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 FDEA201804021245Spar Cap · crackedRT WING REAR SPAR LOWER CAP AT XORS 446 HAS A 2.0 INCH CRACK AT THE AFT EDGE OF TEE CAP EXTENDING THROUGH THE RADIUS AND TERMINATING 1.0 IN UP THE VERTICAL LEG. REPAIRED PER EA 8-5710-T0340000.SDR Q5QA201805010202Spar · crackedDURING A ROUTINE INSPECTION, THE FORWARD CARRY-THRU SPAR AFT WEB WAS FOUND TO HAVE A SMALL CRACK IN THE UPPER RH CORNER. BEECHCRAFT FRONT SPAR CARRY THRU STRUCTURE REINFORCEMENT DOUBLER KIT 58-4008 HAD BEEN PREVIOUSLY INSTALLED. REPAIRS REQUIRED INSTALLATIONSDR FDEA201803271246Spar Cap · crackedRT WING REAR SPAR LOWER CAP AT XORS 421 HAS A .200 INCH CRACK PROPAGATING FWD OF A PREVIOUS TRIM OUT REPAIR AND EXTENDING INTO THE RADIUS. REPAIRED PER EA 8-5710-T0340000.SDR EE4Y2018041906385Spar · crackedDURING THE INSPECTIONS IAW SB 737-57A1318 R0 AND AD2014-12-13, THE LT WING, REAR SPAR UPPER SECTION CRACKED AT RSS 221. THE DAMAGED SPAR WAS REPAIRED IAW SRM 57-20-10, REPAIR 4.SDR IPXA2018041328528Spar Cap · corrodedINSPECTION TYPE: 3C, RT WING UPPER SURFACE T/E PANEL BULGING AND FASTENERS PULLING THROUGH JUST FWD OF OTBD AILERON. REPAIRED THE WING UPPER SPAR CAP BETWEEN XORS 961.8 TO 1044 IAW EA 011-5710-01-A7202, REV IR, AND EO MD11-5710-68124-A.SDR ABXA20180318020Spar · corrodedCORROSION ON THE RIGHT WING AFT SPAR UPPER ANGLE AT WS 470. THE ANGLE WAS REPAIRED. THE ACFT WAS GROUNDED.SDR IXXA20180405015Spar Cap · corrodedCORRODED UPPER AFT SPAR CAP AT LEFT WS 180. REPAIRED THE SPAR CAP IAW 47313REA05.SDR DALA2018031601727Rib · crackedCRACK ON RIB OF FIXED LEADING EDGE INTERIOR SURFACE SATA XOS 530 APROX LT WING. RIB WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05, DWG 9919331-39 REV N.SDR SWAA2022020931370Spar · out of toleranceSUPPLEMENTAL INFORMATION: RIGHT WING STA 450 REAR SPAR UPPER FASTENER HOLE OUT OF ROUND. / REMOVED FASTENERS AT STA 450 R/H AFT SPAR OVERSIZE UPPER HOLE REAMED TO 261 VISUALLY INSPECTED HOLE FOUND HOLE TRUE ROUND IAW SRM 51-40-05-0G-00 AND BOEING DWG 115A6100 SDR FDEA201802140390Former · crackedLEFT WING LEADING EDGE COMPARTMENT LOWER SURFACE FORMER AT XOS 1025 FOUND CRACKED. THE FORMER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G. FABRICATED FORMER IAW DRAWING ARB2920, REVISION BB. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR SWAA2018032820820Former · crackedRIGHT WING FIXED LEADING EDGE INBOARD FAIRING FORMER CRACKED, WS 70.5. R & R THE FORMER IAW SRM & DWG.SDR DXTA201802090093Spar Web · corrodedLEFT WING SPAR WEB BULKHEAD FITTING CORRODED.SDR IPXA2018030227059Spar Cap · crackedINSPECTION TYPE: 3C, LEFT OUTER WING UPPER REAR SPAR CAP IS CRACKED BETWEEN XORS 1082.3 AND 1090. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A7131, REV I/R, AND EO MD11-5710-67636-A. MAJOR.SDR EE4Y2018030406051Spar · corrodedDURING THE MAINTENANCE INSPECTION, IT WAS FOUND AT THE LT WING L/E CAVITY, THE FRONT SPAR LOWER CHORD FLANGE WITH CORROSION AT WS 583, THE REPAIR WAS CARRIED OUT IAW INSTRUCTIONS AND APPROVED UNDER DOCUMENT COO-SOF-18-0006-04B(R1).SDR IPXA2018022826976Spar Cap · crackedINSPECTION TYPE: 3C, LEFT WING LOWER REAR SPAR CAP CRACKED AT XORS 1085. REPAIRED THE SPAR CAP IAW SRM 57-20-10, REPAIR 1, FIG. 201, SRM 51-38-01, FIG 15, AND SRM 51-38-01, GENERAL, PAR 6 D, REV 64. MAJOR.SDR