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 08FDEA01352Spar · crackedFOUND CRACKS IN CENTER SPAR WEB VARIOUS LOCATION (HOLE 2, 3, 5, 7) REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTALLING A BUSH IN HOLE 5 IAW RAS057091/022/2007 ISS A, APPROVED BY EA 6-5710-114861.SDR CA080414001Spar · crackedCRACKS FOUND WHILE COMPLYING WITH SB2/47. CRACKS JUST VISIBLE WITH FLUORESCENT PENETRANT INSPECTION. WHEN SPAR REMOVED CRACKS WERE VISIBLE TO NAKED EYE ON THE INTERIOR OF SPAR AND ON GUSSET BETWEEN SPAR AND GUSSET.SDR UIEA200800136Spar · corrodedRIGHT WING WS 1392 TO WS 1485 FROM (NR 24, AND 25 LEADING EDGE FLAP AREA) FRONT SPAR AREA SURROUNDING AND MID SPAR SURROUND AREA FOUND 8 AREAS OF CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.SDR UIEA200800133Spar · corrodedRIGHT WING WS 1250 TO WS 1392 FROM NR 23,AND 24 LEADING EDGE FLAP AREA, FRONT SPAR AREA SURROUNDING FOUND 7 AREAS OF CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02.SDR DL76G080511Spar · damagedLT WING FRONT SPAR CONTACTED RT HORIZ STAB OF 737 WHILE PARKING AT HANGAR. LT SPAR UPPER AND LOWER CAPS AND WEB SPLICED.SDR DHL2008805532Fitting · crackedCENTER WING REAR SPAR UPPER CAP FITTING CRACKED STA 857.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D AND SRM 51-3-1 (TORQUE).SDR CA080331003Spar Cap · cracked(CAN) WHILE PERFORM AD CF-1992-26R1, ULTRA SONIC INSPECTION OF THE WING REAR SPAR CAP, CRACKS WERE INDICATED ON BOTH REAR SPAR CAPS. VISUAL INSPECTIONS WERE CARRIED OUT AND CRACKS DISCOVERED ON BOTH SPAR CAPS AT WS 51.00 FS 434.80. THIS AD WAS DUE AT A/F TIMSDR CA080331001Frame · cracked(CAN) WHILE PERFORMING AD CF-1997-07R2, NDT INSP OF FRONT AND REAR SPAR WING TO FUSELAGE FRAME ANGLES A CRACK WAS DETECTED ON THE REAR LT OB ANGLE. THE CRACK ORIGINATED AT THE TOP HI-LOK AND WAS HEADED UP ABOUT .1250 TH OF AN INCH. IT COULD NOT BE DETECTED BY SDR ABXA080131Strap · crackedSTRAP ON UPPER CAP OF FRONT SPAR WAS CRACKED LES 485. REMOVED AND REPLACED UPPER SPAR CAP STRAP SECTIONS IAW B767 SRM.SDR TAMF20080014SSpar · corrodedDURING C2 CHECK INSPECTION WAS FOUND CORROSION ON THE CENTER WING REAR SPAR WEB NEAR RBBL 75 AT THE REAR SPAR BULKHEAD FITTINGS. DAMAGED AREA WAS BLENDED TO A MINIMUM WEB THICKNESS OF 0.288 INCHES AND NDT (EDDY CURRENT) INSPECTION DID NOT REVEAL ANY REMAINING SDR TAMF20080012SSplice · crackedDURING C2 CHECK INSPECTION WAS FOUND A CRACK ON SPLICE PLATE FRONT SPAR LOWER CHORD STA ISS 256.15 261.26 - RT. DAMAGED AREA WAS REPAIRED IAW EWO 767 57-041 AND MFG SERVICE REQUEST 1-789000676. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUSDR SWAA081331Stiffener · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING AFT SPAR UPPER CHORD INBOARD STIFFENER CRACKED. REPAIRED STIFFENER PER ER.SDR UIEA200800082Spar · corrodedRIGHT WING STA 610 TO WING STA 615 UPPER FACE REAR SPAR LEVEL 1 CORROSION EVIDENT. CORROSION CLEANED UP AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02.SDR SWIA200819374Spar · damagedLEFT WING ROOT AUXILIARY SPAR DAMAGED FROM BIRD STRIKE. REPAIRED THE LEFT WING ROOT SPAR IAW EMB REF IC2008-120/01998-A.
