N244CA, cancelled Aug 21, 2013
Service difficulty reports · 47
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 = 'N244CA' AND deregistration_id = 'N244CA-2013-08-21' 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 = 'N244CA' AND deregistration_id = 'N244CA-2013-08-21' 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 COMA9910035Skin · dentedDURING 1C INSPECTION, FOUND SMALL DENT IN FUSELAGE SKIN BETWEEN FS 6462.6 AND 6653.1 AND BETWEEN STRINGERS 19L AND 18L. REPAIRED DAMAGED AREA IAW EMB 120 SRM 53-00-01 PG 202-204.SDR COMA9910036Plate · dentedDURING ENGINE REPLACEMENT, THE LEFT NACELLE CENTER PLATE SECTION WAS FOUND TO HAVE A DENT AND CHAFING DAMAGE ON THE AFT OUTBOARD SIDE. BOTH THE DENT AND CHAFING DAMAGE WERE REPAIRED PER AERODESIGN REPORT NR 3133-1, REV IR, 2-12-99.SDR COMA9910031Lens · missingEMERGENCY EXIT LIGHT COVER IS MISSING AT ROW 5. REPLACED LIGHT COVER.SDR COMA9910015Valve · malfunctionedAIR CONDITIONING SYSTEM EMITS SMOKE. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RIGHT HAND ENGINE P2.5/3 SWITCHING VALVE FOR TROUBLESHOOTING.SDR COMA9810266Bulb · failedEMERGENCY FLOOR LIGHT AT ROW 5 INOPERABLE. REMOVED AND REPLACED BULB.SDR COMA9810128Roller · wornFLAPS WOULD NOT RETRACT AFTER TAKEOFF. REPLACED FLAP ROLLERS AT LEFT HAND OUTBOARD FLAP.SDR COMA9810118Sensor · malfunctionedWHEN LANDING GEAR RETRACTED, THE NLG DOWN LIGHTS AND INTRANSIT LIGHTS REMAINED ON. REPLACED THE NLG DOWN LOCK PROXIMITY SENSOR.SDR COMA9810099Intransit Light · illuminatedLEFT HAND MLG INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. ENTERED DISCREPANCY IN DEFERRED MAINTENANCE LOG PER MEL.SDR COMA9810098Support · corrodedDURING 2C INSPECTION TASK 5310-131/132-01I, FOUND FLOOR SUPPORT-T AT FRAME 20R CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.SDR COMA9810097Sill · corrodedDURING 2C INSPECTION TASK 151/152-01Z, FOUND AFT EMERGENCY EXIT SILL AND PIN RECEPTACLES CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PARTS AND INSTALLED SERV PARTS IAW EMB-120 SRM, CHAPTER 51.SDR COMA9810096Support · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 20L CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.SDR COMA9810095Sill · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FIRST LEFT FLOOR SILL CORRODED BYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.SDR COMA9810094Sill · corrodedDURING 2C INSPECTION TASK 161/162-01Z, FOUND RIGHT CARGO FORWARD FLOOR SILL CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.SDR COMA9810093Support · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 16L CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51.SDR COMA9810092Support · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 16R CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.SDR COMA9810091Strap · corrodedDURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FIRST RIGHT BUTT STRAP CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51.SDR COMA9810090Sill · corrodedDURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND FIRST RIGHT FLOOR SILL CORRODED BYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51.SDR COMA9810089Strap · corrodedDURING 2C INSPECTION TASK 5310-131/01I, FOUND FIRST LEFT HAND BUTT STRAP CORRODED BEYOND EMB-LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51.SDR COMA9810088Strap · corrodedDURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND FIRST CENTER BUTT STRAP CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51.SDR COMA9710485Control Box · failedLEFT HAND MLG UNSAFE INDICATION DURING TAKEOFF. REPLACED THE LANDING GEAR CONTROL BOX.SDR COMA9710468Regulator Valve · failedRT BLEED AIR DUCT LEAK WARNING ON. FOUND THE DRAIN CUP ON THE DE-ICE PRESSURE REGULATOR HAD FALLEN OFF. THIS ITEM IS RETAINED BY A WORN CLAMP. REINSTALLED DRAIN CUP.SDR COMA9710403Gear Control · failedLANDING GEAR CONTROL WAS CYCLED 3 TIMES BEFORE GEAR RESPONDED. REPLACED THE LANDING GEAR CONTROL.SDR COMA9710402Tq Signal Cond · malfunctionAUTO FEATHER AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE RIGHT ENGINE TORQUE SIGNAL CONDITIONER.SDR COMA9710352Bulb · failedRIGHT GEAR INDICATED UP ATER PLACING GEAR HANDLE DOWN. USED ELECTRICAL OVERRIDE, GEAR CONFIRMED DOWN, APPEARS TO BE AN INDICATION PROBLEM. REMOVED AND REPLACED ALL LANDING GEAR INDICATOR DOWN BULBS. PERFORMED SEVERAL GEAR SWINGS, NO DEFECTS NOTED.SDR COMA9710268Lockwasher · wornDURING E-5 INSPECTION, FOUND LEFT MAIN GEAR OUTBOARD TRUNNION BEARING NUT TO BE LOOSE. REMOVED NUT AND FOUND LOCKWASHER INNER TAB TO BE SHEARED OFF. ALSO, NOTICED THAT LOCK WASHER WAS OUT OF ROUND AND APPEARED TO BE STRETCHTED IN AREA OF INNER TAB. REPLACEDSDR COMA970150Roller · dirtyFLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP ROLLERS.SDR COMA9710096Pitchlock Screw · bentACTUATOR ASSEMBLY REMOVED FROM AIRCRAFT DUE TO FEATHER STOP TAB BEING FOUND DISPLACED. AIRCRAFT BROUGHT IN FOR SCHEDULED MAINTENANCE. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N S0561 WAS FOUND TO BE BENT APPROXIMATELY 0.125 INCH. PITCHLOCK SSDR COMA9710048Apu · malfunctionedAUXILIARY POWER UNIT START CYCLE HUNG AT 45 DEGREES, START CYCLE WAS ABORTED, DISCHARGED AUXILIARY POWER UNIT FIRE EXTINGUISHER AFTER REPORT OF FIRE. INSPECTED AUXILIARY POWER UNIT AND COMPARTMENT, NO DEFECTS NOTED. DEFERRED AUXILIARY POWER UNIT AND AUXILIARSDR COMA9710041Tracks · dirtyFLAP DISAGREEMENT AFTER TAKEOFF. CLEANED AND INSPECTED FLAP TRACKS AND ROLLERS, OPERATIONAL CHECK GOOD.SDR COMA9710035Bushing · failedWHEN CAPTAIN'S FEET CONTACT RUDDER PEDALS, PEDAL ADJUSTMENT WILL NOT HOLD. REPLACED BUSHING IN PEDAL ADJUSTMENT ASSEMBLY.SDR COMA9710127Pitchlock Screw · malfunctionedPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR BLADE AND HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION, THE FEATHER STOP TABS S/N S0455 WERE FOUND DISPLACED APPROXIMATELY 0.125 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTUSDR COMA9610333Eec · out of adjustON INITIAL CLIMBOUT, THE NR 1 ENGINE TORQUE FLUCTUATED FROM 92 PERCENT TO 100 PERCENT. WHEN POWER WAS REDUCED THE FLUCTUATION WAS FROM 72 PERCENT TO 90 PERCENT, OPERATION BECAME NORMAL SHORTLY. TRANSFERRED TO DEFERRED LIST CAT C, MEL 73-21-1, EXPIRES 11-29-9SDR COMA9610279Indication · malfunctionedWHEN LANDING GEAR SELECTED TO RETRACT, BOTH THE GREEN DOWN AND RED INTRANSIT LIGHTS WERE ON. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL AND FUNCTIONAL CHECKS OF LANDING GEAR RETRACTION SYSTEM WERE NORMAL.SDR COMA9610258Control Unit · malfunctionFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED FLAP CONTROL BOX.SDR COMA9610155Tcas · malfunctionPILOT'S RED HEADING FLAG LIGHT ON ALONG WITH FAILURE OF TCAS. REPLACED THE AHC-85. PART TOTAL CYCLES, 13,044.SDR COMA9610150Radar · malfunctionedRADAR DISPLAY IS ERRATIC AND ERRONEOUS. PLACED WEATHER RADAR SYSTEM ON DEFERRED MAINTENANCE LIST. ACFT RETURNED TO SERVICE.SDR COMA9610140Door Latch · brokenRIGHT MLG OUTBOARD DOOR HANGING OPEN AND WILL NOT CLOSE. REPLACED BROKEN LATCH ASSY.SDR COMA9610139Retract Mech · malfunctionedLANDING GEAR WILL NOT RETRACT. ALL GREEN DOWN INDICATORS AND ALL RED INTRANSIT INDICATORS ARE ILLUMINATED. REVERSED THE NLG UPLOCK PROXIMITY SENSORS AND DEFERRED SYSTEM PER EMB SNL 032-0015.SDR COMA9610118Line · chafedHYDRAULIC FLUID DRIPPING FROM LEFT ENGINE NACELLE. REPAIRED CHAFED HYDRAULIC PRESSURE LINE UNDER ENGINE FIRE DECK.SDR COMA9610107Leak Sensor · defectiveLEFT DUCT LEAK WARNING ACTIVATED DURING FLIGHT. REPLACED DUCT LEAK SENSOR IN LT WING ROOT.SDR COMA9610031Door Seal · looseCABIN PRESSURIZATION FAILED DURING FLIGHT. REPLACED CARGO DOOR SEAL WHICH HAD COME LOOSE.SDR COMA9610014Wheel · damagedMECHANIC REMOVED TIRE FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION IN WHEEL SHOP, FOUND DAMAGE TO SUB ASSY AND KEY INSERTS ANTICIPATE BRAKE FAILURE. SUB ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO BFG FOR FURTHER INSPECTION AND EVALUATION.SDR COMA9511964Controller · defectiveAFTER TAKEOFF, CABIN PRESSURE WAS RISING OUT OF CONTROL, SWITCHED TO MANUAL CONTROL WITH SAME RESULTS. AIRCRAFT RETURNED TO BHM. REPLACED THE ELECTRONIC PRESSURE CONTROLLER.SDR COM11858Hmu · defectiveLEFT ENGINE STARTS, BUT WILL NOT ACCELERATE BEYOND MIN FLOW. REPLACED THE ENGINE HMU.SDR COM11790Lead · brokenRT PROPELLER ANTI-ICE IS INOP. REPLACED BROKEN DE-ICE LEAD.SDR COM11779Sensor · defectiveLANDING GEAR CONTROL COULD NOT BE SELECTED TO UP UNTIL OVERRIDE RELEASE WAS USED. REPLACED THE LEFT MLG WEIGHT ON WHEELS PROXIMITY SENSOR.SDR COM11763Rollers · wornFLAP DISAGREEMENT WARNING, WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED THE LEFT OUTBD FLAP ROLLERS.
Back to N244CA, cancelled Aug 21, 2013