N168CA, cancelled Mar 1, 2001
Service difficulty reports · 71
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 = 'N168CA' AND deregistration_id = 'N168CA-2001-03-01' 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 = 'N168CA' AND deregistration_id = 'N168CA-2001-03-01' 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 COMA9910079Sign · brokenEXIT SIGN DETACHED AT SEAT 5A. REPLACED EXIT SIGN.SDR COMA9910076Sensor · failedGEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE LANDING GEAR A SYSTEM PROX SENSOR.SDR COMA9910014Lamp · failedEMERGENCY FLOOR LIGHT AT CABIN DOOR IS INOPERABLE. REPALCED LIGHT BULB.SDR COMA9810291Fitting · failedLEFT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI, IN FLIGHT SHUT DOWN. REPLACED ELBOW FITTING THAT HAD BUCKED OUT ON THE OIL PUMP COVER.SDR COMA9810284Support · crackedRIGHT WING SKIN SUPPORT NR 37 AT RIB NR 9 CRACKED. REPLACED SKIN SUPPORT.SDR COMA9810283Support · crackedRIGHT WING SKIN SUPPORT NR 30 AT RIB 6 CRACKED. REPLACED SKIN SUPPORT.SDR COMA9810280Stringer · crackedRIGHT WING STRINGER NR 10 CRACKED BETWEEN RIBS NR 7 AND NR 8. REPAIRED WITH TWO PIECE DOUBLER.SDR COMA9810279Support · crackedWING SKIN SUPPORT CRACKED. REPLACED SKIN SUPPORT.SDR COMA9810281Support · brokenDURING FUEL LEAK REPAIR, FOUND SKIN SUPPORT BROKEN IN THE RIGHT WING, RIB 16, BOTTOM CENTER. REPLACED SKIN SUPPORT.SDR COMA9810273Window Post · crackedFOUND CRACK ON POST BETWEEN PILOTS WINDSHIELD AND DV WINDOW. INSTALLED DOUBLER ON WINDOW POST IAW EMB EST-474/95 DATE 01NOV95.SDR COMA9810226Sign · brokenEXIT SIGN ROW 5 IS BROKEN. REPLACED EXIT SIGN.SDR COMA9810189Connector · looseEAD1 AND EHS1 TUBES FAILED DURING TAKEOFF. REPAIRED LOOSE WIRE CONNECTION AT CIRCUIT BREAKER CB0256.SDR COMA9810190Deice Indication · malfunctionedABNORMAL DEICE, F/O FCP AND FO EFIS TUBE INDICATIONS DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE.SDR COMA9810184Relay Box · malfunctionLANDING GEAR DID NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX.SDR COMA9810114Battery · dischargedEMERGENCY FLOOR PATH LIGHTING VERY DIM. REPLACED EMERGENCY BATTERY.SDR COMA9810053Battery · dischargedCABIN DOOR EMERGENCY EXIT SIGN IS INOPERABLE, EMERGENCY FLOOR PATH LIGHTING TO ROW 3 IS INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY.SDR COMA9710398Tee Section · corrodedDURING 2C INSPECTION, TASK REVEALED CORROSION ON FLOOR T-SECTION THAT WAS OUT OF LIMITS. REMOVED CORRODED FLOOR T-SECTION AND INSTALLED SERVICEABLE T-SECTION USING EMB SRM STANDARD PRACTICES.SDR COMA9710400Support · corrodedDURING 2C INSPECTION, TASK 5310-132-01I REVEALED LAV SUPPORT ASSY TO BE HEAVILY CORRODED. REMOVED CORRODED LAV SUPPORT AND INSTALLED SERVICEABLE SUPPORT AS PER EMB 120 MAINTENANCE MANUAL.SDR COMA9710399Sill · corrodedDURING 2C INSPECTION, TASK REVEALED RIGHT CARGO FLOOR SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES.SDR COMA9710397Tee Section · corrodedDURING 2C INSPECTION, TASK REVEALED FLOOR T-SECTION AT FRAME 28 TO BE CORRODED. REMOVED T-SECTION AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES.SDR COMA9710396Crossbeam · corrodedDURING 2C INSPECTION, TASK REVEALED LEFT FLOOR CROSSBEAM TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE PART USING EMB-SRM STANDARD PRACTICES.SDR COMA9710395Crossbeam · corrodedDURING 2C INSPECTION, TASK REVEALED RIGHT MIDDLE FLOOR CROSSBEAM AT FRAME 23 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB SRM STANDARD PRACTICES.SDR COMA9710394Sill · corrodedDURING 2C INSPECTION, TASK 5310-131-01I REVEALED CORROSION ON FLOOR SILL THAT IS BEHIND GALLEY. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES.SDR COMA9710225Wire · chafedLEFTHAND BLEED AIR DUCT WARNING CAME ON DURING BOARDING. REPAIRED DAMAGED WIRE AT CENTER WING BLEED LEAK DETECTOR.SDR COMA9710094Windshield · crackedCAPTAIN'S WINDSHIELD CRACKED IN LOWER LEFT CORNER. REPLACED CAPTAIN'S WINDSHIELD.SDR COMA9710090Tire · failedRT INBOARD MAIN TIRE BLEW ON LANDING ROLL ANTI-SKID WARNING SOUNDED. REPLACED RT BRAKE CONTROL VALVE AND RT INBOARD WHEEL AND TIRE ASSY.SDR COMA9610388Skin · crackedDURING 20K LANDING INSPECTION, FOUND ONE FASTENER HOLE CRACK INDICATION ON LEFT WING UPPER SKIN AT RIB NR 11. HOLE WAS REPAIRED PER EMBRAER DOCUMENT EST431/96.SDR COMA9610387Sill · corrodedINSPECTION REVEALED SEVERE CORROSION ON THE FUSELAGE RIGHT AFT EMERGENCY EXIT CUTOUT LOWER SILL. THE SILL WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES CHAPTER 51.SDR COMA9610386Skin · misdrilledDURING COMPLIANCE OF S/B 120-57-0031, ONE FASTENER HOLE IN THE LEFT WING UPPER SKIN WAS MISDRILLED AT RIB 18. THE HOLE WAS REPAIRED PER EMBRAER DOCUMENT EST 430/96.SDR COMA9610385Bracket · crackedINSPECTION REVEALED THE LEFT FWD FUSELAGE SKIN SUPPORT BRACKET, AT FRAME 9 TO BE CRACKED. THE BRACKET WAS REPLACED PER AERODESIGN REPORT 660-1.SDR COMA9610384Butt Strap · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT LT BUTT STRAP TO BE CORRODED. THE BUTT STRAP WAS REPLACED PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610383Butt Strap · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT CENTER BUTT STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610382Butt Strap · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT RT BUTT STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610381Sill · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT RT SILL CORRODED. THE RT SILL WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610380Support · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT T-SECTION, AT FRAME 16 CORRODED. THE T-SECTION WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610379Stringer · corrodedINSPECTION REVEALED THE FUSELAGE FWD SECTION OF STRINGER 18L CORRODED. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-A, REV IR, DATED 11-6-96.SDR COMA9610378Skin · corrodedINSPECTION REVEALED THE LOWER FUSELAGE SKIN CORRODED BENEATH THE NR 2 COM ANTENNA. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 2089-1 REV IR, DATED 11-7-96.SDR COMA9610377Support · corrodedINSPECTION REVEALED THE FUSELAGE FWD LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB 120 SRM PRACTICES, CHAPTER 51.SDR COMA9610376Support · corrodedINSPECTION REVEALED THE FUSELAGE CENTER SECTION LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610374Support · corrodedINSPECTION REVEALED THE FUSELAGE CENTER SECTION AFT LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610373Crossbeam · corrodedINSPECTION REVEALED THE FUSELAGE FLOOR SUPPORT CROSSBEAM AT FRAME 16 CORRODED. THE CROSSBEAM WAS REPLACED WITH A NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610372Butt Strap · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT CENTER BUTT-STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.SDR COMA9610371Support · looseINSPECTION REVEALED THE AFT RIGHT EMERGENCY EXIT MECHANISM BELLCRANK SUPPORT MOUNTING RIVETS, THROUGH DOOR SKIN TO BE LOOSE CAUSING EXCESSIVE PLAY IN THE DOOR OPENING MECHANISM. THE RIVETS WERE REPLACED PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51, NO OTHER SDR COMA9610370Skin · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING LOWER SKIN NR 2 LEFT AND RIGHT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR COMA9610369Skin · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING LOWER SKIN NR 1 LEFT AND RIGHT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR COMA9610368Rib · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING RIB NR 1, CL RIB DAMAGED. REMOVED AND REPLACED IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR COMA9610367Spar Cap · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR CAPS, LOWER LT AND RT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR COMA9610366Spar Web · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR WEB LT AND RT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR COMA9610365Aux Spar Cap · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING AUXILIARY SPAR CAPS, LOWER LT AND RT DAMAGED. PERFORMED REPAIR IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR COMA9610364Aux Spar Web · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING AUXILIARY SPAR WEB LT AND RT DAMAGED. PERFORMED REPAIR IAW EMBRAER ENGINEERING DRAWING 120-44623.
Back to N168CA, cancelled Mar 1, 2001