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Aircraft record

N8934E1968 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 Jan 2, 2008.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched59 service difficulty reports

Registration
Deregistered
Last based in
Minneapolis, MN
owner city / state
Owners
1
since 2004
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
59
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Northwest Airlines INC
Owner type
Corporation
City, state
Minneapolis, MN
Certificate issued
Jun 16, 2004
Canceled
Jan 2, 2008
Airworthiness
Standard · Transport
Airworthiness date
Jan 14, 1968

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
1968
Serial number
47143
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
AC5362

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. 2004 – 2008Northwest Airlines INCMinneapolis, MN

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 (59)

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.

  • Flight controls · trim system · out of rigJul 2, 2006

    AS THE AIRCRAFT ACCELERATED FOR TAKEOFF THE CREW NOTED THAT THE PLANE ATTEMPTED TO ROTATE AND LIFT OFF ON ITS OWN PRIOR TO SCHEDULED VR SPEED. NO OTHER INDICATIONS NOTED TO EXPLAIN EARLY ROTATION BUT BECAUSE OF A -STIFF- FEELING YOKE, THE TAKEOFF WAS SAFELY ABORTED AT ABOUT 100 KTS. MAINTENANCE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · cap · crackedOct 22, 2001

    During H ck in Atl, The rear spar, lower cap aft flange at approx. at approximately sta xrs 80 was found to be corroded and cracked. The damage was blended out and protected against corrosion. Material 2024-t3511 EA 99-185232

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door frame · crackedOct 17, 2001

    During H-ck in Atl inspection of subject area revealed a typical crack less than 2 inches in the door corner. Repair was accomplished per sr09530117 and EA 99-185210. Section 1 provides for an alternate fastener configuration due to restricted access and structural interferance as shown on figure 1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · door frame · crackedOct 17, 2001

    During H-ck in ATL inspection of subject area per Ref A revealed a typical crack under 2 inches in the door corner. Repaired per EA and SRM 53-04. Reported as part of repair assesment program. Repaired EA 99-185209.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · support fitting · crackedOct 17, 2001

    During H ck at ATL base maintenance, two 1.00" cracks were found on verticle stabilizer actuator support fittings. Both cracks emenated from the end fastener hole forward the edge of the firrigns flange. The repair involved the installation of a repair doubler at each location with a min of 5…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · transformer · overheatedMay 22, 2001

    ON DESCENT, THE LEAD FLIGHT ATTENDANT REPORTED A SMOKE ODOR IN THE AREA OF THE FORWARD FLIGHT ATTENDANT JUMPSEAT WHICH DISSIPATED IN 1-2 MINUTES. FOUND THE LEFT FORWARD READING LIGHT TRANSFORMER WIRING COVER MELTED AND BURNT. REPLACED TRANSFORMER T1-52, WIRING TERMINAL ENDS, AND TERMINAL COVER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine oil · connector · damagedAug 5, 2000

    DURING CRUISE FLIGHT, THE LEFT ENGINE OIL TEMPERATURE INDICATION ROSE TO 145 DEGREES. THE FLIGHT CREW FOLLOWED COM PROCEDURES, DECLARED AN EMERGENCY, SHUT DOWN THE LEFT ENGINE PRECAUTIONARY, AND LANDED AT MEM WITHOUT INCIDENT. MAINTENANCE DETERMINED THIS TO BE AN INDICATION PROBLEM AND REPLACED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · shaft · shearedAug 3, 2000

    DURING DESCENT INTO MSP, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT PRECEEDED BY AN OIL LOW PRESSURE LIGHT INIDICATION AND A RIGHT ENGINE GENERATOR OFF LIGHT INDICATION. THE FLIGHT CREW FOLLOWED THE EMERGENCY CARD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN FUEL PUMP.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · stop · wornJun 27, 2000

    DURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ROLL TO THE LEFT ON SLAT EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND STOPS ON LEFT TELESCOPING DUCT WORN. REPLACED STOPS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · brake fuse · leakingNov 26, 1999

    LEFT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO AFTER TAKEOFF. CREW DECLARED A YELLOW EMERGENCY AND FLIGHT WAS RETURNED TO YYZ. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT LOWER BRAKE FUSE LEAKING. REPLACED BRAKE FUSE. LEAK AND OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED…

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

Showing the 10 most recent of 59 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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