FDEA201802070570Frame · crackedLEFT WING LEADING EDGE SKIN HAS A .500 INCH. THE CRACK AT THE UPPER INBD CORNER OF THE SLAT ANTI-ICE DUCT CUT OUT. REPAIRED IAW SRM 57-10-00, FIG 104, VOL 1.SDR SWAA2018022720107Spar · corrodedLEFT WING AFT SPAR CORRODED AT UPPER AND LOWER BONDING STRAP ATTACH POINTS FOR NR 1 FUEL BOOST PUMP. REPAIRED THE AFT SPAR IAW EA.SDR KCSA201802021021Spar · corrodedABOVE THE NR 2 PYLON, UPPER WING L/E SPAR HAS CORROSION ON SPLICE PLATE.SDR SWAA2022020756124Stiffener · crackedMAIN LANDING GEAR WHEEL WELL REAR SPAR VERTICAL STIFFENER AT RBL25 CRACKED 2' AT THE BOTTOM. / REMOVED AND REPLACED STIFFENER REF SRM 51-40-02.SDR IPXA2018013026043Spar Cap · corrodedINSPECTION TYPE: 2C, LT WING UPPER REAR SPAR VERTICAL LEG HAS CORROSION AT XORS 480. REPAIRED IAW EA 011-5710-01-A7077, REV IR, AND EO MD11-5710-67214-A.SDR 2018FA0000010Spar · corrodedDURING GENERAL VISUAL INSPECTION OF THE LEFT MAIN WHEEL WELL INSPECTION, FOUND CORROSION ON THE AFT LOWER WING SPAR ASSEMBLY.SDR CA180104006Spar Cap · cracked(CAN) RT WING LOWER FORWARD SPAR CAP CRACKED AT RT WS 58. (TC# 20180104006)SDR CA180104005Spar Cap · cracked(CAN) LT WING LOWER FORWARD SPAR CAP CRACKED AT LT WS 58. (TC# 20180104005)SDR JGVR20171220001Spar Cap · corrodedFOUND CORROSION AROUND TWO LOCK FASTENERS LOCATED IN THE RT WING LOWER SPAR CAP NEAR RWS 49.50. REMOVED AFFECTED LOCK FASTENERS, PERFORMED BLEND AND TREAT REPAIR, AND REPLACED THE FASTENERS WITH NEW 10563M1 RRL.SDR DALA2017121908703Former · crackedCRACKED FORMER RWS 290 AT FIXED LEADING EDGE INTERNAL STRUCTURE. REPAIRED IAW SRM 57-06B, PARA 7, FIG 18.SDR DALA2018010400070Spar Web · corrodedCORROSION LEVEL: 2 CORROSION WAS FOUND ON THE WING CTR SECTION REAR SPAR WEB UNDER THE RT SIDE FRAME FITTING ON THE FS 955 BULKHEAD. C/W ERA 563342-14.SDR FDEA201712113358Spar Cap · crackedL/W WING REAR SPAR AFT LOWER CAP HAS .400 IN. CRACK PROPAGATING AFT FROM FASTENER HOLE AT XORS 412. REPAIRED L/H REAR SPAR CAP REF EA 8-5710-T0336600 PARTS 1 - 4. REPAIR CLASSIFIED AS MAJOR.SDR SWIA201744066Spar · corrodedLT LOWER LANDING OF THE REAR SPAR BETWEEN WS 52 TO 56 CORROSION WAS FOUND. (C-CHECK) REPAIRED CORROSION DAMAGE AT LT WING LOWER PLANK BETWEEN WS53-60 - WS58.88 IAW REO.SDR DALA2020111803771Spar · crackedA CRACK WAS FOUND IN FASTENER HOLE COMMON TO LT WING REAR SPAR/MLG SUPPORT RIB. CORRECTIVE ACTION: COMPLIED WITH ER/A 563876-14AD AND ER/A 588640-14AD.SDR 2017FA0000578Spar · corrodedRIGHT WING SPAR INSPECTED IAW SB 1006. FOUND TO BE CORRODED WITH INTERGRANULAR CORROSION ON FORWARD FACE OF SPAR WEB, UPPER SPAR CAP IN FRONT OF LANDING GEAR STRUT HOUSING. RIGHT WING REMOVED AND REPLACED.SDR 2018F00026Spar · corrodedCORROSION IN LEFT AND RIGHT WING AFT SPAR COVES.SDR 2018F00027Spar Cap · corrodedREPAIR OF LEFT AND RIGHT WING REAR SPAR CAP CORROSION.SDR 8HBR20180412011Spar · crackedCRACKS FOUND IN BOTH MAIN WING SPARS AT MLG SUPPORT BRACE TRUNNION FITTING ATTACK POINT. 1 CRACK PER WING IS APPROXIMATELY 1 INCH RUNNING BETWEEN THE NUTPLATE RIVET HOLES. 