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 = '5751' 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 = '5751' 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 04FDEA01092Skin · wornLEFT WING INBOARD AILERON, LEADING EDGE SKIN PART NUMBER ARC1283-7 IS WORN BEYOND LIMITS AND NEEDS TO BE FABRICATED. LIMITS DOCUMENTED ON CARD N00519. MATERIAL ID PANEL AND FABRICATED PANEL IAW DOUGLAS DRAWING ARC1283. PART TO BE INSTALLED ON N00519.SDR 04FDEA001101Skin · erodedRT OUTBOARD AILERON TRAILING EDGE, INBOARD END IS ERRODED. CUTOUT AND REPLACED DAMAGED SECTION, FABRICATED ZEE FOR REPAIR IAW DC-10 SRM 57-20-00 FIGURE 10 VOLUME 1.SDR 04FDEA001099Skin · crackedRT OUTBOARD AILERON INBOARD SUDE HAS SKIN SEPERATING AND CRACKED. FABRICATED NEW SKIN SECTION AND REPAIR DOUBLERS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. INSTALLED REPAIR PARTS IAW DC-10 SRM 57-10-00 FIGURE 6 VOLUME 1. COMPLIED WITH WEIGHT AND BALANCE, AILESDR 04FDEA001092Skin · wornLEFT WING INBOARD AILERON, LEADING EDGE SKIN PART NUMBER ARC1283-7 IS WORN BEYOND LIMITS AND NEEDS TO BE FABRICATED. LIMITS DOCUMENTED ON CARD N00519. MATERIAL ID PANEL AND FABRICATED PANEL IAW DOUGLAS DRAWING ARC1283. PART TO BE INSTALLED ON N00519.SDR DHL2004803526Skin · crackedRT WING AILERON INBD L/E FASTENER HOLE, SKIN CRACKED 0.500, STA XA 500.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-8-1 PAGE 2 SRM 57-1-0 PAGE 1. REMOVED CRACKED PLATE IAW SRM 51-1-21, SRM 51-3-0 PAGE 1. FABRICATED NEW PLATE (7075 T6 AL 0.040) IAW SDR GAIA04068OPSkin Panel · missingON POST FLIGHT INSPECTION FOUND RT OB AILERON DAMAGE AT IB LOWER SURFACE EDGE IB PANEL MISSING FROM AILERON. AIRCRAFT LANDED WITHOUT INCIDENT. INSTALLED MISSING PANEL AT IB HINGE LEADING EDGE. REPAIRED DAMAGED IB LOWER SURFACE EDGE IAW SRM, SHEET (5) PG 169SDR 04FDEA00782Fitting · crackedLEFT WING INBOARD AILERON HINGE FITTING AND WEB IS CRACKED. REMOVED AND REPLACED WEB IAW SRM 51-10-1, REMOVED AND REPLACED AILERON HINGE FITTING IAW SRM 51-10-1 AND BOEING DWG 65-21709.SDR DHL2004803513Structure · crackedRT WING OTBD AILERON L/E PLATING CRACKED 0.250 AROUND STA XA 646.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-8-01 FIG 4 PG 9. REMOVED CRACKED PLATING IAW DC8 SRM 51-1-21 PG 1. FABRICATED NOSE PLATING (2024-T3 0.032) IAW DCSDR 04FDEA00686Fitting · crackedRIGHT INBOARD AILERON O/B HINGE SUPPORT FITTING CRACKED. REMOVED SUPPORT FITTING IAW M/M 53-23-01, RECEIVED SUPPORT FITTING WITH TRAVLER T4/414610, FIT AND DRILLED IAW SRM 51-35-01 AND INSTALLED SUPPORT FITTING IAW SRM 53-33-01.SDR CALA0400261Panel · brokenINSPECTION FOUND LEFT AILERON PANEL 8106L BROKEN AT CENTER OF PANEL. REPAIRED IAW SRM 51-70-05.SDR 2004UALA00233Fitting · crackedI/B ACTUATOR FITTING CRACKED. REPLACED ACTUATOR FITTING.SDR AWXA200400284Panel · separatedMCN - MAJOR REPAIR - DURING C-15 CHECK FOUND THE LT AILERON LEADING EDGE PANEL LAND SEPARATING AT SECOND HINGE FROM OUTBOARD END WS 574.698. MAINTENANCE PERFORMED A BOND REPAIR ON LT AILERON LEADING EDGE PANEL LAND IAW B737-300 SRM 51-70-17 FIG 20 PG 26 & 57.SDR AWXA200400235Skin · delaminatedMCN - MAJOR REPAIR - DURING C-20 CHECK FOUND THE RT AILERON LEADING EDGE ACCESS PANEL LOWER LAND DELAMINATED 33.5 INCHES FROM THE INBOARD END. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-17, REPAIR 6, FIG 2, 6, 8 & 20.SDR AALA20040367Fitting · crackedAFW - RIGHT HAND INBOARD AILERON HINGE FITTING HAS A TIME LIMITED REPAIR INSTALLED AT WING STATION 467. CRACK LENGTH INITIALLY MEASURED AT 1.24 INCHES. FINAL MEASUREMENT AT 1.70 INCHES. REMOVED TIME LIMITED REPAIR (STRAP) AND REPLACED WITH PERMANENT REPAIR SDR AALA20040308Hinge Fitting · crackedAFW - RIGHT HAND AILERON HINGE FITTING HAS A TIME LIMITED REPAIR INSTALLED AT WING STATION 467. CRACK LENGTH INITIALLY MEASURED WAS 1.24 INCHES AND FINAL MEASUREMENT IS 1.70 INCHES. REMOVED TIME LIMITED REPAIR (STRAP) AND REPLACED WITH PERMANENT REPAIR (CUP)SDR 0390Hinge Fitting · crackedVISUALLY DETECTED LT OB AILERON CENTER HINGE FITTING CRACKED.SDR TZ02004F00000Hinge · crackedCONDUCTED ANNUAL INSPECTION ON AIRCRAFT. FOUND BOTH LEFT AND RT AILERON CONTROL ROD ATTACH POINTS TO CONTROL SURFACES TO BE CRACKED. SPECULATE DAMAGE MAY HAVE BEEN INDUCED BY WIND ACTION AND LACK OF USE OF CONTROL SURFACE LOCK.SDR UPS04841844Bracket · crackedINSPECTION TYPE: C3, RIGHT O/B AILERON HINGE BRACKET IS CRACKED AT STATION 610.882. REMOVED AND REPLACED BRACKET IAW DWG 3653812 AND SRM 51-1-21.SDR UPS04841849Panel · corrodedINSPECTION TYPE: C3, LT WING OUTBOARD AILERON WEIGHT PANEL IS CORRODED BEYOND LIMITS BETWEEN XA 614 TO XA 638. REMOVED, FABRICATED AND REPLACED WEIGHTED PANEL IAW DWG 5764617 AND DOUBLER IAW DWG 5763133 AND SRM 51-1-21, 51-3-0.SDR DHL2004806561Skin · crackedITEM REF. NR. 1305: RT IB AILERON L/E WITH 1.500 CRACK AROUND FASTENER HOLE STA XA 502.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR, REMOVED DAMAGED AREA. FABRICATED NEW SKIN (7075-T6AL 0.040) CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INNER SIDE. APPLIEDSDR C2XA04TY022Fairing · gougedTYS DURING A SCHEDULED INSPECTION A GOUGE WAS FOUND ON THE RIGHT HAND AILERON TO PCA INBOARD FITTING. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EC5750-01177 AND CPM 51-21-05AND 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR AWXA200400023Spar · delaminatedMCN - MINOR REPAIR - DURING C-18 CHECK THE RT AILERON FORWARD SPAR LOWER FLANGE WAS FOUND DELAMINATED AT ACCESS PANEL ATTACHMENT WS 430. MAINTENANCE TRIMMED OUT DAMAGE ON RT AILERON FORWARD SPAR, LOWER FLANGE; CLEANED AND PREPARED SURFACE; PERFORMED BOND REPAISDR 2004FA0000540Attach Fitting · corrodedFOUND SEVERE GALVANIC CORROSION BETWEEN THE AILERON ATTACH BRACKETS AND REAR SPAR