N258CA, cancelled Dec 3, 2012
Service difficulty reports · 93
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 = 'N258CA' AND deregistration_id = 'N258CA-2012-12-03' 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 = 'N258CA' AND deregistration_id = 'N258CA-2012-12-03' 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 COMA0110030Channel · crackedDURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE CHANNEL, THIRD FROM BOTTOM, WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA0110029Channel · crackedDURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE LOWER CHANNEL WAS FOUND TO BE CRACKED AT BOTH ENDS. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA0110028Control Cable · wornDURING 1C CHECK TASK 27-62, THE RIGHT SIDE OUTBOARD RUDDER CONTROL CABLE WAS FOUND TO BE WORN WHERE IT PASSES THROUGH THE WING BOX FAIRLEADS. THE CABLE WAS REPLACED PER THE AMM.SDR COMA0110027Channel · crackedDURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE U-CHANNEL WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA0110026Angle · crackedDURING 1C CHECK TASK 194-01Z, THE RIGHT OVERWING FAIRING ATTACH ANGLE ON TOP OF THE WING WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT 1226-21, REV IR, 7/6/99.SDR COMA0110006Landing Gear · lack of lubeRT MLG INDICATED UNSAFE. CLEANED AND LUBRICATED LANDING GEAR.SDR COMA0010373Battery · dischargedSEVERAL EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.SDR COMA0010315Pickup · out of adjRIGHT HAND ENGINE NP OSCILLATING 99 T 102.8 PERCENT. ADJUSTED PROP SYNC. PULSE PICKUP GAPS TO M/M SPECIFICATIONS.SDR COMA0010300Tire · dischargedRIGHT HAND MLG TIRE LOW PRESSURE. REPLACED WHEEL TIRE ASSY.SDR COMA0010106Lever · malfunctionedLEFT ENGINE POWER LEVER ADVANCED CAUSING OVER TORQUE AND OVER TEMP. DOWN LOADED DFDR AND FOUND TORQUE AND TEMP EXCEEDENCE TO BE WITHIN M/M LIMITATIONS.SDR COMA0010105Door · not closedSERVICE DOOR WARNING. FOUND FUEL SERVICE DOOR NOT SECURE. LATCHED DOOR AND AIRCRAFT RETURNED TO SERVICE.SDR COMA0010104Warning Light · illuminatedRIGHT MLG DISAGREE INDICATION DURING EXTENSION. CLEANED AND LUBRICATED LANDING GEAR. A/C RETURNED TO SERVICE.SDR COMA0010103Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5400-432-01I, THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR COMA0010102Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-01I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGE PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR COMA0010101Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR COMA0010100Fitting · misdrilledUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT WING FRONT OUTBOARD MAIN LANDING GEAR FITTING WAS FOUND TO BE MISDRILLED FROM PREVIOUS REPAIR. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR SDR COMA0010099Stringer · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3656-1-REV IR, 5-10-00.SDR COMA0010098Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3364-1, REV IR, 7-25-99.SDR COMA0010097Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-141/142-01I, THE FUSELAGE SKIN SUPPORT AT FRAME 21, BETWEEN STRINGERS 21L AND 21R, WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010096Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 163-01Z, THE LT AFT FUSELAGE BUTT STRAP (SILL) WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010095Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 162-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010094Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010093Support Bracket · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 242-01Z, THE RT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010092Support Bracket · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 232-01Z, THE RT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010091Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FUSELAGE FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010090Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE FUSLAGE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010089Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010088Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010087Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010086Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE RT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010085Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 142-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010083Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 142-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010082Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RT FWD FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010081Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010080Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL MANUAL STANDARD PRACTICES.SDR COMA0010079Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010078Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LT FWD FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010077Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 232-01Z , THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A AND STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3653-1, REV IR, SDR COMA0010076Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 222-01Z, THE RT FUSELAGE SKIN SUPPORT AT FRAME 9 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, REV IR, 2-16-93.SDR COMA0010075Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LT COCKPIT FLOOR SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR EST-145-/96.SDR COMA0010074Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 231-01Z, WHILE GAINING ACCESS THE LT COCKPIT SKIN SUPPORT BRACKET BEHIND TO DV WINDOW FRAME WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010073Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE RT COCKPIT FLOOR SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR EST-145/96.SDR COMA0010072Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-02I, THE RT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-13, REV IR, 2-SDR COMA0010071Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-02I, THE LT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-13 REV IR, 2-7SDR COMA0010070Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 25-12, WHILE ACQUIRING ACCESS THE CARGO DOOR TORSION BAR FWD SUPPORT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1397-1, SDR COMA0010069Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 261-01Z, THE FUSELAGE SKIN SUPPORT BRACKET AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010068Skin · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 813-022, THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 52-30-01 PG 201-204.SDR COMA0010045Selector Knob · contaminatedFLAPS FAILED AT 25 DEGREES WHEN SELECTED TO 45 DEGREES FOR LANDING. REMOVED DEBRIS FROM FLAP SELECTOR FLAP, OPERATION NORMAL.SDR COMA0010036Sensor · malfunctionedNLG WOULD NOT RETRACT. REPLACED THE NLG DOWN LOCK SWITCH.SDR COMA9910188Sign · inoperativeEXIT SIGN AT ROW 5 WAS INOPERATIVE. REPLACED EXIT SIGN.
Back to N258CA, cancelled Dec 3, 2012