N728PL, cancelled Jan 7, 2014
Service difficulty reports · 107
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 = 'N728PL' AND deregistration_id = 'N728PL-2014-01-07' 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 = 'N728PL' AND deregistration_id = 'N728PL-2014-01-07' 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 IXXA0300086ODownlock Switch · brokenWHEN GEAR WAS EXTENED THE LT GEAR LIGHT DID NOT ILLUMINATE. AFTER CYCLING GEAR ALL THREE GEAR LIGHTS WERE NORMAL. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR DOWN LOCK INDICATION SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.SDR IXXA0300070OBearing · lack of lubeDURING CLIMB FROM FJDG CREW LOST CABIN PRESSURIZATION. CREW RETURNED TO FJDG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED OUTFLOW VALVE. THEY LUBED MECHANICAL ARMS AND BEARINGS. OPERATIONAL CHECK GOOD BOTH IN AUTO AND MANUAL PER ALL APPLICABLE MANUALS. TSDR IXXA0300061OUplock Sensor · contaminatedON APPROACH, WITH ALL 3 MLG'S DOWN AND LOCKED, BOTH (DOOR NOT LATCHED, GEAR NOT LATCHED) LIGHTS WERE ILLUMIN, ALSO AUDIBLE WARNING HORN. GEAR WAS RECYCLED TWICE, THIS CORRECTED PROBLEM. MAINT INSPECTED LANDING GEAR, GEAR DOOR WARNING SYS. NO DEFECTS WERE NOTEDSDR IXXA0300059OValve · malfunctionedDURING CLIMB NR 4 ENG QTY DROPPED & OIL PRESS ROSE TO 60 PSI, TEMP INCREASED. POWER WAS REDUCED PARAMETERS REDUCED OIL PRESS, OIL TEMP REDUCED 20 DEGREES & OIL QTY INCREASED. OIL PRESS LIGHT NEVER ILLUM & OIL PRESS NEVER DROPPED BELOW 40 PSI. MX REMOVED & ISDR IXXA0300037OOutflow Valve · contaminatedDURING CRUISE AT FLIGHT LEVEL 28K CABIN ALTITUDE BEGAN TO CLIMB. CREW ELECTED TO DEPLOY PASSENGER O2 MASKS. FLIGHT CONTINUED TO WSAP AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION MAINTENANCE CLEANED OUTFLOW VALVE, INSPECTED DUCTING AND OPERATIONALLY CHECKED SDR IXXA0300029OLanding Gear · false indicationDURING FLIGHT FROM KWAK TO RJTY LANDING GEAR WAS PUT IN DOWN POSITION. THERE WAS NO LEFT GEAR INDICATION. THE GEAR WAS RECYCLED AND IT INDICATED GEAR DOWN. MAINTENANCE JACKED AIRCRAFT AND SWUNG GEAR A TOTAL OF FIVE TIMES. OPERATIONAL CHECK GOOD IN ACCORDANSDR IXXA0300012OO-Ring · leakingDURING CRUISE CREW NOTED HYD QTY DROPPING ABNORMALLY. CREW COMPLETED ABNORMAL CHECKLIST AND PROCEEDED TOWARDS QPG. WHILE ON FINAL APPROACH, AFTER ADVISING QPG ATC OF ABNORMAL CHECKLIST COMPLETION. QPG ATC DENIED LANDING CLEARANCE. CREW ELECTED TO PROCEED TSDR IXXA0200116OO-Ring · leakingEN ROUTE FROM NKW TO BAH. FLIGHT CREW NOTED MAIN HYDRAULIC SYSTEM FLUID QUANITY DECLINING. CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED WITHOUT INCIDENT TO BAH. MAINTENANCE DISCOVERED O-RING LEAKING AT MAIN HYDRAULIC SYSTEM SELECTOR VALVE. REPLACED O-RING ANSDR IXXA0200114OStriker · looseENROUTE KWA TO HIK, THE GEAR DOOR NOT LATCH LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE GEAR, PERFORMED AN GEAR UPLOCK CHECK AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEASDR IXXA0200073SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE STATION XFS 178 TO XFS 285. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND REPAIR DOUBLER IN ACCOURDSDR IXXA0200072SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 857 TO 902 BETWEEN LONGERONS 10L TO 21L. REPAIR ACCOMPLISHED CORROSION REMOVAL AND FOUND TO BE WITHIN LIMITATIONS. CORROSION REMOVAL AT FUSELAGESDR IXXA0200071SWing · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING UPPER LEADING EDGE OUTBOARD OF NUMBER FOUR PYLON. REPAIR ACCOMPLISHED REOMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERMAL DOUBLER IN ACCORDANCE WISDR IXXA0200070SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 902, LONGERONS 14,17 AND 18 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL AND DETERMINED TO BE WITH LIMITATION IN ACCORDANCE WITH THE DOUGLAS STRUCTURSDR IXXA0200069SDoor · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 15OO, AFT PASSENGER DOOR FRAME AT THE LOWER AFT CORNER. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGE AREA, FABRICATION AND INSTALLATION OF A NEW INTERNAL REPAIR ANGLE AND FRAME IN ACCOSDR IXXA0200067SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD ENTRANCE DOOR CUT OUT FORWARD UPPER CORNER. REPAIR ACCOMPLISHED, REMOVAL OF THE TEMPORARY REPAIR AND DAMAGED AREA, FABRICATION AND INSTALLATIN OF A REPAIR FILLER, SDR IXXA0200066SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HAND SIDE FUSELAGE SKIN BELOW THE AFT PASSENGER DOOR SKIN CUT OUT AT STATION 1480 TO 1510. