N161US, cancelled Oct 30, 2002

Service difficulty reports · 30

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 = 'N161US' AND deregistration_id = 'N161US-2002-10-30'
  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 0200811161ProjectorDuring cruise electrical odor noticed around door 3 area when overhead projector on. Flight continued to DTW and landed without incident. Maintenance replaced overhead projector.See Logpage 6991285.No previous history in last 30 days.Mar 14, 2002 · N161US · Doug DC1040 · Entertainment SystemSDR 9904381161Slide · malfunctionedDURING CRUISE DOOR 1L EMERGENCY EVACUATION SLIDE PARTIALLY INFLATED AND BROKE OUT OF THE COVER. THE SLIDE WAS PUNCTURED TO DEFLATE AND MOVED OUT OF GALLEY AREA. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SLIDE, COVER, AND Oct 15, 1999 · N161US · Doug DC1040 · Escape SlideSDR 9901341161Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 27R WEB STRUCTURE AT FS 1522 TO 1540. REPAIRED PER EA 11-162951.Feb 18, 1999 · N161US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9900991161Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON LONGERON 44R FROM FS 1009 TO 1039. REPAIRED PER EA 11-164772. REPAIRED PER EA 11-164772.Feb 17, 1999 · N161US · Doug DC1040 · Fuselage Main, Longeron/StringerSDR 9901181161Floorbeam · crackedDURING M-CHECK, FOUND CRACK ON FLOOR I BEAM AT FS 791, LBL 18 TO RBL 18. REPAIRED PER EA 11-162954.Feb 16, 1999 · N161US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9900981161Seat Track · corrodedDURING M-CHECK, FOUND GOUGING AND CORROSION ON THE OUTBOARD AFT CABIN SEAT TRACK LBL 108 AT FS 1661 TO 1700. REPAIRED PER EA 11-164769.Feb 12, 1999 · N161US · Doug DC1040 · Fuselage, Seat/Cargo Attach FittingsSDR 9901191161Frame · crackedDURING M-CHECK, FOUND CRACK IN FORWARD CARGO FLOOR FRAME AT FS 1099 AT LBL 38. REPAIRED PER EA 11-158134.Feb 5, 1999 · N161US · Doug DC1040 · Fuselage Main, FrameSDR 9811261161Power Supply · inopDURING LINE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT TEST. REPLACED OVERWING POWER SUPPLY. OPERATIONAL CHECK OK.Sep 30, 1998 · N161US · Doug DC1040 · Emergency LightingSDR 9811251161Power Supply · inopDURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING FROM DOOR 3L AND 3R TO ROW 32 INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY AND CONTROL UNIT. OPERATIONAL CHECK OK.Sep 22, 1998 · N161US · Doug DC1040 · Emergency LightingSDR 9811271161Battery Pack · dischargedDURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE FROM DOOR 3L AND 3R TO ROW 32. REPLACED BATTERY PACK ABOVE DOOR 3L. OPERATIONAL CHECK OK.Sep 18, 1998 · N161US · Doug DC1040 · Emergency LightingSDR 9804391161Cadc · failedON TAKEOFF ROLL, CAPTAIN'S AIRSPEED INDICATOR INDICATED 20 KTS BELOW FIRST OFFICER'S. ABORTED TAKEOFF AT 140 KTS AND RETURNED TO THE GATE. REPLACED THE NR 1 CADC, OPERATIONAL CHECK OK.Mar 14, 1998 · N161US · Doug DC1040 · Air Data ComputerSDR 9723131161Start Valve · malfunctionedDURING CRUISE, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLIMINATED. CREW FOLLOWED COM PROCEDURE AND THEN DIVERTED TO BOS FOR MAINTENANCE. START VALVE WAS FOUND IN THE CLOSED POSITION WHEN AIRCRAFT ARRIVED BUT WAS CHANGED PRECAUTIONARY. START VALVE INDICATIONDec 4, 1997 · N161US · Doug DC1040 · Engine Start Valves/ControlsSDR 9717151161Cadc · failedDURING CRUISE, THE NR 2 AIR DATA COMPUTER FAILED, (NR 3 CADC WAS ON PREVIOUS MEL). FLIGHT DIVERTED INTO BOS. MAINTENANCE REPLACED NR 2 CADC.Sep 10, 1997 · N161US · Doug DC1040 · Air Data ComputerSDR 9715571161Engine · failedWHILE CLIMBING THRU 2000 FEET AFTER TAKEOFF, THE NBR 2 ENGINE EGT WENT OFF SCALE HIGH AND EPR DROPPED. ENGINE WAS SHUT DOWN AND 55,000 LBS OF FUEL WAS DUMPED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE WITH NO DEFEAug 14, 1997 · N161US · Doug DC1040 · Engine (Turbine/Turboprop)SDR 9710391161Transducer · seizedDURING FLAP RETRACTION AFTER TAKEOFF, STICK SHAKER ACTIVATED, SLAT DISAGREE LIGHT AND RESET LIGHT ILLUMINATED AND COULD NOT GET SLATS TO RETRACT. DUMPED 10,000 LBS OF FUEL AND RETURNED TO SFO. MAINTENANCE REPLACED THE STALL TRANSDUCER, OPERATIONAL CHECK OK.May 25, 1997 · N161US · Doug DC1040 · Stall Warning SystemSDR 