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 engine_model_key = 'CF343A2' 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 engine_model_key = 'CF343A2' 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 2019FA0000302Bleed Valve · leakingDUCT AIR FLASHING LIGHT ILLUMINATED. LOOKED ON OVERHEAD PANEL AND SAW DUCT FAIL LIGHT ILLUMINATED. TURNED BOTH
14TH STAGE VALVES OFF ACCORDING TO CHECKLIST AND LIGHT STAYED ON. PULLED #2 ENGINE TO IDLE AND LIGHT DID NOT
EXTINGUISH. RETURNED #2 ENGINE TO FULLSDR J6BA2019091200000Bleed Valve · leakingDUCT AIR FLASHING LIGHT ILLUMINATED. LOOKED ON OVERHEAD PANEL AND SAW DUCT FAIL LIGHT ILLUMINATED. TURNED BOTH 14TH STAGE VALVES OFF ACCORDING TO CHECKLIST AND LIGHT STAYED ON. PULLED #2 ENGINE TO IDLE AND LIGHT DID NOT EXTINGUISH. RETURNED #2 ENGINE TO FULL PSDR WWQA20190403102Gearbox · brokenAIRCRAFT WAS IN FLIGHT WHEN LEFT ENGINE RPM ROLLED BACK AND ENGINE SHUTDOWN UN-COMMANDED, AIRCRAFT DIVERTED AND LANDED. MAINTENANCE TROUBLESHOT TO A FAULTY ACCESSORY GEARBOX WITH DAMAGED GEARS.SDR CA190402010Pitot System · contaminated(CAN) AIRPLANE DIVERTED FOR UNSCHEDULED LANDING WITH FOLLOWING ISSUE: AT FLIGHT LEVEL CRUISE AT FL370 WITH MODERATE RAIN AND BUMPINESS THE AIRSPEED OF THE LH PRIMARY FLIGHT DISPLAY (PFD) STARTED GRADUALLY DECREASING,LH 200 KTS AND RH 280 KTS. MACH TRIM DISENGASDR 2017F00074Hydraulic System · malfunctionedAFTER LANDING, AND DURING TAXI LEAVING THE RUNWAY, LOST HYDRAULIC POWER, RECEIVED A STICK SHAKER AND AURAL ALERT FOR A STALL. LOST NOSE WHEEL STEERING AND BRAKES FOR ABOUT THREE SECONDS. AFTER THE TURN ALL SYSTEMS NORMAL.SDR 2017FA0000108Tire · failedWHEN ACFT DEPARTED, THE NR 2 TIRE TREAD SEPARATION, SIDEWALL OF THE TIRE. THE CREW DID NOT FEEL OR HEAR ANYTHING. TIRE DAMAGE FOUND ON POST FLIGHT INSPECTION.SDR CA151111001Bolt · failed(CAN) DURING PRE-FLIGHT, FOUND ONE BOLT SHEARED ON NUMBER 3 MAIN WHEEL. AFTER INVESTIGATION IT WAS FOUND THAT THE WHEEL HAD LAST BEEN OVERHAULED AND NO BOLT WERE REPLACED. NDT HAD NOT REVEALED ANY PROBLEMS WITH THE WHEEL BOLTS. NO HEAVY LANDING OR OTHER STRESSSDR CA151002001Line · leaking(CAN) IN FLIGHT, LH HYDRAULIC ENGINE PUMP FAIL LIGHT CAME ON - PRESSURE 0 PSI AT NR 1 HYDRAULIC SYSTEM, AS REPORTED BY CREW. ON GROUND, FOUND EVIDENCE OF HYDRAULIC FLUID COMING FROM LH PYLON AND INSIDE AFT COMPARTMENT. FURTHER INVESTIGATION SHOWED LH HYDRAULICSDR CA150820012Transceiver · failed(CAN) WEATHER RADAR TRANSCEIVER FAILED DURING CRUISE. WEATHER RADAR WAS INOPERATIVE.SDR 2013FA0000766Tire · failedAFTER LANDING, THE CREW FOUND THAT THE NR 1 MLG TIRE HAD LOST MOST OF THE TIRE TREAD. THE TIRE ONLY HAD 101 LANDING ON IT WITH .0937 TREAD REMAINING.SDR CA131121013Tire · damaged(CAN) ON CREW WALK AROUND, FOUND TIRE WITH PARTIAL TREAD LOSS.SDR CA130916007Fitting · leaking(CAN) FITTING, PN MS 21926-6D IN MLG RUN AROUND AND DUMP VALVE STARTED TO LEAK DURING GEAR SWINGS DUE TO GEAR REPLACEMENT. FITTING WAS REMOVED AND INSPECTED. A CRACK WAS FOUND RUNNING PERPENDICULAR TO