SDR GLBA20061081Spar · corrodedDURING STRUCTURAL INSP MAINT FOUND CORROSION ON THE RT WING SPAR AT APPROX WS 126.5. MAINTENANCE REMOVED CORROSION AND INSTALLED REINFORCEMENT STRAP PER E.O. 08-UE153-02. REAPAIR APPROXIMATELY 14" . .190 7075-T73. RII INSPECTION COMPLIED WITH PER TASKCARD 8.SDR UPS08851939Fitting · crackedINSPECTION TYPE:C2 NR 4 ALT THRU 560A BETWEEN XRS 428 AND XRS 463 STRINGER TO FRONT SPAR FITTING CRACKED. FABRICATED AND INSTALLED FRONT SPAR FITTING IN NR 4 ALT XRS 428 TO XRS 463 IAW DWG 3644046 AND SRM 51-1-8 AND SRM 51-01-20D.SDR HALA0800358Spar · corrodedLEVEL 1 CORROSION ARROUND FASTENER AT LT WING STA 860, ON TOP SURFACE, 6 INCHES AFT OF FRONT SPAR. REPAIRED PER SRM 57-20-01.SDR HALA0800357Spar · corrodedLEVEL 1 CORROSION AROUND 2 FASTENERS AT LT WING STA 825, ON TOP SURFACE, ON FRONT SPAR. REPAIRED PER SRM 57-20-01.SDR USAA920080654Spar · crackedMCN - MAJOR REPAIR - C20 CHECK - LEFT WING REAR SPAR UPPER CHORD CRACKED, RSS 222.5. REPAIRED LEFT WING REAR SPAR UPPER CHORD CRACKED, RSS 222.5 IAW USAIRWAYS EA 100282.SDR HALA0800361Spar · corrodedLEVEL 1 CORROSION AROUND FASTENER AT LT WING STA 1070, ON TOP SURFACE, ON FRONT SPAR. REPAIRED PER SRM 57-20-01.SDR KCSA081116Stiffener · corrodedRIGHT WING FRONT SPAR STIFFENER CORRODED AT L/E/ STA 1310.SDR USAA920080653Spar · crackedMCN - MAJOR REPAIR - C20 CHECK - RIGHT WING REAR SPAR UPPER CHORD CRACKED, RSS 222.5. REPAIRED RIGHT WING REAR SPAR UPPER CHORD CRACKED, RSS 222.5 IAW USAIRWAYS EA 100283.SDR 08FDEA00525Spar · damagedLT WING LEADING EDGE FRONT SPAR FASTENER HOLE HAS NO EDGE DISTANCE AT WS 167, LE STA 90. REPAIRED IAW EA 7-5710-116957.SDR HALA0800308Frame · crackedCRACK ON O/B SECTION OF L-2 FORMER LEFT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK.SDR HALA0800310Frame · crackedCRACK ON O/B SECTION OF NR 3 FORMER LT WING BELOW CENTER SECTION, VIEWED FROM 4TH WITNESS HOLE. REPAIR IN WORK.SDR HALA0800309Frame · crackedCRACK ON O/B SECTION OF MOST FWD FORMER LEFT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK.SDR HALA0800313Frame · crackedCRACK ON O/B SECTION OF MOST FWD FORMER RIGHT WING BELOW CENTER SECTION, VIEW FROM 2ND WITNESS HOLE. REPAIR IN WORK.SDR HALA0800314Frame · crackedCRACK ON O/B SECTION OF FORMER NR 2 RIGHT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK. REPAIR IN WORK.SDR UIEA200800046Spar · corrodedWS 410 - WS 470 FRONT SPAR CORROSION EVIDENT ON RIGHT WING. BLENDED