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 = '1430' 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 = '1430' 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 FMAA2004001Bolt · brokenTHE HEAD OF THE BOLT ATTACHING THE REAR OF THE NOSE GEAR DRAG LINK TO THE AIRCRAFT WAS FOUND LAYING IN THE NOSE GEAR WELL. THIS BOLT IS IN A SHEAR LOAD AND SHOULD NOT HAVE BEEN SUBJECT TO ANY FORCES THAT WOULD FORCE THE HEAD OF THE BOLT TO THE POINT OF CRACKISDR CA040601008Bolt · brokenGROUND HANDLING PERSONAL ATTEMPTED TO TOW THE AIRCRAFT INTO THE HANGAR FOR A MAINTENANCE FUNCTION. THE TOW BAR BECAME DETATCHED FOLLOWING HOOK UP. THERE WAS NO DAMAGE TO THE AIRCRAFT OTHER THAN THE BROKEN LOWER TORQUE LINK BOLT ON THE NOSE GEAR.SDR 2004FA0000619Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE SDR 2004FA0000614Bolt · corrodedDURING ANNUAL INSPECTION THE STABILATOR WAS REMOVED FOR FURTHER INSPECTION. THIS IS DUE TO PREVIOUS PROBLEMS ON OTHER PA24 AND PA30/39 AIRCRAFT WITH STABILATOR TORQUE TUBE AND ATTACHMENT BOLTS WITH EXCESSIVE CORROSION. BOTH BOLTS AN175C33A THAT ATTACHES THE SDR MWEA040038Fastener · corrodedRIGHT WING EXTERIOR BOTTOM AFT SKIN HAS 3 EACH SPOTS OF CORROSION BETWEEN STATION XRS69 AND XRS91, ALL CORROSION SPOTS ARE WITHIN 14 INCHES OF AFT SPAR T. REMOVED CORROSION AND REMOVED AND REPLACED FASTENERS.SDR CA040415003Clevis Bolt · misinstalled(CAN) INCORRECT INSTALLATION OF UPPER ELEVATOR CABLE TO ELEVATOR BELLCRANK. AFTER A RECENT PAINT JOB WHERE THE ELEVATOR HAD BEEN REMOVED, THE UPPER BOLT WAS INSTALLED INCORRECTLY. THE AIRCRAFT SERVICE MANUAL MAKES (SPECIAL NOTE) THAT THE UPPER CABLE MUST BE ATSDR 2004FA0000362Bolt · corrodedWHEN PERFORMING MAINT. ON A/C, NOTED RUST ON HEADS OF MAIN SPAR WING ATTACHING BOLTS. REMOVED BOLTS FINDING THEM BADLY CORRODED AND RUSTED. INSPECTED FUSELAGE BEARING BORE AND SPAR BOAR AND INSTALLED NEW AN8-24A BOLTS. AGE AND ENVIRONMENT MAY BE PROBLEM, RECOMSDR 2004FA0000366Bolt · corrodedWHILE REMOVING WING BOLTS, FOUND BOLTS RUSTED AND CORRODED. RECOMMENDED BOLTS BE INSPECTED AND COATED WITH EPOXY PRIMER, INSTALLING NEW BOLTS.SDR AUS20040211Nut · missing(AUS) RT IB FLAP CARRIAGE DEAD WEIGHT ROLLER NUT AND LOCK WASHER MISSING. BOLT WAS STARTING TO MIGRATE FROM POSITION. SUSPECT CAUSED BY FAILURE OF LOCK WASHER TAB.SDR 2004UALA00418Bolt · shearedNOSE GEAR LT DOOR LINK ROD HINGE BOLT IS SHEARED. FOUND DURING NR 1 SERVICE. BOLT NOT RECOVERED, CAUSE OF FAILURE UNKNOWN. REPLACED BOLT.SDR ABXA040126Fastener · wrong partATTACH ANGLE TO FLOOR SUPPORT CENTER WING BOX, RIGHT SIDE 857, ANGLE HAD IMPROPER FASTENER INSTALLED. REPAIRED AREA IAW REA D857-48854MR.SDR DHL2004748001Bolt · brokenLEFT-HAND OUTBOARD FLAP, OUTBOARD