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 UALA2010101103766Actuator · faultyRUDDER RATIO ISSUES. REPLACED RUDDER RATIO ACTUATOR. OPS NORMAL.SDR UALA2010082403121Actuator · failedVIBRATION-NOISE ENCOUNTERED IN FLIGHT, REF FLT MANUAL 12.20.1 NEED TO COMPLETE VIBRATION REPORTING CHECKLIST AND DEBRIEF MX ON ARRIVAL TO DESTINATION STA. VIBRATION IN AFT GALLEY AREA DURING CLIMB. AIR-SPEED 250-305 KNOTS. END-ED AROUND FL 180. CHECK FLAP FAIRSDR UIEA2010060300025Actuator · leakingEO; 4455A041 IS TO DOCUMENT A MAJOR REPAIR. DURING REPLACEMENT OF UPPER RUDDER PCA (FOR LEAK), HIGH-LIFT CONTACTED RUDDER CAUSING DAMAGE TO RUDDER COMPOSITE STRUCTURE (REF FIGURE 1), MEASURING 12.0 IN. X 15.0 IN. DAMAGE IS BEYOND THE SRM LIMITS IAW THE SRM 55-SDR HALA2010053000235Actuator · malfunctionedETOPS SIGNIFICANT SYS - AFTER T/O & DURING CLIMB ACFT REQUIRES 4-5 RUDDER UNITS OF TRIM 2-3 UNITS OF RUDDER TRIM AS WEIGHT DECREASES. R & R RUDDER TRIM ACTUATOR IAW AMM 27-21-11, OK FOR SVC.SDR SWIA201023958Cable · corrodedRUDDER TRIM FROZE INFLIGHT. (FLT 6821) REPLACED RUDDER TRIM ACTUATOR CABLE.SDR CA091202002Bolt · dirty(CAN) F/CREW NOTED A LOSS OF YELLOW HYD FLUID DURING FLIGHT MCO TO YYZ. MAINTENANCE IN YYZ NOTED EVIDENCE OF HEAVY BUILD-UP ON THE RUDDER. FURTHER INVESTIGATION FOUND TWO OF THREE ATTACH BOLTS FOR ONE OF THE ACTUATOR RODS SHEARED. BOLTS SHANKS REMAINED BUT SDR CA091214008Actuator · misrepaired(CAN) DURING DISASSEMBLY OF 27427-3 ACTUATOR ASSEMBLY (ITEM 2-1) IAW CMM 27-23-01 REV 5, DATED AUG 21/07, IT WAS NOTED THAT THE TWO (2) DYNAMIC SEALS USED TO PREVENT EXTERNAL FLUID LEAKAGE TO ATMOSPHERE ON BOTH ENDS OF THE PISTON ROD WERE INSTALLED IN THE WRONSDR CA091209001Actuator · misinstalled(CAN) DURING DISASSEMBLY OF 27427-3 ACTUATOR ASSY (ITEM 2-1) IAW CMM 27-23-01 REV 5, DATED AUG 21/07, IT WAS NOTED THAT THE (2) DYNAMIC SEALS USED TO PREVENT EXTERNAL FLUID LEAKAGE TO ATMOSPHERE ON BOTH ENDS OF THE PISTON ROD WERE INSTALLED IN WRONG GROVE LOCASDR AALA20091031DFW01Actuator · leakingON APPROACH RIGHT HYDRAULIC SYSTEM FAILED. LEFT MAIN LANDING GEAR DOOR DAMAGED ON LANDING. REVERSER UNLOCK LIGHT REMAINED ILLUMINATED. FLUID RETURNED TO 6 AFTER SHUTDOWN AND FLAPS RETRACTED. AIRCRAFT OUT OF SERVICE. REPLACED LEFT MAIN LANDING GEAR DOOR. SDR 2009FA0000811Actuator · leakingTESTING PLUG BACKED OUT OF THE RUDDER ACTUATOR CASE, BECAUSE IT WAS NOT SAFTIED, RESULTING IN THE RIGHT HYDRAULIC SYSTEM DRAINING TO ZERO IN FLIGHT.SDR UALA2009100103085Union · damagedHYDRAULIC FLUID COMING FROM BOTTOM OF RUDDER ALSO EVIDENCE AROUND APU EMPENNAGE FOUND ON ARRIVAL. CARRIED OUT T-S, REMOVED LEFT PANELS TO ACCESS YAW DAMPER SERVOS, NO LEAKS NOTED. REMOVED PANELS 324GL, JL AND LL FOUND LEAK ON PRESSURE LINE CONNECTOR TO CENTESDR UALA2009082502657Actuator · unreliableRUDDER TRIM KNOB UNRESPONSIVE FOR RUDDER TRIM. INTERMITTENT, WHEN TRIMMING LT OR RT. REPLACED RUDDER TRIM ACTUATOR. INSPECTED INSTALLATION OF RUDDER TRIM ACTUATOR.SDR