OUT CORROSION IAW SRM 51-10-01. REPROTECTED PER 51-10-02.SDR UIEA200800043Spar · corrodedW/S 780 UPPER SKIN MIDSPAR CORROSION EVIDENT. LEVEL 1 RIGHT WING, BLENDED OUT CORROSION IAW SRM 51-10-01. REPROTECTED PER 51-10-02.SDR 2008FA0000086Spar · corrodedWINGS WERE PREVIOUSLY REMOVED TO FACILITATE TRANSPORTATION. INSP OF THE LT AND RT FWD SPAR BEARING BLOCKS IN THE FUSELAGE (P/N 0411129) FOUND SEVERE CORROSION DAMAGE. IT APPEARS TO BE DISSIMILAR METAL CORROSION BETWEEN THE SPAR BLOCKS AND THE AN3-21A ATTACHMENSDR CA080212001Adapter · cracked(CAN) UPON COMPLIANCE WITH SB 6/540 (WING-FRONT SPAR ADAPTER ASSEMBLY (P/N C6WM1027-1) INSPECTION FOR CRACKS) A CRACK WAS FOUND ON THE LT FRONT SPAR ADAPTER. REPLACED LT FRONT SPAR ADAPTER ASSY PN C6WM1027-1 WITH PN C6WM1027-3 IAW SB NR 61542. (TC NR 200802120SDR S9BA200800002Spar · corrodedCPCP INSPECTION, FWD LT WING SPAR HAS CORROSION BETWEEN STATIONS 72.5 AND WS 135. REPLACED AND SPLICED FWD SPAR WS 72.5 TO 135 IAW RD6-57-191. AIRCRAFT GROUNDED, YES.SDR S9BA200800007Spar · corrodedCPCP INSPECTION, RT WING NOSE SPAR CORRODED WS 35.15 TO WS 135. REPLACED NOSE SPAR WITH FACTORY NEW PART IAW AC43.13-1B CHAP 4 PARA 4-57. EMERGENCY MEASURES EXECUTED. NO
AIRCRAFT GROUNDED.
SDR SWAA080778Support Angle · crackedDURING SCHEDULED BRDG CHECK, FOUND WING CENTER SECTION FRONT SPAR STIFFENER SUPPORT ANGLE CRACKED AT BS 540, LBL 57. REMOVED AND REPLACED SUPPORT ANGLE PER SRM.SDR QXEA200800217Spar Cap · damagedPDX - C4 CHECK - RIGHT WING LOWER FRONT SPAR CAP HAS 4 EACH DAMAGED SLEEVES AT INBOARD MOST END OF 611AR. REPAIRED SLEEVES IAW TASK CARD 6-57-551 AND Q400 SRM 51-42-05.SDR QXEA200800216Spar Cap · corrodedPDX - C4 CHECK - RIGHT HAND WING, LOWER FRONT SPAR CAP HAS FRETTING CORROSION FORMING AT APPROXIMATELY YW57.00 TO YW67.00 (I/B CONTACT AREA FOR 611AR). REPAIRED IAW Q400 RD8/4-57-935 AND NDTM PART 6 51-00-01.SDR QXEA200800215Spar Cap · corrodedPDX - C4 CHECK - RIGHT WING LOWER SPAR CAP HAS FRETTING CORROSION FORMING AT APPROXIMATELY YW145.2 TO 155.2. REPAIRED IAW Q400 RD 8/4-57-935, AND NDTM PT-6 51-00-01.SDR DHL2008752610Spar · crackedRT WING INBOARD L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B727 SRM 51-10-1. HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6SDR UIEA200800039Spar · delaminatedEVIDENCE OF DELAMINATION AND CRACKING ON LEADING EDGE TO FRONT SPAR UPPER SURFACE PANEL APPROX WS 380. REPAIRED IAW SRM 51-40-12.
