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 = '340B' 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 = '340B' 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 29GA2015111600001Connector · unsecureCIRCUIT BREAKER L8, EMERGENCY LIGHT, TRIPPED RESET AND TRIPPED AGAIN. FOUND LOOSE CONNECTION AT 29LN SWITCH, RESECURED, RESET CIRCUIT BREAKER L8 SYSTEM. OPERATIONAL CHECK NORMAL.SDR 29GA2015111200001Sign · detachedCABIN DOOR EXIT SIGN UNATTACHED. REATTACHED FORWARD EXIT SIGN.SDR S9BA20150016Computer · faultedRIGHT HOT PIPE LIGHT CAME ON AFTER TAKEOFF 2,000 FT. R & R WARNING ELECTRONIC COMPUTER.SDR 29GA2015110900001Brake Sys · unresponsiveON TAXI-IN AFTER LANDING, APPLY BRAKES WITH NO RESPONSE. TURN ANTI-SKID SWITCH OFF AND BRAKES WORK. BLED ALL BRAKES AND PERFORMED OPS CHECK OF BRAKES WITH ANTI-SKID ON AND OFF SYSTEM OPS CHECKS GOOD.SDR 29GA2015110900002Light · unsecureFORWARD EMERGENCY LIGHTING ON LT SIDE BECAME UNATTACHED. RESECURED EMERGENCY LIGHTING SECTION 2J-M.SDR PNSA2015103004Duct · failedLEFT INTAKE LIGHT ON. R & R LOWER INLET DUCT.SDR 29GA2015112800001Transducer · inoperativeSUP: DURING THE TAXI INTO THE GATE, BOTH CAPTAIN AND F/O LOST FULL BRAKING AUTHORITY. INSPECTED FOUND NR 1 ANTI-SKID TRANSDUCER INOPERATIVE. ALSO, FOUND EXCESSIVE AIR IN BRAKE SYSTEM. R & R NR 1 ANTI-SKID TRANSDUCER IAW 32-43-15-04 MM. ALSO, BLED THE BRAKSDR PNSA2015102805Power Supply · failedEMERGENCY POWER SUPPLY FAILED A 12 MONTH INSPECTION, R & R THE POWER SUPPLY.SDR 29GA2015102900001Brake Sys · failedDURING THE TAXI INTO THE GATE BOTH CAPTAIN AND F/O LOST FULL BRAKING AUTHORITY.SDR 29GA2015102800005Valve · malfunctionedFLIGHT 100, BRAKES WORK INTERMITTENTLY. BRAKES MUSHY AT TIMES. AT TIMES THERE IS ZERO BRAKING ACTION. R & R BRAKE VALVE. OPS CHECK/ LEAK CHECK GOOD.SDR 29GA2015102800004Brake Sys · inoperativeBRAKES NOT WORKING PROPERLY DURING TAXI. BLED ALL 4 MAIN BRAKES. OPS CHECK GOOD IAW AMM 32-42-40.SDR 29GA2015102800003Sign · detachedEMERGENCY EXIT SIGN FELL OFF DURING FLIGHT OVER EXIT DOOR 2A. R & R EMERGENCY EXIT SIGN AT EXIT DOOR 2A IAW CMM REF 25-25-15-5. OPS CHECK OK.SDR 29GA2015102800001Brake Sys · malfunctionedFLIGHT 9002: BRAKE AUTHORITY IS INTERMITTENT. PERFORMED OPS CHECK OF THE ACFT BRAKE SYSTEM IAW AMM 32-42-40-05. CHECK GOOD.SDR 29GA2015102800002Control Box · malfunctionedFLIGHT 81: ON TAXI USING BRAKES, PLANE IS VERY HARD TO STOP. HAVING TO PRESS FULL BRAKES AND REVERSE TO STOP ACFT. R & R ANTI-SKID CONTROL BOX IAW AMM 