N918RW, cancelled Oct 24, 2007

Service difficulty reports · 39

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 = 'N918RW' AND deregistration_id = 'N918RW-2007-10-24'
  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 NWAA072449953Unknown · unknownCABIN CREW REPORTED A PRESSURE LEAK TYPE SQUEAL COMING FROM THE AFT EMERGENCY ESCAPE HATCH. WHEN FLIGHT CREW REDUCED THRUST THE CABIN ALTITUDE CLIMBED UNCONTROLLABLY. THE PILOT PERFORMED A RAPID DESCENT TO A LOWER ALTITUDE AND CONTINUED TO SCHEDULED DESTINATJul 10, 2007 · N918RW · Doug DC931 · Cabin Pressure Control SystemSDR 0700219953Compressor · stalledDURING TAKEOFF ROLL, AT APPROXIMATELY 100KTS, NR 1 ENGINE COMPRESSOR STALLED. TAKEOFF WAS ABORTED AND THE AIRCRAFT SKIDDED OFF THE RUNWAY. THE AIRCRAFT IS BEING REPAIRED AND THE NR 1 ENGINE IS BEING REPLACED.Jan 21, 2007 · N918RW · Doug DC931 · Turbine Engine Compressor SectionSDR 0401909953Stiffener · crackedDURING H-CHECK, FOUND CRACKS IN VERTICAL STIFFENERS AT BS 756 L28R, L28L AND ABOVE L26L. REPAIRED PER EA 99-200337.Sep 22, 2004 · N918RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 0401189953Controller · intermittentFLIGHT CREW WAS NOT ABLE TO CONTROL THE PRESSURIZATION WITH AUTOMATIC CONTROL AFTER TAKEOFF, UTILIZED MANUAL CONTROL. MANUAL CONTROL FAILED AND THE OUTFLOW VALVE WENT FULL OPEN AT FL230. EMERGENCY DESCENT TO 10,000 FT AND THEN NORMAL DESCENT TO 6,000 FT. CAJul 15, 2004 · N918RW · Doug DC931 · Cabin Pressure ControllerSDR 0300509953Skin · corrodedDuring "L" check found cracks in fuselage nose skin BS 69.5 fastener holes. Repaired per EA 99-190934.Mar 7, 2003 · N918RW · Doug DC931 · Fuselage Main, Plate/SkinSDR 9810469953Angle · crackedDURING M-CHECK, FOUND CRACK AT FORWARD ENTRY DOOR JAMB LOWER DEPRESSOR ANGLES FS 180. REPAIRED PER EA 99-160834 (P/N 5957094-1).Nov 6, 1998 · N918RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9808119953Batteries · dischargedDURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS BETWEEN ROWS 9 THRU 11 AND AT LEFT FORWARD OVERWING EMERGENCY EXIT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.May 1, 1998 · N918RW · Doug DC931 · Emergency LightingSDR 9808109953Power Supply · inoperativeFLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS BETWEEN ROWS 8 THRU 10 WOULD NOT EXTINGUISH WITH SWITCH IN OFF POSITION. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.May 1, 1998 · N918RW · Doug DC931 · Emergency LightingSDR 9805169953Battery Pack · dischargedFLIGHT ATTENDANT REPORTED FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Mar 25, 1998 · N918RW · Doug DC931 · Emergency LightingSDR 9805129953Computer · failedSTALL WARNING INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 STALL WARNING COMPUTER AND TRANSDUCER, OPERATIONAL CHECK NORMAL.Mar 25, 1998 · N918RW · Doug DC931 · Stall Warning SystemSDR 9723399953Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT FORWARD EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Dec 15, 1997 · N918RW · Doug DC931 · Emergency LightingSDR 9723349953Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT AFT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Dec 15, 1997 · N918RW · Doug DC931 · Emergency LightingSDR 9713899953Temp Sensor · failedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TEMPERATURE SENSOR, OPERATIONAL CHECK NORMAL.Jul 16, 1997 · N918RW · Doug DC931 · Overheat DetectionSDR 9713569953Slide · failed testDURING PERIODIC CHECK, MAIN CABIN DOOR EMERGENCY EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE.Jul 