IN SEVERAL LOCATIONS. STEEL HAD ORIGINALLY BEEN CADIMUM PLATED. THIS WAS CRITICAL AS IT COULD ALLOW THE AILERON TO DEPART THE AIRPLANE. COULD NOT FIND A PN IN THE CATALOG AS TSDR COOSDR030088Skin · delaminatedLT WING, OB AILERON PN65-21766-19, SN BN319 TRAILING EDGE DELAMINATED.SDR COOSDR030054Skin · delaminatedRT WING, AILERON (PN-65-46454-2) SN 305, SKIN DELAMINATED.SDR COOSDR030034Skin · delaminatedLT WING, OB AILERON TRAILING EDGE LOWER SURFACE DELAMINATED.SDR QXEA200301598Structure · damagedPDX - A HOLE WAS FOUND IN THE JOINT OF THE TRAILING EDGE OF THE RIGHT AILERON, 2 INCHES FROM THE OUTBOARD TIP. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE IAW THE D-8 SRM, 200, 57-40-00. THE AILERON WAS BALANCED IAW SRM 57-60-71.SDR DHL2003742545Rib · crackedDURING C-CHECK, LT WING O/B AILERON INTERNAL RIB CRACKED (11TH) FROM O/B. REMOVED AILERON INTERNAL RIB CRACKED 11TH FROM O/B IAW B727 SRM 51-30-2. FABRICATED NEW RIB 11TH FROM MAT 7075-T6 .025 PO 9912281 DIM14.125 X 5.5 INCH IAW B727 SRM 57-20-2 FIG 8. TREASDR DHL200374245Rib · crackedDURING C-CHECK, LT WING O/B AILERON INTERNAL RIB CRACKED (11TH) FROM O/B. REMOVED AILERON INTERNAL RIB CRACKED 11TH FROM O/B IAW B727 SRM 51-30-2, FABRICATED NEW RIB 11TH FROM MAT 7075-T6 .025 PO 9912281 DIM 14.125 X 5.5 INCH IAW B727 SRM 57-20-2 FIG 8. TREASDR QXEA200301531Skin · crackedRT AILERON HAS A SMALL .25 INCH CRACK IN OUTBOARD TAB HINGE CUTOUT. REPAIRED IAW DHC-8 SRM 57-60-71 AND HORIZON AIR EA 2-57-244.SDR DHL2003802576Hinge Fitting · crackedNR 6 LEFT AILERON HINGE FITTING CRACK. REMOVED NR 6 LEFT AILERON HINGE FITTING IAW MM 20-16-0 PG 208. REFER TO JC 8-27-11-026 FOR NEW NR 6 LEFT AILERON HINGE FITTING INSTALLATION.SDR DHL2003802577Hinge Fitting · crackedNR 4 LT AILERON HINGE FITTING CRACK. REMOVED AND REPLACED NR 4 LT AILERON HINGE FITTING IAW MM 20-16-0 PG 208.SDR DHL200374246Skin · separatedDURING A C-CHECK, LT WING OUTBOARD AILERON HAS THREE LOOSE RIVETS IN UPPER SKIN. REMOVED OLD SKIN FOR LT WING O/B AILERON IAW B727 SRM 51-30-2, FABRICATED NEW SKIN O/B AILERON FROM MAT 2024-T3 .020 PO900355 DIM 121 X 15.25 INCH AND DOUBLER SKIN FROM MAT 2024-SDR CA031114009Spar · cracked(CAN) AS A FOLLOW UP INSPECTION ON THE REST OF OUR FLEET FOLLOWING THE DISCOVERY OF THE CRACKED AILERON SPAR ON OUR AIRCRAFT, THE LT AILERON SPAR WAS FOUND CRACKED ON THIS AIRCRAFT. THE CRACKS ARE ALL LOCATED IN THE SAME AREA AS PREVIOUSLY REPORTED AND ARE APSDR CA031113004Spar · cracked(CAN) DURING ANNUAL INSPECTION A CRACK WAS NOTED ON THE AILERON SPAR AT IB HINGE FITTING ATTACH POINT. THE CRACK IS APPROXIMATELY .5000 INCH IN LENGTH, AND STARTS AT THE IB END OF THE SPAR AND IS RUNNING SPAN WISE APPROXIMATELY .1250 INCH BELOW THE IB LOWER FSDR QXEA200301448Skin · damagedPDX- RIGHT HAND AILERON TOP SKIN HAS A BURN HOLE AT RIVET ON TRAILING EDGE. REPAIRED IAW DHC-8 RD 