N162CA
Service difficulty reports not matched to an aircraft · 43
They name N162CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N162CA' AND registry_match IS NULL 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 = 'N162CA' AND registry_match IS NULL 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 SWIA200110068Switch · failedON TAXI, FLAPS SELECTED 15 DEGREES. FLAP INDICATOR GOES FROM 15 DEGREES TO 0 DEGREES EVERY MINUTE. GREEN BARS DISAPPEAR WHEN FLAPS ARE AT 0 DEGREES. THEY REAPPEAR AT FLAP 15. NO MAP INDICATION, JUST ONE CHIME ALERT. AS WE TAXIED BACK, ADVANCED SWS/FLAP ONSDR SWIA200110067Warning System · activatedABORTED TAKEOFF - TRIPLE CHIME - AURAL WARNING - BRAKES, FLAPS, AUTO FEATHER OCCURRED DURING TAKEOFF ROLL. REPLACED AND SECURED AURAL WARNING UNIT. PERFORMED OPS CHECK OF AUTO FEATHER SYSTEM. OPS CHECK GOOD. SN ON 0419 SN OFF 0224.SDR SWIA200110066Control Unit · failedDURING CRUISE, ASWS & FLAP LIGHTS ON MAP & ASYMMETRY DISSAGREEMENT, CONTROL FAULT LIGHTS ON OVERHEAD. PANEL FLAP INDICATOR FLUCTUATING 0 DEGREES - 45 DEGREES SEVERAL TIMES INTERMITTENTLY. INSTALLED SERVICEABLE FCU. OPS CHECK GOOD.SDR SWIA972628Actuator · failedCONTROL FAULT WHEN SELECTING FLAPS 15, RESET AS PER QRH. CONTROL FAULT AGAIN WHEN SELECTING FLAPS 25. PERFORMED ACTUATOR TEST ON BOTH OUTBOARD ACTUATORS. FOUND LEFT OUTBOARD ACTUATOR TO BE BAD. REMOVED AND REPLACED LEFT OUTBOARD ACTUATOR IAW MM 27-50-09. RSDR SWIA972550Sequence Valve · defectiveEN ROUTE A SYSTEM GREEN LIGHT ON FOR RIGHT MAIN GEAR AFTER LOWERING GEAR HANDLE. ALL SIX DISAGREEMENT LIGHTS ON AND NO ADDITIONAL GREEN LIGHTS. AFTER APPROXIMATELY A 1 MINUTE DELAY, ALL SIX GREEN INDICATIONS. INSPECTED LANDING GEAR FOR DEFECTS FOUND RIGHT ISDR SWIA972549Actuator · failedLANDING GEAR WOULD NOT EXTEND NORMALLY. PERFORMED GEAR EXTENSION BY ELECTRIC OVERRIDE CHECK LIST IN QRH. ALL EXTENDED NORMALLY. REPLACED MAIN ACTUATING CYLINDER WITH A SERVICEABLE UNIT AND ADJUSTED INBOARD SEQUENCE VALVE ON RIGHT GEAR. ALL WORK DONE PER MMSDR SWIA972353Rccb · failedRIGHT PROPELLER HEAT CONTINUES TO FAIL IN FLIGHT. EN ROUTE LAX DIVERTED TO PSP. INSPECTED LEFT AND RIGHT PROPELLER DEICE LEADS, LOOKED OK. CHECKED RIGHT PROPELLER HEAT RCCB. INSPECTED WIRING AT SWITCH AND RELAYS. FOUND POWER AT A2 OF RCCB 226 DROPS TO BELSDR SWIA972302Sensor · failedLANDING GEAR WOULD NOT EXTEND NORMALLY. CYCLED TWICE, NO EFFECT. PERFORMED QRH GEAR EXTENSION BY ELECTRICAL OVERRIDE TO EXTEND GEAR. REPLACED RIGHT MAIN A DOWNLOCK PROXIMITY SENSOR AND HARNESS PER MM 32-61-01. PERFORMED MULTIPLE GEAR SWINGS. OPS CHECK GOOSDR SWIA972258Actuator · malfunctionedCONTROL FAULT ON FLAP DURING RETRACTION ON GROUND. PRESS RESET AS PER QRH, FAULT CLEARED BUT REOCCURS WHEN RESELECTING FLAPS TO 15 DEGREES. INSTALLED SERVICEABLE LEFT NACELLE ACTUATOR AS PER RII 27-307. OPS CHECK. P/N ON 308200-1007, S/N ON 0195, S/N OFF 0SDR SWIA972255Actuator · failedAFTER SELECTING FLAPS 45 DEGREES DISAGREEMENT ILLUMINATED OUTBOARD PAIRS WERE AFFECTED WITH 4 LIGHT PAIRS NOT ILLUMINATED. DID NOT FIX ITSELF. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE ACTUATOR. PN ON 320300-1007 SN ON 0780 SN OFF 0SDR SWIA972209Warning System · activated''TAKEOFF TRIM'' WARNING SOUNDS ON POWER LEVER ADVANCEMENT WITH TRIM INDEX WELL WITHIN GREEN ARC. INSPECTED OUT OF TRIM PROX SENSORS. BOTH FOUND GOOD. PERFORMED SEVERAL FUNCTIONAL CHECKS OF TRIM WARNING SYSTEM. ALL FOUND GOOD. UNABLE TO DUPLICATE DISCREPANSDR SWIA972205Wire · brokenON TAKEOFF AURAL WARNING ''TAKE OFF'' CAME ON. ABORTED TAKEOFF. TRIM WAS IN THE GREEN BAND. UPON RETURN TO GATE, WARNING PERSISTED REGARDLESS OF TRIM WHEEL POSITION. REPAIRED BROKEN WIRE AT ELEVATOR TRIM PROXIMITY SENSORS IAW EMB120 MM 27-32-05. OPS CHECK SDR SWIA971524Mask · malfunctionedROW 7 OXYGEN MASKS FELL DOWN. RETURNED TO SEA. SECURED OXYGEN MASK. EXAMINED LATCHING DEVICE AND FOUND NO DEFECTS. OPS CHECKS GOOD.SDR SWIA971508Circuit Breaker · trippedLANDING GEAR WOULD NOT RETRACT. RETURNED TO PDX. RESET UP/DOWN CONTROL AND DOWN CONTROL OVERRIDE CIRCUIT BREAKERS.SDR SWIA971298Line · failedRIGHT ENGINE LOST OIL PRESSURE ON DESCENT. PRESSURE DROPPED BELOW 40 PSI AND ENGINE HAD TO BE SHUT DOWN. REPLACED OIL COOLER CROSS FLOW LINE. RAN ENGINE, LEAK AND OPS CHECKS GOOD.SDR COMA9810054Sign · brokenEMERGENCY EXIT SIGN AT SEAT 5A IS BROKEN. REPLACED EXIT SIGN.SDR COMA9810038Tq Indicator · malfunctionDURING TAKEOFF, THE RIGHT HAND TORQUE INDICATION WAS 195 PERCENT. REPLACED THE TORQUE INDICATOR.SDR COMA9710478Unsafe Light · malfunctionedWHEN LANDING GEAR SELECTED DOWN, THE RIGHT HAND MLG INDICATED UNSAFE. LANDING GEAR CYCLED TWICE BEFORE GREEN INDICATION. COULD NOT DUPLICATE DISCREPANCY. SYSTEM INDICATION AND EXTENSION AND RETRACTION CHECKS SATISFACTORY.SDR COMA9710404Nozzle · leakingFUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE ENGINE FUEL NOZZLES AND TRANSFER TUBES.SDR COMA9710340Relay · overheatedOVERHEATED ELECTRIC SMELL IN COCKPIT. REPLACED FEEDER PROTECTION RELAY K0152.SDR COMA9710232Bulb · failedEMERGENCY LAMP OVER ENTRANCE DOOR IS INOP. REPLACED BULB.SDR COMA9710224Rollers · wornFLAP DISAGREE WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED RIGHT HAND OUTBOARD FLAP ROLLERS.SDR COMA9710173Trim Tab Sensor · defectiveTAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR.SDR COMA9710129Wire · damagedWHEN FLAPS SELECTED TO 15 DEGREES, CONTROL FAULT WARNING ON. REPAIRED DAMAGED WIRING CONNECTION AT RT OUTBOARD FLAP ACTUATOR.SDR COMA9710027Control Unit · inoperativeON LANDING, AIRCRAFT YAWED