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 aircraft_model_key = '7772Q8' 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 aircraft_model_key = '7772Q8' 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 ASMF201007006Wheel · damagedDURING PUSH BACK THE TOW FITTING WAS BROKEN. MX PERFORMED GENERAL VISUAL INSP TO THE NLG IAW MM 05-51-01 DETECTING DAMAGE OUT OF LIMIT IN THE RT NOSE LANDING WHEEL. TECH REPLACED BOTH NOSE LANDING WHEELS IAW MM 32-45-02, TESTED CORRECT.SDR ASMF201008004Skin · damagedDURING TRANSIT CHECK WAS DETECTED A LIGHTNING STRIKE IN THE FUSELAGE SKIN. MX PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-51-19 DETECTING RIVETS WITH HEAD BURNED IN FUSELAGE SKIN STA 220.5 BETWEEN LT STR 14-15 AND STA 239 THROUGH 382. THE NON ROUTINE CARDS A01SDR ASMF201006004Flap System · malfunctionedACFT REJECTED TAKEOFF AT 65 KNOTS, DURING TAKEOFF ACCELERATION A FLAP CONFIGURATION ALARM WITH RED ANNOUNCEMENT TURNED ON. MX PERSONNEL VERIFIED FOR FAILURE DETECTING 27-20272 AND 27-20722 FAILURE CODES IN THE FSEU NR 2, PREVIOUSLY DEFERRED AND THE FSEU NR 1 SDR ASMF201006002Seal · out of positionACFT RETURNED TO DEPARTURE, DURING CLIMB WAS DETECTED A LOAD COMPARTMENT PRESSURIZATION LEAK NOISE. MX FOUND THE FWD ACCESS ELEC DOOR SEAL, UPSIDE DOWN, THE DOOR SEAL WAS REPOSITIONED IAW MM 52-08-00 AND PRESSURIZATION TEST WAS PERFORMED IAW MM 52-00-05, TESTESDR ASMF20100405Compressor · damagedDURING A BORESCOPE INSP OF THE HPC AND HPT MODULES OF RT ENGINE WERE DETECTED 41 BLADES OF HPC 8TH STAGE AND 23 BLADES OF 9TH STAGE WITH TEARS, NICKS, BENDS AND MISSING MATERIAL FROM THE LEADING TO THE T/E. OPENSDR ASMF201004002Blades · damagedDURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENGINE WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGISDR ASMF20100321001Blade · damagedDURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENG WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGINE SDR ASMF200911001Brake Assy · leakingDURING TRANSIT CHECK, A HYD LEAK WAS DETECTED ON THE RT MLG BRAKE NR 8. MX REPLACED THE BRAKE ASSY NR 8 IAW MM 32-45-07, TESTED CORRECT.SDR ASMF20090704Skin · damagedDURING OVERNIGHT CHECK SEVERAL LIGHTNING STRIKES IN FUSELAGE SKIN BS 340.5 / S39L; STA368.5 / S39L; STA 410.5 / S-40L; STA411.5 / S-39L; STA 421.5 / S-39L; STA 453.5 / S-40L; STA 472.5 / S-38L; STA 519 / S-39L; STA 535.5 / S-39L; STA 599.5 / S-38L WERE DETECTESDR ASMF 20081201Tire · separatedDURING TAKE OFF, CAPTAIN REPORTED STRONG VIBRATION IN MLG. MX PERSONNEL DETECTED TREAD LOSS IN THE WHEEL POSITION NR 1 IN THE LT MLG, CRACK IN THE LT FLAP LOWER SKIN AT STA 261 AND A DENT OF 8 IN LONG X 4 IN WIDTH 0.200” DEPTH IN THE LOWER ACCESS PANEL 511JB SDR ASM2008F00005Hose · damagedDURING TRANSIT CHECK, MAINT DETECTED DAMAGE AND HYDRAULIC LEAK ON SUPPLY HOSE ASSEMBLY TO RT ENGINE EDP. THE HOSE ASSY, PN AE70970110 WAS REMOVED AND REPLACED AND PERFORMED LEAK CHECK IAW AMM 29-11-05, NO LEAKS WERE FOUND. (K)SDR MAS2008F00062Thrust Reverser · damagedDURING TRANSIT CHECK WAS DETECTED THE OUTBOARD REVERSER OF THE RT ENGINE WITH EXTENDED DAMAGE ON FAN DUCT INNER WALL WITH MATERIAL MISSING OF 70 X 60 INCH BY IMPACT OF THE BOROSCOPE L PLUG, THE ACFT WAS SENT TO HANGAR FOR REVERSER REPLACEMENT WHICH WILL BE SENSDR ASM2008F00000Warning System · malfunctionedACFT REJECTED TAKEOFF AT 80 KNOTS DUE TO THE E/E COMPARTMENT LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED DOOR LIGHT TEST IAW MM 62-71-00, ALL CORRECT. THE HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-51-14, ALL CORRECT. (S)SDR ASM2008F00001Blade · bentDURING TRANSIT CHECK, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPIC INSPECTION DETECTING BLADES TIP BENDED IN THE FIRST STAGE OF HIGH PRESSURE COMPRESSOR ROTABLE SECTION AND A IGV SCRATCHED IN THE RT ENG, OUT OF LIMITS IAW MM 72-00-00. THE RT ENG WAS REPLASDR 2008FA0000472Engine · failedDURING TRANSIT CHECK, THE RT ENGINE WAS DETECTED WITH DAMAGES. MAINT PERFORMED BOROSCOPIC INSPECTION, DETECTING DAMAGES OUT OF LIMITS, SO RT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02 AND 71-00-00, ALL CORRECT. (K)SDR 2008FA0000471Sensor · failedAC RETURNED TO DEPARTURE DUT TO RT ENGINE STALLED. MAINT PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES. NO DAMAGES WERE DETECTED IAW MM 71-00-00. RT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED CORRECT. THE OVERWEIGHTSDR ASMF200806001Sensor · failedAIRCRAFT RETURNED OF FLIGHT DUE TO RIGHT ENGINE STALLED. MAINTENANCE PERSONNEL PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES, NO DAMAGES WERE DETECTED IAW MM 71-00-00. RIGHT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED
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