# N12539: Douglas DC-9-32, registration cancelled 2001-03-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 19, 2001 - Status when cancelled: Valid registration - Airframe: [Douglas DC-9-32](https://openairdocs.org/model/douglas-dc-9-32) (registry code 3022066) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 45792 - Type of aircraft: Fixed wing multi engine - Certificate issued: June 28, 2000 - Last registry action: August 10, 2000 - Mode S code: A06928 - Owner when cancelled: [Victory Aeroparts LLC](https://openairdocs.org/faa-owner/VICTORY%20AEROPARTS%20LLC) - Location: [Wellington, KS](https://openairdocs.org/faa-place/KS/Wellington) - Owner type: Corporation - Owner's area on the map: 37.2630° N, 97.4115° W: Placed by OpenAirDocs at the center of ZIP code 67152, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N12539 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12539 - Page: https://openairdocs.org/deregistered/N12539-2001-03-19 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Douglas DC-9-32: https://openairdocs.org/model/douglas-dc-9-32.md ## Service difficulty reports (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA9900014](https://openairdocs.org/sdr/CALA9900014), Jan 12, 1999: SWITCH. INTERMITTENT. EMERGENCY FLOOR PATH LIGHTS INTERMITENT FROM COCKPIT SWITCH. REMOVED AND REPLACED COCKPIT SWITCH PER MM 33-00-00. - [SDR CALA9802188](https://openairdocs.org/sdr/CALA9802188), Dec 18, 1998: BATTERY. DISCHARGED. 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, - [SDR CALA9802187](https://openairdocs.org/sdr/CALA9802187), Dec 18, 1998: POWER SUPPLY. INOP. 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 - [SDR CALA9802186](https://openairdocs.org/sdr/CALA9802186), Dec 18, 1998: BATTERY PACK. DISCHARGED. 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 - [SDR CALA9802177](https://openairdocs.org/sdr/CALA9802177), Dec 15, 1998: FITTING. CRACKED. 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. - [SDR CALA9802161](https://openairdocs.org/sdr/CALA9802161), Dec 8, 1998: SKIN. CORRODED. 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, - [SDR CALA9701487](https://openairdocs.org/sdr/CALA9701487), Oct 20, 1997: SKIN. WORN. 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. - [SDR CALA9701486](https://openairdocs.org/sdr/CALA9701486), Oct 17, 1997: BEAM. CRACKED. INSPECTION FOUND A 2 INCH CRACK AT LIGHTENING HOLE INSIDE DOOR FORWARD LOWER CORNER OF FORWARD CARGO DOOR BEAM WEB. THE DOOR ASSEMBLY WAS REMOVED AND REPLACED I - [SDR CALA9701485](https://openairdocs.org/sdr/CALA9701485), Oct 17, 1997: ANGLE. CRACKED. INSPECTION FOUND CORROSION ON ANGLE AT STA 965 IN AFT BAGGAGE BIN FROM LONGERON 30L TO 25L AND A 20 INCH CRACK WAS FOUND AT LONGERON 28L. A REPAIR WAS INSTALLED - [SDR CALA9701484](https://openairdocs.org/sdr/CALA9701484), Oct 17, 1997: BULKHEAD WEB. CORRODED. INSPECTION FOUND CORROSION ON LOWER BULKHEAD WEB AT STA 996 FROM LONGERON 24L TO 25L. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. - [SDR CALA9701483](https://openairdocs.org/sdr/CALA9701483), Oct 17, 1997: BULKHEAD WEB. CORRODED. 