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 jasc_code = '2722' 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 jasc_code = '2722' 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 AUS20010560Pcu · leaking(AUS) RUDDER POWER CONTROL UNIT (PCU) LEAKING INTERNALLY.SDR AUS20010529Pcu · faulty(AUS) RUDDER POWER CONTROL UNIT (PCU) INTERNAL LEAK. FOUND DURING INSPECTION IAW ER B73-27-20-15 AND BOEING SL 737-SL-27-119. WORKSHOP INSPECTION FOUND THE LEAK WITHIN LIMITS.SDR SWIA972535Actuator · failedRUDDER BLUE SYSTEM INOP. (PILOT REPORTED RUDDER ACTUATOR LOCKED UP IN FLIGHT.) RUDDER PCU STARTING TO LEAK AND TESTS ON THE LOW END OF THE RUDDER HEALTH CHECK FOR BLUE SYSTEM. REMOVED AND REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-22-024. PERFORMEDSDR GLBA2001075Actuator · stiffRUDDER TRIM STIFF. CLEANED AND LUBRICATED RUDDER TRIM ACTUATORS, OPS CHECKED SYSTEM SATISFACTORY.SDR SWIA972464Actuator · failedRIGHT RUDDER PEDAL JAMMED IN FLIGHT. REMOVED AND REPLACED BLUE RUDDER HYDRAULIC ACTUATOR IAW 27-20-00. OPS AND LEAK CHECK GOOD AT THIS TIME. P/N: 308104-1003, S/N ON: 0165, P/N OFF: 308140-1003, S/N OFF: 0767.SDR SWIA972424Actuator · failedON LANDING APPROACH AT APPROXIMATELY 130 KNOTS WITH THE YAW DAMPER OFF, UNABLE TO MOVE THE RIGHT RUDDER PEDAL TO THE RIGHT PAST APPROX .25 TRAVEL. NO ASSOCIATED RUDDER LIGHTS ILLUMINATED. REPLACED BLUE SYSTEM RUDDER LINEAR ACTUATOR. S/N IN 0142, S/N OUSDR F3LA200100043Pcu · leakingDURING C-1 CHECK, INSPECTION REPORTED RUDDER PCU FAILED INTERNAL LEAK TEST. REPLACED RUDDER PCU. PERFORMED RIG CHECK PER MM 27-21-00 AND CHECKED GOOD. PERFORMED LEAK CHECK, NO LEAKAGE NOTED.SDR SWIA972368Actuator · failedDURING DESCENT, RUDDER REQUIRED FULL NOSE LEFT RUDDER TRIM TRAVEL TO STOP. RUDDER TRIM INEFFECTIVE. PERFORMED RUDDER ACT HEALTH CHECK, AND PCU CHECK IAW EMB 120 MM 27-22-00. FOUND GREEN RUDDER ACTUATOR TO FAIL. REMOVED AND REPLACED GREEN RUDDER ACTUATOR WISDR SWIA972269Actuator · frozenAFTER LEAVING FL240 RUDDER TRIM FROZEN. RUDDER FREE WITH AND WITHOUT YAW DAMPNER TRIM BEGAN WORKING OUT OF 8-7 THOUSAND FEET. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW RII 27-301. OPS CHECKS GOOD.SDR UPS00834222Actuator · inoperativeINSPECTION TYPE:N/A, ABORTED TAKEOFF DUE TO LIMITED RUDDER MOVEMENT. REMOVED RUDDER HYD PACKAGE PER MM 27-21-06. INSTALLED RUDDER HYD PACKAGE STEPS 1-21 MM 27-21-06 LEAK AND OPS CHECKS OK. ACCOMPLISHED RUDDER ADJ TEST IAW 27-20-00, OPS CHECKS GOOD.SDR 20001019SH015Roll Pin · backed outPILOT RETURNED FROM FLIGHT, REPORTED RUDDER TRIM INOPERABLE. FOUND ONE OF THE TWO ROLL PINS THAT SECURE THE ROD END THAT CONNECTS THE ACTUATOR SCREW TO THE TRIM TAB PUSH/PULL TUBE HAD MIGRATED ALMOST COMPLETELY OUT, THE OTHER ROLL PIN WAS MISSING. THIS CAUSESDR AU001316Actuator · faulty(AUS) RUDDER ACTUATOR ASSEMBLY FAULTY.SDR UPS00833782Actuator · out of