# N905DE: 1992 Mcdonnell Douglas MD-88, registration cancelled 2022-11-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 29, 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: 53410
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: May 6, 1992
- Certificate issued: June 3, 1992
- Last registry action: July 16, 2020
- Mode S code: AC820F
- 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/N905DE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=905DE
- Page: https://openairdocs.org/deregistered/N905DE-2022-11-29

From the FAA registry file of November 7, 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 (154, newest 50)

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

- [SDR DALA2019101605927](https://openairdocs.org/sdr/DALA2019101605927), Oct 16, 2019: SWITCH. MALFUNCTIONED. SHIP 9005 - ATO - REJECTED TAKE-OFF AT 110 KNOTS DUE TO STABILIZER CONFIGURATION WARNING. CORRECTIVE ACTION: REPLACED HORIZONTAL STAB SWITCH (S1-491) AND CAW UN
- [SDR DALA2019060323357](https://openairdocs.org/sdr/DALA2019060323357), Jun 1, 2019: GENERATOR. DISCONNECTED. AT 12,000 MSL, AUTO THROTTLES/AUTOPILOT DISCONNECTED L AC BUSS OFF, AND AC CROSS TIE LOCKOUT, L GEN OFF STALL IND FAIL, ON OAP, RAN QRH FOR LAC BUS OFF & AC CRO
- [SDR DALA2018091805641](https://openairdocs.org/sdr/DALA2018091805641), Sep 17, 2018: CHANNEL. CRACKED. CHANNEL CRACKED TWO PLACES AFT SIDE OF NOSE COWL AFT BULKHEAD 6 O'CLOCK POSITION. REPLACED NR 1 NOSE COWL REF AMM 71-10-01.
- [SDR DALA2018090405399](https://openairdocs.org/sdr/DALA2018090405399), Sep 1, 2018: SLIDE. UNSECURE. L1 DOOR SLIDE PIN PULLED AND SLIDE PACKAGE STARTED TO OPEN. R&R L1 DOOR SLIDE PER W/C 2561-01358-04A.
- [SDR DALA2018052903616](https://openairdocs.org/sdr/DALA2018052903616), May 29, 2018: LAMP. INOPERATIVE. EMERGENCY LIGHTS WERE INOPERATIVE AT 1CD. REPLACED THE LAMP. OPS CHECKED GOOD.
- [SDR DALA2018030701444](https://openairdocs.org/sdr/DALA2018030701444), Mar 4, 2018: SLIDE. LOW PRESSURE. R1 DOOR SLIDE PRESSURE OUTSIDE OF GREEN RANGE. REPLACED THE SERVICE DOOR SLIDE IAW WORK CARD 2561-4964.
- [SDR DALA2018010200008](https://openairdocs.org/sdr/DALA2018010200008), Dec 30, 2017: LIGHT. INOPERATIVE. L1 DOOR EMERG LIGHT INOP. RELAMPED IAW AMM 33-50.
- [SDR DALA2017081806299](https://openairdocs.org/sdr/DALA2017081806299), Aug 18, 2017: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ROWS 22-25 CELING INOPERATIVE. R & R THE BATTERIES IN B5104. OPS CHECKED GOOD.
- [SDR DALA2017022301496](https://openairdocs.org/sdr/DALA2017022301496), Feb 21, 2017: SENSOR. LOOSE. DURING TAXI IN, FIRST OFFICER`S WINDSHIELD HAD A LARGE SPARK. WINDSHIELD HEAT IS NO LONGER FUNCTIONING. FOUND THE WINDOW ANTI-FOG SENSOR LOOSE AND IN CONTACT WI
- [SDR DALA2017011800478](https://openairdocs.org/sdr/DALA2017011800478), Jan 17, 2017: BATTERY PACK. INOPERATIVE. COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE BATTERY PACK AND TESTED IAW AMM 33-53. OPS CHECKED OK.
- [SDR DALA2016081706054](https://openairdocs.org/sdr/DALA2016081706054), Aug 16, 2016: LANYARD. DAMAGED. DAMAGE IN L1 SLIDE RELEASE LANYARD CABLE. L1 RELEASE LANYARD CABLE WAS REPLACED IAW AMM 25-62-01.