32-43-05-04. PERFORMED OPS CHECK, OPS CHECK IS SATISFACTORY.SDR 29GA2015102400001Flap System · out of rigFLIGHT 108: AT T/O NOSE TRYING TO LIFT OFF WELL BEFORE ROTATION SPEED. THEN NOTICED TRIM WAS .5 TO .7500 NOSE DOWN ON THE TRIM INDICATOR IN LEVEL FLIGHT, TO HOLD A NORMAL APPROACH/LANDING CONFIGURATION, TRIM INDICATED .7500 TO 1 UNIT NOSE DOWN BELOW GREEN ARC,SDR 29GA2015112800002Actuator · leaking"SUP: LOST BRAKES AROUND 100 FT FROM RUNWAY. NEVER REGAINED BRAKING. USE OF GROUND FINE & REVERSE WAS USED TO STOP. PULLED FIRE HANDLES TO SHUTOFF FUEL WHILE ACFT WAS ROLLING. AFTER ACFT WAS ABLE TO STOP, WE THEN HAD TIME TO CHECK THE ANTI-SKID BY TURNING SDR 29GA2015102200001Brake Sys · failedLOST BRAKES AROUND 100 FEET FROM RUNWAY. NEVER REGAINED BRAKING. USE OF GROUND FINE & REVERSE WAS USED TO STOP. PULLED FIRE HANDLES TO SHUTOFF FUEL WHILE ACFT WAS ROLLING. AFTER ACFT WAS ABLE TO STOP.SDR 29GA2015102100004Pump · malfunctionedHYDRAULIC PUMP DOES NOT TURN ON DURING TAXI, TURNING, AND BRAKING. SITS AT 2000 PSI. HARD TO TAXI. SERVICED HYD SYSTEM IAW AMM 12-10-29, AND BLEEDED BRAKES IAW AMM 32-42-00-02.SDR 29GA2015102100002Brake · malfunctionedUNABLE TO STOP ACFT OR HAVE BRAKE EFFECTIVENESS UNTIL TURNING ANTI-SKID SWITCH TO OFF. LOUD POP WAS HEARD AND BRAKES WERE NORMAL AFTER THAT. R & R NR 2 BRAKE ASSY IAW AMM 32-42-40-04 W/OPS CHECK NORMAL.SDR 29GA2015102100001Battery Pack · inoperativeFLIGHT 100: EMERGENCY LIGHTING FROM ROWS 2A TO 7A AND OVERHEAD EMERGENCY LIGHT AT 7A INOPERATIVE. R & R EMERGENCY BATTERY PACK 20LN IAW AMM 33-50-10-04-1. OPS CHECK GOOD.SDR 29GA2015101800001Seal · not reportedF/A HAD A HARD TIME OPENING AND CLOSING THE MAIN CABIN DOOR. R & R AFT LWR SEAL SEAT IAW SRM 53-70-30-208.SDR PNSA2015101602Power Supply · failedEMERGENCY LIGHTING POWER SUPPLY FAILED TEST, R & R.SDR 29GA2015101700001Seal · malfunctionedF/A SAYS CABIN DOOR IS HARD TO OPEN AND CLOSE. R & R CABIN NIPP SEAL SRM 53-70-30-208, OPS CHECKED GOOD.SDR PNSA2015101201Indicator · failedRIGHT ITT ROLLS DOWN TO ZERO INFLIGHT, BOTH ANALOG AND DIGITAL INTERMITTENT. CLEANED RT ENGINE DECU YELLOW CABLE AND AIRFRAME CONNECTORS. R & R RT ITT INDICATOR.SDR 29GA2015100700003Windshield · crackedRIGHT FRONT WINDSHIELD CRACKED. R & R RT FRONT WINDSHIELD IAW AMM 56-10-05. RT FRONT WINDSHIELD HEAT OPS CHECK NORMAL IAW 30-42-00. PAINT ON MCO, DEFECT 30264. SEALANT CURED AND SPEED TAPE REMOVED, DEFECT 30263.SDR 29GA2015100700002Brake Sys · stiffBRAKES HARD TO STOP AIRCRAFT. BRAKES VERY STIFF. BLEED