AFT FLAP CARRIAGE ECCENTRIC BOLT BROKEN AND ECCENTRIC MISSING. REPLACED BOLT AND ECCENTRIC AT LEFT-HAND OUTBOARD AFT TRAILING EDGE FLAP P/N: 69-39608-1 AND P/N: 69-39619-2 IAW B-727 M/M 27-51-11. OPS CHECKED NORMAL ON GROUNDSDR 04FDEA00679Bolt · undertorquedBOLT FAILED TORQUE CHECK ON POS 556JT LT OUTBOARD FLAP VANE. MX TORQUED PER FCD REQUIREMENTS.SDR GTIA040208Screw · looseFLL - FLT 1123 - WHEN SELECTING L WING LIGHT ON DURING APPROACH CHECKLIST SMOKE AND SPARKS SHOT OUT FROM UNDER GLARE SHIELD. TIGHTENED SCREW ON L WING SWITCH THAT WAS LOOSE, OPS CHECKED NORMAL. (M)SDR ASAA0410137Nut Plate · corrodedOKC - DURING MAINTENANCE, FOUND FORWARD PIT FRAME AT STATION 500 NUT PLATES CORRODED. REPAIR IAW SRM. (M)SDR HYTA2004003Bolt · corrodedWHILE CONDUCTING INITIAL INSPECTION, BOTH AFT WING TO FUSELAGE ATTACH BOLTS WERE FOUND SLIGHTLY RUSTED. DAMAGE WAS NEGLIGIBLE. THESE BOLTS AS WELL AS FORWARD ATTACH BOLTS AND UPPER AND LOWER STRUT ATTACH BOLTS WERE APPARENTLY INSTALLED DRY. THIS HARDWARE SHSDR 04FDEA00680Bolt · undertorquedBOLT FAILED TORQUE CHECK ON POS 656GT RT OUTBOARD FLAP VANE. *S/D* MX TORQUED PER FCD REQUIREMENTS.SDR 04FDEA00678Bolt · undertorquedBOLT FAILED TORQUES CHECK AT POSN 556GT LT OUTBOARD FLAP VANE. MX TORQUED PER FCD REQUIREMENTS.SDR 04FDEA00676Bolt · incorrectI/B FLAP O/B FITTING BOLT HAS THE INCORRECT BOLT IN THIS POSITION. *S/D* MX INSTALLED CORRECT BOLT IN A FOREMENTIONED POSITION.SDR 2004FA0000388Bolt · shearedON LANDING ROLLOUT THE NOSEGEAR COLLAPSED. INSPECTION REVEALED THE DRAG BRACE CENTER PIVOT BOLT (PN NAS464P4-27) HAD SHEARED. THESE SAME BOLTS WERE REMOVED AND REPLACED WITH NEW BOLTS ON THE REST OF THE FLEET. ALL BOLTS WERE FOUND TO BE WORN IN A SHEAR TO SSDR 04FDEA00677Bolt · undertorquedMX FOUND BOLT INSTALLED IN INBOARD FLAP VANE INSTALLED, UNDER TORQUED. MX INSTALLED BOLT IN LEFT I/B FLAP VANE ATTACH POINTS.SDR 251TR0008Bolt · looseFOUND NINE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER AD 2003-26-01(A) (B) AND BOEING SB 737-55A1087. RETORQUED BOLTS F5, F6, F7, F8, F10 AND REPLACED BOLTS F1, F2, F3, F4 PER SB 737-55A1087.SDR AUS20040181Screw · wrong part(AUS) ELEVATOR CONTROL CABLE RUBBING ON SCREW. INVESTIGATION FOUND (A LONGER THAN NORMAL) SCREW HOLDING THE FORWARD CABIN FLOOR IN POSITION. INCORRECT SCREW HAD BEEN FITTED DURING REUPHOLSTERING CARRIED OUT APPROXIMATELY TWO WEEKS PREVIOUSLY. UNAPPROVED PARTSDR A6WA200460007Rivet · broken6TH RIVET ABOVE PAX WINDOW AT FRAME STATION 755.48, RIVET MISSING HEAD. MAINTENANCE INSTALLED BLIND CHERRY-MAX FASTENER. (M)SDR 072041Screw · looseDURING FLIGHT CONTROL CHECK, CONTROL COLUMN WOULD NOT RETURN TO FULL FORWARD POSITION. INSPECTED AND FOUND ONE SCREW MIGRATED FROM