- [SDR DALA2016081405973](https://openairdocs.org/sdr/DALA2016081405973), Aug 13, 2016: STRINGER. CRACKED. CRACK OF 0.750" WAS FOUND ON STRINGER 17R . REPAIRED PER ERA 547891-14AD REV. ORG. AND ERA 547892-14 REV. ORG. .
- [SDR DALA2016081205954](https://openairdocs.org/sdr/DALA2016081205954), Aug 11, 2016: FRAME. CRACKED. INITIAL INSPECTION CRACK ON FRAME OF CANT STA Y=1510 BETWEEN 12:00 TO 1:00 POSITION AT AFT ACCESSORIES COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-30-2 AND DWG 9
- [SDR DALA2016081205953](https://openairdocs.org/sdr/DALA2016081205953), Aug 11, 2016: FLOOR PANEL. DAMAGED. ELONGATED HOLES ON GENERATION FLOOR PANEL NR 826G, 389G AND 769G. DUE TO EXCESSIVE ELONGATED HOLE FLOOR PANEL 769G WAS REPAIRED IAW SRM 51-70-4, FIG 1, SH 2 FLO
- [SDR DALA2016081105935](https://openairdocs.org/sdr/DALA2016081105935), Aug 10, 2016: CARGO TRACK. CORRODED. CORROSION ON LEFT CARGO TRACK BETWEEN BS 1145 - 1222. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, SRM 51-30-1 AND DWG 5936663 REV "Y".
- [SDR DALA2016081105934](https://openairdocs.org/sdr/DALA2016081105934), Aug 10, 2016: CARGO TRACK. CORRODED. CORROSION ON RIGHT CARGO TRACK BETWEEN BS 1145 - 1155. THE CARGO TRACK WAS REPLACED IAW DWG 5936663 REV "Y", SRM 51-10-1 AND 51-30-2.
- [SDR DALA2016081105933](https://openairdocs.org/sdr/DALA2016081105933), Aug 10, 2016: ACCESS PANEL. CORRODED. CORROSION ON FUEL ACCESS PANEL 1331C. THE ACCESS PANEL WAS REPLACED IAW AMM 20-30-01.
- [SDR DALA2016081105929](https://openairdocs.org/sdr/DALA2016081105929), Aug 10, 2016: CARGO TRACK. CORRODED. CORROSION ON RIGHT CARGO TRACK FROM BS 1231 - 1322. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, SRM 51-30-1. SRM, 51-10-4, SRM.51-10-3 PAR. 14-21 AND DWG 5936
- [SDR DALA2016081105928](https://openairdocs.org/sdr/DALA2016081105928), Aug 10, 2016: CARGO TRACK. CORRODED. CORROSION ON LEFT CARGO TRACK BS 1221 - 1322. CARGO TRACK WAS REPLACED IAW DWG 5936660 REV BZ.
- [SDR DALA2016081005917](https://openairdocs.org/sdr/DALA2016081005917), Aug 9, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL ACCESS PANEL 1311C ON LT WING. THE ACCESS PANEL WAS REPLACED.
- [SDR DALA2016080905886](https://openairdocs.org/sdr/DALA2016080905886), Aug 8, 2016: DOUBLER. CORRODED. CORROSION ON INTERNAL DOUBLER AT INNER FUSELAGE MID CARGO BAY BETWEEN BS 636 - 645 LONGERON 29R AND 29L. THE DOUBLER WAS REPLACED IAW SRM 51-10-4, 51-10-3 PAR 1
- [SDR DALA2016080805858](https://openairdocs.org/sdr/DALA2016080805858), Aug 8, 2016: LONGERON. CORRODED. CORROSION ON LONGERON 22L BETWEEN BS 1287 - 1309. THE LONGERON WAS FOUND OUT LIMITS AND REPAIRED IAW 53-02 FIG 18.
- [SDR DALA2016080805859](https://openairdocs.org/sdr/DALA2016080805859), Aug 6, 2016: PAN. CRACKED. CRACKED FWD EDGE PAN ON FWD CARGO DOOR OVER BEAM NR 5. THE EDGE PAN WAS REPAIRED IAW SRM 53-05D FIG.
- [SDR DALA2016080605853](https://openairdocs.org/sdr/DALA2016080605853), Aug 5, 2016: CUSP WEB. CRACKED. A CRACK WAS FOUND ON LT CUSP WEB BETWEEN BS 845 - 864 AND X 44 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG 131A-10.
