N12539Douglas DC-9-32
This N-number isn't registered right now. Below is its last known registration, canceled Mar 19, 2001.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched38 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Victory Aeroparts LLC
- Owner type
- Corporation
- City, state
- Wellington, KS
- Certificate issued
- Jun 28, 2000
- Canceled
- Mar 19, 2001
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
- Serial number
- 45792
- 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
- A06928
Engine
- Type
- Turbo-jet
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2000 – 2001Victory Aeroparts LLCWellington, KS
- 1973 – 1975Individual ownerPepper Pike, OH · different airframe: Cessna 172m S/N 17262054
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (38)
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 · switch · intermittentJan 12, 1999
EMERGENCY FLOOR PATH LIGHTS INTERMITENT FROM COCKPIT SWITCH. REMOVED AND REPLACED COCKPIT SWITCH PER MM 33-00-00.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · dischargedDec 18, 1998
THE FORWARD AND AFT EMERGENCY AISLE PATH LIGHTING BATTERY PACKS FAILED TIME LIMIT CHECK. THE BATTERY PACKS WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-0, PAGE 1.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · power supply · inopDec 18, 1998
INSPECTION FOUND CABIN OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE AT SEATS 16AC AND 16DEF. THE POWER SUPPLY WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00, PAGE 501.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Lights · battery · dischargedDec 18, 1998
INSPECTION FOUND TAILCONE EMERGENCY LIGHT AT RIGHT AFT LAV CEILING INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-00, PAGE 501.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · fitting · crackedDec 15, 1998
INSPECTION FOUND A .5 INCH CRACK IN C-1 DOOR AFT LOWER STOP INTERCOSTAL TEE FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-8 AND 51-10-4.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedDec 8, 1998
INSPECTION FOUND FUSELAGE SKIN BULGED AT STA 218 BETWEEN LONGERONS 17R AND 18R. THE BULGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-04, PAGE 208, 51-10-3, AND 51-30-2.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · skin · wornOct 20, 1997
INSPECTION FOUND FORWARD BAG BIN DOUBLER ON DOOR SKIN WORN AND WITH A SHARP EDGE. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-01 AND ECRA 5231-01001. THE SKIN AROUND DOOR HANDLE WAS FOUND BENT AND GOUGED. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5231-01001, FIGURE 2.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · doubler · corrodedOct 17, 1997
FORWARD CARGO DOOR JAMB DOUBLER IS CORRODED AT AFT DOOR STOP. REPAIRED DOUBLER PER EC/RA 5330-02587 AND SRM 53-01-2.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · door pan · corrodedOct 17, 1997
FORWARD BAG BIN DOOR JAMB PAN CORRODED AROUND HI-SHEARS. REMOVED AND REPLACED DOOR PAN PER SRM 53-05.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bulkhead web · corrodedOct 17, 1997
INSPECTION FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT STA 996, LONGERON 24L AND 25L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 24.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 38 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026