N17085

Service difficulty reports · 33

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 = 'N17085' AND registry_match = 'registration'
  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 CNMA20060032Battery Pack · dischargedWHILE TESTING EMERGENCY LIGHTS MID-CABIN BATTERY FAILED. REMOVED AND REPLACED MID-CABIN EMERGENCY LIGHT BATTERY PACK OPS CHECK GOOD IAW MM 33-51.Dec 18, 2006 · N17085 · Doug DC1030 · Emergency LightingSDR CNMA20060010Rotor · damagedNR 3 ENGINE 3RD STAGE LPT ROTOR IS RUBBING ON 4TH STAGE ROTOR. REMOVED AND REPLACED ENGINE S/N 517720.May 15, 2006 · N17085 · Doug DC1030 · Turbine SectionSDR 2005000011Pump · failedREJECTED TAKE OFF AT 80 KNOTS NR 2 ENGINE WILL NOT MAKE POWER ONLY WENT TO 110 PERCENT N1 LOWER THAN 1&3. CORRECTIVE ACTION REMOVED AND REPLACED THE FUEL PUMP AND M.E.C. STILL IN WORK.Jul 19, 2005 · N17085 · Doug DC1030 · Engine Fuel PumpSDR 2005000004Power Supply · failedON PRE-FLIGHT, FOUND EMERGENCY LIGHT TEST LAMP INOP (GREEN LIGHT ON OVERHEAD PANEL). REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY PER MM 33-51.May 18, 2005 · N17085 · Doug DC1030 · Emergency LightingSDR 2004000012Floor Panel · overheatedEXCESSIVE HEAT COMING FROM FLOOR AND WALL FORWARD AND AFT OF L-2 DOOR. TROUBLESHOOTING AS OF 10/5/04.Oct 4, 2004 · N17085 · Doug DC1030 · Aircraft StructuresSDR 2004000013Duct · blownAIRCRAFT DIVERTED TO BWI ,DUE TO BLEED AIR LEAK IN L2 DOOR AREA. NR 3 PNEUMATIC SYSTEM ALREADY DEFERRED. REPLACED BLOWN DUCT IN FWD CARGO AREA.Oct 3, 2004 · N17085 · Doug DC1030 · Pneumatic Distribution SystemSDR CNMA200300007Battery Pack · failedEMERGENCY EGRESS LIGHTS FAIL TO TEST. BATTERY PACK FAILED.Dec 2, 2003 · N17085 · Doug DC1030 · Emergency LightingSDR CALA0100815Skin · crackedINSPECTION FOUND A 1" CRACK IN FORWARD CARGO DOOR SKIN(DOUBLER) ON LATCH ACCESSORY DOOR CUTOUT AREA. THE CRACKED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 9.Aug 28, 2001 · N17085 · Doug DC1030 · Cargo/Baggage DoorsSDR CALA0100814Seat Track · corrodedINSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT Y = 1860, X = -60.00, JUST AFT OF R-4 ATTENDANT SEAT. THE CORRODED SECTION OF SEAT TRACK WAS CUT OUT AND A NEW SECTION OF SEAT TRACK WAS INSTALLED USING SPLICE HAT AND SPLICE PLATE IAW SRM 53-70-00, FIGURE 1.Aug 28, 2001 · N17085 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0100808Seat Track · corrodedINSPECTION FOUND MAIN DECK SEAT TRACK CORRODED AT X = 107.25 AND Y = 800-824. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK SECTION WAS SPLICED IN IAW SRM 53-70-00, FIGURE 1.Aug 26, 2001 · N17085 · Doug DC1030 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001209Panel · delaminatedINSPECTION FOUND NR 2 ENGINE NOSE COWL PANEL 363AL DELAMINATED. THE PANEL WAS REPLACED IAW MM 20-50-02.Aug 5, 2000 · N17085 · Doug DC1030 · Engine Cowling SystemSDR CALA9900784Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 2 ENGINE PYLON SKIN WITH LOOSE FASTENERS ON PYLON FIN. THE SKIN WAS REPAIRED IAW SRM 54-20-00, FIGURE 6 AND FASTENERS WERE REPLACED IAW SRM 51-31-00.Jul 2, 1999 · N17085 · Doug DC1030 · Nacelle/Pylon, Plate/SkinSDR CALA9900783Skin · corrodedINSPECTION FOUND LT WING O/B AILERON UPPER SKIN CORRODED AT STA 917. THE AILERON WAS REPLACED IAW MM 27-10-02.Jul 2, 1999 · N17085 · Doug DC1030 · AileronsSDR CALA9900782Skin · delaminatedINSPECTION FOUND THE UPPER AND LOWER SURFACE OF RT WING NR 4 SPOILER SKIN DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-60-01.Jul 2, 1999 · N17085 · Doug DC1030 · SpoilersSDR CALA9900800Longeron · crackedINSPECTION FOUND A 1 CRACK IN LEFT LONGERON AND A 1 CRACK IN RT LONGERON OF NR 2 ENGINE CORE COWL. THE CRACKS WERE LOCATED NEAR HINGES. THE LONGERONS WERE REPAIRED IAW ECRA 7110-01496.Jun 29, 1999 · N17085 · Doug DC1030 · Engine Cowling SystemSDR CALA9900799Floorbeam · crackedINSPECTION FOUND A 3 CRACK IN CENTER CARGO STRUCTURAL FLOORBEAM NR 12 BETWEEN STA 1721 AND 1741. A NEW BEAM WAS INSTALLED IAW MM 53-00-00 AND DRAWING AFT7009.Jun 26, 1999 · N17085 · Doug DC1030 · Fuselage Main, Floor BeamSDR CALA9900798Jamb · crackedINSPECTION FOUND A 1 CRACK IN CENTER CARGO DOOR JAMB AT STA 1721. THE JAMB WAS REPLACED IAW SRM 53-10-00.Jun 26, 1999 · N17085 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900797Floorbeam · crackedINSPECTION FOUND ONE EACH 1 CRACK IN CENTER CARGO STRUCTURAL FLOORBEAMS NR 9 AND NR 10 BETWEEN STA 1761 AND 1741. THE BEAMS WERE REPLACED IAW SRM 53-00-00 AND MM 25-52-00.Jun 26, 1999 · N17085 · Doug DC1030 · Fuselage Main, Floor BeamSDR CALA9900796Angle · crackedINSPECTION FOUND A 1 CRACK IN ANGLE AT UPPER AFT SECTION OF CENTER CARGO DOOR. THE ANGLE WAS REPLACED IAW SRM 51-30-00.Jun 26, 1999 · N17085 · Doug DC1030 · Cargo/Baggage DoorsSDR CALA9900795Beam · crackedINSPECTION FOUND A 3 CRACK IN CENTER CARGO NR 12 FLOOR STRUCTURAL BEAM AT STA 1821. A NEW BEAM WAS INSTALLED IAW SRM 51-30-00 AND MM 25-50-00.Jun 26, 1999 · N17085 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9900794Skin · delaminatedINSPECTION FOUND LEFT WING INBOARD FLAP UPPER SKIN UNBONDED ON INBOARD SIDE. THE SKIN WAS REPLACED IAW SRM 51-30-00.Jun 26, 1999 · N17085 · Doug DC1030 · Trailing Edge FlapsSDR CALA9900793Skin · dentedINSPECTION FOUND LEFT WING LOWER SKIN DENTED AT STA 1090. THE SKIN WAS REPLACED IAW SRM 51-30-00.Jun 24, 1999 · N17085 · Doug DC1030 · Wing, Plate/SkinSDR CALA9900792Skin · crackedINSPECTION FOUND A 2 CRACK