1 CRACK PER WING APPROXIMATELY 2" RUNNING LATERALLY ALONG LOWER RADIUS OF SPAR.SDR MTNA20171020001HSpar · corrodedCORROSION ON THE RT WING SPAR.SDR COEA2017101539804Spar · corrodedWO 176596 NR 600031 HEAVY CHECK COE/MAJOR REPAIR: R/H WING SKIN RIB 9 LOWER REAR SPAR HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS PCE-2735/17...12148 DATED 11/23/2017.SDR FDEA201710122911Frame · crackedLEFT WING LEADING EDGE CAVITY FRAME FOUND CRACKED AT XOS 801. THE FRAME WAS REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW FRAME IAW DRAWING ARB2922, REV B. INSTALLED THE NEW FRAME AIW SRM 51-35-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR 2018F00007Spar · corrodedLEFT AND RIGHT AFT WING SPAR WEB BULKHEAD FITTING CORRODED.SDR JGVR20171003001Spar Cap · corrodedMECHANICALLY BLENDED 5 AREAS OF CORROSION ON THE RT WING UPPER SPAR CAP AT WING STATIONS 190, 121.7, 99.7, 96.7 AND 88.7 AND 4 AREAS OF CORROSION ON THE LT WING UPPER SPAR CAP AT WING STATIONS 104.5, 119.5, 130.5 AND 141.0. FOUND TO BE BEYOND LIMITS IAW SRM 51SDR IPXA2017100522345Spar Cap · corrodedINSPECTION TYPE: 1C, LEFT WING REAR SPAR UPPER CAP HAS CORROSION AT XORS. 897 TO 1042.3. REPAIRED THE SPAR UPPER CAP IAW EA 011-5710-01-A7015, REV I/R, AND EO MD11-5710-65911-A.SDR CALA2017092203266Spar · corrodedRIGHT OTBD FLAP FRONT SPAR FWD FACE HAS CORROSION OTBD OF THE NR 3 FLAP TRACK INSIDE CAVITY PANEL NR 2. BLENDED CORROSION AND OUT OF LIMITS IAW SRM 51-73-11. REMOVED AND REPLACED THE RT OTBD FLAP FRONT SPAR WEB AT THE FLAP TRACK IAW SRM 57-53-21-300-004.SDR HYIA20170921002Spar Cap · corrodedCORROSION WAS DISCOVERED ON THE AFT LOWER OUTBOARD SPAR CAP. CORROSION WAS FOUND AT RWS 107.21 TO 111.781 ON THE BOTTOM OF THE HORIZONTAL LEG OF THE CAP. DEEPER THAN THE ALLOWABLE LIMITS IAW MEB 91-11 R1, SECTION 3, ITEM B. THE SPAR CAP WAS REPLACED.SDR HYIA09052017001Spar Cap · corrodedCORROSION WAS DISCOVERED IN TWO PLACES INSIDE THE FUEL TANK, ON THE FORWARD VERTICAL LEG OF THE RT AFT OUTBOARD SPAR CAP. ONE OF THE AREAS OF CORROSION WAS AT WS 219.2 TO WS 229.71. THE OTHER AREA OF CORROSION WAS AT WS 208.7 TO WS 215.7. BOTH AREAS OF CORROSDR QXEA2017091100753Spar Cap · gougedFWD SPAR, YW-32.0, LOWER CAP SPLICE ANGLE GOUGED, FASTENERS HEAVILY DAMAGED AND SPAR WEB GOUGED ABOVE SPLICE ANGLE. BLENDED GOUGES ON FWD SPAR WEB AND LWR SPAR CAP JOINT ANGLE. WITHIN LIMITS IAW RD 84-57-3791. REMOVED THE FWD SPAR JOINT PLATE IAW RD 84-57-37SDR HYIA09012017001Spar Cap · corrodedWHILE CONDUCTING OTHER MAINTENANCE, CORROSION WAS DISCOVERED IN TWO PLACES INSIDE THE FUEL TANK, ON THE FORWARD RADIUS OF THE LH AFT OUTBOARD SPAR CAP (P/N 5122041-21.) THE FIRST AREA WAS FOUND AT W.S. 228.71 TO W.S. 225.71. THE SECOND AREA WAS DISCOVERED AT WSDR DXTR2017082901Spar Cap · corrodedCORROSION ON THE RT AFT LOWER SPAR CAP INSIDE WHEEL WELL BOX, REPAIRED.SDR FDEA201708282387Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 1 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708282385Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 4 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708282384Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 10 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708282383Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 52 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA 6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201708282382Spar · crackedLEFT REAR SPAR INTERNAL ANGLE NR 60 HOLE FOUND CRACKED DURING AN NDT INSPECTION. REPAIRED IAW EA:6-5710-T0335292 P1. MAJOR REPAIR IAW GMM 6-2-100.
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