N946VJ1967 Douglas DC-9-32
This N-number isn't registered right now. Below is its last known registration, canceled Jul 17, 2003.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched21 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- US Airways INC
- Owner type
- Corporation
- City, state
- Arlington, VA
- Certificate issued
- Apr 7, 1983
- Canceled
- Jul 17, 2003
- Airworthiness
- Standard · Transport
- Airworthiness date
- Oct 29, 1976
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
- 1967
- Serial number
- 47026
- 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
- AD2556
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- 1983 – 2003US Airways INCArlington, VA
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 (21)
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 · battery · dischargedJan 8, 1999
PHL - THE COCKPIT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE COCKPIT EMERGENCY LIGHT. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · power supply · inoperativeOct 28, 1998
DTW - THE GALLEY AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE GALLEY AREA EMERGENCY LIGHT POWER SUPPLY. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · control panel · failedMar 20, 1998
CMH - FLT 920 - ON TAKEOFF THE AC CROSSTIE LOCKOUT AND RIGHT GENERATOR OFF LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT GENERATOR CONTROL PANEL. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · battery pack · dischargedAug 18, 1997
IND - FOUND GALLEY DOOR EMERGENCY DOOR LIGHT WEAK. MAINTENANCE REPLACED THE BATTERY PACK. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead · crackedApr 9, 1996
PIT - DURING C-4 CHECK INSPECTION, FOUND A 1.25 INCH AND 3 INCH CRACK IN REAR PRESSURE BULKHEAD Z-63 LEFT SIDE OF DOOR FRAME AT STATION 996. CUT OUT CRACKED AREAS AND INSTALLED FILLER AND DOUBLER PER USAIR EA NR 32410A. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead doubler · crackedJan 9, 1996
PIT - DURING AGING VISIT 89K, FOUND 1.125 INCH CRACK IN 591013-13 BULKHEAD DOUBLER, 1.25 INCH CRACK IN 5910130-22 DOUBLER, .25 INCH CRACK IN 5910130-13 DOUBLER, 4.25 INCH CRACK IN THE RADIUS OF 5910130-13 DOUBLER. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedMar 15, 1995
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION UNDER FWD BELLY AT MARKER BEACON ANTENNA. INSTALLED DOUBLER REPAIR PER USAIR EA 29959. (W)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedMar 7, 1995
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION STATION 912-996 SKIN PANEL 5919707 LONGERON 26R TO 26L SKIN PANEL 5911424 LONGERON 18R-26R. SPLICED IN 2 EACH SKIN PANELS PER USAIR EA 29955. (W)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedMar 6, 1995
PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION LONGERON NR 1 AND SKIN LAP JOINT STATION 263-275 NR ADF LOOP AND STATION 300-308 NR 2 ADF LOOP ANTENNA. CLEANED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 29 AND USAIR EA 29614A. (W)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · damagedFeb 28, 1995
PIT - DURING Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR INSTALLED STATION 313-332 LONGERON 22-24 RIGHT. INSTALLED CLASS I REPAIR PER SRM 53-04 FIG 12B. (W)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 21 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