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 UPS01836330Doubler · brokenINSPECTION TYPE:C2 LEFT WING LOWER FRONT SPAR STRAP AND DOUBLER ARE BROKEN AT XS 520. REMOVED, FABRICATED AND REPLACED DOUBLER AND STRAP IAW SRM 57-2-1 FIG 14A.SDR 2002FA0000347Spar · crackedTROUBLE AREA IN THE REGION OF LIFT STRUT ATTACHMENT POINT, REMOVED VARNISH AND SMALL AMOUNT OF WOOD, COULD IDENTIFY SMALL CRACK IN THE GLUE JOINT ON REAR FACE OF RT REAR WING SPAR. ALSO DETECTED ON UPPER EDGE OF RT REAR SPAR A TOTAL OF 5 COMPRESSION TYPE CRASDR CA010810013Spar · cracked(CAN) BOTH WINGS WERE STRIPPED OF FABRIC & L/E MATERIAL REMVD DURING INSP. BOTH WING TIPS WERE REMVD ALONG WITH FUEL TANKS & AILERON BELLCRANKS. SPARS WERE BLOWN WITH COMPRESSED AIR THEN WASHED DOWN WITH MILD SOAP & WARM WATER. THE INSP THEN PROCEEDED USING HISDR UPS01836379Spar Cap · crackedINSPECTION TYPE:C2 STA 855 LT WING REAR SPAR LOWER CAP IS CRACKED FROM XCW 0 TO XCW 10. REPAIRED SPAR IAW 8110-3 APPROVED DH SK 807-357.SDR 2001FA0000081Spar · crackedBOTH FRONT SPARS HAD SEVERE CRACKS AT ATTACH POINTS INTO BUSHINGS.SDR 2001FA0000104Spar · corrodedWHILE RE-SKINNING THE LEFT UPPER INBOARD WING SKIN, WE FOUND CORROSION IMMEDIATELY OUT BOARD OF THE LEFT MAIN LANDING GEAR CASTING ON THE LOWER AFT SIDE OF THE MAIN SPAR INSIDE THE WING. THE CORROSION SEEING TO BE CENTRALIZED AROUND ONE RIVET AND RADIATING OUSDR COOSDR010044Spar · crackedWING - CENTER WING BOX - REAR SPAR CRACKED - STA 663.0/ RBL6.150/ WL 170.4SDR QXEA0101120Spar · corrodedPDX - LEFT-HAND WING FORWARD SPAR, LOWER FLANGE WHERE LEADING EDGE ATTACHES HAS MILD FRETTING CORROSION BETWEEN STATION 178 THROUGH 225. REPAIRED IAW HORIZON AIR EA 2-57-114.SDR ABXA010395Spar Cap · crackedRIGHT WING AFT UPPER SPAR CAP WAS CRACKED BETWEEN XCW 69.5 AND XCW 46. REPLACED RIGHT WING UPPER SPAR CAP BETWEEN XCW 0 TO XRS 74.8 IAW REA D857-41242MR.SDR DL72W011018Spar · chafedFOUND ON F1 LETTER CK, MLG AUX SPAR CHAFED AT INBD END. REPAIRED PER MM 57-43-000-8.SDR QXEA0101100Spar · gougedPDX - LEFT-HAND WING FORWARD SPAR, UPPER FLANGE AT STATION 285 THROUGH STATION 325 HAS SEVERAL GOUGES IN FLANGE SURFACE. REPAIRED IAW RD 8-57-1119.SDR 2002FA0000242Spar · failedCRACK IN REAR SPAR OF LEFT WING OUTBOARD OF DOUBLER AT SPAR ATTACH FITTING. WING HAS HIT GROUND BEFORE WHEN INBOARD LANDING GEAR BOLT FAILED. TIP OF FORWARD SPAR HAS REPAIR AND DOUBLER.SDR 2001F00583Spar Cap · corrodedDURING FUEL TANK INSPECTION, CORROSION ON LEFT AND RIGHT WING LOWER SPAR CAP AT WING STATION 124.5 WAS NOTED. (M)SDR 2001F00417Spar Cap · corrodedDURING C-CHECK, FOUND CORROSION IN THE NR 3 ENGINE WING SPAR FITTING BULKHEAD UPPER CAP NR 3 ATTACH HOLE. THE CORROSION WAS REMOVED AND THE UPPER CAP WAS REPAIRED IAW EA 10-5720-24-A0865. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR AUS20010629Spar Cap · corroded(AUS) RH WING UPPER SPAR CAP CONTAINED PITTING CORROSION IN AN AREA LOCATED 355.6MM (14IN) OUTBOARD OF THE ENGINE NACELLE. THE PITTED AREA MEASURES APPROXIMATELY 152.4MM (6IN) SPANWISE AND 19.05MM(0.75IN) CHORDWISE. DEPTH OF CORROSION APPROXIMATELY 0.508MM(0.0SDR MWEA010852Spar · damagedPREVIOUS REPAIR, LEFT WING AFT SPAR AFT SIDE STATION XRS 164. REMOVED REPAIR, DRILLED AND INSTALLED LOWER SPAR T SECTION.SDR QXEA0100930Spar Cap · chafedPDX - LOWER, LEADING EDGE SPAR CAP CHAFED AT YW57-60, AT LEADING EDGE PANEL 611AR, INBOARD ATTACH POINT. REPAIRED IAW RD 8-57-811, STEP 4, PAGE 3.SDR 2001FA0000019Spar · crackedCRACK ON BOTTOM SURFACE OF SPAR, LEFT SIDE REAR. (BUTT) FOUND PRIOR TO CRACK INSPECTION AS PER AD OWNER DISCONTINUED ANNUAL INSPECTION PRIOR TO FULL INSPECTION.SDR DL72S010908Spar · crackedAT HMV FOUND FAST SPAR LWR CHORD - CRACK, REPAIR LOOSE LOC AT LWR END OF NR 7 SPOILER ACT FITTING. REMOVED NR 6/7 SPOILER MOUNT ARM, REMOVED DAMAGED SECTION OF BEAM PER MM 57-55-00-08 FIG 805, FABD AND DRILLED UP PARTS PER MM 57-55-00-08 FIG 805, OK TO INSTALSDR UPS01236103Spar · crackedINSPECTION TYPE:C, LEFT WING REAR SPAR UPPER CHORD AT WING STATION APPROX CRACK INDICATION IS ABOUT 2 INCHES LONG OUTBOARD OF NR 1 FUEL SOV. REMOVE CRACK AT REAR SPAR UPPER CHORD AT WS 190 AND INSTALL FILLER AND DOUBLER REPAIR AS PER BOEING DRAWING 65C196447,SDR AALA20011149ASpar · corrodedTUL - FOUND RIGHT WING FORWARD SPAR CORRODED AT LOWER CHORD 8 INCHES INBOARD OF DEFUEL VALVE BELOW NR 4 L/E FLAP ACT MOUNT. CUT OUT DAMAGED MATERIAL AND INSTALLED DOUBLER PER ESO 11697. (M)SDR 0102056626Spar · corrodedDuring L-check found corrosion on Rt wing front spar web at OLES 1381 outboard and behind stiffener. Repaired per EA 66-183239.SDR CA010628043Spar · cracked(CAN) TO CARRY OUT AD 2000-25-02, ADDITIONAL HOLES WERE CUT IN EACH LOWER WING PANEL. NO PROBLEMS WERE FOUND. REMOVED WING ROOT FAIRINGS AND FABRIC ON TOP OF BOTH WINGS JUST TO BE SURE IN WING ROOT AREA. FOUND BOTH FWD SPAR ROOT ATTACH POINTS CRACKED AT THE ENSDR QXEA0100871Spar · scratchedPDX - LEFT-HAND WING, OUTER WING, FORWARD SPAR, LOWER FLANGE HAS LIGHT SCRATCHING FROM LEADING EDGE REMOVAL ALONG ENTIRE LENGTH. REPAIRED IAW HORIZON AIR EA 9-57-577 AND RD 8-57-1675.SDR AALA20011066Spar · corrodedTUL - FOUND CORROSION AT RIGHT WING AFT SPAR BOOST PUMP LOWER BOND JUMPER AREA. REPAIR PER ESO 90309 DATED 05-15-2001. (M)SDR QXEA0100872Spar · scratchedPDX - LEFT-HAND WING, OUTER WING, FORWARD SPAR, UPPER FLANGE HAS LIGHT SCRATCHING FROM LEADING EDGE REMOVAL ALONG ENTIRE LENGTH. REPAIRED IAW RD 8-57-1119.SDR