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Aircraft record

N8960E1968 Douglas DC-9-31

DeregisteredNot yet verified by ownerSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jun 10, 2013.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched50 service difficulty reports

Registration
Deregistered
Last based in
Mcminnville, OR
owner city / state
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
50
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Mcminnville, OR
Canceled
Jun 10, 2013
Airworthiness
Standard · Transport
Airworthiness date
Mar 5, 2001

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
45869
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
AC5DFB

Engine

Make and model
P & W Jt8d Series
Type
Turbo-jet
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
  1. until 2013Individual ownerMcminnville, OR

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 (50)

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.

  • Lights · power supply · dischargedFeb 19, 2009

    DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT HAD ALL (3) OF THE CATWALK LIGHTS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · fuse · failedJul 26, 2008

    DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE AFT RT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED FUSE IN THE PERTINENT CIRCUIT BOARD. OPERATIONAL CHECK WAS GOOD. (A)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · fuse · inoperativeJul 26, 2008

    DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-17 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED FUSE IN THE PERTINENT CIRCUIT BOARD AT THE AFT RIGHT EXIT SIGN. OPS CHECK WAS GOOD. (A)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Lights · light · inoperativeNov 3, 2007

    TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BULBS AND POWER PACK. OPERATION CHECKS GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · crackedJan 23, 2007

    DURING "H" CHECK, FOUND CRACK IN FORWARD CARGO COMPARTMENT LONGERON AT S29L BETWEEN BS 560-579. REPAIRED PER EA 99-208433.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · duct · damagedJul 28, 2006

    AS THE AIRCRAFT WAS CLIMBING THROUGH FL180 THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED. CREW NOTED AT THAT TIME THAT THE CABIN WAS AT 10,000 FEET AND THAT THEY COULD NOT HOLD VESSEL PRESSURE WITH LESS THAN 70% N1. THE CREW INITIATED A DESCENT TO FL130 AND RETURNED BACK TO DEPARTURE POINT. A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor support · crackedFeb 16, 2001

    DURING H-CHECK FOUND CRACK IN THE RADIUS OF THE CABIN FLOOR SUPPORT. THE CRACK IS LOCATED IN THE VERTICAL WEB OF THE T-CAP, BELOW THE RADIUS. REPAIRED PER EA. 99-180963.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · corrodedFeb 14, 2001

    During H-check found corrosion on the horizontal flange of the floor support tee on RHS of the aft pressure bulkhead. Repaired per EA. 99-180937.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rib · crackedFeb 13, 2001

    During H-check found LH wing leading edge ribs cracked. Repaired per EA. 99-180959.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rib · crackedFeb 13, 2001

    During H-check found LH wing leading edge ribs cracked. Repaired per EA. 99-180959.

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

Showing the 10 most recent of 50 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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