# N59083: 1975 Mcdonnell-Douglas DC-10-30, registration cancelled 2013-08-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 15, 2013 - Status when cancelled: First renewal notice - Airframe: [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30) (registry code 3023501) - Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 47926 - Year built: 1975 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 29, 1997 - Certificate issued: February 15, 2007 - Last registry action: February 16, 2010 - Mode S code: A7A0F3 - Owner when cancelled: [Omni Air International Inc](https://openairdocs.org/faa-owner/OMNI%20AIR%20INTERNATIONAL%20INC) - Location: [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa) - Owner type: Corporation - Owner's area on the map: 36.1993° N, 95.9089° W: Placed by OpenAirDocs at the center of ZIP code 74115, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N59083 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=59083 - Page: https://openairdocs.org/deregistered/N59083-2013-08-15 From the FAA registry file of November 12, 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-10-30: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30.md ## Service difficulty reports (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CNMA20060023](https://openairdocs.org/sdr/CNMA20060023), Aug 23, 2006: SEAL. CUT. ABOUT 1.5 HRS INTO FLIGHT NR3 ENG OIL PRESSURE WENT TO 10 PSI, NR3 ENG OIL QUANTITY WENT TO ZERO. PERFORMED PRECAUTIONARY ENG SHUTDOWN NR3 ENG. UPON INSPECTION - [SDR CNMA20060015](https://openairdocs.org/sdr/CNMA20060015), Jun 24, 2006: OVEN. ODOR. WHEN FORWARD OVENS 307 & 308 WHERE TURNED ON A STRONG ODOR CAME FROM THEM. WHEN TURNED OFF ODOR DISSIPATED. CLEANED TRAYS BOTH OVENS 307 & 308, OPS CHECK, NO OD - [SDR CNMA20060007](https://openairdocs.org/sdr/CNMA20060007), Apr 24, 2006: PUSH-PULL CABLE. BROKEN. DURING TAKEOFF ROLL NR 3 ENGINE WOULD NOT SPOOL UP. INDICATIONS DID NOT CHANGE NO MATTER THROTTLE POSITION. ENGINE REMAINED IN IDLE THRUST. ABORTED TAKEOFF AT 6 - [SDR CNMA200600002](https://openairdocs.org/sdr/CNMA200600002), Feb 23, 2006: CHARGER. MALFUNCTIONED. DURING CLIMBOUT BATTERY VOLTAGE READ 0 WITH NO CLOCKS. BATTERY CHARGER RELAY RESET 2 TIMES IN-FLIGHT WITH BATTERY VOLTAGE NORMAL AND CLOCKS RETURNED. CHARGER FA - [SDR CNMA2006002](https://openairdocs.org/sdr/CNMA2006002), Feb 23, 2006: CHARGER. INOPERATIVE. DURING CLIMBOUT BATTERY VOLTAGE READ 0 WITH NO CLOCKS. BATTERY CHARGER RELAY RESET 2 TIMES IN-FLIGHT WITH BATTERY VOLTAGE NORMAL AND CLOCKS RETURNED. CHARGER FA - [SDR CNMA200500015](https://openairdocs.org/sdr/CNMA200500015), Aug 31, 2005: CHECK VALVE. LEAKING. FUEL VENTING OUT OF THE LEFT WING VENT BOX AREA. RIGHT SIDE OK. NO TANK OVERFILLED LT ON. APPROX 1600 LBS VENTED. AFTER BLOCK IN FUEL LEAKING OUT OF LEFT FUEL V - [SDR 2005000015](https://openairdocs.org/sdr/2005000015), Aug 