THE THREADS STARTING AT THE BASE OF THE FITTING. THE CRACKSDR CA130114012Tie Bolt · sheared(CAN) DURING WALK AROUND INSPECTION, NOTICED NR 3 MAIN WHEEL ASSY MISSING TIE BOLT. REMOVED WHEEL AND FOUND THE BOLT HAD SHEARED LEAVING THE HEAD AND WASHER BETWEEN THE WHEEL ASSY AND BRAKE ASSY. NO DAMAGE TO BRAKE ASSY, WHEEL ASSY SENT FOR REPAIR/TIRE CHANGESDR 2012FA0000545Tire · wornAFTER LANDING, CREW FOUND THAT THE NR 2 MLG TIRE HAD LOST MOST OF THE TIRE TREAD. THE TIRE ONLY HAD 131 LANDINGS, WITH .1562 TREAD REMAINING.SDR CA110908001Engine · malfunctioned(CAN) AFTER DEPARTURE, THE ACFT WAS CLIMBING THROUGH, APPROX 20,000- 21,000 FEET, WHEN THE CREW NOTICED THE RT ENGINE, "RED LOW OIL PRESSURE LIGHT", ON, AS WELL AS THE CORRESPONDING OIL PRESSURE GAGE READING ZERO. ALL OTHER ENGINE PARAMETERS WERE INDICATING NSDR CA110803015Engine · inoperative(CAN) THEY WERE AT CRUISE ALTITUDE WHEN THE CAPTAIN NOTICED THE LT ENGINE OIL PRESSURE WAS ON THE RISE AND REACHING THE YELLOW BAND. HE PULLED THE POWER BACK A BIT AND NOTICED THE PRESSURE CAME DOWN. HE CONTINUED TO PULL THE POWER BACK AND STILL REMAIN ABOVESDR CA110106010Actuator · wornDURING AN APPROACH AT QB, THE CAPTAIN DURING THE DESCENT TRIED TO SET THE FLAPS DOWN AND HE HAD FLAP FAIL AT 15 DEGREES (JAM), CALLED THE TOWER FOR EMERGENCY LANDING AND LANDED SAFELY THE AME FOUND THE RT INBD FLAP ACTUATOR LOOSE AND REPLACED. NOTE HAD FLAP FASDR 2012FA0000557Tire · wornAFTER LANDING, THE CREW FOUND THAT THE NR3 MLG TIRE HAD LOST MOST OF THE TIRE TREAD. THE TIRE HAD 115 LANDING ON IT WITH .1562 TREAD REMAINING.SDR 2012FA0000556Tire · wornAFTER LANDING, CREW FOUND THA THE NR 2 MLG TIRE HAD LOST MOST OF THE TIRE TREAD. TIRE HAD 113 LANDINGS WITH .1562 TREAD REMAINING.SDR CA081017005Line · burst(CAN) AFTER TAKEOFF IN CRUISE AND ON THE WAY NR 2 HYD PRESS LOST MASTER CAUTION ON REPORT BY THE CAPTAIN, HE STILL HAD HIS NR 1 AND NR 3 HYD SYSTEM. ACFT LANDED SAFELY WITHOUT ANY EMERGENCY REQUEST. NR 2 ENGINE HYD PUMP OUTLET LINE FOUND BUSTED, LINE REPLACED.SDR CA080813003Hydraulic Line · burst(CAN) IN FLIGHT NR 2 HYDR "LO PRESS" CAME ON, FWD BY "LO LEVEL". NR 2 HYDR FLUID COMPLETLY LOST THROUGH A BURST HYDR PRESSURE HOSE IN RT NACELLE.SDR CA080225005Shaft · broken(CAN) 3 MINUTES AFTER TAKEOFF, GENERATOR FAILED, AC RETURNED TO BASE. GENERATOR REMOVED, FOUND BROKEN SHAFT INSIDE THE IDG (NOT THE MAIN SHAFT). IT BROKE, MELTED THE COVER AND CAME OUT (TC NR 20080225005)SDR CA080304001Computer · faulty(CAN) IT TOOK (3) STALL WARNING COMPUTER BEFORE GETTING ONE THAT WAS SERVICEABLE , THEY ALL FAIL THE TEST IAW TEST PROCEDURE MM PSP601-2 CHAP 27-39-00 P 206 207 NB MFG PRODUCTS (TC NR 20080304001).SDR CA071022001Tube · cracked(CAN) DURING POWER PLANT BUILD UP, FOUND LINE P/N 228-52402-115 FOR PYLON STATIC PRESSURE TO FCU CRACKED AT MIDDLE. THE CRACK WAS HIDDEN BY A LINE IDENTIFICATION DECAL. LINE WAS REMOVED AND REPLACED AIRCRAFT WILL BE RETURNED TO SERVICE. (TC NR 20071022001)
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