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 06FDEA1614Spar · corrodedCORROSION RT WING REAR SPAR UPPER SURFACE BETWEEN BS 786-799. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.SDR 06FDEA1613Spar · corrodedCORROSION LT WING REAR SPAR UPPER SURFACE BETWEEN BS 738-773. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL2 AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG16 VOL1.SDR UPS06M46814Spar Cap · corrodedINSPECTION TYPE:1C LT WING UPPER O/B TRAILING EDGE FIXED PANEL I/B LEADING EDGE BULGING OUT JUST O/B OF NR 5 SPOILER. BULGE FOUND TO BE EXFOLIATION CORROSION. REMOVED CORROSION AND REPAIRED IAW SAA EA 011-5700-01-A0173, UPS ENGINEERING FILE MD11-57-20057, ANSDR BSAASDR0609Spar · corrodedTWO SPOTS OF PITTING CORROSION WAS FOUND ON THE LOWER FORWARD FACE OF THE LEFT WING SPAR AT APPROXIMATELY WS 125 TO 128, JUST AFT AND JUST INBOARD OF THE FWD WING SUMP DRAIN OUTBOARD OF THE NACELLE. TIME SINCE LAST INSPECTION 8 MONTHS. CORROSION WILL BE DRESSDR CA060419002Spar · crackedCRACK WAS NOTICED DURING AN ANNUAL INSPECTION WITH THE AID OF FLASHLIGHT AND MIRROR. THE DEFECT AREA IS JUST AFT OF THE NR 2 ENGINE FIREWALL THROUGH AN INSPECTION PANEL LOCATED ON THE WING UPPER SURFACE. MORE INFORMATION TO FOLLOW CONFIRMING THE CRACK(S) WITSDR DHL2006764519Stiffener · crackedLT WING FRONT SPAR VERTICAL STIFFENER AT WS 90 SHOWS CRACK FROM BOTTOM END. REMOVED FASTENERS FOR ACCESS IAW SRM 51-30-2 HFEC AT ANGLE MARKED END OF CRACK NDT MAN PART6 51-00-00 FIG23 STOP DRILLED .250 END OF CRACK IAW SRM51-10-1 FAB REPAIR MAT USED 7075 T6 .SDR 06FDEA1437Spar · corrodedFOUND LEFT WING, REAR SPAR AT ABOUT XORS 1042 CORRODED. CORRODED AREA AT LEFT HAND WING - REAR SPAR LOWER CHORD AT ABOUT XORS 1042 REPAIRED AS PER FEDEX E.A. #1-5710-95809, TITLE: WINGS - LEFT HAND REAR SPAR LOWER CAP AFT TANG UPPER SURFACE CORROSION SDR QXEA200601091Spar · crackedPDX - C4 LEFT WING LEADING EDGE 511AL LOWER MOUNT FITTING BY NACELLE ON FORWARD SPAR IS CRACKED. REPAIRED IAW DHC-8-200 SRM 51-40-00.SDR QXEA200601090Spar · crackedPDX - C4 RIGHT WING LEADING EDGE 611AR LOWER MOUNT FITTING BY NACELLE ON FORWARD SPAR IS CRACKED. REPAIRED IAW DHC-8-200 SRM 51-40-00.SDR 06FDEA1402Spar Cap · corrodedRIGHT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1062 FOUND CORROSION. CORROSION ON RIGHT HAND WING, REAR SPAR UPPER SPAR CAP AT STA XORS 1062 REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. ORIGINALSDR 06FDEA1401Spar Cap · corrodedRIGHT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1027 TO STA XORS 1045 FOUND CORROSION. REPAIR CARRIED OUT ON RIGHT HAND WING REAR SPAR UPPER SPAR CAP AT STA XORS 1027 TO XORS 1045 AS PER FEDEX EA 1-5710-95811, TITLE: WINGS - RIGHT HAND REAR SPAR CAP UPSDR 06FDEA1400Spar Cap · corrodedLEFT HAND WING - REAR SPAR UPPER SPAR CAP AT STA XORS 1025 TO STA XORS 1045 FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. ORIGINAL THICKNESS = 0.145" MATERIAL REMOVED = 0.054SDR 06FDEA1396Frame · crackedRIGHT WING LEADING EDGE CANTED AREA FORMER AT STA XORS 480, SUSPECTED CRACKED. CRACK FORMER ON RT WING LEADING EDGE CANTED AREA AT STA XORS 480. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. NEW FORMER FABRICATED AS PER DWG ARB2931. REPAIR CLASSIFIED ASSDR QXEA200601043Fastener · looseYYC - C4 LEFT WING INTERIOR, STATION YW138.0 ON FRONT SPAR HAS TWO LOWER LOOSE HILOCKS. REPLACED IAW DHC-8-200 SRM 51-40-00.SDR QXEA200600954Spar Cap · chafedPDX - C4 RIGHT WING FORWARD LOWER SPAR CAP IS CHAFED AT WING STATION YW56.00. REPAIRED IAW RD 8-57-811.SDR P5CA0601468Spar · corrodedWS 1010-1038 RT FRONT SPAR WEB CORROSION. REPAIRED PER BOEING 8100-9, PER ECRA 921FT-57-747-013.SDR P5CA0601467Spar · corrodedCORROSION ON LEFT WING LEADING EDGE CAVITY - SPAR WEB - LOWER CHORD LES 1322. REPAIRED PER BOEING 8100-9. REPLACED LEFT WING L/E SPAR WEB LWR CHORD PER ECRA 921-57-747-011.SDR 2006FA0000349Spar Cap · crackedDURING ACCOMPLISHMENT OF SB NR 32, A 0.625 INCH LONG, SPANWISE CRACK WAS NOTED ON THE RT UPPER SPAR CAP IN THE MAIN SPAR CENTER SECTION APPROX 0.250 INCH IB OF THE CENTER SECTION OB END. PROBABLE CAUSE IS UNKNOWN. (K)SDR 06FDEA1195Spar · damagedRIGHT WING, REAR SPAR AT STA XORS 564 UPPER CHORD FOUND ELONGATED HOLE. ELONGATED HOLE ON RIGHT WING REAR SPAR STA XORS 564 UPPER CHORD REPAIRED AS PER FEDEX EA NR 1-5710-95804, TITLE: WINGS, RIGHT WING AFT SPAR UPPER CAP AFT TANG AT STATION XORS = 564 (REAR SDR 06FDEA1196Spar Cap · corrodedRIGHT WING REAR SPAR UPPER END CAP BETWEEN STA XORS 949 TO XORS 981 FOUND CORROSION. CORROSION AT RIGHT WING REAR SPAR UPPER END CAP BETWEEN STA XORS 949 TO XORS 981 REMOVED AS PER SRM 51-21-01 VOLUME II. MINIMUM ORIGINAL THICKNESS =0.182" (0.197"-0.015"),SDR 06FDEA1194Spar Cap · corrodedLT WING REAR SPAR UPPER END CAP STA XORS 1042 FOUND CORROSION. CORRODED AREA ON LEFT WING REAR SPAR UPPER END CAP STA XORS 1042 REPAIRED AS PER FEDEX EA NR 1-5710-95805, TITLE: WINGS, LEFT REAR SPAR UPPER CAP AFT TANG CORROSION CENTERED AT STATION XORS = 1042SDR 06FDEA1193Spar · corrodedLT WING, REAR SPAR AT STA XORS 590 - 593 UPPER CHORD UPPER SURFACE FOUND CORROSION. CORROSION AT LEFT WING REAR SPAR STA XORS 590-593 UPPER CHORD UPPER SURFACE REPAIRED AS PER FEDEX E.A. NR 1-5710-95800, TITLE: WINGS, LEFT HAND REAR SPAR UPPER CAP CORROSIONSDR TSAA0657023Spar · corrodedWBL 157 CORROSION BY WING REAR SPAR. REMOVED CORROSION AND REPLACED RIVETS. REPAIR COMPLETED IAW ALOHA'S ECO 3091. FAA 8100.9 RECEIVED.SDR TSAA0657025Spar · corrodedCORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-560.SDR TSAA0657021Spar · corrodedCORROSION ON LOWER SURFACE CHORD FORWARD FLANGE FRONT SPAR AT FSS-560.SDR AUCR200600002Spar Cap · corrodedUPPER REAR SPAR CAP STRESS CORROSION CRACKED IN AFT RADIUS FORWARD OF NR 4 FLAP HANGER. DAMAGE CENTERED AT