adjINSPECTION TYPE:N/A, PILOT REPORT-A/C REQUIRES EXCESSIVE RUDDER TRIM ON TAKEOFF AND LANDING DURING CALM WIND CONDITIONS. IN CRUISE FLIGHT AIRCRAFT REQUIRES 5 DEGREES RUDDER TRIM. ADJUSTED RUDDER POWER PACK IAW MM 27-21-02, SYS OPS CHECKS GOOD.SDR CA000928008Pcu · failed(CAN) ON SERVICE CHECK FOUND LOWER RUDDER DEFLECTED TO THE LEFT WITH ZERO INPUT, A SYSTEM PRESSURIZED. FURTHER TROUBLE SHOOTING REVEALED LOWER RUDDER PCU BYPASSING. LOWER RUDDER PCU REPLACED AND INSTALLATION LEAK, FUNCTION INSPECTED SERVICEABLE IN ACCORDANCE WSDR SWIA971977Pressure Switch · leakingAPPROX 5 MINUTES AFTER DEPARTURE RIGHT SIDE HYDRAULIC RESERVOIR LOW PRESSURE LIGHT ILLUMINATED FOLLOWED BY TOTAL LOSS OF THE BLUE HYDRAULIC FLUID ACTUATING THE LOW LEVEL LIGHT. RETURNED TO SLC PER QRH. FOUND BLUE RUDDER SYSTEM PRESSURE SWITCH TO BE LEAKING. SDR DL73E001600Actuator · malfunctionedNOTICED A SHARP ABRUPT YAW INPUT SHORTLY AFTER NOSE WHEEL LIFTOFF. NO ABNORMAL WINDS OR AIRCRAFT WAKE EXISTING. YAW WAS SIGNIFICANT NO INPUTS NOTED IN RUDDER PEDALS BY PILOT FLYING. REPLACING RUDDER PACK.SDR 20000908SH007Actuator · defectivePILOTS FELT VIBRATION IN RUDDER PEDALS. FOUND EXCESSIVE PLAY (LINEAR) IN UPPER RUDDER TRIM ACTUATOR. REPLACED ACTUATOR. (X)SDR 00FDEA00483Actuator · dislodgedVERTICAL STAB LWR RUDDER ACTUATOR UPPER ATTACHMENT BLOCK ASSY FOUND BUSHING, WASHER RETAINER AND ATTACHMENT BOLT FOUND DISLODGED. *S/D* REMOVED AND REPLACED PARTS PER AMM 20-50-02.SDR AALA006096Packing · failedLAX - BURNING SMELL IN CABIN ON TAKEOFF WENT AWAY AFTER A FEW MINUTES. FOUND HYDRAULIC LEAK ON RUDDER SHUTOFF VALVE. FLUID GOING IN APU INTAKE. INSTALLED NEW PACKING. LEAK CHECK OK. (M)SDR SWIA971731Actuator · malfunctionedAFTER TAKEOFF ABOVE 120 KIAS, FOUND RUDDER UNPOWERED AND NO RUDDER INOP LIGHTS WERE ILLUMINATED, NO MAP LIGHT EITHER. RETURNED TO LAX. REPLACED RELAY K0318, GROUND TESTED RUDDER, OPS CHECKS GOOD.SDR CA000320029Actuator · failed(CAN) HIGH FREQUENCY VIBRATION FELT IN AFT GALLY DURING CLIMB. VIBRATION DISSIPATED DURING CRUISE. YELLOW SYSTEM RUDDER ACTUATOR FOUND AT FAULT. REPLACED.SDR SWIA971720Actuator · failedWHILE DESCENDING INTO SUN LOST RUDDER TRIM CONTROL. RETURNED TO SLC. THIRTY MINUTES LATER, DESCENDING INTO SLC, TRIM CONTROL REGAINED. REPLACED RUDDER TRIM ACTUATOR IAW MM 272302 AND 272000, OPS CHECKS GOOD ON GROUND. (P/N 5298) (S/N 334) ON.SDR CA000410024Bolt · loose(CAN) RUDDER LOWER POWER CONTROL ACTUATOR INPUT CRANK LH PIVOT BOLT LOOSE AND NUT BACKED OFF. LOOSE BOLT ALSO FOUND FOULING ADJACENT CRANK LH LUG. NUT STILL HAD SELF LOCKING ABILITY. NEW BOLT, BUSHING, NUT AND WASHER INSTALLED.SDR PLGA000215Actuator · intermittentBGR - FLT 4612 - ON FLIGHT 4612, BGR-LGA - THE CREW REPORTED THE RUDDER POSITION FELT NORMAL ON LINE-UP CHECK. HOWEVER, THE RUDDER FELT STIFF ABOVE 80 KNOTS, AND WITH NO RUDDER AUTHORITY THE CREW ABORTED THE TAKEOFF. THE