UALA2009080302310Actuator · failedEXPERIENCED AT LEAST 3 UNCOMMANDED YAWS IN CLIMB AND CRUISE. SPEED AROUND 280 KIAS. SPOKE TO CREW IN FLIGHT, STATED THAT NOSE YAWED 5-10 DEGREE'S LEFT TO RIGHT AND RUDDER TRIM WENT FROM 0 TO 1.7 UNITS DURING THE OCCURRENCE. REPLACED RUDDER TRIM ACTUATOR. OSDR HNAA2009908090024Actuator · malfunctionedON JULY 27, CREW REPORTED RUDDER TRIM WOULD NOT WORK IN SLOW MODE. PHL MAINTENANCE COULD NOT DUPLICATE PROBLEM, RUDDER TRIM OPS CHECK GOOD. ON JULY 28, CREW REPORTED RUDDER TRIM WOULD NOT WORK IN SLOW MODE. PHL MAINTENANCE REMOVED AND REPLACED TRIM PANEL IASDR UALA2009061601722Actuator · failedRUDDER CONTROL FAILURE. RTFL.SUPPLEMENTAL DATA UPDATE REPLACED RUDDER TRIM ACTUATOR AND PERFORMED OP TEST. ALSO PASSED AFS TEST AND NO MESSAGES.SDR DXTA2009040203575Actuator · faultedON TAKEOFF ROLL, HAD A DEICE PRESS HI/LO CAS ACCOMPANIED BY A YAW TO THE RIGHT. OCCURED PRIOR TO 80 KIAS WITH T/O POWER SET, TAKEOFF WAS ABORTED. DURING A RUN UP AFTER THE ABORTED T/O IT WAS DISCOVERED THAT THE RUDDER BIAS WAS WORKING WHEN SELECTED OFF. TROSDR QXEA2009033000201Actuator · intermittentPDX - RUDDER TRIM ACTUATOR ONLY MOVED INTERMITTENTLY DURING CLIMBOUT, BUT SEEMED TO WORK NORMALLY FOR THE REMAINDER OF FLIGHT. C/W OPERATIONAL TEST PER AMM TASK 27-22-00-710-801. NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED.SDR HALA2009031600088Actuator · inoperativeETOPS SIGNIFICANT SYSTEM - ON APPROACH RUDDER TRIM KNOB WOULD NOT TRIM RUDDER. KNOB WILL TURN BUT INDICATOR WOULD NOT MOVE EITHER DIRECTION. REMOVED RUDDER TRIM ACTUATOR REPLACED RUDDER TRIM ACTUATOR PER AMM 27-21-111-422-012, ALL TEST GOOD. ACFT OKAY FOR SSDR UALA2009031300786Actuator · leakingEICAS L HYD QTY SHOWS .42. FLIGHT DIVERTED. FOUND RUDDER RATIO CHANGER ACTUATOR PISTON LEAKING. REPLACED ACTUATOR. SERVICED LEFT HYD QTY TO FULL.SDR C2XA09SH066Bushing · migratedSHV - DURING C-CHECK HYD SYSTEM 2 RUDDER ACTUATOR UPPER HAT BUSHING AT RUDDER 1 ATTACHMENT MIGRATED. MAINTENANCE INSTALLED NEW RUDDER 1 IAW EMB-145 AMM 27-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH065Bushing · migratedSHV - DURING C-CHECK HYDRAULIC SYSTEM 1 RUDDER ACTUATOR UPPER HAT BUSHING AT RUDDER ATTACHMENT MIGRATED. MAINTENANCE INSTALLED NEW RUDDER 1 IAW EMB-145 AMM 27-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR CA090112010Actuator · cracked(CAN) DURING A C CHECK , A TECHNICIAN FOUND A SPOT OF SURFACE (BUBBLE) CORROSION ON THAT PART, HE CLEANED AND FOUND A CRACK (TC NR 20090112010)SDR GLBA200901094Actuator · inoperativeON CLIMB OUT NOTICED UNABLE TO CONTROLL THE BALL USING RUDDER TRIM, WENT TO 10 RT WITH NO EFFECT. IN CRUISE FROM 3 TO 10 RT THE RUDDER TRIM DID NOT HAVE ANY EFFECT ON RUDDER. TURNED OFF HYDRAULICS TO RUDDER AND LANDED IN MANUAL. MX INSPECTED RUDDER TRIM FOR TRSDR 2008UALA06376Actuator · leakingFOUND MIDDLE RUDDER PCA LEAKING HYDRAULIC FLUID. REPLACED MIDDLE RUDDER PCA. OPS CHECK NORMAL.SDR SWIA200820165Actuator · malfunctionedAFTER TAKEOFF, AT APPROXIMATELY 130 KTS, RIGHT RUDDER JAMMED (FLT 5416). REPLACED BLUE SYSTEM RUDDER ACTUATOR. VPN 308140-1003, S/N ON 0581, S/N OFF 0701.