SDR UPS08M52084Spar · crackedINSPECTION TYPE:C LT WING FRONT SPAR ENCLOSURE APPROX STA XORS 514 UPPER SKIN FOUND CRACKED. CRACK AREA TRIM OFF PER EN1007-08. HFEC CARRIED OUT IAW DAC NDT SPM R.13 PART06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR ANGLES FAB USING 7075-0-0.063" MAT`L PER SRSDR HALA0800359Spar · corrodedLEVEL 1 CORROSION AROUND FASTENER AT LT WING STA 775, ON TOP SURFACE ON FRONT SPAR. REPAIRED PER SRM 57-20-01.SDR O7Z2008F00000Spar Cap · crackedFWD OB LOWER WING SPAR CAPS ARE CRACKED. LT AND RT ASSY CRACKS RADIATE FROM THE (4) HUCK RIVET FWD THROUGH WING ATTACH HINGE. THE AIRCRAFT WAS INSPECTED 15 MONTHS AND 404.2 HOURS AGO BY EDDY CURRENT AND NO CRACKS WERE FOUND AT THAT TIME. (K)SDR UPS08M51972Spar · crackedINSPECTION TYPE:C LEFT WING FIXED WING FRONT SPAR ENCLOSURE APPROX STA XORS 506 UPPER SKIN FOUND CRACKED. CRACKED AREA TRIMMED OFF AS PER SRM 57-10-00 FIG.27V.1R.40. HFEC C/OUT IAW DA CNDTSPM R.13 PART 06-10-01.001, FOUND NO CRACK EVIDENT. REP ANGLES FAB USSDR USAA920080245Spar · crackedCLT - MAJOR REPAIR - C20 CHECK - RIGHT WING AFT SPAR CHORD CRACKED, WS 135.5. REPAIRED RIGHT WING AFT SPAR CHORD, WS 135.5 IAW USAIRWAYS EA 100161.SDR 08FDEA00095Spar · corrodedCORROSION ON RIGHT WING REAR SPAR DOUBLER AROUND SPOILER NR 7 ACTUATOR REMOVED CORROSION IAW A310-200 SRM 51-74-10 ITEM 3. ORIGINAL THICKNESS .206 IAW AIRBUS DRAWING N : A 571-50824. REMOVED .002, REMAINING THICKNESS .204. WITHIN LIMITS IAW A310-200 SRM 57SDR QXEA200802068Spar · crackedPDX - C5 CHECK - LEFT WING FORWARD SPAR APPROXIMATELY YW 42.0, Z ANGLE CRACKED AT UPPER END. REMOVED Z ANGLE BRACKET AND FABRICATED NEW ANGLE IAW T/C 2-57-205. INSTALLED FABRICATED Z ANGLE IAW -8 200 SRM 51-40-11.SDR DL76S071659Spar · gougedLT WING FRONT SPAR WEB DENTED/GOUGED. CUTOUT DAMAGE AND INSTALLED A REPAIR DOUBLER.SDR SWAA076468Fitting · corrodedDURING SCHEDULED BRIDGE CHECK, FOUND RT WING AFT SPAR SUPPORT FITTING NR 7 MAIN FLAP TRACK CORRODED AT OUTBOARD FLAP TRACK MOUNT HOLE. REMOVED AND REPLACED AFT SPAR SUPPORT FITTING PER MM.SDR SWAA076467Support Fitting · corrodedDURING SCHEDULED BRIDGE CHECK, FOUND LT WING AFT SPAR SUPPORT FITTING NR 1 MAIN FLAP TRACK CORRODED AT OUTBOARD FLAP TRACK MOUNT HOLE. REMOVED AND REPLACED AFT SPAR SUPPORT FITTING PER MM.
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