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 = '5711' 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 = '5711' 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 KQ72002F00001Spar · corrodedDURING C5 AND C6 CHECK, GPCP VISUAL INSPECTION OF WING REAR SPAR FOR CORROSION, DISCOVERED SEALANT COVERING UP SPAR. MECH REMOVED SEALANT IN SAMPLING AREAS, FOUND PREVIOUS REPAIRS FOR CRACKING AND BLEND OUT AREAS OF CORROSION AND CRACKING. PERFORMED NDT INSSDR QXEA0201442Spar · chafedPDX- RIGHT HAND WING FORWARD SPAR BOTTOM FLANGE IS CHAFED WITH BARE METAL AT STATION YW57.000. REPAIRED IAW DHC-8 RD 8-57-811.SDR AUS20020995Spar Cap · corroded(AUS) LH WING LOWER REAR SPAR CAP CORRODED IN AREA BETWEEN THE VERTICAL FLANGE AND THE SPAR WEB. CORRODED AREA IS LOCATED FORWARD OF THEAILERON FROM WS 206 TO WS 229.SDR AUS20021019Spar Cap · corroded(AUS) LH AND RH WING LOWER FORWARD SPAR CAPS CONTAINED SEVERE EXFOLIATION CORROSION IN AREA LOCATED AT WS 62 DUE TO ENGINEEXHAUST GASSES. AT LEAST 10% OF THE SPAR CAP MATERIAL IS AFFECTED BUT CAN ONLY BE SEEN WITH THE FUEL TANK BAYS REMOVED.SDR CA020912011Spar · cracked(CAN) RT WING REAR SPAR CRACKED AT STA 200.SDR CA020913009Spar · cracked(CAN) CRACK FOUND IN THE FUEL CELL STIFFENER SPAR ON THE WING.SDR CA020826008Doubler · cracked(CAN) LT WING LOWER SPAR CAP DOUBLER CRACKED AT OUTER BOLT HOLE.SDR AUS20020928Spar · corroded(AUS) LH WING INBOARD SPAR LOWER SPAR CAP ASSEMBLY SEVERELY CORRODED. CORROSION IS INITIATED BY INGRESS OF EXHAUST GASSES THROUGH A FUEL DRAIN HOLE IN A PANEL FORWARD OF THE SPAR. THE FUEL DRAIN IS PART OF CANCELLED AD/PA30&39/20.SDR CA020830020Spar · cracked(CAN) - INSPECTION REVEALED CRACK AT BOTTOM ANGLE OF AILERON HINGE. FURTHER INSPECTION REVEALED CRACKED REAR SPAR AT HINGE ATTACH POINT AND CRACKED RIB STA 109. INSPECTION OF RIB AND REAR SPAR IS DIFFICULT BECAUSE OF LACK OF INSPECTION PANELS. THE INSPECTIONSDR TSAA0253182Spar · crackedRIGHT WING FRONT SPAR CRACK AND CORRODED AT FSS124.79 AND FSS134.80. AIRCRAFT RETURNED TO SERVICE.SDR UPS02239199Spar · corrodedINSPECTION TYPE:C SUSPECT CRACK ON RT WING REAR SPAR UPPER CHORD AT APPROX WS 198 AND WS 194. UPPER CHORD HORIZONTAL FLANGE BLENDED TO REMOVE DAMAGE AT WS 196, WS 201 AND WS 205 IAW SRM 51-10-6. ADDITIONAL CORROSION FOUND AT 3 FASTENER LOCATION BETWEEN WS 17SDR AUS20020934Fitting · corroded(AUS) LT AND RT REAR SPAR ATTACHMENT PLATES CORRODED. ATTACHMENT ANGLEFLOOR PLATE ATTACHMENT RIVETS CORRODED AND RIVET HEADS MISSING.SDR DHL2002721516Spar · corrodedDURING C-CHECK, LT WING UPPER FRONT SPAR ATTACH TO L/E WS 140/150 CORROSION UNDERNEATH L/E SKIN. REMOVED CORROSION FROM FRONT SPAR UPPER CHORD UPPER SURFACE WS 140 TO WS 150. MAT LOSS BEYOND ALLOWABLE LIMITS. FABRICATED 2 SPAR CHORD REPAIR ANGLES. INSTALLESDR 02FDEA00638Spar · crackedRIGHT REAR SPAR