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 = '200' 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 = '200' 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 DXTA2010111804309Landing Gear · malfunctionedNOSE GEAR WOULD NOT RETRACT. PERFORMED VISUAL INSPECTION OF ALL NLG COMPONENTS FOR LEAKING , LOOSE OR UNSERVICEABLE PARTS ,NO DEFECTS NOTED. CLEANED AND LUBRICATED NLG WITH PROPER GREASE, ALL WORK DONE IAW MM 12-22-00. HOOKED UP EXTERNAL HYD SERVICE MULE ANDSDR DXTA2010110804293Flap System · malfunctionedON PREFLIGHT, FLAPS VISUALLY APPEARED TO MOVE FREELY BUT FLAP INDICATOR HESITATED AT 12 & 20 DEGREE POSITIONS. AT 12000', STRAIGHT & LEVEL, SLATS, KRUEGERS & FLAPS ALL WORKED PROPERLY. AT 12000', LEVEL BUT TURNING, SELECTED FLAPS 12 & GOT "SLAT/FLAP MX" EICSDR DXTA2010110804298Ecu · malfunctionedWHILE CRUISING AT FL230 WE GOT A "GEAR NOT DOWN" CAS MESSAGE ALONG WITH THE GEAR WARNING HORN AND THE RT PFD AIRSPEED INDICATOR TURNED RED. RECEIVED ALL NORMAL INDICATIONS ONCE GEAR WAS DOWN & LOCKED. TROUBLESHOT TO A BAD FLAP/SLAT ECU. REPLACED WITH AN INSSDR DXTA2010101804264Brake Assy · wornEVEN PRESSURE BRAKING CAUSES ACFT TO AGGRESSIVELY VEER LEFT. R & R NR 4 MAIN BRAKE ASSY. BLED ALL AIR FROM BRAKE HYD SYS. PERFORMED TAXI CHECK WITH NO DEFECTS NOTED. ALL WORK DONE IAW MM 32-40-21.SDR DXTA2010101804263Rudder Control · malfunctionedUNCOMMANDED RUDDER TRIM MOVEMENT IN FLIGHT. RUDDER MOVES FROM 1 UNIT RT TO 1 UNIT LT WITH A CORRESPONDING CHANGE IN ACFT COORDINATION.SDR DXTA2010101404262Monitor · shortedWHILE ENROUTE, PAX NOTIFIED CREW THAT THERE WAS SMOKE IN THE CABIN, TURNED AROUND, THERE WAS A PLUME OF SMOKE COMING FROM THE NR 4 AIRSHOW MONITOR. SHUTDOWN CABIN ELECTRICAL POWER AND DIVERTED. CHECKED WIRING FROM MASTER CONTROLLER CONNECTOR PIN "U" TO PINS 2SDR DXTA2010092404251Actuator · inoperativeON CLIMBOUT WHEN RAISING THE SLATS, WHITE EICAS MESSAGE SLAT/FLAP MAINT COME ON, DID THE CHECKLIST AFTER 4 CYCLES, THE SLATS WOULD NOT COME UP. INSPECTED SLATS AND FOUND LT NR 2 SEAT ACTUATOR LEAKING. REMOVED LEAKING ACTUATOR AND INSTALLED REPAIRED ACTUATOR SDR DXTA2010092004244Display · intermittentCOPILOT'S PFD TURNS ON AND OFF INTERMITTENTLY. REMOVED CO-PILOT MFD. CHECKED THE FILTER SCREEN ON BACK OF MFD. FOUND DEBRIS ON SCREEN. REMOVED AND CLEAN ALL DEBRIS FROM THE FILTER SCREEN. RE-INSTALLED THE CO-PILOT MFD INTO ITS ORIGINAL POSITION. OPS CHECKSDR DXTA2010090704221Slat System · bindingFLAPS JAMMED AT 18 DEGREES AT 400 AGL AFTER TAKEOFF. FLAP HANDLE PLACED TO 20 & FLAPS & KRUEGERS RETURNED. FLAPS 0 SELECTED & FLAP RETRACTED TO 0. SLATS 0 SELECTED & SLATS JAMMED AT APPROX 2-3 DEGREES. FLAP HANDLE MOVED TO VARIOUS POSITIONS, SLATS REMAINED JSDR DXTA2010081804196Warning