N931L1968 Douglas DC-9-32
This N-number isn't registered right now. Below is its last known registration, canceled Oct 19, 2005.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched35 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 19, 2026- Last registered owner
- Alameda Corp Trustee
- Owner type
- Corporation
- City, state
- San Antonio, TX
- Certificate issued
- Feb 7, 2005
- Canceled
- Oct 19, 2005
- Airworthiness
- Standard
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-9-32
- Year
- 1968
- Serial number
- 47173
- 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
- ACEA5A
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- 2005Alameda Corp TrusteeSan Antonio, TX
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (35)
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 · amplifier · defectiveAug 24, 2001
TWO TIMES IN FLIGHT THE RH TEMPERATURE CONTROL VALVE WENT FULL HOT IN AUTO. WAS OK IN MANUAL CONTROL. CHANGED THE RH TEMPERATURE CONTROL AMPLIFIER, PN 607146-2-1. CHANGED BOTH WATER SEPARATORS ACCOUNT SMOKE CONTAMINATION, PN 1794608-1. CHECK-C 7-4-00 MCI.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · power supply · defectiveDec 3, 2000
THE EGRESS LIGHTS WERE INTERMITTENTLY GOING ON AND OFF DURING FLIGHT. REPLACED THE EGRESS LIGHT POWER SUPPLY. CHECK-C 7-4-00 MCI.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · connector · looseDec 2, 2000
THE LAST 4 ROWS OF EGRESS LIGHTS FLICKERED IN CLIMB. RESEATED THE CONNECTION OF THE EGRESS LIGHTING. CHECK-C 7-4-00 MCI.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · frame · crackedSep 8, 2000
DURING OP 15 MAINT CHECK FORMER CASTING WAS CRACKED AT STA 658, LBL 58 INCHES. REMOVED AND REPLACED WITH NEW CASTING PER DOUGLAS DRAWING 9919615, TWA ARA 17117A, DOUGLAS DRAWING 5918374, AND DOUGLAS DRAWING 5910537.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · retainer · corrodedSep 8, 2000
DURING OP 15 MAINT CHECK AT STA 996, RBL 0 TO 24 INCHES, THE TOP RT CAM LOCK RETAINER ON AFT SIDE OF BULKHEAD HAD HEAVY CORROSION UNDER IT. CUT OUT CORRODED T ANGLE WEB. SPLICED PER SRM 53-01 PAGE 10. PAINTED PER SRM 51-10-3. MADE WEB REPAIR PER SRM 51-70-4 PAGE 4 AND 5.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · crackedSep 6, 2000
DURING OP 15 MAINT CHECK, THE FUSELAGE TO WING TIE ANGLE WAS CRACKED AT STA 605, BETWEEN LONGERON 22L AND 23L. REPLACED WING TO FUSELAGE TIE ANGLE PER DOUGLAS DRAWING 5910068.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar · crackedSep 6, 2000
DURING OP 15 MAINT CHECK ON THE RT WING HAD A CRACK INDICATION ON REAR SPAR AT TOP HOLE FOR CENTER FLAP HINGE MOUNT AT STA XW251. REPAIRED HOLE PER DOUGLAS DRAWING JO6022.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · spar · crackedSep 1, 2000
DURING OP 15 MAINT CHECK, FOUND ON RT WING A CRACK APPROX .0625 INCH LONG ON REAR SPAR AT XW154, I/B FLAP HINGE LOWER O/B HOLE. CRACK CONTAINED PER NDT TWA 51-10-03 PART 6 HFEC. MADE REPAIR DOUBLER AND INSTALLED PER REPAIR DRAWING JO60271. REPAIR WORK IN CONJUNCTION WITH NON ROUTINE 02-193.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · galley track · corrodedAug 30, 2000
DURING OP 15 MAINT CHECK, FOUND GALLEY TRACK NUMBER 1 AT STA 237 TO 247, LBL 44 INCHES, WAS CORRODED. REPLACED TRACK FROM STA 200 TO 301. INSTALLED SPLICE PER SRM 53-05 FIG 4F.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedAug 30, 2000
DURING OP 15 MAINT CHECK, FOUND CRACK IN FUSELAGE SKIN AT NOSE GEAR STRUT DOOR, AFT HINGE, LT SIDE. REPAIRED CRACK IN SKIN PER SRM 53-05 PAGE 169 TO 171, FIG 62, SHEETS 1 AND 2.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 35 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026