N152CA, cancelled Jan 11, 2001
Service difficulty reports · 59
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 = 'N152CA' AND deregistration_id = 'N152CA-2001-01-11' 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 = 'N152CA' AND deregistration_id = 'N152CA-2001-01-11' 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 COMA0010014Battery · dischargedAFT SECTION OF CABIN EMERGENCY LIGHTS WERE INOPERABLE. REPLACED THE NR 3 EMERGENCY BATTERY.SDR COMA0010013Warning System · activatedFLAP DISAGREE WHEN FLAPS SELECTED UP. COULD NOT DUPLICATE. OPERATON OF FLAPS NORMAL.SDR COMA0010010Battery · dischargedEMERGENCY FLOOR PATH LIGHTS ARE INOPERABLE ROWS 1-5. REPLACED EMERGENCY BATTERY.SDR COMA0010001Warning System · activatedSERVICE DOOR WARNING DURING TAKEOFF. CLOSED AND SECURED SIGNLE POINT FUEL SERVICE DOOR.SDR COMA9910162Np Indicator · failedDURING TAKEOFF ROLL, THE RIGHT PROPELLER INDICATED 97.6 PERCENT NP. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT NP INDICATOR.SDR COMA9910107Sign · brokenEMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPAIRED EXIT SIGN.SDR COMA9910088Batteries · dischargedHTS - FLT 5730 - EMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE EMERGENCY BATTERIES. (M)SDR COMA9910085Battery · dischargedLAN - FLT 5076 - EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERIES. (M)SDR COMA9910078Actuator · failedFLAP CONTROL FAULT AT 80 KTS ON TAKEOFF. REPLACED RIGHT INBOARD FLAP ACTUATOR.SDR COMA9910068Warning · activatedFLAP CONTROL FAULT WARNING. COULD NOT DUPLICATE, NO DEFECTS FOUND.SDR COMA9810292Bulb · failedEMERGENCY LIGHT AT SEAT 2A IS INOPERABLE. REPLACED LIGHT BULB.SDR COMA9810272Actuator · malfunctionFLAP CONTROL FAULT DURING APPROACH. REPLACED THE LEFT HAND NACELLE FLAP ACTUATOR.SDR COMA9810258Connector · defectiveFLAP CONTROL FAULT. REPLACED ACTUATOR WIRNG CONNECTOR JO 365.SDR COMA9810254Battery · dischargedROW 1 AND ROW 4 EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA9810194Sign · brokenEMERGENCY LIGHT COVER AT 5C IS BROKEN. REPLACED EXIT SIGN.SDR COMA9810167Warning · activatedFLAP SYSTEM WARNING DURING TAKEOFF. COULD NOT DUPLICATE, SYSTEM TEST NORMAL.SDR COMA9810126Battery · dischargedFORWARD CABIN EMERGENCY LIGHTING IS INOP. REPLACED EMERGENCY BATTERY.SDR COMA9810115Sign · brokenEXIT SIGN AT ROW 5A IS BROKEN. REPLACED EXIT SIGN.SDR COMA9810111De-Ice Boot · wornRIGHT ENGINE INLET DE-ICE SYSTEM FAILURE DURING CRUISE FLIGHT. REPLACED LEFT AND RIGHT ENGINE INLET DE-ICE BOOTS.SDR COMA9810073Rollers · wornFLAP CONTROL FAULT WHEN FLAPS SELECTED FOR LANDING APPROACH. REPLACED THE RIGHT HAND INBOARD FLAP ROLLERS.SDR COMA9810041Actuator · malfunctionFLAP CONTROL FAULT WARNING. REPLACED THE RIGHT HAND NACELLE FLAP ACTUATOR.SDR COMA9710489Press Regulator · malfunctionLEFT AIR FOIL DE-ICE SYSTEM INOP. REPLACED THE DE-ICE PRESSURE REGULATOR.SDR COMA9710327Battery · dischargedFORWARD CABIN EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHT BATTERY.SDR COMA9710323Channel · wornLEFT WING FAIRING COMPOSITE HAS SLIGHT DELAMINATION AT EDGE. REPAIRED WING FAIRING IAW SRM.SDR COMA9710297Battery · dischargedEMERGENCY LIGHTS FAIL AFTER 5 SECONDS OF USE. REPLACED THE EMERGENCY LIGHT BATTERIES (S/N 1236, 810, AND 956).SDR COMA9710222Rollers · wornFLAP DISAGREEMENT AFTER TAKEOFF. REPLACED RT OUTBOARD FLAP ROLLERS.SDR COMA9710128Pitchlock Screw · malfunctionedPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR ACTUATOR AND HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB WAS FOUND DISPLACED .025 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER. PART TOTAL CYCLES, SDR COMA9710126Connector · looseWHEN FLAPS EXTENDED, INBOARD FLAPS REMAINED UP AND OUTBOARD FLAPS WENT FULL DOWN. REPAIRED LOOSE WIRE CONNECTOR AT THE FLAP CONTROL UNIT.SDR COMA9710098Flap Contl Unit · malfunctionFLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,093.SDR COMA9710091Hinge · brokenLT M.L.G. DOORS DO NOT CLOSE PROPERLY. REPLACED BROKEN DOOR HINGE ON LT M.L.G. AFT DOOR.SDR COMA9610422Butt Strap · misdrilledDURING 2C CHECK THE FUSELAGE AFT FLOOR SUPPORT STRUCTURE BUTT STRAP AT CARGO DOOR OPENING WAS FOUND TO HAVE MISDRILLED HOLES. THE BUTT STRAP WAS REPAIRED PER AERODESIGN REPORT NR 2139-1, REV IR, DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610421Joint Sheet · gougedDURING 2C CHECK, INSPECTION REVEALED THE WING AUX SPAR CENTER SECTION JOINT SHEET DAMAGED BY SCREWS THAT ATTACH THE LOWER FAIRING. THE DAMAGE CONSISTS OF A SMALL GOUGE ALONG THE BOTTOM EDGE, ONE ON THE LEFT SIDE AND ONE ON THE RIGHT SIDE OF THE SHEET. THE SHSDR COMA9610420Butt Strap · corrodedDURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT RT BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610419Sill · corrodedDURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL REPLACED WITH NEW PART PER SRM CHAPT. 51 STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610418Sill · corrodedDURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL CORRODED. SILL WAS REPAIRED PER AERODESIGN REPORT NR 2140-1, REV IR, DATED 12-22-96. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610417Sill · corrodedDURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES.SDR COMA9610416Sill · corrodedDURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. REPLACED SILL WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610415Butt Strap · corrodedDURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. REPLACED BUTT STRAP WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610414Butt Strap · corrodedDURING 2C CHECK FWD FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610413Butt Strap · corrodedDURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP FOUND CORRODED. BUTT STRAP WAS REPLACED WITH NEW PART PER SRM CHAPT 51, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610412Sill · corrodedDURING 2C CHECK FUSELAGE FWD CABIN FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM 51-40, STANDARD PRACTICES. AIRCRAFT TOTAL CYCLES, 20,051.SDR COMA9610411Stringer · corrodedDURING 2C CHECK INSPECTION FOUND CORROSION ON FUSELAGE STRINGER 19L BETWEEN FRAMES 19 AND 20. STRINGER 19L WAS REPAIRED PER AERODESIGN REPORT NR 1990-2, REV.IR DATED 9-15-96.SDR COMA9610405Hydraulic Hose · failedHYDRAULIC FLUID LEAKING FROM LT LANDING GEAR AREA. REPLACED LEAKING LANDING GEAR ACTUATOR HYDRAULIC HOSE.SDR COMA9610309Flap Contl Unit · malfunctionFLAP CONTROL FAULT WARNING, INBD FLAPS ARE FAILED. REPLACED THE FLAP CONTROL UNIT.SDR COMA9610306Flap Selector · malfunctionFLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR UNIT.SDR COMA9610301T Section · corrodedFOUND FUSELAGE FLOOR SUPPORT STRUCTURE T-SECTION CORRODED IN FWD CABIN AREA. REMOVED CORRODED T-SECTION AND INSTALLED NEW PART PER REPORT NR 2057-1, REV. IR, DATED 10-6-96. AIRCRAFT TOTAL CYCLES, 19,871.SDR COMA9610300Butt Strap · corrodedFOUND FUSELAGE FLOOR SUPPORT STRUCTURE FORWARD LT BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER EMB120 SRM STANDARD PRACTICES, CH 51-40-02. AIRCRAFT TOTAL CYCLES, 19,871.SDR COMA9610272Battery · dischargedAFT SECTION OF CABIN EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY. PART TOTAL CYCLES, 13,088.SDR COMA9610260Circuit Breaker · damagedEMERGENCY BUS LOST POWER, CONTROL BUS INOP, RT ENGINE INSTRUMENTS INOP, COPILOTS EFIS AND COMM RADIO INOP, A LANDING GEAR INDICATION INOP. FOUND BUS BAR CONNECTION TO CIRCUIT BREAKER 0470 LOOSE WITH HEAT DAMAGE TO BREAKER. REPLACED C/B 0470 AND ATTACHING HARSDR COMA9610224Flap Warning · activatedFLAP CONTROL FAULT WARNING AFTER LANDING. INSPECTED FLAP SYSTEM AND FOUND TO OPERATE NORMALLY. COULD NOT DUPLICATE DISCREPANCY.
Back to N152CA, cancelled Jan 11, 2001