# N12061: 1980 Mcdonnell-Douglas DC-10-30, registration cancelled 2017-06-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 7, 2017 - 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: 47851 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 25, 1980 - Certificate issued: July 15, 2002 - Last registry action: November 4, 2005 - Mode S code: A056F6 - Owner when cancelled: [Prop Three Ltd](https://openairdocs.org/faa-owner/PROP%20THREE%20LTD) - Location: [Stateline, NV](https://openairdocs.org/faa-place/NV/Stateline) - Owner type: Corporation - Owner's area on the map: 38.9552° N, 119.9115° W: Placed by OpenAirDocs at the center of ZIP code 89449, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N12061 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=12061 - Page: https://openairdocs.org/deregistered/N12061-2017-06-07 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HALA0100248](https://openairdocs.org/sdr/HALA0100248), Oct 10, 2001: RCCB. FAILED. LAX - FLT 32 - AIR DIVERSION AT 3 HOURS INTO FLIGHT, LT EMERGENCY AC BUS OFF LIGHT ILLUMINATED, RESTORED SYSTEM. FOLLOWED CHECKLIST, 5 MINUTES LATER PROBLEM REO - [SDR CALA0100470](https://openairdocs.org/sdr/CALA0100470), May 17, 2001: FLOOR SUPPORT. CRACKED. INSPECTION FOUND A 6 INCH CRACK IN CENTER CARGO FLOOR SUPPORT FLANGE AT STA 1601, X = 18R. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM - [SDR CALA0100469](https://openairdocs.org/sdr/CALA0100469), May 17, 2001: SEAT TRACK. CORRODED. INSPECTION FOUND SEAT TRACK CORRODED AT STA Y = 2000-2007, X = 90L. THE SEAT TRACK WAS REPAIRED IAW SRM 53-70-00, FIGURE 5 AND ECRA 5100-01844. - [SDR CALA0100466](https://openairdocs.org/sdr/CALA0100466), May 16, 2001: SKIN. CRACKED. INSPECTION FOUND A CRACK IN RT WING LEADING EDGE SKIN AT SLAT NR 7 I/B TRACK, XORS 79.9. REPAIRED IAW SRM 57-10-00. - [SDR CALA0100465](https://openairdocs.org/sdr/CALA0100465), May 16, 2001: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR CLEAT IN CENTER CARGO BILGE CORRODED AT STA 1801 BETWEEN LONGERON 49L AND 49R. THE SHEAR CLEAT WAS REMOVED AND A NEW SHEAR CLEAT WAS INST - [SDR CALA0100464](https://openairdocs.org/sdr/CALA0100464), May 16, 2001: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR CLEAT CORRODED AT STA 1841 BETWEEN LONGERON 48R AND 47R. THE SHEAR CLEAT WAS REMOVED AND A NEW SHEAR CLEAT WAS INSTALLED IAW SRM 51-30-01 - [SDR CALA0100463](https://openairdocs.org/sdr/CALA0100463), May 16, 2001: SHEAR TIE. CORRODED. INSPECTION FOUND SHEAR CLEAT CORRODED AT STA 1902 BETWEEN LONGERONS 51R AND 50R AND BETWEEN LONGERONS 48L AND 47L. THE SHEAR CLEATS WERE REMOVED AND NEW SHEAR C - [SDR CALA0100462](https://openairdocs.org/sdr/CALA0100462), May 16, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND J-SECTION FLOOR SUPPORT CORRODED AT STA Y = 824, X = 50 TO 74. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-14-01 AND GMM 10-900-01. - [SDR CALA0100456](https://openairdocs.org/sdr/CALA0100456), May 13, 2001: FLOOR SUPPORT. CORRODED. INSPECTION FOUND LAV J O/B FLOOR SUPPORT BEAM CORRODED IN AREAS OF TIE DOWN BOLTS AT STAY = 1887-2007 AT X = 58R. THE FLOOR SUPPORT BEAM WAS REMOVED AND A NEW F - [SDR CALA0100450](https://openairdocs.org/sdr/CALA0100450), May 8, 2001: BEAM. CORRODED. INSPECTION FOUND REAR PRESSURE BULKHEAD T-SECTION LATERAL BEAM CORRODED AT ATTACHMENT POINTS AT STA Y = 2007 AND X = 58R, 58L, 27R, AND 27L. A NEW BEAM WAS INST - [SDR HALA0000237](https://openairdocs.org/sdr/HALA0000237), Jul 22, 2000: FUSE. FAILED. FLT 006 - OGG - AFTER ENGINE START AC BUS TIE WAS NOT POWERED BY ANY GENERATOR. PERFORMED AC BUS TIE. ISOL LIGHTS ILLUMINATED. NO CHANGE. TROUBLESHOT AND FOUND - [SDR HALA0000236](https://openairdocs.org/sdr/HALA0000236), Jul 22, 2000: PUMP. FAILED. FLT 006 - OGG - NR 2 ENGINE DRIVEN HYDRAULIC PUMP WOULD NOT DEPRESSURIZE WITH SWITCH IN OFF POSITION. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP, LEFT PUM - [SDR CALA0000395](https://openairdocs.org/sdr/CALA0000395), Apr 4, 2000: HINGE. CRACKED. INSPECTION FOUND A 0.2 INCH CRACK IN RT WING TRAILING EDGE HINGE AT STA XORS 714. THE HINGE WAS REPLACED IAW SRM 57-31-01. - [SDR CALA9900664](https://openairdocs.org/sdr/CALA9900664), Jun 10, 1999: FUSE. BLOWN. THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE FROM ROWS 35-45 A/B. MAINTENANCE FOUND A FUSE BLOWN FOR THAT SECTION. THE FUSE WAS REPLACED. OPERATION OF THE LIGHTS - [SDR CALA9900333](https://openairdocs.org/sdr/CALA9900333), Mar 27, 1999: SKIN. CORRODED. INSPECTION FOUND RT WING O/B AILERON LOWER SKIN CORRODED. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-02. - [SDR CALA9900331](https://openairdocs.org/sdr/CALA9900331), Mar 26, 1999: PANEL. CRACKED. INSPECTION FOUND A 3 INCH CRACK ON NR 3 PYLON PANEL NR 487ER. THE PANEL WAS REPLACED IAW SRM 51-30-00. - [SDR CALA9900330](https://openairdocs.org/sdr/CALA9900330), Mar 26, 1999: PANEL. CRACKED. INSPECTION FOUND A 3 INCH CRACK IN RT WING LEADING EDGE ACCESS PANEL NR 617CT. THE PANEL WAS REPLACED IAW SRM 51-31-01. - [SDR CALA9900325](https://openairdocs.org/sdr/CALA9900325), Mar 25, 1999: SKIN. CRACKED. INSPECTION FOUND A 1 CRACK IN NR 3 PYLON SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5450-01212. A DIP WAS ISSUED TO CHECK BLIND FASTENERS FOR SECURITY EVERY - [SDR CALA9900324](https://openairdocs.org/sdr/CALA9900324), Mar 25, 1999: BATTERY. DISCHARGED. INSPECTION FOUND FLASHLIGHTS INOPERATIVE AT FLIGHT ATTENDANT SEATS 1L-4L AFT. THE FLASHLIGHT BATTERIES WERE REPLACED IAW MM 25-60-00. - [SDR CALA9900321](https://openairdocs.org/sdr/CALA9900321), Mar 24, 1999: SKIN. CRACKED. INSPECTION FOUND A 1 CRACK IN RT WING OUTBOARD FLAP SKIN. THE SKIN WAS REPLACED IAW DOUGLAS DRAWING ARC1653. - [SDR CALA9900320](https://openairdocs.org/sdr/CALA9900320), Mar 24, 1999: INLET. CRACKED. INSPECTION FOUND TWO INCH CRACKS IN THE NR 3 ENGINE FAN INLET. REPAIRED IAW SRM 54-11-00, PAGE 23. - [SDR CALA9900319](https://openairdocs.org/sdr/CALA9900319), Mar 24, 1999: SKIN. CRACKED. INSPECTION FOUND A 1.5 