LEFT ELEVATOR, RESET SCREW AND SECURED WITH SPEED TAPE, FERRIED AIRCRAFT TO HEF, FOUND BALANCE WEIGHT ASSY AT O/B ELEVATOR L/E WSDR F3LA200400032Screw · looseDURING C-7 CHECK, INSPECTION REPORTED SCREWS F2 AND F4 WERE FOUND LOOSE PER RUDDER INSPECTION PERFORMED PER EO B3-55-00AD-0001-DY, PART 2, STEPS 2 AND 4. REPLACED BOLTS PER EO B3-55-00AD-004-DY.SDR 374PA0007Bolt · looseFOUND FIVE BOLTS LOOSE DURING INSPECTION OF RUDDER FLANGE BOLTS PER PARA (A) & (B) OF AD 2003-26-01 AND BOEING SB 737-55A1087. REPLACED HARDWARE AT LOCATIONS F1, F2, F3, F4, F10 PER BOEING SERVICE BULLETIN.SDR CALA0400209Bolt · shearedTHE LEADING EDGE DEVICE WAS FOUND HANGING ON RIGHT WING JUST INBOARD OF RIGHT ENGINE DURING WALKAROUND. MAINTENANCE FOUND BOLT FROM LINK SHEARED AND LINK DAMAGED AT KRUEGER SEAL DRIVE. THE LINK AND BOLT WERE REPLACED IAW MM 767-400-27-81-19, PAGE 401. OPERASDR GKZR200482310Rivet · shearedKEELBEAM AREA HAS SEVERAL RIVET HEADS SHEARED OFF BUTTLINE -0-. REMOVED FASTENERS AND DOUBLERS IAW DC-8 SRM 51-1-20. REMOVED CORROSION IAW DC-8 SRM 53-2-0 FOUND OUT OF LIMITS MORE THAN 20 PERCENT ORIGINAL MAT LOSS. FABRICATED DOUBLER REPAIR IAW DC-8 SRM 53-1-SDR AUS20040153Rivet · failed(AUS) RT MAIN LANDING GEAR NR 3 BRAKE ASSEMBLY BRAKE PADS LOCATED BETWEEN NR 2 AND NR 3 ROTORS HAD SEPARATED AND JAMMED THE BRAKE UNIT. INVESTIGATION FOUND PAD SEPARATION WAS DUE TO RIVET FAILURE.SDR AUS20040146Bolt · failed(AUS) RT MAIN LANDING GEAR TOP TORQUE LINK BOLT FAILED.SDR YDB2004F00000Bolt · brokenRETURNING FROM LAST FLIGHT OF DAY PILOTS REPORTED A LOUD BANG IN UPPER MID CABIN AREA. MAINTENANCE INVESTIGATED AND FOUND UPPER CABIN DOOR FWD TORSION BAR ANCHOR BOLT BROKEN. BOLT APPEARS TO HAVE FATIGUE TYPE FAILURE.SDR 513NA0002Bolt · missingMAIN WHEEL BOLTS MISSING. REPLACED NR 8 MAIN TIRE (WHEEL ASSEMBLY) PER MM 32-45-01.SDR CALA0400191Bolt · galledINSPECTION FOUND UPPER BOLT GALLED ON LT HORIZONTAL STABILIZER FORWARD POSITION. THE BOLT WAS REPLACED IAW EA 5510-01696, REV B, OP 1.SDR RO32004F00001Screw · chafed39TH SCREW IB OF RIB 20 ON RT WING UPPER FIXED STRUCTURE BOX RIB 13 TO 20 IS CHAFFING ON HYDRAULIC RETURN LINE FOR RT AILERON SERVO.SDR AUS20040129Bolt · cracked(AUS) RUDDER FIXED HINGE BOLT CRACKED UNDER BOLT HEAD. BOLT IS LOCATED AT VERTICAL STABILISER RIB 5. CRACK LENGTH 2.286MM (0.090IN). FOUND DURING NDT INSPECTION.SDR SWAA040614Bolt · corrodedDURING SCHEDULED D CHECK, FOUND LT MLG SIDE STRUT TO UNIVERSAL ATTACHMENT BOLT CORRODED. REMOVED AND REPLACED BOLT PER MM.SDR SWIA200413031Nut · brokenDISCOVERED DURING C-CHECK INSPECTION, RUDDER LEFT SIDE ANCHOR NUT BROKEN AT CENTER HINGE PANEL ATTACH POINT. REPLACED ANCHOR NUT IAW CRJ SRM 51-45-00. REPLACED SEALANT IAW SRM 