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. - [SDR CALA9701455](https://openairdocs.org/sdr/CALA9701455), Oct 17, 1997: DOOR PAN. CORRODED. FORWARD BAG BIN DOOR JAMB PAN CORRODED AROUND HI-SHEARS. REMOVED AND REPLACED DOOR PAN PER SRM 53-05. - [SDR CALA9701454](https://openairdocs.org/sdr/CALA9701454), Oct 17, 1997: DOUBLER. CORRODED. FORWARD CARGO DOOR JAMB DOUBLER IS CORRODED AT AFT DOOR STOP. REPAIRED DOUBLER PER EC/RA 5330-02587 AND SRM 53-01-2. - [SDR CALA9701439](https://openairdocs.org/sdr/CALA9701439), Oct 16, 1997: SKIN. CORRODED. SKIN CORRODED AT AFT STOP OF FWD BAG BIN DOOR JAMB OUTER SKIN. REMOVED AND REPLACED SKIN PER ECRA 5330-02587 AND SRM 51-30-2. - [SDR CALA9701438](https://openairdocs.org/sdr/CALA9701438), Oct 15, 1997: BULKHEAD TEE. CRACKED. AFT PRESSURE BULKEAD LOWER TEE CAP AT LONG 30 HAS BULGED SKIN UNDER BOLT HEADS STA 996. CUT OUT DAMAGED AREA OF SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PE - [SDR CALA9701428](https://openairdocs.org/sdr/CALA9701428), Oct 12, 1997: SPAR WEB. CRACKED. CRACKS (.75 AND .3125) AT RT SPAR DOUBLER AND WEB VERTICAL FITTING AT TRAP PANEL. REMOVED AND INSTALLED FITTING AFTER CRACK REWORK IN ACCORDANCE WITH EA 5761-01 - [SDR CALA9701429](https://openairdocs.org/sdr/CALA9701429), Oct 10, 1997: SPAR WEB. CRACKED. LEFT SPAR DOUBLER WEB CRACKED (1.25) AT TRAP PANEL VERTICAL FITTING. REPAIRED PER DOUGLAS DRAWING 5935248. - [SDR CALA9701426](https://openairdocs.org/sdr/CALA9701426), Oct 10, 1997: SPAR WEB. CRACKED. LEFT SPAR DOUBLER WEB CRACKED AT TRAP PANEL VERTICAL FITTING. REPAIRED PER DOUGLAS DRAWING 5935248. - [SDR CALA9701425](https://openairdocs.org/sdr/CALA9701425), Oct 10, 1997: PAN. WORN. FWD DOOR HAS ELONGATED HI SHEAR HOLE ON RIGHT SIDE OF DOOR PAN. FABRICATED AND INSTALLED DOUBLER IN ACCORDANCE WITH EC/RA 5200C01015. - [SDR CALA9701424](https://openairdocs.org/sdr/CALA9701424), Oct 9, 1997: PAN. CRACKED. FWD CARGO DOOR LOWER AFT EXTERIOR RADIUS CRACK 3 EXTENDS BEYOND DOUBLER REPAIR BELOW STOP ON PAN. STOP DRILLED AND INSTALLED DOUBLER PER SRM 52-03 FIG 8. - [SDR CALA9701422](https://openairdocs.org/sdr/CALA9701422), Oct 8, 1997: JAMB. CORRODED. INSPECTION FOUND CORROSION ON LOWER DOOR JAMB FRAME OF AFT CARGO DOOR CUTOUT AFT OF HANDLE TORQUE SHAFT. A REPAIR SPLICE SECTION AND SCUFF PLATE WERE INSTALLED - [SDR CALA9701421](https://openairdocs.org/sdr/CALA9701421), Oct 8, 1997: INTERCOSTAL. CRACKED. INSPECTION FOUND A 1 CRACK IN RADIUS AFT OF HANDLE TORQUE SHAFT OF MAIN CABIN DOOR INTERIOR INTERCOSTAL. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30- - [SDR CALA9701418](https://openairdocs.org/sdr/CALA9701418), Oct 7, 1997: LONGERON. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN LONGERON 2R AT STA 699. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 18 - [SDR CALA9701404](https://openairdocs.org/sdr/CALA9701404), Oct 1, 1997: SKIN. CRACKED. INSPECTION FOUND A .75 AND .25 CRACK IN MAIN CABIN DOOR SKIN AT HOLD OPEN HOOK CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 20A. - [SDR CALA9601335](https://openairdocs.org/sdr/CALA9601335), Sep 24, 1996: PAN. CRACKED. INSPECTION FOUND A 3 AND 2.5 INCH CRACK IN RT FORWARD SIDE UPPER CORNER OF DOOR JAMB PAN. A REPAIR WAS INSTALLED IAW DAC DRAWING J060088. - [SDR CALA9601336](https://openairdocs.org/sdr/CALA9601336), Sep 22, 1996: BULKHEAD. CRACKED. INSPECTION FOUND AFT PRESSURE BULKHEAD DOME CRACKED IN UPPER LEFT AND RIGHT CORNERS OF VENTRAL DOOR CUTOUT. DOUBLERS WERE INSTALLED IAW DAC DRAWING J060088, SHE - [SDR CAL951050](https://openairdocs.org/sdr/CAL951050), Nov 18, 1995: CONNECTOR. WIRING PULLED. FLT NR 1401 - IAH - THE LEFT MLG HAD NO TRANSIT LIGHT OR GEAR DOWN LIGHT WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. THE CHECKLIST WAS COMPLIED WITH, A TOWER FLY - [SDR CAL950931](https://openairdocs.org/sdr/CAL950931), Oct 4, 1995: ANGLE. CORRODED. HOU - INSPECTION FOUND CUSP ANGLE CORRODED ON LOWER FRAME AT FS 990, LEFT SIDE. THE CORRODED SECTION OF CUSP ANGLE WAS REMOVED AND A NEW SECTION WAS SPLICED IN - [SDR CAL950906](https://openairdocs.org/sdr/CAL950906), Sep 29, 1995: FRAME. CRACKED. HOU - INSPECTION FOUND A 3 INCH CRACK IN LEFT OVERHEAD FRAME IN FORWARD ACCESSORY COMPARTMENT AT STATION 37. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-05 - [SDR CAL950882](https://openairdocs.org/sdr/CAL950882), Sep 28, 1995: SPAR WEB. CRACKED. HOU - INSPECTION FOUND A 1.25 INCH CRACK IN RT WING SPAR WEB AT STA XCW 58.1. THE CRACK WAS ROUTED OUT IAW EA 5761-01003. (X) - [SDR CAL950909](https://openairdocs.org/sdr/CAL950909), Sep 27, 1995: SKIN. CRACKED. HOU - INSPECTION FOUND A 1 INCH CRACK AT RIVET OF FUSELAGE SKIN STATION 990, LONGERON 14L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 41. (M) - [SDR CAL950908](https://openairdocs.org/sdr/CAL950908), Sep 27, 1995: FRAME. CORRODED. HOU - INSPECTION FOUND CORROSION ON BELT FRAME IN AFT BAGGAGE BIN AT STATION 870. THE CORROSION WAS REMOVED AFTER REMOVING THE FASTENERS. THE AREA WAS ALODINED - [SDR CAL950907](https://openairdocs.org/sdr/CAL950907), Sep 27, 1995: WINDOW FRAME. CRACKED. HOU - INSPECTION FOUND A .25 INCH CRACK IN LEFT WINDOW NR 23 FRAME. THE FRAME WAS REPAIRED IAW SRM 53-01, FIGURE 2. (M) - [SDR CAL950883](https://openairdocs.org/sdr/CAL950883), Sep 27, 1995: BLKHD ANGLE. CRACKED. HOU - INSPECTION FOUND A 1 INCH CRACK IN ANGLE CLIP ON AFT PRESSURE BULKHEAD AT OUTBOARD NR 1L HORIZONTAL BEAM. THE CLIP WAS REMOVED AND A NEW CLIP INSTALLED PE - [SDR CAL950930](https://openairdocs.org/sdr/CAL950930), Sep 26, 1995: BELT FRAME. CORRODED. HOU - INSPECTION FOUND CORROSION ON BELTFRAME FROM LONGERON 25L TO 24R AT STATION 832. THE CORROSION WAS REMOVED. A DOUBLER AND REPAIR ANGLE WERE INSTALLED IAW - [SDR CAL950884](https://openairdocs.org/sdr/CAL950884), Sep 25, 1995: ANGLE. CRACKED. HOU - INSPECTION FOUND A 1 INCH CRACK IN LT WING L/E SPLICE ANGLE BETWEEN NR 3 AND NR 4 SLAT TRACKS. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND IN - [SDR CAL50885](https://openairdocs.org/sdr/CAL50885), Sep 25, 1995: SKIN. CRACKED. HOU - INSPECTION FOUND SKIN AND DOUBLER CRACKED AND BULGED AT STA 579, LONGERONS 29L-29R. THREE CRACKS WERE FOUND AND MEASURED .25 INCH, .50 INCH, AND .75 INCH - [SDR CAL950272](https://openairdocs.org/sdr/CAL950272), Apr 14, 1995: SEAL. WORN. THE NR 2 ENGINE OIL QUANTITY DECREASED TO EIGHT QUARTS DURING CRUISE, BUT THE QUANTITY STABILIZED. THE QUANTITY DECREASED TO FOUR QUARTS DURING APPROACH, BUT ST ## Other aircraft with N12539 - [Cancelled 1975-07-29](https://openairdocs.org/deregistered/N12539-1975-07-29): Cessna 172M, S/N 17262054. Exported to Canada. Owner: [Altemus Richard B](https://openairdocs.org/faa-owner/ALTEMUS%20RICHARD%20B), [Pepper Pike, OH](https://openairdocs.org/faa-place/OH/Pepper%20Pike) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.