WS275. DAMAGE WAS INITIALLY DETECTED VISUALLY DURING SCHEDULED SPECIAL INSPECTION. DAMAGE WAS FURTHER EVALUATED WITH EDDY CURRENT INSPECTION AND WAS FSDR 2006FA0000339Spar · corrodedDURING 100 HR INSPECTION ON REAR SPAR CHANNEL, RIVET HEADS WERE POPPED ON BOTH SIDES. A COMPLETE INSPECTION REVEALED SEVERE CORROSION BETWEEN CHANNEL AND STEEL PLATES. ALSO, SEVERE CORROSION EXISTED BETWEEN REAR IB ATTACH FITTINGS TO SPAR. THE ATTACH FITTINSDR 2006FA0000338Spar · corrodedDURING 100 HR INSPECTION ON REAR SPAR CHANNEL, RIVET HEADS WERE POPPED ON BOTH SIDES. A COMPLETE INSPECTION REVEALED SEVERE CORROSION BETWEEN CHANNEL AND STEEL PLATES. ALSO, SEVERE CORROSION EXISTED BETWEEN REAR IB ATTACH FITTINGS TO SPAR. THE ATTACH FITTINSDR QXEA200600818Spar · gougedPDX C4 - RIGHT HAND WING FORWARD SPAR HAS TOOL MARKS (GOUGES) AT YW178.000. REPAIRED IAW HORIZON AIR EA 2-57-356.SDR 06FDEA1090Spar Cap · corrodedRT WING REAR SPAR CAP UPPER SURFACE FOUND WITH CORROSION AT XORS 1040. RT WING REAR SPAR CAP UPPER SURFACE XORS 1040 CORROSION AREA REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5710-95791, TITLE: WINGS, RIGHT REAR SPAR UPPER CAP CORROSION AT STATIONS XORS = 1040 TSDR 06FDEA1091Spar Cap · corrodedLT WING REAR SPAR CAP UPPER SURFACE FOUND WITH CORROSION AT XORS 1042. LT WING REAR SPAR CAP UPPER SURFACE AT XORS 1042 CORROSION REMOVED AND FOUND BEYOND ALLOWABLE LIMITS AS PER SRM 57-20-00 FIGURE 6 VOLUME I. ORIGINAL THICKNESS =0.137", MATERIAL REMOVED =SDR UPS06146532Spar · crackedFOUND LEFT WING AFT OF REAR SPAR O/B SIDE OF RIB 16 WEB CRACKED. REMOVED AND REPLACED RIB PER A300 SRM 51-40-00.SDR ACE030906Flange · corrodedMAINTENANCE FOUND CORROSION ON FORWARD SPAR LOWER CAP FORWARD FLANGE, IN THE CENTER FUSELAGE BAY, UNDER PREVIOUSLY REPLACED SEALANT. REPAIR REQUIRED REMOVAL OF CORROSION AND STRAP DOUBLER PER FR-CO FACTORY REPAIR DESIGN.SDR QXEA200600770Spar Cap · chafedPDX C4 , LEFT HAND WING FRONT SPAR LOWER CAP IS CHAFED AT APPROXIMATELY YW57-YW78. REPAIRED IAW RD 8-57-1119, RD 8-57-811, PARAGRAPH A7 AND DHC-82 SRM 51-20-36.SDR TAMF20060009SSpar · crackedDURING INSPECTION C-CHECK, FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA WS 962 RT. DAMAGE WILL BE REPAIRED IAW EWO 767 57-006 AND BOEING SERVICE REQUEST ID: 1-170340546. FAA FORM 8100-9 MUST BE ISSUED APPROVING THIS REPAIR.SDR QXEA200600759Spar · crackedYYC C4, LEFT HAND WING FORWARD SPAR, SUPPORT ANGLE FOR WET LINE ATTACH AT YW57 IS CRACKED AT TOP ANCHOR NUT. REPLACED IAW DHC-8-200 SRM 51-40-11.SDR 06FDEA0891Spar Cap · damagedDURING NDT INSPECTION FOUND CRACK ON LOWER SPAR CAP HOLE. PERMANENT REPAIR ACCOMPLISHED IAW FEDEX EO 8-5710-7-3318 P2 CONDITION 3 STEP 5 AND DWG SR10570048 CONFIGURATION -7015.SDR BSAASDR0607Spar Cap · damagedPITTING CORROSION WAS FOUND ON THE RIGHT WING ON THE LOWER WING SPAR CAP IN THE THIRD ELEMENT SPAR STRAP JUST AFT OF THE WING DRAIN LOCATED