CALA0100458Spar · crackedINSPECTION FOUND A 0.1 INCH CRACK IN RT REAR SPAR UPPER CHORD AT RT MLG BEAM O/B END AFT SPAR FITTING ATTACH AREA. THE CRACK WAS REPAIRED IAW ECRA 5743-01033. A DIP WAS ISSUED TO REINSPECT THE AREA AT 3,000 FLIGHT CYCLE INTERVALS.SDR QXEA0100893Spar · scratchedPDX - RIGHT-HAND WING FRONT SPAR TOP CAP SCRATCHED ALONG SEALANT LINE BETWEEN STATION YW261 AND YW297. REPAIRED IAW DHC-8 RD 8-54-119.SDR 0102486638Fitting · crackedIn M check, found crack at L wing aft spar kick fitting #2 bolt hole. Repaired per EA66-162195.SDR 20010511CW010Spar Cap · crackedDURING AN ANNUAL INSPECTION, A CRACK APPROX 3 INCHES LONG WAS FOUND ON LEFT WING AFT SPAR, UPPER AFT CAP. BELOW BAGGAGE RACELLE.SDR 20010613CW023Spar · corrodedDURING THE INSTALLATION OF SHOULDER HARNESS KITS THE HEAD LINER WAS REMOVED. CORROSION WAS PRESENT AT FORE AND AFT UPPER, SPAR CAPS AND SKINS. OWNER WAS ADVISED. FURTHER INSPECTION FOUND CORROSION PRESENT UNDER LEAD SHEETS IN THE SAME AREA. LEFT AND RIGHT SDR AALA20010992Spar · corrodedTUL - FOUND CORROSION ON FRONT SPAR UPPER CHORD ABOVE NR 5 SLAT ACTUATOR. INSTALLED REPAIR ANGLE PER ESO 11697, DATED 5-1-01. (M)SDR 2002FA0000238Spar · crackedINSPECTED AIRCRAFT AS PER AD, FOUND LEFT AFT SPAR HAS COMPRESSION CRACK AT OUTBOARD END OF DOUBLER PLATES FOR STRUT ATTACH FITTING.SDR GAIA01184STSpar · corrodedDURING A LTC INSPECTION, THE LEFT FRONT SPAR LOWER CHORD WAS DISCOVERED CORRODED BELOW NR 3 SLAT OUTBOARD TRACK. ACCOMPLISHED LEFT WING LOWER SPAR CHORD REPAIR FSS 450 IAW REPAIR ORDER FASI-009RO-1 REV IR DATED 4/26/02. (M)SDR GAIA01183STSpar · corrodedDURING A LTC INSPECTION, THE LEFT LOWER SPAR CHORD WAS DISCOVERED CORRODED AT WING LEADING EDGE STATION 305 THROUGH STATION 325. ACCOMPLISHED LEFT WING LOWER SPAR CHORD REPAIR FSS 327 IAW REPAIR ORDER FASI-0099O-1 REV IR DATED 4/26/01. (M)SDR AUS20010430Flange · cracked(AUS) AFT WING SPAR WEB FLANGE CRACKED ON THE LH SIDE IN THE AREA OUTBOARD OF THE ATTACHMENT FITTING. FOUND DURING INSPECTION IAW AD/P68/22, AD/P68/45 AND SB 65.SDR MWEA010711Spar · damagedREWORK PREVIOUS REPAIR, CENTER FUEL TANK LEFT WING FORWARD SPAR AFT FACE BETWEEN XCW 58 AND 79 (3 BLEND OUTS, FROM IB .070, .020 APPROXIMATELY 1 INCH DIAMETER AROUND FASTENERS) UPPER SPAR. BLENDED AREAS, INSTALLED TENSION MINI-NUTS AND WASHERS.SDR MWEA010709Spar · damagedREWORK PREVIOUS REPAIR ON RIGHT WING FORWARD SPAR AFT FACE BETWEEN XCW 58 AND 79, APPROXIMATELY 1 INCH AROUND FASTENERS. BLENDED AREAS, INSTALLED TENSION NUTS AND WASHERS.SDR AALA20010904Spar Cap · corrodedTUL - FOUND CORROSION ON UPPER REAR SPAR CAP AT STATION WS 160-204 ALSO HAS BULGING FASTENERS. FABRICATED 2 REPAIR STRAPS AND ATTACH ON LOWER SIDE OF WING