31, 2005: VALVE. MALFUNCTIONED. FUEL VENTING OUT OF THE LEFT WING VENT BOX AREA. RIGHT SIDE OK. NO TANK OVERFILLED LIGHT ON. APPROX 1600 LBS VENTED. AFTER BLOCK IN FUEL LEAKING OUT OF LEFT FUE - [SDR CNMA200500014](https://openairdocs.org/sdr/CNMA200500014), Aug 29, 2005: CHECK VALVE. LEAKING. AFTER T/O, GOT THE TANK OVERFILLED LT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OUT - [SDR CNMA2005014](https://openairdocs.org/sdr/CNMA2005014), Aug 29, 2005: CHECK VALVE. MALFUNCTIONED. AFTER T/O, GOT THE TANK OVERFILLED LEFT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED OU - [SDR 2005000014](https://openairdocs.org/sdr/2005000014), Aug 29, 2005: CHECK VALVE. MALFUNCTIONED. AFTER T/O, RECEIVED TANK OVERFILLED LIGHT ON. VISUAL CHECK CONFIRMED FUEL VENTING OUT OF THE LEFT WING VENT. FUEL VENTED FOR APPROX 20 MIN. FUEL LOSS CONFIRMED - [SDR 2004000015](https://openairdocs.org/sdr/2004000015), Nov 24, 2004: COWLING. DEPARTED. AT CLIMB-OUT, NR 3 ENG LOST ENGINE COWLING DUMPED FUEL RETURNED TO EDDF. - [SDR 2004000007](https://openairdocs.org/sdr/2004000007), Jun 13, 2004: ENGINE. FAILED. ON T/O ROLL, NR 1 ENGINE MADE LOUD BANG, ENGINE FAIL LIGHT ILLUMINATED AND EGT PEGGED. N1 WAS 130 PERCENT AND SPEED WAS 125 KIAS. T/O ABORTED. TOWER NOTED FIRE - [SDR 2004000001](https://openairdocs.org/sdr/2004000001), Mar 9, 2004: SEAL. LEAKING. NR 2 ENGINE OIL QUANITY STEADILY DECREASED DURING CRUISE. LOST 2.5 QTS IN 50 MINUTES. SHUTDOWN ENGINE TO PRESERVE OIL QTY. RESTARTED ENGINE AT ALT. FL 240, QTY - [SDR CNMA200300011](https://openairdocs.org/sdr/CNMA200300011), Dec 17, 2003: RUDDER. STUCK. ON SHORT FINAL AND FLARE RUDDER PEDALS COULD NOT BE MOVED. RUDDER PEDALS COULD NOT BE MOVED ON TAXI IN. TILLER OPERATION NORMAL. CAPTAINS AND CO-PILOTS SAME. LI - [SDR CNMA200300008](https://openairdocs.org/sdr/CNMA200300008), Dec 10, 2003: ENGINE. OVERTEMP. ON INITIAL CLIMBOUT NR 1 ENGINE OIL TEMP CLIMBED TO AND EXCEEDED LIMITS. (PEGGED OUT) SHUT DOWN ENGINE. - [SDR CNMA200300001](https://openairdocs.org/sdr/CNMA200300001), Jan 17, 2003: SLIDE. DISLODGED. WHILE AT GATE FLIGHT ATTENDANT OPENED R-1 DOOR WITHOUT DISARMING DOOR. SLIDE CAME OUT OF ITS CONTAINER AND LANDED ON TOP OF CATERING TRUCK AWAITING TO DELIVER. - [SDR CNMA200200007](https://openairdocs.org/sdr/CNMA200200007), Dec 20, 2002: ELECTRICAL BOX. Overspeed warning sounded at 270 knots - slats confirmed retracted. Removed and replaced Proximity Electronic Unit. Bite test normal. - [SDR CALA0100762](https://openairdocs.org/sdr/CALA0100762), Aug 15, 2001: SPAR. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN NR 3 PYLON LOWER SPAR WEB AT FAN DUCT CUTOUT. A REPAIR ANGLE AND STIFFENER WERE INSTALLED IAW SRM 54-20-00, FIGURE 19A. - [SDR 20000810SH021](https://openairdocs.org/sdr/20000810SH021), Aug 10, 2000: HARNESS. CHAFED. D-CHECK, FQI SYSTEM WIRING CHAFING AND ARCING INSIDE FUEL TANK NR 3, PROBE NR 6, HARNESS FOUND CHAFING ON MOUNT BRACKET OF THE FILL ALOT VALVE IN BAY R07 (XORS- - [SDR 20000829SH007](https://openairdocs.org/sdr/20000829SH007), Jul 28, 2000: HARNESS. CHAFED. D-CHECK, FQI SYSTEM WIRING CHAFING AND ARCING INSIDE FUEL TANK NR 3, PROBE NR 6. HARNESS FOUND CHAFING ON MOUNT BRACKET OF THE FILL PILOT VALVE IN BAY R07 (XORS - [SDR CALA0001384](https://openairdocs.org/sdr/CALA0001384), Jul 26, 2000: HARNESS. FRAYED. INSPECTION FOUND RT WING FUEL TANK WIRING OUTER AND INNER INSULATION CHAFING AND ARCING DAMAGE ON FLOAT SWITCH BRACKET ZONE R07-11, LOCATION T2-104, PROBE XORS - [SDR CALA9901355](https://openairdocs.org/sdr/CALA9901355), Oct 10, 1999: FLOORBEAM. CORRODED. FLOORBEAM J SECTION AT STN 1887 AT 27R - 33R CORRODED. REMOVED CORRODED AREA. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01. - [SDR CALA9901354](https://openairdocs.org/sdr/CALA9901354), Oct 10, 1999: FLOORBEAM. CORRODED. FLOORBEAM J SECTION AT STA 1887 AT 60L - 90L CORRODED. REMOVED CORRODED AREA. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01. - [SDR CALA9901353](https://openairdocs.org/sdr/CALA9901353), Oct 10, 1999: FLOORBEAM. CORRODED. FLOORBEAM J SECTION CORRODED AT ST 1887 AT 60R - 90R. REMOVED CORROSION. FABRICATED AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01. - [SDR CALA9901352](https://openairdocs.org/sdr/CALA9901352), Oct 10, 1999: FLOORBEAM. CORRODED. FLOOR BEAM J SECTION CORRODED AT ST 1887 AT 39L TO 58 L. REMOVED CORROSION AND INSTALLED NEW SECTION PER SRM 51-21-00 AND GMM 10-900-01. - [SDR CALA9900878](https://openairdocs.org/sdr/CALA9900878), Jul 28, 1999: DECODER. SHORTED. SMOKE APPEARED IN THE AIRCRAFT CABIN NEAR THE VICINITY OF SEATS 37 AND 38KL WHILE ON FINAL APPROACH TO DUS. THE FLIGHT ATTENDANT'S PULLED OVERHEAD PANEL IN THE - [SDR CALA9801129](https://openairdocs.org/sdr/CALA9801129), Jun 18, 1998: BATTERY CHARGER. INOPERATIVE. INSPECTION FOUND THE EMERGENCY AISLE LIGHTING INOPERATIVE AT ROWS 9 AND 10 (LEFT AND RIGHT). THE BATTERY CHARGER AT DOOR 2R AND 2L GALLEY OVERHEAD PANEL WAS REP - [SDR CALA9800537](https://openairdocs.org/sdr/CALA9800537), Mar 23, 1998: SLIDE. INOPERATIVE. INSPECTION FOUND THE R-3 DOOR SLIDE BOTTLE PRESSURE LIGHT ILLUMINATED. THE R-3 DOOR SLIDE WAS REMOVED AND REPLACED AND THE LIGHT TESTED NORMAL. - [SDR CALA9800206](https://openairdocs.org/sdr/CALA9800206), Feb 10, 1998: FIRE DETECTOR. CHAFED. THE NR 2 ENGINE A FIRE LOOP DETECTOR LIGHT BEGAN TO FLICKER WHILE IN CRUISE FLIGHT FROM LGW TO EWR. WHEN THE NR 2 ENGINE THRUST WAS REDUCED THE FLICKERING STOPP ## Other aircraft with N59083 - [Cancelled 1973-12-19](https://openairdocs.org/deregistered/N59083-1973-12-19): Cessna 210L, S/N 210960078. Exported to Brazil --- 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, except the copies of manufacturers’ service documents, which belong to their rights holders.