# N12536: 1967 Mcdonnell Douglas DC-9-32, registration cancelled 2006-12-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 21, 2006 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47113 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, transport - Airworthiness date: June 18, 1981 - Certificate issued: March 1, 2004 - Last registry action: March 1, 2004 - Mode S code: A06925 - Owner when cancelled: [Alameda Corporation Trustee](https://openairdocs.org/faa-owner/ALAMEDA%20CORPORATION%20TRUSTEE) - Location: [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio) - Owner type: Corporation - Owner's area on the map: 29.5387° N, 98.4913° W: Placed by OpenAirDocs at the center of ZIP code 78216, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N12536 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12536 - Page: https://openairdocs.org/deregistered/N12536-2006-12-21 From the FAA registry file of November 5, 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 (238, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR GTIA030164](https://openairdocs.org/sdr/GTIA030164), Mar 18, 2003: BEAM. CRACKED. EDDY CURRENT INSPECTION REVEALED 2.25 INCH CRACKS EMANATING FROM FASTENER HOLE IN OUTER PAN OF AFT LOWER CARGO DOOR FWD EDGE AT BEAM 1. STOP DRILLED CRACKS AND - [SDR GTIA030114](https://openairdocs.org/sdr/GTIA030114), Feb 28, 2003: FITTING. LEAKING. RIGHT WHEEL WELL AFT FUEL MANIFOLD INBOARD SIDE DRIPPING FUEL. RESECURED LOOSE FITTING AT APU FUEL LINE SHROUD CONNECTION. LEAK CHECK GOOD. - [SDR GTIA021045](https://openairdocs.org/sdr/GTIA021045), Oct 6, 2002: ISOLATOR. CORRODED. DTW - NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR IS CORRODED AND PLATING IS FLAKING OFF ON INNER CONICAL AREA. REMOVED AND REPLACED NR 2 ENGINE FORWARD LOWER - [SDR GTIA020965](https://openairdocs.org/sdr/GTIA020965), Sep 10, 2002: ODOR. DETECTED. ACY - FLT 276 - FLIGHT ATTENDANTS DETECTED A FAINT ODOR DURING THE INITIAL CLIMB BUT IT DISSIPATED BY LEVEL OFF. COULD NOT DETECT ANY ODOR WITH PACKS ON AND A/C - [SDR GTIA020843](https://openairdocs.org/sdr/GTIA020843), Jul 27, 2002: LIGHT. INOPERATIVE. FLT 276 - TPA - FOUND RIGHT LANDING GEAR BUTTON INDICATOR LIGHT INOPERATIVE, GREEN LENS. REMOVED AND REPLACED GEAR DOWNLOCK SWITCH ON RIGHT MAIN GEAR AND OPS CH - [SDR GTIA020831](https://openairdocs.org/sdr/GTIA020831), Jul 17, 2002: STRUCTURE. DAMAGED. DTW - FOUND RIGHT FLAP TRAILING EDGE SPLICE APPROX 1.5 INCHES INBOARD END OF FLAP AT FIRST EXPANSION JOINT. SANDED AND INSTALLED FIBERGLASS LAYUP REPAIR ON RIGH - [SDR GTIA020580](https://openairdocs.org/sdr/GTIA020580), Jun 3, 2002: SERVO. FAULTY. TPA - FLT 276 - AUTO PILOT AILERON SERVO IS ERRATIC IN ALL REQUIRES OF FLIGHT 276. REMOVED AND REPLACED SERVO AUTO DRIVE. OPS CHECK OK. BITE CHECK FOR SERVO POR - [SDR GTIA020431](https://openairdocs.org/sdr/GTIA020431), May 7, 2002: MOTOR. MALFUNCTIONED. ACY - PRIMARY TRIM HESITATES NOSE UP DIRECTION OCCURS USING