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 R61A2019041033372Spar · crackedA CRACK 2 EACH .750 INCH LONG WAS FOUND AT RH WINGLET FRONT SPAR. WINGLET WAS REPLACED IAW AMM 57-30-00-400-801A. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR HYIA20190319003Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE RIGHT HAND UPPER AFT SPAR CAP (P/N: 5122041-22) AT APPROXIMATE RWS 223.71. THIS CORROSION MEASURES APPROXIMATELY .036 DEEP AND IS GREATER THAN THE MAXIMUM REMOVABLE LIMITS ALLOWED UNDER MEB95-11R1 SECTION 3. TSDR HYIA20190319002Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE RIGHT WING LOWER AFT SPAR CAP (P/N: 5122041-24) AT APPROXIMATE RWS 220.71. THIS CORROSION HAS A MAX DEPTH OF APPROXIMATELY .033 INCHES DEEP. THIS IS GREATER THAN THE MAXIMUM REMOVABLE LIMITS ALLOWED UNDER MEB9SDR HYIA20190319001Spar · crackedDURING MAINTENANCE A SMALL CRACK AND SEVERAL AREAS OF CORROSION WERE DISCOVERED ON THE RIGHT HAND AFT SPAR WEB BETWEEN RWS 163.29 AND 229.71. THE CRACK IS AT APPROXIMATE RWS 178.29 ON THE BOTTOM EDGE OF THE WEB ONLY AND MEASURES APPROXIMATELY .228 INCHES LONG.SDR SWAA2022030481261Spar · corrodedSUPPLEMENTAL INFORMATION: L\H WING REAR SPAR HAS CORROSION AT TANK #1 BOOST PUMP LOWER BONDING STRAP CONNECTION POINT. / REMOVED CORROSION ON L/H WING REAR SPAR WEB BOOST PUMP LOWER BOND STRAP ATTACH POINT IAW SRM 51-10-02-0G-0. VERIFIED ALLOWABLE LIMITS ORIGISDR SWAA2022030481260Spar · corrodedR\H WING REAR SPAR HAS CORROSION AT TANK #2 BOOST PUMP LOWER BONDING STRAP CONNECTION POINT. / REMOVED CORROSION ON R/H WING REAR SPAR BOOST PUMP LOWER BONDING STRAP ATTACH POINT IAW SRM 51-10-02-0G-0. VERIFIED ALLOWABLE LIMITS; ORIGINAL .685' LOSS .126' REMAISDR SWAA2022030404599Spar · corrodedLW AFT FUEL BOOST PUMP FAILS RESISTANCE MEASUREMENT (REF 723-150-00-01 STEP 2) DUE TO CORROSION NOTED AT BONDING STRAP LOCATIONS. LW IRSS 145 / REPAIRED CORROSION DAMAGE ON L/W REAR SPAR WEB BELOW FUEL BOOST PUMP AT BONDING STRAP LOCATIONS IAW ATS ER # 19-0249SDR SWAA2022030481204Spar · corrodedL\H WING FWD SPAR AT #2 L\E FLAP; TANK 1 BOOST PUMP; AT UPPER BONDING STRAP ATTACH POINT HAS CORROSION. / REMOVED CORROSION ON L/H WING FWD SPAR #2 L/E BOOST PUMP .485' ORIG .163' LOSS .322' REMAINING OUT OF LIMITS IAW B737 SRM 57-20-10 ALLOWABLE DAMAGE 3. REPSDR CA190311015Spar · cracked(CAN) RH WING AFT SPAR WEB FOUND CRACKED AT RWS 134.00 WHERE RH OB FLAP OB TRACK ATTACHES. (AIRCRAFT OVER-SPEED NOT REPORTED) FOLLOWING REMOVAL OF FLAP AND ASSOCIATED SHEET-METAL PARTS THE AREA WAS INSPECTED. IT LOOKS AS