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 CALA9700031Web · crackedINSPECTION FOUND A 2 INCH CRACK IN FORWARD SPAR WEB OF LT WING AT WS 780. THE WEB WAS REPAIRED IAW SRM 51-40-02, FIGURE 1.SDR DLL13970118Spar Web · fatigueDURING INSP OF CENTER WING TANK, FS 1043, 1103, 1163 SPAR WEBS WERE FOUND WITH A MISSING ROW OF FASTENERS AT LBL AND RBL 116 END RIBS. THIS WAS A MANUFACTURE DEFECT. NUMEROUS CRACKS WERE FOUND EMANATING FROM THE HOLES.SDR CA961230007Spar · cracked(CAN) CRACK FOUND AT THE RADIUS OF THE REAR SPAR WING ROOT FITTING.SDR CKSA96389Spar Web · corrodedDURING C-1 CHECK INSPECTION, FOUND RIGHT WING AFT UPPER SPAR WEB CORRODED AT STA XRS -6.0. REMOVED PARTS AND CORROSION IAW DRAWING AIA/E/2424, EA 96-348 REPORT 96 AIA-197 DATED 12-12-96. CORROSION CARD NR 124R-0551. NON-ROUTINE TASK CARD NR 91051, LEVEL 2.SDR CKSA96362Spar · corrodedDURING C-1 CHECK INSPECTION, FOUND LEFT WING UPPER REAR SPAR STA XRS295 HAS SEVERE CORROSION, WITH SEPARATION. REPAIRED IAW SKETCH NR AIA/E/2415. CORROSION CARD NR 117L-0551. NON-ROUTINE TASK CARD NR 88649, LEVEL 2.SDR 97ZZZM106Spar · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND LEFT WING MAIN TANK REAR SPAR LOWER FLANGE XW 58.458 HAS A .125 CRACK FROM RADIUS TO A FASTENER HOLE. (M)SDR 96FDEA01701Spar Web · mis-manufacturedNR 1663 RT WING, FRONT SPAR WEB MILLED BEYOND DRAWING 65C29064 SPECIFICATIONS. FABRICATED NEW SPLICES AND INSTALLED SPICES PER EA 7-5710-28952DATED 12/10/96 AND ACCOMPLISHED REMAINING EA 7-5710-28952 DTD 12/10/96 INSTRUCTIONS.SDR HAL960130Spar · corrosionDURING C-CHECK, FOUND CORROSION AROUND HI LOCK FASTENERS AT FRONT SPAR LOCATION LOWER SKIN AT RIGHT WING AT STATION XORS 376. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER ESO 7349, DATED 12/5/96. (M)SDR COMA9610367Spar Cap · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR CAPS, LOWER LT AND RT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR COMA9610366Spar Web · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR WEB LT AND RT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.SDR 96ZZZX6159Spar · crackedINSP SPAR CARRY-THROUGH WEB STRUCTURE. FOUND LT FWD AND AFT RT FWD CORNERS CRACKED. THIS AIRCRAFT IS 4 SERIAL NUMBERS NEWER THAN BEECH AD 90-18-14 APPLIES TO. SUBMITTER STATED AD 90-18-14 NEEDS REVISING TO INCLUDE NEW AIRCRAFT.SDR CKSA96354Spar Cap · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: FORWARD LOWER SPAR CAP CRACKED AT OUTBOARD SPLICE. REPAIRED LOWER SPAR CAP CRACK IAW AIA ENGINEERING SKETCH NR'S AIA/E/2335, AIA/E/2337, AIA/E/2340, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82127.SDR CKSA96353Spar Cap · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: FORWARD UPPER SPAR CAP CRACKED AT OUTBOARD SPLICE. REPAIRED UPPER SPAR CAP CRACK IAW AIA ENGINEERING SKETCH NR'S AIA/E/2234, AIA/E/2341, AIA/E/2336, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 82126.SDR CKSA96352Spar Cap · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: RIGHT WING AFT SPAR LOWER CAP CRACKED AT STA 408 SPLICE. REPAIRED IAW DRAWING AIA/E/2285, AIA/E/2342, AIA/E/2343 AND DAC DRAWING NR 5613922. REFERENCE REPORT 96AA-156, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NSDR CA961218006Spar · failed(CAN) ON LANDING, THERE WAS A MAJOR FAILURE OF THE RIGHT WING STRUCTURE BETWEEN THE NACELLE AND THE FUSELAGE. TSB INVESTIGATING. PART TC: 22,672.SDR 97ZZZM8Spar · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XRS 