CHORD CRACKED APPROX BS 200.SDR DLM88020903Spar · damagedPERMANENT REPAIR FOR DAMAGE TO THE LT WING FRONT SPAR. DAMAGE RESULTED IN SPLICING IN NEW SECTION OF LOWER WING SKIN AT XRS540, SPLICING LOWER SPAR CHORD AT XFS 563 AND LEADING EDGE REPAIR AT XFS 596.SDR 2002FA0000873Spar · crackedDURING ANNUAL INSPECTION SB1006 PERFORMED. FOUND CRACKS AND CORROSION IN AFT REAR SPAR FLANGE-APPROX 3 INCHES OUTBOARD OF LANDING GEAR ATTACH. CAUSE DUE TO STANDING WATER IN WING. FIX BY ADDING DRAIN HOLE IN THIS AREA.SDR DHL2002806533Spar Cap · corrodedLT WING INBOARD LEADING EDGE UPPER CAP SHOWS CORROSION AND CRACK BETWEEN XFS 20.000 AND XFS 195.000. REMOVED CRACKED UPPER CAP IAW SRM 51-1-20D PAGE 21 AND SRM 51-1-21. INSTALLED NEW UPPER CAP IAW SRM 57-3-3 PAGE 5 DRAWING 9750482, SRM 51-1-21 PAGE 1, SRM 51SDR QXEA0201071Spar Cap · gougedPDX- THERE ARE GOUGES AND SCRATCHES IN UPPER SPAR CAP OF RIGHT HAND WING FROM STATION YW297 TO YW324. REPAIRED IAW DHC-8 RD 8-57-2054.SDR DHL2002806854Skin Panel · corrodedITEM N/R 0762 RH WING CTR SPAR SKIN CORRODED AROUND STA. XRS 34.500CORR: PERFORMED MAJOR REPAIR IAW EO DHL020609 ED-3094, EO SEMAN 2002683 REMOVED CORROSION ON RH WING IAW SRM 51-1-8 PG. 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG. 16 REMOVED FASTNERS IAW SRMSDR 2002FA0000831Spar Cap · crackedDURING COMPLIANCE WITH AD 00-25-02R1, THE RIGHT WING REAR SPAR WAS FOUND TO HAVE A COMPRESSION CRACK AT THE AILERON CENTER HINGE ATTACH BRACKET, UPPER HOLE. THE CRACK IS VISIBLE ON THE FORWARD AND AFT FACE OF THE SPAR EXTENDING UP FROM THE BOLT HOLE AND ACROSSSDR CA020730005Spar · cracked(CAN) WING SPARS, RIGHT FRONT WING WITH SMALL CRACKS FROM NAIL HOLES VARIOUS LOCATIONS. RIGHT REAR SPAR WITH CRACK FROM TIP DAMAGE PREVIOUS.BOTH SPARS REPLACED.SDR CA020715002Spar Cap · cracked(CAN) CRACK FOUND AT REAR LOWER SPAR CAP AT WS51 AND FS434 DURING NDT REQUIRED BY AD 92-26 WHOSE REQUIREMENTS ARE EVERY 600 FLIGHT HOURS OR 2000 WATER DROPS, WHICHEVER COMES FIRST.THE NDT INDICATION IS OF A 1/4 INCH CRACK AND IS NOT VISIBLE. THIS AIRCRAFT HAD SDR QXEA0200994Spar Cap · scratchedPDX - RT WING FRONT SPAR BOTTOM CAP SCRATCHED BETWEEN YW207 AND YW279. REPAIRED IAW RD 8-57-1119.SDR QXEA0200993Spar Cap · scratchedPDX - RT WING FRONT SPAR TOP CAP SCRATCHED APPROXIMATELY 10 INCHES LONG OUTBOARD OF YW279. REPAIRED IAW RD 8-57-1119.SDR QXEA0200992Spar Cap · scratchedPDX - RT WING FRONT SPAR TOP CAP SCRATCHED APPROXIMATELY 10 INCHES LONG AT YW225. REPAIRED IAW RD 8-57-1119.SDR QXEA0201003Spar · chafedPDX - CENTER, AFT WING SPAR FLANGE HAS CHAFING FROM LEFT HAND WING YW48.00 TO RIGHT WING YW48.00. REPAIRED IAW RD 8-57-1434.SDR ARWA20020806Spar · crackedDURING C-CHECK, LEFT WING FRONT LOWER SPAR WITH CRACKS, STA XFS 526.7 (0.125 INCH) AND STA XFS 518 (1.25 INCH). ACCOMPLISHED REPAIR OF LEFT WING FRONT