N196CA, cancelled Jan 25, 2006
Service difficulty reports · 76
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 = 'N196CA' AND deregistration_id = 'N196CA-2006-01-25' 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 = 'N196CA' AND deregistration_id = 'N196CA-2006-01-25' 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 2006FA0000047Window Frame · crackedPILOTS SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT LEFT WINDSHIELD AFT BEAM. NORMAL OPS. (K)SDR SWIA200211201Engine · overtempON CLIMBOUT (LEFT) T6 RAISED WITH POWER REDUCTION. T6 CONTINUED TO RISE TO THE POINT OF T6 WARNING. T6 FINALLY CAME DOWN TO ABOUT 684 DEGREES, PRODUCING NO TORQUE. DID A PRECAUTIONARY ENGINE SHUTDOWN. RETURNED TO LAX. REMOVED AND REPLACED LEFT ENGINE IAW SDR SWIA200211150Control Box · malfunctionedLEFT LANDING RED LIGHTS REMAIN ON (A & B) WITH GEAR HANDLE SELECTED. INSTALLED SERVICEABLE LANDING GEAR RELAY BOX ASSY, SWUNG LANDING GEAR 35 PLUS TIMES. OPS CHECKS GOOD.SDR SWIA200211114Battery · dischargedDURING TAXI FOR TAKEOFF, FLOOR LEVEL EMERGENCY LIGHTING FROM ROW 6 TO AFT OF AIRCRAFT ILLUMINATED. COULD NOT BE EXTINGUISHED. REPLACED EMERGENCY LIGHT BATTERY AT ROW 8. OPS CHECK GOOD.SDR SWIA200211025Striker · out of adjustAFTER TAKEOFF, CARGO DOOR LIGHT ILLUMINATED, MASTER WARNING DOORS AND DOOR CAPTION ON MAP ILLUMINATED. WARNING DOES NOT OCCUR ON GROUND. RETURNED TO RDD. ADJUSTED CARGO DOOR AFT STRIKER PLATE. OPS CHECK GOOD.SDR SWIA200210835Wire Harness · faultyWITH GEAR HANDLE DOWN THE LANDING GEAR REMAINED UP AND LOCKED. LEFT THE GEAR HANDLE DOWN AND ON GO-AROUND THE LANDING GEAR CAME DOWN AND LOCKED. REPLACED WIRING HARNESS FOR LEFT MAIN LANDING GEAR PROXIMITY SENSOR. OPS CHECKS GOOD.SDR SWIA200210765Battery · dischargedFORWARD FLOOR EMERGENCY LIGHTS ARE OUT. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PER MM 33-50-02. OPS CHECK GOOD.SDR SWIA200210600Wire Harness · malfunctionedLEFT EEC FAILED ON TAKEOFF. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE UPPER WIRE HARNESS IAW POWER PLANT BUILDUP MANUAL 71-00-00. OPS CHECKED IAW MM 71-00-00. ALL PARAMETERS GOOD. P/N ON 31159-11-01, S/N OFF AA9663.SDR SWIA200110574Structure · crackedC-CHECK, PAX DOOR LOWER AFT TRACK, CRACK ON DOOR STRUCTURE. PERFORMED REPAIR ON PASSENGER DOOR UNDER LOWER AFT TRACK PER SB 120-052-0034.SDR SWIA200110355Fastener · looseSERVICE DOOR LIGHT ILLUMINATED ON CLIMB THROUGH 10,000 FEET. LIGHT WENT OUT ON DESCENT WHILE SLOWING. RETURNED TO FAT. FOUND 1 CAMLOCK ON INBOARD FUEL SERVICE DOOR LOOSE. RESECURED CAMLOCK AND INSPECTED ALL SERVICE DOORS MICROSWITCHES. NO FAULTS FOUND. WSDR SWIA200110159Uplock Sensor · dirtyRIGHT 'A' RED GEAR LIGHT DID NOT EXTINGUISH AFTER TAKEOFF. ALL GEAR DOORS REMAINED OPEN WITH GEAR SELECTED IN UP POSITION. CYCLED AS PER QRH.CLEANED AND INSPECTED RIGHT MAIN UPLOCK SENSORS AND SWUNG GEAR 20+ TIMES. NO FAULTS FOUND.SDR SWIA200110045Window Post · crackedCRACK FOUND IN RIGHT POST BETWEEN DIRECT VIEW WINDOW AND WINDSHIELD.FABRICATED AND INSTALLED DOUBLER IAW SB120-053-0010/3-18-88.SDR SWIA972351Battery · dischargedEMERGENCY LIGHTS WILL NOT STAY ON WHEN TURNED ON. REPLACED FORWARD EMERGENCY LIGHT BATTERY. OPS CHECKS GOOD. P/N ON: D366-04-00, S/N ON: 1213, S/N OFF: 349.SDR SWIA972350Fire Loop · damagedRIGHT DET INOP ENGINE/WW LIGHT ILLUMINATED INFLIGHT. RETURNED TO LAX. INSTALLED SERVICEABLE ENGINE FIRE DETECTION