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Aircraft record

N8926E1967 Douglas DC-9-31

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 23, 2010.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched42 service difficulty reports

Registration
Deregistered
Last based in
Atlanta, GA
owner city / state
Owners
1
since 2009
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
42
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Delta Air Lines INC
Owner type
Corporation
City, state
Atlanta, GA
Certificate issued
Dec 31, 2009
Canceled
Nov 23, 2010
Airworthiness
Standard · Transport
Airworthiness date
Mar 21, 1977

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 data

Airframe

Manufacturer
Douglas
Model
DC-9-31
Year
1967
Serial number
45863
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
85
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
AC4FF1

Engine

Make and model
P & W Jt8d-1
Type
Turbo-jet
Power
14,000 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
  1. 2009 – 2010Delta 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, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

ADs 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 (42)

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.

  • Nacelles and pylons · web · buckledSep 24, 2009

    DURING ENGINE CHANGE FOUND PYLON VERTICAL WEB BUCKLED BETWEEN UPPER AND LOWER SPARS FOR AFT ENGINE MOUNT AT XN39.250. REPAIRED PER EA 99-216590.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedDec 21, 2007

    DURING "H" CHECK, FOUND CRACKS IN SKIN AT FORWARD PASSENGER ENTRY DOOR CUTOUT AT AFT DOOR STOPS NR 3 AND NR 4. REPAIRED PER EA 99-211049.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · inoperativeAug 16, 2007

    TAIL CONE PATH LIGHTS INOP. REPLACED BATTERY PACK. OPERATION CHECKS GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Lights · power supply · inoperativeAug 8, 2007

    TAIL COMPARTMENT EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED POWER SUPPLY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · inoperativeJul 26, 2007

    AFT EMERGENCY CAT-WALK LIGHT OUT DURING EMERGENCY LIGHT CHECK. REPLACED BATTERY PACK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · line · leakingApr 7, 2003

    ON CLIMB SHORTLY AFTER GEAR RETRACTION THE RIGHT HYDRAULIC PRESSURE BEGAN FLUCTUATING BY FLUID LOSS. THE THE LEFT HYDRAULIC SYSTEM LOST PRESSURE AND LOST FLUID. THE LANDING GEAR WAS LOWERED BY ALTERNATE METHOD. FLIGHT DIVERTED TO IND AND LANDED SAFELY. MAINTENANCE FOUND 3 HYDRAULIC LINES…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · web · crackedJan 14, 2002

    During Hck in ATL, A crack was found in the lower outboard corner of the diagonal web in the L/H engine pylon just forward of the rear spar. Repaired per EA 99-185474.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · crackedJan 9, 2002

    DURING HCK IN ATL, A CRACK WAS FOUND IN THE UPPER VERTICLE FLANGE OF THE STATION 237 FLOORBEAM AT X=6. REPAIRED PER EA 99-185447.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · corrodedJan 8, 2002

    During HCK in ATL, corrosion was found on the R/H wing upper skin doubler flange attachment holes for the fuel access door. Repaired per EA 99-185451.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · wire · brokenMay 17, 1998

    DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ON CATWALK ILLUMINATED WITH SWITCH IN OFF POSITION. REPAIRED BROKEN WIRING TO SPLICE NEAR TAILCONE BATTERY PACK. OPERATIONAL CHECK NORMAL.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 42 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

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