SPAR LOWER OUTBOARD CAP IAW RED SKETCH 02-07-11-001 SHEET 1 TO 6. BOEING MESSAGE ARW-MIA-02-00016H. THIS RSDR AUS20020674Web · cracked(AUS) WING SPAR INNER WEB CRACKED. FOUND DURING INSPECTION IAWAD/SWSA226/86.SDR CA020722013Spar · cracked(CAN) ALL 4 SPARS REPLACED DUE TO SMALL CRACKS AT NAIL HOLES, EDGE OF PLYWOOD REINFORCING AS A PRECAUTIONARY MEASURE. NO LARGE CRACKS FOUND.4 NEW METAL SPARS INSTALLED.SDR CA020718010Spar · corroded(CAN) WING SPAR CENTRE SECTION LOWER FORWARD CAP ANGLE VERTICAL FLANGE LEG WHERE RIVETED TO SPAR WEB HAS 25 PERCENT LOSS OF THICKNESS IN SEVERAL AREAS PROBABLY DUE TO INTERGRANULAR STRESS CORROSION. NO STRUCTURES REPAIR MANUAL EXISTS FOR THICKNESS LIMITS. ANOTSDR 2002FA0000995Spar · crackedFRONT WING SPAR WEB WAS CRACKED IN THE SAME LOCATION ON BOTH WINGS JUST ABOVE THE LOWER SPAR CHORD AT THE LANDING GEAR BEAMSDR 1001Spar · crackedFORWARD WING SPAR WEB WAS CRACKED IN THE SAME LOCATION BOTH SIDES STA. 85 CENTER WING. 3 DIFFERENT LOWER WING STRINGER ATTACH ANGLES CRACKED IN THE SAME FASHION CWS 216 LT SIDE. LOWER WING STRINGER CRACKED CWS 216 LEFT. LEFT WING LOWER SKIN CRACKED CWS 218.SDR UPS02838858Spar Cap · damagedINSPECTION TYPE:C2 RIGHT WING REAR SPAR UPPER CAP HAS ELONGATED HOLES BETWEEN XRS 456 AND XA 500. OVERSIZED HOLES, NDT VERIFIED NO CRACKS AT HOLES, FABRICATED AND INSTALLED BUSHINGS IAW 8110-3 APPROVED SAA SK 730-143, AND UPS ENGINEERING FILE NUMBER DC8-57-20SDR UPS02238798Spar · corrodedINSPECTION TYPE:C+SI DURING INSPECTIONS OF THE WING CENTER SECTION AFT SPAR AREA AIR CON, TWO FASTENERS FOUND POPPED ON THE WING CENTER SECTION REAR SPAR LOWER CHORD VERTICAL FLANGE AT BS 870 LBL38. NDT CONFIRMS CORROSION PRESENCE. REAR SPAR CHORD AND ASSOCISDR 2002FA0000762Spar · crackedDURING INSPECTION PER AD2000-25-02 R1 CRACKS FOUND IN LT FRONT SPAR APPROXIMATELY THE OUTBOARD 3 FEET AND ON THE RT FRONT SPAR FROM THE STRUT ATTACH POINT OUTBOARD. RIB NAILS MISSING ON THE RIB JUST OUTBOARD OF THE STRUT ATTACH POINT AND SPAR DAMAGE ACROSS THSDR 2002F01101Spar Cap · crackedFOUND DURING DOUGLAS D-CHECK INSPECTION, RIGHT WING LOWER FRONT SPAR CAP FORWARD TANG APPROXIMATELY STATION 520 SPAR CAP HAS CRACK. REMOVED INTERNAL REPAIR ANGLE FOR EVALUATION IAW DC-8 SRM 51-1-20D. REPAIR IS ACCEPTABLE AS TEMP REPAIR PER BOEING LETTER TEK-SDR ASAA0210144Frame · crackedPAE - DURING SCHEDULED C-CHECK, FOUND CHORD AT LEFT WING STATION 126 CRACKED. REPAIRED REAR CHORD PER SRM. (M)SDR 2002F00762Spar · crackedTHE RIGHT WING REAR SPAR WEB WAS CRACKED AT INBOARD AILERON, INBOARD ACTUATOR FITTING W.S 606.20. MAINTENANCE REPAIRED THE SPAR WEB IN ACCORDANCE WITH SRM 57-11-00, FIG 813.SDR AUS20020505Spar · cracked(AUS) WING SPAR INNER WEB CRACKED IN TWO PLACES. CRACK LENGTH 12.7MM (0.5IN) LOCATED AT THE UPPER CENTER OF THE PORT STRINGER 13 CUTOUT. CRACK LENGTH 