BOTH CAPTAINS OR F/O'S YOKE SWITCHES AND USING SUIT CASE HANDLES. REMOVED AND REPLACED PRIMARY TRIM - [SDR GTIA020295](https://openairdocs.org/sdr/GTIA020295), Apr 21, 2002: CONTROL VALVE. MALFUNCTIONED. DTW - FLT 9536 - LEFT GEAR UNSAFE LIGHT ILLUMINATED WITH GEAR UP. RECYCLED GEAR. UPLATCH CHECK GEAR DOOR OPEN LIGHT ILLUMINATED. REPLACED LANDING GEAR CONTROL V - [SDR GTIA020296](https://openairdocs.org/sdr/GTIA020296), Apr 21, 2002: UPLOCK SWITCH. FAULTY. FLT 8019 - DTW - PUT GEAR UP, LEFT GEAR UNSAFE LIGHT CAM ON, UP LATCH CHECK RED LIGHT STAYED ON AND GEAR DOOR LIGHT (AMBER) CAME ON COMPLETED QRH PROCEDURE. REP - [SDR GTIA020294](https://openairdocs.org/sdr/GTIA020294), Apr 20, 2002: LATCH. OUT OF ADJUST. DTW - FLT 9536 - FOUND LEFT LANDING GEAR UNSAFE LIGHT AND DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. GEAR RECYCLED IAW QRH SAME INDICATIONS. FOUND LEFT - [SDR GTIA020273](https://openairdocs.org/sdr/GTIA020273), Mar 30, 2002: ADC. FAULTY. FLT 616 - ACY - AUTO PILOT PITCH CONTROL PORPOISES DURING CLIMB AND DESCENTS AND WILL NOT HOLD ALTITUDE ALL OTHER FUNCTIONS OK FLT 616. REMOVED AND REPLACED AIR - [SDR GTIA020242](https://openairdocs.org/sdr/GTIA020242), Mar 22, 2002: CONTROLLER. FAULTY. ACY - FLT 8012 - A/P WILL NOT STAY ENGAGED. REMOVED AND REPLACED AUTOMATIC PILOT CONTROLLER. OPERATIONAL CHECK NORMAL IAW DC9 MM 22-10-2. (M) - [SDR GTIA020220](https://openairdocs.org/sdr/GTIA020220), Mar 8, 2002: COMPUTER. MALFUNCTIONED. FLT 8011 - ACY - ON STABILIZED DESCENT AUTOPILOT SUDDENLY PITCHED DOWN THEN PITCHED UP. REMOVED AND REPLACED PITCH AXIS COMPUTER IAW MM 27-13-1, OPS CHECK NORMA - [SDR GTIA012218](https://openairdocs.org/sdr/GTIA012218), Jan 17, 2002: WEB. CRACKED. FTW - NR 1 ENGINE PYLON LOWER SURFACE AFT HINGE PANEL OUTBOARD LOWER WEB CRACKED AT ANGLE. REMOVED WEB. FABRICATED NEW WEB. INSTALLED WEB. REMOVED DAMAGED SECTI - [SDR GTIA020012](https://openairdocs.org/sdr/GTIA020012), Jan 13, 2002: BATTERY PACK. DISCHARGED. DTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM. OPS CHECK GOOD PER MM 33-53-01. (M) - [SDR GTIA020009](https://openairdocs.org/sdr/GTIA020009), Jan 13, 2002: BATTERY PACK. DISCHARGED. DTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM, OPS CHECK GOOD PER DC9 MM 33-53-01. (M) - [SDR GTIA012321](https://openairdocs.org/sdr/GTIA012321), Jan 3, 2002: OXYGEN MASK. MALFUNCTIONED. FTW - FOUND OXYGEN MASK DID NOT DROP IN AUTO. PERFORMED TROUBLE SHOOTING AND FOUND OXYGEN LEAK ON OXYGEN LINES. INSTALLED PROPERLY OXYGEN LINES. OPS CHECK GOOD - [SDR GTIA012319](https://openairdocs.org/sdr/GTIA012319), Dec 20, 2001: RIB. CRACKED. FTW - FOUND RIGHT WING NR 4 SLAT 8TH INNER RIB FROM OUTBOARD END OF SLAT IS CRACKED. REMOVED RIB. FABRICATED NEW RIB. INSTALLED NEW RIB IAW DC9 SRM 51-30-2. (M) - [SDR GTIA012313](https://openairdocs.org/sdr/GTIA012313), Dec 20, 2001: PANEL. WARPED. FTW - FOUND RIGHT WING INBOARD FLIGHT SPOILER WARP. REMOVED RIGHT INBOARD SPOILER