IF FATIGUE OVER TIME CAUSED SUPPORTING SDR 2019F00143Spar Cap · corrodedCORROSION, RT WING, SPAR CAP AND WEB, BETWEEN WS 37 AND WS 52. ACCOMPLISHED ENGINEERING FIELD REPAIR FR-680-0144-5291 REV- FAA FORM 8100-9 DATED 3/01/2019; FIELD REPAIR - CORROSION, RT WING, SPAR CAP AND WEB, BETWEEN WS 37 AND WS 52.SDR DALA20190402084Spar · corrodedREAR SPAR LOWER CHORD / BS 161 / LEFT WING / CORROSION REMOVAL PSE 57.11.02.2 - PERMANENT REPAIR ACCOMPLISHMENT. CURRENT REVISION OF ER/A 525623-14AD IS REV. C. RESULTS OF STAGE II DTE/DTA HAVE BEEN COMPLETED AND INCORPORATED AT THIS REVISION LEVEL. ACCOMPLISHSDR SWAA2022030162673Balance Weight · corroded***CORROSION*** ON AILERON BALANCE WEIGHTS AT RIGHT WING REAR SPAR ORSS532. MARKED / REMOVED AND REPLACED; WITH SERVICABLE PART; RT AILERON I/B BALANCE PANEL I/B WEIGHT AT ORSS532 IAW SOPM 20-50-01 & AMM 20-50-11-910-801 TABLE 208. PERFORMED 10X VISUAL INSPECTSDR RJEY2019030800001Spar · corrodedDURING INITIAL INSPECTION, INSPECTOR FOUND CORROSION ON TRAILING EDGE REAR SPAR BTW RIB6 TO RIB7 ON LT WING.SDR IPXA2019032840540Spar · crackedINSPECTION TYPE:D2 CRACK WAS FOUND ON FASTENER HOLE ON FRONT SPAR WEB (P/N: 112U2007-3) OF LT WING FSSI 655.72 WHEN PERFORM 747-SB-57A2357.REPAIR IAW SRID: 3-4407802419 AND EO B747-5710-71777-B.SDR DALA2019030101413Spar · corrodedSHIP 5635 RIGHT WING T/E REAR SPAR UPPER SURFACE AT APPROX BBL 70.5 HAS PITTING CORROSION. CORRECTIVE ACTION: REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS REF SRM. REPAIRED AREA IAW ERA 575214-14 REV ORIG. (0963504)SDR DALA2019030101409Spar Cap · corrodedSHIP 5635 UPON REMOVAL OF RIGHT WING UPPERINBD T/E FIXED PANEL FOUND REAR SPAR UPPER T-CAP (CHORD) CORRODED APPROX WS 177.50. CORRECTIVE ACTION: REMOVED CORROSION FROM RIGHT WING UPPER I/B T/E FIXED PANEL REAR SPAR UPPER T-CAP WS 177.50 UT READINGS SENT TO BOESDR COEA2019022227805Plate · chafedWO 193437 NR 600024 HEAVY CHECK COE/MAJOR REPAIR: RT WING REAR SPAR STRIP SLAT BOND PLATES CHAFFED BETWEEN RIBS 3-4. LEVEL 2 CORRECTIVE ACTION: REPAIRED PER SRAS ES-0095441-01...14495 ISSUE A, DATED 4/19/2019.SDR DXTA2019F00018Spar Cap · damagedRT WING FORWARD SPAR CAP ANGLE REPAIR. ACCOMPLISHED IAW AQRD ENGINEERING ORDER ERO-102798 DATED 01/15/2019.SDR COEA2019022005912Spar · damagedWO 194688 NR 500018 HEAVY CHECK COE/MAJOR REPAIR: FLAW INDICATION AT REAR SPAR LOWER FLANGE AT INBOARD HOLE RIB2L. CORRECTIVE ACTION: REPAIRED PER SRAS ES-0094005-01...14292 ISSUE A, DATED 3/14/2019.SDR FDEA201902140407Spar Cap · corrodedEXFOLIATION CORROSION AT LT WING AFT SPAR