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED SKIN, FABRICATION AND INSTALLATION OF FILLER REPAIR DOULBESDR IXXA0200065SSkin · crackedDURING ROUTINE C-CHECK, A CRACK WAS DETECTED IN THE AFT PASSENGER DOOR FORWARD LOWER SKIN CORNER AT SKIN CUTOUT. REPAIR ACCOMPLISHED, REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOUGSDR IXXA0200064SSpar · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN XRS 190 INBOARD TO WING WALK AREA TO INCLUDE THE MAIN SKIN EXTENSION OVER GEAR TRUNNION AREA. REPAIR ACCOMPLISHED CORROSION REMOVAL. FABRICATION AND INSTASDR IXXA0200063SSpar · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE UPPER WING EXTERNAL PLATING BETWEEN WING STATION XFS 172 AND XFS 255. REPAIR ACCOMPLISHED, CORROSION REMOVAL OF THE DAMAGE ARE, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITHSDR IXXA0200062SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, LIGHT CORROSION WAS DETECTED ON THE TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN STATION XW 408 XRS 590 TO STATION XRS 590. REPAIR ACCOMPLISHED CORROSION REMOVAL OF THE AFFECTED AREA IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL RSDR IXXA0200061SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACKED WAS DETECTED ON THE RIGHT WING OUTBOARD LEADING EDGE PANEL AT THE INBOARD AREA AT STATION XRS 634. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A FILLER AND REPAIR DOUBLER IN ACCSDR IXXA0200060SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE AT WING STATION XES710, UPPER CHORD MOUNTS. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBSDR IXXA0200059SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE LEFT WING OUTBOARD LOWER LEADING EDGE AT STATION XFS 566. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBLER IN ACCOSDR IXXA0200058SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LT WING OUTBOARD UPPER LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH THE DOUGLAS SSDR IXXA0200057SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RT WING OUTBOARD LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH SDR IXXA0200056SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED IN THE LEFT WING LEADING EDGE TOP SIDE AT STATION XFS 825. REMOVAL ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIRSDR IXXA0200055SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AROUND THE SCREW HEADS ON THE TOP LEFT WING LEADING EDGE XFS 885. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS SDR IXXA0200054SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE AT STATION 1440 AT LONGERON 22RT. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH THE DOUGLAS STSDR IXXA0200053SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE AFT LOWER FUSELAGE FORWARD OF ACCESS PANEL NUMBER 60, STATION 1557 TO 1574, LONGERON 35 RT. REPAIR ACCOMPLISHED, REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A INTERNAL FILLER ANSDR IXXA0200052SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE AFT LOWER FUSELAGE STATION 1520 BETWEEN LONGERONS 30LT TO 30RT. REPAIR ACCOMPLISHED, DAMAGED AREA CUT OUT, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLASDR IXXA0100074OFan · defectiveENROUTE FROM KWA TO HIK, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT AND THE AFT PASSENGER COMPARTMENT WHEN THE RIGHT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDINSDR IXXA0100038Uplock · lack of lubeEN ROUTE FROM HIK TO SUU, THE LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO SUU FOR AN UNEVENTFUL LANDING. MAINTESDR IXXA0100005Door · missingAFTER AN UNEVENTFUL LANDING AND DURING POST FLIGHT INSPECTION AT WRI. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR LOWER FLYING DOOR MISSING FROM THE GEAR. NO OTHER DAMAGE TO THE AIRCRAFT WAS NOTED. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY FOR RESDR IXXA01000052Door · missingAFTER AN UNEVENTFUL LANDING AND DURING POST FLIGHT INSPECTION AT WRI. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR LOWER FLYING DOOR MISSING FROM THE GEAR. NO OTHER DAMAGE TO THE AIRCRAFT WAS NOTED.SDR IXXA0000025Fan · defectiveEN ROUTE FROM ASI TO ANU, THE FLIGHT CREW DETECTED SMOKE IN THE COCKPIT ACCOMPANIED BY THE LEFT RECIRCULATION FAN SHUTING DOWN, SMOKE SUBSIDED. THE FLIGHT CONTINUED TO ANU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECT THE LEFT RECIRCULATION FAN AND FOUND ITSDR IXXA0000017Fan · defectiveEN ROUTE FROM FJR TO NKW, THE FLIGHT CREW NOTICED SMOKE INTO THE COCKPIT WHEN THE LEFT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE SMOKE SUBSIDED. THE FLIGHT CONTINUED TO NKW FOR AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE FSDR IXXA9900032Fan · failedEN ROUTE FROM QPG TO NKW, AN ELECTRICAL ODOR WAS SENSED IN THE COCKPIT WHEN THE RIGHT RECIRCULATING FAN WAS TURNED ON. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO NKW. MAINTENANCE INSPECTED THE FAN AND WAS FOUND DEFECTIVESDR IXXA9900007Turbine · failedEN ROUTE FROM PKWA TO PHIK DURING CLIMB, A LOUD NOISE WAS HEARD FROM THE NUMBER TWO ENGINE, ACCOMPANIED BY INCREASING ENGINE GAS TEMPERATURE AND A DECLINE IN OIL PRESSURE. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND CONTINUED TO PHIK FSDR IXXA9800080Tires · wornAFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW HEARD AND FELT A VIBRATION THROUGH THE COCKPIT FLOOR. THE AIRCRAFT RETURNED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE NOSE TIRES OUT OF ROUND. SDR IXXA9800079Retract Mech · lack of lubeAFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A NOSE GEAR DOOR HAD FALLEN OPEN CAUSING A LOUD NOISE AND SLIGHT VIBRATION FROM THE NOSE WHEEL WELL AREA. THE CREW CYCLED THE GEAR, THE VIBRATION CONDITION WAS STILL PRESENT. THE AIRSDR IXXA9800068Switch · defectiveEN ROUTE FROM BWI TO WRI, WHEN THE LANDING GEAR WAS RETRACTED, THE LANDING GEAR UNSAFE LIGHT REMAINED ON. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO WRI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THESDR IXXA9800060Ballast · failedEN ROUTE FROM KWA TO HIK, SMOKE EMANATED FROM THE FIRST OFFICERS RIGHT PEDESTAL CONSOLE. THE CREW EXTINGUISHED THE MAIN INSTRUMENT GLARESHIELD WHITE LIGHTING, THE SMOKE STOPPED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND THAT TSDR IXXA9800057Actuator · misriggedEN ROUTE, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCH WARNING LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR WITH THE INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO SUU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR AND INDSDR IXXA9800034Fan · failedENROUTE, A BURNT ELECTRICAL ODOR WAS SENSED IN THE COCKPIT WITH THE RIGHT RECIRCULATION FAN OPERATING. THE FAN WAS SHUT OFF FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED AND FOUND THE FAN DEFECTIVE. MAINTENANCE DEFERRED THE RIGHT RECIRCULATION FAN.SDR IXXA9800035Switch · defectiveENROUTE, GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCHED WARNING LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE GEAR EXTINGUSHING THE WARNING LIGHT. GROUND INSPECTION FOUND THE LEFT MAIN GEAR UPLATCH SWITCH INTERMITTENT AND ELECTRICAL CONNECTOR DAMAGED. SDR IXXA980016Sealing Tape · misinstalledDURING DESCENT INTO HIK, THE NUMBER TWO AND FIVE MAIN CARGO COMPARTMENT SMOKE DETECTOR WARING LIGHTS ILLUMINATED. THE FLIGHT CREW TURNED OFF THE CARGO COMPARTMENT LIGHTING AND THE WARNING LIGHTS EXTINGUISHED. MAINTENANCE INSPECTED THE CARGO COMPARTMENT WITH TSDR IXXA9800027Plating · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 1120 TO 1160, LONGERON 31 RIGHT. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND AN EXTERNSDR IXXA9800041Frame · corrodedDURING ROUTINE D-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE FRAME AT FUSELAGE STATION 133 LONGERON 21 RIGHT. REPAIR ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF TWO NESTED ANGLE REPAIR DOUBLERS IN ACCORDANCE WITH FAA PER APPROSDR IXXA9800024Bulkhead Panel · crackedDURING ROUTINE D-CHECK INSPECTION, A CRACK WAS FOUND ON THE PRESSURE BULKHEAD PANEL BETWEEN FUSELAGE STATIONS 133 AND 148. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF FILLER, NESTED ANGLE DOUBLERS AND FINGER DOUBLER IN ACCOSDR IXXA980014Access Panel · corrodedDURING ROUTINE D CHECK INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING LEADING EDGE ACCESS PANEL LAND AT STATION XFS 361. REPAIR ACCOMPLISHED REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND TWO REPAIR DOUBLERS AND THIPLERS IN
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