# Service difficulty reports: N87070, cancelled May 14, 2004 A list on [N87070, cancelled May 14, 2004](https://openairdocs.org/deregistered/N87070-2004-05-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR CALA0001835](https://openairdocs.org/sdr/CALA0001835.md): Floorbeam · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Main, Floor Beam > INSPECTION 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. - [SDR CALA0001834](https://openairdocs.org/sdr/CALA0001834.md): Structure · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001833](https://openairdocs.org/sdr/CALA0001833.md): Beam · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001832](https://openairdocs.org/sdr/CALA0001832.md): Structure · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001831](https://openairdocs.org/sdr/CALA0001831.md): Beam · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001830](https://openairdocs.org/sdr/CALA0001830.md): Beam · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001829](https://openairdocs.org/sdr/CALA0001829.md): Structure · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001828](https://openairdocs.org/sdr/CALA0001828.md): Support Bracket · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001827](https://openairdocs.org/sdr/CALA0001827.md): Angle · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001826](https://openairdocs.org/sdr/CALA0001826.md): Structure · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001825](https://openairdocs.org/sdr/CALA0001825.md): Support Bracket · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001824](https://openairdocs.org/sdr/CALA0001824.md): Structure · corroded · Nov 24, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001823](https://openairdocs.org/sdr/CALA0001823.md): Support Bracket · corroded · Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001822](https://openairdocs.org/sdr/CALA0001822.md): Support Bracket · corroded · Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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 EC - [SDR CALA0001821](https://openairdocs.org/sdr/CALA0001821.md): Support Bracket · corroded · Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA0001820](https://openairdocs.org/sdr/CALA0001820.md): Seat Track · corroded · Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION 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. - [SDR CALA0001819](https://openairdocs.org/sdr/CALA0001819.md): Floor Support · corroded · Nov 23, 2000 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9901497](https://openairdocs.org/sdr/CALA9901497.md): Beam · corroded · Nov 14, 1999 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD AVIONICS BAY CROSS BEAM CORRODED AT STA Y475, LT SIDE. REPAIRED IAW ECRA 5312-01015 AND FLS DRAWING 90-53-1057. - [SDR CALA9801430](https://openairdocs.org/sdr/CALA9801430.md): Skin · cracked · Aug 7, 1998 · N87070 · Doug DC1030 · Passenger/Crew Doors > INSPECTION FOUND A SMALL CRACK WITH SOME PULLED RIVETS IN TOP EDGE OF DOOR L-4 SKIN. REPAIRED IAW ECRA 5210-01332. - [SDR CALA9800958](https://openairdocs.org/sdr/CALA9800958.md): Bracket · failed · Jun 3, 1998 · N87070 · Doug DC1030 · Landing Gear Brake System > THE 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 LINK - [SDR CALA9800001](https://openairdocs.org/sdr/CALA9800001.md): Hyd Line · ruptured · Jan 4, 1998 · N87070 · Doug DC1030 · Hydraulic System, Main > THE 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 REPLACE - [SDR CALA9701528](https://openairdocs.org/sdr/CALA9701528.md): Support · corroded · Sep 18, 1997 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9701527](https://openairdocs.org/sdr/CALA9701527.md): Floor Support · corroded · Sep 17, 1997 · N87070 · Doug DC1030 · Fuselage Miscellaneous Structure > INSPECTION 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. - [SDR CALA9601798](https://openairdocs.org/sdr/CALA9601798.md): Skin · cracked · Oct 10, 1996 · N87070 · Doug DC1030 · Wing, Plate/Skin > A-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. - [SDR CALA9601470](https://openairdocs.org/sdr/CALA9601470.md): Skin · cracked · Oct 10, 1996 · N87070 · Doug DC1030 · Wing, Plate/Skin > RIGHT HAND WING LEADING EDGE LOWER SKIN AT STATION XOS602 HAS A ONE INCH CRACK. INSTALLED DOUBLER PER EC/RA 5730-01421 REV A. - [SDR CALA9601203](https://openairdocs.org/sdr/CALA9601203.md): Trim Motor · leaking · Aug 21, 1996 · N87070 · Doug DC1030 · Stabilizer Control System > THE 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 WER - [SDR CAL960187](https://openairdocs.org/sdr/CAL960187.md): Air Duct · failed · Feb 22, 1996 · N87070 · Doug DC1030 · Turbine Engine Compressor Section > IAH - 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 REVEALE - [SDR CAL950105](https://openairdocs.org/sdr/CAL950105.md): Linkage · binding · Feb 7, 1995 · N87070 · Doug DC1030 · Power Lever > EWR - 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 ADD - [SDR CAL950082](https://openairdocs.org/sdr/CAL950082.md): Oil Tube · leaking · Feb 1, 1995 · N87070 · Doug DC1030 · Engine Oil Distribution (Airframe Furnished) > EWR - 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 OPE ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N87070-2004-05-14/reports --- 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.