# N12532: 1968 Mcdonnell Douglas DC-9-32, registration cancelled 2018-01-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 11, 2018 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 45791 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: December 19, 1980 - Certificate issued: February 26, 1998 - Last registry action: April 2, 2012 - Mode S code: A06921 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.8659° N, 112.0391° W: Placed by OpenAirDocs at the center of ZIP code 84116, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N12532 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12532 - Page: https://openairdocs.org/deregistered/N12532-2018-01-11 From the FAA registry file of November 3, 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 Mcdonnell Douglas DC-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.md ## Service difficulty reports (13) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 20000502SH002](https://openairdocs.org/sdr/20000502SH002), Mar 26, 2000: POWER SUPPLY. DIRTY. DURING ACCOMPLISHMENT OF B-CHECK WORK CARD 0617, DISCOVERED WHEN THE EMERGENCY LIGHTS WERE SELECTED TO THE ON POSITION, THE EMERGENCY LIGHTS ABOVE THE AFT OVERW - [SDR 2000ZZZM87](https://openairdocs.org/sdr/2000ZZZM87), Nov 20, 1999: ANGLE. OUT OF ADJUST. AFTER ARRIVING AT SFB AIRPORT AND PRIOR TO THE DISEMBARKATION OF PASSENGERS AN INADVERTENT DEPLOYMENT OF THE L-1 DOOR SLIDE OCCURRED. THE FLT ATTENDANT HAD OPEN - [SDR 2000ZZZX89](https://openairdocs.org/sdr/2000ZZZX89), Oct 13, 1999: BATTERY. DISCHARGED. DURING ACCOMPLISHMENT OF B-CHECK WORK CARD 0617, DISCOVERED WHEN THE EMERGENCY LIGHTS WERE SELECTED TO THE ON POSITION, THE AFT EMERGENCY LIGHTS ABOVE THE TALL - [SDR CALA9800899](https://openairdocs.org/sdr/CALA9800899), May 25, 1998: RELAY. INOPERATIVE. WHEN GEAR WAS EXTENDED ON APPROACH, ONLY UPPER HALF OF GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. THE GEAR WAS RECYCLED AND CIRCUIT BREAKERS WERE CHECKED. A GO-A - [SDR CALA9700228](https://openairdocs.org/sdr/CALA9700228), Feb 11, 1997: SKIN. GOUGED. INSPECTION FOUND SKIN GOUGED AT OUTBOARD NR 3 HINGE OF LT ELEVATOR UPPER SURFACE. THE GOUGE WAS REMOVED AND REPAIRED IAW SRM 55-03, FIGURE 14. - [SDR CALA9700225](https://openairdocs.org/sdr/CALA9700225), Feb 11, 1997: RIB. CRACKED. INSPECTION FOUND A .25 INCH CRACK IN TOP RIB AND A .25 INCH CRACK IN 7TH RIB FROM BOTTOM OF VERTICAL STABILIZER LEADING EDGE. BOTH CRACKS WERE STOP DRILLED AND - [SDR CALA9700226](https://openairdocs.org/sdr/CALA9700226), Feb 6, 1997: FRAME. DENTED. INSPECTION FOUND AFT CARGO PIT BELTFRAME UPPER FLANGE DENTED AT F.S. 917, STRINGER 29L TO 30L. THE DENT WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW S - [SDR CALA9700227](https://openairdocs.org/sdr/CALA9700227), Feb 4, 1997: BRACKET. CORRODED. INSPECTION FOUND CORROSION ON AFT CARGO INTERCOSTAL ATTACH BRACKET AT STA 775, STRINGER 26L. THE ATTACH BRACKET WAS REPLACED WITH A NEW BRACKET IAW SRM 53-21-0 - [SDR CALA9700224](https://openairdocs.org/sdr/CALA9700224), Jan 28, 1997: WEB. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON WEB AT STA 1021. THE CRACK WAS LOCATED AT INTERSECTION WITH UPPER SKIN. THE CRACKED AREA WAS REMOVED. REPAIR ANG - [SDR CALA9700223](https://openairdocs.org/sdr/CALA9700223), Jan 28, 1997: STRIP. CRACKED. INSPECTION FOUND NR 1 ENGINE PYLON STRIP ON LOWER STRUCTURE CRACKED FORWARD OF STA 1039.5. THE CRACK WAS 2 INCHES LONG. A REPAIR WAS FABRICATED AND INSTALLED IA - [SDR CAL960279](https://openairdocs.org/sdr/CAL960279), Feb 27, 1996: SKIN. CRACKED. HOU - INSPECTION FOUND A 4.5 INCH CRACK IN LEFT UPPER RUDDER SKIN. THE CRACKED AREA WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IA - [SDR CAL960278](https://openairdocs.org/sdr/CAL960278), Feb 27, 1996: SKIN. CRACKED. HOU - INSPECTION FOUND A 2 INCH CRACK BETWEEN FOUR RIVETS AT RIVET LINE FOR UPPER CAP AND A .5 INCH CRACK BETWEEN TWO RIVETS AT RIVET LINE FOR UPPER CAP IN RIGH - [SDR CAL950350](https://openairdocs.org/sdr/CAL950350), Apr 5, 1995: VENT VALVE. MALFUNCTIONED. FLT NR 1454 - IAH - ON CLIMB-OUT FUEL VENTING OVERBOARD OUT LEFT WING. AIRCRAFT RETURNED TO IAH. FOUND THAT CLIMB VENT VALVE NEEDED TO BE REPLACED. REMOVED AND ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19991130035779I](https://openairdocs.org/incident/19991130035779I), Nov 30, 1999: Doug DC932 (N12532), St Petersburg-C, FL, Minor damage. (-23) On November 30, 1999, at 10:15 EST, a Douglas DC-9-32, N12532, operated by southeast airlines, inc., experienced airframe vibration climbing through… --- 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.