N965N1969 Douglas DC-9-31
This N-number isn't registered right now. Below is its last known registration, canceled Mar 20, 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
- Individual owner
- City, state
- Mcminnville, OR
- Canceled
- Mar 20, 2013
- Airworthiness
- Standard · Transport
- Airworthiness date
- Oct 2, 1969
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
- 1969
- Serial number
- 47417
- 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
- AD6FE5
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- 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, 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.
- Air conditioning and pressurization · pressure system · malfunctionedJun 20, 2005
LEVEL AT FL 340, FLIGHT WAS DIVERTED DUE TO WEATHER. RED MASTER WARNING AND CABIN PRESS LIGHTS ILLUMINATED AS CABIN ALTITUDE CLIMBING THROUGH 10,000 FT. COM PROCEDURES COMPLIED WITH BUT DID NOT HELP. CREW INITIATED RAPID DESCENT AND DECLARED EMERGENCY. CABIN NEVER WENT ABOVE 11,000 FT AND O2 MASKS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedAug 4, 2004
DURING L-CHECK, FOUND CRACK IN FUSELAGE FRAME AT BS 1019 BELOW L14L. REPAIRED IAW EA 99-200165.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedAug 3, 2004
DURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 RBL 20. REPAIRED PER EA 99-200164.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Hydraulic power · relief valve · failedJan 28, 2004
AT ABOUT 100 MILES OUT FROM LANDING THE AIRCRAFT, PRODUCED SMOKE IN THE COCKPIT. ALSO NOTICED THE LOSS OF THE RT HYDRAULIC SYSTEM AS QUANTITY WENT TO ZERO ACCOMPANIED BY 'R HYD PRES LOW' LIGHT. FLIGHT CREW DECLARED AN EMERGENCY, REQUESTED CFR, AND LANDED UNEVENTFULLY AT MCO. CREW SUSPECTED THAT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead · crackedDec 9, 2002
During an Hck in ATL and while accomplishing an inspection, a crack was found in the aft pressure bulkhead doorjamblower sill channel. The crack is in the upper flange of the channel and extends approximately .75" through a screw hole. Repaired per EA 99-190869.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · cap · corrodedNov 25, 2002
During HCK in ATL, corrosion was found in the upper flange of the center wing skin cap. Corrosion was out of limits. Repaired per EA 99-190861.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · door frame · crackedJul 10, 2001
DURING L-CK IN DHN, A CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE DOOR JAMB. REPAIRED PER AMITASK 5330-01130-2C. REPAIRED PER EA 99-183995.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · door frame · crackedJul 10, 2001
DURING L-CK IN DHN, A CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE DOOR JAMB. REPAIRED PER AMITASK 5330-01130-2C. REPAIRED PER EA 99-183995.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedJul 10, 2001
During L-CK in DHN, A crack was found in the upper aft corner of the FWD Cargo Jamb. Repaired per EA 99-183995.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · volt regulator · failedFeb 2, 2001
DURING TAKEOFF ROLL, THE RIGHT GENERATOR FAILED. NUMEROUS ELECTRICAL SYSTEM ANNUNCIATORS LIT UP INDICATING LEFT GENERATOR DID NOT CROSSTIE SUCCESSFULLY. CREW ABORTED TAKEOFF AT 120 KTS. AIRCRAFT STOPPED SAFELY AND TAXIED TO GATE. CROSSTIE ACCOMPLISHED DURING TAXI. MAINTENANCE REPLACED THE RIGHT…
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