- [SDR DALA2016080505784](https://openairdocs.org/sdr/DALA2016080505784), Aug 4, 2016: STRINGER. CRACKED. CRACKED STR NR 20 LT STA Y, 1003 ABOVE TRAPEZOIDAL PANEL AT LT WHEEL WELL. STRINGER NR 20 WAS REPAIRED IAW SRM 53-02, FIG 22.
- [SDR DALA2016080405769](https://openairdocs.org/sdr/DALA2016080405769), Aug 3, 2016: SKIN. CRACKED. CRACK ON OUTER SKIN BETWEEN BEAMS NR 1 TO 2 AND PROJECTION STA Y:658 OF AFT MID CARGO COMPARTMENT DOOR. SKIN WAS REPAIRED IAW ERA 486446-14MA, REV ORIGINAL.
- [SDR DALA2016080405767](https://openairdocs.org/sdr/DALA2016080405767), Aug 3, 2016: LONGERON. CRACKED. INITIAL INSPECTION, CRACK ON LONG 4RT AND STA Y=1437 AT AFT ACCESSORIES COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA2016080405766](https://openairdocs.org/sdr/DALA2016080405766), Aug 3, 2016: LONGERON. CRACKED. INITIAL INSPECTION, CRACK ON LONG 3LT AND STA Y=1437 AT AFT ACCESSORIES COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.
- [SDR DALA2016080405764](https://openairdocs.org/sdr/DALA2016080405764), Aug 3, 2016: SKIN. CRACKED. CRACK OF 0.062" ON FUSELAGE SKIN AT THE UPPER FWD DOOR JAMB CORNER STA Y=375.5 BETWEEN LONG 19-20 RT OF THE FWD CARGO COMPARTMENT. FUSELAGE SKIN AT THE UPPER FW
- [SDR DALA2016080305732](https://openairdocs.org/sdr/DALA2016080305732), Aug 2, 2016: BEAM. CRACKED. CRACK ON BEAM NR 5 AND BS 427 OF FWD CARGO DOOR. THE BEAM WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR DALA2016080305729](https://openairdocs.org/sdr/DALA2016080305729), Aug 2, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA ON FUEL ACCESS PANEL 1335. ACCESS PANEL WAS REPLACED.
- [SDR DALA2016080305728](https://openairdocs.org/sdr/DALA2016080305728), Aug 2, 2016: ACCESS PANEL. CORRODED. CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1414C ON RT WING. THE ACCESS PANEL WAS REPLACED.
- [SDR DALA2016080305724](https://openairdocs.org/sdr/DALA2016080305724), Aug 2, 2016: ANGLE. CRACKED. CRACKED ANGLE ON DOOR STOP AT RT AFT OVERWING EMERGENCY EXIT. THE ANGLE WAS REPLACED IAW DWG 9957735 REV. G AND SRM 51-30-5 AND 51-30-2.
- [SDR DALA2016080305723](https://openairdocs.org/sdr/DALA2016080305723), Aug 2, 2016: DOOR FRAME. CRACKED. CRACK ON EMERGENCY EXIT DOOR FRAME (UPPER AREA) BS 919 LT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-05 FIG.32.
- [SDR DALA2016080205714](https://openairdocs.org/sdr/DALA2016080205714), Aug 2, 2016: FRAME. CRACKED. CRACK ON FRAME BS 1322 LONGERON 17R. THE FRAME WAS REPAIRED IAW ER 493697-14MA REV. B.
- [SDR DALA2016080205712](https://openairdocs.org/sdr/DALA2016080205712), Aug 1, 2016: FLOOR PANEL. DAMAGED. DAMAGED FERRULS ON FLOOR PANEL. FLOOR PANEL REPAIRED IAW AMM 53-20-01-201 AND AMM 88 53-20-01-201.
- [SDR DALA2016080205711](https://openairdocs.org/sdr/DALA2016080205711), Aug 1, 2016: LONGERON. CRACKED. CRACK FOUND ON LONGERON 16L, BS 1437. THE LONGERON WAS REPLACED IAW SRM 53-14-4 FIG 4, SRM 51-30-5, AND SRM 51-30-2.
