# N926RC: 1985 Mcdonnell Douglas DC-9-32, registration cancelled 2007-03-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 21, 2007 - Exported to: Venezuela - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47473 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, normal - Airworthiness date: December 13, 1985 - Certificate issued: October 27, 2006 - Last registry action: October 27, 2006 - Mode S code: ACD5EE - Owner when cancelled: [New Horizons Asset Management Corp](https://openairdocs.org/faa-owner/NEW%20HORIZONS%20ASSET%20MANAGEMENT%20CORP) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.7655° N, 80.1843° W: Placed by OpenAirDocs at the center of ZIP code 33131, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N926RC - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=926RC - Page: https://openairdocs.org/deregistered/N926RC-2007-03-21 From the FAA registry file of October 31, 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 (30) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0003299924](https://openairdocs.org/sdr/0003299924), Sep 12, 2000: ENGINE. FAILED. AFTER TAKEOFF, THE LEFT ENGINE QUIT WITH SLIGHT VIBRATION NOTED. THE FLIGHT CREW PERFORMED THE RED BORDER CHECK LIST, RETURNED TO DTW AND LANDED WITHOUT INCIDEN - [SDR 9904719924](https://openairdocs.org/sdr/9904719924), Oct 27, 1999: SEAT TRACK. BROKEN. DURING M CHECK, FOUND OUTBOARD FLANGE OF THE RIGHT OUTBOARD SEAT TRACK FS 270 BROKEN. REPAIRED PER EA 99-169290. - [SDR 9902429924](https://openairdocs.org/sdr/9902429924), Jul 9, 1999: FIRE LOOP. DIRTY. LEFT ENGINE FIRE DETECTOR LOOP B-LIGHT ILLUMINATED ON SHORT FINAL. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED E - [SDR 9808959924](https://openairdocs.org/sdr/9808959924), May 10, 1998: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT EXTERIOR OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9807149924](https://openairdocs.org/sdr/9807149924), Apr 21, 1998: POWER SUPPLY. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL. - [SDR 9806169924](https://openairdocs.org/sdr/9806169924), Apr 7, 1998: LINE. LEAKING. RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO EN ROUTE. CREW DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT - [SDR 9805329924](https://openairdocs.org/sdr/9805329924), Mar 31, 1998: SPRING. MISINSTALLED. DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ALSO, FOUND THAT TAIL CONE RELEASE HANDLE CABLE WAS NOT INSTALLE - [SDR 9723459924](https://openairdocs.org/sdr/9723459924), Dec 10, 1997: SKIN. CORRODED. DURING LINE CHECK, FOUND CORROSION ON SKIN AT FS 604 BETWEEN LONGERON 29L - 29R. REPAIRED PER EA 99-153395. - [SDR 9721039924](https://openairdocs.org/sdr/9721039924), Nov 8, 1997: LIGHT. BROKEN. DURING LINE CHECK, FOUND EMERGENCY LIGHT BROKEN AT SEAT 20. MAINTENANCE REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK OK. - [SDR 9716699924](https://openairdocs.org/sdr/9716699924), Sep 3, 1997: RIVET. BROKEN. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR DOOR OPEN LIGHT AND ALL UNSAFE LIGHTS WERE ILLUMINATED. GEAR HANDLE WAS PLACED DOWN AND DOOR OPEN LIGHT REMAI - [SDR 9701629924](https://openairdocs.org/sdr/9701629924), Jan 23, 1997: PRESSURE PANEL. CRACKED. DURING H-CHECK, FOUND CRACK IN THE NOSE WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 106. REPAIRED PER EA 99-112006. - [SDR 9701639924](https://openairdocs.org/sdr/9701639924), Jan 20, 1997: FRAME. CORRODED. DURING H-CHECK, FOUND CORROSION ON FRAME AT FS 218 BETWEEN LONGERONS 28L AND 28R. REPAIRED PER EA 99-112021. - [SDR 9701019924](https://openairdocs.org/sdr/9701019924), Jan 18, 1997: BATTERIES. DISCHARGED. DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS AT TAILCONE, OVERWING EXITS, AND LEFT AFT AIRSTAIR AREA INOPERATIVE. CHARGED BATTERIES FOR TEN HOURS, OPERATIONAL - [SDR 9701219924](https://openairdocs.org/sdr/9701219924), Jan 17, 1997: PRESSURE WEB. CRACKED. DURING PERIODIC CHECK, FOUND PRESSURE PANEL IN NOSE