CRACK IN SKIN OF PACK DOOR NR 3. THE AREA WAS REPAIRED IAW SRM 53-50-00, FIGURE 3. - [SDR CALA9900302](https://openairdocs.org/sdr/CALA9900302), Mar 20, 1999: SKIN. CRACKED. INSPECTION FOUND A .75 INCH CRACK IN LT MLG DOOR SKIN. REPAIRED IAW SRM 53-00-01. - [SDR CALA9900242](https://openairdocs.org/sdr/CALA9900242), Mar 10, 1999: SKIN. CRACKED. INSPECTION FOUND A .25 INCH CRACK NEAR WING SKIN PANEL 515AB HOLE. A REPAIR WAS PERFORMED IAW SRM 57-00-01, FIGURE 4. - [SDR CALA9801806](https://openairdocs.org/sdr/CALA9801806), Sep 20, 1998: FUSE. REQD BLEEDING. THE LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION AFTER TAKEOFF. THE APPROPRIATE CHECKLIST WAS COMPLETED WITH NO HELP. THE AIRCRAFT WAS RETURNED TO IAH WHER - [SDR CALA9800267](https://openairdocs.org/sdr/CALA9800267), Feb 16, 1998: JAMB. CRACKED. INSPECTION FOUND TWO, 2 INCH CRACKS AT UPPER SIDE OF FORWARD VERTICAL DOOR JAMB OF LT FORWARD AIR CONDITIONING COMPARTMENT. ONE AREA WAS TRIMMED AND BLENDED OUT - [SDR CALA9601511](https://openairdocs.org/sdr/CALA9601511), Oct 25, 1996: CONNECTOR. PULLED WIRE. THE RT MLG RED UNSAFE LIGHT ILLUMINATED DURING APPROACH FOR LANDING AT LGW. THE APPROACH WAS ABORTED AND ALTERNATE GEAR EXTENSION WAS USED. GEAR DOWN INDICATION - [SDR CALA9601319](https://openairdocs.org/sdr/CALA9601319), Sep 18, 1996: HYD LINE. LEAKING. THE AIRCRAFT LOST THE NR 1 HYDRAULIC SYSTEM WHILE IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGIN - [SDR CAL950500](https://openairdocs.org/sdr/CAL950500), Jun 18, 1995: HYD LINE. LEAKING. EWR - FLT 0010 - THE NR 1 HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ENROUTE FROM IAH TO ORY. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. M - [SDR CAL950406](https://openairdocs.org/sdr/CAL950406), May 19, 1995: HARNESS. BURNED. FLT 57 - LGW - SEVERAL C/B'S POPPED AND BOTH THE NR 1 AND NR 2 GEN'S HAD NO VOLTS AND NO FREQUENCY WHILE EN ROUTE FROM ORY TO EWR. THE CREW WAS UNABLE TO RESTOR - [SDR CAL950343](https://openairdocs.org/sdr/CAL950343), Apr 24, 1995: FIRE LOOP. DAMAGED. EWR - FLT 56 - AFTER TAKEOFF. NR 3 ENGINE 'A' FIRE LIGHT AND BELL CAME ON. DUMPED FUEL AND RETURNED TO EWR. FOUND FWD PYLON DETECTION ASSY DAMAGED. REF MM 26-15 - [SDR CAL950319](https://openairdocs.org/sdr/CAL950319), Apr 24, 1995: LOOP. DAMAGED. FLT NR 56 - EWR - ON TAKEOFF WARNING BELL CAME ON AIRCRAFT RETURNED TO EWR 'NO EMERGENCY DECLARED'. MAINTENANCE FOUND DAMAGE TO FIRE LOOP FWD HALF. REPAIRED 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 19920730030639I](https://openairdocs.org/incident/19920730030639I), Jul 30, 1992: Doug DC1030 (N12061), San Francisco, CA. Aircraft developed leak in NR3 hydraulic system. All pressure lost. Diverted. Found o ring oil leak. ## Other aircraft with N12061 - [Cancelled 1933-01-11](https://openairdocs.org/deregistered/N12061-1933-01-11): Lester E Swain SWAIN, S/N 1. Owner: [Swain Lester E](https://openairdocs.org/faa-owner/SWAIN%20LESTER%20E) --- 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.