CREW REPORTED RUDDER TRAVEL WAS NORMASDR SWIA971614Actuator · malfunctionedUNABLE TO APPLY NORMAL RIGHT RUDDER AFTER TAKEOFF. LEFT RUDDER WORKED OK AND SYSTEM WORKED NORMALLY ON DESCENT. REPLACED BLUE SYSTEM RUDDER ACTUATOR. NO LEAKS NOTED. GROUND FUNCTIONAL CHECKS GOOD.SDR SWIA971611Actuator · failedRIGHT RUDDER STUCK JUST PAST HALF TRAVEL. SHUT OFF BLUE RUDDER SYSTEM AND RUDDER TRAVEL BECAME FREE. RETURNED TO SLC. INSTALLED SERVICEABLE RUDDER ACTUATOR FOR BLUE SYSTEM IAW 27-20-00. NO LEAKS NOTED. OPS CHECKS GOOD.SDR 99UAL900570Actuator · failedRUDDER TRIM INOP. DIVERTED TO ORD. C/B RESET, NO HELP. *S/D* THE INOP CONDITION OF THE RUDDER TRIM SYSTEM WAS DUE TO AN INTERMITTENT INTERNAL FAULT OF THE OF THE RUDDER TRIM ACTUATOR. THE SUBJECT ACTUATOR WAS REPLACED PER MM 27-21-11 AND ALL OPS CHECKS ARSDR 99ZZZX4001Spring · shatteredSPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. IMPROPER HEAT TREATING, AUSTENITE, FATIGUE, AND INCREASED SPRING COIL STRESSES. SPRINGS, PN 69-77855-1, ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MANUFACTURED PRIOR SDR 99ZZZX4003Springs · shatteredSPRINGS, P/N 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREASED SPRING COIL STRESSES. SPRINGS, P/N 69-77855-1 ARE TO BE REPLACED WITH P/N 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MANUFACTURED PRIORSDR 99ZZZX4002Spring · crackedSPRINGS, P/N 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM. IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE, AND INCREASED SPRING OIL STRESSES. SPRINGS, P/N 69-77855-1, ARE TO BE REPLACED WITH P/N 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MANUFACTURED PRIOSDR SWIA971557Actuator · failedAFTER TAKEOFF IN CLIMB, RIGHT RUDDER LOCKED AND RESTRICTED IN FORWARD TRAVEL. RETURNED TO SAN. REPLACED BLUE HYDRAULIC SYSTEM RUDDER ACTUATOR PER MM 27-22-02. NO LEAKS NOTED.SDR CA990927002Actuator · rough(CAN) CREW REPORTED RUDDER FEELS ROUGH. UPPER ACTUATOR REPLACED.SDR VTZA990186Actuator · lack of lubeIAD/RDU - FLT 7617 - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RUDDER TRIM FROZE AND WOULD NOT MOVE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND LUBRICATED RUDDER JACK SCREW TRIM TAIL. OPS CHECK OK. AIRCRAFSDR CA990707055Pcu · failed(CAN) DURING BACKLASH CHECK WITH ONLY 10 POUNDS SIDE LOAD, PCU WOULD DEFLECT 1.5 INCHES ONE WAY BYPASSING INTERNALLY ONLY 323 HRS, 265 DAYSSDR AU990492Actuator · faulty(AUS) RUDDER SERVO CONTROL/ACTUATOR FAULTY.SDR AALA990698Actuator · malfunctionedMIA - FLT 916 - DURING APPROACH AFTER GEAR EXTENSION, A/C EXPERIENCED UNCOMMANDED RUDDER INPUTS. FLT CREW DECIDED TO GO AROUND TO RESOLVE PROBLEM. YAW DAMPERS WERE CYCLED W/NO HELP AND LEFT OFF UNTIL APPROACH. DURING GO AROUND RUDDER INPUTS BECAME VIOLENT ASDR SWIA971474Actuator · malfunctionedON DEPARTURE OUT OF SLC, RIGHT RUDDER PEDAL STUCK AT APPROX ONE-HALF TRAVEL. RUDDER