N93351971 Douglas DC-9-31
This N-number isn't registered right now. Below is its last known registration, canceled Feb 6, 2013.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched41 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Wells Fargo Bank Northwest NA Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Nov 9, 2007
- Canceled
- Feb 6, 2013
- Airworthiness
- Standard · Transport
- Airworthiness date
- Nov 27, 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 dataAirframe
- Manufacturer
- Douglas
- Model
- DC-9-31
- Year
- 1971
- Serial number
- 47337
- 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
- ACF3D5
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- 2007 – 2013Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT
- until 1932Individual ownerLincoln, NE · different airframe: Arrow Aircraft & Motors Arrow Sport S/N 351
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.
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 (41)
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.
- Doors · door · out of rigJan 18, 2007
UNABLE TO OPEN MAIN CABIN DOOR, TRIED FROM INSIDE AND OUTSIDE OF AIRCRAFT. MAINTENANCE DISCOVERED UPPER FORWARD CORNER OF MAIN CABIN DOOR BINDING AGAINST DOOR CUTOUT STRUCTURE. PRESSED IN ON UPPER FORWARD CORNER AND WAS ABLE TO OPEN MAIN CABIN DOOR. PRESSURIZED AIRCRAFT TO 3.5 PSI, DOOR JAMMED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ice and rain protection · duct · bindingFeb 10, 2002
FLIGHT DIVERTED TO AN AIRPORT WITH A LONGER RUNWAY WHEN THE CREW DETERMINED THAT THE LEFT WING SLATS WOULD NOT EXTEND. THE AIRCRAFT DID ROLL TO THE LEFT AND THE SLAT DISAGREEMENT LIGHT DID ILLUMINATE. FOLLOWED COM PROCEDURES AND MADE AN UNEVENTFUL LANDING AT GRR AT 86,000 LBS AND 253 KTS.…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · crackedJun 12, 2001
During A H Ck inATL, a crack was found in the lower skin of the LH inbd slat at station Xis =136.42. Stopped drilled and doubler installed 2014-t6 AL. Repaired per EA 99-181273
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · stiffener · crackedJun 8, 2001
During H ck in ATL, two .75" long cracks were found in the Sta 756 bulkhead. The cracks are located in the upper ends of the verticle stiffeners at x=-11 and x=-22. Repaired per EA 99-181222. Material 2014-t6511 AL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · stiffener · crackedJun 8, 2001
During HCK in ATL., two .75" cracks were found in the 756 bulkhead. The cracks are located in the upper ends of the verticle stiffeners at sta X=-11. EA 99-181222.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · pressure panel · crackedJun 7, 2001
During H ck in ATL, two cracks were found in the horizontal pressure panel at station 105 at x=25 and x=27. The crack at x=25 is typical of the cracks repaired in the dc-9 trm, 53-10-02 except this crack is 2.4" long. The crack at station x=27 is 1/2" long. Material 0.040" 2024-t3 Al. Repaired per…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · doubler · crackedJun 7, 2001
During Hck in ATL, A crack was found on the upper fuel tank access panel doubler. Repaired per EA 99-181239.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · pressure panel · crackedJun 7, 2001
During Hck in ATL, Two cracks were found in the horizontal pressure panel at station 105 at X=25 2.4" and X=27 .5"long. Repaired per EA 99-181213.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · seat track · corrodedJun 6, 2001
During H ck in ATL, The outboard seat track x=-22 rh was found corrosion between 588 and 746. Repaired per EA 99-1812575.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · pan · crackedMay 31, 2001
During H-check found crack on RH aft emergency exit door lower pan. Repaired per EA. 99-181208.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 41 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