8-57-2702 AND HORIZON AIR EA 2-57-241.SDR CA031013001Balance Weight · cracked(CAN) UPON INSPECTION IT WAS DISCOVERED THAT THERE WERE SMALL HAIRLINE CRACKS (HORIZONTAL) AT THE THREE MOST OUTBOARD MASS BALLANCE WEIGHT ATTACH SCREW LOCATIONS. ONE INCH IN LENGTH.SDR 0704022Skin · delaminatedRT WING AILERON DELAMINATED AT WBL 481SDR 2003FA0001020Control Cable · misinstalledTHE PILOTS CONTROL WHEEL EMITS A GRINDING NOISE WHEN OPERATING THE AILERONS. FOUND THE AFT AILERON CONTROL CABLE WAS FOUND TO BE INCORRECTLY ROUTED INSIDE THE PILOTS CONTROL COLUMN. THE CABLE TENSION WAS LOW AND THE TURNBUCKLE WAS ADJUSTED TO THE END OF ITS TSDR IXXA060530SFitting · crackedDURING ROUTINE C CHECK, FOUND RT WING INBOARD AILERON INBOARD HINGE FITTING CRACKED. REMOVED CRACKED FITTING. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0.SDR AWXA200301088Web · chafedLCQ - MAJOR REPAIR - DURING C-16 CHECK THE LT WING INBOARD AILERON ATTACH HINGE SUPPORT WEB WAS FOUND CHAFED. MAINTENANCE CUTOUT CHAFED AREA OF LT WING INBOARD AILERON ATTACH HINGE SUPPORT WEB; FABRICATED A SPLICE REPAIR; INSTALLED REPAIR PART IAW B737-300 SRMSDR 0021Sprocket · defectiveDURING COMPLIANCE, THE AILERON SPROCKET WAS FOUND TO HAVE A POSSIBLE DEFECT. DOING A VISUAL INSPECTION BETWEEN THE TWO GEARS OF THE AILERON SPROCKET, ON THE LARGE GEAR NEAR THE SHAFT AREA, IT APPEARS THE WELDING MAY NOT HAVE BEEN COMPLETED IN A SMALL AREA, APSDR 2003UALA00648Fitting · crackedI/B & O/B ACTUATOR FITTINGS CRACKED. LEFT AILERON WAS REPLACED.SDR 2003F00652Skin · damagedFOUND C-CHECK SERVICE, LEFT WING AILERON UPPER SKIN WITH WEAR, STA 370, INBOARD HINGE. (M)SDR 2003FA0001019Rod End · brokenPLANE CAME IN FOR ANNUAL. CUSTOMER REPORTED AILERON CONTROL STIFF. UPON MOVING YOKE TO CONFIRM STIFFNESS. RT AILERON ROD END AT AILERON BROKE. IT BROKE WHERE THREADED PORTION MEETS BEARING. REMOVED ROD END AND FOUND BEARING WAS FROZEN. ALL MOVEMENT WAS IN THE SDR SWAA031820Aileron · delaminatedDURING SCHEDULED PM CHECK, FOUND RT AILERON DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED RT AILERON PER MM.SDR AMCR200300003Hinge Fitting · looseDURING PILOT'S PREFLIGHT, NOTICED THE RIGHT AILERON, INBOARD SIDE, HAVING EXCESSIVE PLAY. FURTHER INSPECTION REVEALED THAT THE TWO BOLTS (AN4-12A)HOLDING THE INBOARD AILERON HINGE AND THE OUTBOARD FLAP HINGE WERE LOOSE. THIS ALLOWED THE AILERON HINGE BRACKET TSDR 2003UALA00682Fitting · crackedLT & RT AILERON INBD AND OUTBOARD PCU FITTINGS CRACKED. LT AND RIGHT AILERONS WERE REPLACED.SDR 2003FA0000974Rib · crackedDURING INSPECTION OF LT AILERON, FOUND ALL THREE AILERON ATTACH POINT RIBS CRACKED ADJACENT TO MOUNTING BELL CRANKS.SDR QXEA200300936Aileron · chafedPDX- LEFT AILERON BOTTOM FORWARD HAS CHAFE 12 INCHES FROM INBOARD EDGE. REPAIRED IAW CRJ SRM 51-20-06, 51-25-01 AND 51-21-11.
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