N12061, cancelled Jun 7, 2017

Service difficulty reports · 32

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N12061' AND deregistration_id = 'N12061-2017-06-07'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR HALA0100248Rccb · failedLAX - FLT 32 - AIR DIVERSION AT 3 HOURS INTO FLIGHT, LT EMERGENCY AC BUS OFF LIGHT ILLUMINATED, RESTORED SYSTEM. FOLLOWED CHECKLIST, 5 MINUTES LATER PROBLEM REOCCURRED. NR 1 GALLEY POWER OFF LIGHT ILLUMINATED. COULD NOT RESTORE POWER BY RESETTING, REMAINED Oct 10, 2001 · N12061 · Doug DC1030 · DC Power Distribution SystemSDR CALA0100470Floor Support · crackedINSPECTION 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 53-30-1 AND GMM 10-900-01.May 17, 2001 · N12061 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0100469Seat Track · corrodedINSPECTION 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.May 17, 2001 · N12061 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100466Skin · crackedINSPECTION 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.May 16, 2001 · N12061 · Doug DC1030 · Wing, Plate/SkinSDR CALA0100465Shear Tie · corrodedINSPECTION 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 INSTALLED IAW SRM 51-30-01 AND GMM 10-900-01.May 16, 2001 · N12061 · Doug DC1030 · Fuselage Main, StructureSDR CALA0100464Shear Tie · corrodedINSPECTION 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 AND GMM 10-900-01.May 16, 2001 · N12061 · Doug DC1030 · Fuselage Main, StructureSDR CALA0100463Shear Tie · corrodedINSPECTION 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 CLEATS WERE INSTALLED IAW SRM 51-30-01 AND GMM 10-900-01.May 16, 2001 · N12061 · Doug DC1030 · Fuselage Main, StructureSDR CALA0100462Floor Support · corrodedINSPECTION 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.May 16, 2001 · N12061 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0100456Floor Support · corrodedINSPECTION 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 FLOOR SUPPORT BEAM WAS INSTALLED IAW SRM 53-16-01.May 13, 2001 · N12061 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0100450Beam · corrodedINSPECTION 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 INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.May 8, 2001 · N12061 · Doug DC1030 · Fuselage Miscellaneous StructureSDR HALA0000237Fuse · failedFLT 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 BCU INPUT FUSE LIGHT ON. REPLACED FUSE. RAN ALL 3 ENGINES. AC BUS TIE ISOLATION OFF. BUSSES Jul 22, 2000 · N12061 · Doug DC1030 · AC Power Distribution SystemSDR HALA0000236Pump · failedFLT 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 PUMP. OPERATIONAL AND LEAK CHECK GOOD. ALL HYDRAULIC QUANTITIES ARE AT NORMAL FULL LEVEL. WORK DONEJul 22, 2000 · N12061 · Doug DC1030 · Hydraulic Pump (Electric/Engine), MainSDR CALA0000395Hinge · crackedINSPECTION 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.Apr 4, 2000 · N12061 · Doug DC1030 · Wing Miscellaneous StructureSDR CALA9900664Fuse · blownTHE 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 CHECKED GOOD.Jun 10, 1999 · N12061 · Doug DC1030 · Emergency LightingSDR CALA9900333Skin · corrodedINSPECTION FOUND RT WING O/B AILERON LOWER SKIN CORRODED. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-02.Mar 27, 1999 · N12061 · Doug DC1030 · AileronsSDR CALA9900331Panel · crackedINSPECTION FOUND A 3 INCH CRACK ON NR 3 PYLON PANEL NR 487ER. THE PANEL WAS REPLACED IAW SRM 51-30-00.Mar 26, 1999 · N12061 · Doug DC1030 · Nacelle/Pylon, Plate/SkinSDR CALA9900330Panel · crackedINSPECTION FOUND A 3 INCH CRACK IN RT WING LEADING EDGE ACCESS PANEL NR 617CT. THE PANEL WAS REPLACED IAW SRM 51-31-01.Mar 26, 1999 · N12061 · Doug DC1030 · Wing, Plate/SkinSDR CALA9900325Skin · crackedINSPECTION 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 1000 CYCLES UNTIL A PERMANENT REPAIR IS INSTALLED WITHIN 400 DAYS.Mar 25, 1999 · N12061 · Doug DC1030 · Nacelle/Pylon, Plate/SkinSDR CALA9900324Battery · dischargedINSPECTION FOUND FLASHLIGHTS INOPERATIVE AT FLIGHT ATTENDANT SEATS 1L-4L AFT. THE FLASHLIGHT BATTERIES WERE REPLACED IAW MM 25-60-00.Mar 25, 1999 · N12061 · Doug DC1030 · Emergency LightingSDR CALA9900321Skin · crackedINSPECTION FOUND A 1 CRACK IN RT WING OUTBOARD FLAP SKIN. THE SKIN WAS REPLACED IAW DOUGLAS DRAWING ARC1653.Mar 24, 1999 · N12061 · Doug DC1030 · Trailing Edge FlapsSDR CALA9900320Inlet · crackedINSPECTION FOUND TWO INCH CRACKS IN THE NR 3 ENGINE FAN INLET. REPAIRED IAW SRM 54-11-00, PAGE 23.Mar 24, 1999 · N12061 · Doug DC1030 · Engine Cowling SystemSDR CALA9900319Skin · crackedINSPECTION FOUND A 1.5 CRACK IN SKIN OF PACK DOOR NR 3. THE AREA WAS REPAIRED IAW SRM 53-50-00, FIGURE 3.Mar 24, 1999 · N12061 · Doug DC1030 · Air Conditioning DoorsSDR CALA9900302Skin · crackedINSPECTION FOUND A .75 INCH CRACK IN LT MLG DOOR SKIN. REPAIRED IAW SRM 53-00-01.Mar 20, 1999 · N12061 · Doug DC1030 · Landing Gear DoorsSDR CALA9900242Skin · crackedINSPECTION FOUND A .25 INCH CRACK NEAR WING SKIN PANEL 515AB HOLE. A REPAIR WAS PERFORMED IAW SRM 57-00-01, FIGURE 4.Mar 10, 1999 · N12061 · Doug DC1030 · Wing, Plate/SkinSDR CALA9801806Fuse · reqd bleedingTHE 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 WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TRIM CYLINDER INTERLOCK FUSE IN THE RT WHEEL Sep 20, 1998 · N12061 · Doug DC1030 · Landing Gear Retraction/Extension SystemSDR CALA9800267Jamb · crackedINSPECTION 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. THE OTHER AREA WAS REWORKED AND REINFORCED WITH A DOUBLER IAW SRM 53-30-00, FIGURE 4. NEW RIVETFeb 16, 1998 · N12061 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9601511Connector · pulled wireTHE RT MLG RED UNSAFE LIGHT ILLUMINATED DURING APPROACH FOR LANDING AT LGW. THE APPROACH WAS ABORTED AND ALTERNATE GEAR EXTENSION WAS USED. GEAR DOWN INDICATIONS WERE NORMAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG PROXIMITY DOOct 25, 1996 · N12061 · Doug DC1030 · Landing Gear Position and WarningSDR CALA9601319Hyd Line · leakingTHE 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 ENGINE LT HYDRAULIC PUMP SUPPLY LINE LEAKING. THE HYDRAULIC SUPPLY LINE WAS REMOVED AND REPLACED. THESep 18, 1996 · N12061 · Doug DC1030 · Hydraulic System, MainSDR CAL950500Hyd Line · leakingEWR - 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. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE FROM THE LEFT ENGINE DRIVEN PUMP TO THE PRESSURE MODUJun 18, 1995 · N12061 · Doug DC1030 · Hydraulic System, MainSDR CAL950406Harness · burnedFLT 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 RESTORE EITHER GEN AND THE A/C WAS DIVERTED TO LGW WHERE IT LANDED W/O INCIDENT. ALL TRIPPED C/B'S WERE May 19, 1995 · N12061 · Doug DC1030 · Electrical Power System WiringSDR CAL950343Fire Loop · damagedEWR - 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 26-15-01 ITEM 117, REPLACED PART AUL7122-1 OPS. CHECK SYSTEM, ALL NORMAL. (Z)Apr 24, 1995 · N12061 · Doug DC1030 · Fire DetectionSDR CAL950319Loop · damagedFLT 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 REPLACED DAMAGED AREA AND PARTS. OPS CHECKED, SYSTEMS ALL NORMAL. AIRCRAFT DEPARTED NO FURTHER Apr 24, 1995 · N12061 · Doug DC1030 · Fire Detection
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