SKIN LAND. THE LOWER STRAP THAT IS AGAINST WING SKIN SHOULD EXTENDED ONE ROW OF FASTENERS BEYOND THE UPSDR AUS20010552Spar Cap · corroded(AUS) RH WING UPPER SPAR CAP CORRODED IN THE AREA OF THE FORWARD HINGEEDGE AND FORWARD CAP FLANGE.SDR AUS20010535Spar · corroded(AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED IN AREA BETWEEN RIB 13 AND RIB 18.SDR TSAA0153043Spar · corrodedEXFOLIATED CORROSION DISCOVERED ON RIGHT UNDER WING T/E AFT SPAR LOWER APPROXIMATELY 21 INCHES OUTBOARD OF WBL 355 SKIN PANEL. CLEANED AND TREATED AS EP SRM 51-10-6 PAGE 12. EVALUATED AND REPAIRED IAW ECO 3213. AIRCRAFT RETURNED TO SERVICE. (M)SDR ABXA010200Spar · corrodedTHE REAR SPAR UPPER PLANK WAS FOUND TO HAVE INTERGRANULAR CORROSION, BELOW AND ADJACENT TO SLAT PANEL 24 INCHES TO THE LEFT OF THE KEEL. MAINTENANCE REPAIRED THE AREA IAW ABX REA D957-40679.SDR CA010509005Spar Cap · chafed(CAN) WE HAVE FOUND CHAFING AT YW279 LT & RT ON THE WING REAR SPAR CAP, BEHIND THE NR 1 AND NR 4 NACELLES. THIS CHAFING IS CAUSED BY A WIRE BUNDLE IN BOTH LOCATIONS. WE HAVE SEEN THIS DAMAGE IN THREE EARLIER MAINTENANCE PROJECTS, ON THE FOLLOWING AIRCRAFT:(1) SDR CA010509004Spar Cap · chafed(CAN) WE HAVE FOUND CHAFING AT YW279 LT & RT ON THE WING REAR SPAR CAP, BEHIND THE NR 1 AND NR 4 NACELLES. THIS CHAFING IS CAUSED BY A WIRE BUNDLE IN BOTH LOCATIONS. WE HAVE SEEN THIS DAMAGE IN THREE EARLIER MAINTENANCE PROJECTS, ON THE FOLLOWING AIRCRAFT:(1) SDR CA010509003Spar Cap · chafed(CAN) WE HAVE FOUND CHAFING AT YW279 LT & RT ON THE WING REAR SPAR CAP, BEHIND THE NR 1 AND NR 4 NACELLES. THIS CHAFING IS CAUSED BY A WIRE BUNDLE IN BOTH LOCATIONS. WE HAVE SEEN THIS DAMAGE IN THREE EARLIER MAINTENANCE PROJECTS, ON THE FOLLOWING AIRCRAFT:(1) SDR CA010509002Spar Cap · chafed(CAN) WE HAVE FOUND CHAFING AT YW279 LT & RT ON THE WING REAR SPAR CAP, BEHIND THE NR 1 AND NR 4 NACELLES. THIS CHAFING IS CAUSED BY A WIRE BUNDLE IN BOTH LOCATIONS. WE HAVE SEEN THIS DAMAGE IN THEE EARLIER MAINTENANCE PROJECTS, ON THE FOLLOWING AIRCRAFT: (1) SDR MWEA010601Spar · corrodedRIGHT WING INTERNAL AFT LOWER SPAR TEE HAD HEAVY CORROSION. FABRICATED REPAIR FILLERS, INSTALLED IAW BOEING TELEX MWX-ORD-01-00272H, DATED 03 APRIL 2001. PLACED ON WATCH ITEM 5720 FOR FINAL DISPOSITION.SDR MWEA010594Spar · gougedREMOVED LEFT WING SPAR WEB AT TRUNNION AND FOUND GOUGES OUT OF LIMITS. FABRICATED, DRILLED AND INSTALLED NEW WEB SECTION.SDR MWEA010578Spar Cap · corrodedLEFT WING INTERNAL HAS LIGHT CORROSION ON LOWER TEE CAP LEG FORWARD OF AFT SPAR AT APPROX XRS 67. LOCATED, DRILLED, AND DEBURRED HORIZONTAL FLANGE OF SPAR CAP AND VERTICAL FLANGE OF SPAR CAP. INSTALLED FASTENERS.
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