N87070, cancelled May 14, 2004

Service difficulty reports · 29

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 = 'N87070' AND deregistration_id = 'N87070-2004-05-14'
  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 CALA0001835Floorbeam · corrodedINSPECTION FOUND FORWARD GALLEY/LAV AREA FLOORBEAM SECTIONS CORRODED AT Y = 375-475, X = 30R, 46R-48R, AND 50R-60R. THE FLOORBEAM SECTIONS WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW SRM 53-11-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Main, Floor BeamSDR CALA0001834Structure · corrodedINSPECTION FOUND GALLEY G3 FORWARD J-SECTIONS CORRODED AT STA Y = 450, X = 2L-19L, AND AT X = 2R-19R. THE J-SECTIONS WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW ECRA 5100-01844 AND SRM 53-11-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001833Beam · corrodedINSPECTION FOUND LAV E AND F I/B SUPPORT BEAMS CORRODED AT Y = 1844-1857, X = 5R AND AT X = 5L. THE SUPPORT BEAMS WERE REMOVED AND NEW SUPPORT BEAMS WERE INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001832Structure · corrodedINSPECTION FOUND GALLEY G3 FORWARD J-SECTION CORRODED AT STA Y = 450, X = 25R-50R. THE J-SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5100-01844 AND SRM 53-11-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001831Beam · corrodedINSPECTION FOUND GALLEY G3 L/H AND R/H O/B SUPPORT BEAMS CORRODED AT STA Y = 450-535, X = 24L AND AT X = 23R. THE SUPPORT BEAMS WERE REMOVED AND NEW SUPPORT BEAMS WERE INSTALLED IAW ECRA 5100-01844 AND SRM 53-11-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001830Beam · corrodedINSPECTION FOUND LAV E O/B SUPPORT BEAM CORRODED AT STA Y = 1821-1884, X = 36L. THE SUPPORT BEAM WAS REMOVED AND A NEW SUPPORT BEAM WAS INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001829Structure · corrodedINSPECTION FOUND TRANSVERSE J-SECTION AFT OF LAVS E AND F CORRODED AT STA Y = 1884, X = 38L-58L, AND AT X = 39R-58R. THE J-SECTIONS WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001828Support Bracket · corrodedINSPECTION FOUND LONGITUDINAL J-SECTION FLOOR SUPPORT BEAM CORRODED AT STA Y = 1900-2007, X = 24L. THE SUPPORT BEAM WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001827Angle · corrodedINSPECTION FOUND T-ANGLE ON REAR PRESSURE BULKHEAD CORRODED AT ATTACHMENT POINTS TO FORE AND AFT BEAMS AT STA Y = 2007, X = 24L, 58L, 24R, AND 58R. THE T-ANGLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-40-00, FIGURE 16.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001826Structure · corrodedINSPECTION FOUND TRANSVERSE J-SECTIONS AFT OF LAVS E AND F CORRODED AT STA Y = 1884, X = 60R-90R, X = 60L-90L, AND X = 27R-33R. THE J-SECTIONS WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001825Support Bracket · corrodedINSPECTION FOUND LONGITUDINAL J SECTION FLOOR SUPPORT BEAM CORRODED AT STA Y = 1900-2007, X = 24R. THE SUPPORT BEAM WAS REMOVED AND A NEW SUPPORT BEAM WAS INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001824Structure · corrodedINSPECTION FOUND TRANSVERSE J SECTION AFT OF LAVS E AND F CORRODED AT STA Y = 1884, X = 27L-33L. THE J SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001823Support Bracket · corrodedINSPECTION FOUND LAV F O/B SUPPORT BEAM CORRODED AT STA Y = 1821-1884, X = 36R. THE SUPPORT BEAM WAS REMOVED AND A NEW SUPPORT BEAM WAS INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001822Support Bracket · corrodedINSPECTION FOUND GALLEY G6 SUPPORT BEAMS CORRODED AT POSITION JUST FORWARD OF REAR PRESSURE BULKHEAD AND AT EACH ATTACHMENT POINT, STA 1884-2007, X = 24L AND AT STA 1900-2007, X = 58L. THE SUPPORT BEAMS WERE REMOVED AND NEW SUPPORT BEAMS WERE INSTALLED IAW ECNov 23, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001821Support Bracket · corrodedINSPECTION FOUND GALLEY G7 SUPPORT BEAMS CORRODED AT STA 1900-2007, X= 57R, AND AT STA 1884-2007, X= 25R. THE SUPPORT BEAMS WERE REMOVED AND NEW SUPPORT BEAMS WERE INSTALLED IAW ECRA 5100-01844 AND SRM 53-16-01.Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA0001820Seat Track · corrodedINSPECTION FOUND O/B LEFT AND RIGHT SEAT TRACKS CORRODED AT ATTACHMENT TO REAR PRESSURE BULKHEAD T-PIECE AT STA 1986-2007, X= 72L AND X= 72R. THE CORRODED SECTIONS OF SEAT TRACK WERE REMOVED AND NEW SECTIONS WERE INSTALLED IAW SRM 53-70-00, FIGURE 2.Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001819Floor Support · corrodedINSPECTION FOUND FLOOR PANEL 293HF CENTER U-CHANNEL SUPPORT CORRODED AT STA Y = 1900-2007, X = 0. THE CORRODED SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-16-01 AND ECRA 5100-01844.Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9901497Beam · corrodedINSPECTION FOUND FORWARD AVIONICS BAY CROSS BEAM CORRODED AT STA Y475, LT SIDE. REPAIRED IAW ECRA 5312-01015 AND FLS DRAWING 90-53-1057.Nov 14, 1999 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9801430Skin · crackedINSPECTION FOUND A SMALL CRACK WITH SOME PULLED RIVETS IN TOP EDGE OF DOOR L-4 SKIN. REPAIRED IAW ECRA 5210-01332.Aug 7, 1998 · N87070 · Doug DC1030 · Passenger/Crew DoorsSDR CALA9800958Bracket · failedTHE LT MLG RED LIGHT REMAINED ILLUMINATED ON BOTH PANELS WITH GEAR UP AFTER TAKEOFF FROM EWR. A VISUAL CHECK THROUGH VIEWPORT INDICATED DOOR PARTIALLY OPEN. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TORQUE LINKJun 3, 1998 · N87070 · Doug DC1030 · Landing Gear Brake SystemSDR CALA9800001Hyd Line · rupturedTHE AIRCRAFT LOST NR 1 HYDRAULIC SYSTEM QUANTITY WHILE EN ROUTE. FLIGHT MANUAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE LEFT PUMP SUCTION LINE RUPTURED. THE LINE WAS REMOVED AND REPLACEJan 4, 1998 · N87070 · Doug DC1030 · Hydraulic System, MainSDR CALA9701528Support · corrodedINSPECTION FOUND CORROSION ON FLOOR SUPPORT PANEL IN MID DECK FORWARD LAV/GALLEY AT STA 420. THE PANEL WAS REMOVED AND A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-33-01, FIGURE 1.Sep 18, 1997 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9701527Floor Support · corrodedINSPECTION FOUND MID DECK AFT LAV/GALLEY FLOOR SUPPORT CORRODED AT STA 1841 TO 1887. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, FIGURE 10E AND 51-33-01, FIGURE 1.Sep 17, 1997 · N87070 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9601798Skin · crackedA-1 CRACK WAS FOUND IN THE RT WING LOWER LEADING EDGE SKIN AT XOS 602. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5730-01421, REV A.Oct 10, 1996 · N87070 · Doug DC1030 · Wing, Plate/SkinSDR CALA9601470Skin · crackedRIGHT HAND WING LEADING EDGE LOWER SKIN AT STATION XOS602 HAS A ONE INCH CRACK. INSTALLED DOUBLER PER EC/RA 5730-01421 REV A.Oct 10, 1996 · N87070 · Doug DC1030 · Wing, Plate/SkinSDR CALA9601203Trim Motor · leakingTHE HYDRAULIC SYSTEM NR 3 ELEVATOR OFF CAUTION LIGHT ILLUMINATED AND THE NR 3 HYDRAULIC QUANTITY BEGAN TO DECREASE WHILE EN ROUTE FROM FRA TO EWR. SHORTLY AFTERWARDS, THE NR 3 LEFT HYDRAULIC PUMP PRESSURE LOW LIGHT ILLUMINATED. ALL APPROPRIATE CHECKLISTS WERAug 21, 1996 · N87070 · Doug DC1030 · Stabilizer Control SystemSDR CAL960187Air Duct · failedIAH - FLT 0010 - TAKEOFF WAS REJECTED AT 100 KNOTS AFTER THE NR 3 ENGINE EXPERIENCED LOSS OF POWER. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT: PRELIMINARY INVESTIGATION REVEALEFeb 22, 1996 · N87070 · Doug DC1030 · Turbine Engine Compressor SectionSDR CAL950105Linkage · bindingEWR - FLT 0063 - TAKEOFF WAS ABORTED AT 110 KNOTS WHEN THE NR 2 ENGINE THROTTLE WOULD NOT MOVE PAST THE 25 DEGREE ANGLE POSITION. MAINTENANCE FOUND THE NR 2 ENGINE THROTTLE BINDING. THE POWER LEVER LINKAGE WAS MISALIGNED AT THE QUADRANT CONNECTION AND AN ADDFeb 7, 1995 · N87070 · Doug DC1030 · Power LeverSDR CAL950082Oil Tube · leakingEWR - FLT 0004 - THE NR 2 ENGINE LOST OIL QUANTITY WHILE IN-FLIGHT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TAKEN OUT OF SERVICE AND AN ENGINE CHANGE IS PLANNED. THE SDR WILL REMAIN OPEFeb 1, 1995 · N87070 · Doug DC1030 · Engine Oil Distribution (Airframe Furnished)
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