LWR CAP AT STA XORS 738. REMOVED CORROSION ON LT WING AFT SPAR LOWER CAP AT STA XORS 738. REF SRM 51-21-01-06. COMPLIED WITH EA 1-5710-T0344783.SDR FDEA201902140406Spar Cap · corrodedEXFOLIATION CORROSION LT WING AFT SPAR LWR CAP AT STA XORS 593. REMOVED CORROSION ON LT WING AFT SPAR LOWER CAP. CORROSION T STA XORS 593 REF SRM 51-21-01-06. COMPLIED WITH EA 1-5710-T0344783.SDR FDEA201902130404Spar Cap · corrodedEXFOLIATION CORROSION LT WING SPAR LWR CAP AT STA XORS 593. REMOVED CORROSION ON LT WING AFT SPAR LOWER CAP CORROSION AT STA XORS 593. REF SRM 51-21-01-06. COMPLIED WITH EA 1-5710-T0344783.SDR FDEA201902110372Spar · corrodedWHILE REMOVING LOCK FASTENERS FROM UPPER WING PANEL, FOUND CORROSION ON LH WING REAR SPAR UNDER #5 SPOILER, BEHIND BRACKET (ARH 0357-3) COMPLIED WITH E.A. #1-5700-T0345190. REINSTALLED BRACKET PN ARB005-345 IAW SRM 51-33-01.SDR CVGA20190124001Spar Cap · corrodedCORROSION DAMAGE ON LEFT WING, AFT LOWER SPAR CAP, FORWARD FLANGE (BETWEEN WS 20.0 AND WS 41.00) IN WHEEL WELL OPENING.SDR HYIA20190123001Spar Cap · crackedDURING MAINTENANCE A CRACK WAS VISUALLY DISCOVERED ON THE RIGHT HAND FORWARD UPPER SPAR CAP P/N: 5122031-6. THIS CRACK HAS BEEN CONFIRMED BY SURFACE EDDY CURRENT INSPECTION AND IS LOCATED IN THE FORWARD RADIUS BETWEEN THE VERTICAL AND HORIZONTAL LEGS OF THE CASDR COEA2019011105Spar · corrodedHEAVY CHECK COE/MAJOR REPAIR: RT WING AFT SPAR STRIP SLAT LOWER SURFACE BETWEEN RIBS 19-20 HAS LEVEL 2 CORROSION. REPAIRED PER SRAS S572R0391...14113 ISSUE C, DATED 2/13/2019.SDR JGVR20180111001Spar Cap · corrodedMECHANICALLY BLENDED CORROSION ON THE LT WING AFT SPAR LOWER CAP APX 8 INCHES INBD OF W.S. 37.00, ACCESSIBLE THROUGH THE LT LANDING GEAR WHEEL WELL AREA. APPLIED GRIDS AND PERFORMED NDT, AND SUBMITTED FINDINGS TO ENGINEERING. PERFORMED BLEND, TREAT, PRIME REPASDR FDEA201901060034Former · crackedRIGHT WING LEADING EDGE COMPARTMENT AT STATION XOS 993 FOUND FORMER CRACK RT WING LEADING EDGE COMPARTMENT AT STATION XOS 993 CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DRAWING ARB1164 REVISION M AND INSTALLED AS PER SRM 51-31-01-0SDR C77A2019010600001Spar · crackedFOUND CRACK IN LT WING SPAR II LOWER FLANGE AT HOLE A3. CRACK EXTENDED FROM HOLE A3 FORWARD TO EDGE OF LOWER FLANGE AND FROM HOLE A3 AFT TO AFT EDGE OF FLANGE AND APPROXIMATELY .25" UP THE WEB. SB 170-53-0053 PART III PREVENTIVE MODIFICATION HAD BEEN ACCOMPLSDR HYIA20180104002Spar Cap · crackedA CRACK WAS IDENTIFIED AT THE LT SIDE OF LWR FWD CARRYTHROUGH SPAR CAP, IB MOST AFT FASTENER HOLE WHILE PERFORMING