BRAKE SYSTEM IAW AMM 32-42-00-02. BRAKE SYS OPS CHECK GOOD.SDR 29GA2015100700001Pump · failedDURING TAXI OUT HYD PUMP FAILED. ENGINE NR 1 SHUTDOWN WITH T-HANDLE. R & R HYDRAULIC PUMP REF AMM 29-10-10-04. OPS CHECK GOOD. NO LEAKS, FOUND AND SAFETY WIRE REPLACED ON T-HANDLE.SDR 29GA2015100500001Battery Pack · inoperativeCABIN EXIT SIGN IN ROW 7 NOT ILLUMINATING ON EMERGENCY LIGHT TEST. REPLACED SIGN EXIT LOCATOR AND EMERGENCY BATTERY PACK. EXIT SIGN PN ON/OFF 2LA006842-00.SDR 29GA2015100300001Acm · odorINFLIGHT DURING LEVELING OFF AND STARTING DECENT, STRONG SULFER ODOR BY ALL CREW. F/A NOTED HEARD NOISE WHERE ACM LOCATED. R & R NR 2 ACM IAW SILVER MM4 21-50-02/2S. PERFORMED OPS TESTS IAW AMM 21-00 00 & 21-60-00, OPS CHECKS GOOD.SDR TSAA20150929005Engine · flamed outNUMBER 2 ENG FLAMED OUT AFTER POWER LEVER WAS BROUGHT TO FLIGHT IDLE UPON LANDING. CREW TAXIED CLEAR OF RNWY & COMPLETED ALL APPLICABLE CHECKLISTS & TAXIED TO PARKING WITHOUT INCIDENT. INSPECTED NR 2 ENG FOR FUEL LEAK, BUT NO FUEL LEAK NOTED. OPERATED NR 2 SDR PNSA2015092902Indicator · erraticLEFT ITT INDICATOR ERRATIC.SDR 29GA2015092600001Control Valve · malfunctionedAFTER TAKEOFF, DURING GEAR RETRACTION, NOSEWHEEL DID NOT INITIALLY LOCK IN PLACE. IT FELT LIKE IT FAILED TO LOCK AND MOMENTARILY DROPPED. HYDRAULIC PUMP KICKED BACK IN TO RAISE NOSE WHEEL BUT AGAIN FELT LIKE IT FAILED TO LOCK AND DROPPED. AFTER ABOUT THE THISDR S9BA201509230012Windshield · crackedWHEN ENROUTE, CAPTAIN WINDSHIELD CRACKED. DECLARED EMERGENCY AND LANDED. THE WINDSHIELD WAS REPLACED.SDR PNSA2015090801Processor · failedRIGHT EFIS SCREEN BLANK, MFD SCREEN BLANK.SDR 29GA2015090800001Switch · malfunctionedIN CABIN LIGHTING PANEL EMERGENCY LIGHT, ARM PORTION OF LIGHT DOES NOT ILLUMINATE. REPLACED THE LIGHT SWITCH IAW AMM 33-50-00, OPS CHECKED NORMAL.SDR 29GA2015090200001Door · missingAT ROTATION, F/A NOTIFIED CREW OF NR 2 ENGINE MISSING INSIDE COVER. EMERGENCY DECLARED. AIR RETURN WAS NORMAL. POST INSPECTION SHOWS COWL MISSING ON NR 2 ENGINE. R & R FWD COWLINGS AND FRAMES IAW AMM 71-10-05-04.SDR PNSA2015082501Latch · unsecureNR 2 ENGINE COWLING FORWARD INBD LATCH NOT SECURED.SDR PNSA2015082402Power Supply · no testEMERGENCY LIGHTING POWER SUPPLY FAILED 6 MONTH INSPECTION.SDR 29GA2015082600001Lamp · inoperativeCABIN LIGHTING PANEL EMERGENCY LIGHT SWITCH "ARM" DOESN'T ILLUMINATE. R & R LAMP ON CABIN EMERGENCY LIGHT SWITCH IAW AMM 33-50-00, OPS CHECK NORMAL.SDR 29GA2015082100001Accumulator · low pressureMAIN HYDRAULIC