109 LOWER AUX SPAR UPPER FLANGE IS CORRODED.SDR 97ZZZM7Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK XW 58.768 REAR SPAR LOWER CAP TO STRINGER 11 WAS CORRODED.SDR 97ZZZM64Spar · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT MAIN TANK REAR SPAR LOWER CAP XRS 70 HAS CORROSION AROUND 1 FASTENER.SDR 97ZZZM46Spar Cap · corrodedDURNIG SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK AFT SPAR LOWER CAP SHELF IS CORRODED XRS 67-89.SDR 97ZZZM44Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE LEFT WING TANK FORWARD SPAR LOWER CAP XRS 115 IS CORRODED.SDR 97ZZZM37Spar · damagedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE RIGHT WING AFT SPAR LOWER SPAR CAP FS 699 XRS 86 HAS A .375 INCH HOLE .090 DEEP WITH A AREA 1.25 INCH BLEND OUT .060 DEEP.SDR 97ZZZM20Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK REAR SPAR CAP LOWER FLANGE XRS 92-97 IS CORRODED.SDR 97ZZZM15Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FUOND RIGHT WING TANK REAR SPAR CAP XRS 69-91 LOWER CAP HAS CORROSION ON LOWER FLANGE AND LOWER FLANGE TO WEB SHELF.SDR 97ZZZM14Spar · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING TANK STATION 88 REAR SPAR HAS .5 INCH CRACK EMANATING FROM FASTENER.SDR DLL15962722Spar · crackedSEVERAL HOLES IN THE RT REAR SPAR, UPPER CAP AND UPPER WING SKIN WERE FOUND CRACKED FROM THE FASTENER HOLES.SDR UPS96821754Spar Cap · crackedINSPECTION TYPE-C, NR 2 TO NR 4 LEFT HAND LEADING EDGE SPAR ATTACHMENT HOLES HAVE CRACKS. REAMED HOLES 2 + 3 TO .500 REAMED HOLE 4 TO .747 NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHINGS ANGLE DOUBLERS, FILLERS AND STRESS COI NED ALL HOLES IAW DAC DWG J0SDR UPS96821756Spar Cap · crackedINSPECTION TYPE-C, NR 2 TO 5 HOLES HAVE CRACKS ON RT L/E SPAR ATTACHMENT HOLE INB OF NR 4 PYLON REAMED HOLES 2, 4, 5 TO .500 AND NR 3 HOLE TO .747, NO CRACKS NOTED. FABRICATED AND INSTALLED BUSHINGS, STRAPS, FILLERS AND ANGLES IAW DAC DW G J06032 AND DC8 SDR CALA9601888Spar Web · crackedINSPECTION FOUND A 2 INCH CRACK IN OUTBOARD RADIUS OF RT WING TRAILING EDGE REAR SPAR WEB AT STA XCW 58. THE AREA WAS REPAIRED IAW DOUGLAS DRAWING 593528.SDR RAIA961138Spar · damagedSTL - FOUDN RIGHT WING AFT SPAR IS DAMAGED, OUTBOARD OF RIB 28. REPAIRED DAMAGED AREA OF AFT SPAR PER ATR DRAWING ATR25512/96. (M)SDR DLL10962663Spar · corrodedTHE CENTER WING REAR SPAR AT FS 1212 WAS FOUND WITH CORROSION ON THE UPPER WEB AT RBL 102.SDR CKSA96200Spar · corrodedDURING C-4 CHECK INSPECTION, FOUND RIGHT UPPER WING SPAR HAS CORROSION. REPAIRED IAW DC-8 SRM 57-2-1 FIGURE 38. CORROSION CARD NR 121R-0552 AND 112R-0551, NON-ROUTINE TASK CARD NR 87403.SDR UPS96821753Spar · crackedINSPECTION TYPE-C, CRACK INDICATIONS NOTED HOLE F IN SPAR, HOLES C AND D IN SKIN/SPAR INTERFACE OF RT WING C/W S/B 57 88 PER UPS EO DC8 5730.SDR 96ZZZX6071Spar · corrodedDURING C-CHECK, FOUND CORROSION IN NR 1 TANK ON AFT SPAR XW58.50 TO XRS111.5.SDR UPS96221748Spar Chord · corrodedINSPECTION TYPE-C, CENTER WING TANK FWD LOWER SPAR CHORD SEVERELY CORRODED FROM LBL 26 TO LBL 40 REF N/R 588971. REMOVED AND REPLACED SPAR CHORD IAW SRM 51-30-2, 51-30-10, 51-30-1.SDR 96ZZZX6025Spar Cap · corrodedFOUND CORROSION ON RT WING SPAR FITTING INSIDE RT FUEL TANK WHILE C/W PHASE 50H INSPECTION AND SB 28-10 FOAM REMOVAL. CLEANED CORROSION TO .040 INCH DEPTH. REMOVED ALL PITTING. CONTRACTED FACTORY. MAJOR REPAIR REQUIRED EVEN THOUGH AREA OF CORROSION WAS