N93391969 Douglas DC-9-31
This N-number isn't registered right now. Below is its last known registration, canceled Sep 23, 2009.
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 20, 2026- Last registered owner
- Individual owner
- City, state
- Marana, AZ
- Canceled
- Sep 23, 2009
- 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-9-31
- Year
- 1969
- Serial number
- 47382
- 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
- ACF461
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 2009Individual ownerMarana, AZ
- until 1939Co-ownersRichmond, VA · different airframe: Arrow Aircraft & Motors Arrow Sport S/N 355
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 (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.
- Lights · battery pack · inoperativeJul 12, 2008
DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 18-21 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED FUSE AND THE BATTERY PACK. OPERATIONAL CHECK WAS GOOD. (A)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · relief valve · leakingAug 27, 2002
DURING GEAR UPLATCH CHECK AFTER TAKEOFF, THE RIGHT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO. GEAR DOOR OPENED AND MAIN LANDING GEAR EXTENDED AS THE HYDRAULIC SYSTEM FAILED. CREW ENSURED GEAR WAS PROPERLY EXTENDED PER COM. FLIGHT RETURNED TO MDT AND LANDED SAFELY. MAIN GEAR DOORS WERE DAMAGED…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead · crackedJul 9, 2002
During HCK in ATL, a crack was found on the LH portion of the APB Door cutout upper jamb. A repair of the upper jamb area was extended to incorporate the the cracked area. Repaired per EA 99-190542.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · cap · corrodedJun 27, 2002
During Mck in Atl, corrosion was found in the upper flange of the center wing upper skin cap. The cap is located at sta 681. The corrosion was blended out and at one location was determined to be out of limit. Repaired per EA 99-190519.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · cap · corrodedJun 27, 2002
During an MCK in ATL, corrosion was found in the upper flange of the center wing upper skin cap. The cap is located at sta 681. The corrosion was blended out and at three locations was determined to be ouit of limits. Repaired per EA 99-190532.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedJun 21, 2002
During H-CK at ATL base MTC. a 1/2" crack was found at sta 1132 on the forward side of the 9911839-19 doubler. The crack extended from the upper pulley bracket hole for NAS 1105 on the LH side of the aircraft in the outboard direction. Repaired per EA 99-190511.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery · inoperativeSep 17, 2000
DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE IN THE FORWARD AISLE AND CEILING. MAINTENANCE REPLACED BATTERIES IN THE POWER SUPPLY.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · valve · malfunctionedFeb 16, 2000
DURING APPROACH TO MBS WHEN SLATS WERE EXTENDED, THE AIRCRAFT ROLLED SLIGHTLY TO THE LEFT. SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. SLATS AND FLAPS WERE RETRACTED, FOLLOWED COM PROCEDURES, AND RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · dischargedJul 7, 1999
DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND REPAIRED BAD WIRE TO CONNECTOR, OPERATIONAL CHECK NORMAL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · intercostal · crackedJun 21, 1999
DURING PERIODIC CHECK, FOUND INTERCOSTAL 9911557-3 AT FS 154, LONGERON 14R CRACKED. REPAIRED PER EA 99-164421.
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 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