9707441161Prox Control · failedDURING GEAR RETRACTION, ALL LANDING GEAR UNSAFE LIGHTS ILLUMINATED WITH GEAR HANDLE UP. RECYCLED GEAR, NO HELP. GEAR VISULALY CHECKED UP. MAINTENANCE REPLACED MAIN LANDING GEAR PROXIMITY CONTROL.Apr 11, 1997 · N161US · Doug DC1040 · Landing Gear Position and WarningSDR 9623541161Fitting · corrodedDURING L-CHECK, FOUND THE LONGERON 48L, 49L, AND 48R END FITTINGS CORRODED FROM FS 1509 - 1521. REPLACED BOTH FITTINGS.Oct 28, 1996 · N161US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9623521161Skin · crackedDURING L-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT THE LEFT AIR CYCLE MACHINE DOOR JAMB UPPER AFT CORNER, FS 587. REPAIRED SKIN (P/N ACA 3108) PER EA 11-110287.Oct 27, 1996 · N161US · Doug DC1040 · Fuselage Main, Plate/SkinSDR 9623501161Skin · crackedDURING L-CHECK, FOUND A 1.6258 INCH CRACK IN THE RIGHT WING LOWER LEADING EDGE SKIN AT XOS 611. REPAIRED SKIN (P/N ARB2887-502) PER EA 11-110210.Oct 25, 1996 · N161US · Doug DC1040 · Wing, Plate/SkinSDR 9621511161Compressor · stalledDURING APPLICATION OF POWER FOR TAKEOFF, THE NR 3 ENGINE EXPERIENCED COMPRESSOR STALL. CREW ABORTED THE TAKEOFF AS EGT CLIMBED TO 990 DEGREES WITHIN ONE SECOND. AIRCRAFT RETURNED TO THE GATE AND VISUAL INSPECTION REVEALED NO DISCREPANCIES. BORESCOPE INSPECTOct 8, 1996 · N161US · Doug DC1040 · Turbine Engine Compressor SectionSDR 9615301161Skin · crackedDURING LINE CHECK, FOUND A CRACK IN THE LEFT OUTBOARD AILERON UPPER SKIN AT THE NR 5 RIB. REPAIRED PER EA 11-105126.Jun 27, 1996 · N161US · Doug DC1040 · AileronsSDR 9608541161Tach Generator · malfunctionedDURING CLIMBOUT, THE NR 3 ENGINE N1, N2 AND NR 3 EPR BECAME ERRATIC, ALL OTHER INDICATIONS NORMAL. CREW FOLLOWED COCKPIT OPERATING PROCEDURES AND RETURNED TO DTW WITHOUT FURTHER INCIDENT. REPLACED THE N1 AND N2 INDICATORS. ALSO, REPLACED THE NR 3 N2 TACH GEApr 13, 1996 · N161US · Doug DC1040 · Engine RPM Indicating SystemSDR 9603531161Power Supply · inoperativeDURING LINE CHECK, THE EMERGENCY LIGHT TEST LIGHT WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY AND BATTERY.Feb 10, 1996 · N161US · Doug DC1040 · Emergency LightingSDR 9601141161Controller · failedDURING CRUISE, THE TANK OVER FILLED LIGHT ILLUMINATED AND FUEL WAS STREAMING FROM THE LEFT DUMP NOZZLE. DUMPED 92,500 LBS OF FUEL AND RETURNED TO DTW. REPLACED FUEL CONTROLLER.Jan 19, 1996 · N161US · Doug DC1040 · Aircraft Fuel Distribution SystemSDR 9516921161Slat Sensor · malfunctionedDURING TAKEOFF, THE SLAT DISAGREE LIGHT AND THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE. ADJUSTED SLAT SENSORS AND REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL BOX.Oct 28, 1995 · N161US · Doug DC1040 · Leading Edge Slat Position Indicating SystemSDR 9512641161Floorbeam · crackedDURING T-CHECK, CRACKS WERE FOUND AT THE NUTPLATE HOLES ON THE FS 1887 FLOORBEAM UPPER CHORD FLANGE AT RBL 26. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLES PER EA 11-99176, MFG PART NUMBER AGA 3793-19.Aug 10, 1995 · N161US · Doug DC1040 · Fuselage Main, Floor BeamSDR 9512611161Bulkhead · crackedDURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE BULKHEAD AT FS 515, STR 27R AND LONGERON 27L. REPLACED WEB PER EA 11-98526 AND INSTALLED DOUBLER PER EA 11-98525.Aug 3, 1995 · N161US · Doug DC1040 · Fuselage Main, BulkheadSDR 9512621161Support · crackedDURING T-CHECK, A CRACK WAS FOUND ON THE FLOOR SUPPORT AT FS 495 RBL 24 TO 26. INSTALLED REPAIR STRAP PER EA 11-99021, MFG PART NUMBER 0048-33.Aug 2, 1995 · N161US · Doug DC1040 · Fuselage Miscellaneous StructureSDR 9512631161Spar Cap · crackedDURING INSPECTION OF THE RIGHT HORIZONTAL SPAR CAP, A CRACK WAS FOUND AT THE FORWARD FLANGE AT STA XFS 82. INSTALLED REPAIR PER EM 5511-01014 AND EA 11-99036.Jul 28, 1995 · N161US · Doug DC1040 · Horizontal Stabilizer, Spar/RibSDR 9501121161Evc · malfunctionedDURING TAKEOFF ROLL (AMS), THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. THE TAKEOFF WAS ABORTED. THE ENGINE WAS INSPECTED AND BOROSCOPED. THE EVC WAS REPLACED AND A PRECISION TRIM WAS ACCOMPLISHED. GROUND RUN-UP CONFIRMJan 17, 1995 · N161US · Doug DC1040 · Compressor Bleed Control
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