N952CA
Service difficulty reports · 268
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 = 'N952CA' AND registry_match = 'registration' 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 = 'N952CA' AND registry_match = 'registration' 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 U2RA201403170002Liner · crackedON POST FLIGHT INSPECTION, FOUND CRACK ON NR 4 ENGINE EXHAUST NOZZLE INNER LINER AFT RING WELD AT 1 O'CLOCK POSITION.SDR U2RA201403170001Liner · crackedON POST FLIGHT INSPECTION, FOUND CRACK ON NR 2 ENGINE EXHAUST INNER LINER AFT RING WELD AT 7 O'CLOCK POSITION.SDR U2RA201402070001Smoke Detector · failedMAIN DECK CARGO FIRE ALARM ACTIVATED DURING CRUISE. CREW CHECKED AND NO INDICATION OF FIRE OBSERVED. TROUBLESHOT SYSTEM IAW FIM 26-16 AND FOUND DETECTORS 10, 11, 12, 14, 16 ON LOOP "B" FAILED.SDR U2RA201312120001Skin · wornLEFT OTBD AFT FLAP PANEL 588 EXTERNAL SKIN HAS SEVERAL AREAS OF WEAR OUT OF LIMITS. NO CORROSION OR CRACKS FOUND. REPAIRED IAW DWG 5750D1751, REV IR DTD.SDR U2RA201311200001Battery Pack · dischargedLEFT UPPER DECK DOOR EMERGENCY OPENING SYSTEM DOES NOT TEST.SDR U2RA201306020001Bulb · inoperativeUPPER DECK EMERGENCY LIGHT OPS TEST FOUND FOUR BULBS INOPERATIVE.SDR U2RA201306020002Skin · crackedLT WING L/E UPPER FIXED PANEL FOUND CRACKED BETWEEN WING STATIONS 730 TO 862. CRACK LENGTH 38" REF NRCMOL0209. GENERATED FROM TASK CARD 57-806-01-01.SDR U2RA201306010002Structure · crackedLEFT WING L/E CAVITY LOWER FIXED PANEL AT WS 850 FOUND STRUCTURE CRACKED. CRACK IS 1.5" IN LENGTH.SDR U2RA201306010001Support · crackedLEFT WING LEADING EDGE CAVITY AT WING STATION 780 FOUND SUPPORT ROD FRACTURED, REF NRC MOL0217 GENERATED FROM TASK 57-804-01-01.SDR U2RA201302140001Bolt · backed outGEAR DISAGREE AND GEAR DOOR EICAS RT BODY GEAR UNSAFE INDICATION ON LANDING. ALTERNATE GEAR EXTENSION METHOD PERFORMED AND ALL LIGHTS GREEEN. FOUND MLG DOOR SEQUENCE VALVE CARRIER BOLT FALLEN OUT. NUT MISSING. REPLACED HARDWARE WITH NEW LOCKING NUT.SDR U2RA2012120387201Engine · power lossREJECTED TAKEOFF AT 80KTS - NR 3 ENG N1 ROLLED BACK.SDR 2012F00261Ecu · failedAT APPROX 65 KNOTS, NR 3 ENGINE FAILED. N1 WAS APPROX 100 PERCENT. COMPLETED FAULT ISOLATION IAW FIM 71-00, FIG 114. R & R NR 3 ENGINE ECU IAW AMM 73-21-15, ALSO R & R NR 3 ENGINE HMU IAW AMM 73-21-14. ALL OPS CHECK NORMAL IAW AMM 73-21-15 AND 73-21-14.SDR 2012F00262Ecu · failedAT APPROX 65 KNOTS, NR 3 ENGINE FAILED. N1 WAS ABOVE 100 PERCENT. COMPLETED FAULT ISOLATION IAW FIM 71-00, FIG 114. R & R NR 3 ENGINE ECU IAW AMM 73-21-15, ALSO R & R NR 3 ENGINE HMU IAW AMM 73-21-14. ALL OPS CHECK NORMAL IAW AMM 73-21-15 AND 73-21-14.SDR U2RA20121128001Engine · failedAT APPROX 65KTS, NR 3 ENGINE FAILED. N1 WAS APPROX 100 PERCENT.SDR 2012F00264Apu · malfunctionedAIR PORTION OF THE APU FAILED WITH APU ELECTRONICS OPERATIONAL. COMPLETED FIM 49-11 TASK 827 WITH NO FAULTS NOTED. STARTED APU, ALL OPS CHECKED GOOD.SDR 3POR201204300003Structure · misrepairedINCORRECT REPAIR, INCORRECT FASTENERS.SDR 3POR201204300002Skin · misrepairedINCORRECT REPAIR OF FUSEALAGE SKIN DAMAGE.SDR 3POR201204290001Skin · misrepairedAFT FUSELAGE SKIN, BS 1795, S48L, MISREPAIRED
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