JUST OUTBOARD OF THE NACELLE IN THE WING LEADING EDGE. THE DAMAGE AREA IS APPROXIMATELY .5 INCH WIDE AND WENT INTO THE SDR UPS06846488Spar Cap · crackedINSPECTION TYPE:C3 LH LWR REAR SPAR HAS A 9" CRACK AT STA 857 LBL 53 TO LBL 60, STOPPED DRILLED CRACK AT STA 857 LBL53 IAW SRO 8570009 NOTE 19 FABRICATED AND INSTALLED -63 ANGLE,-7,-9,-11,-15,-17,-21,-23 -25,-27,-29,-33 STRAP ANGLES,-35,-37,-39,-41 SHIMS, AND SDR USAA060364Fitting · crackedOUTBOARD MID SPAR SUPPORT FITTING CRACKED. CRACK WAS CUT OUT, REPAIR PARTS INSTALLED PER TR 57-41-02, DEFECT SIZE: .25 INCH.SDR UPS06846438Spar Cap · crackedRT WW LWR SPAR CAP CRACKED 1/2" LONG AT STA 857.125. STOP DRILLED CRACK AT AT RT WW LWR SPAR CAP IAW SRO 8570009 INSTALLED -47 PLUG IN WING SKIN, FABRICATED AND INSTALLED REPAIR ANGLES, AND -66 SPACER IAW SRO 8570009, AND SRM 51-1-20D AT STA 857.125 RT WW LWRSDR QXEA200600630Spar Cap · chafedPDX - C4 CHECK, RIGHT HAND WING FRONT SPAR, LOWER CAP IS CHAFED AT INBOARD ATTACH POINT FOR 611AR. REPAIRED IAW SRM 51-20-16, SRM 51-40-00 AND RD 8-57-811.SDR UVVR200600001Nut · crackedWHILE PERFORMING MAINTENANCE ON AIRCRAFT, IT WAS DISCOVERED THAT APPROXIMATELY 10 NUTS ON EACH WING THAT SECURES UPPER WING PLANK TO REAR SPAR UPPER FLANGE, FROM REAR SPAR STATION 161.1 TO 281.8 WERE CRACKED, WITH SOME MISSING PARTS OF THE NUT. AS A PRECAUTIONSDR DHL2006760532Spar · crackedLEFT INBOARD MID-FLAP, REAR SPAR AT WBL 124, JUST BELOW INBOARD AFT FLAP ACTUATION DRUM HAS CRACK. REMOVED DAMAGED AREA DIM 47 X 2.25 INCHES ON LEFT INBOARD MID FLAP LOWER, AND FAB NEW PART, MAT BAC 1517-1367-6511 EXTRUSIONDIM 47 X 2.25 INCHES IAW B727 SRM 57SDR CA060216003Frame · crackedUPON BEGINNING A PHASE 3 INSPECTION, A TECHNICIAN DISCOVERED A SMALL CRACK ON THE RIGHT FORWARD LOWER SPAR HINGE CAP. THE CRACK WAS OUT FROM THE FOURTH FASTENER FORWARD TOWARD THE HINGE EDGE. A SMALL AREA OF PAINT HAD BEEN FLAKED AWAY IN THIS AREA. MORE PAISDR 1051229025Spar Cap · corrodedCORROSION ON LT WING MAIN SPAR FWD SPAR CAP FLANGE. FOUND DURING INSPECTIONSDR 1051229028ASpar Cap · corrodedBIO CORROSION ON RIGHT WING MAIN SPAR CAP FLANGE NEAR WS 124588. MAINTENANCE FOUND DURING INSPECTION.SDR 1051229028Spar Cap · corrodedBIO CORROSION ON LEFT WING MAIN SPAR FWD SPAR CAP FLANGE. FOUND DURING INSPECTION.SDR 06FDEA0678Spar Cap · corrodedRIGHT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1044 TO 1047. REPAIR CARRIED OUT AT RIGHT HAND WING REAR SPAR UPPER CAP AT XORS 1044 TO 1047 CORROSION AREA AS PER FEDEX EA 1-5710-90756, TITLE: WINGS - RIGHT HAND REAR SPAR UPPER CAP CORROSION AT SSDR 06FDEA0677Spar Cap · corrodedRIGHT HAND WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1041 TO 1044. REPAIR CARRIED OUT AT RIGHT HAND WING REAR SPAR UPPER CAP AT XORS 1041 TO 1044 CORROSION AREA AS PER FEDEX EA 1-5710-90756, TITLE: WINGS - RIGHT HAND REAR SPAR UPPER CAP CORROSION AT ST
Back to JASC 5711