51-23-00.SDR CA040310008Bolt · sheared(CAN) UPON APPLICATION OF 27 FT/LBS TO 2 OF THE MOUNTING BOLTS AT THE THREADS FAILED. BOLTS FORWARDED TO COMPANY FOR EVALUATION.SDR CA040308001Bolt · broken(CAN) DURING INSTALLATION OF THE PROPELLER, WHEN TIGHTENING THE BOLTS TO THE SPECIFIC TORQUE OF 25-30 POUNDS FOOT. ONE OF THE BOLTS BROKE AT APPROXIMATELY 27 POUNDS FOOT. THE BOLT BROKE AT THE BASE OF THE THREADS NEAR THE START OF THE GRIP. A SECOND BOLT WASSDR MASA200300091Rivet · shearedA/C WOULD NOT PRESSURIZE AFTER TAKEOFF, MX WAS CALLED. MX FOUND SHEARED RIVETS ON THE PAX DOOR VENT ACTUATOR ROD. MX REPLACED THE RIVETS, OP CHECKS GOOD.SDR QXEA200400158Nut Plate · brokenPDX - MAINTENANCE FOUND SEVERAL NUT PLATES BROKEN ON PANEL 122BR. REMOVED AND REPLACED BROKEN NUT PLATES IAW SRM 51-40-11.SDR NI1R200400001Bolt · shearedNOSE GEAR DID NOT RETRACT AFTER TAKE OFF. GEAR HANDLE SELECTED UP INDICATIONS: ALL THREE GREEN LAMPS OUT, GEAR UNSAFE LAMP STAYS ILLUMINATED, HYDRAULIC PUMP MOTOR CYCLES OFF AFTER A NORMAL PERIOD OF TIME. GEAR SELECTED DOWN INDICATIONS: LT AND RT MAIN GEAR DSDR F3LA200400012Screw · missingFLIGHT CREW REPORTED FASTENER MISSING FROM FLAP TRACK ON RT WING IB OF ENGINE PYLON. PLACED ON MAC 0001276. DETERMINED THIS DID NOT AFFECT SAFETY OF FLIGHT. ON 2/10/04, REPLACED SCREW.SDR CA040211009Screw · out of adjust(CAN) RT ENGINE WOULD NOT MAKE TARGET TORQUE ON TAKE OFF AFTER 'MAX TORQUE' ADJUSTMENT. AIRCRAFT ABORTED TAKE OFF AND RETURNED TO BLOCKS. MAINTENENACE FOUND GOVERNOR INTERFERENCE DUE TO INPROPER SCREW 'X' ADJUSTMENT. SCREW 'X' WAS ADJUSTED TO MANUFACTURERS SDR 2004FA0000236Fastener · chafedDEFLECTION OF LT AILERON UP CAUSES IT TO RUB AGAINST AN EXPOSED RIVET. DEFLECTION OF RT AILERON UP CAUSES IT TO RUB AGAINST TWO EXPOSED RIVETS POSSIBLY HINDERING TRAVEL. (GL13200405339)SDR DAT2004F00007Bolt · crackedDURING THE SCHEDULED MAINTENANCE AD86-06-02 (PROP TORQUE) WAS COMPLIED WITH ON THE RT SIDE. ONE PROP ATTACHMENT BOLT, PN B3339 WAS FOUND CRACKED. ALL (8) PROP ATTACHMENT BOLTS, PN B3339, AND WASHERS PN A2048-2 WERE REMOVED AND REPLACED WITH NEW ONES PURCHASESDR MWEA040013Bolt · misinstalledDURING GEAR RETRACTION A LOUD NOISE COMING FROM THE NOSE GEAR AREA. LT FORWARD NOSE GEAR DOOR RETRACT LINK NOT LATCHED COMPLETELY, FOUND RELEASE HANDLE BOLT INSTALLED IMPROPERLY. REPOSITIONED BOLT CLOSED AND LOCKED FORWARD NOSE GEAR DOOR.SDR 2004FA0000217Nut · crackedNUTS ON SEVERAL HORIZONTAL STABILIZER REAR SPAR BOLTS WERE CRACKED OR BROKEN. NUT INSTALLED, NO NUTS HAD COME OFF AND BOLTS WERE NOT LOOSE IN SPAR. REPLACED NUTS AND NEW BOLTS WITH CURRENT HARDWARE.SDR HJB2004F00000Screw · defectiveBAD LOCKING SCREW.
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