RIGHT ENGINE FIRE LIGHT BELLS PASSING APPROX. 800 FT ON TAKEOFF. NO ENGINE INDICATIONS OF FIRE OR DAMAGE. FIRE LIGHT WENT OUT BEFORE BLOWING FIRE BOTTLE OR SHUT
- [SDR DALA2019012500515](https://openairdocs.org/sdr/DALA2019012500515), Jan 25, 2019: SLIDE. FAILED. RT SLIDE FAIL DEPLOYMENT TEST. FORECAST NR 88-0526-8-0406, MPN. D29982, S/N 0883, DATE, OCT 1986. RT SLIDE REMOVED & REPLACED REF. STK# 97-2561-9-0001, W/C 2561
- [SDR DALA2019011300217](https://openairdocs.org/sdr/DALA2019011300217), Jan 13, 2019: BATTERY. DISCHARGED. FWD OVHD EM LIGHTS IN-OP. REPLACED BATTERIES IN EM LT PWR SUPPLY 5-23 IAW AMM 33-55 CKS GOOD. (LP4753077)
- [SDR DALA2018121807253](https://openairdocs.org/sdr/DALA2018121807253), Dec 17, 2018: UNKNOWN. ODOR. BOTH PILOTS SMRLT RUBBER ODER WHEN DEPARTING BHM ON T/O ODER DISSIPATED BEFORE REACHING 10000 FT. REF NO GO ODI LOG 0867036. OPENED SADDLE DUCTS CAPS ON NBR 1 A
- [SDR DALA2018121707224](https://openairdocs.org/sdr/DALA2018121707224), Dec 16, 2018: UNKNOWN. ODOR. DURING TO AND INITIAL CLIMB, THE FA AT THE TAILCONE SMELLED AN ODOR. THE RUBBERY ODOR SMELL DISSIPATED 5 MINUTES AFTER TO. IT WAS A NORMAL PWR TO. PACKS ON, ENG
- [SDR DALA2018120607058](https://openairdocs.org/sdr/DALA2018120607058), Dec 5, 2018: RIB. CRACKED. UPPER RIB FORMER IS CRACKED OUT OF RIVET HOLE. ( P/N 9936146-13) UPPER ROW, THIRD HOLE RT FROM CENTER. REPAIRED PER 573506-14 REV O. (LP0852904)
- [SDR DALA2018082905334](https://openairdocs.org/sdr/DALA2018082905334), Aug 28, 2018: DOUBLER. WORN. WORN REPAIR DOUBLER, FWD, UPPER CORNER AT THE L1 DOOR. THE REPAIR DOUBLER WAS REPLACED IAW SRM 52-05, FIG 18A.
- [SDR DALA2018082805308](https://openairdocs.org/sdr/DALA2018082805308), Aug 27, 2018: FLOOR PANEL. DELAMINATED. DELAMINATED FLOOR PANEL 826D IN THE PAX CABIN. THE FLOOR PANEL WAS FABRICATED AND REPLACED IAW AMM 53-20-01-201.
- [SDR DALA2018082765254](https://openairdocs.org/sdr/DALA2018082765254), Aug 25, 2018: SKIN. WORN. WEAR ON THE AFT UPPER SURFACE OF THE RT WING GROUND SPOILER. REPAIRED IAW SRM 51-70-1B, P.11.
- [SDR DALA2018082765248](https://openairdocs.org/sdr/DALA2018082765248), Aug 25, 2018: PANEL. DAMAGED. LAVATORY SERVICE PANEL DAMAGED. REPAIRED IAW ER/A 536216-14, REV A, SECT III, AND ETI-88-18-068, REV 2.
- [SDR DALA2018082875314](https://openairdocs.org/sdr/DALA2018082875314), Aug 24, 2018: SKIN. CORRODED. FUSELAGE SKIN, AFT LAVATORY SERVICE DOOR CUTOUT BS 1307, LONGERON 22L WAS CORRODED. ACCOMPLISH ERA 536216-14 REV A SECTION IV.
- [SDR DALA2018082705252](https://openairdocs.org/sdr/DALA2018082705252), Aug 23, 2018: SLIDE. DAMAGED. BROCKEN SAFETY THREADS AT L1 SLIDE. THE SLIDE WAS REPLACED IAW AMM 25-62-00-201.
- [SDR DALA2018042902888](https://openairdocs.org/sdr/DALA2018042902888), Apr 28, 2018: LIGHT. INOPERATIVE. SEAT 14ED EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-53. OPS CHECKED GOOD.
