N992Z1967 Douglas DC-9-31
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 matched66 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
- Feb 7, 2005
- Canceled
- Oct 19, 2005
- Airworthiness
- Standard · Transport
- Airworthiness date
- Apr 29, 1975
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
- 1967
- Serial number
- 47095
- 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
- ADDC50
Engine
- Make and model
- P & W Jt8d-9 Ser
- Type
- Turbo-jet
- Power
- 14,500 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 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 (66)
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.
- Fuselage · angle · crackedApr 6, 2001
DURING OP 15 MAINT CHECK FOUND POSSIBLE CRACK IN SUPPORT ANGLE AT STA 1046, LONGERON 3L. ACCOMP NDT USING HFEC PER 51-00-03, PART 6 AND FOUND 1 .25 IN LONG CRACK. INSTALLED DOUBLER PER SRM 53-05, PAGE 506, FIG 23B, AND SRM 51-30-5.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floorbeam · corrodedApr 5, 2001
DURING OP 15 MAINT CHECK AT STA 965, RBL 5 INCHES AND RBL 14 INCHES, BOTTOM OF CABIN FLOORBEAM HAD A BULGE. REMOVED CORRODED SECTIONS OF FLOORBEAM. INSTALLED REPAIR DOUBLERS AND ANGLES PER SRM 53-05, FIG 79, AND ARA 17099.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedMar 30, 2001
DURING OP 15 MAINT CHECK FOUND POSSIBLE CRACK IN SKIN AT STA 1104, LONGERON 5L TO 4L. COMPLIED WITH ARA 17573 REFERRING TO LISTED SRM 53-04, FIG 27 AND SRM 51-01 PARAGRAPH 3B1.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · skin · crackedMar 29, 2001
DURING OP 15 MAINT CHECK FOUND FUSELAGE SKIN CRACKED AT STA 1079, CANTED BULKHEAD, LONGERON 3L AND 5L. INSTALLED REPAIR DOUBLER PER SRM 53-04, FIG 27, PAGE 143 AND SRM 51-01, PAGE 2 PARAGRAPH 3.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedMar 28, 2001
DURING OP 15 MAINT CHECK FOUND CORROSION ON SKIN AT STA 351 ON RT SIDE AT LONGERON 29R. INTERIM REPAIR WAS INSTALLED. REPAIRED PER SRM 53-04, FIG 38, SHEET 24, AND ARA 17539.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedMar 27, 2001
DURING OP 15 MAINT CHECK FOUND CRACK IN SKIN AT STA 1087, LONGERON 4R. ACCOMP HIGH FREQ EDDY CURRENT AND CONFIRMED .75 INCH CRACK PER 51-00-03 PART 6. REPAIRED PER SRM 53-04, FIG 27.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · cargo track · corrodedMar 20, 2001
DURING OP 15 MAINT CHECK IN THE FWD CARGO COMPT, THE RT FWD CARGO TRACK WAS BADLY CORRODED, STA 218 TO 370. MADE NEW TRACK FROM STOCK. DRILLED HOLES FROM OLD TRACK AND COUNTERSUNK HOLES. TREATED AND PRIMED TRACK. ACCOMPLISHED PER SPM 6-70-01.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · web · corrodedMar 15, 2001
DURING OP 15 MAINT CHECK FOUND MEMBRANE SKIN UNDER CABIN FLOOR AT STA 200 TO 218, RBL 57, WAS CORRODED. FABRICATED NEW MEMBRANE AND INSTALLED RIVETS AND BOLTS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · crackedMar 14, 2001
DURING OP 15 MAINT CHECK FOUND LONGERONS 17R, 12R, AND 16R WERE CRACKED AT STA 965. SPLICED IN NEW LONGERON FROM STA 965 TO 996 PER SRM 53-02, FIG 18.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedMar 9, 2001
DURING OP 15 MAINTENANCE CHECK, FLOOR SUPPORT AT STA 160 TO 200, RBL 47 IN, WAS CORRODED. FABRICATED NEW FLOOR SUPPORT, TREATED, PAINTED AND INSTALLED FASTENERS.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 66 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