N932VJ1968 Douglas DC-9-31
This N-number isn't registered right now. Below is its last known registration, canceled Feb 7, 2005.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched16 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Alameda Corp Trustee
- Owner type
- Corporation
- City, state
- San Antonio, TX
- Certificate issued
- May 21, 2003
- Canceled
- Feb 7, 2005
- Airworthiness
- Standard · Transport
- Airworthiness date
- Sep 15, 1978
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
- 1968
- Serial number
- 47189
- 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
- ACEEFB
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- 2003 – 2005Alameda Corp TrusteeSan Antonio, TX
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 (16)
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.
- Wings · spar · crackedMar 17, 2000
PIT - FOUND 4 INCH CRACK IN LEFT UPPER FORWARD SPAR CAP ENGINE MOUNT, STATION 965 LONG 14 LT, LT ENGINE PYLON. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EO 5490D056, DOUGLAS DWG SRO 954004 AND 54427. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · stop · crackedMar 14, 2000
PIT - FOUND DOOR STOP CRACKED .25 INCH, TOP AFT MAIN ENT. INSTALLED DOUBLERS PER SRO 09530252. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar · crackedFeb 24, 2000
PIT - FOUND SPAR CAP 1.25 INCH CRACK, LEFT WING AFT SPAR STATION 164 LOWER INBOARD FLAP STUD. INSTALLED DOUBLER PER J9-15-93807 (EO 5788D220). (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Landing gear · socket · failedSep 9, 1999
PIT-CMH - FLT 933 - AFTER TAKEOFF AND LANDING GEAR RETRACTION THE LEFT GEAR GREEN LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT LANDING GEAR GREEN LIGHT INDICATION SOCKET. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · controller · failedAug 15, 1999
PIT - ITH - FLT 1572 - AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PRESSURIZATION CONTROLLER. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · actuator · failedAug 8, 1999
ROC-DCA - FLIGHT 887 - DURING LANDING GEAR EXTENSION, ON APPROACH, THE NOSE GEAR DID NOT EXTEND. THE LANDING GEAR WAS CYCLED BUT THE NOSE GEAR REMAINED RETRACTED. THE EMERGENCY GEAR EXTENSION LEVER WAS USED AND THE NOSE GEAR EXTENDED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · crackedFeb 22, 1999
PIT - DURING C-6 CHECK, FOUND 1.5 INCH LONGERON CRACKED IN HALF LONGERON NR 4 AND NR 5 AT STATION 756 LT SIDE. INSTALLED DOUBLER PER SRM 53-02 FIG 18, 119-5572 SPLICE AND 119-5573 LONGERON. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · crackedFeb 22, 1999
PIT - DURING C-6 CHECK, FOUND LONGERON CRACKED IN HALF 2 INCHES BY 1 INCH, DISCONTINUITY AT INTERSECTION OF L5R AT STATION 639. DETECTED BY EDDY CURRENT. REPAIRED PER SRM 53-02 FIG 18. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery · dischargedApr 26, 1998
IND - THE CARRY AROUND EMERGENCY LIGHT AT THE ENTRANCE DOOR WAS DIM. MAINTENANCE REPLACE THE CARRY AROUND EMERGENCY LIGHT BATTERY. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · power supply · inoperativeDec 27, 1997
PIT - EMERGENCY LIGHTS AT AFT EXIT WINDOWS ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 16 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