N905AX1967 Douglas DC-9-32F
This N-number isn't registered right now. Below is its last known registration, canceled Apr 27, 2012.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched90 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Individual owner
- City, state
- Xxx, OK
- Canceled
- Apr 27, 2012
- Airworthiness
- Standard · Transport
- Airworthiness date
- Nov 7, 1968
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-9-32F
- Year
- 1967
- Serial number
- 47147
- 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
- AC81D5
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 2012Individual ownerXxx, OK
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 (90)
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 · dischargedDec 8, 2007
CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead · crackedApr 23, 2007
AFT PRESSURE BULKHEAD SKIN CRACKED AT 4:00 POSITION ADJACANT TO DOOR PIN ALIGNMENT RECEPTACLE. REPAIRED CRACK IN SKIN IAW DWG 5934886-502 AND REA D953-55733.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · cusp web · crackedApr 23, 2007
CUSP WEB CRACKED AT STA 598 TO 617 AT BUTT LINE 58 LEFT. REPAIRED AREA OF WEB IAW DC9 SRM 53-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · skin · crackedApr 20, 2007
FUSELAGE SKIN CRACKED 2 PLACES FS 1087 LONGERON 3 - LONGERON 4 RIGHT. REPAIRED FUSELAGE SKIN AT STA 1095, LONGERON 3 - 4 RIGHT IAW DC9 SRM 53-04.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · jackscrew · obstructedFeb 9, 2007
HORIZONTAL STABILIZER JACKSCREW FOUND TO BE HITTING MECHANICAL STOPS DURING OPERATION. REMOVED AND REPLACED JACKSCREW IAW DC9 MM, REF WORK ORDER 600265725.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery · dischargedSep 23, 2006
EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedApr 18, 2005
EVIDENCE OF CORROSION EMITTING FROM FINGER DOUBLER JUST FORWARD OF FS 332 TO 351, LONGERON 26 RT OUTBOARD AND INBOARD SIDES. REPAIRED CORRODED SKIN IAW DC-9 SRM 53-04.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · panel · crackedApr 15, 2005
RIGHT BUTT LINE '0' ANGLE FITTING COMMON TO KEEL WEB AND RIGHT SLANT PANEL CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-5.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedApr 14, 2005
SKIN BULGING AND RIVET HEAD POPPED AT STA 949, LONGERON 24 LEFT. REPLACED LONGERON 24 LEFT, FS 927-996 IAW DC-9 SRM 51-30-2, 51-30-5 AND 53-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · corrodedApr 14, 2005
SKIN BULGING, RIVETS CUPPED AT STA 342, LONGERON 29 RIGHT AND LONGERON 28 RIGHT. REMOVED FASTENERS, EVALUATED. SPLICED LONGERON IAW DC-9 SRM.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 90 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