12.7MM (0.5IN) LOCATED AT THE LOWER RH CORNER OF THE STARBOARD STRINGER 13 CUTOUT. FOUND DURING INSPECTION IAWSDR COOSDR02126Spar · corrodedWING CENTER SECTION, FRONT SPAR LOWER CHORD FROM RBL 24.5 TO RBL 70.5, CORRODED.SDR IXXA0200071SWing · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING UPPER LEADING EDGE OUTBOARD OF NUMBER FOUR PYLON. REPAIR ACCOMPLISHED REOMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERMAL DOUBLER IN ACCORDANCE WISDR AK62002F00000Bracket · corrodedUPON REMOVAL OF WING TO STUB WING ATTACHMENT PANELS FOR AN ANNUAL INSPECTION. A SEVERELY CORRODED UPPER REAR SPAR ATTACH BRACKET WAS FOUND. THIS FITTING HAS SEVERE INTER GRANULAR CORROSION. THE AIRCRAFT IS BASED OUT OF TEXAS AND HAS SPENT LOTS OF TIME ON THSDR AUS20020506Strap · faulty(AUS) AIRCRAFT HAS HDH SPAR STRAP MODIFICATION FITTED. INVESTIGATIONFOUND NO EVIDENCE OF ONGOING NDT INSPECTION IAW HDH EDD/6 ISSUE 2 BEING CARRIED OUT. NDT TECHNIQUE IS NOT POSSIBLE IN THIS MODELAIRCRAFT.SDR DL72E020609Spar · crackedINSPECTION OF THE CENTER WING REAR SPAR WEB PER AD 2000-14- 07 AND BAC S/B 727-57A0182 REVEALED A .25 INCH CRACK IN THE WEB BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE WEB WITH A 2 INCH CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ERSDR CA020530011Spar · cracked(CAN) SPARS CRACKED AT HINGE ATTACH AS A RESULT OF FLAPS - FLAPPING IN WIND WHEN TIED DOWN.SDR GAIA02060STSpar · corrodedDURING A C-CHECK INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED LEFT WING FRONT SPAR LOWER CHORD IS CORRODED UNDER AND INBOARD OF EXISTING REPAIR INSIDE L/E COVE AREA AT LES 200-240. ACCOMPLISHED LEFT WING LEADING EDGE LOWER SKIN AND SPAR CHORD REPAIR IAW AVITASSDR GAIA02061STSpar · corrodedDURING A C-CHECK INSPECTION AT FLIGHT STAR, IT WAS DISCOVERED LEFT WING FRONT SPAR UPPER SURFACE AT WS 410 IS CORRODED. ACCOMPLISHED LEFT WING FRONT SPAR LOWER CHORD UPPER SURFACE REPAIR IAW B727 SRM 57-30-4 FIG 6. (M)SDR CA020529001Spar · cracked(CAN) WHILE PERFORMING THE INSPECTION REQUIRED BY SID 57-10-02 ON WING STATION 9 OF THE LOWER FORWARD SPAR. CORROSION WAS FOUND IN THIS AREA ON THE FORWARD SIDE OF THE FORWARD SPAR, REMOVAL OF THE FORWARD PRESSURE PLATE REVEALED THE CORROSION EXTENDED FROM LT SDR IXXA0200064SSpar · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON TOP OF THE LEFT WING INTERSPAR SKIN BETWEEN XRS 190 INBOARD TO WING WALK AREA TO INCLUDE THE MAIN SKIN EXTENSION OVER GEAR TRUNNION AREA. REPAIR ACCOMPLISHED CORROSION REMOVAL. FABRICATION AND INSTASDR IXXA0200063SSpar · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE UPPER WING EXTERNAL PLATING BETWEEN WING STATION XFS 172 AND XFS 255. REPAIR ACCOMPLISHED, CORROSION REMOVAL OF THE DAMAGE ARE, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH
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