SDR CA080908004Actuator · bypassing(CAN) FLT CREW REPORTED RUDDER TRIM INDICATOR SHOWS 40% RT DEFLECTION TO CENTRE BALL ON HSI. MX REPLACED THE RUDDER TRIM ACTUATOR AND CHECKED SYSTEM SERVICEABLE. ON THE NEXT FLIGHT THE CREW REPORTED NO APPRECIABLE CHANGE AND THAT IT APPEARED THEY WERE CROSS COSDR DXTA200803116Actuator · faultyDURING CLIMB OUT PASSING THROUGH FL180 AND 250 KIAS THE UPPER RUDDER BEGAN TO OSCILLATE, THIS WAS PHYSICALLY NOTICABLE IN THE AIRFRAME. TROUBLESHOT AND FOUND UPPER RUDDER ACTUATOR TO BE FAULTY. REPLACED UPPER RUDDER ACTAUTOR PERFORMED UPPER RUDDER SYS ADJUSTMSDR DXTA200803047Actuator · defectiveRUDDER CONTROL REQUIRES EXCESSIVE CONTROL INPUTS TO GET DESIRED RESULTS. REMOVED AND REPLACED ACTUATOR IAW MM 27-30-05. OPS AND LEAK CHECK GOOD.SDR BB08006Gasket · leakingCUN FLT 803 PHL-CUN DURING LANDING GEAR EXTENSION, LEFT HYD SYSTEM QTY DROPPED TO .48 RF. MAINTENANCE FOUND RUDDER RATIO ACTUATOR SOLENOID GASKET LEAKING. REPLACED GASKET.SDR DXTA200802749Actuator · malfunctionedRUDDER BIAS FAULT CAS MESSAGE CAME ON AFTER ROTATION. R & R ACTUATOR NO FAULTS FOUND ON INSPECTION OF RUDDER BIAS COMPONENTS. C/W SATISFACTORY OPERATIONAL CHECKS IAW MM 27-20-00 & FT-680-0022.SDR CA071026005Actuator · failed(CAN) WHILE PERFORMING AN A-CHECK, THE RUDDER TRIM ACTUATOR (PN: 793500-501) FAILED THE FREE PLAY CHECK IAW MM 5-20-06 PARA: 1.F.(4) AND MM 27-20-00 PAGE 503 PARA: 4.A. A NEW RUDDER TRIM LOWER ACTUATOR (PN: 793500-501) (ALTERNATE PN:1092AS100-3) WAS ORDERED. WSDR 2007UALA03682Actuator · out of adjustIN MANUAL REVERSION THE AIRCRAFT ROLLS LEFT REQUIRING HARD RIGHT YOKE JO MAINTAIN LEVEL. STANDBY RUDDER ACTUATOR OUT OF ADJUSTMENT (A/C FLOWN IN MANUAL REVERSION DUE TO FLIGHT CONTROL WORK ACCOMPLISHED AT HMV). DURING ATTEMPT AT LEVEL FLIGHT IN MANUAL REVERSSDR 2007UALA01743Actuator · malfunctionedCREW REPORTS RUDDER BINDING, REQUIRED MORE RUDDER PRESSURE TO USE. PEDAL ALSO STICKS AND STUCK ON APPROACH TO IAD. REPLACED RUDDER ACTUATOR.SDR AALA20070560Actuator · inoperativeDURING CRUISE RUDDER TRIM WOULD NOT RESPOND LEFT OR RIGHT. DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. REPLACED RUDER TRIM ACTUATOR AND OVERHEAD CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR HALA0700078Actuator · leakingRUDDER RATIO CHANGER ACTUATOR LEAKING FROM PISTON DYNAMIC SEAL. REPLACED RRCA PER AMM 27 21 42 024, TASK ALL TESTS AND LEAK CKS OK.SDR AWXA200602011Actuator · failedDFW - ATB - DURING CLIMB-OUT OF DFW, THE A/C REQUIRED EXCESSIVE RUDDER INPUT TO MAINTAIN STRAIGHT FLIGHT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. THE PAX DID NOT BRACE. MX REMOVED AND REPLACED THE RUDDER TRIM ACTUATOR. THIS DID NOT CORRECT THE SDR CA061107001Actuator · malfunctioned(CAN) DISC-RUDDER TRIM MOVING ON ITS OWN WITHOUT INPUT FROM COCKPIT CONTROLS. PULLED C/B 2F2 