N917DE1993 Mcdonnell Douglas Aircraft Co MD-88
This N-number isn't registered right now. Below is its last known registration, canceled Sep 16, 2019.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched77 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Delta Air Lines INC
- Owner type
- Corporation
- City, state
- Atlanta, GA
- Certificate issued
- Sep 17, 1993
- Canceled
- Sep 16, 2019
- Airworthiness
- Standard · Transport
- Airworthiness date
- Aug 19, 1993
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Mcdonnell Douglas Aircraft Co
- Model
- MD-88
- Year
- 1993
- Serial number
- 49958
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 142
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- ACB0FC
Engine
- Make and model
- P & W Jt8d Series
- Type
- Turbo-fan
- Power
- 7,700 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1993 – 2019Delta Air Lines INCAtlanta, GA
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (0)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (77)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Ice and rain protection · terminal block · burnedApr 13, 2017
RETURNED TO DEPARTURE DUE TO AN ACRID ODOR IN THE FLIGHT DECK REPORTED TO BE FROM THE F/O'S WINDSHIELD. MAINTENANCE FOUND TERMINAL BLOCK R5-38 AND THE F/O'S WINDSHIELD BURNED AT CONNECTION P WHICH IS THE GROUND SIDE FOR WINDOW ANTI-ICE. THE TERMINAL BLOCK, WINDOW, AND WINDOW HEAT CONTROLLER WERE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · jackscrew · wornMar 13, 2017
WEAR CHECK FAILED STEP 50. READS .045. REPLACED THE HORIZONTAL JACKSCREW ASSY IAW WC 2742-4540. ALSO PERFORMED WORKCARD 2740-01113-08 WEAR CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · panel · crackedMar 8, 2017
A 12 INCH CRACK IN RT WING FIXED T/E PANEL. REMOVED DAMAGE , INSTALLED A REPAIR IAW SRM 51-90-0.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · battery pack · inoperativeJan 23, 2017
CEILING EMERGENCY LIGHTS 4DC & 24DC INOPERATIVE. REPLACED THE BATTERY PACKS IAW AMM 33-53. OPS CHECKED OK. OK FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · latch · wornJun 4, 2016
UPPER LEFT TAIL CONE ATTACH LATCH LOCK IS WORN. R & R AND ADJUSTED LATCH IAW AMM 53-53-00.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · dentedSep 14, 2015
ACFT ON RT FUSELAGE, SIGNIFICANT DENT 8.5" FORWARD AND 11.8" ABOVE THE ALTERNATE STATIC PORT CENTER. ALSO, THERE ARE 8 OTHER SMALL DENTS WITHIN THE CONTROLLED AREA 18", WHICH EXCEEDS THE MAXIMUM OF 2 DENTS, 1 SIDE IN THIS AREA. NR FOR ADDITIONAL INFORMATION 044-0001: 3411-2108/001 00197 COMPLIED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · wornSep 14, 2015
VERTICAL STABILIZER RT SIDE EXTERIOR HAS 7 X .3750" AREA OF DEEP WEAR APPROXIMATELY .10" ABOVE & FWD OF HORIZONTAL STABILIZER CTR AFT SPAR. NR FOR ADDITIONAL INFORMATION 001-0341:5300-2551/010 00141. REPAIRED IAW PRI 539282-14, REV "0" AND ER/A 539282-14, REV ORIGINAL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedSep 14, 2015
SKIN HAS A .5" LONG CRACK, LATERAL AXIS, AT BS 1436.5. OTBD END OF CRACK IS 1.25" INBD OF L4R RIVET ROW. INSTALLED REPAIR IAW SRM 53-01, FIG 4, SHT 4.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedSep 12, 2015
TAIL INTERIOR, AFT CANTED FRAME AT BS 1510 HAS .5 INCH LONG CRACK AT CONE ALIGN PIN, 11:30 O`CLOCK POSITION. REPAIRED IAW PRI 538315-14, REV "0" AND ER/A 538315-14, REV ORIGINAL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · shear tie · corrodedSep 10, 2015
AFT CARGO HAD SIGNS OF CORROSION ON SHEAR TIE BS 1149 BETWEEN LONGERONS 29 AND 30R. REMOVED AND REPLACED THE SHEAR TIE IAW DWG 9936074.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 77 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026