Light · false activationDURING FLIGHT LT AND RT T/R ENG FAIL ICAS MESSAGES APPEARED THEN SHORT FINAL SP INHIBIT INOP AND EICAS MIS-COMPARE MESSAGES APPEARED. ONCE ON THE GROUND, LT AND RT FADEC MAJOR ICAS MESSAGES APPEARED. WENT THROUGH LT AND RT PROPULSION SYS DIAGNOSTICS AND THE LSDR DXTA201007160415Engine · overtempRT ENGINE SHUTDOWN INFLIGHT DUE TO VIBRATION DETECTOR AT MAX LEVEL WITH CORRESPONDING RISING HIGH ITT LEVEL (NOT IN RED) AND ENGINE FIRE CAS MESSAGE. THERE WAS ALSO THE SMELL OF SMOKE IN THE CABIN BUT NOT VISIBLE. ENGINE WAS SECURED BY POWER TO IDLE AND FUELSDR DXTA2010071604156Turbine Blades · crackedABOUT 45 MINUTES INTO THE FLIGHT, CLIMBING THRU FL 360, CREW HEARD A LOUD "BANG", FELT A VIBRATION, ITT BEGAN AN IMMEDIATE CLIMB, FOLLOWED BY THE "FIRE" LIGHT AND SMOKE IN THE CABIN. CREW BROUGHT THE THROTTLE TO IDLE, SHUT THE ENGINE DOWN VIA THE FUEL CUTOFF SSDR DXTA2010071904160Pump · leakingDEPARTING, CLIMBING OUT OF 17 THOUSAND FEET, NOTICED LOW AIRFLOW INTO CABIN WITH ECS ON BOTH, THEN HEAVY SMOKE AND ODOR STARTED TO FILL THE COCKPIT AND CABIN. EMERGENCY WAS DECLARED AND DECENT BACK TO DEPARTURE. R & R BOTH LT & RT ENGINE OIL PUMP ASSY IAW MM SDR 2010FA0000701Placard · missingNO PLACARD INSTALLED MEETING FAR 25.1547 LOCATED IN OR ON THE ACFT .SDR DXTA2010070604142Brake Sys · inoperativeUPON LANDING, WITH GROUND AIRBRAKES DEPLOYED & T/RS DEPLOYED, NORMAL BRAKING NOT AVAILABLE. NORMAL BRAKING RESTORED WHEN THE T/RS WERE RETRACTED. CHECKED SERVICING OF ALL 3 GEAR STRUTS & FOUND THEM LOW. SERVICED NITROGEN IAW MM 32-10-25. R & R 4 EA WOW RELAYSDR DXTA2010063004134Engine · overservicedAT FL190 EXPERIENCED SMOKE IN CABIN AND COCKPIT. WENT THRU SMOKE ELIM PROCEDURES AND SELECTED LT ENGINE ECS. SMOKE STOPPED BILLOWING AND SLOWLY DISAPPATED. SMELL REMAINED. EXPERIENCED SAME ODOR ON PREVIOUS LEGS WITH THROTTLES IN A MIDRANGE POSITION. EXTERNASDR CA100629005Limiter · intermittent(CAN) SLATS FAIL ON THREE OCCASIONS. SLAT FAIL TO RETRACT- INOP, MAY 17TH 2010. THE SYSTEM WAS TROUBLE SHOOT BY GULFSTREAM USING TEST BOX TO CHECK FAILURE, SYSTEM STARTED TO OPERATE PROPERLY COULD NOT DUPLICATE PROBLEM. THE SLAT SYSTEM WAS INSPECTED AND NR 3SDR DXTA2010060904118Selector Valve · leakingAFTER TAKEOFF AND ON INITIAL GEAR RETRACTION, RT HYD PUMP PRESS LOW, AUX HYD PUMP ON, AND RT HYD LOW LEVEL CAUTION MESSAGES ILLUMINATED. FLUID QTY LEVEL WAS AT 24 ON RT HYD SYS. RAN QRH PROCEDURES AND LANDED SJC. ON POSTFLIGHT, HYD FLUID NOTED ON BOTTOM ON PLASDR DXTA2010060304109Brake · malfunctionedWHEN BRAKES ARE APPLIED DURING TAXI THERE IS A INTERMITTENT LOUD BANG IN THE NOSE OF THE ACFT WITH THE BRAKES GRABBING. BLED ALL 4 BRAKES AND TAXI CHECKED ACFT, NO DISCREPANCIES NOTED. SERVICED RT HYD RESERVOIR