IAW AOM VOL 1. INDICATOR STILL SHOWS UNCOMMANDED MOVEMENT AND PLANE STILL FLIES SIDEWAYS, FDR DOWLNLOAD WAS REQUESTED TO CONFIRM THE TRIM MOUVEMENT. MAINTENANCE WAS UNSDR SIMA200631002Actuator · malfunctionedRUDDER TRIM MOVING ON ITS OWN WITHOUT INPUT FROM COCKPIT CONTROLS, PULLED CIRCUIT BREAKER 2F2, IAW AIRCRAFT OPERATING MANUAL VOLUME 1. INDICATOR STILL SHOWS UNCOMMANDED MOVEMENT AND PLANE STILL FLYS SIDEWAYS. REMOVED AND REPLACED RUDDER TRIM ACTUATOR, IAW CSDR HNAA0600123Circuit Breaker · not closedAFTER TAKEOFF RUDDER PRESSURE AND RUDDER FULL PRESSURE CAUTION LIGHTS ILLUMINATED FOLLOWED BY NR 1 RUDDER HYDRAULIC CAUTION LIGHT ILLUMINATED. FOUND CIRCUIT BREAKER N7 NR 2 RUDDER IS NOT FULLY SEATED. RESET BREAKER SYSTEM OPERATED NORMALLY.SDR CA061004004Tube · cracked(CAN) CREW NOTICED FLUID STAINS AND ACCUMULATION ON RT SIDE OF RUDDER AND TAIL CONE. MAINTENANCE FOUND CRACK AT FIRST ELBOW FROM TOP FITTING OF NO. 1 HYDRAULIC SYSTEM PRESSURE LINE TO THE RUDDER ACTUATOR. LINE REPLACED AND SYSTEM LEAK CHECKED SERVICEABLE. IPSDR SWIA200617200Actuator · malfunctionedRIGHT RUDDER PEDAL WOULD NOT MOVE WITH BOTH RUDDER SWITCHES ON. REPLACED BLUE HYDRAULIC RUDDER ACTUATOR IAW AMM 27-22-02. OPERATIONAL CHECKS GOOD.SDR ASM200608020Actuator · leakingDURING OVERNIGHT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT RUDDER ACTUATOR. RUDDER ACTUATOR WAS REPLACED IAW MM 27-21-20, TESTED CORRECT.SDR MASA200602127Actuator · malfunctionedASH 7163 CLE - RUDDER TRIM MOVES TO RT LIMIT UNCOMMANDED. MX REPLACED THE TRIM CONTROL PANEL AND RUDDER TRIM ACTUATOR.SDR MASA20061733Actuator · failedASH 6359 TUS - RUDDER TRIM FAULT STATUS MESSAGE EN ROUTE TO PHX. MX REPLACED NR 1 RTL ACTUATOR.SDR DL76L060415Actuator · failedRUDDER RATIO LIGHT AND EICAS STATUS MSG ILLUMINATED. LIGHT/MSG WOULD NOT RESET. FOUND RUDDER RATIO CHANGER ACTUATOR AT FAULT. REPLACED AND OPS CK OK.SDR ARWA20051202Actuator · leakingLOG PAGE NR 116558. ON POST FLIGHT FOUND LEAKING BY EMPANAGE LOWER SIDE REAR STRIKE PAD REAR ACCESS PANEL. REMOVED AND REPLACED RUDDER PACK ACTUATOR IAW MM 27-21-6. LEAK CHECK AND OPERATIONAL CHECK IAW MM 27-20-0 FOUND NORMAL, NO LEAKS NOTICE.SDR MASA200500480Actuator · malfunctionedRUDDER UNCOMMANDED MOVEMENT IN FLIGHT. REMOVED AND REPLACED NR 1 AND NR 2 LINEAR ACTUATOR.SDR SWIA200514620Actuator · malfunctionedRUDDER LIMIT FAULT STATUS MESSAGE. REPLACED NR 1 RUDDER LIMITER ACTUATOR (A203) IAW CRJ MM 27-25-03. OPERATIONAL CHECK GOOD. P/N BA670-93490-3, S/N OFF 0513.SDR P5CA0501317Actuator · malfunctionedINBOUND CREW REPORTED RUDDER RATIO LIGHT ON STEADY. T/S FOUND LOWER RUDDER ACTUATOR STUCK IN HIGH SPEED MODE. REMOVED AND REPLACED LOWER RUDDER RATIO ACTUATOR AND CONTROLLER PER MM 27-21-12. ALL OPS NORMAL.SDR SWIA200514339Actuator · malfunctionedON TAKEOFF, THE RIGHT RUDDER HAD VERY LIMITED TRAVEL. REPLACED GREEN HYDRAULIC RUDDER ACTUATOR IAW 27-22-02. OPS AND LEAK CHECK GOOD.
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