NDT PROCEDURE AS AMOC FOR AD2018-03-03R1. THE CRACK WAS CONFIRMED WITH BOLT HOLE EDDY CURRENT AFTER THE FASTENER WAS REMOVED. WE BELIEVE THIS SSDR SWAA2022030127008Spar · corroded***CORROSION*** ON AFT SPAR AROUND LOWER BONDING JUMPER AT RIGHT WING BOOST PUMP TANK2 AFT. MARKED / ACESSED HYDRAULIC LINES AS REQUIRED TO BLEND CORROSION ON RT WING AFT SEAL AT BOOST PUMP TANK 2 AFT; IAW AMM 20-10-51-000-801. BLENDED CORROSION; FINAL DIMENSISDR SWAA2022022573309Web · corrodedPRIORITY LEVEL 1: L/H WING; REAR SPAR WEB; TANK 1 AFT BOOST PUMP LOCATION; CORROSION FOUND AT LOWER BONDING JUMPER ATTACH POINT. MARKED IN RED. / REMOVED CORROSION ON L/H WING REAR SPAR WEB LOWER BOOST PUMP ATTACH POINT; VERIFIED MATERIAL LOSS; ORIGINAL MATERISDR REXA2018121031224Spar · scratchedINITIAL INSPECTION: RH WTF REAR SPAR LINK ASSY IS SCRATCHED ALSO RIGHT FUSELAGE FRAME IS SCRATCHED. SCRATCHES ARE ON THE OUTBD SURFACES ONLY (LINKS WERE FOUND NOT TOUCHING THE STRUCTURE. REF EO R57200 STEP 6. "COMPLETE: SUMMARY OF NRC 00353: REAR SPAR LINK ASSDR FDEA201811163247Former · crackedRIGHT WING FIXED LEADING EDGE UPPER FORMER AT XOS 584 FOUND CRACK. FIXED LEADING EDGE UPPER AT XOS 584 , NEW FORMER FABRICATED AS PER DOUGLAS DRAWING ARB2931 REVISION H. CRACKED FORMER REMOVED AND REPLACED WITH NEW FORMER AS PER SRM 51-31-01-0G. REPAIR CLSDR FDEA201811163240Former · crackedLEFT WING FIXED LEADING EDGE UPPER FORMER AT XOS 584 FOUND CRACK. A NEW FORMER FABRICATED AS PER DOUGLAS DRAWING ARB2931 REVISION H. CRACKED FORMER REMOVED AND REPLACED WITH NEW FORMER AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR JGVR20181114004Spar Cap · corrodedFOUND CORROSION IN LH MLG WHEEL WELL AFT SPAR CAP APX W.S. 27.00. FOUND WHILE CLEANING FOD FROM DRAG ANGLE CORROSION REPAIRS.SDR HNAA2918120600309Rib · crackedDURING HEAVY CHECK MAINTENANCE FOUND RT WING RIB 5 CRACKED AT AFT LIGHTNING HOLE. R&R RT WING RIB 5 WITH P/N 145-67083-602 IAW ETD2018-145-118003 AND TI-145-14-306.SDR 2019F00077Spar Cap · corrodedCORROSION, LH AND RH WINGS, LOWER REAR SPAR CAPS, WS 33 TO 36. ACCOMPLISHED REPAIR DEFINITION NO. FR-680-0010-4784, MAJOR REPAIR, FIELD REPAIR - CORROSION, LH AND RH WINGS, LOWER REAR SPAR CAPS, WS 33 TO 36 DATED OCT.31, 2018 - AND FAA FORM 8100-9 DATED OCT.31SDR IPXA201811145944Spar Cap · corrodedINSPECTION TYPE: 4C, RT WING REAR SPAR UPPER CAP HAD CORROSION BETWEEN XORS 452.75 - 488.25, AND XORS 523.75 - 544.5. REPAIRED THE SPAR CAP IAW EA 011-5710-01-A7539, REV I/R, AND EO MD11-5710-70589-A. MINOR.SDR HYIA20181031002Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE LEFT HAND UPPER AFT SPAR CAP (P/N: 5122041-21). THIS CORROSION IS LOCATED BETWEEN LWS 229.71 AND 224.71, AND MEASURES .032 INCHES DEEP. THIS MEASUREMENT EXCEEDS THE LIMITS FOUND IN MEB95-11R1. THIS CAP WILL BESDR R61A2018110261102Spar · crackedLEFT WINGLET FWD SPAR AT ATTACH POINT TO WING IS CRACKED IN THREE REMOVED AND REPLACED THE LT WING WINGLET IAW SRM 51-40-02 AND AMM 57-30-00-400-801-A.SDR R61A2018110261101Spar · crackedRIGHT WINGLET, FWD SPAR AT ATTACH POINT TO THE WING CRACKED IN 2 LOCATIONS. CRACK 1 IS .4" AND CRACK 2 IS 2" IN LENGTH. REMOVED AND REPLACED RH ENHANCED WING TIP (171-16240-412) IAW EMB 170/175 AMM 57-30-00-400-801-A.SDR ABXA201811213112Spar · corrodedCORROSION ON THE LEFT WING LEADING EDGE FRONT SPAR AT LEADING EDGE STATION 867. THE FRONT SPAR'S WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR HYIA20181024001Spar Cap · corrodedDURING MAINTENANCE CORROSION WAS DISCOVERED ON THE LEFT HAND LOWER AFT SPAR CAP P/N 5122041-23, AT APPROXIMATE L.W.S. 215.20. THIS CORROSION IS MEASURED TO A DEPTH OF .019 INCHES AND IS BEYOND LIMITS FOUND IN MEB95-11R1. THIS CAP WILL BE REPLACED.SDR IPXA2018111205851Spar · corrodedRIGHT WING UPPER SKIN HAD CORROSION AT THE AFT SPAR AND T/E PANEL FWD OF THE NR 2 & 3 SPOILERS, WAS BULGED. REPAIRED THE RT WING UPPER SKIN AND AFT SPAR UPPER AFT FLANGE IAW EA 011-5710-01-A7533, REV IR, AND EO MD11-571070578-A. MINOR.SDR DALA2018101706131Splice · crackedINITIAL INSPECTION: CRACKED SPLICE AND ANGLE STA XRS=164 AT RT WING FRONT SPAR. SPLICE AND ANGLE AT STA XRS=164 ON RT WING FRONT SPAR WERE REPLACED PER PER SRM 51-30-5, ER/A378293-14 REV. ORIG. AND DWG 9937517 REV J. (LP0785943)SDR IPXA2018110985798Frame · crackedLEFT WING L/E COMPARTMENT FRAME AT XORS 630 WAS CRACKED. REMOVED AND REPLACED THE FRAME IAW SRM 51-31-01, 51-33-01, AND 51-35-01. MINOR.SDR DXTA2018F00132Spar Cap · corrodedRIGHT WING AFT SPAR AREA, FWD OF OUTBOARD END OF AILERON SHOWS SIGNS OF CORROSION. FIELD REPAIR FR-750-0183-4697 REV- DATED:10/12/2018.SDR DXTA2018FA0000409Spar Cap · corrodedCORROSION, CENTER WING, LOWER SKIN C/T REAR SPAR WS 18 - WS 23. ACCOMPLISHED FAA FORM 8100-9, FIELD REPAIR FR-680-0057-4639 REV-.SDR HYIA20181003001Spar Cap · corrodedDURING MAINTENANCE CORROSION DAMAGE WAS FOUND ON THE RIGHT WING AFT LOWER CAP (P/N: 5122041-24). THIS CORROSION IS LOCATED AT APPROXIMATE RIGHT WING STATION 204.71 AND MEASURES APPROXIMATELY .019 DEEP. THIS IS GREATER THAN REMOVABLE LIMITS ALLOWED UNDER MEB95-
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