WHEEL WELL CRACKED AT FS 106 UNDER OUTBOARD VERTICAL BEAM. INSTALLED REPAIR DOUBLER PER EA 99-112006. - [SDR 9700839924](https://openairdocs.org/sdr/9700839924), Jan 16, 1997: WEB. CRACKED. DURING PERIODIC CHECK, FOUND PRESSURE PANEL IN NOSE WHEEL WELL CRACKED ABOVE FRAME AT FS 83 OUTBOARD EDGE. REPAIRED PER EA 99-112007. - [SDR 9625209924](https://openairdocs.org/sdr/9625209924), Nov 22, 1996: SLIDE. LOW BATTERY. DURING PERIODIC CHECK, FOUND FORWARD GALLEY SERVICE DOOR EVACUATION SLIDE BATTERY PACK INOPERATIVE. REPLACED SLIDE. - [SDR 9623859924](https://openairdocs.org/sdr/9623859924), Nov 6, 1996: FRAME. CRACKED. DURING H-CHECK, FOUND A 2.5 INCH CRACK IN THE FS 658L FRAME LOWER OUTBOARD LEG. REPAIRED FRAME (PSE 53.09.013) PER SRM 51-30, 53-03. - [SDR 9623849924](https://openairdocs.org/sdr/9623849924), Nov 6, 1996: FRAME. CRACKED. DURING H-CHECK, FOUND A 2 INCH CRACK IN THE FS 639R FRAME LOWER OUTBOARD LEG. REPAIRED FRAME (PSE 53.04.014) PER SRM 51-10, 51-30, 53-03. - [SDR 9623809924](https://openairdocs.org/sdr/9623809924), Oct 31, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION IN THE FUEL TANK TO FUSELAGE ATTACH FITTING BETWEEN FS 598 TO 617. REPLACED FITTING PER SRM 51-10, 51-30. - [SDR 9608259924](https://openairdocs.org/sdr/9608259924), Apr 14, 1996: WIRE. BROKEN. DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN GROUND WIRE AND OPERATIONAL CHECK NORMAL. - [SDR 9607819924](https://openairdocs.org/sdr/9607819924), Apr 2, 1996: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9604769924](https://openairdocs.org/sdr/9604769924), Feb 22, 1996: FUEL CONTROL. FAILED. NR 1 ENGINE EPR INDICATION WAS BELOW TARGET ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL CONTRO - [SDR 9520529924](https://openairdocs.org/sdr/9520529924), Dec 16, 1995: STRUT. REQD SERVICE. DURING CLIMB, CREW WAS UNABLE TO RAISE THE LANDING GEAR HANDLE. UTILIZED GROUND SHIFT OVERRIDE TO RAISE THE HANDLE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT - [SDR 9517149924](https://openairdocs.org/sdr/9517149924), Oct 31, 1995: DOOR. NOT CLOSED. DURING CLIMB, THE AIRCRAFT DID NOT PRESSURIZE. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. FOUND AFT CARGO DOOR OPEN, INSPECTED AND CLOSED DOOR. O - [SDR 9508729924](https://openairdocs.org/sdr/9508729924), May 29, 1995: CONTROL PANEL. MALFUNCTIONED. LEFT AC GENERATOR TRIPPED OFF LINE DURING TAKEOFF ROLL AT APPROXIMATELY 80 KNOTS. AFTER CLEARING RUNWAY, GENERATOR WAS RESET AND REMAINED ON LINE. REPLACED THE - [SDR 9507809924](https://openairdocs.org/sdr/9507809924), May 1, 1995: SKIN. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 160 - 200, LONGERON 22L. REPAIRED PER EA 99-097481. MFG PART NUMBER: 5911401-3. - [SDR 9507829924](https://openairdocs.org/sdr/9507829924), Apr 29, 1995: ANGLE. CRACKED. DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE FS 1095. REPAIRED PER EA 99-097075. MFG PART NUMBER: 5912141-59 - [SDR 9507819924](https://openairdocs.org/sdr/9507819924), Apr 28, 1995: SKIN. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON FUSEALGE SKIN FS 160, LONGERON 30. REPAIRED PER EA 99-097479. MFG PART NUMBER: 5911401-5. - [SDR 9507849924](https://openairdocs.org/sdr/9507849924), Apr 20, 1995: FRAME. CRACKED. DURING PERIODIC CHECK, FOUND CRACK IN THE FS 389 FRAME FLANGE AT THE LONGERON 29R END FITTING. REPAIRED PER EA 99-097483. MFG PART NUMBER: 3912347-503. - [SDR 9507189924](https://openairdocs.org/sdr/9507189924), Apr 9, 1995: DOOR FRAME. CRACKED. DURING LINE CHECK, FOUND 2 CRACKS, 2.25 INCHES AND 3.50 INCHES LONG IN THE AFT CABIN DOOR FRAME UPPER RIGHT SIDE FS 817. REPAIRED PER EA 99-091494. ## 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 19870312028889I](https://openairdocs.org/incident/19870312028889I), Mar 12, 1987: Doug DC932 (N926RC), Memphis, TN. Fire warning on left engine on takeoff. Light went out with reduced thrust. Returned. 13 stage duct was split. --- 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.