- [SDR DALA2017122608875](https://openairdocs.org/sdr/DALA2017122608875), Dec 22, 2017: CONNECTOR. DISCONNECTED. EXTERIOR EMERGENCY LIGHTS INOPERATIVE. FOUND THE RT OVERWING EMERGENCY LIGHT NOT CONNECTED. RECONNECTED THE CONNECTOR. ALL LIGHTS CHECKED GOOD.
- [SDR DALA2017112008219](https://openairdocs.org/sdr/DALA2017112008219), Nov 17, 2017: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS INOPERATIVE, ROW 27 AFT TO REAR DOOR. REPLACED THE BATTERIES IN PAX OVERHEAD BIN 33. OPS CHECKED OK.
- [SDR DALA2017110307924](https://openairdocs.org/sdr/DALA2017110307924), Nov 2, 2017: DOOR FRAME. CRACKED. DURING A CHECK, FOUND THE RT WHEEL WELL FWD DOOR FRAME CRACKED. VISUALLY INSPECTED AND STOP DRILLED IAW ENGINEERING. REMOVED & REPLACED FWD RT WHEEL WELL DOOR F
- [SDR DALA2017071405470](https://openairdocs.org/sdr/DALA2017071405470), Jul 13, 2017: WHEEL. UNDERTORQUED. AFTER LANDING & NORMAL BRAKING, DURING LANDING BOTH BRAKES EXHIBITED SIGNIFICANT SHUDDER DURING STOP ATTEMPTS. AIRPLANE HAD TROUBLE STOPPING DUE TO THE BRAKE CH
- [SDR DALA2017071005346](https://openairdocs.org/sdr/DALA2017071005346), Jul 9, 2017: WIRE HARNESS. DEFECTIVE. ON SERVICE CHECK FOUND SEAT 35C EMERGENCY SEAT LIGHT INOP. REPLACED EMERGENCY LIGHT SEAT HARNESS AT 35C. OPERATION IS NOW NORMAL. OK FOR SERVICE.
- [SDR DALA2017040602773](https://openairdocs.org/sdr/DALA2017040602773), Apr 6, 2017: LAMP. INOPERATIVE. ONE RED EMERGENCY LIGHT ON SEAT 24D INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-53. CHECKED GOOD.
- [SDR DALA2016072605568](https://openairdocs.org/sdr/DALA2016072605568), Jul 25, 2016: HAND RAIL. MISINSTALLED. FUNCTIONAL FAIL ON AFT EMERGENCY DOOR HANDLE. EMERGENCY VENTRAL DOOR HANDLE ASSEMBLIES REMOVED AND INSTALLED CORRECTLY AND FAILURE WAS CORRECTED IAW 52-63-1.
- [SDR DALA2016072605566](https://openairdocs.org/sdr/DALA2016072605566), Jul 25, 2016: HINGE. WORN. FREE PLAY ON FWD & AFT HINGE AT FWD CARGO DOOR. HINGES WERE REMOVED REPAIRED AND INSTALLED IAW ER/A 497387-14 REV B AND FREE PLAY WAS CORRECTED INSTALLATION OF 
- [SDR DALA2016072605565](https://openairdocs.org/sdr/DALA2016072605565), Jul 25, 2016: HINGE. WORN. FREE PLAY ON FWD & AFT HINGE AT MID CARGO DOOR. FWD. AFT HINGES REMOVED, REPAIRED AND INSTALLED IAW ERA 497387-14MA REV B AND AMM 52-31-02.
- [SDR DALA2016072505535](https://openairdocs.org/sdr/DALA2016072505535), Jul 25, 2016: RIB. CRACKED. CRACKED RT WING LEADING EDGE RIB XRS 276. RIB WAS REPLACED IAW SRM 51-30-2, 51-10-4, AND 51-10-3.
- [SDR DALA2016072505537](https://openairdocs.org/sdr/DALA2016072505537), Jul 24, 2016: ANGLE. CRACKED. CRACKED FORMER ANGLES ON FIXED LEADING EDGE COMPARTMENT XOS 354, XOS 361, XOS 251, XOS 257 AND XOS 470 AT LT WING. FORMER ANGLES WERE REPLACED IAW SRM 51-30-2/5
- [SDR DALA2016072505536](https://openairdocs.org/sdr/DALA2016072505536), Jul 24, 2016: SUPPORT FITTING. CORRODED. CORROSION BUSHING BORE AND SPOT FACE AT RIGHT GEAR RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD RE
- [SDR DALA2016072505534](https://openairdocs.org/sdr/DALA2016072505534), Jul 24, 2016: STRINGER. CRACKED. CRACK OF 0.250 WAS FOUND ON STRINGER 17R XCW 10, INSIDE CENTER TANK. STRINGER 17 WAS REPAIRED PER ER/A 547822-14 REV. ORIG. 547823-14 REV. ORIG.