PANEL. INSTALLED RIGHT INBOARD SPOILER PANEL IAW MM DC9 27-61-1. (M) - [SDR GTIA012095](https://openairdocs.org/sdr/GTIA012095), Dec 15, 2001: DOUBLER. CRACKED. FTW - NR 2 ENGINE NOSE COWL 2ND INTERNAL RIB (FROM AFT) 6 O'CLOCK POSITION REPAIR DOUBLER CRACKED. REMOVED DOUBLER REPAIR CRACKED. FORMED NEW SPLICE DOUBLER, IN - [SDR GTIA012156](https://openairdocs.org/sdr/GTIA012156), Dec 15, 2001: WEB. CRACKED. FTW - RIGHT NOSE COWL INBOARD AREA AT 6 O'CLOCK POSITION DOUBLER CRACKED. REMOVED CRACKED DOUBLER. AFTER FURTHER EVALUATION FOUND WEB ALSO CRACKED. CUT DAMAGED - [SDR GTIA012191](https://openairdocs.org/sdr/GTIA012191), Dec 7, 2001: SPLICE. CORRODED. FTW - FOUND LEFT WING LEADING EDGE UPPER FRONT SPAR PREVIOUS REPAIR HAS CORROSION FROM XFS 550-XFS 77. REMOVED CORROSION. SPLICE PLATE FOUND TO BE OUT OF LIMITS - [SDR GTIA012122](https://openairdocs.org/sdr/GTIA012122), Dec 6, 2001: CHANNEL. CRACKED. FTW - FOUND FORWARD ENTRY FLOOR PANEL HAT CHANNEL HAS CRACKED. REMOVED CRACKED CHANNEL. FABRICATED CHANNEL. INSTALLED CHANNEL IAW DC9 SRM 51-30-2. (M) - [SDR GTIA012187](https://openairdocs.org/sdr/GTIA012187), Dec 4, 2001: FLOORBOARD. DAMAGED. FTW - CO-PILOT FLOORBOARD DAMAGED AT UPPER FACE. PUNCTURE AT STATION Y=150. REMOVED DAMAGED AREA. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER PER DC9 SRM 51-30 - [SDR GTIA012174](https://openairdocs.org/sdr/GTIA012174), Dec 4, 2001: FLOORBOARD. DAMAGED. FTW - FOUND FLOORBOARD WEB HAS HOLE Y211-X27. REMOVED DAMAGE. FABRICATED REPAIR PARTS FILLER AND DOUBLER. INSTALLED PER DC9 SRM 53-01. (M) - [SDR GTIA012182](https://openairdocs.org/sdr/GTIA012182), Dec 3, 2001: ANGLE. CHAFED. NR 4 SLAT RIGHT CHORD ANGLE CHAFFED MORE THAN 50 PERCENT THICKNESS OF MATERIAL. REMOVED CHAFFED ANGLE. FABRICATED NEW CHORD ANGLE. INSTALLED NEW CHORD ANGLE IAW - [SDR GTIA012176](https://openairdocs.org/sdr/GTIA012176), Dec 2, 2001: ANGLE. CHAFED. FTW - FOUND NR 3 RIGHT SLAT OUTBOARD LOWER CHORD ANGLE CHAFFED MORE THAN 50 PERCENT OF MATERIAL THICKNESS. FORMED NEW CHORD ANGLE. INSTALLED FASTENERS IAW DC9 S - [SDR GTIA012175](https://openairdocs.org/sdr/GTIA012175), Dec 1, 2001: RETAINER. CRACKED. FORWARD CARGO DOOR HAS TWO CRACKS AT RETAINER MOUNT HOLE 2 INCHES BELOW UPPER AFT CORNER. FABRICATED REPAIR DOUBLERS. INSTALLED DOUBLERS IAW DC9 SRM 52-01. (M) - [SDR GTIA012308](https://openairdocs.org/sdr/GTIA012308), Nov 29, 2001: FLOOR SUPPORT. CORRODED. FTW - FOUND FLOOR SUPPORT CORRODED AT STATION Y=200 FROM -24 INCH TO -X43, FOUND AFTER G-1 REMOVED DUE A CORROSION BEYOND LIMITS AT FLOOR SUPPORT. DRILLED AND L - [SDR GTIA012127](https://openairdocs.org/sdr/GTIA012127), Nov 29, 2001: FLOOR SUPPORT. CORRODED. FTW - FOUND FLOOR SUPPORT CORRODED AT STA Y = 160 FROM -X=1 TO -X=21. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED NEW FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT I - [SDR GTIA012148](https://openairdocs.org/sdr/GTIA012148), Nov 29, 2001: FLOOR SUPPORT. CORRODED. FTW - FOUND FLOOR SUPPORT CORRODED AT STA Y=200 FROM -X47 INCHES TO -X=56 INCHES. REMOVED SUPPORT ANGLE. FORMED NEW FLOOR SUPPORT ANGLE IAW DC9 SRM 53-11-1. INS - [SDR GTIA012236](https://openairdocs.org/sdr/GTIA012236), Nov 27, 2001: SUPPORT BRACKET. CRACKED. FTW - FOUND SUPPORT BRACKET CRACKED AT LEFT TRAPEZOIDAL PANEL STRUCTURE STA Y 729 X=59.500 Z=13.100. REMOVED BRACKET. INSTALLED NEW FILLER IAW DC9 SRM 51-30-1. - [SDR GTIA012109](https://openairdocs.org/sdr/GTIA012109), Nov 27, 2001: SKIN. CRACKED. FTW - FOUND ANGLE SUPPORT HAS ELONGATED HOLES, AT LEFT TRAPEZOIDAL PANEL AFT UPPER AREA STA Y 730. UPON FURTHER INVESTIGATION, FOUND CRACK IN SKIN AREA FOUND TO - [SDR GTIA012126](https://openairdocs.org/sdr/GTIA012126), Nov 27, 2001: FLOOR SUPPORT. CRACKED. FTW - FOUND FLOOR SUPPORT CRACKED AT STATION Y=238 INCHES. REMOVED DAMAGED FLOOR SUPPORT. FABRICATED LOCATED AND DRILLED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT - [SDR GTIA012171](https://openairdocs.org/sdr/GTIA012171), Nov 26, 2001: DOUBLER. CRACKED. FTW - AFT LOWER CARGO, CARGO DOOR OUTBOARD LOWER CORNER DOUBLER PREVIOUS REPAIR CRACKED/WORN-OUT. REMOVED DAMAGE AREA. FORMED REPAIR. INSTALLED REPAIR IAW DC9 S - [SDR GTIA012110](https://openairdocs.org/sdr/GTIA012110), Nov 26, 2001: SKIN. CRACKED. FTW - FOUND RUDDER RIGHT UPPER SKIN, .50 INCH DIAMETER DENT IN SKIN BETWEEN RIBS 17 AND 18. UPON FURTHER INVESTIGATION CRACK FOUND IN SKIN AREA FOUND TO BE OUT - [SDR GTIA012196](https://openairdocs.org/sdr/GTIA012196), Nov 25, 2001: FLOOR SUPPORT. CORRODED. FTW - FOUND ENTRY AREA, FLOOR SUPPORT CORRODED FROM STATION Y=160 TO STA Y=200. REMOVED FLOOR SUPPORT STA 160-200. LOCATED AND DRILLED NEW FLOOR SUPPORT. INSTAL - [SDR GTIA012223](https://openairdocs.org/sdr/GTIA012223), Nov 25, 2001: FLOOR SUPPORT. CORRODED. FTW - FORWARD ENTRY FLOOR SUPPORT CORRODED FROM STA Y=162 TO Y=198. FABRICATED FLOOR SUPPORT. INSTALLED REPLACEMENT FLOOR SUPPORT IAW DC9 SRM 51-10-4 AND 51-30- - [SDR GTIA012222](https://openairdocs.org/sdr/GTIA012222), Nov 25, 2001: FLOOR SUPPORT. CORRODED. FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STA Y=200 FROM X-24 INCH TO X-43 INCH. FABRICATED NEW FLOOR SUPPORT. INSTALLED FLOOR SUPPORT PER DC9 SRM 51- - [SDR GTIA012258](https://openairdocs.org/sdr/GTIA012258), Nov 24, 2001: LONGERON. CORRODED. FTW - FOUND E/E BAY LONGERON 28 LEFT HAS CORROSION AT STATION 170-180. CUT OUT DAMAGE AND REMOVED. INSTALLED LONGERON AND SPLICE PER DC9 SRM 51-30-2. (M) - [SDR GTIA012197](https://openairdocs.org/sdr/GTIA012197), Nov 23, 2001: FLOOR SUPPORT. CORRODED. FTW - FORWARD ENTRY AREA, FLOOR SUPPORT CORRODED AT STATION Y200 FROM X2 INCHES TO -X21. REMOVED FLOOR SUPPORT. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPOR - [SDR GTIA012264](https://openairdocs.org/sdr/GTIA012264), Nov 23, 2001: ANGLE. CRACKED. FTW - FOUND FORWARD CARGO DOOR JAMB WEB STRAP AND ANGLES HAVE TOOLING MARKS, CORROSION AND CRACKS STATION 427-436. ONE ANGLE WAS CRACKED FORMED A NEW ANGLE. FOR - [SDR GTIA012221](https://openairdocs.org/sdr/GTIA012221), Nov 23, 2001: SUPPORT. CORRODED. FTW - ANGLE SUPPORT CORRODED AT STATION Y916. FABRICATE NEW ANGLE SUPPORT. INSTALLED NEW ANGLE SUPPORT IAW DC9 SRM 51-30-1. (M) - [SDR GTIA012133](https://openairdocs.org/sdr/GTIA012133), Nov 23, 2001: FLOOR SUPPORT. CORRODED. FTW - FOUND FORWARD ENTRY AREA FLOOR SUPPORT CORRODED AT STATION Y200 FROM X= 1 INCH TO X= 20 INCHES. FABRICATED FLOOR SUPPORT. INSTALLED FLOOR SUPPORT. (M) - [SDR GTIA012146](https://openairdocs.org/sdr/GTIA012146), Nov 23, 2001: STRAP. CORRODED. FTW - FOUND FORWARD CARGO DOOR JAMB AFT STATION 427-438 WEB STRAPS HAVE TOOLING MARKS AND SURFACE CORROSION. FORMED STRAP. LOCATED AND DRILLED STRAP IAW DC9 SRM - [SDR GTIA012192](https://openairdocs.org/sdr/GTIA012192), Nov 22, 2001: WEB. CORRODED. FTW - FOUND CUSP WEB CORRODED AT STATION Y=200 X=56. CORROSION WAS FOUND DURING OPEN UP FOR WEB REPAIR AT FRAME STATION -200, X=57. REMOVED CORROSION. REMOVED S - [SDR GTIA012124](https://openairdocs.org/sdr/GTIA012124), Nov 21, 2001: WEB. DAMAGED. FTW - FOUND LOWER INNER WEB FORWARD BAG DOOR FS 370 TO FS 427 HAS OVERSIZED HOLES, EXTRA HOLES, CORRODED HOLES, A BAD PREVIOUS REPAIR AND NUMEROUS DENTS FROM OV - [SDR GTIA012263](https://openairdocs.org/sdr/GTIA012263), Nov 19, 2001: STRUCTURE. CRACKED. FTW - FORWARD CARGO COMPARTMENT HAS A CRACK BETWEEN STATION 465-484 BETWEEN LONGERON 30 AND 29L. FORMED INTERCOSTAL IAW DOUGLAS PRING SR09530005. FORMED AND INS - [SDR GTIA012112](https://openairdocs.org/sdr/GTIA012112), Nov 19, 2001: WEB. CORRODED. FTW - FOUND CABIN LEFT SIDE CORRODED AT MEMBRANE WEB STATION 908. REMOVED MEMBRANE WEB FROM STATION 897 TO 964. FORMING MEMBRANE/WEB. INSTALLED NEW MEMBRANE/WEB All 238: https://openairdocs.org/deregistered/N12536-2006-12-21/reports.md ## FAA accident and incident reports (2) 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 20020326004329I](https://openairdocs.org/incident/20020326004329I), Mar 26, 2002: Doug DC932 (N12536), Erie, PA. (-23) The aircraft touched down 2300 feet from the threshold (end) of runway 24 (RW24 is 6500 feet long - thus leaving 4300 feet for stopping). Upon contact… - [Incident 19950625021829I](https://openairdocs.org/incident/19950625021829I), Jun 25, 1995: Doug DC932 (N12536), Ft Lauderdale, FL, Minor damage. Position and hold. Smoke from right main gear. No fire,cleared runway. Deplaned passengers. Inner wheel bearing siezed ## Other aircraft with N12536 - [Registered now](https://openairdocs.org/aircraft/N12536): Robinson Helicopter R22 BETA, S/N 0786 - [Cancelled 1974-01-30](https://openairdocs.org/deregistered/N12536-1974-01-30): Cessna 172M, S/N 17262051. Exported to Australia. Owner: [L T A Export Inc](https://openairdocs.org/faa-owner/L%20T%20A%20EXPORT%20INC), [Ft Lauderdale, FL](https://openairdocs.org/faa-place/FL/Ft%20Lauderdale) --- 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.