WITH FLUID AFTER BRAKE BLEED. ALL WORK DONE IAWSDR DXTA2010060104107Actuator · faultyUPON LANDING GEAR EXTENTION THE RT MLG SHOWED A AMBER UNKNOWN POSITION THEN A RED UNSAFE POSITION. AFTER A MINUTE IT SHOWED A DOWN AND LOCKED POSITION. REMOVED RT MLG HYD ACTUATOR AND INSTALLED MODIFIED UNIT IAW CMP 321004. OPS AND LEAK CHECKS GOOD.SDR DXTA2010052604103Brake · wornBRAKES WEAK. ON LANDING IT TAKES AN ABNORMAL AMOUNT OF TOE PRESSURE TO INSURE STOPPING. DURING TAXI IN AT BRISK WALK SPEED APPLIED BRAKE PRESSURE SIMULATING EMERGENCY STOP NECESSITY. MOMENTARY FELT BRAKES ENGAGE, BUT THE ACFT CONTINUED COASTING. IT APPEARS ASDR DXTA2010052404097Control Unit · bindingON APPROACH AFTER DISENGAGING THE AUTO PILOT/YAW DAMP AT 180KTS THE ACFT WOULD ONLY ROLL (5) DEGREES TO THE RT. BOTH THE CAPTAIN AND COPILOTS CONTROLS SEEMED JAMMED. ONCE ON THE GROUND WE ARE ABLE UNJAM THE CONTROLS WITH FULL MOVEMENT. REPLACED AILERON AFU.SDR DXTA2010052404099Line · leakingFUEL LEAK ICAS MESSAGE ANNUNCIATION 10 MIN BEFORE INITIAL DESCENT. MONITORED FUEL FOR 15 MIN & NOTED A 150 LB LOW IMBALANCE IN LT WING. REBALANCED FUEL & AFTER AN ADDITIONAL 15 MIN, NOTED ANOTHER 150 LB LOW IMBALANCE IN LT WING. TAXIED ONTO RAMP FUEL LEAKING SDR DXTA2010051704094Switch · out of adjustON TAKEOFF, AFTER SELECTING GEAR UP, IT SEEMS LIKE ALL THE GEAR RETRACT NORMALLY EXCEPT THE LT MAIN INDICATES RED HASH MARKS. THE OTHER (2) INDICATE UP, BUT THE LT MAIN STAYS RED HASH MARKS. IT STAYS THIS WAY WITH NO CHANGE OR INPUT FROM US FOR 3 TO 4 MINUTES SDR DXTA2010051004091A/C Pack · malfunctionedUNABLE TO COOL COCKPIT BELOW 27C OR CABIN BELOW 25C IN AUTO OR MANUAL MODES DURING FLT. TEMPS GOT AS HIGH AS 32C IN COCKPIT & 28C IN CABIN. DETECTED MILD BURNING ODOR FROM COCKPIT WEMACS AFTER LANDING. THIS WAS ALL WITH ECS SET TO BOTH & APU OFF. NO SMOKE DETESDR DXTA2010050304082Valve · weakBRAKES FEEL AS IF THERE IS PARTIAL HYD PRESSURE ON WITHOUT PILOT INPUT. REMOVED OLD POWER BRAKE VALVE. INSTALLED INSPECTED POWER BRAKE VALVE IAW CMP CARD 324002 COMPLIED WITH NORMAL PARKING AND EMERGENCY BRAKE BLEEDING IAW MM CH 32-40-20. COMPLIED WITH NORMALSDR DXTA2010050304081Brake · weakBRAKES FEEL AS IF THERE IS PARTIAL HYD PRESSURE ON WITHOUT PILOT INPUT.SDR DXTA2010041904071Windshield · failedRT WINDSHIELD SHATTERED DURING FLIGHT. REPLACED COPILOT WINDSHIELD WITH NEW. OPS/LEAK CHECKS GOOD. DONE IAW MM 56-10-05.SDR DXTA2010041504067Battery · overtempLEFT BATTERY OVERTEMPED TO 170 DEGREES AT FL320; DISCONNECTED BATTERY IAW CK LIST BUT TEMP REMAINED AT 170 DEGREES AND CONTINUED TO DECREASE TO NORMAL DURING THE LANDING AND TAXI. EICAS MISCOMPARE MESSAGE ILLUMINATED THROUGH DESCENT FL310 AND REMAINED ON UNTISDR DXTA2010031704037Landing Gear · malfunctionedNOSE WHEEL INDICATOR DID NOT SHOW GEAR UP AND LOCKED. RECYCLED THE GEAR ACCORDING TO QRH G-200 PROCEDURE. NOSE WHEEL INDICATOR SHOWED "UP" INDICATION. JACKED ACFT AND PERFORMED NUMEROUS GEAR SWINGS, UNABLE TO DUPLICATE. DISCONNECTED CONNECTOR PLUG 854YP AND SDR DXTA2010031604036Battery · overheatedEMERGENCY BATTERY OVERHEATED IN FLIGHT; TEMP WENT TO 170 DEGREES F, VOLTS REMAINED AT 26.7. R & R EMERGENCY BATTERY WITH O/H UNIT MM 24-30-20, CMP 243019. OPS CHECKS GOOD.SDR DXTA2010F00059Deice System · malfunctionedWHILE ENROUTE, NOTICED THAT THE RT WING DEICE BOOTS WERE INFLATED WHILE IN CRUISE. ON POST FLIGHT INSP, NOTED 24 PIN HOLES IN RT DEICE BOOTS.SDR 2010FA0000159Landing Gear · malfunctionedNOSE GEAR DOES NOT INDICATE DOWN AND LOCKED AFTER PULLING EMERGENCY GEAR HANDLE.SDR DXTA2010012503954Proximity Switch · malfunctionedLT MAIN GEAR WOULD NOT RETRACT, YELLOW THEN RED INDICATOR. CYCLED 3 TIMES, NO CHANGE. JACKED ACFT FOUND LT MLG PROX SWITCH FAULTY. REPLACED PROX SWITCH. PERFORMED OPS CHECK. ALL WORK DONE IAW MM 32-10-11.SDR DXTA2011010504397Structure · leakingSTRONG FUEL ODOR FOUND IN THE REAR OF THE CABIN. 11,000 POUNDS OF FUEL ON BOARD. ODOR FOUND ONLY AFTER THE APU IS STARTED. NO LEAKS FOUND ON THE OUTSIDE OF THE ACFT. NO LEAKS FOUND ON THE INSIDE OF THE ACFT. WAITED 2 HOURS TO LET AIR OUT AND WHEN STARTED APSDR DXTA2009122303940Duct · cracked20 MINUTES INTO FLT DETECTED AN ODOR LIKE EXHAUST OR BLEED AIR 10 MINUTES LATER AT 41000. BAGGAGE SMOKE AMBER CAS MESSAGE ILLUMINATED MESSAGE REMAINED ON FOR REMAINDER OF 20 MINUTES DIVISION THE MESSAGE BRIEFLY WENT OUT ON TOUCHDOWN BUT CAME BACK ON. INSPECTEDSDR DXTA2009122103908Limiter · inoperativeLOST CABIN AT FL 400. HEARD PRESSURIZATION BUMP AND CABIN BEGAN CLIMBING RAPIDLY APPROX 1500FT/MIN OR GREATER. GOT CABIN HIGH EICAS. AFTER LANDING FELT ALMOST NO FROM ECS. REMOVE DUCT TEMP LIMITER AND INSTALLED NEW DUCT TEMP LIMITER REF MM 21-50-03. PERFORSDR DXTA2009120703881Proximity Switch · faultyWHEN STARTING DESCENT OUT OF 23,000, RED GEAR UNSAFE INDICATION ON LT MAIN LANDING GEAR CAME ON AND AIRSPEED WENT RED. SLOWED BELOW 195 MAX GEAR SPEED, AIRSPEED WENT BACK GREEN, GEAR INDICATION STILL UNSAFE. GEAR EXTENDED NORMALLY WITH 3 GREEN. REMOVED LT MLSDR DXTA2009112503869Tire · failedBOTH RT MAIN TIRES ARE BLOWN OUT AFTER ATTEMPTING TO STOP WITH NORMAL BRAKING, THEN HAVING TO SWITCH TO EMERGENCY BRAKING TO STOP. REMOVED AND REPLACED BOTH NR 3 & NR 4 MLG WHEEL ASSY IAW AMM 32-40-15.SDR DXTA2009112303867Transceiver · inoperativeAT FL 400, RED "GEAR NOT DOWN" CAS MESSAGE AND TONE ACTIVATED THEN EXTINGUISHED. REMOVED AND REPLACED RAD ALT TRANSCEIVER IAW CMP 344402, OP CHECKS GOOD IAW CMP 344410 AND AMM 32-60-00.SDR DXTA2009112003864Shim · interferenceIN LEVEL FLIGHT FL 260 RT MAIN GEAR INDICATOR WENT AMBER THEN RED AND STAYED LIT UNTIL BELOW 250 KTS ON APPROACH TO LAND. ADJUSTED RT MLG DOOR FWD STOP, LOWER ROD ON MLG DOOR 1 FULL TURN TO TIGHTEN UP GEAR DOOR DUE TO EXCESSIVE PLAY WITH GEAR UP. NOTICED THASDR DXTA2009110603851Tube · crackedRIGHT HYDRAULIC SYSTEM FAILED IN FLIGHT. PRESSURE INDICATED 0 AS QUANTITY INDICATED 24%. FOUND RT ENG HYD PUMP PRESSURE LINE CRACKED AT PRESSURE FILTER. LINE REPAIRED IAW MM 20-10-13 W/ PERMASWAGE BY MFG. RT EDP REPLACED, AUX PUMP REPLACED, RT PRESSURE FISDR DXTA09110203838ASwitch · inoperativeREMOVED AND REPLACED LT MLG HARNESS IAW CMP 321601. OP TESTED MAIN LANDING GEAR WOW SW IAW MM 82-60-05. PERFORMED BRAKES FUNCTIONAL TEST IAW CMP 276016. PERFORMED ANTISKID TOUCHDOWN PROTECTION FUNCT TEST IAW MM 82-40-30. PERFORMED ANTISKID LOCK WHEEL PROTESDR DXTA2009102803828Thrust Reverser · malfunctionedLT T/R FAIL MESSAGE CAME ON AFTER T/O AND REMAINED ON FOR DURATION OF FLIGHT.SDR 2009F00095Controller · malfunctionedUNABLE TO CONTROL COCKPIT OR CABIN TEMP IN BOTH MANUAL AND AUTO CONTROLLER MODES. THE CONTROLLER DID NOTHING IN BOTH MODES UNTIL 10,000', SEEMED TO WORK LOWER.SDR DXTA2009092803798Latch · out of adjustABNORMAL GEAR INDICATION FOR RIGHT MAIN. AFTER FEELING AND HEARING A "THUMP" .320 KIAS, FL220, AMBER IN TRANSIT INDICATION, THEN RED UNSAFE GEAR. DESCENDED TO BELOW FL190 AND SLOWED TO .240KIAS, INDICATIONS NORMAL. ADJUSTED RT INBOARD DOOR LATCH ASSY AS RESDR DXTA2009092803797Proximity Switch · out of adjustABNORMAL GEAR INDICATION FOR RT MAIN AT CRUISE FLIGHT: 310KIAS, FL220. INITIAL AMBER INDICATION FOLLOWED BY RED. SLOWED AIRCRAFT TOWARD GEAR EXTENSION SPEED. INDICATION NORMAL BETWEEN 250-260 KIAS. PERFORMED MTC CHECK MEASURMENT OF RT AFT PROXIMITY SWITCH & RSDR DXTA2009091103786Slat System · inoperativeON DEPARTURE FROM SBA, "KRUEGER FAIL" EICAS MESSAGE CAME ON & KRUEGER & SLATS WOULD NOT RETRACT. ON THE GROUND FLAPS & SLATS OPS NORMAL. PER CUSTOMER REQUEST PERFORMED CMP 275101 FLAP/SLAT CONTROL AND DRIVE SYSTEM- FUNCTIONAL TEST. NO DEFECTS NOTED. PERFORMEDSDR DXTA2009091103785Landing Gear · inoperativeON DEPARTURE FROM SBA, ALL 3 MLG`S WOULD NOT RETRACT. INSPECTED MLG, MLG SELECTOR VALVE & CABLE, GEAR CONTROL LINKAGE, LATCHES, CONTROL LEVER, WOW SWITCHES, WIRING HARNESS, UPLOCKS & SURROUNDING AREAS. CHECKED FREEDOM OF MOVEMENT OF GEAR SELECTOR HANDLE. APPSDR DXTA2009090803774Actuator · malfunctionedA/P PITCH TRIM CAUTION LIGHT CAME ON WHILE CLIMBING THROUGH 10-12 THOUSAND FEET. UPON DISENGAGING THE AUTO PILOT, ACFT PITCHED UP SLIGHTLY DUE TO NOSE UP PITCH SETTING, PITCH TRIM ADJUSTED BACK DOWN WITH THE NORMAL TRIM SWITCH AND CAUTION LIGHT WENT OUT. UP
Back to Beech 200