- [SDR DALA2016072505533](https://openairdocs.org/sdr/DALA2016072505533), Jul 24, 2016: STRINGER. CRACKED. CRACK OF 0.312 "WAS FOUND ON STRINGER 17L XCW=12, INSIDE CENTER TANK. STRINGER WAS REPAIRED PER ER/A 547822-14 REV. ORIG. 547823-14 REV. ORIG.
- [SDR DALA2016072505532](https://openairdocs.org/sdr/DALA2016072505532), Jul 24, 2016: SUPPORT FITTING. CORRODED. CORROSION ON BUSHING BORE OF BEARING AT RIGHT GEAR RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD RE
- [SDR DALA2016072505531](https://openairdocs.org/sdr/DALA2016072505531), Jul 24, 2016: SUPPORT FITTING. CORRODED. CORROSION ON BUSHING BORE AND SPOT FACE AT LEFT GEAR, RETRACT ACTUATOR SUPPORT FITTING. THE REPAIR WAS ACCOMPLISHED IAW ETI-88-16-248 REV 4 AND ER/A 547834-14AD
- [SDR DALA2016072505529](https://openairdocs.org/sdr/DALA2016072505529), Jul 24, 2016: PAN. CRACKED. CRACKED PLATE ON AFT EDGE AND BEAM 1 BEHIND STOP NR 1 AT AFT CARGO DOOR. INNER PAN WAS REPAIRED IAW ETI-88-16-254 REV:2 AND ERA 547852-14 REV. ORIGINAL.
- [SDR DALA2016072505528](https://openairdocs.org/sdr/DALA2016072505528), Jul 24, 2016: PAN. WORN. WORN PLATE AND PAN ON AFT EDGE LWR CORNER OUTER SURFACE AT FWD CARGO DOOR. AFT EDGE LWR CORNER WAS REPAIRED I.A.W. DC-9/MD-80 ETI- 88-16-253 REV. 2 AND ERA:5478
- [SDR DALA2016072505539](https://openairdocs.org/sdr/DALA2016072505539), Jul 23, 2016: SKIN. CRACKED. DURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND ON LOWER SKIN BETWEEN XRS=163 TO 168 REAR SPAR AT RT WING. REPAIRED IAW ER/A 547818-14 REV. ORIGINAL.
- [SDR DALA2016072505538](https://openairdocs.org/sdr/DALA2016072505538), Jul 23, 2016: SKIN. CRACKED. DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN BETWEEN XRS=163 TO 168 REAR SPAR AT LT WING. REPAIRED IAW ER/A 547818-14 REV.ORIGINAL.
- [SDR DALA2016072405524](https://openairdocs.org/sdr/DALA2016072405524), Jul 23, 2016: SUPPORT FITTING. CORRODED. CORROSION ON BUSHING BORE OF BEARING AT LEFT GEAR RETRACT ACTUATOR SUPPORT FITTING. REPAIR ACCOMPLISHED IAW ETI-88-16-248 REV. 4 AND ER/A 547834-14AD REV ORIG.
- [SDR DALA2016072405523](https://openairdocs.org/sdr/DALA2016072405523), Jul 23, 2016: FRAME. CRACKED. CRACK VISIBLE ON FRAME BS 1510 AFT SIDE NEXT TO UPPER LEFT TAIL CONE LATCH HOOK. REPLACED THE FRAME IAW SRM 51-30-1, 51-30-2, 51-10-4, 51-10-3 AND DWG 9911843 R
- [SDR DALA2016072405522](https://openairdocs.org/sdr/DALA2016072405522), Jul 23, 2016: SKIN. CRACKED. TWO CRACKS IN FUSELAGE SKIN BS 1463 -1446. REPAIRED IAW ETI 88-16-255 REV 2 ER/A 547855-14 REV ORG.
- [SDR DALA2016072205482](https://openairdocs.org/sdr/DALA2016072205482), Jul 21, 2016: ANGLE. CORRODED. CORRODED ANGLE BS 1350 X 17LT TO 17RT Z 0, LOWER VENTRAL DOOR JAMB ANGLE. LOWER VENTRAL DOOR JAMB WAS REPAIRED IAW SRM 53-05 FIG.34 AND ER/A 547838-14 REV.1.