10, 1997 · N918RW · Doug DC931 · Escape SlideSDR 9624339953Strap · crackedDURING LINE CHECK, FOUND A BROKEN NR 2 PYLON UPPER AFT ENGINE MOUNT STRAP. ALSO, FOUND CRACKS IN THE PYLON WEB LOWER CHANNEL 10 OUTBOARD FROM THE FUSELAGE AT THE LOWER ENGINE MOUNT STRAP AND IN THE UPPER INBOARD PYLON TO FUSELAGE ATTACH ANGLE 15 FORWARD OF THNov 12, 1996 · N918RW · Doug DC931 · Nacelle/Pylon StructureSDR 9618579953Generator · failedRIGHT ENGINE GENERATOR TRIPPED OFF LINE AFTER TAKEOFF. RIGHT GEN OFF LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT GENERATOR, OPERATIONAL CHECK NORMAL.Aug 26, 1996 · N918RW · Doug DC931 · AC Generator-AlternatorSDR 9613619953Fitting · corrodedDURING LINE CHECK, FOUND CORROSION ON THE LONGERON 23L END FITTING AT FS 980 TO 995. REPLACED FITTING PER SRM 51-30-2, 51-30-5.Jun 16, 1996 · N918RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9604289953Batteries · dischargedDURING PREFLIGHT CHECK, FOUND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK NORMAL.Feb 22, 1996 · N918RW · Doug DC931 · Emergency LightingSDR 9602109953O-Ring · splitDURING CLIMB AFTER CENTER TANK WAS EMPTY, THE RIGHT FUEL PRESSURE LOW LIGHT ILLUMINATED. RIGHT FUEL INDICATION DID NOT DECREASE AND THE LEFT FUEL INDICATION WAS DECREASING AT THE RATE OF EQUAL TO BOTH ENGINE BURNS. ACCOMPLISHED COCKPIT OPERATING MANUAL PROCEJan 28, 1996 · N918RW · Doug DC931 · Fuel Boost PumpSDR 9520359953Pt2 Probe · malfunctionedNR 1 ENGINE EPR INDICATION LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CLEANED THE PT2 LINE, LEAK CHECKED THE PT2 SYSTEM AND REPLACED THE NOSE DOME/PT2 PROBE ASSEMBLY. SUBSEQUENT RUNUP WAS SATISFACTORY.Dec 8, 1995 · N918RW · Doug DC931 · Fuel Controlling SystemSDR 9520349953Epr Indicator · failedNR 1 EPR INDICATION LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR AND PERFORMED A TAKEOFF POWER ASSURANCE RUN. THE NR 1 EPR SYSTEM OPERATION WAS NORMAL ON RUNUP.Dec 8, 1995 · N918RW · Doug DC931 · Engine Pressure Ratio (EPR)SDR 9520269953Compressor · stalledONE OR BOTH ENGINES EXPERIENCED A COMPRESSOR STALL ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED BOTH ENGINES. THE NR 1 ENGINE WAS REPLACED WITH A SERVICEABLE UNIT. SNOW AND SLUSH INGESTION IS SUSPECTED ASDec 6, 1995 · N918RW · Doug DC931 · Turbine Engine Compressor SectionSDR 9514359953Fuel Press Sw · failedWHEN TAKEOFF POWER WAS APPLIED, THE NR 2 ENGINE INLET FUEL PRESSURE LOW WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE SYSTEM WAS PLACED ON MEL AND AIRCRAFT CONTINUED IN SERVICE. SUBSEQUENT REPLACEMENT OF THE LSep 14, 1995 · N918RW · Doug DC931 · Fuel Pressure IndicatingSDR 9514689953Longeron · crackedDURING H-CHECK, FOUND A ONE INCH CRACK IN LONGERON 17R, FS 945 BOTH FRAME ATTACH POINTS. REPAIRED LONGERON (P/N 5911427-9), PER EA 99-100870.Sep 13, 1995 · N918RW · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9514269953Release Syst · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. ADJUSTED THE CLIPS AND RELEASE, SYSTEM CHECKED OK.Sep 11, 1995 · N918RW · Doug DC931 · Aerodynamic FairingsSDR 9513999953Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 758 TO 760. REPLACED END FITTING PER SRM 53-02 FIG 12.Sep 6, 1995 · N918RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9515499953Skin · corrodedDURING H-CHECK, FOUND CORROSION IN THE INNER SKIN AT FS 639, LONGERON 18L. REPAIRED PER EA 99-10973.Sep 5, 1995 · N918RW · Doug DC931 · Fuselage Main, Plate/SkinSDR 9514589953Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON LONGERON 30 AT THE FS 570 SPLICE. REPAIRED SPLICE (P/N 5920319-504), PER EA 99-97125.Aug 31, 1995 · N918RW · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9513709953Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR FRAME AND FITTING LOCATED IN THE UPPER FORWARD ACCESS NR 1. REPLACED THE FITTING.Aug 31, 1995 · N918RW · Doug DC931 · Cargo/Baggage DoorsSDR 9513499953Hinge · corrodedDURING H-CHECK, FOUND CORROSION IN THE NR 3 FORWARD FLAP HINGE STUD HOLES. REPLACED HINGE PER CITEXT 09-5740-1-9800.Aug 28, 1995 · N918RW · Doug DC931 · Trailing Edge FlapsSDR 9513289953Fittings · corrodedDURING H-CHECK, FOUND CORROSION ON FRAME FITTINGS FORWARD AND AFT OF THE GALLEY SERVICE DOOR FS 168 AND FS 200. REPLACED FITTINGS PER SRM 51-10-04.Aug 26, 1995 · N918RW · Doug DC931 · Fuselage Miscellaneous StructureSDR 9510819953Connector · malfunctionedCLIMBING OUT OF MSP, THE NR 1 OIL TEMPERATURE INDICATED 170 DEGREES, THEN BEGAN FLUCTUATING BETWEEN 100 TO 170 DEGREES. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE CANNON PLUG ON THE OIL TEMPERATURE SENSOR, SYSTEM CHECK OK. Jul 13, 1995 · N918RW · Doug DC931 · Engine Oil TemperatureSDR 9510799953Temp Sensor · malfunctionedCLIMBOUT OF MSP, THE NR 1 ENGINE OIL TEMPERATURE WAS FLUCTUATING AND SEEMED TO STABILIZE AT 170 DEGREES. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TEMPERATURE SENSOR, SYSTEM OPERATION APPEARED TO BE NORMAL. AIRCRAFT RJul 13, 1995 · N918RW · Doug DC931 · Engine Oil TemperatureSDR 9510059953Indication · malfunctionedSLAT EXTEND, BLUE LIGHT DID NOT ILLUMINATE WITH FLAPS EXTENDED TO 15 DEGREES FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. PULLED AND RESET SLAT EXTEND SWITCH CIRCUIT BREAKERS, CYCLED SLATS SEVERAL TIMES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERJun 15, 1995 · N918RW · Doug DC931 · Leading Edge Slat Position Indicating SystemSDR 9509449953Pressurization · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED CHECK OF AUTO AND MANUAL PRESSURIZATION SYSTEM. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE.Jun 13, 1995 · N918RW · Doug DC931 · Cabin Pressure Control SystemSDR 9503769953Vert Gyro · malfunctionedCAPTAIN'S ATTITUDE INDICATOR GYRO FLAG APPEARED DURING CLIMB-OUT. PITCH WENT TO 15 DEGREES AND LOCKED. FLIGHT RETURNED TO GTF AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S VERTICAL GYRO AND ADI. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Mar 9, 1995 · N918RW · Doug DC931 · Attitude Gyro and Indicating SystemSDR 9502819953Fuel Tank · ventingFUEL BEGAN VENTING FROM THE RIGHT MAIN TANK EN ROUTE MSP-HPN. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. PERFORMED BACKFLUSH PROCEDURE PER MM 28-20-0. AIRCRAFT RETURNED TO SERVICE.Feb 16, 1995 · N918RW · Doug DC931 · Fuel StorageSDR 9502799953Fuel Sys · ventingFUEL BEGAN LEAKING FROM LEFT WING ENROUTE HPN-MSP. FUEL WAS VENTING FROM THE RIGHT TANK AT A RATE OF 800 POUNDS PER HOUR. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED FUEL TANK BACKFLUSH PROCEDURE PER MAINTENANCE MANUAL. NO TRANSFER PROBFeb 15, 1995 · N918RW · Doug DC931 · Fuel StorageSDR 9501799953Wing · fuel leakFUEL BEGAN LEAKING FROM LEFT WING EN ROUTE HPN-MSP. FUEL WAS VENTING FROM RIGHT TANK AT A RATE OF 800 LBS PER HOUR. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED FUEL TANK BACKFLUSH PROCEDURE PER MAINTENANCE MANUAL. NO TRANSFER PROBLEMS WEFeb 15, 1995 · N918RW · Doug DC931 · Aircraft Fuel Distribution System
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