WOULD CENTER BUT WOULD NOT GO PAST ONE-HALF TRAVEL. FOLLOWED QRH AND UPON SELECTION OF BLUE RUDDER SYSTEM TO OFF, RUDDER TRAVEL WAS NORMAL. RETURNED TO SLC. REMOVED AND REPSDR VNAA9904004Actuator · failedVIBRATIONS ORIGINATING FROM THE REAR OF THE AIRCRAFT WERE NOTED BY THE CREW AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED. MAINTENANCE INSPECTED AND REPLACED THE RUDDER LIMIT ACTUATOR, IN ACCORDANCE WITH DORNSDR CA990416014Pcu · failed(CAN) ON TWO OCCASIONS UNCOMMANDED YAW EXCURSIONS, ON CLIMB AND IN CRUISE. BOTH TIMES THE YAW WAS QUITE PRONOUNCED AND OF SHORT DURATION, YAW TO RIGHT. YAW DAMPER AND AUTOPILOT WERE ENGAGED. RUDDER POWER CONTROL UNIT REPLACED.SDR CA990416007Pcu · failed(CAN) PILOT REPORTED VIBRATION THROUGHOUT THE AIRCRAFT WITH B-PUMPS ON. RUDDER OBSERVED TO OSCILLATE 1 TO 1.5 INCH RANGE, RUDDER FUNCTIONED, VIBRATION QUIT. RUDDER PCU REPLACED.SDR CA990416006Pcu · failed(CAN) CREW REPORTED DEFLECTION OF RUDDER LEFT TO RIGHT, HAPPENED TWICE IN CRUISE. CLIMB-OUT AT 260 NOTICED SHARP YAW MOVEMENT THEN RETURNED TO NORMAL, TOO QUICK TO NOTICE YAW FLUCTUATION. YAW COUPLER REPLACED. IN CRUISE, AT FL 310, YAW OSCILLATION STARTED, SDR DL76L990414Actuator · leakingA/C 178 ATB FOR PARTIAL LOSS OF LEFT SYS HYDRAULIC FLUID, REPORTED IN FLT. FOUND RUDDER RATIO ACT EHV LEAKING. REPLACED SAME, OPS CHECK.SDR CA981230010Cap · broken(CAN) HYDRAULIC FLUID FOUND LEAKING FROM EMPENNAGE ON WALK-AROUND. RUDDER PCU CAP BODY SEPARATED FROM THREADED PORTION, RETAINED IN AREA BY LOCKING WIRE. THE CAP BODY HAD BROKEN AWAY FROM THE THREADED PORTION WITH THE THREADED PORTION STILL INSERTED IN THE PSDR QXEA01775Lugs · damagedFORE RUDDER ACTUATOR ATTACHMENT LUGS HAVE MECHANICAL DAMAGE ON BOTTOM SURFACES. REPAIRED IAW DHC-8 SRM 51-30-26.SDR CA981109031Line · chafed(CAN) LARGE HYDRAULIC LEAK FOUND IN TAIL AREA. WIRING HARNESS FOR RUDDER SYNCHRO TRANSIMTTER CHAFED THROUGH RETURN LINE FOR NR 2 RUDDER ACTUATOR. WIRING HARNESS WRAPPED WITH SPIRAL WRAP. LEAK FOUND IN UPPER PORTION OF LINE JUST BELOW RUDDER SYNCHRO TRANSMISDR CA980928026Servo · malfunctioned(CAN) VERY HIGH VIBRATION IN AFT CABIN ON CLIMB OUT FOR ABOUT 30 SECONDS. GREEN SYSTEM RUDDER SERVO REPLACED. PART TC: 8,813.SDR SWIA971247Actuator · failedAFTER DEPARTURE RIGHT RUDDER PEDALS REFUSED FURTHER MOVEMENT BEYOND NEUTRAL POSITION. RETURNED FOR LANDING. REPLACED GREEN SYSTEM RUDDER ACTUATOR IAW MM 27. OPS CHECKS GOOD.SDR QXEA9801183Housing · brokenRUDDER ACTUATOR TO RUDDER POST RETAINING BOLT ANTI ROTATION HOUSING IS BROKEN. REPAIRED IAW HORIZON AIR EA 4-27-52.SDR AU980853Pcu · failed(AUS) RUDDER PCU SUSPECT FAULTY. PART TOTAL CYCLES: 3,637.SDR QXEA9800813Fitting · wornFORE RUDDER LOWER CENTER HINGE ASSEMBLY, BEARING BORE FOR RUDDER ACTUATOR FOUND BEYOND LIMITS. REPLACED FITTING ASSEMBLY IAW DASH 8 SRM 51-40-00.
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