N867BX, cancelled Dec 20, 2005
Service difficulty reports · 51
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 = 'N867BX' AND deregistration_id = 'N867BX-2005-12-20' 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.
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 = 'N867BX' AND deregistration_id = 'N867BX-2005-12-20' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA0300011OEngine · wornAFTER DEPARTURE FROM KBFI ENROUTE TO KPDX CREW NOTICED OIL QUANTITY IN NUMBER 2 ENGINE DROPPED ABNORMALLY. AS A PRECAUTIONARY MEASURE THE #2 ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO KBFI FOR AN UNEVENTFUL LANDING. POSITIVE OIL PRESSURE WAS MAINTAINED THRU SDR IXXA0300006OMechanism · out of adjustAFTER TAKEOFF GEAR DOORS NOT LATCHED LIGHT ILLUM, AFTER GEAR RETRACTION. CREW PERFORMED UPLATCH CHECK DOORS NOT LATCHED CONTINUED TO BE ILLUM. CREW PERFORMED GEAR CYCLE, DOORS NOT LATCHED LIGHT CONTINUED TO REMAIN ILLUM. CREW NOTED NO BUFFET, YAW OR ABNORMASDR IXXA0300003OUplock · lack of lubeAFTER DEPARTURE FROM FWA DURING GEAR RETRACTION DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR AND LIGHT REMAINED ILLUMINATED, APPROX 3 MINUTES LATER LIGHT EXTINGUISHED. CREW PROCEEDED TO LAX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED SDR IXXA0200009OConnector · contaminatedAFTER TAKEOFF FROM PDX, THE TAKEOFF WARNING HORN SOUNDED WHEN THE LANDING GEAR AND FLAPS WERE RETRACTED AND COULD NOT BE SILENCED. THE FLIGHT RETURNED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE FLAP LIMIT SWITCH CSDR IXXA0200008OStriker · wornENROUTE FROM BFI TO PDX, THE LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECSDR IXXA0200007OWarning Light · illuminatedENROUTE FROM TOL TO LAX, AFTER THE LANDING GEAR WAS RETRACTED THE DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR, PERFORMED A SUCCESSFUL GEAR UP LATCH CHECK, BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TSDR IXXA0000042Control Valve · defectiveENROUTE FROM TOL TO DFW, THE GEAR DOOR NOT LATCH LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR, BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED AN OPSDR IXXA0000035Harness · misriggedENROUTE FROM DFW TO TOL, THE GEAR DOOR NOT LATCH WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED A GEAR SWINSDR IXXA0000034Uplock Target · looseEN ROUTE FROM TOL TO DFW, AFTER GEAR RETRACTION THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR, THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO DFW FOLLOWING COMPANY PROCEDURES FOR AN UNEVENFUL LANSDR IXXA0000033Rod · out of adjEN ROUTE FROM TOL TO DFW, THE LANDING GEAR DOOR NOT LATCH LIGHT ILLUMINATED AFTER THE LANDING GEAR WAS RETRACTED. THE FLIGHT CREW CYCLED THE LANDING GEAR AND PERFORMED AN UNSUCCESSFUL UPLATCH CHECK. THE LANDING GEAR HANDLE WAS PLACED IN THE UP POSITION AND TSDR IXXA0000027Wire · brokenDURING DESCENT INTO TOL, WHEN THE LANDING GEAR WAS EXTENDED FOR LANDING THE NOSE LANDING GEAR DOWN AND LOCKED INDICATION LIGHT FAILED TO ILLUMINATE. THE FLIGHT CREW CYCLED THE GEAR. THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CREW FOLLOWED COMPANY PSDR IXXA9900013Indication · malfunctionedEN ROUTE FROM IAH TO TOL, THE MAIN LANDING GEAR NOT LATCHED LIGHT ILLUMINATED DURING THE