SHARPLY AFTER CLEARING RUNWAY NWS DID NOT RESPOND WITH INPUTS FROM TILLER OR PEDALS. REPLACED STEERING ECU, TAXI CHECK GOOD.SDR COMA9610299Butt Strap · corrodedFOUND FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER REPORT NR 1671-1, REV. IR, DATED 10-22-95. AIRCRAFT TOTAL CYCLES, 19,871.SDR COMA9610290Actuator · leakingRT OUTBD MAIN GEAR DOOR ACTUATOR LEAKING. REPLACED GEAR DOOR ACTUATOR.SDR COMA9610247Switch · out of adjustSERVICE DOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. ADJUSTED THE AVIONICS DOOR MICROSWITCH.SDR COMA9610196Flap Warning · activatedFLAP CONTROL FAULT WARNING AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND WITH FLAP SYSTEM.SDR COMA9610197Seals · leakingFUEL DRIPPING FROM RT ENGINE NACELLE. REPLACED THE O-RING SEALS ON THE ENGINE FUEL NOZZLES.SDR COMA9610124Skin · dentedDURING ROUTINE MAINTENANCE, A LARGE DENT WAS FOUND ON THE FUSELAGE AFT RIGHT LOWER SKIN JUST FORWARD OF FRAME 45 BETWEEN STRINGERS 19R AND 20R. THE DAMGE WAS REPAIRED PER EMB120 SRM 53-00-01.SDR COMA9610099Swivel · leakingHYDRAULIC FLUID LEAKAGE ON LEFT MLG STRUT. REPLACED BROKEN LINE SWIVEL FITTING.SDR COMA9610089Actuator · defectiveLEFT INBD FLAP WILL NOT RETRACT. REPLACED THE LT INBD FLAP ACTUATOR.SDR COMA9610082Actuator · defectiveFLAP CONTROL FAULT WARNING. REPLACED THE RT OUTBD FLAP ACTUATOR. PART TOTAL CYCLES, 2,517.SDR COMA9610039Seal · defectiveRIGHT ENGINE NP FLUCTUATES. REPLACED PROPELLER TRANSFER TUBE SEALS.SDR COMA9610028Annunicator Pnl · malfunctionedDURING TAKEOFF, RECEIVED FLAP CONTROL FAULT WARNING. REPLACED THE FLAP ANNUNCIATOR PANEL.SDR COMA9512012Ahrs Computer · failedNR 1 AHRS IS INOP. REPLACED THE NR 1 AHRS COMPUTER.SDR COM11891Support · crackedTHE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED, DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO DESIGN REPORT 1327-2 P/N 120-17059-015, 1 EA; 120-17056-007, 5 EA; 120-17056-015, 4 EA; 120-17056-01SDR COM11822Roller · bindingFLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP DURING CLIMB. REPLACED ROLLERS ON RT OUTBD FLAP.SDR COM11817Skin Support · crackedFUEL WAS FOUND LEAKING FROM THE LEFT WING UPPER SKIN. TWO RIVET HEADS WERE FOUND BROKEN AT RIB NR 20 BETWEEN STRINGERS NR 2 AND NR 3. INTERNAL INSPECTION REVEALED THE SKIN SUPPORT BRACKET CRACKED AT THAT LOCATION. THE SKIN SUPPORT WAS REPLACED PER AERODESIGSDR COM11816Actuator · defectiveFLAP DISAGREEMENT WARNING, FLAPS WOULD NOT RETRACT. REPLACED THE RT OUTBD FLAP ACTUATOR.SDR COM11815Roller · defectiveFLAP DISAGREEMENT WARNING, FLAPS STUCK AT 15 DEGREES. REPLACED DEFECTIVE ROLLER ON LT OUTBD FLAP.SDR COM11760Actuator · defectiveFLAP CONTROL FAULT WARNING WILL NOT RESET. REPLACED RT OUTBD FLAP ACTUATOR.
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