ACCUMULATOR WILL NOT HOLD PRESSURE. BRAKES AND NOSE STEERING INTERMITTENT DUE TO LACK OF PRESSURE. PERFORMED OPS CHECK ON MAIN HYDRAULIC SYSTEM. NO DEFECTS FOUND. OPS CHECK NORMAL IAW AMM 29-10-00-02.SDR S9BA201508140010Skin · dentedDENT AT RT FUSELAGE UNDER 11TH CABIN WINDOW. EVALUATED DAMAGE AT FUSELAGE BS 580.0, WATERLINE 100. REPAIRED IAW SRM 53-70-10-205, FIG 203. NDT MANUAL 51-06-00. PRIMED AND PAINTED TO MATCH ACFT COLORS. NO CHANGE IN ACFT WEIGHT AND BALANCE.SDR S9BA201508140009Skin · dentedDENT ON SEAM AFT OF 9TH WINDOW RT SIDE. EVALUATED DAMAGE AT FUSELAGE BS 516. REPAIRED IAW SRM 53-70-10-205, FIG 203. NDT INSPECTED IAW NDT MANUAL 51-06-00. PRIMED AND PAINTED TO MATCH ACFT COLORS. NO CHANGE IN ACFT WEIGHT AND BALANCE.SDR 29GA2015081200002Overheat Sensor · failedRT BLEED AIR LEAK ILLUMINATED. RAN THE QRH, THE LIGHT WENT OUT THEN CAME BACK ON. WE RAN THE QRH AGAIN AND SHUT THE NR 2 ENGINE DOWN. HEAVY SOOT DEPOSITS IN DUCT AREA. LOOP INSULATOR GROMMETS ON AFT ELEMENT DRY-ROTTED. R & R RT NACELLE DUCT ASSY ELEMENT SDR 29GA2015081200001Overheat Sensor · bentRIGHT BLEED AIR LEAK ILLUMINATED. IT EXTINGUISHED AND RE-ILLUMINATED. WE RAN QRH WITH 2 RESET ATTEMPTS, THEN SHUTDOWN THE NR 2 ENGINE. ALL PARAMETERS OTHER. R & R ELEMENT SENSING OVER HEAT TUBE IAW AMM 36-23-10-02. OPS CHECK GOOD ON GROUND.SDR 29GA2015071200001Overheat Sensor · bentRT BLEED AIR LEAK ILLUMINATED. IT EXTINGUISHED AND RE-ILLUMINATED. WE RAN QRH WITH 2 RESET ATTEMPTS, THEN SHUTDOWN THE NR 2 ENGINE. ALL PARAMETERS OTHER. R & R ELEMENT SENSING OVER HEAT TUBE IAW AMM 36-23-10-02. OPS CHECK GOOD ON GROUND.SDR S9BA2015081400011Switch · bentAIRCRAFT WILL NOT TURN LEFT ON GROUND USING NOSE WHEEL STEERING. R & R STEERING SYSTEM CONTROL MICRO SWITCH AND PERFORMED OPS CHECK GOOD IAW MM 32-50-35-02.SDR 29GA2015073000002Seal · out of adjustPASSENGER DOOR DIFFICULT TO CLOSE. INSP AND FOUND PAX DOOR SEAL OUT OF ADJUSTMENT. ADJUSTMENT PAX DOOR SEAL IAW AMM 52-10-15-04. OPS CHECKED GOOD.SDR 29GA2015073000001Light · detachedEMERGENCY LIGHT STRIP ON FLOOR CAME OFF. SECURED EMERGENCY LIGHT STRIP ON FLOOR IAW 33-50-20-04. OPS CHECK GOOD.SDR S9BA201507220008Blade · damagedLEFT ENGINE STAGE 1 ROTOR BLADE MISSING MATERIAL. DAMAGE DISCOVERED VIA BORESCOPE INSPECTION. PICTURE TAKEN AND FORWARDED TO TECH SUPPORT AND THEY DETERMINE THAT ENGINE NEED TO BE REPLACE.SDR 29GA2015072300004Spring · bindingCHECK MAIN DOOR DIFFICULT TO CLOSE. REPLACED GAS SPRING ON STAIRS, OPS CHECKED GOOD.
Back to Saab 340B