LOOP ON RIGHT ENGINE IAW MM 26-11-00. OPS CHECKS GOOD. S/N ON: 92233, S/N OFF: 80052.SDR SWIA972214Sequence Valve · malfunctionedON DEPARTURE RETRACTED LANDING GEAR, RIGHT MAIN WOULD NOT RETRACT. BOTH A & B RED LIGHTS ILLUMINATED. CREW IN AIRCRAFT BEHIND US NOTED THE RIGHT GEAR WOULD NOT RETRACT. NOSE/LEFT RETRACTED FINE. RETURNED TO PDX. TROUBLESHOT SYSTEM, FOUND RIGHT GEAR SEQUENCSDR SWIA972068Actuator · stuckAT SETTINGS BEYOND 1.0 UNITS NOSE DOWN, ELEVATOR TRIM WHEEL STICKS. THE ELECTRIC TRIM WHEEL ACTUATOR IS INCAPABLE OF OVERCOMING BEING STUCK, BUT IT CAN BE MANUALLY FORCED. NOTICEABLE AT SPEEDS GREATER THAN APPROXIMATELY 250 KIAS. REMOVED MOISTURE AND LUBED SDR SWIA971978Harness · chafedLEFT NH GAUGE BOTH ANALOG AND DIGITAL INOP DURING FLIGHT. ANALOG NEEDLE JUMPING BETWEEN 10 - 70 PERCENT AND DIGITAL JUMPING 90 - 150 PERCENT NH. DIVERTED TO PDX FROM RDM. REMOVED AND REPLACED LEFT NH GAUGE IAW 77-11-00. ALSO PERFORMED RESISTANCE CHECK OF WSDR SWIA971615Uplock · out of adjustUPON GEAR RETRACTION THE RIGHT MAIN GEAR RED A LIGHT WORLD NOT EXTINGUISH. ALSO HEARD BANGING SOUNDS AND FELT VIBRATION. RETURNED TO FAT. ADJUSTED RIGHT MLG UPLOCK INDICATION PLUNGER SCREW IAW 32-61-01. ALL GEAR SWING CHECKS GOOD.SDR SWIA971447Pin · bentRIGHT MAIN FORWARD GEAR DOOR HAS COME UNLATCHED TWO TIMES IN LAST TWO FLIGHTS. STRAIGHTENED LOCK PIN AND FUNCTION APPEARS NORMAL ON GROUND.SDR COMA9810148Lamp · failedEMERGENCY FLOOR LIGHT AT ROW 9 IS INOPERABLE. REPLACED LAMP.SDR COMA9810146Actuators · malfunctionINBOARD FLAPS ASYMMETRY WARNING DURING TAKEOFF. REPLACED THE INBOARD FLAPS ACTUATORS.SDR COMA9810139Mechanism · malfunctionedFLAP ASYMMETRY, INBOARD FLAPS WOULD NOT DEPLOY. COULD NOT DUPLICATE DISCREPANCY, SYSTEM OPERATIONAL CHECK SATISFACTORY.SDR COMA9810085Support · crackedCREW PREFLIGHT INSPECTION FOUND ONE RIVET HEAD BROKEN OFF IN FUSELAGE SKIN, LEFT HAND SIDE, FRAME NR 9, JUST BELOW CAPTAIN'S DV WINDOW. FURTHER INVESTIGATION REVEALED A CRACKED SKIN SUPPORT AT THAT LOCATION. THE SUPPORT WAS REPLACED PER AERODESIGN REPORT NR SDR COMA9710502Actuator · failedFLAP CONTROL FAULT WARNING. REPLACED THE RIGHT OUTBOARD FLAP ACTUATOR.SDR COMA9710470Autopilot · malfunctionedAUTO PILOT AND TRIM FAIL WARNINGS DURING TAKEOFF. DEFERRED AUTO PILOT SYSTEM PER MEL.SDR COMA9710464Angle · crackedDURING 2C INSPECTION, TASK 5320-244-02I FOUND WING TO FUSELAGE FAIRING ATTACH ANGLE PART NR 120-31657-002 CRACKED. REPAIRED ANGLE IAW APPROVED AERO-DESIGN REPORT 1226-3 REV A 2-18-95.SDR COMA9710463Sill · corrodedDURING 2C INSPECTION TASK 161-01Z, FOUND LEFT HAND CARGO FLOOR SILL CORRODED BEYOND LIMITS. REPLACED CORRODED SILL IAW EMB 120 SRM.SDR COMA9710462Cables · wornWHILE PERFORMING TASK 5720-681-01I ON RIGHT WING, 2C INSPECTION, FOUND BOTH AILERON CABLES WORN BADLY AT NACELLE FAIR LEADS. REPLACED CABLES IAW EMB 120 MM.SDR COMA9710461Control Cable · wornWHILE PERFORMING TASK 5720-581-01I ON LEFT WING, 2C INSPECTION, FOUND BOTH AILERON CABLES WORN BADLY AT NACELLE FAIRLEADS. REPLACED CABLES IAW EMB 120 MM.SDR COMA9710460Buttstrap · corrodedDURING 2C INSPECTION, TASK 5310-132-01I, FOUND NR 1 RIGHT SIDE BUTTSTRAP CORRODED BEYOND LIMITS. REPLACED BUTTSTRAP IAW SRM EMB-120.SDR COMA9710459Crossbeam · corrodedDURING 2C INSPECTIN TASK 5310-132-01I, FOUND RIGHT CROSSBEAM AT FRAME 16 CORRODED BEYOND LIMITS. REPLACED CROSSBEAM IAW EMB 120 SRM.SDR COMA9710458Crossbeam · corrodedDURING 2C INSPECTION, TASK 5320-142-03I, FOUND RIGHT CROSSBEAM AT FRAME 23 CORRODED BEYOND LIMITS. REPLACED CROSSBEAM IAW EMB 120 SRM.SDR COMA9710457Sill · corrodedDURING 2C INSPECTION, TASK 162-01Z, FOUND RIGHT FORWARD CARGO SILL CORRODED BEYOND LIMITS. REPLACED SILL IAW EMB-120-SRM.SDR COMA9710456T Section · corrodedDURING 2C INSPECTION, TASK 5310-132-O1I FOUND RIGHT FRAME 16 T-SECTION CORRODED BEYOND LIMITS. REPLACED T-SECTION IAW EMB-120 SRM.SDR COMA9710455Buttstrap · corrodedDURING 2C INSPECTION TASK 161-01Z, FOUND LEFT HAND CARGO THRESHOLD BUTTSTRAP CORRODED BEYOND LIMITS. REPLACED BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710454Butt Plate · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED CENTER BUTT PLATE TO BE CORRODED. REPLACED CENTER BUTT PLATE USING APPROVED AERODESIGN REPORT NR 1671-1.SDR COMA9710453Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED CENTER BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB SRM STANDARD PRACTICES.SDR COMA9710452Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED LEFT BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB SRM STANDARD PRACTICES.SDR COMA9710451Buttstrap · corrodedDURING 2C INSPECTION TASK 0 152-01Z, REVEALED LEFT HAND BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB SRM STANDARD PRACTICES.SDR COMA9710450Buttstrap · corrodedDURING 2C INSPECTION TASK 161-01Z REVEALED LEFT HAND CARGO BUTTSTRAP TO BE CORRODED. ALSO, FOUND THAT CARGO LINING SCREW HAD BEEN SCREWED INTO STRAP. REPLACED BUTTSTRAP USING EMB SRM STANDARD PRACTICES.SDR COMA9710449Buttstrap · corrodedDURING 2C INSPECTION TASK 5320-147-03I REVEALED CENTER BUTTSTRAP TO BE CORRODED. REPLACED BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710448Sill · corrodedDURING 2C INSPECTION TASK 5310-131-O1I REVEALED RIGHT FLOOR SILL (UNDER LAV) TO HAVE HEAVY CORROSION. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710447Sill · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED LEFT SILL (UNDER GALLEY) TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710446Sill · corrodedDURING 2C INSPECTION TASK 5310-141-03I REVEALED LEFT NR 2 SILL TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710445Sill · corrodedDURING 2C INSPECTION TASK 151-01Z REVEALED RIGHT SILL TO BE CORRODED. REPLACED SILL USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710444Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131-O1I REVEALED LEFT FLOOR CROSSBEAM AT FRAME 15 TO BE CORRODED. REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710443Crossbeam · corrodedDURING 2C INSPECTION TASK 141-01Z REVEALED FLOOR CROSSBEAMS LEFT AT FRAME 20 AND LEFT AT FRAME 23 (BOTH THE SAME PART NUMBER) TO HAVE CORRODED BEYOND LIMITS. REPLACED CROSSBEAMS USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710442Crossbeam · corrodedDURING 2C INSPECTION TASK 151-01Z REVEALED RIGHT FLOOR CROSSBEAM AT FRAME 33 TO BE CORRODED BEYOND LIMITS. REPLACED CROSSBEAM USING EMB120 SRM STANDARD PRACTICES.SDR COMA9710441T Section · corrodedDURING 2C INSPECTION TASK 5310-131-01I REVEALED LEFT CENTER T-SECTION TO BE CORRODED BEYOND LIMITS. REPLACED T-SECTION USING EMB 120 SRM STANDARD PRACTICES.SDR COMA9710439T Section · corrodedDURING 2C INSPECTION TASK 141-012 REVEALED T-SECTION AT FRAME 23 TO BE CORRODED. REPLACED T-SECTION USING EMB 120 STANDARD PRACTICES.
Back to N196CA, cancelled Jan 25, 2006