# N13066: 1979 Mcdonnell-Douglas DC-10-30, 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-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: 46591 - Year built: 1979 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 23, 1987 - Certificate issued: December 30, 1997 - Last registry action: April 21, 2009 - Mode S code: A07E7A - Owner when cancelled: [Provident Bank](https://openairdocs.org/faa-owner/PROVIDENT%20BANK) - Location: [Cincinnati, OH](https://openairdocs.org/faa-place/OH/Cincinnati) - Owner type: Corporation - Owner's area on the map: 39.1053° N, 84.5335° W: Placed by OpenAirDocs at the center of ZIP code 45203, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N13066 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13066 - Page: https://openairdocs.org/deregistered/N13066-2018-01-11 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 Mcdonnell-Douglas DC-10-30: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CALA0100085](https://openairdocs.org/sdr/CALA0100085), Jan 31, 2001: CHARGER. INOPERATIVE. INSPECTION FOUND EMERGENCY SEAT LIGHTS INOPERATIVE AT ROWS 29 - 45 A, B. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-55-00 - [SDR CALA0000913](https://openairdocs.org/sdr/CALA0000913), Jun 17, 2000: SKIN. DELAMINATED. INSPECTION FOUND INTERNAL SURFACE OF NR 2 ENGINE LT TRANSLATING COWL DELAMINATED. THE LT TRANSLATING COWL WAS REMOVED AND REPLACED IAW MM 78-32-17. - [SDR CALA0000910](https://openairdocs.org/sdr/CALA0000910), Jun 15, 2000: BRACKET. CRACKED. INSPECTION FOUND A .5 INCH CRACK IN LT WING O/B FLAP INTERNAL AFT ANGULAR BRACKET. THE BRACKET WAS REPLACED IAW SRM 51-31-01. - [SDR CALA0000907](https://openairdocs.org/sdr/CALA0000907), Jun 15, 2000: STRUCTURE. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT CORNER OF LT MLG DOOR. THE DOOR CORNER WAS REPAIRED IAW SRM 51-31-01. - [SDR CALA9900649](https://openairdocs.org/sdr/CALA9900649), Jun 1, 1999: SKIN. CORRODED. INSPECTION FOUND RT WING OUTBOARD AILERON LOWER SKIN INTERNALLY CORRODED. THE AILERON SKIN WAS REPLACED IAW SRM 51-31-01 AND 51-33-01. - [SDR CALA9900648](https://openairdocs.org/sdr/CALA9900648), Jun 1, 1999: PANEL. CRACKED. INSPECTION FOUND A FOUR INCH CRACK IN RT WING PANEL NR 617CT. REPAIRED IAW SRM 57-10-00, PAGE 25. - [SDR CALA9900647](https://openairdocs.org/sdr/CALA9900647), Jun 1, 1999: SPAR. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN RT WING DROOPED LEADING EDGE ON INTERNAL SPAR AT STA XORS 317. A REPAIR WAS PERFORMED IAW ECRA 5720-01738. - [SDR CALA9900646](https://openairdocs.org/sdr/CALA9900646), Jun 1, 1999: SPAR. CRACKED. INSPECTION FOUND A 0.8 INCH CRACK IN RT WING DROOPED LEADING EDGE ON LATERAL SPAR AT STA XORS 317. A REPAIR WAS PERFORMED IAW ECRA 5720-01738. - [SDR CALA9900645](https://openairdocs.org/sdr/CALA9900645), Jun 1, 1999: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE OUTBOARD LOWER SKIN AT STA XORS 402. A REPAIR WAS PERFORMED IAW SRM 57-10-00, PAGE 216. - [SDR CALA9900644](https://openairdocs.org/sdr/CALA9900644), May 29, 1999: SKIN. DELAMINATED. INSPECTION FOUND LT WING LOWER SKIN PANEL OF LANDING GEAR VANE DELAMINATED ON THE UPPER AND LOWER SURFACE. THE UPPER AND LOWER SKIN WAS REPAIRED IAW SRM 51-71-0 - [SDR CALA9900643](https://openairdocs.org/sdr/CALA9900643), May 28, 1999: BEAM. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING TRAILING EDGE PANEL FITTING BEAM AT STA XORS 299. A REPAIR WAS PERFORMED IAW SRM 57-00-01. - [SDR CALA9900642](https://openairdocs.org/sdr/CALA9900642), May 28, 1999: SKIN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN LT OUTBOARD ELEVATOR TRAILING EDGE. THE TRACK SECTION TRAILING EDGE WAS REPLACED IAW SRM 55-30-00. - [SDR CALA9900641](https://openairdocs.org/sdr/CALA9900641), May 28, 1999: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE INTERNAL SKIN AT OUTBOARD LOWER CORNER. A REPAIR WAS PERFORMED IAW SRM 57-00-01. - [SDR CALA9900640](https://openairdocs.org/sdr/CALA9900640), May 28, 1999: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD FLAP OUTBOARD AFT FITTING ANGLE. THE ANGLE WAS REPLACED IAW SRM 51-30-00. - [SDR CALA9900627](https://openairdocs.org/sdr/CALA9900627), May 28, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 1887 AND 2007 ON LT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01. - [SDR CALA9900626](https://openairdocs.org/sdr/CALA9900626), May 28, 1999: FLOOR. CORRODED. INSPECTION FOUND FORWARD CARGO RT SUPPORT FLOOR PANEL CORRODED AT STA 1099. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-00. - [SDR CALA9900625](https://openairdocs.org/sdr/CALA9900625), May 28, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 427.668 AND 450.162 ON LT SIDE. THE BEAM WAS REPLACED IAW SRM 51-30-00. - [SDR CALA9900624](https://openairdocs.org/sdr/CALA9900624), May 28, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 450.162 IN CENTER AND ON RT SIDE. THE FLOORBEAM SECTIONS WERE REPLACED IAW SRM 51-30-00. - [SDR CALA9900623](https://openairdocs.org/sdr/CALA9900623), May 28, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 450.162 AND 515, LT SIDE. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-30-00. - [SDR CALA9900620](https://openairdocs.org/sdr/CALA9900620), May 28, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 449.250 ON RT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-30-00. - [SDR CALA9900639](https://openairdocs.org/sdr/CALA9900639), May 27, 1999: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACKS CORRODED AT STA 824, LT AND RT SIDES. THE SEAT TRACKS WERE REPLACED IAW MM 53-20-00. - [SDR CALA9900619](https://openairdocs.org/sdr/CALA9900619), May 25, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED BETWEEN STA 1902 AND 2007, RT SIDE. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01. - [SDR CALA9900618](https://openairdocs.org/sdr/CALA9900618), May 25, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CENTRAL FLOORBEAM (NR 2) CORRODED BETWEEN STA 1841 AND 1887. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01. - [SDR CALA9900617](https://openairdocs.org/sdr/CALA9900617), May 24, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED AT RT SIDE BETWEEN STA 1905 AND 2007. THE FLOORBEAM WAS REPLACED IAW SRM 51-31-01. - [SDR CALA9900616](https://openairdocs.org/sdr/CALA9900616), May 24, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND CABIN FLOORBEAM CORRODED ON LT AND RT SIDES AT STA 1821-1887. THE FLOORBEAM SECTIONS WERE REPLACED IAW SRM 51-30-00. - [SDR CALA9900615](https://openairdocs.org/sdr/CALA9900615), May 20, 1999: FLOORBEAM. CORRODED. INSPECTION FOUND FLOORBEAM CORRODED BETWEEN STA 859 AND 879, RT SIDE. THE BEAM WAS REPLACED IAW SRM 51-30-00. - [SDR CALA9800722](https://openairdocs.org/sdr/CALA9800722), Apr 29, 1998: ACTUATOR. FAILED. THE LT MLG WOULD NOT RETRACT AFTER TAKEOFF. CYCLING THE GEAR DID NOT HELP. FUEL WAS DUMPED AND THE GEAR WAS VISUALLY CONFIRMED DOWN BY TOWER. THE AIRCRAFT WAS R - [SDR CALA9800688](https://openairdocs.org/sdr/CALA9800688), Apr 23, 1998: SKIN. CORRODED. INSPECTION FOUND LT WING INBOARD FLAP SKIN TORN AND CORRODED AT OUTBOARD EDGE CLOSURE RIB. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, AND - [SDR CALA9800683](https://openairdocs.org/sdr/CALA9800683), Apr 18, 1998: FITTING. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN R-3 DOOR LOWER FITTING. THE LOWER FITTING WAS REMOVED, A NEW BEAM AND FASTENERS WERE INSTALLED IAW SRM 51-31-01. - [SDR CALA9800682](https://openairdocs.org/sdr/CALA9800682), Apr 18, 1998: STIFFENER. CRACKED. INSPECTION FOUND A 2 INCH CRACK ON LT MLG WHEEL WELL AFT WEB VERTICAL STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW - [SDR CALA9800483](https://openairdocs.org/sdr/CALA9800483), Mar 18, 1998: HYD HOSE. PUNCTURED. THE NR 2 HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE EN ROUTE FROM IAH TO LGW. THE AIRCRAFT LANDED AT LGW WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE FROM 2 - [SDR CALA9601256](https://openairdocs.org/sdr/CALA9601256), Sep 2, 1996: BATT CHARGER. INOPERATIVE. THE CREW REPORTED EMERGENCY LIGHT TEST IN COCKPIT DID NOT GIVE GREEN LIGHT. MAINTENANCE FOUND MID CABIN OVERWING BATTERY CHARGER SUPPLY AT FAULT. THE BATTERY CH - [SDR CAL960226](https://openairdocs.org/sdr/CAL960226), Jan 31, 1996: INTERCOSTAL. CORRODED. KUL - INSPECTION FOUND INTERCOSTAL CORRODED ON LEFT SIDE OF AVIONICS COMPARTMENT AT STATION 470, STRINGER 48L. THE INTERCOSTAL WAS REPLACED IAW SRM 53-11-01, FI - [SDR CAL960225](https://openairdocs.org/sdr/CAL960225), Jan 31, 1996: INTERCOSTAL. CORRODED. KUL - INSPECTION FOUND INTERCOSTAL CORRODED AT LOWER FUSELAGE FORWARD SECTION STATION 464R. THE INTERCOSTAL WAS REPLACED IAW SRM 53-11-01, FIGURE 5. (M) - [SDR CAL960228](https://openairdocs.org/sdr/CAL960228), Jan 30, 1996: SUPPORT. CORRODED. KUL - INSPECTION FOUND A GALLEY 'G' SUPPORT CORRODED. THE SUPPORT WAS REPLACED IAW SRM 53-70-00, FIGURE 13. (M) - [SDR CAL960229](https://openairdocs.org/sdr/CAL960229), Jan 18, 1996: SUPPORT. CORRODED. KUL - INSPECTION FOUND GALLEY 7 INBOARD SUPPORT CORRODED. THE SUPPORT WAS REPAIRED IAW SRM 53-70-00, FIGURE 13. (M) - [SDR CAL960227](https://openairdocs.org/sdr/CAL960227), Jan 17, 1996: SUPPORT. CORRODED. KUL - INSPECTION FOUND LAV 'E' OUTBOARD SUPPORT CORRODED AT STATION 1871. THE SUPPORT WAS REPAIRED IAW SRM 53-70-00, FIGURE 13. (M) ## 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 19920306008939I](https://openairdocs.org/incident/19920306008939I), Mar 6, 1992: Doug DC1030 (N13066), Newark, NJ, Minor damage. Had a left outboard flap vane failure on final. Landed safely. 5 ft section of left flap vane had departed airplane - [Incident 19900717035659I](https://openairdocs.org/incident/19900717035659I), Jul 17, 1990: Doug DC1030 (N13066), Honolulu, HI, 1 fatal. Passenger under control of a doctor lapsed into a terminal condition and expired while en route to Honolulu. ## Other aircraft with N13066 - [Registered now](https://openairdocs.org/aircraft/N13066): DJI AGRAS T50, S/N 1581F6BUB24820019316 - [Cancelled 1968-06-26](https://openairdocs.org/deregistered/N13066-1968-06-26): Waco UIC, S/N 3716. Owner: [Lassiter Charles E](https://openairdocs.org/faa-owner/LASSITER%20CHARLES%20E), [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco) --- 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.