UPLATCH CHECK, THE MAIN GEAR DOOR NOT LATCHED LIGHT REMAINED EXTINGUISHED. THE FLIGHT CREW CYCLED THE LANDING GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLSDR IXXA9800069Retract Mech · out of adjustAFTER TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A NOISE AND VIBRATION COMING FROM THE NOSE WHEEL WELL AREA. THE CREW CYCLED THE GEAR BUT THE VIBRATION CONDITION WAS STILL PRESENT. THE AIRCRAFT RETURNED TO TOL FOR AN UNEVENTFUL LANDSDR IXXA9800065Mechanism · misriggedAFTER TAKEOFF, WHEN THE FLIGHT CREW RETRACTED THE LANDING GEAR, THE CONTROL HANDLE WOULD NOT POSITION TO THE UP POSITION. THE CREW RETURNED THE GEAR HANDLE TO THE DOWN POSITION, RECEIVING THREE DOWN AND LOCK INDICATIONS. A SECOND ATTEMPT TO RETRACT THE GEAR SDR IXXA9800095Bulkhead Fitting · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON AFT PRESSURE BULKHEAD LOWER SUPPORT FITTING AT FUSELAGE STATION 1744, LONGERON 36. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLASSDR 98ZZZX2958Spar Cap · crackedFOUND LT WING INBD LOWER AUXILIARY SPAR CAP CRACKED ON VERTICAL FLANGE AT XRS22. SUSPECT CAUSE OF THE CRACK WAS VIBRATION.SDR 98ZZZX2957Plank · crackedPYLON PLANK HAS CRACK LOCATED AT 19.5 INCHES AFT FROM YN190. SUSPECT CAUSE OF THE CRACK WAS VIBRATION.SDR 98ZZZX2956Plank · crackedPYLON PLANK CRACK LOCATED AT YN226. SUSPECT CAUSE OF THE CRACK IS VIBRATION.SDR IXXA9800094Plating · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER FUSELAGE EXTERNAL PLATING FROM FUSELAGE STATIONS 1752 AND 1766, BETWEEN LONGERONS 35 LEFT AND 35 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL IN ACCORDANCE WITH DOUGLAS FAX ACTION NUMBER 37266SDR IXXA9800090Angle · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED BETWEEN FUSELAGE STATION 380 AND 400, LONGERON 27 LEFT. REPAIR ACCOMPLISHED REMOVAL OF CORRODED ANGLE, FABRICATION AND INSTALLATION A NEW LONGERON ANGLE IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-SDR IXXA9800071Frame · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE FRAME AT FUSELAGE STATION 70, BETWEEN LONGERON 32 AND 34 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION AN INTERNAL REPAIR ANGLE IN ACCORDANCE WITH THE DOUGLSDR IXXA9800092Doubler · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON CENTER WING UPPER JOINT DOUBLER AT FUSELAGE STATION 816, STRINGER 6. REPAIR ACCOMPLISHED BLENDED OUT CORROSION IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS, COO-SJO-98-0393DDAC, COO-SJO-98-0394DAC, SDR IXXA9800088Fitting · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON A FUSELAGE FITTING BETWEEN FUSELAGE STATION 70 AND 80, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING. FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLAS DRAWISDR IXXA9800091Plating · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RUDDER RIGHT SIDE EXTERNAL PLATING AND STATION ZR208.625. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWISDR IXXA9800087Plank · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER FOUR PYLON INTERMEDIATE OUTBOARD PLANK AT STATION YIP 241. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION OF AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH DSDR IXXA9800075Plating · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING LOWER LEADING EDGE AT STATION XFS 304. REPAIR ACCOMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-8-57SDR IXXA9800085Longeron · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED BETWEEN FUSELAGE STATION 180 AND 220, LONGERON 31 LEFT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION A NEW LONGERON SPLICE FITTING IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS COSDR IXXA9800084Plank · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER TWO PYLON OUTBOARD INTERMEDIATE PLANK PANEL AT STATION YN 190. REPAIR ACCOMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH FAASDR IXXA9800083Plank · wornDURING ROUTINE C CHECK INSPECTION, WEAR WAS DETECTED ON THE NUMBER FOUR PYLON UPPER INBOARD PLANK SIX INCHES FORWARD OF STATION YUS 297. REPAIR ACCOMPLISHED BLENDING, POLISH THE AFFECTED AREA IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-SJO-98-0351, FAX ACSDR IXXA9800093Jamb · crackedDURING ROUTINE C CHECK INSPECTION, A CRACKED FITTING WAS DETECTED AT UPPER TORQUE BOX FORWARD DOOR JAMB, AFT CARGO COMPARTMENT AT FUSELAGE STATION 1177 - X 68. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCORSDR IXXA9800089Plating · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED AT AFT ACCESSORY COMPARTMENT INTERNAL DOUBLER AT FUSELAGE STATION 1620, BETWEEN LONGERONS 24 AND 27 LEFT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION REPAIR FILLERS, REPAIR DOUBSDR IXXA9800086Doubler · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER FUSELAGE, EIGHT EACH EXTERNAL FINGER DOUBLERS BETWEEN FUSELAGE STATIONS 1352 AND 1586.5. REPAIR ACCOMPLISHED TRIMMING OFF THE CORRODED FINGERS OF THE AFFECTED DOUBLERS IN ACCORDANCE WITH DOUGLSDR IXXA9800072Plating · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 1610 AND 1700, LONGERONS 31 LEFT AND 31 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION A NEW SECTION OF PLATINSDR IXXA9800074Floor · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON MAIN CABIN FLOOR PRESSURE PANEL BETWEEN FUSELAGE STATION 863 AND 878, BL +X4 TO -X5.50. REPAIR ACCOMPLISHED CORROSION BLEND OUT, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH FSDR IXXA9800073Plating · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 301.5 AND 324, LONGERONS 33 AND 34 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION TWO INTERNAL FILLERS AND AN EXTSDR IXXA980002Fire Warning · malfunctionedEN ROUTE, THE NUMBER FOUR ENGINE FIRE WARNING INTERMITTENTLY SOUNDED IN LIGHT TURBULENCE. THE FLIGHT CONTINUED TO TOL FOR AND UNEVENTFULL LANDING. MAINTENANCE INSPECTED THE ENGINE AND THE ASSOCIATED WIRING, WITH NO DISCREPANCIES NOTED. MAINTENANCE ACCOMPLISSDR IXXA9700146Clamp · looseEN ROUTE TOL TO BFI, THE NR 4 ENGINE FIRE WARNING SOUNDED WITH NUMBER 4 HIGH STAGE BLEED VALVE SELECTED TO HIGH. NR 4 BLEED VALVE WAS SELECTED TO LOW AND FIRE WARNING EXTINGUSHED. FLIGHT CONTINUED TO BFI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE SDR IXXA9700144Wire · defectiveDURING APPROACH, THE NUMBER FOUR ENGINE FIRE WARNING SOUNDED. THE CREW SECURED THE ENGINE, FIRE WARNING EXTINGUISHED. MAINTENANCE INSPECTED THE ENGINE, NO EVIDENCE OF A FIRE WAS NOTED. MAINTENANCE PERFORMED AN INTENSIFIED INSPECTION OF THE WARNING SYSTEM WIRSDR IXXA9700143Fire Warning · malfunctionedENROUTE, THE NUMBER FOUR ENGINE FIRE WARNING SOUNDED AND AN ENGINE SHUTDOWN WAS ACCOMPLISHED FOLLOWING COMPANY PROCEDURES. THE FIRE WARNING EXTINGUISHED SHORTLY AFTER THE SHUTDOWN. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO EVIDENCE OF A FIRE. THE ENGISDR IXXA9700107Ballast · burntAFTER TAKEOFF TOL, SMOKE EMANATED FROM FLIGHT ENGINEER'S PANEL IN THE VICINITY OF THE CABIN PRESSURE CONTROLLER AND THE HYDRAULIC SELECTOR CONSOLE. FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND THAT THE F/E'S INSTRUMENT WHITE LIGHTING BSDR IXXA9700085Electrical Syst · odorEN ROUTE, CREW NOTICED HOT ELECTRICAL SMELL IN COCKPIT BELOW THE CIRCUIT BREAKER PANEL. SMELL DISSIPATED AFTER ABOUT 1 MINUTE. FOLLOWING AN UNEVENTFUL LANDING IN TOL, MAINTENANCE INVESTIGATED THE ORIGIN OF THE SMELL. NO CAUSE WAS FOUND AFTER A COMPLETE ENGISDR IXXA9700005Uplatch Switch · unsecureON CLIMBOUT, GEAR DOORS NOT LATCHED LIGHT WOULD NOT EXTINGUISH ON GEAR RETRACTION. LANDING GEAR WAS CYCLED AND THE DOORS LIGHT EXTINGUSHED. AFTER LANDING TOL, MAINTENANCE FOUND AND SECURED THE RIGHT HAND MAIN LANDING GEAR DOOR UPLATCH SWITCH. MAINTENANCE ACSDR IXXA9700004Wire · brokenAFTER TAKEOFF, GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. FLIGHT CREW CYCLED GEAR, LIGHT EXTINGUSHED, GEAR UPLATCH CHECK WAS NORMAL. THE FLIGHT CONTINUED TO TOL WITH AN UNEVENTFUL LANDING. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT THE LEFT MAIN LSDR IXXA96130Structure · vibrationDURING APPROACH TO CLT, AIRCRAFT EXPERIENCED A SIGNIFICANT VIBRATION WITH FLAP 23 SELECTED. MAINTENANCE INSPECTED THE AIRCRAFT FLIGHT CONTROL SYSTEMS, LANDING GEAR SYSTEMS, WINGS, AND FUSELAGE WITH NO CAUSE FOUND. A SUBSEQUENT TEST FLIGHT WAS ACCOMPLOSHED WISDR IXXA96121Linkage · brokenEN ROUTE BETWEEN ATL AND TOL, CREW NOTED SPOILER UNLOCK INDICATION LIGHT ILLUMINATED WITH STANDBY SPOILER PUMP OFF. FLIGHT CONTINUED WITH AN UNEVENTFUL LANDING AT TOL. MAINTENANCE FOUND AND REPLACED A BROKEN LEFT INBOARD SPOILER CRANK/LINKAGE IAW THE DOUGLASSDR CKSA6004Fire Loop · brokenKTOL - FLT 71266 - NR 4 ENGINE FIRE WARNING CAME ON IN-FLIGHT DURING DESCENT. PERFORMED IN-FLIGHT SHUT DOWN AND DISCHARGED FIRE BOTTLE. LANDED WITHOUT INCIDENT. FOUND NR 4 ENGINE BOTTOM FIRE LOOP BROKEN. REPLACED LOWER FIRE LOOP. GROUND OPS CHECK GOOD IAWSDR CKSA95167Ballast · failedKTOL-KPHL - ELECTRICAL SMELL IN FRONT RIGHT SIDE OF COCKPIT. SUBMITTER STATES, SUSPECT RIGHT GLARESHIELD LIGHT, PULLED BREAKER. NO MORE SMELL, DEFERRED PER MEL 33-1 CAT C DMI NR 654. REPLACED LIGHT BALLAST TRANSFORMER ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MMSDR CKSA95062Fitting · corrodedKYIP - DURING B-CHECK INSPECTION, FOUND LONGERON 30L AT FS 1660, CORRODED. REPAIRED PER DC-8 SRM 53-2-2. REPLACED LONGERON END FITTING, STA 1660 LONGERON 30L. (X)SDR CKSA95061Skin · corrodedKYIP - DURING B-CHECK INSPECTION, FOUND FUSELAGE SKIN BULGING FROM CORROSION AT STATION 1660, LONGERON 30L. REPAIRED FUSELAGE SKIN AT STATION 1660, LONGERON 30L IAW EA NR 95-178. (M)SDR CKSA95018Wire · bareKTOL - ON SHORT FINAL NR 1 ENGINE FIRE WARNING CAME ON MOMENTARILY. REPAIRED BARE WIRE NEAR FIRE LOOP PLUG, CHECKS OK IAW MM CHAPTER 26. (W)
Back to N867BX, cancelled Dec 20, 2005