N21CX, cancelled Apr 1, 2010

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 = 'N21CX' AND deregistration_id = 'N21CX-2010-04-01'
  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 IXXA0200115OBushing · defectiveAFTER TAKEOFF FROM WRI ENROUTE TO BWI LANDING GEAR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. CREW PERFORMED LANDING GEAR UPLATCH CHECK, LIGHT REMAINED ILLUMINATED WITH RUMBILING NOISE NOTED FROM NOSE LANDING GEAR AREA. AIRCRAFT RETURNED TO WRI FOR ANov 19, 2002 · N21CX · Doug DC862 · Landing Gear Retraction/Extension SystemSDR IXXA0200050OO-Ring · damagedAFTER TAKEOFF FROM COF, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC QUANTITY AND THE OIL LOW LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO COF FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND LOCATED A DAAug 19, 2002 · N21CX · Doug DC862 · Hydraulic System, MainSDR IXXA0200020OFan · defectiveENROUTE FROM BWI TO WRI, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE RIGHT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHIMay 19, 2002 · N21CX · Doug DC862 · Air Distribution FanSDR IXXA0100079SFloorbeam · crackedDURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED ON THE FLOORBEAM LEFT HAND FRAME ATTACHMENT PLATES AND CLIPS AT FS 320 TO 480. ACCOMPLISHED REMOVAL OF DAMAGED PLATES AND CLIPS. FABRICATED AND INSTALLED NEW ATTACHMENT PLATES AND CLIPS IN ACCORDANCE WITH Nov 20, 2001 · N21CX · Doug DC862 · Fuselage Main, Floor BeamSDR IXXA0100080SClip · corrodedDURING ROUTINE C-CHECK INSPECTION CORROSION WAS DETECTED IN THE AFT CABIN FLOORBEAM AT STATION 1584. REMOVED DAMAGED FLOORBEAM AND INSTALLED NEW FLOOR SUPPORT AND CLIP NUTS IN ACCORDANCE WITH DOUGLAS STRUCTURAL MAINTENANCE MANUAL.Nov 18, 2001 · N21CX · Doug DC862 · Aircraft StructuresSDR IXXA0100078SWing · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE AT STATION XW485 JUST OUTBOARD OF THE #4 PYLON. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERINov 11, 2001 · N21CX · Doug DC862 · Leading Edge DevicesSDR IXXA0100025Belt · looseEN ROUTE FROM KWA TO HIK, AN ODOR WAS SENSED IN THE COCKPIT EMITTING FROM THE COCKPIT AIR CONDITIONING UNIT. THE FLIGHT CREW SECURED THE AIR CONDITIONER AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE May 23, 2001 · N21CX · Doug DC862 · Cabin Cooling SystemSDR IXXA0100010Hydraulic Line · defectiveDURING CLIMBOUT FROM AVB, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC QUANTITY AND PRESSURE INDICATION SYSTEMS. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO AVB FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATINGMar 21, 2001 · N21CX · Doug DC862 · Hydraulic System, MainSDR IXXA9900011Compressor · defectiveEN ROUTE FROM WRI TO COF, AN ODOR WAS SENSED IN THE COCKPIT ACCOMPANIED BY A LOUD NOISE EMITTING FROM THE NUMBER THREE TURBO COMPRESSOR. THE FLIGHT CREW SECURED THE TURBO COMPRESSOR AND THE ODOR SUBSIDED. MAINTENANCE PLACED THE TURBO COMPRESSOR ON DEFERRAL AJun 21, 1999 · N21CX · Doug DC862 · Cabin Compressor SystemSDR IXXA9900003Fan · failedEN ROUTE FROM AJK TO AVB, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT EMITTING FROM THE LEFT RECIRCULATION FAN. THE CREW TURNED OFF THE FAN AND THE ODOR DIMINISHED. MAINTENANCE INSPECTED AND FOUND THE FAN DEFECTIVE. MAINTENANCE DEFERRED THE LEFT RECIRCULAFeb 16, 1999 · N21CX · Doug DC862 · Air Distribution FanSDR IXXA9800081Wire · looseEN ROUTE, THE FLIGHT CREW DETECTED WHITE SMOKE EMITTING FROM UNDER THE CAPTAIN'S INSTRUMENT PANEL, ACCOMPANIED WITH AN ODOR, THEN DIMINISHED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO KBWI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTEDNov 1, 1998 · N21CX · Doug DC862 · Altimeter, Barometric/EncoderSDR IXXA9800103Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEEN STATIONS XE 221 AND XE 272. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAug 4, 1998 · N21CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA9800101Panel · corrodedDURING ROUTINE C CHECK INSPECTION, A CORROSION BULGE WAS DETECTED ON THE RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEEN STATION XE 77 AND XE 148. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDJul 17, 1998 · N21CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA9800100Bulkhead Doubler · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED IN THE LOWER RADOME COMPARTMENT BULKHEAD INNER DOUBLER AT FUSELAGE STATION 44. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW DOUBLER AND TWO REPAIR SPLICE DOUBLERS INJul 17, 1998 · N21CX · Doug DC862 · Fuselage Main, BulkheadSDR IXXA9800098Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEEN STATIONS XE 272 AND XE 275. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH Jul 17, 1998 · N21CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA9800097Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEEN STATIONS XE 149 AND XE 221. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH Jul 17, 1998 · N21CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA9800102Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT HORIZONTAL STABILIZER LOWER TRAILING EDGE PANEL BETWEEN STATIONS XE 221 AND XE 272. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FJul 16, 1998 · N21CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA9800099Plating · corrodedDURING ROUTINE C CHECK INSPECTION, A CORROSION BULGE WAS DETECTED ON LOWER FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 1500 BETWEEN LONGERON 31 LEFT AND 31 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND AN Jul 15, 1998 · N21CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA9800104Panel · damagedDURING ROUTINE C CHECK INSPECTION, RIGHT WING LOWER LEADING EDGE ACCESS PANEL WAS DAMAGED AT STATION XW 408. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER, DOUBLER AND AN L ANGLE IN ACCORDANCE WITH FAA DER APPROVJul 14, 1998 · N21CX · Doug DC862 · Wing, Plate/SkinSDR IXXA9800096Plating · corrodedDURING ROUTINE C CHECK INSPECTION, A CORROSION BULGE AND POPPED RIVET HEADS WERE DETECTED ON THE RIGHT AILERON LOWER PLATING BETWEEN STATIONS XA 605 AND XA 622. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING, FABRICATION AND INSTALLATION OF A NEW LOWER PLATINJul 14, 1998 · N21CX · Doug DC862 · AileronsSDR IXXA9700167Control Box · defectiveDURING LANDING ROLL, ALL HYDRAULIC BRAKING ACTION WAS LOST. THE CREW INITIATED THE EMERGENCY BRAKING SYSTEM AND MAXIMUM REVERSE THRUST TO DECELERATE THE AIRCRAFT. MAINTENANCE INSPECTED THE AIRCRAFT ANTI-SKID SYSTEM AND REPLACED THE ANTI-SKID CONTROL BOX. ANNov 14, 1997 · N21CX · Doug DC862 · Brake Anti-Skid SectionSDR IXXA9700162Control Box · defectiveDURING LANDING ROLL AT WRI, ALL HYDRAULIC BRAKING ACTION WAS LOST. THE CREW INITIATED THE EMERGENCY AIR BRAKE SYSTEM TO DECELERATE THE AIRCRAFT. NORMAL BRAKING WAS RESTORED AFTER THE CREW DISARMED THE ANTI-SKID SYSTEM. MAINTENANCE INSPECTED THE AIRCRAFT ANDNov 9, 1997 · N21CX · Doug DC862 · Brake Anti-Skid SectionSDR IXXA9700160Battery Pack · dischargedAFTER ARRIVING AND ENGINE SHUTDOWN WITH NO EXTERNAL ELECTRICAL POWER, THE COCKPIT AND PASSENGER COMPARTMENT DOOR