LESSDR DL72K962563Spar Stiffener · crackedLE SPAR STIFFENER CRACKED AT NR 3 SLAT INBD TRACK. REPAIRED PER M/M 57-20-21.SDR 97ZZZX698Spar · corrodedDURING A PRELIMINARY INSPECTION OF AIRCRAFT. HEAVY INTERGRANULAR CORROSION WAS FOUND IN THE AFT CABIN SPAR HAT SECTION. PART WAS REMOVED AND REPLACED. AIRCRAFT WAS BASED IN CENTRAL FLORIDA. NO PRIMER PROTECTION NOTED.SDR 97ZZZX697Spar · corrodedDURING A PRELIMINARY INSPECTION ON THE AIRCRAFT, HEAVY INTERGRANULAR CORROSION WAS FOUND IN THE FWD CABIN SPAR. PART WAS REMOVED AND REPLACED. AIRCRAFT WAS BASED IN CENTRAL FLORIDA. NO PRIMER ON INTERNAL PARTS BY CESSNA.SDR 97ZZZX696Spar Channel · corrodedHEAVY INTERGRANULAR AND SURFACE CORROSION WAS FOUND ON FWD SPAR CHANNEL OF RT WING. REMOVED AND REPLACED SPAR CHANNEL WITH NEW CESSNA PART. AIRCRAFT WAS BASED IN CENTRAL FLORIDA. PARTS NOT PROTECTED WITH PRIMER BY CESSNA.SDR 97ZZZX695Spar Channel · corrodedHEAVY INTERGRANULAR AND SURFACE CORROSION WAS FOUND ON FWD SPAR CHANNEL OF RT WING. REMOVED AND REPLACED PART WITH NEW CESSNA PART. AIRCRAFT WAS BASED IN CENTRAL FLORIDA. NO PRIMER PROTECTION.SDR 97ZZZX694Spar Cap · corrodedHEAVY INTERGRANULAR AND SURFACE CORROSION FOUND IN RT WING FWD SPAR CAP. REMOVED AND PRELACED PART WITH NEW CESSNA PART. AIRCRAFT WAS BASED IN CENTRAL FLORIDA. PARTS WERE NOT PROTECTED WITH PRIMER AT TIME OF MANUFACTURE.SDR 97ZZZX690Spar · corrodedHEAVY INTERGRANULAR CORROSION ON OUTBOARD SPAR CHANNEL LT WING. RMEOVED ADN REPLACED PART. AIRCRAFT BASED IN CENTRAL FLORIDA. WINGS DID NOT HAVE ANY PRIMER PROTECTION FROM FACTORY.SDR 97ZZZX689Spar · corrodedCORROSION ON AFT SPAR CHANNEL STA 105. REMOVED AND REPLACED PART. AIRCRAFT WAS BASED IN CENTRAL FLORIDA. PARTS DID NOT HAVE ANY PRIMER PROTECTION FROM FACTORY.SDR 97ZZZX688Spar · corrodedHEAVY SURFACE CORROSION ON AFT SPAR OF LT WING BETWEEN STA 148-137. REMOVED AND REPLACED PART. AIRCRAFT WAS BASED IN CENTRAL FLORIDA. PART HAD NO PRIMER PROTECTION FROM FACTORY.SDR CALA9700015Fitting · crackedINSPECTION FOUND SPLICE FITTING AND UPPER SPLICE PLATE CRACKED AT LT WING REAR SPAR. THE CRACKS WERE 0.040 AND .25 INCH LONG. THE SPLICE PLATE AND SPLICE FITTING WERE REPLACED IAW EA 5710-01199 AND BOEING SB 57-2110.SDR CALA9700021Spar Web · crackedINSPECTION FOUND A .1875 INCH CRACK AT FASTENER HOLE OF NR 2 PYLON WING FRONT SPAR VERTICAL WEB AT INBOARD NACELLE RIB POST ATTACH AREA, WS 688. THE FRONT SPAR VERTICAL WEB WAS REPAIRED PER BOEING DRAWING 112U8040, FCD 5710-01758 AND SRM 51-10-01.SDR UPS96221489Spar · corrodedINSPECTION TYPE: SI. CORROSION L/W LOWER SPAR CHORD IS CORRODED 28 TO 30 OF I/B END AT OUTER RADIUS. REPAIRED SPAR CHORD (LOWER) IAW TRAMCO EWO 96-2549 (UPS EO FILE NR 727-57-1745).SDR DLL13962478Spar Cap · crackedA FASTENER WAS FOUND CRACKED IN THE LT LOWER SPAR CAP AND SKIN. IT AND THE ADJACENT FASTENER HOLE WERE O/S. THE HOLES WERE COLD-WORKED AND INSTALLED WITH HI-LOKS.SDR DHL9672044CSpar · corrosionAT C-CHECK, LEFT WING L/E SPAR LOWER CHORD HAS EXFOLIATION CORROSION JUST FWD AND I/B OF NR 3 SLAT, WS 519. REMOVED CORROSION, FOUND OUT OF LIMITS. INSTALLED REPAIR PER SRM 57-10-6 AND S/B 57-145, DOUBLER 12 BY 4.SDR 96FDEA01597Spar Chord · corrodedNR0172 - 001, CORROSION (C53-132-02-01) ON LOWER 740 CHORD AT LBL 4. *S/D* REMOVED CORRODED BS 740 FRONT SPAR LOWER CHORD AND INSTALLED NEW BS 740 FRONT SPAR LOWER CHORD PER FEDEX EA NR 7-5710-31160.
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