- [SDR DALA2016072105451](https://openairdocs.org/sdr/DALA2016072105451), Jul 20, 2016: INTERCOSTAL. CRACKED. CRACKED INTERCOSTAL ON BS 1485 AND BTW 1 AND 2 HRS POSITION AT AFT ACCESSORY COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 53-01, 51-30-2, 51-30-5, AND DWG. 991
- [SDR DALA2016072005443](https://openairdocs.org/sdr/DALA2016072005443), Jul 19, 2016: FRAME. CRACKED. CRACKED FRAME BS 1510. FRAME WAS REPLACED IAW DWG 9911843 AND SRM 51-30-2.
- [SDR DALA2016072005442](https://openairdocs.org/sdr/DALA2016072005442), Jul 19, 2016: CUSP WEB. CRACKED. CRACK ON CUSP WEB BS 459 - 479 AND X -54 TO X -60. REPAIRED IAW SRM 53-05 FIG 131A-14.
- [SDR DALA2016072005441](https://openairdocs.org/sdr/DALA2016072005441), Jul 19, 2016: PAN. CRACKED. CRACKED INNER PAN ON AFT EDGE AND BEAM 5 AT FWD CARGO DOOR. PAN REPAIRED IAW SRM 52-03 D FIG 8.
- [SDR DALA2016071905432](https://openairdocs.org/sdr/DALA2016071905432), Jul 18, 2016: CARGO TRACK. CORRODED. CORRODED CARGO TRACK BETWEEN BS 1007 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-10-4, 51-10-3 PAR 21 AND 14 , 51-30-2, 51-30-1 AND 51-30-5.
- [SDR DALA2016071905434](https://openairdocs.org/sdr/DALA2016071905434), Jul 17, 2016: BELLCRANK. CORRODED. CORROSION ON BELLCRANK AT RUDDER THROW-LIMITER. RUDDER BELLCRANK ASSY WAS REPLACED IAW AMM 27-20-03.
- [SDR DALA2016071805375](https://openairdocs.org/sdr/DALA2016071805375), Jul 17, 2016: STRINGER. CRACKED. CRACK ON STRINGER 11 AT THE OUTBOARD FLAP, INBOARD DRIVE HINGE AT STA XRS=160. LH SIDE. CRACKED LH STRINGER 11 AT THE OUTBOARD FLAP, INBOARD DRIVE HINGE AT STA 
- [SDR DALA2016071805374](https://openairdocs.org/sdr/DALA2016071805374), Jul 17, 2016: LONGERON. CORRODED. SEVERAL AREAS OF CORROSION ON LONGERON 22L BETWEEN BS 1287 -- 1309. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG. 18 / 51-10-3 / 51-30-5.
- [SDR DALA2016071805373](https://openairdocs.org/sdr/DALA2016071805373), Jul 17, 2016: DOUBLER. WORN. WORN FWD & AFT DOUBLER ON LWR EDGE AT MID CARGO COMPARTMENT DOOR. THE DOUBLER WAS REPLACED IAW SRM 51-30-2 AND AFT DOUBLER WAS CLEANED IAW PSM 900-1-2 AND NO FO

All 225: https://openairdocs.org/deregistered/N995DL-2022-10-26/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA13CA106](https://openairdocs.org/ntsb/DCA13CA106), Jun 13, 2013: Mcdonnell Douglas MD-88 (N995DL), Nashville, TN, substantial damage. Probable cause: The flight crews failure to maintain clearance from the light pole while taxiing.

## FAA accident and incident reports (2)

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.

- [Accident 20130613010889A](https://openairdocs.org/incident/20130613010889A), Jun 13, 2013: Mcdonnell Douglas Aircraft Co MD-88 (N995DL), Nashville, TN, Substantial damage. Crew was taxiing from gate B-7 in the north ramp area to await flow control time to atl in a non movement area which is not marked with taxiway lines. Aircraft…
- [Incident 20000522016939I](https://openairdocs.org/incident/20000522016939I), May 22, 2000: Doug MD88 (N995DL), Kansas City, MO. (-23)On may 22, 2000, at approximately 1843 CDT, delta airlines flight 1545, a Douglas MD-88, N995DL, left Kansas City International Airport, Kansas City,…

---
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.