OVERHEAD EMERGENCY LIGHTING FAILED TO ILLUMINATE. MAINTENANCE INSPECTED THE EMERGENCY LIGHTING SYSTEM AND FOUND TWO BATTERY PACKS DEFECTIVE, WHICNov 1, 1997 · N21CX · Doug DC862 · Emergency LightingSDR IXXA9700007Floorbeam · crackedDURING ROUTINE C-CHECK INSPECTION, FLOORBEAM BETWEEN FUSELAGE STATION 226 AND 270 WAS FOUND TO BE CRACKED. REPAIR OF THE FLOORBEAM WAS ACCOMPLISHED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITH FAA DER APPROVED SKETCH B68-R29 AND THE DOUGLNov 22, 1996 · N21CX · Doug DC862 · Fuselage Main, Floor BeamSDR IXXA9700010Gusset · corrodedDURING ROUTINE C-CHECK INSPECTION, A CORRODED GUSSET AT FUSELAGE STATION 128 AND LONGERON 22 LEFT WAS FOUND. THE GUSSET WAS REMOVED, FABRICATED AND INSTALLED IN ACCORDNACE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 53-1-0, AND FAA DER APPROVED SKETCH B68-R16.Nov 18, 1996 · N21CX · Doug DC862 · Fuselage Miscellaneous StructureSDR IXXA9700009Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR ATTACH FITTING WAS FOUND TO BE CRACKED. THE ATTACH FITTING WAS REPLACED IN ACCORDANCE WITH THE DOUGLAS REPLACEMENT GUIDE AND SRM 51-1-21.Nov 10, 1996 · N21CX · Doug DC862 · Wing, Landing Gear Attach FittingsSDR IXXA9700008Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR ATTACH FITTING WAS FOUND TO BE CRACKED. THE ATTACH FITTING WAS REPLACED IN ACCORDANCE WITH THE DOUGLAS REPLACEMENT GUIDE AND SRM 51-1-21.Nov 10, 1996 · N21CX · Doug DC862 · Wing, Landing Gear Attach FittingsSDR IXXA9700006Longeron · crackedDURING ROUTINE C-CHECK INSPECTION, LONGERON 24 RIGHT WAS FOUND TO BE CRACKED IN TWO PLACES ADJACENT TO THE BATHTUB FITTING AT FUSELAGE STATION 870. THE CRACKS WERE STOP DRILLED, REPAIR DOUBLERS FABRICATED AND INSTALLED IN ACCORDANCE WITH DOUGLAS STRUCTURAL RENov 10, 1996 · N21CX · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA9636Prox Switch · dirtyON TAKEOFF OUT OF BGTL, THE MLG 'NOT LATCHED' LIGHT CAME ON AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, WITH NO CHANGE IN THE INDICATION. THE UPLATCH CHECK WAS NORMAL. AT KWRI, MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE PROBLEM TO BE CAUSED BY DIMar 12, 1996 · N21CX · Doug DC862 · Entrance StairsSDR IXXA9606Air Distr · odorEN ROUTE BETWEEN LPLA AND KWRT, THE AIR CONDITIONING SYSTEM INTERMITTENTLY PRODUCED THE STRONG SMELL OF OIL IN THE COCKPIT. THE FLIGHT CREW SUSPECTED A TURBOCOMPRESSOR OIL SEAL FAILURE. INSPECTION ON THE GROUND IN KWRT SHOWED THE TC'S TO BE NORMAL, WITH NO LJan 31, 1996 · N21CX · Doug DC862 · Air Distribution SystemSDR IXXA199577Fan · failedDURING FLIGHT BETWEEN PJON AND PHNL, THE LEFT RECIRCULATION FAN PRODUCED FUMES WHICH WERE THEN CIRCULATED INTO THE AIRCRAFT. THE RECIRCULATION FAN WAS DEFERRED AND SCHEDULED FOR REPLACEMENT. (M)Sep 15, 1995 · N21CX · Doug DC862 · Air Distribution FanSDR IXXA199565Fire Detector · malfunctionedKWRI - ON DEPARTURE OUT OF KWRI, A NR 3 ENGINE FIRE WARNING WAS EXPERIENCED. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO KWRI FOR MAINTENANCE. WINDMILLING OIL PRESSURE WAS 30 PSI. INSPECTION AT KWRI REVEALED AN INTERMITTENTLY BAD Jun 30, 1995 · N21CX · Doug DC862 · Fire DetectionSDR IXXA199563Duct Clamp · failedLPLA/KWRI - IN CRUISE BETWEEN LPLA AND KWRI, A NR 3 ENGINE FIRE WARNING WAS EXPERIENCED WITH NORMAL ENGINE PARAMETERS OBSERVED. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE FIRE BOTTLES DISCHARGED. THE FIRE WARNING EXTINGUISHED AND THE ENGINE MAINTAINEDJun 29, 1995 · N21CX · Doug DC862 · Pneumatic Distribution System
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