- [SDR DALA2016080105699](https://openairdocs.org/sdr/DALA2016080105699), Jul 31, 2016: CUSP WEB. CRACKED. CRACK ON LEFT CUSP WEB BS 905 - 927, X 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-14 51-30-2, 51-30-5, AND 51-10-3 PAR. 14,21 & 38.
- [SDR DALA2016080105709](https://openairdocs.org/sdr/DALA2016080105709), Jul 30, 2016: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB BS 1003 - 1020. THE CUSP WEB WAS REPAIRED IAW SRM 51-30-2, 53-05 FIG. 131A-14 , 51-10-3 PAR. 21,14 AND 51-30-5 CABIN.
- [SDR DALA2016080105708](https://openairdocs.org/sdr/DALA2016080105708), Jul 30, 2016: CUSP WEB. CORRODED. CORROSION ON PREVIOUS REPAIR DOUBLER ON LT CUSP WEB BS 934 - 946, X 54-60. REPAIRED IAW SRM 53-05 FIG 131. AND 51-30-2.
- [SDR DALA2016080105707](https://openairdocs.org/sdr/DALA2016080105707), Jul 30, 2016: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB BS 1060 - 1079. CUSP WEB REPAIRED IAW SRM 53-05 FIG. 131A-14 AND SRM 51-30-5.
- [SDR DALA2016080105706](https://openairdocs.org/sdr/DALA2016080105706), Jul 30, 2016: CUSP WEB. CORRODED. CORROSION ON RT CUSP WEB BS 1041 - 1050. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIG. 131A-13.
- [SDR DALA2016080105703](https://openairdocs.org/sdr/DALA2016080105703), Jul 30, 2016: ANGLE. CRACKED. CRACK ON ANGLE BEAM FWD AT FWD ENTRY DOOR. ANGLE WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND DWG 9955752 REV M.
- [SDR DALA2016080105702](https://openairdocs.org/sdr/DALA2016080105702), Jul 30, 2016: RIB. CRACKED. CRACK ON RIB XOS 455 ON RT WING FIXED LE STRUCTURE. THE RIB WAS REPAIRED IAW SRM 57-06B D FIG. 12 SHEET 4.
- [SDR DALA2016073105662](https://openairdocs.org/sdr/DALA2016073105662), Jul 30, 2016: CUSP WEB. CORRODED. CORRODED PREVIOUS REPAIR DOUBLER ON LT CUSP WEB BETWEEN BS 446 - 459 , X 54 - 60. THE DOUBLER WAS REPLACED IAW SRM 53-05 FIGURE 131A-2.
- [SDR DALA2016073105661](https://openairdocs.org/sdr/DALA2016073105661), Jul 30, 2016: CUSP WEB. CORRODED. CORRODED REPAIR DOUBLERS ON LT CUSP WEB BETWEEN BS 984 - 1003, AND BS 1003 - 1022, X 54 - 60. REPAIR REPLACED IAW SRM 53-05 FIG. 131A-4, 131A-6, 51-10-3 PAR. 14
- [SDR DALA2016073105660](https://openairdocs.org/sdr/DALA2016073105660), Jul 30, 2016: CUSP WEB. CORRODED. CORROSION ON LT CUSP WEB BETWEEN BS 965 - 984 AND X 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05 FIGURE 131A-2.
- [SDR DALA2016080105710](https://openairdocs.org/sdr/DALA2016080105710), Jul 29, 2016: DOUBLER. CORRODED. CORROSION ON REPAIR DOUBLER BS 446 - 465 AND X -44 TO -60. AREA WAS REPAIRED IAW SRM 53-05 FIG.131A-11, 51-10-3, 51-30-1, 51-30-2 & 51-30-5.
- [SDR DALA2016080105700](https://openairdocs.org/sdr/DALA2016080105700), Jul 29, 2016: LONGERON. CRACKED. CRACK ON LONGERON 3R BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG.18.
- [SDR DALA2016080105692](https://openairdocs.org/sdr/DALA2016080105692), Jul 29, 2016: CUSP WEB. CRACKED. CRACK ON LT CUSP WEB OF STA Y642 BETWEEN STA X54 TO X60 AT PAX CABIN. REPAIRED IAW SRM 53-05 FIG 131A-14, 51-30-2, 51-10-3 PAR 21,14, 51-30-5 AND 51-10-3.

All 154: https://openairdocs.org/deregistered/N905DE-2022-11-29/reports.md

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