IN LEFT WING NR 2 SLAT SKIN. REPAIRED IAW SRM 57-10-00, FIGURE 31.Jun 24, 1999 · N17085 · Doug DC1030 · Leading Edge DevicesSDR CALA9900791Skin · crackedINSPECTION FOUND A 1.25 CRACK ON RT WING UPPER SKIN DROOPED LEADING EDGE. A REPAIR WAS INSTALLED IAW SRM 57-10-00.Jun 23, 1999 · N17085 · Doug DC1030 · Wing, Plate/SkinSDR CALA9900790Bolt · brokenINSPECTION FOUND TRAPEZOIDAL PANEL BOLT IN RT MLG WHEEL WELL BROKEN AT STA 1370. THE BOLT WAS REPLACED IAW MM 20-50-02.Jun 23, 1999 · N17085 · Doug DC1030 · Wing Miscellaneous StructureSDR CALA9900789Strap · crackedINSPECTION FOUND A 1.5 CRACK IN RT WING LOWER SKIN LEADING EDGE STRAP BETWEEN STA XORS 433 AND XORS 455. A NEW STRAP WAS INSTALLED IAW DRAWING ARB2935 AND SRM 51-31-01.Jun 19, 1999 · N17085 · Doug DC1030 · Wing Miscellaneous StructureSDR CALA9900788Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN INTERNAL SKIN OF RT WING LEADING EDGE SLAT NR 4. A REPAIR WAS PERFORMED IAW SRM 57-00-01, PAGE 12, FIGURE 4, SHEET 2.Jun 19, 1999 · N17085 · Doug DC1030 · Leading Edge DevicesSDR CALA9900787Strap · crackedINSPECTION FOUND A 2 INCH EFTACK IN LEFT WING LEADING EDGE STRIP AT STA XORS 455 AND XORS 506. REPAIRED IAW DRAWING 2933 AND SRM 51-30-00.Jun 19, 1999 · N17085 · Doug DC1030 · Wing Miscellaneous StructureSDR CALA9900498Bottle · blownDOOR 4L DOOR ASSIST BOTTLE BLOWN. RESET HANDLE AND SERVICED DOOR ASSIST BOTTLE, OPERATES NORMAL.May 7, 1999 · N17085 · Doug DC1030 · Service DoorsSDR CALA9800777Recirc Fan · failedA/C DIVERTED TO MAD FROM FCO DUE TO ELECTRIC SMELL IN CABIN. FOUND NR 4 CABIN AIR RECIRCULATION FAN FAILED. FAN TO BE REPLACED.May 5, 1998 · N17085 · Doug DC1030 · Air Distribution FanSDR CALA9800515Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK ON LOWER CAP OF INTERCOSTAL AT CEILING CENTER CARGO, RBL 82, STA 1721 WITH DISTORTION ON CEILING SUPPORT AT RBL 78. A REPAIR WAS ACCOMPLISHED IAW SRM 51-21-01 AND 51-33-01.Mar 20, 1998 · N17085 · Doug DC1030 · Fuselage Miscellaneous StructureSDR CALA9701787Transfer Valve · leakingTHE AIRCRAFT LOST NR 1 HYDRAULIC SYSTEM QUANTITY AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 AND NR 3 REVERSIBLE PUMP LEAKING AT HYDRAULIC TRANSFER VALVE. THE TRANSFER VALVE, FITTINGS, ANDec 21, 1997 · N17085 · Doug DC1030 · Hydraulic System, MainSDR CALA9701360Blade · misinstalledT/O WAS REJECTED AT 5 KNOTS WHEN NR 3 ENG COMPRESSOR STALLED. THE NR 3 ENG WAS SHUT DOWN AND THE ACFT RETURNED TO THE GATE. MX INSPECTED THE NR 3 ENG AND FOUND DAMAGE. THE NR 3 ENG WAS REMOVED AND REPLACED. *S/D* THE PRIMARY CAUSE OF THE ENGINE FAILURE TOSep 14, 1997 · N17085 · Doug DC1030 · Turbine Engine Compressor Section
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